Started by upstream project "gplibrary_PR_Models" build number 86
originally caused by:
 GitHub pull request #165 of commit f08d0abb912431f7fa14d583dd199557c0f2e32a, no merge conflicts.
Building remotely on macys in workspace /Users/jenkins/workspace/gplibrary_PR_Models/mosek
Wiping out workspace first.
Cloning the remote Git repository
Cloning repository https://github.com/convexengineering/gplibrary
 > git init /Users/jenkins/workspace/gplibrary_PR_Models/mosek # timeout=10
Fetching upstream changes from https://github.com/convexengineering/gplibrary
 > git --version # timeout=10
 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/*
 > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10
 > git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10
 > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10
Fetching upstream changes from https://github.com/convexengineering/gplibrary
 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master
Merging Revision a7764a21dff699d3c7f74e09f50361a18c36fcff (refs/remotes/origin/pr/165/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='default', fastForwardMode='--ff'}
 > git rev-parse origin/master^{commit} # timeout=10
 > git config core.sparsecheckout # timeout=10
 > git checkout -f origin/master # timeout=3
 > git merge --ff a7764a21dff699d3c7f74e09f50361a18c36fcff # timeout=10
 > git rev-parse HEAD^{commit} # timeout=10
Seen branch in repository origin/1682literate
Seen branch in repository origin/1682master
Seen branch in repository origin/Breakdown
Seen branch in repository origin/SPaircraft
Seen branch in repository origin/aerosurf
Seen branch in repository origin/atmosphere
Seen branch in repository origin/bounds5
Seen branch in repository origin/boxspar
Seen branch in repository origin/breguet_range
Seen branch in repository origin/breguetsetup
Seen branch in repository origin/climb
Seen branch in repository origin/commercial_sizing
Seen branch in repository origin/d8
Seen branch in repository origin/d8fuselage
Seen branch in repository origin/electric_motor
Seen branch in repository origin/fits
Seen branch in repository origin/flightsegments
Seen branch in repository origin/interactive_simpleflight
Seen branch in repository origin/master
Seen branch in repository origin/materials
Seen branch in repository origin/md_template
Seen branch in repository origin/motor
Seen branch in repository origin/ncrit
Seen branch in repository origin/one_element
Seen branch in repository origin/performance
Seen branch in repository origin/pr/10/head
Seen branch in repository origin/pr/100/head
Seen branch in repository origin/pr/103/head
Seen branch in repository origin/pr/105/head
Seen branch in repository origin/pr/105/merge
Seen branch in repository origin/pr/107/head
Seen branch in repository origin/pr/109/head
Seen branch in repository origin/pr/11/head
Seen branch in repository origin/pr/11/merge
Seen branch in repository origin/pr/110/head
Seen branch in repository origin/pr/112/head
Seen branch in repository origin/pr/113/head
Seen branch in repository origin/pr/113/merge
Seen branch in repository origin/pr/114/head
Seen branch in repository origin/pr/115/head
Seen branch in repository origin/pr/115/merge
Seen branch in repository origin/pr/116/head
Seen branch in repository origin/pr/118/head
Seen branch in repository origin/pr/119/head
Seen branch in repository origin/pr/119/merge
Seen branch in repository origin/pr/12/head
Seen branch in repository origin/pr/120/head
Seen branch in repository origin/pr/121/head
Seen branch in repository origin/pr/121/merge
Seen branch in repository origin/pr/122/head
Seen branch in repository origin/pr/123/head
Seen branch in repository origin/pr/124/head
Seen branch in repository origin/pr/125/head
Seen branch in repository origin/pr/127/head
Seen branch in repository origin/pr/128/head
Seen branch in repository origin/pr/129/head
Seen branch in repository origin/pr/13/head
Seen branch in repository origin/pr/13/merge
Seen branch in repository origin/pr/131/head
Seen branch in repository origin/pr/132/head
Seen branch in repository origin/pr/133/head
Seen branch in repository origin/pr/134/head
Seen branch in repository origin/pr/135/head
Seen branch in repository origin/pr/136/head
Seen branch in repository origin/pr/137/head
Seen branch in repository origin/pr/138/head
Seen branch in repository origin/pr/139/head
Seen branch in repository origin/pr/14/head
Seen branch in repository origin/pr/14/merge
Seen branch in repository origin/pr/141/head
Seen branch in repository origin/pr/143/head
Seen branch in repository origin/pr/144/head
Seen branch in repository origin/pr/144/merge
Seen branch in repository origin/pr/145/head
Seen branch in repository origin/pr/145/merge
Seen branch in repository origin/pr/146/head
Seen branch in repository origin/pr/147/head
Seen branch in repository origin/pr/149/head
Seen branch in repository origin/pr/15/head
Seen branch in repository origin/pr/150/head
Seen branch in repository origin/pr/151/head
Seen branch in repository origin/pr/152/head
Seen branch in repository origin/pr/153/head
Seen branch in repository origin/pr/154/head
Seen branch in repository origin/pr/154/merge
Seen branch in repository origin/pr/155/head
Seen branch in repository origin/pr/156/head
Seen branch in repository origin/pr/157/head
Seen branch in repository origin/pr/158/head
Seen branch in repository origin/pr/159/head
Seen branch in repository origin/pr/16/head
Seen branch in repository origin/pr/160/head
Seen branch in repository origin/pr/160/merge
Seen branch in repository origin/pr/161/head
Seen branch in repository origin/pr/162/head
Seen branch in repository origin/pr/163/head
Seen branch in repository origin/pr/165/head
Seen branch in repository origin/pr/165/merge
Seen branch in repository origin/pr/166/head
Seen branch in repository origin/pr/166/merge
Seen branch in repository origin/pr/17/head
Seen branch in repository origin/pr/17/merge
Seen branch in repository origin/pr/19/head
Seen branch in repository origin/pr/19/merge
Seen branch in repository origin/pr/20/head
Seen branch in repository origin/pr/22/head
Seen branch in repository origin/pr/22/merge
Seen branch in repository origin/pr/23/head
Seen branch in repository origin/pr/23/merge
Seen branch in repository origin/pr/24/head
Seen branch in repository origin/pr/25/head
Seen branch in repository origin/pr/26/head
Seen branch in repository origin/pr/26/merge
Seen branch in repository origin/pr/27/head
Seen branch in repository origin/pr/29/head
Seen branch in repository origin/pr/30/head
Seen branch in repository origin/pr/31/head
Seen branch in repository origin/pr/33/head
Seen branch in repository origin/pr/34/head
Seen branch in repository origin/pr/35/head
Seen branch in repository origin/pr/36/head
Seen branch in repository origin/pr/37/head
Seen branch in repository origin/pr/38/head
Seen branch in repository origin/pr/39/head
Seen branch in repository origin/pr/40/head
Seen branch in repository origin/pr/40/merge
Seen branch in repository origin/pr/42/head
Seen branch in repository origin/pr/42/merge
Seen branch in repository origin/pr/43/head
Seen branch in repository origin/pr/44/head
Seen branch in repository origin/pr/44/merge
Seen branch in repository origin/pr/45/head
Seen branch in repository origin/pr/46/head
Seen branch in repository origin/pr/46/merge
Seen branch in repository origin/pr/47/head
Seen branch in repository origin/pr/47/merge
Seen branch in repository origin/pr/5/head
Seen branch in repository origin/pr/54/head
Seen branch in repository origin/pr/54/merge
Seen branch in repository origin/pr/55/head
Seen branch in repository origin/pr/57/head
Seen branch in repository origin/pr/58/head
Seen branch in repository origin/pr/60/head
Seen branch in repository origin/pr/61/head
Seen branch in repository origin/pr/62/head
Seen branch in repository origin/pr/63/head
Seen branch in repository origin/pr/63/merge
Seen branch in repository origin/pr/64/head
Seen branch in repository origin/pr/69/head
Seen branch in repository origin/pr/70/head
Seen branch in repository origin/pr/70/merge
Seen branch in repository origin/pr/71/head
Seen branch in repository origin/pr/72/head
Seen branch in repository origin/pr/72/merge
Seen branch in repository origin/pr/73/head
Seen branch in repository origin/pr/73/merge
Seen branch in repository origin/pr/75/head
Seen branch in repository origin/pr/75/merge
Seen branch in repository origin/pr/77/head
Seen branch in repository origin/pr/77/merge
Seen branch in repository origin/pr/78/head
Seen branch in repository origin/pr/78/merge
Seen branch in repository origin/pr/80/head
Seen branch in repository origin/pr/82/head
Seen branch in repository origin/pr/82/merge
Seen branch in repository origin/pr/83/head
Seen branch in repository origin/pr/83/merge
Seen branch in repository origin/pr/85/head
Seen branch in repository origin/pr/85/merge
Seen branch in repository origin/pr/86/head
Seen branch in repository origin/pr/88/head
Seen branch in repository origin/pr/88/merge
Seen branch in repository origin/pr/89/head
Seen branch in repository origin/pr/89/merge
Seen branch in repository origin/pr/9/head
Seen branch in repository origin/pr/90/head
Seen branch in repository origin/pr/90/merge
Seen branch in repository origin/pr/91/head
Seen branch in repository origin/pr/91/merge
Seen branch in repository origin/pr/92/head
Seen branch in repository origin/pr/92/merge
Seen branch in repository origin/pr/94/head
Seen branch in repository origin/pr/96/head
Seen branch in repository origin/pr/96/merge
Seen branch in repository origin/pr/97/head
Seen branch in repository origin/pr/97/merge
Seen branch in repository origin/pr/98/head
Seen branch in repository origin/pr/99/head
Seen branch in repository origin/qstr
Seen branch in repository origin/quadrotor
Seen branch in repository origin/revert-120-SPaircraft
Seen branch in repository origin/rockets
Seen branch in repository origin/sigeq_paper
Seen branch in repository origin/simple_HT_sizing
Seen branch in repository origin/simple_flight_profile
Seen branch in repository origin/standard_atmosphere
Seen branch in repository origin/sutherland
Seen branch in repository origin/troposphere
Seen branch in repository origin/vectorizeplanform
Seen branch in repository origin/wide_body
Seen branch in repository origin/wvl
Seen 201 remote branches
 > git show-ref --tags -d # timeout=10
Checking out Revision a7764a21dff699d3c7f74e09f50361a18c36fcff (origin/pr/165/merge, origin/master)
 > git config core.sparsecheckout # timeout=10
 > git checkout -f a7764a21dff699d3c7f74e09f50361a18c36fcff # timeout=3
Commit message: "Merge f08d0abb912431f7fa14d583dd199557c0f2e32a into 3a49468fa5aaae9c1d48b1aa4ecd1644c5205fd9"
Using 'Changelog to branch' strategy.
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[description-setter] Description set: <a title="Multiple blade element model" href="https://github.com/convexengineering/gplibrary/pull/165">PR 165</a>: Multiple blade element model
[Execution node] check if [macys] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[mosek] $ /bin/bash -xe /var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/jenkins291911268573687919.sh
+ [[ macys == *macys* ]]
+ export PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
+ PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
+ virtualenv /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit
New python executable in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/python
Installing setuptools, pip, wheel...done.
+ . /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/activate
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ '[' -n /bin/bash ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH
++ '[' -z '' ']'
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ '[' x '!=' x ']'
+++ basename /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit
++ PS1='(venv2_gpkit) '
++ export PS1
++ alias pydoc
++ '[' -n /bin/bash ']'
++ hash -r
++ which pip
+ export PIP=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip
+ PIP=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip
+ python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade pip
Requirement already up-to-date: pip in ./venv2_gpkit/lib/python2.7/site-packages (10.0.1)
+ [[ macys == *reynolds* ]]
+ [[ macys == *macys* ]]
+ [[ mosek == mosek ]]
+ [[ macys == macys ]]
+ export PATH=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin
+ PATH=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin
+ export DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin
+ DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin
+ python /Users/jenkins/mosek/8/tools/platform/osx64x86/python/2/setup.py install
running install
running build
running build_py
running build_ext
copying mosek/_msk.so -> build/lib.macosx-10.13-intel-2.7/mosek
copying mosek/fusion/impl/fragments.so -> build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl
running install_lib
creating /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying build/lib.macosx-10.13-intel-2.7/mosek/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying build/lib.macosx-10.13-intel-2.7/mosek/_msk.so -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
creating /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
creating /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl
copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl
copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl/_implementation.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl
copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl/fragments.so -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl
copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/Utils.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/__init__.py to __init__.pyc
byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/__init__.py to __init__.pyc
byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl/__init__.py to __init__.pyc
byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl/_implementation.py to _implementation.pyc
byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/Utils.py to Utils.pyc
running install_egg_info
Writing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/Mosek-8.1.41-py2.7.egg-info
Fixing library paths
copying /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/
copying /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libcilkrts.5.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/
+ [[ mosek == mosek ]]
+ python -c '__import__("mosek").Env()'
+ msktestlic
Mosek license manager: License path: /Users/jenkins/mosek/mosek.lic
Mosek license manager:  Checkout license feature 'PTS' from flexlm.
Mosek license manager:  Checkout time 0.01. r: 0 status: 0
Problem
  Name                   :                 
  Objective sense        : min             
  Type                   : LO (linear optimization problem)
  Constraints            : 1               
  Cones                  : 0               
  Scalar variables       : 5000            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Presolve started.
Eliminator started.
Freed constraints in eliminator : 0
Eliminator terminated.
Eliminator - tries                  : 1                 time                   : 0.00            
Lin. dep.  - tries                  : 0                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.00    
Optimizer terminated. Time: 0.00    

************************************
A license was checked out correctly.
************************************
+ export 'GPKITSOLVERS=mosek, mosek_cli'
+ GPKITSOLVERS='mosek, mosek_cli'
+ [[ mosek == cvxopt ]]
+ python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade xmlrunner
Collecting xmlrunner
Installing collected packages: xmlrunner
Successfully installed xmlrunner-1.7.7
+ python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade pint
Collecting pint
Installing collected packages: pint
Successfully installed pint-0.8.1
+ python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade numpy
Collecting numpy
  Using cached https://files.pythonhosted.org/packages/55/4d/6fde74ef447202a20e4c1be37475f515d1554d4d677bfe619e408a57c1be/numpy-1.14.2-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl
Installing collected packages: numpy
Successfully installed numpy-1.14.2
+ python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade scipy
Collecting scipy
  Using cached https://files.pythonhosted.org/packages/aa/48/517a82fbbe1746318c19ffb32bb0e9592a0e2fd26adcb1506b383999721f/scipy-1.0.1-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl
Requirement not upgraded as not directly required: numpy>=1.8.2 in ./venv2_gpkit/lib/python2.7/site-packages (from scipy) (1.14.2)
Installing collected packages: scipy
Successfully installed scipy-1.0.1
+ python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade ctypesgen
Collecting ctypesgen
Installing collected packages: ctypesgen
Successfully installed ctypesgen-0.post125
+ python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade pandas
Collecting pandas
  Using cached https://files.pythonhosted.org/packages/82/62/e9058dc7f4d3be74d1111c14bc69a6edb8aeefbd4f6974f151d9d724fe04/pandas-0.22.0-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl
Collecting python-dateutil (from pandas)
  Using cached https://files.pythonhosted.org/packages/0c/57/19f3a65bcf6d5be570ee8c35a5398496e10a0ddcbc95393b2d17f86aaaf8/python_dateutil-2.7.2-py2.py3-none-any.whl
Requirement not upgraded as not directly required: numpy>=1.9.0 in ./venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.2)
Collecting pytz>=2011k (from pandas)
  Using cached https://files.pythonhosted.org/packages/dc/83/15f7833b70d3e067ca91467ca245bae0f6fe56ddc7451aa0dc5606b120f2/pytz-2018.4-py2.py3-none-any.whl
Collecting six>=1.5 (from python-dateutil->pandas)
  Using cached https://files.pythonhosted.org/packages/67/4b/141a581104b1f6397bfa78ac9d43d8ad29a7ca43ea90a2d863fe3056e86a/six-1.11.0-py2.py3-none-any.whl
Installing collected packages: six, python-dateutil, pytz, pandas
Successfully installed pandas-0.22.0 python-dateutil-2.7.2 pytz-2018.4 six-1.11.0
+ python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade matplotlib
Collecting matplotlib
  Using cached https://files.pythonhosted.org/packages/61/38/d70e8bf77d5cb27d5f3595edd0b3978825063feadd023786d2591e393e6e/matplotlib-2.2.2-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl
Collecting kiwisolver>=1.0.1 (from matplotlib)
  Using cached https://files.pythonhosted.org/packages/79/d8/94633718f3f77dcb638687a77ba199325a1cb158d2d4b00c9dc17f2b5c72/kiwisolver-1.0.1-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl
Collecting cycler>=0.10 (from matplotlib)
  Using cached https://files.pythonhosted.org/packages/f7/d2/e07d3ebb2bd7af696440ce7e754c59dd546ffe1bbe732c8ab68b9c834e61/cycler-0.10.0-py2.py3-none-any.whl
Collecting subprocess32 (from matplotlib)
Requirement not upgraded as not directly required: pytz in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2018.4)
Requirement not upgraded as not directly required: six>=1.10 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.11.0)
Collecting backports.functools-lru-cache (from matplotlib)
  Using cached https://files.pythonhosted.org/packages/03/8e/2424c0e65c4a066e28f539364deee49b6451f8fcd4f718fefa50cc3dcf48/backports.functools_lru_cache-1.5-py2.py3-none-any.whl
Requirement not upgraded as not directly required: numpy>=1.7.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.14.2)
Collecting pyparsing!=2.0.4,!=2.1.2,!=2.1.6,>=2.0.1 (from matplotlib)
  Using cached https://files.pythonhosted.org/packages/6a/8a/718fd7d3458f9fab8e67186b00abdd345b639976bc7fb3ae722e1b026a50/pyparsing-2.2.0-py2.py3-none-any.whl
Requirement not upgraded as not directly required: python-dateutil>=2.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2.7.2)
Requirement not upgraded as not directly required: setuptools in ./venv2_gpkit/lib/python2.7/site-packages (from kiwisolver>=1.0.1->matplotlib) (39.0.1)
Installing collected packages: kiwisolver, cycler, subprocess32, backports.functools-lru-cache, pyparsing, matplotlib
Successfully installed backports.functools-lru-cache-1.5 cycler-0.10.0 kiwisolver-1.0.1 matplotlib-2.2.2 pyparsing-2.2.0 subprocess32-3.2.7
+ export GPKITBUILD=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/build_gpkit
+ GPKITBUILD=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/build_gpkit
+ python -c 'import scipy; print scipy.__version__'
1.0.1
+ python -c 'import numpy; print numpy.__version__'
1.14.2
+ python -c 'import pint; print pint.__version__'
0.8.1
+ git clone --depth 1 https://github.com/convexengineering/gpkit.git
Cloning into 'gpkit'...
+ python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit
Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit
Requirement already satisfied: numpy>=1.12.1 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.7.0.0) (1.14.2)
Requirement already satisfied: pint>=0.7 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.7.0.0) (0.8.1)
Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.7.0.0) (1.0.1)
Collecting ad (from gpkit==0.7.0.0)
  Downloading https://files.pythonhosted.org/packages/3b/f0/16776411190d53745d0d020a242e2890a59c0752b133a3476d35aa63e4a2/ad-1.3.2.zip
Installing collected packages: ad, gpkit
  Running setup.py install for ad: started
    Running setup.py install for ad: finished with status 'done'
  Running setup.py develop for gpkit
Successfully installed ad-1.3.2 gpkit
+ python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_PR_Models/mosek
Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/mosek
Requirement already satisfied: numpy>=1.12 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.8.1)
Installing collected packages: gpkitmodels
  Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels
+ cat /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/env/settings
installed_solvers : mosek, mosek_cli
mosek_bin_dir : /Users/jenkins/mosek/8/tools/platform/osx64x86/bin

+ ls /Users/jenkins/workspace/gplibrary_PR_Models/mosek/build_gpkit
expopt.so
+ export MSK_IPAR_NUM_THREADS=2
+ MSK_IPAR_NUM_THREADS=2
+ export MKL_NUM_THREADS=2
+ MKL_NUM_THREADS=2
+ export NUMEXPR_NUM_THREADS=2
+ NUMEXPR_NUM_THREADS=2
+ export OMP_NUM_THREADS=2
+ OMP_NUM_THREADS=2
+ python -c 'from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)'
Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/mosek
Installing collected packages: gpkitmodels
  Found existing installation: gpkitmodels 0.0.0.0
    Uninstalling gpkitmodels-0.0.0.0:
      Successfully uninstalled gpkitmodels-0.0.0.0
  Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels
Cloning into 'shopping'...

Running tests...
----------------------------------------------------------------------
...
----------------------------------------------------------------------
Ran 3 tests in 0.230s

OK

Generating XML reports...
adding test for 'test.py'
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0116 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0103 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.0348 seconds.
Cloning into 'gassolar'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0)
Collecting git+https://github.com/hoburg/gpfit.git
  Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-OmPQPP
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-lLeg5G/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
Installing collected packages: gpfit
Successfully installed gpfit-0.1
Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gassolar
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.7.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2018.4)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0)
Building wheels for collected packages: gassolar
  Running setup.py bdist_wheel for gassolar: started
  Running setup.py bdist_wheel for gassolar: finished with status 'done'
  Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-06qcpm/wheels/62/18/d3/616f96cc7315a5d96e00418a41713828819a211a1260f4c2f6
Successfully built gassolar
Installing collected packages: gassolar
Successfully installed gassolar-0.0.0.0

Running tests...
----------------------------------------------------------------------
../Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
..
----------------------------------------------------------------------
Ran 4 tests in 21.793s

OK

Generating XML reports...
adding test for 'gassolar/gas/gas.py'
adding test for 'gassolar/solar/solar.py'
Using solver 'mosek'
Solving for 592 variables.
Solving took 0.0537 seconds.
Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Beginning signomial solve.
Solving took 4 GP solves and 0.531 seconds.
Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Using solver 'mosek'
Solving for 592 variables.
Solving took 0.0572 seconds.
Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Beginning signomial solve.
Solving took 4 GP solves and 0.551 seconds.
Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Using solver 'mosek'
Solving for 1250 variables.
Solving took 0.21 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1529 but bound is 150000.0000
Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.1347 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 1.63 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0522 but bound is 150000.0000
Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.9089 but bound is 150000.0000
Using solver 'mosek_cli'
Solving for 1250 variables.
Solving took 0.266 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.0147 but bound is 150000.0000
Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.3302 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 2.88 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134552.5355 but bound is 150000.0000
Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.8810 but bound is 150000.0000
Cloning into 'jho'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0)
Collecting git+https://github.com/hoburg/gpfit.git
  Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-xHUmIA
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-lXcd0g/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit

Running tests...
----------------------------------------------------------------------
....
----------------------------------------------------------------------
Ran 4 tests in 27.998s

OK

Generating XML reports...
adding test for 'model/jho.py'
adding test for 'model/print_perf.py'
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.015015738437436e-14.
Allowing negative dual variable(s) as small as -7.79740855216815e-14.
Allowing negative dual variable(s) as small as -2.308023997615871e-12.
Allowing negative dual variable(s) as small as -1.297437634759091e-13.
Solving took 4 GP solves and 1.45 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.015015738437436e-14.
Allowing negative dual variable(s) as small as -7.79740855216815e-14.
Allowing negative dual variable(s) as small as -2.308023997615871e-12.
Allowing negative dual variable(s) as small as -1.297437634759091e-13.
Solving took 4 GP solves and 1.64 seconds.
Allowing negative dual variable(s) as small as -5.83851543500824e-13.
Allowing negative dual variable(s) as small as -3.4046550301258804e-13.
Allowing negative dual variable(s) as small as -1.0241512499176153e-12.
Allowing negative dual variable(s) as small as -1.0239153275248825e-12.
Allowing negative dual variable(s) as small as -2.7765468960452844e-13.
Allowing negative dual variable(s) as small as -1.1531824486207126e-12.
Allowing negative dual variable(s) as small as -1.117775360118256e-12.
Allowing negative dual variable(s) as small as -1.1157938993328759e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.2101656482466083e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.145445974957401e-11.
Allowing negative dual variable(s) as small as -1.4546894177382983e-12.
Allowing negative dual variable(s) as small as -6.463011491635323e-12.
Allowing negative dual variable(s) as small as -6.468955737738273e-12.
Solving took 4 GP solves and 1.47 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.02 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.83851543500824e-13.
Allowing negative dual variable(s) as small as -3.4046550301258804e-13.
Allowing negative dual variable(s) as small as -1.0241512499176153e-12.
Allowing negative dual variable(s) as small as -1.0239153275248825e-12.
Allowing negative dual variable(s) as small as -2.7765468960452844e-13.
Allowing negative dual variable(s) as small as -1.1531824486207126e-12.
Allowing negative dual variable(s) as small as -1.117775360118256e-12.
Allowing negative dual variable(s) as small as -1.1157938993328759e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.2101656482466083e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.145445974957401e-11.
Allowing negative dual variable(s) as small as -1.4546894177382983e-12.
Allowing negative dual variable(s) as small as -6.463011491635323e-12.
Allowing negative dual variable(s) as small as -6.468955737738273e-12.
Solving took 4 GP solves and 1.42 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.27 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Cloning into 'turbofan'...
Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/turbofan
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.8.1)
Building wheels for collected packages: turbofan
  Running setup.py bdist_wheel for turbofan: started
  Running setup.py bdist_wheel for turbofan: finished with status 'done'
  Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-lPPTdW/wheels/5a/d9/61/61e35684062bfcf52c1d9781b80aeffbe3c3604f4de326b4d2
Successfully built turbofan
Installing collected packages: turbofan
Successfully installed turbofan-0.0.0.0

Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 1.102s

OK

Generating XML reports...
adding test for 'turbofan/engine_validation.py'
Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528317 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%)

Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485057 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%)

Cloning into 'SPaircraft'...
Collecting git+https://github.com/hoburg/turbofan.git
  Cloning https://github.com/hoburg/turbofan.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-vC4P_z
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.8.1)
Building wheels for collected packages: turbofan
  Running setup.py bdist_wheel for turbofan: started
  Running setup.py bdist_wheel for turbofan: finished with status 'done'
  Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-11KAde/wheels/49/e6/3a/5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5
Successfully built turbofan

Running tests...
----------------------------------------------------------------------
adding test for 'SP_aircraft.py'
Solving over 9 passes.
Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2519605.42574 force_pound * meter but the right hand side evaluated to 2468463.56985 force_pound * meter (Allowable error: 0.1%, Actual error: 2.1%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.5694486 force_pound but the right hand side evaluated to 32399.9999985 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116797 meter but the right hand side evaluated to 1.96396120849 meter (Allowable error: 0.1%, Actual error: 11%)

Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) [N]...] is not tight because the left hand side evaluated to 48608.9319484 newton but the right hand side evaluated to 48529.7510812 newton (Allowable error: 0.1%, Actual error: 0.16%)

Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) [N]...] is not tight because the left hand side evaluated to 49704.3762642 newton but the right hand side evaluated to 49411.0961982 newton (Allowable error: 0.1%, Actual error: 0.59%)

Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) [N]...] is not tight because the left hand side evaluated to 18949.0851002 newton but the right hand side evaluated to 18923.0868505 newton (Allowable error: 0.1%, Actual error: 0.14%)

Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(4, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(4, 0) [N]...] is not tight because the left hand side evaluated to 16591.9845547 newton but the right hand side evaluated to 16565.7840788 newton (Allowable error: 0.1%, Actual error: 0.16%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1002807.59585 joule / kilogram but the right hand side evaluated to 1.15239018522 megajoule / kilogram (Allowable error: 0.1%, Actual error: 7.1%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 895037.788007 joule / kilogram but the right hand side evaluated to 0.897466920342 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.13%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1072947.09808 joule / kilogram but the right hand side evaluated to 1.19569715055 megajoule / kilogram (Allowable error: 0.1%, Actual error: 5.6%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 596870.328654 joule / kilogram but the right hand side evaluated to 0.615556916263 megajoule / kilogram (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 786921.973197 joule / kilogram but the right hand side evaluated to 0.790360758381 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.22%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.3465537267 meter but the right hand side evaluated to 16.3967763464 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 11.085407105454614 but the right hand side evaluated to 4.680786125345706 (Allowable error: 0.1%, Actual error: 58%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.791743267028139 but the right hand side evaluated to 4.6807861213361495 (Allowable error: 0.1%, Actual error: 52%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.229124608162419 but the right hand side evaluated to 4.68078612660884 (Allowable error: 0.1%, Actual error: 43%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4249260653 meter but the right hand side evaluated to 18.165984758 meter (Allowable error: 0.1%, Actual error: 1.4%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4249260653 meter but the right hand side evaluated to 18.2854539141 meter (Allowable error: 0.1%, Actual error: 0.76%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3101211943345108 but the right hand side evaluated to 0.1929269522419905 (Allowable error: 0.1%, Actual error: 2.5%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.24134425443932273 but the right hand side evaluated to 0.17650174128637633 (Allowable error: 0.1%, Actual error: 1.4%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.2750340326703 but the right hand side evaluated to 4.6159830063373 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.453663691950036 but the right hand side evaluated to 4.646340160191905 (Allowable error: 0.1%, Actual error: 38%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2504977.92996 force_pound * meter but the right hand side evaluated to 2454471.04284 force_pound * meter (Allowable error: 0.1%, Actual error: 2.1%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4784956 force_pound but the right hand side evaluated to 32399.9999983 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116785 meter but the right hand side evaluated to 1.96383095925 meter (Allowable error: 0.1%, Actual error: 11%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 982256.725725 joule / kilogram but the right hand side evaluated to 1.20547009438 megajoule / kilogram (Allowable error: 0.1%, Actual error: 10%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1151137.26793 joule / kilogram but the right hand side evaluated to 1.88379329658 megajoule / kilogram (Allowable error: 0.1%, Actual error: 25%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4111622782 meter but the right hand side evaluated to 16.4524814604 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 11.089309994629579 but the right hand side evaluated to 4.731320782719332 (Allowable error: 0.1%, Actual error: 57%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.749133323810398 but the right hand side evaluated to 4.731320773888456 (Allowable error: 0.1%, Actual error: 51%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.19783376011938 but the right hand side evaluated to 4.731320785813131 (Allowable error: 0.1%, Actual error: 42%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4749969046 meter but the right hand side evaluated to 18.2223420087 meter (Allowable error: 0.1%, Actual error: 1.4%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4749969046 meter but the right hand side evaluated to 18.3384468009 meter (Allowable error: 0.1%, Actual error: 0.74%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.30927817177907624 but the right hand side evaluated to 0.19273723801703138 (Allowable error: 0.1%, Actual error: 2.5%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.24172887227172968 but the right hand side evaluated to 0.17659971719802256 (Allowable error: 0.1%, Actual error: 1.4%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.430222316685087 but the right hand side evaluated to 4.666980393866118 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.495476936542261 but the right hand side evaluated to 4.696716351444317 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2481462.90961 force_pound * meter but the right hand side evaluated to 2426090.4509 force_pound * meter (Allowable error: 0.1%, Actual error: 2.3%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.2914541 force_pound but the right hand side evaluated to 32399.9999964 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116708 meter but the right hand side evaluated to 1.83120395513 meter (Allowable error: 0.1%, Actual error: 17%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1203378.02307 joule / kilogram but the right hand side evaluated to 1.66379767201 megajoule / kilogram (Allowable error: 0.1%, Actual error: 17%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4693761029 meter but the right hand side evaluated to 16.6431977458 meter (Allowable error: 0.1%, Actual error: 11%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 11.047304624262775 but the right hand side evaluated to 4.801802854383902 (Allowable error: 0.1%, Actual error: 57%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.67070488118125 but the right hand side evaluated to 4.801802833918823 (Allowable error: 0.1%, Actual error: 50%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.221371545668486 but the right hand side evaluated to 4.801802860093242 (Allowable error: 0.1%, Actual error: 42%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.6280035734 meter but the right hand side evaluated to 18.3449848697 meter (Allowable error: 0.1%, Actual error: 1.5%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.6280035734 meter but the right hand side evaluated to 18.4743985847 meter (Allowable error: 0.1%, Actual error: 0.82%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.32683342981649144 but the right hand side evaluated to 0.19660324036000026 (Allowable error: 0.1%, Actual error: 2.8%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2527501332422961 but the right hand side evaluated to 0.17938924062999267 (Allowable error: 0.1%, Actual error: 1.5%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.455615366207265 but the right hand side evaluated to 4.729216558041436 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.548873889072465 but the right hand side evaluated to 4.762578563421205 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2455571.78 force_pound * meter but the right hand side evaluated to 2407713.43641 force_pound * meter (Allowable error: 0.1%, Actual error: 2%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.3827342 force_pound but the right hand side evaluated to 32399.9999923 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116651 meter but the right hand side evaluated to 1.99551861649 meter (Allowable error: 0.1%, Actual error: 9.9%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1227633.79562 joule / kilogram but the right hand side evaluated to 1.72359452722 megajoule / kilogram (Allowable error: 0.1%, Actual error: 18%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 677538.123532 joule / kilogram but the right hand side evaluated to 0.679181192317 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.11%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4156411721 meter but the right hand side evaluated to 16.4239811728 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.974966459382099 but the right hand side evaluated to 4.762553603366843 (Allowable error: 0.1%, Actual error: 57%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.752891334834139 but the right hand side evaluated to 4.762553560750228 (Allowable error: 0.1%, Actual error: 51%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.15871708630364 but the right hand side evaluated to 4.762553615749261 (Allowable error: 0.1%, Actual error: 42%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4488810125 meter but the right hand side evaluated to 18.2046710439 meter (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4488810125 meter but the right hand side evaluated to 18.3176359046 meter (Allowable error: 0.1%, Actual error: 0.71%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3059470678699041 but the right hand side evaluated to 0.19198948973923569 (Allowable error: 0.1%, Actual error: 2.4%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23933780407159055 but the right hand side evaluated to 0.17598662398681225 (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.504817928878604 but the right hand side evaluated to 4.699782404256913 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.527661581251126 but the right hand side evaluated to 4.728945813116001 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2436789.79574 force_pound * meter but the right hand side evaluated to 2390897.93309 force_pound * meter (Allowable error: 0.1%, Actual error: 1.9%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.3045315 force_pound but the right hand side evaluated to 32399.9999987 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116781 meter but the right hand side evaluated to 2.03199484871 meter (Allowable error: 0.1%, Actual error: 8.3%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1233971.49451 joule / kilogram but the right hand side evaluated to 1.62320665168 megajoule / kilogram (Allowable error: 0.1%, Actual error: 15%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4095813573 meter but the right hand side evaluated to 16.3813704555 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.93104306470805 but the right hand side evaluated to 4.787725249164657 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.87336258618397 but the right hand side evaluated to 4.787725237216685 (Allowable error: 0.1%, Actual error: 52%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.154651983212306 but the right hand side evaluated to 4.787725252089411 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4102861096 meter but the right hand side evaluated to 18.1746934334 meter (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4102861096 meter but the right hand side evaluated to 18.2839529544 meter (Allowable error: 0.1%, Actual error: 0.69%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3021007156917337 but the right hand side evaluated to 0.19112068244169325 (Allowable error: 0.1%, Actual error: 2.3%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2368489981371864 but the right hand side evaluated to 0.17534269724576 (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.53648087231217 but the right hand side evaluated to 4.726728502324815 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.551412933049222 but the right hand side evaluated to 4.755143842266746 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2418323.74682 force_pound * meter but the right hand side evaluated to 2374882.83896 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4857763 force_pound but the right hand side evaluated to 32399.9999985 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116785 meter but the right hand side evaluated to 2.08235544751 meter (Allowable error: 0.1%, Actual error: 6%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1244506.52759 joule / kilogram but the right hand side evaluated to 1.55926547761 megajoule / kilogram (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 664750.028026 joule / kilogram but the right hand side evaluated to 0.667401363964 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.18%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4000470113 meter but the right hand side evaluated to 16.3223774638 meter (Allowable error: 0.1%, Actual error: 13%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.904037784794486 but the right hand side evaluated to 4.789502341054556 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.025977028879563 but the right hand side evaluated to 4.789502330545116 (Allowable error: 0.1%, Actual error: 52%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.145555668651518 but the right hand side evaluated to 4.789502343665673 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.3617986888 meter but the right hand side evaluated to 18.1374295856 meter (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3617986888 meter but the right hand side evaluated to 18.2416886261 meter (Allowable error: 0.1%, Actual error: 0.65%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.29596125700054543 but the right hand side evaluated to 0.18972182821747074 (Allowable error: 0.1%, Actual error: 2.2%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23297699496494229 but the right hand side evaluated to 0.1743351864753014 (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.565345085134277 but the right hand side evaluated to 4.731317049831014 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.583815760845391 but the right hand side evaluated to 4.75851398937749 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2405736.49288 force_pound * meter but the right hand side evaluated to 2358168.34222 force_pound * meter (Allowable error: 0.1%, Actual error: 2%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4755431 force_pound but the right hand side evaluated to 32399.9999987 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116803 meter but the right hand side evaluated to 1.97491276363 meter (Allowable error: 0.1%, Actual error: 11%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1245747.48287 joule / kilogram but the right hand side evaluated to 1.35773206791 megajoule / kilogram (Allowable error: 0.1%, Actual error: 4.7%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4441332172 meter but the right hand side evaluated to 16.4749746381 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.933106363922247 but the right hand side evaluated to 4.831717141926778 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.19213927812854 but the right hand side evaluated to 4.831717132670499 (Allowable error: 0.1%, Actual error: 53%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.195655302003852 but the right hand side evaluated to 4.831717144082085 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4861277387 meter but the right hand side evaluated to 18.2368480851 meter (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4861277387 meter but the right hand side evaluated to 18.3518593506 meter (Allowable error: 0.1%, Actual error: 0.73%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.31020212005842485 but the right hand side evaluated to 0.19294179971694433 (Allowable error: 0.1%, Actual error: 2.5%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.24191742878583433 but the right hand side evaluated to 0.17664743357231227 (Allowable error: 0.1%, Actual error: 1.4%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.542128431098089 but the right hand side evaluated to 4.7669778872448685 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.597025912250877 but the right hand side evaluated to 4.797040985718126 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2391780.61733 force_pound * meter but the right hand side evaluated to 2346059.52804 force_pound * meter (Allowable error: 0.1%, Actual error: 1.9%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4560694 force_pound but the right hand side evaluated to 32399.999998 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116792 meter but the right hand side evaluated to 2.01208173003 meter (Allowable error: 0.1%, Actual error: 9.2%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1263254.5804 joule / kilogram but the right hand side evaluated to 1.32933808934 megajoule / kilogram (Allowable error: 0.1%, Actual error: 2.8%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 643003.182889 joule / kilogram but the right hand side evaluated to 0.644587786543 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.11%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4391891716 meter but the right hand side evaluated to 16.4333025757 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.92705825676323 but the right hand side evaluated to 4.827096972645318 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.332847861194049 but the right hand side evaluated to 4.827096843291057 (Allowable error: 0.1%, Actual error: 53%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.188196185801203 but the right hand side evaluated to 4.82709688161273 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4531707658 meter but the right hand side evaluated to 18.2123808519 meter (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4531707658 meter but the right hand side evaluated to 18.3237323749 meter (Allowable error: 0.1%, Actual error: 0.7%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3054476676812694 but the right hand side evaluated to 0.19187591944839252 (Allowable error: 0.1%, Actual error: 2.4%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23885888073596728 but the right hand side evaluated to 0.17586214887743853 (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.554289296298087 but the right hand side evaluated to 4.764562145015105 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruc.
----------------------------------------------------------------------
Ran 1 test in 77.980s

OK

Generating XML reports...
t**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.61783370644863 but the right hand side evaluated to 4.79369294649962 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2376291.45227 force_pound * meter but the right hand side evaluated to 2334601.79239 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.2995963 force_pound but the right hand side evaluated to 32399.999993 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116652 meter but the right hand side evaluated to 2.09816858196 meter (Allowable error: 0.1%, Actual error: 5.3%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1283646.09578 joule / kilogram but the right hand side evaluated to 1.28937951091 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.25%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4146080744 meter but the right hand side evaluated to 16.3183521457 meter (Allowable error: 0.1%, Actual error: 13%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.937461473951318 but the right hand side evaluated to 4.8243798977520544 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.57132916673029 but the right hand side evaluated to 4.824379817151666 (Allowable error: 0.1%, Actual error: 54%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.193849678782172 but the right hand side evaluated to 4.82437991732318 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.3565689555 meter but the right hand side evaluated to 18.1377648781 meter (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3565689555 meter but the right hand side evaluated to 18.2402000203 meter (Allowable error: 0.1%, Actual error: 0.63%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.294174218474355 but the right hand side evaluated to 0.18931132678407792 (Allowable error: 0.1%, Actual error: 2.2%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23164829833081413 but the right hand side evaluated to 0.17398683913627952 (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.6200778878048245 but the right hand side evaluated to 4.767021260056057 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.689407107165492 but the right hand side evaluated to 4.793943568509399 (Allowable error: 0.1%, Actual error: 38%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission

Sweeping took 74.9 seconds.
Cloning into 'solar'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0)
Collecting git+https://github.com/convexengineering/gpfit.git
  Cloning https://github.com/convexengineering/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-JBOcCJ
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-ZkTxFp/wheels/d5/94/ac/b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
Collecting git+https://github.com/convexengineering/gassolar.git
  Cloning https://github.com/convexengineering/gassolar.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-eRcgmd
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.7.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2018.4)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0)
Building wheels for collected packages: gassolar
  Running setup.py bdist_wheel for gassolar: started
  Running setup.py bdist_wheel for gassolar: finished with status 'done'
  Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-Ub4tDO/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/solar
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in /Users/jenkins/workspace/gplibrary_PR_Models/mosek (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2.7.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2018.4)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.11.0)
Building wheels for collected packages: solar
  Running setup.py bdist_wheel for solar: started
  Running setup.py bdist_wheel for solar: finished with status 'done'
  Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-vk02f3/wheels/1f/1c/61/aec93436439dcd4a965e159a026d3a7ed265e591b64e6d6bfc
Successfully built solar
Installing collected packages: solar
Successfully installed solar-0.0.0.0

Running tests...
----------------------------------------------------------------------
/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
  tau = np.exp(-0.175/costhsun)
adding test for 'solar/solar.py'
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
Using solver 'mosek'
Solving for 9118 variables.
Solving took 1.59 seconds.
Allowing negative dual variable(s) as small as -5.637461551016999e-11.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2782 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 867386.8412 but bound is 600000.0000
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500
Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 60.5767236173 ampere but the right hand side evaluated to 573.501894545 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.87%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 60.5526061732 ampere but the right hand side evaluated to 573.573306404 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.81%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 60.517240906 ampere but the right hand side evaluated to 573.639284144 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.74%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 60.4636210941 ampere but the right hand side evaluated to 573.740530562 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.64%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 60.3827402599 ampere but the right hand side evaluated to 573.915474021 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.47%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 52.7191575278 volt but the right hand side evaluated to 52.2547688559 volt (Allowable error: 0.0001%, Actual error: 0.89%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 52.63362609 volt but the right hand side evaluated to 52.1977309528 volt (Allowable error: 0.0001%, Actual error: 0.84%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 52.5116980439 volt but the right hand side evaluated to 52.1139034235 volt (Allowable error: 0.0001%, Actual error: 0.76%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 52.3220338784 volt but the right hand side evaluated to 51.9820120324 volt (Allowable error: 0.0001%, Actual error: 0.65%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 52.0211456741 volt but the right hand side evaluated to 51.7700751378 volt (Allowable error: 0.0001%, Actual error: 0.48%)

Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 51.1761794325 ampere but the right hand side evaluated to 488.624349908 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 36.7374730327 volt but the right hand side evaluated to 36.7317996097 volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1593767198 ampere but the right hand side evaluated to 488.477338043 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7101513819 volt but the right hand side evaluated to 36.7055364295 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1753645561 ampere but the right hand side evaluated to 488.617202515 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7361512925 volt but the right hand side evaluated to 36.73052782 volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1605707683 ampere but the right hand side evaluated to 488.487785438 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7120926095 volt but the right hand side evaluated to 36.7074024894 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1741339094 ampere but the right hand side evaluated to 488.606424254 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7341522215 volt but the right hand side evaluated to 36.7286054332 volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1613468438 ampere but the right hand side evaluated to 488.49458291 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7133529137 volt but the right hand side evaluated to 36.7086144984 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1724887448 ampere but the right hand side evaluated to 488.592044265 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7314740822 volt but the right hand side evaluated to 36.7260320582 volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1617041951 ampere but the right hand side evaluated to 488.49772228 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7139314092 volt but the right hand side evaluated to 36.7091714952 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.170422177 ampere but the right hand side evaluated to 488.573968728 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7281125056 volt but the right hand side evaluated to 36.7228011141 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 51.1616360977 ampere but the right hand side evaluated to 488.497105067 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 36.7138249173 volt but the right hand side evaluated to 36.709067609 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1679308491 ampere but the right hand side evaluated to 488.552162638 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7240631835 volt but the right hand side evaluated to 36.718908054 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.16114906 ampere but the right hand side evaluated to 488.49284471 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7130328759 volt but the right hand side evaluated to 36.7083063087 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1650169855 ampere but the right hand side evaluated to 488.526682567 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7193224479 volt but the right hand side evaluated to 36.7143519786 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1602390099 ampere but the right hand side evaluated to 488.484892469 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7115513225 volt but the right hand side evaluated to 36.7068828557 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.161672196 ampere but the right hand side evaluated to 488.497422743 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7138832403 volt but the right hand side evaluated to 36.7091238033 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1588991829 ampere but the right hand side evaluated to 488.473160986 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7093748052 volt but the right hand side evaluated to 36.7047900063 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1578932244 ampere but the right hand side evaluated to 488.464361595 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7077389227 volt but the right hand side evaluated to 36.7032176272 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1571316816 ampere but the right hand side evaluated to 488.457706409 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.706499358 volt but the right hand side evaluated to 36.7020266251 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1536750164 ampere but the right hand side evaluated to 488.427454046 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7008816805 volt but the right hand side evaluated to 36.6966258736 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [A]... >= 9.55*i0_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1549284235 ampere but the right hand side evaluated to 488.438428758 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [v_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [V]... >= Kv_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7029176149 volt but the right hand side evaluated to 36.6985835483 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [A]... >= 9.55*i0_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1490147289 ampere but the right hand side evaluated to 488.386693548 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.01%)

Warning: Constraint [v_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [V]... >= Kv_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6933033464 volt but the right hand side evaluated to 36.689341979 volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [i_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1522856916 ampere but the right hand side evaluated to 488.415301297 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [v_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6986225703 volt but the right hand side evaluated to 36.6944544511 volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [i_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1439021657 ampere but the right hand side evaluated to 488.341962748 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0095%)

Warning: Constraint [v_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.684993091 volt but the right hand side evaluated to 36.6813535269 volt (Allowable error: 0.0001%, Actual error: 0.0099%)

Warning: Constraint [i_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1491995177 ampere but the right hand side evaluated to 488.388297324 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.01%)

Warning: Constraint [v_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.693606267 volt but the right hand side evaluated to 36.689632247 volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [i_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1383326015 ampere but the right hand side evaluated to 488.293234905 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%)

Warning: Constraint [v_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6759405976 volt but the right hand side evaluated to 36.6726516264 volt (Allowable error: 0.0001%, Actual error: 0.009%)

Warning: Constraint [i_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1456637519 ampere but the right hand side evaluated to 488.357360237 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0098%)

Warning: Constraint [v_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6878593274 volt but the right hand side evaluated to 36.6841077143 volt (Allowable error: 0.0001%, Actual error: 0.01%)

Warning: Constraint [i_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1322964427 ampere but the right hand side evaluated to 488.240411138 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0076%)

Warning: Constraint [v_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6661333491 volt but the right hand side evaluated to 36.6632231692 volt (Allowable error: 0.0001%, Actual error: 0.0079%)

Warning: Constraint [i_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1416719694 ampere but the right hand side evaluated to 488.32243399 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0091%)

Warning: Constraint [v_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6813714612 volt but the right hand side evaluated to 36.6778709671 volt (Allowable error: 0.0001%, Actual error: 0.0095%)

Warning: Constraint [i_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1257872089 ampere but the right hand side evaluated to 488.183446846 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0065%)

Warning: Constraint [v_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6555587396 volt but the right hand side evaluated to 36.6530568844 volt (Allowable error: 0.0001%, Actual error: 0.0068%)

Warning: Constraint [i_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1372166053 ampere but the right hand side evaluated to 488.28344908 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0084%)

Warning: Constraint [v_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6741311247 volt but the right hand side evaluated to 36.6709106623 volt (Allowable error: 0.0001%, Actual error: 0.0088%)

Warning: Constraint [i_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1187952098 ampere but the right hand side evaluated to 488.122251849 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0054%)

Warning: Constraint [v_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6442023308 volt but the right hand side evaluated to 36.6421384938 volt (Allowable error: 0.0001%, Actual error: 0.0056%)

Warning: Constraint [i_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.132290073 ampere but the right hand side evaluated to 488.240340888 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0076%)

Warning: Constraint [v_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6661258534 volt but the right hand side evaluated to 36.6632149335 volt (Allowable error: 0.0001%, Actual error: 0.0079%)

Warning: Constraint [i_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1113158725 ampere but the right hand side evaluated to 488.056821651 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0042%)

Warning: Constraint [v_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6320499433 volt but the right hand side evaluated to 36.6304568661 volt (Allowable error: 0.0001%, Actual error: 0.0043%)

Warning: Constraint [i_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1268848638 ampere but the right hand side evaluated to 488.1930511 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0067%)

Warning: Constraint [v_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6573421755 volt but the right hand side evaluated to 36.654771342 volt (Allowable error: 0.0001%, Actual error: 0.007%)

Warning: Constraint [i_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1033294947 ampere but the right hand side evaluated to 487.986919797 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0029%)

Warning: Constraint [v_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6190825453 volt but the right hand side evaluated to 36.6179891463 volt (Allowable error: 0.0001%, Actual error: 0.003%)

Warning: Constraint [i_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1209870628 ampere but the right hand side evaluated to 488.141426525 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0057%)

Warning: Constraint [v_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6477639126 volt but the right hand side evaluated to 36.6455620932 volt (Allowable error: 0.0001%, Actual error: 0.006%)

Warning: Constraint [i_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.0948288086 ampere but the right hand side evaluated to 487.912510981 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0015%)

Warning: Constraint [v_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6052830876 volt but the right hand side evaluated to 36.6047209301 volt (Allowable error: 0.0001%, Actual error: 0.0015%)

Warning: Constraint [i_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1145929261 ampere but the right hand side evaluated to 488.085481501 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0047%)

Warning: Constraint [v_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6373759063 volt but the right hand side evaluated to 36.6355759391 volt (Allowable error: 0.0001%, Actual error: 0.0049%)

Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500
Using solver 'mosek'
Solving for 9118 variables.
Solving took 1.23 seconds.
Allowing negative dual variable(s) as small as -2.313440721590491e-09.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2362 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 996075.4701 but bound is 600000.0000
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500
Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.4798616871 ampere but the right hand side evaluated to 615.823395675 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.5%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.4269127364 ampere but the right hand side evaluated to 615.859202474 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.3537333659 ampere but the right hand side evaluated to 615.885775157 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.2456906087 ampere but the right hand side evaluated to 615.959108991 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.0888352278 ampere but the right hand side evaluated to 616.178367729 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.87%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.6834494748 volt but the right hand side evaluated to 60.7350325814 volt (Allowable error: 0.0001%, Actual error: 1.6%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.5680978571 volt but the right hand side evaluated to 60.6741449399 volt (Allowable error: 0.0001%, Actual error: 1.5%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.403171487 volt but the right hand side evaluated to 60.5822248617 volt (Allowable error: 0.0001%, Actual error: 1.4%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.1439843961 volt but the right hand side evaluated to 60.4342120569 volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 60.7249433363 volt but the right hand side evaluated to 60.1877256234 volt (Allowable error: 0.0001%, Actual error: 0.89%)

Warning: Constraint [i_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [A]... >= 9.55*i0_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.6299754066 ampere but the right hand side evaluated to 530.630584974 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [V]... >= Kv_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6648736993 volt but the right hand side evaluated to 43.613851537 volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [i_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [A]... >= 9.55*i0_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.6243884554 ampere but the right hand side evaluated to 530.618911306 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [V]... >= Kv_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6483041578 volt but the right hand side evaluated to 43.600854668 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [A]... >= 9.55*i0_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5948643794 ampere but the right hand side evaluated to 530.318096321 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [V]... >= Kv_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6045512376 volt but the right hand side evaluated to 43.5555115701 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [A]... >= 9.55*i0_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5877072087 ampere but the right hand side evaluated to 530.261822004 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [V]... >= Kv_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.590897874 volt but the right hand side evaluated to 43.5428971027 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [A]... >= 9.55*i0_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5601201048 ampere but the right hand side evaluated to 530.01450216 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [V]... >= Kv_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.5438558952 volt but the right hand side evaluated to 43.4972568249 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [A]... >= 9.55*i0_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5647544258 ampere but the right hand side evaluated to 530.130697953 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.089%)

Warning: Constraint [v_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [V]... >= Kv_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.5380173524 volt but the right hand side evaluated to 43.4975646379 volt (Allowable error: 0.0001%, Actual error: 0.093%)

Warning: Constraint [i_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [A]... >= 9.55*i0_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5290030681 ampere but the right hand side evaluated to 529.772839355 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.093%)

Warning: Constraint [v_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [V]... >= Kv_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4839513395 volt but the right hand side evaluated to 43.4421185843 volt (Allowable error: 0.0001%, Actual error: 0.096%)

Warning: Constraint [i_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [A]... >= 9.55*i0_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5246672489 ampere but the right hand side evaluated to 529.724504082 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.094%)

Warning: Constraint [v_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [V]... >= Kv_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4783029815 volt but the right hand side evaluated to 43.4358813765 volt (Allowable error: 0.0001%, Actual error: 0.098%)

Warning: Constraint [i_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [A]... >= 9.55*i0_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4902108071 ampere but the right hand side evaluated to 529.409774432 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.091%)

Warning: Constraint [v_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [V]... >= Kv_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4206769046 volt but the right hand side evaluated to 43.3795027734 volt (Allowable error: 0.0001%, Actual error: 0.095%)

Warning: Constraint [i_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [A]... >= 9.55*i0_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4897590772 ampere but the right hand side evaluated to 529.405661954 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.091%)

Warning: Constraint [v_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [V]... >= Kv_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4199186847 volt but the right hand side evaluated to 43.3787620594 volt (Allowable error: 0.0001%, Actual error: 0.095%)

Warning: Constraint [i_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [A]... >= 9.55*i0_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4542367411 ampere but the right hand side evaluated to 529.095767663 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.086%)

Warning: Constraint [v_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [V]... >= Kv_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.357843237 volt but the right hand side evaluated to 43.3192140578 volt (Allowable error: 0.0001%, Actual error: 0.089%)

Warning: Constraint [i_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [A]... >= 9.55*i0_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4561813378 ampere but the right hand side evaluated to 529.111760873 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.086%)

Warning: Constraint [v_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [V]... >= Kv_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.3614185611 volt but the right hand side evaluated to 43.3225682458 volt (Allowable error: 0.0001%, Actual error: 0.09%)

Warning: Constraint [i_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [A]... >= 9.55*i0_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4177323953 ampere but the right hand side evaluated to 528.776676561 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.08%)

Warning: Constraint [v_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [V]... >= Kv_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2942101429 volt but the right hand side evaluated to 43.2581210109 volt (Allowable error: 0.0001%, Actual error: 0.083%)

Warning: Constraint [i_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [A]... >= 9.55*i0_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4222562631 ampere but the right hand side evaluated to 528.815779271 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.081%)

Warning: Constraint [v_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [V]... >= Kv_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.3021765533 volt but the right hand side evaluated to 43.2657352122 volt (Allowable error: 0.0001%, Actual error: 0.084%)

Warning: Constraint [i_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [A]... >= 9.55*i0_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3807635124 ampere but the right hand side evaluated to 528.4536646 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.074%)

Warning: Constraint [v_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [V]... >= Kv_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2297646482 volt but the right hand side evaluated to 43.1962561859 volt (Allowable error: 0.0001%, Actual error: 0.078%)

Warning: Constraint [i_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [A]... >= 9.55*i0_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.387753025 ampere but the right hand side evaluated to 528.514053914 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%)

Warning: Constraint [v_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [V]... >= Kv_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2420726449 volt but the right hand side evaluated to 43.2080185375 volt (Allowable error: 0.0001%, Actual error: 0.079%)

Warning: Constraint [i_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [A]... >= 9.55*i0_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3433025753 ampere but the right hand side evaluated to 528.126447186 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.069%)

Warning: Constraint [v_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [V]... >= Kv_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1644690894 volt but the right hand side evaluated to 43.1335799071 volt (Allowable error: 0.0001%, Actual error: 0.072%)

Warning: Constraint [i_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [A]... >= 9.55*i0_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3528999313 ampere but the right hand side evaluated to 528.21045122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.07%)

Warning: Constraint [v_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [V]... >= Kv_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1811655499 volt but the right hand side evaluated to 43.1496203198 volt (Allowable error: 0.0001%, Actual error: 0.073%)

Warning: Constraint [i_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [A]... >= 9.55*i0_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3052417482 ampere but the right hand side evaluated to 527.793480995 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%)

Warning: Constraint [v_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [V]... >= Kv_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0982622581 volt but the right hand side evaluated to 43.0699871692 volt (Allowable error: 0.0001%, Actual error: 0.066%)

Warning: Constraint [i_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [A]... >= 9.55*i0_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3172781621 ampere but the right hand side evaluated to 527.898341597 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.065%)

Warning: Constraint [v_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [V]... >= Kv_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1192776784 volt but the right hand side evaluated to 43.0901391272 volt (Allowable error: 0.0001%, Actual error: 0.068%)

Warning: Constraint [i_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [A]... >= 9.55*i0_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2666576938 ampere but the right hand side evaluated to 527.456149506 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.057%)

Warning: Constraint [v_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [V]... >= Kv_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0311361301 volt but the right hand side evaluated to 43.005525189 volt (Allowable error: 0.0001%, Actual error: 0.06%)

Warning: Constraint [i_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [A]... >= 9.55*i0_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2812116297 ampere but the right hand side evaluated to 527.58314398 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.059%)

Warning: Constraint [v_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [V]... >= Kv_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0564982282 volt but the right hand side evaluated to 43.0298618093 volt (Allowable error: 0.0001%, Actual error: 0.062%)

Warning: Constraint [i_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [A]... >= 9.55*i0_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2275040059 ampere but the right hand side evaluated to 527.113884165 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%)

Warning: Constraint [v_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [V]... >= Kv_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9630434152 volt but the right hand side evaluated to 42.9401358395 volt (Allowable error: 0.0001%, Actual error: 0.053%)

Warning: Constraint [i_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [A]... >= 9.55*i0_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2445672777 ampere but the right hand side evaluated to 527.26286091 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.054%)

Warning: Constraint [v_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [V]... >= Kv_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9927480607 volt but the right hand side evaluated to 42.9686472793 volt (Allowable error: 0.0001%, Actual error: 0.056%)

Warning: Constraint [i_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [A]... >= 9.55*i0_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1877043502 ampere but the right hand side evaluated to 526.765635923 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.045%)

Warning: Constraint [v_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [V]... >= Kv_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8939244497 volt but the right hand side evaluated to 42.8737321349 volt (Allowable error: 0.0001%, Actual error: 0.047%)

Warning: Constraint [i_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [A]... >= 9.55*i0_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2073068961 ampere but the right hand side evaluated to 526.937050485 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.048%)

Warning: Constraint [v_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [V]... >= Kv_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9279827556 volt but the right hand side evaluated to 42.9064444163 volt (Allowable error: 0.0001%, Actual error: 0.05%)

Warning: Constraint [i_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [A]... >= 9.55*i0_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1473269875 ampere but the right hand side evaluated to 526.412698419 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.039%)

Warning: Constraint [v_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [V]... >= Kv_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8237683768 volt but the right hand side evaluated to 42.8063574607 volt (Allowable error: 0.0001%, Actual error: 0.041%)

Warning: Constraint [i_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [A]... >= 9.55*i0_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1695237616 ampere but the right hand side evaluated to 526.607399134 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.042%)

Warning: Constraint [v_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [V]... >= Kv_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8622018079 volt but the right hand side evaluated to 42.8433200008 volt (Allowable error: 0.0001%, Actual error: 0.044%)

Warning: Constraint [i_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [A]... >= 9.55*i0_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.106269551 ampere but the right hand side evaluated to 526.053626704 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.033%)

Warning: Constraint [v_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [V]... >= Kv_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7525051 volt but the right hand side evaluated to 42.7379018937 volt (Allowable error: 0.0001%, Actual error: 0.034%)

Warning: Constraint [i_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [A]... >= 9.55*i0_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1308974109 ampere but the right hand side evaluated to 526.268936037 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.037%)

Warning: Constraint [v_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [V]... >= Kv_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7952623182 volt but the right hand side evaluated to 42.7789690368 volt (Allowable error: 0.0001%, Actual error: 0.038%)

Warning: Constraint [i_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [A]... >= 9.55*i0_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0645199336 ampere but the right hand side evaluated to 525.688432109 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [v_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [V]... >= Kv_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.6800925823 volt but the right hand side evaluated to 42.6683339542 volt (Allowable error: 0.0001%, Actual error: 0.028%)

Warning: Constraint [i_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [A]... >= 9.55*i0_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0916891515 ampere but the right hand side evaluated to 525.926062112 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.031%)

Warning: Constraint [v_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [V]... >= Kv_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7272164064 volt but the right hand side evaluated to 42.7136049383 volt (Allowable error: 0.0001%, Actual error: 0.032%)

Warning: Constraint [i_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [A]... >= 9.55*i0_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0220519828 ampere but the right hand side evaluated to 525.316909027 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.02%)

Warning: Constraint [v_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [V]... >= Kv_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.6064822992 volt but the right hand side evaluated to 42.5976086322 volt (Allowable error: 0.0001%, Actual error: 0.021%)

Warning: Constraint [i_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [A]... >= 9.55*i0_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0517602051 ampere but the right hand side evaluated to 525.576757236 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.025%)

Warning: Constraint [v_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [V]... >= Kv_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.6579808133 volt but the right hand side evaluated to 42.6470853671 volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [i_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [A]... >= 9.55*i0_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9788216225 ampere but the right hand side evaluated to 524.938577691 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [V]... >= Kv_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5316186195 volt but the right hand side evaluated to 42.525665095 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [i_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [A]... >= 9.55*i0_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0110852706 ampere but the right hand side evaluated to 525.220825947 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.018%)

Warning: Constraint [v_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [V]... >= Kv_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5875067004 volt but the right hand side evaluated to 42.5793651841 volt (Allowable error: 0.0001%, Actual error: 0.019%)

Warning: Constraint [i_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [A]... >= 9.55*i0_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9347937916 ampere but the right hand side evaluated to 524.553114112 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0068%)

Warning: Constraint [v_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [V]... >= Kv_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.4554469838 volt but the right hand side evaluated to 42.4524494601 volt (Allowable error: 0.0001%, Actual error: 0.0071%)

Warning: Constraint [i_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [A]... >= 9.55*i0_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9696398387 ampere but the right hand side evaluated to 524.858110522 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [V]... >= Kv_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5157446186 volt but the right hand side evaluated to 42.5104011591 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500
Using solver 'mosek'
Solving for 9118 variables.
Solving took 1.14 seconds.
Allowing negative dual variable(s) as small as -4.902708824484024e-12.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1906 but bound is 0.9465
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 1169782.8867 but bound is 600000.0000
Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2395 but bound is 0.1460
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0362 but bound is 0.0500
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/TailAero.165_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/TailAe could cause inaccurate result because it is above upper bound. Solution is 1085313.8694 but bound is 1000000.0000
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0401 but bound is 0.0500
Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.516711783 ampere but the right hand side evaluated to 674.453825774 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.4533675492 ampere but the right hand side evaluated to 674.320429229 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.365428588 ampere but the right hand side evaluated to 674.109664895 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%)

Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.2343817031 ampere but the right hand side evaluated to 673.811668214 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.95%)

Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.0402156578 ampere but the right hand side evaluated to 673.429963687 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.74%)

Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.8210040886 volt but the right hand side evaluated to 71.9034674852 volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.7202466878 volt but the right hand side evaluated to 71.8535082341 volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.5731317208 volt but the right hand side evaluated to 71.7742699747 volt (Allowable error: 0.0001%, Actual error: 1.1%)

Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.3413332824 volt but the right hand side evaluated to 71.6454702767 volt (Allowable error: 0.0001%, Actual error: 0.97%)

Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.9658463329 volt but the right hand side evaluated to 71.4292573885 volt (Allowable error: 0.0001%, Actual error: 0.75%)

Warning: Constraint [i_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [A]... >= 9.55*i0_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6889846374 ampere but the right hand side evaluated to 578.391971061 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [v_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [V]... >= Kv_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.1934064478 volt but the right hand side evaluated to 52.0866165181 volt (Allowable error: 0.0001%, Actual error: 0.21%)

Warning: Constraint [i_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [A]... >= 9.55*i0_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.685756983 ampere but the right hand side evaluated to 578.360231772 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [v_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [V]... >= Kv_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.1879081645 volt but the right hand side evaluated to 52.0810382722 volt (Allowable error: 0.0001%, Actual error: 0.21%)

Warning: Constraint [i_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [A]... >= 9.55*i0_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6182208355 ampere but the right hand side evaluated to 577.774787213 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [v_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [V]... >= Kv_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.0615462972 volt but the right hand side evaluated to 51.9603362224 volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [i_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [A]... >= 9.55*i0_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6168508358 ampere but the right hand side evaluated to 577.756984887 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [v_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [V]... >= Kv_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.0598387691 volt but the right hand side evaluated to 51.958191197 volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [i_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [A]... >= 9.55*i0_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.5475602182 ampere but the right hand side evaluated to 577.161371188 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [v_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [V]... >= Kv_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.9295281804 volt but the right hand side evaluated to 51.8341441239 volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [i_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [A]... >= 9.55*i0_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.5481451111 ampere but the right hand side evaluated to 577.159342867 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [v_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [V]... >= Kv_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.9316531546 volt but the right hand side evaluated to 51.8355595979 volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [i_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [A]... >= 9.55*i0_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4760446616 ampere but the right hand side evaluated to 576.535460479 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [v_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [V]... >= Kv_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.7967254514 volt but the right hand side evaluated to 51.7067528497 volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [i_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [A]... >= 9.55*i0_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4788110195 ampere but the right hand side evaluated to 576.553267838 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [v_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [V]... >= Kv_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.8028031287 volt but the right hand side evaluated to 51.7120261024 volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [i_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [A]... >= 9.55*i0_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4038853517 ampere but the right hand side evaluated to 575.901050237 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [v_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [V]... >= Kv_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.6632192539 volt but the right hand side evaluated to 51.5784281444 volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [i_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [A]... >= 9.55*i0_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.409253763 ampere but the right hand side evaluated to 575.946041575 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [v_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [V]... >= Kv_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.6734756892 volt but the right hand side evaluated to 51.588094614 volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [i_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [A]... >= 9.55*i0_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.3321487495 ampere but the right hand side evaluated to 575.276881617 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [v_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [V]... >= Kv_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.5295891592 volt but the right hand side evaluated to 51.4505423193 volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [i_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [A]... >= 9.55*i0_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.3391805218 ampere but the right hand side evaluated to 575.332962642 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [v_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [V]... >= Kv_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.5434553558 volt but the right hand side evaluated to 51.4633729217 volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [i_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [A]... >= 9.55*i0_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.2596415905 ampere but the right hand side evaluated to 574.642763879 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [V]... >= Kv_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.3950926708 volt but the right hand side evaluated to 51.3215376188 volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [i_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [A]... >= 9.55*i0_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.2689755628 ampere but the right hand side evaluated to 574.72097375 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [V]... >= Kv_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.4129165466 volt but the right hand side evaluated to 51.3383383367 volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [i_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [A]... >= 9.55*i0_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.1864854308 ampere but the right hand side evaluated to 574.00110751 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [v_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [V]... >= Kv_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.259745152 volt but the right hand side evaluated to 51.1915455364 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [A]... >= 9.55*i0_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.1982205014 ampere but the right hand side evaluated to 574.10323849 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [v_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [V]... >= Kv_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.2815726648 volt but the right hand side evaluated to 51.212441015 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [A]... >= 9.55*i0_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.113178096 ampere but the right hand side evaluated to 573.36082799 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [v_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [V]... >= Kv_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.123781353 volt but the right hand side evaluated to 51.0611850544 volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [i_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [A]... >= 9.55*i0_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.1267614283 ampere but the right hand side evaluated to 573.477423136 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [v_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [V]... >= Kv_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 51.1492801536 volt but the right hand side evaluated to 51.0854577235 volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [i_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [A]... >= 9.55*i0_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.039229174 ampere but the right hand side evaluated to 572.713878305 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [V]... >= Kv_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 50.9868713367 volt but the right hand side evaluated to 50.9298152435 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [A]... >= 9.55*i0_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.0550449147 ampere but the right hand side evaluated to 572.851574997 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [V]... >= Kv_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 51.0162477388 volt but the right hand side evaluated to 50.9579461432 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [A]... >= 9.55*i0_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.9647093302 ampere but the right hand side evaluated to 572.061824373 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%)

Warning: Constraint [v_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [V]... >= Kv_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.8489984781 volt but the right hand side evaluated to 50.7975015303 volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [i_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [A]... >= 9.55*i0_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.982558415 ampere but the right hand side evaluated to 572.217249482 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [V]... >= Kv_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.8821312775 volt but the right hand side evaluated to 50.829234395 volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [i_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [A]... >= 9.55*i0_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8895321465 ampere but the right hand side evaluated to 571.403566674 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%)

Warning: Constraint [v_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [V]... >= Kv_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.7100597456 volt but the right hand side evaluated to 50.6641153928 volt (Allowable error: 0.0001%, Actual error: 0.091%)

Warning: Constraint [i_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [A]... >= 9.55*i0_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.9096032511 ampere but the right hand side evaluated to 571.579967583 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.09%)

Warning: Constraint [v_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [V]... >= Kv_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.7470444742 volt but the right hand side evaluated to 50.6996794879 volt (Allowable error: 0.0001%, Actual error: 0.093%)

Warning: Constraint [i_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [A]... >= 9.55*i0_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8135055106 ampere but the right hand side evaluated to 570.736238917 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%)

Warning: Constraint [v_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [V]... >= Kv_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.5698982625 volt but the right hand side evaluated to 50.52940501 volt (Allowable error: 0.0001%, Actual error: 0.08%)

Warning: Constraint [i_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [A]... >= 9.55*i0_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8359147349 ampere but the right hand side evaluated to 570.935581279 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.08%)

Warning: Constraint [v_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [V]... >= Kv_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.6107858866 volt but the right hand side evaluated to 50.5689304772 volt (Allowable error: 0.0001%, Actual error: 0.083%)

Warning: Constraint [i_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [A]... >= 9.55*i0_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.7373851659 ampere but the right hand side evaluated to 570.073103962 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%)

Warning: Constraint [v_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [V]... >= Kv_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.4288604416 volt but the right hand side evaluated to 50.3942714198 volt (Allowable error: 0.0001%, Actual error: 0.069%)

Warning: Constraint [i_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [A]... >= 9.55*i0_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.7615030091 ampere but the right hand side evaluated to 570.284665688 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.069%)

Warning: Constraint [v_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [V]... >= Kv_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.473306981 volt but the right hand side evaluated to 50.4369825451 volt (Allowable error: 0.0001%, Actual error: 0.072%)

Warning: Constraint [i_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [A]... >= 9.55*i0_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6601940849 ampere but the right hand side evaluated to 569.397913981 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%)

Warning: Constraint [v_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [V]... >= Kv_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.2863566964 volt but the right hand side evaluated to 50.2574894234 volt (Allowable error: 0.0001%, Actual error: 0.057%)

Warning: Constraint [i_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [A]... >= 9.55*i0_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6862643468 ampere but the right hand side evaluated to 569.625847965 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.059%)

Warning: Constraint [v_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [V]... >= Kv_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.334492284 volt but the right hand side evaluated to 50.3036848468 volt (Allowable error: 0.0001%, Actual error: 0.061%)

Warning: Constraint [i_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [A]... >= 9.55*i0_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5817571296 ampere but the right hand side evaluated to 568.708160444 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.045%)

Warning: Constraint [v_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [V]... >= Kv_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.1422411663 volt but the right hand side evaluated to 50.118837034 volt (Allowable error: 0.0001%, Actual error: 0.047%)

Warning: Constraint [i_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [A]... >= 9.55*i0_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6101818669 ampere but the right hand side evaluated to 568.959250548 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.049%)

Warning: Constraint [v_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [V]... >= Kv_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.1942716336 volt but the right hand side evaluated to 50.1689929493 volt (Allowable error: 0.0001%, Actual error: 0.05%)

Warning: Constraint [i_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [A]... >= 9.55*i0_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5030863453 ampere but the right hand side evaluated to 568.021415349 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.034%)

Warning: Constraint [v_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [V]... >= Kv_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.9969712139 volt but the right hand side evaluated to 49.9794948168 volt (Allowable error: 0.0001%, Actual error: 0.035%)

Warning: Constraint [i_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [A]... >= 9.55*i0_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5332879177 ampere but the right hand side evaluated to 568.285849996 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%)

Warning: Constraint [v_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [V]... >= Kv_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.0525990752 volt but the right hand side evaluated to 50.0329215855 volt (Allowable error: 0.0001%, Actual error: 0.039%)

Warning: Constraint [i_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [A]... >= 9.55*i0_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.423247458 ampere but the right hand side evaluated to 567.322309329 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.023%)

Warning: Constraint [v_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [V]... >= Kv_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.8499962943 volt but the right hand side evaluated to 49.8383217168 volt (Allowable error: 0.0001%, Actual error: 0.023%)

Warning: Constraint [i_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [A]... >= 9.55*i0_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.4555188553 ampere but the right hand side evaluated to 567.605001647 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%)

Warning: Constraint [v_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [V]... >= Kv_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.9093743422 volt but the right hand side evaluated to 49.8953665197 volt (Allowable error: 0.0001%, Actual error: 0.028%)

Warning: Constraint [i_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [A]... >= 9.55*i0_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.3423837098 ampere but the right hand side evaluated to 566.613736031 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [v_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [V]... >= Kv_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.7013199694 volt but the right hand side evaluated to 49.6954604524 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [A]... >= 9.55*i0_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.3767252172 ampere but the right hand side evaluated to 566.914629066 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.016%)

Warning: Constraint [v_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [V]... >= Kv_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.7644510763 volt but the right hand side evaluated to 49.7561215774 volt (Allowable error: 0.0001%, Actual error: 0.017%)

Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2395 but bound is 0.1460
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0362 but bound is 0.0500
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0401 but bound is 0.0500
Warning: Constraint [i_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [A]... >= 9.55*i0_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.2969028431 ampere but the right hand side evaluated to 566.215173677 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.005%)

Warning: Constraint [v_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [V]... >= Kv_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.6177509155 volt but the right hand side evaluated to 49.6151517911 volt (Allowable error: 0.0001%, Actual error: 0.0052%)

Using solver 'mosek'
Solving for 4738 variables.
Solving took 0.648 seconds.
Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1350804.7178 but bound is 600000.0000
Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/TailAero.246_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Tail could cause inaccurate result because it is above upper bound. Solution is 1008642.5207 but bound is 1000000.0000
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/TailAero.247_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Tail could cause inaccurate result because it is above upper bound. Solution is 1292032.4332 but bound is 1000000.0000
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.4850831652 ampere but the right hand side evaluated to 734.385479936 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%)

Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.4269319843 ampere but the right hand side evaluated to 734.137719607 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%)

Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.3444447521 ampere but the right hand side evaluated to 733.758465059 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%)

Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.2198444304 ampere but the right hand side evaluated to 733.184380824 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%)

Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.0308211154 ampere but the right hand side evaluated to 732.323549193 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%)

Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 85.0572231972 volt but the right hand side evaluated to 84.4091397813 volt (Allowable error: 0.0001%, Actual error: 0.77%)

Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.9750002042 volt but the right hand side evaluated to 84.3626540077 volt (Allowable error: 0.0001%, Actual error: 0.73%)

Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.8508479081 volt but the right hand side evaluated to 84.2860523858 volt (Allowable error: 0.0001%, Actual error: 0.67%)

Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.6551119176 volt but the right hand side evaluated to 84.1621014005 volt (Allowable error: 0.0001%, Actual error: 0.59%)

Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.3395955732 volt but the right hand side evaluated to 83.9568516261 volt (Allowable error: 0.0001%, Actual error: 0.46%)

Warning: Constraint [i_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [A]... >= 9.55*i0_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.6960931732 ampere but the right hand side evaluated to 625.927938569 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%)

Warning: Constraint [v_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [V]... >= Kv_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 61.275847558 volt but the right hand side evaluated to 61.1323942912 volt (Allowable error: 0.0001%, Actual error: 0.23%)

Warning: Constraint [i_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [A]... >= 9.55*i0_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.6049268827 ampere but the right hand side evaluated to 625.132235268 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [v_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [V]... >= Kv_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 61.0975968447 volt but the right hand side evaluated to 60.9618640561 volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [i_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [A]... >= 9.55*i0_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.5138546039 ampere but the right hand side evaluated to 624.339975894 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [v_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [V]... >= Kv_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.9194879258 volt but the right hand side evaluated to 60.7917117953 volt (Allowable error: 0.0001%, Actual error: 0.21%)

Warning: Constraint [i_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [A]... >= 9.55*i0_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.4219089099 ampere but the right hand side evaluated to 623.532130448 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [v_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [V]... >= Kv_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.7402727238 volt but the right hand side evaluated to 60.6197087949 volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [i_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [A]... >= 9.55*i0_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.3296763367 ampere but the right hand side evaluated to 622.720980228 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [v_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [V]... >= Kv_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.5606085314 volt but the right hand side evaluated to 60.4471824667 volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [i_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [A]... >= 9.55*i0_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.2372264952 ampere but the right hand side evaluated to 621.908688637 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [v_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [V]... >= Kv_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.3805760091 volt but the right hand side evaluated to 60.2743632221 volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [i_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [A]... >= 9.55*i0_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.1449525723 ampere but the right hand side evaluated to 621.102905139 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [v_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [V]... >= Kv_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.2004381111 volt but the right hand side evaluated to 60.1019020923 volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [i_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [A]... >= 9.55*i0_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.0520391234 ampere but the right hand side evaluated to 620.288821137 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [v_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [V]... >= Kv_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.0193678571 volt but the right hand side evaluated to 59.9282708434 volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [i_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [A]... >= 9.55*i0_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.9589067965 ampere but the right hand side evaluated to 619.474985094 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [V]... >= Kv_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.8377275755 volt but the right hand side evaluated to 59.7542833236 volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [i_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [A]... >= 9.55*i0_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.8644114982 ampere but the right hand side evaluated to 618.640133176 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [v_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [V]... >= Kv_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.6543268873 volt but the right hand side evaluated to 59.5777207233 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [A]... >= 9.55*i0_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.7703802198 ampere but the right hand side evaluated to 617.819686965 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [V]... >= Kv_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.4709269147 volt but the right hand side evaluated to 59.4021310591 volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [i_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [A]... >= 9.55*i0_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.6755632625 ampere but the right hand side evaluated to 616.990456595 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [V]... >= Kv_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.2862436518 volt but the right hand side evaluated to 59.2251105997 volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [i_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [A]... >= 9.55*i0_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.5798172048 ampere but the right hand side evaluated to 616.150186449 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%)

Warning: Constraint [v_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [V]... >= Kv_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.1000568606 volt but the right hand side evaluated to 59.0463515886 volt (Allowable error: 0.0001%, Actual error: 0.091%)

Warning: Constraint [i_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [A]... >= 9.55*i0_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.4835800653 ampere but the right hand side evaluated to 615.307908589 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%)

Warning: Constraint [v_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [V]... >= Kv_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.9127539782 volt but the right hand side evaluated to 58.8667215584 volt (Allowable error: 0.0001%, Actual error: 0.078%)

Warning: Constraint [i_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [A]... >= 9.55*i0_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.3863993082 ampere but the right hand side evaluated to 614.455768497 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%)

Warning: Constraint [v_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [V]... >= Kv_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.7238588027 volt but the right hand side evaluated to 58.6853940248 volt (Allowable error: 0.0001%, Actual error: 0.066%)

Warning: Constraint [i_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [A]... >= 9.55*i0_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.2883257876 ampere but the right hand side evaluated to 613.59536851 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%)

Warning: Constraint [v_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [V]... >= Kv_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.5333570681 volt but the right hand side evaluated to 58.5024648612 volt (Allowable error: 0.0001%, Actual error: 0.053%)

Warning: Constraint [i_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [A]... >= 9.55*i0_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.1894287943 ampere but the right hand side evaluated to 612.728584716 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.03.8%)

Warning: Constraint [v_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [V]... >= Kv_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.34122998 volt but the right hand side evaluated to 58.3180344411 volt (Allowable error: 0.0001%, Actual error: 0.04%)

Warning: Constraint [i_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [A]... >= 9.55*i0_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.0894710108 ampere but the right hand side evaluated to 611.851750501 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [v_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [V]... >= Kv_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.1472124301 volt but the right hand side evaluated to 58.1316988809 volt (Allowable error: 0.0001%, Actual error: 0.027%)

Warning: Constraint [i_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [A]... >= 9.55*i0_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 63.9884701057 ampere but the right hand side evaluated to 610.965859479 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [V]... >= Kv_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 57.9512410147 volt but the right hand side evaluated to 57.9434753394 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Using solver 'mosek'
Solving for 9118 variables.
Solving took 1.37 seconds.
Allowing negative dual variable(s) as small as -9.958825169247902e-10.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2782 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 867386.9541 but bound is 600000.0000
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500
Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 60.5767159569 ampere but the right hand side evaluated to 573.501973395 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.87%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 60.5525996925 ampere but the right hand side evaluated to 573.573367396 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.81%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 60.5172357864 ampere but the right hand side evaluated to 573.639323153 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.74%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 60.463617621 ampere but the right hand side evaluated to 573.740540838 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.64%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 60.3827385293 ampere but the right hand side evaluated to 573.915453073 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.47%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 52.7191397853 volt but the right hand side evaluated to 52.25476536 volt (Allowable error: 0.0001%, Actual error: 0.89%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 52.6336128485 volt but the right hand side evaluated to 52.1977292193 volt (Allowable error: 0.0001%, Actual error: 0.84%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 52.5116902531 volt but the right hand side evaluated to 52.1139038525 volt (Allowable error: 0.0001%, Actual error: 0.76%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 52.3220330666 volt but the right hand side evaluated to 51.9820152705 volt (Allowable error: 0.0001%, Actual error: 0.65%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 52.0211523575 volt but the right hand side evaluated to 51.7700813953 volt (Allowable error: 0.0001%, Actual error: 0.48%)

Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 51.1761810965 ampere but the right hand side evaluated to 488.62436091 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 36.7374808976 volt but the right hand side evaluated to 36.7318070999 volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1593789239 ampere but the right hand side evaluated to 488.477354867 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7101589736 volt but the right hand side evaluated to 36.7055436981 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1753666071 ampere but the right hand side evaluated to 488.617218523 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7361590825 volt but the right hand side evaluated to 36.7305353385 volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1605729106 ampere but the right hand side evaluated to 488.487801375 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7121001982 volt but the right hand side evaluated to 36.7074097319 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1741361971 ampere but the right hand side evaluated to 488.606443885 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7341600577 volt but the right hand side evaluated to 36.7286131052 volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1613489867 ampere but the right hand side evaluated to 488.49459893 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7133605109 volt but the right hand side evaluated to 36.7086217559 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1724906555 ampere but the right hand side evaluated to 488.59205819 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.73148186 volt but the right hand side evaluated to 36.7260395061 volt (Allowable error: 0.0001%, Actual error: 0.015%)

Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1617061802 ampere but the right hand side evaluated to 488.497736144 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7139390081 volt but the right hand side evaluated to 36.7091787049 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1704236613 ampere but the right hand side evaluated to 488.573975817 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7281201561 volt but the right hand side evaluated to 36.7228082169 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 51.1616381196 ampere but the right hand side evaluated to 488.497119506 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 36.7138325249 volt but the right hand side evaluated to 36.7090748449 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1679327659 ampere but the right hand side evaluated to 488.552176086 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7240708737 volt but the right hand side evaluated to 36.7189153714 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1611512182 ampere but the right hand side evaluated to 488.49286097 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7130404684 volt but the right hand side evaluated to 36.7083135708 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1650189037 ampere but the right hand side evaluated to 488.526695964 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7193301293 volt but the right hand side evaluated to 36.7143592819 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1602411783 ampere but the right hand side evaluated to 488.484908753 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7115589005 volt but the right hand side evaluated to 36.706890098 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1616741802 ampere but the right hand side evaluated to 488.497436645 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.713890854 volt but the right hand side evaluated to 36.7091310292 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.158901373 ampere but the right hand side evaluated to 488.473177468 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7093823712 volt but the right hand side evaluated to 36.7047972356 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.157895299 ampere but the right hand side evaluated to 488.464376489 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7077464859 volt but the right hand side evaluated to 36.7032248115 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1571339135 ampere but the right hand side evaluated to 488.457723312 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7065069026 volt but the right hand side evaluated to 36.7020338337 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1536775117 ampere but the right hand side evaluated to 488.427474477 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7008891767 volt but the right hand side evaluated to 36.6966331108 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [A]... >= 9.55*i0_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1549306356 ampere but the right hand side evaluated to 488.438445015 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [v_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [V]... >= Kv_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.70292511 volt but the right hand side evaluated to 36.6985906696 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [A]... >= 9.55*i0_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1490172694 ampere but the right hand side evaluated to 488.386714306 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.01%)

Warning: Constraint [v_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [V]... >= Kv_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6933107931 volt but the right hand side evaluated to 36.6893491593 volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [i_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1522882216 ampere but the right hand side evaluated to 488.415321683 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [v_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6986300237 volt but the right hand side evaluated to 36.6944616111 volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [i_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1439051041 ampere but the right hand side evaluated to 488.341988419 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0095%)

Warning: Constraint [v_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.685000426 volt but the right hand side evaluated to 36.6813606845 volt (Allowable error: 0.0001%, Actual error: 0.0099%)

Warning: Constraint [i_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1492021993 ampere but the right hand side evaluated to 488.388319586 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.01%)

Warning: Constraint [v_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6936136933 volt but the right hand side evaluated to 36.6896394136 volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [i_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1383356345 ampere but the right hand side evaluated to 488.293261121 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%)

Warning: Constraint [v_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6759478303 volt but the right hand side evaluated to 36.6726586513 volt (Allowable error: 0.0001%, Actual error: 0.009%)

Warning: Constraint [i_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1456667651 ampere but the right hand side evaluated to 488.357386391 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0098%)

Warning: Constraint [v_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6878666481 volt but the right hand side evaluated to 36.6841148324 volt (Allowable error: 0.0001%, Actual error: 0.01%)

Warning: Constraint [i_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1322994927 ampere but the right hand side evaluated to 488.240436833 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0076%)

Warning: Constraint [v_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6661404892 volt but the right hand side evaluated to 36.6632300478 volt (Allowable error: 0.0001%, Actual error: 0.0079%)

Warning: Constraint [i_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1416748505 ampere but the right hand side evaluated to 488.322457741 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0091%)

Warning: Constraint [v_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6813787014 volt but the right hand side evaluated to 36.6778779148 volt (Allowable error: 0.0001%, Actual error: 0.0095%)

Warning: Constraint [i_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1257903099 ampere but the right hand side evaluated to 488.183472082 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0065%)

Warning: Constraint [v_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6555657035 volt but the right hand side evaluated to 36.6530635159 volt (Allowable error: 0.0001%, Actual error: 0.0068%)

Warning: Constraint [i_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1372195892 ampere but the right hand side evaluated to 488.283473938 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0084%)

Warning: Constraint [v_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6741383081 volt but the right hand side evaluated to 36.6709175631 volt (Allowable error: 0.0001%, Actual error: 0.0088%)

Warning: Constraint [i_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1187983389 ampere but the right hand side evaluated to 488.122276621 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0054%)

Warning: Constraint [v_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6442091397 volt but the right hand side evaluated to 36.6421449162 volt (Allowable error: 0.0001%, Actual error: 0.0056%)

Warning: Constraint [i_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1322930823 ampere but the right hand side evaluated to 488.240365636 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0076%)

Warning: Constraint [v_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6661329567 volt but the right hand side evaluated to 36.6632217262 volt (Allowable error: 0.0001%, Actual error: 0.0079%)

Warning: Constraint [i_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1113196911 ampere but the right hand side evaluated to 488.056856319 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0042%)

Warning: Constraint [v_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6320567561 volt but the right hand side evaluated to 36.6304635547 volt (Allowable error: 0.0001%, Actual error: 0.0043%)

Warning: Constraint [i_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1268883357 ampere but the right hand side evaluated to 488.193082217 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0067%)

Warning: Constraint [v_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.657349249 volt but the right hand side evaluated to 36.6547782593 volt (Allowable error: 0.0001%, Actual error: 0.007%)

Warning: Constraint [i_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1033334437 ampere but the right hand side evaluated to 487.986955698 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0029%)

Warning: Constraint [v_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6190892664 volt but the right hand side evaluated to 36.6179957411 volt (Allowable error: 0.0001%, Actual error: 0.003%)

Warning: Constraint [i_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1209903658 ampere but the right hand side evaluated to 488.141454234 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0057%)

Warning: Constraint [v_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6477708226 volt but the right hand side evaluated to 36.6455687065 volt (Allowable error: 0.0001%, Actual error: 0.006%)

Warning: Constraint [i_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.0948329724 ampere but the right hand side evaluated to 487.912548965 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0015%)

Warning: Constraint [v_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6052896752 volt but the right hand side evaluated to 36.6047273948 volt (Allowable error: 0.0001%, Actual error: 0.0015%)

Warning: Constraint [i_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1145965804 ampere but the right hand side evaluated to 488.085513962 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0047%)

Warning: Constraint [v_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6373827756 volt but the right hand side evaluated to 36.6355826241 volt (Allowable error: 0.0001%, Actual error: 0.0049%)

Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500
Using solver 'mosek'
Solving for 9118 variables.
Solving took 1.33 seconds.
Allowing negative dual variable(s) as small as -2.313440721590491e-09.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2362 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 996075.4701 but bound is 600000.0000
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500
Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.4798616871 ampere but the right hand side evaluated to 615.823395675 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.5%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.4269127364 ampere but the right hand side evaluated to 615.859202474 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.3537333659 ampere but the right hand side evaluated to 615.885775157 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.2456906087 ampere but the right hand side evaluated to 615.959108991 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.0888352278 ampere but the right hand side evaluated to 616.178367729 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.87%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.6834494748 volt but the right hand side evaluated to 60.7350325814 volt (Allowable error: 0.0001%, Actual error: 1.6%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.5680978571 volt but the right hand side evaluated to 60.6741449399 volt (Allowable error: 0.0001%, Actual error: 1.5%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.403171487 volt but the right hand side evaluated to 60.5822248617 volt (Allowable error: 0.0001%, Actual error: 1.4%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.1439843961 volt but the right hand side evaluated to 60.4342120569 volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 60.7249433363 volt but the right hand side evaluated to 60.1877256234 volt (Allowable error: 0.0001%, Actual error: 0.89%)

Warning: Constraint [i_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [A]... >= 9.55*i0_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.6299754066 ampere but the right hand side evaluated to 530.630584974 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [V]... >= Kv_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6648736993 volt but the right hand side evaluated to 43.613851537 volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [i_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [A]... >= 9.55*i0_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.6243884554 ampere but the right hand side evaluated to 530.618911306 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [V]... >= Kv_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6483041578 volt but the right hand side evaluated to 43.600854668 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [A]... >= 9.55*i0_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5948643794 ampere but the right hand side evaluated to 530.318096321 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [V]... >= Kv_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6045512376 volt but the right hand side evaluated to 43.5555115701 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [A]... >= 9.55*i0_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5877072087 ampere but the right hand side evaluated to 530.261822004 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [V]... >= Kv_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.590897874 volt but the right hand side evaluated to 43.5428971027 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [A]... >= 9.55*i0_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5601201048 ampere but the right hand side evaluated to 530.01450216 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [V]... >= Kv_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.5438558952 volt but the right hand side evaluated to 43.4972568249 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [A]... >= 9.55*i0_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5647544258 ampere but the right hand side evaluated to 530.130697953 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.089%)

Warning: Constraint [v_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [V]... >= Kv_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.5380173524 volt but the right hand side evaluated to 43.4975646379 volt (Allowable error: 0.0001%, Actual error: 0.093%)

Warning: Constraint [i_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [A]... >= 9.55*i0_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5290030681 ampere but the right hand side evaluated to 529.772839355 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.093%)

Warning: Constraint [v_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [V]... >= Kv_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4839513395 volt but the right hand side evaluated to 43.4421185843 volt (Allowable error: 0.0001%, Actual error: 0.096%)

Warning: Constraint [i_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [A]... >= 9.55*i0_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5246672489 ampere but the right hand side evaluated to 529.724504082 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.094%)

Warning: Constraint [v_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [V]... >= Kv_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4783029815 volt but the right hand side evaluated to 43.4358813765 volt (Allowable error: 0.0001%, Actual error: 0.098%)

Warning: Constraint [i_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [A]... >= 9.55*i0_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4902108071 ampere but the right hand side evaluated to 529.409774432 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.091%)

Warning: Constraint [v_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [V]... >= Kv_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4206769046 volt but the right hand side evaluated to 43.3795027734 volt (Allowable error: 0.0001%, Actual error: 0.095%)

Warning: Constraint [i_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [A]... >= 9.55*i0_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4897590772 ampere but the right hand side evaluated to 529.405661954 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.091%)

Warning: Constraint [v_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [V]... >= Kv_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4199186847 volt but the right hand side evaluated to 43.3787620594 volt (Allowable error: 0.0001%, Actual error: 0.095%)

Warning: Constraint [i_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [A]... >= 9.55*i0_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4542367411 ampere but the right hand side evaluated to 529.095767663 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.086%)

Warning: Constraint [v_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [V]... >= Kv_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.357843237 volt but the right hand side evaluated to 43.3192140578 volt (Allowable error: 0.0001%, Actual error: 0.089%)

Warning: Constraint [i_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [A]... >= 9.55*i0_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4561813378 ampere but the right hand side evaluated to 529.111760873 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.086%)

Warning: Constraint [v_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [V]... >= Kv_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.3614185611 volt but the right hand side evaluated to 43.3225682458 volt (Allowable error: 0.0001%, Actual error: 0.09%)

Warning: Constraint [i_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [A]... >= 9.55*i0_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4177323953 ampere but the right hand side evaluated to 528.776676561 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.08%)

Warning: Constraint [v_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [V]... >= Kv_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2942101429 volt but the right hand side evaluated to 43.2581210109 volt (Allowable error: 0.0001%, Actual error: 0.083%)

Warning: Constraint [i_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [A]... >= 9.55*i0_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4222562631 ampere but the right hand side evaluated to 528.815779271 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.081%)

Warning: Constraint [v_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [V]... >= Kv_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.3021765533 volt but the right hand side evaluated to 43.2657352122 volt (Allowable error: 0.0001%, Actual error: 0.084%)

Warning: Constraint [i_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [A]... >= 9.55*i0_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3807635124 ampere but the right hand side evaluated to 528.4536646 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.074%)

Warning: Constraint [v_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [V]... >= Kv_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2297646482 volt but the right hand side evaluated to 43.1962561859 volt (Allowable error: 0.0001%, Actual error: 0.078%)

Warning: Constraint [i_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [A]... >= 9.55*i0_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.387753025 ampere but the right hand side evaluated to 528.514053914 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%)

Warning: Constraint [v_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [V]... >= Kv_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2420726449 volt but the right hand side evaluated to 43.2080185375 volt (Allowable error: 0.0001%, Actual error: 0.079%)

Warning: Constraint [i_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [A]... >= 9.55*i0_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3433025753 ampere but the right hand side evaluated to 528.126447186 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.069%)

Warning: Constraint [v_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [V]... >= Kv_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1644690894 volt but the right hand side evaluated to 43.1335799071 volt (Allowable error: 0.0001%, Actual error: 0.072%)

Warning: Constraint [i_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [A]... >= 9.55*i0_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3528999313 ampere but the right hand side evaluated to 528.21045122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.07%)

Warning: Constraint [v_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [V]... >= Kv_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1811655499 volt but the right hand side evaluated to 43.1496203198 volt (Allowable error: 0.0001%, Actual error: 0.073%)

Warning: Constraint [i_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [A]... >= 9.55*i0_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3052417482 ampere but the right hand side evaluated to 527.793480995 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%)

Warning: Constraint [v_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [V]... >= Kv_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0982622581 volt but the right hand side evaluated to 43.0699871692 volt (Allowable error: 0.0001%, Actual error: 0.066%)

Warning: Constraint [i_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [A]... >= 9.55*i0_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3172781621 ampere but the right hand side evaluated to 527.898341597 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.065%)

Warning: Constraint [v_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [V]... >= Kv_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1192776784 volt but the right hand side evaluated to 43.0901391272 volt (Allowable error: 0.0001%, Actual error: 0.068%)

Warning: Constraint [i_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [A]... >= 9.55*i0_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2666576938 ampere but the right hand side evaluated to 527.456149506 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.057%)

Warning: Constraint [v_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [V]... >= Kv_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0311361301 volt but the right hand side evaluated to 43.005525189 volt (Allowable error: 0.0001%, Actual error: 0.06%)

Warning: Constraint [i_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [A]... >= 9.55*i0_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2812116297 ampere but the right hand side evaluated to 527.58314398 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.059%)

Warning: Constraint [v_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [V]... >= Kv_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0564982282 volt but the right hand side evaluated to 43.0298618093 volt (Allowable error: 0.0001%, Actual error: 0.062%)

Warning: Constraint [i_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [A]... >= 9.55*i0_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2275040059 ampere but the right hand side evaluated to 527.113884165 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%)

Warning: Constraint [v_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [V]... >= Kv_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9630434152 volt but the right hand side evaluated to 42.9401358395 volt (Allowable error: 0.0001%, Actual error: 0.053%)

Warning: Constraint [i_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [A]... >= 9.55*i0_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2445672777 ampere but the right hand side evaluated to 527.26286091 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.054%)

Warning: Constraint [v_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [V]... >= Kv_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9927480607 volt but the right hand side evaluated to 42.9686472793 volt (Allowable error: 0.0001%, Actual error: 0.056%)

Warning: Constraint [i_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [A]... >= 9.55*i0_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1877043502 ampere but the right hand side evaluated to 526.765635923 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.045%)

Warning: Constraint [v_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [V]... >= Kv_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8939244497 volt but the right hand side evaluated to 42.8737321349 volt (Allowable error: 0.0001%, Actual error: 0.047%)

Warning: Constraint [i_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [A]... >= 9.55*i0_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2073068961 ampere but the right hand side evaluated to 526.937050485 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.048%)

Warning: Constraint [v_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [V]... >= Kv_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9279827556 volt but the right hand side evaluated to 42.9064444163 volt (Allowable error: 0.0001%, Actual error: 0.05%)

Warning: Constraint [i_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [A]... >= 9.55*i0_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1473269875 ampere but the right hand side evaluated to 526.412698419 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.039%)

Warning: Constraint [v_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [V]... >= Kv_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8237683768 volt but the right hand side evaluated to 42.8063574607 volt (Allowable error: 0.0001%, Actual error: 0.041%)

Warning: Constraint [i_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [A]... >= 9.55*i0_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1695237616 ampere but the right hand side evaluated to 526.607399134 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.042%)

Warning: Constraint [v_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [V]... >= Kv_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8622018079 volt but the right hand side evaluated to 42.8433200008 volt (Allowable error: 0.0001%, Actual error: 0.044%)

Warning: Constraint [i_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [A]... >= 9.55*i0_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.106269551 ampere but the right hand side evaluated to 526.053626704 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.033%)

Warning: Constraint [v_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [V]... >= Kv_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7525051 volt but the right hand side evaluated to 42.7379018937 volt (Allowable error: 0.0001%, Actual error: 0.034%)

Warning: Constraint [i_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [A]... >= 9.55*i0_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1308974109 ampere but the right hand side evaluated to 526.268936037 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.037%)

Warning: Constraint [v_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [V]... >= Kv_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7952623182 volt but the right hand side evaluated to 42.7789690368 volt (Allowable error: 0.0001%, Actual error: 0.038%)

Warning: Constraint [i_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [A]... >= 9.55*i0_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0645199336 ampere but the right hand side evaluated to 525.688432109 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [v_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [V]... >= Kv_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.6800925823 volt but the right hand side evaluated to 42.6683339542 volt (Allowable error: 0.0001%, Actual error: 0.028%)

Warning: Constraint [i_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [A]... >= 9.55*i0_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0916891515 ampere but the right hand side evaluated to 525.926062112 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.031%)

Warning: Constraint [v_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [V]... >= Kv_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7272164064 volt but the right hand side evaluated to 42.7136049383 volt (Allowable error: 0.0001%, Actual error: 0.032%)

Warning: Constraint [i_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [A]... >= 9.55*i0_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0220519828 ampere but the right hand side evaluated to 525.316909027 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.02%)

Warning: Constraint [v_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [V]... >= Kv_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.6064822992 volt but the right hand side evaluated to 42.5976086322 volt (Allowable error: 0.0001%, Actual error: 0.021%)

Warning: Constraint [i_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [A]... >= 9.55*i0_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0517602051 ampere but the right hand side evaluated to 525.576757236 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.025%)

Warning: Constraint [v_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [V]... >= Kv_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.6579808133 volt but the right hand side evaluated to 42.6470853671 volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [i_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [A]... >= 9.55*i0_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9788216225 ampere but the right hand side evaluated to 524.938577691 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [V]... >= Kv_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5316186195 volt but the right hand side evaluated to 42.525665095 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Constraint [i_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [A]... >= 9.55*i0_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0110852706 ampere but the right hand side evaluated to 525.220825947 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.018%)

Warning: Constraint [v_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [V]... >= Kv_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5875067004 volt but the right hand side evaluated to 42.5793651841 volt (Allowable error: 0.0001%, Actual error: 0.019%)

Warning: Constraint [i_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [A]... >= 9.55*i0_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9347937916 ampere but the right hand side evaluated to 524.553114112 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0068%)

Warning: Constraint [v_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [V]... >= Kv_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.4554469838 volt but the right hand side evaluated to 42.4524494601 volt (Allowable error: 0.0001%, Actual error: 0.0071%)

Warning: Constraint [i_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [A]... >= 9.55*i0_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9696398387 ampere but the right hand side evaluated to 524.858110522 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [v_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [V]... >= Kv_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5157446186 volt but the right hand side evaluated to 42.5104011591 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500
Using solver 'mosek'
Solving for 9118 variables.
Solving took 1.25 seconds.
Allowing negative dual variable(s) as small as -7.882573221079504e-12.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1906 but bound is 0.9465
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 1169782.8875 but bound is 600000.0000
Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2395 but bound is 0.1460
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0362 but bound is 0.0500
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/TailAero.165_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/TailAe could cause inaccurate result because it is above upper bound. Solution is 1085313.8703 but bound is 1000000.0000
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0401 but bound is 0.0500
Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.5168182865 ampere but the right hand side evaluated to 674.45458545 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.4534642189 ampere but the right hand side evaluated to 674.321153425 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.3655130557 ampere but the right hand side evaluated to 674.1103426 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%)

Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.2344628527 ampere but the right hand side evaluated to 673.812401354 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.95%)

Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.0402752564 ampere but the right hand side evaluated to 673.430587328 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.74%)

Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.8209509211 volt but the right hand side evaluated to 71.9033874268 volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.7201909843 volt but the right hand side evaluated to 71.8534317964 volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.5730733966 volt but the right hand side evaluated to 71.7741983088 volt (Allowable error: 0.0001%, Actual error: 1.1%)

Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.3412592201 volt but the right hand side evaluated to 71.6453925106 volt (Allowable error: 0.0001%, Actual error: 0.97%)

Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.9657736622 volt but the right hand side evaluated to 71.4291911048 volt (Allowable error: 0.0001%, Actual error: 0.75%)

Warning: Constraint [i_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [A]... >= 9.55*i0_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6891851319 ampere but the right hand side evaluated to 578.395131325 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [v_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [V]... >= Kv_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.1934661094 volt but the right hand side evaluated to 52.0867922473 volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [i_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [A]... >= 9.55*i0_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6859752058 ampere but the right hand side evaluated to 578.363692579 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [v_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [V]... >= Kv_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.1879773659 volt but the right hand side evaluated to 52.0812357523 volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [i_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [A]... >= 9.55*i0_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.618316458 ampere but the right hand side evaluated to 577.776168002 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [v_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [V]... >= Kv_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.0615496229 volt but the right hand side evaluated to 51.9603831473 volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [i_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [A]... >= 9.55*i0_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6169423195 ampere but the right hand side evaluated to 577.758296396 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [v_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [V]... >= Kv_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.0598400272 volt but the right hand side evaluated to 51.958233287 volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [i_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [A]... >= 9.55*i0_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.5476223168 ampere but the right hand side evaluated to 577.162197699 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [v_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [V]... >= Kv_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.9295164915 volt but the right hand side evaluated to 51.8341542297 volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [i_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [A]... >= 9.55*i0_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.5481663977 ampere but the right hand side evaluated to 577.159468316 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [v_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [V]... >= Kv_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.9316178826 volt but the right hand side evaluated to 51.8355172084 volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [i_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [A]... >= 9.55*i0_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4761420094 ampere but the right hand side evaluated to 576.536889243 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [v_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [V]... >= Kv_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.7967337047 volt but the right hand side evaluated to 51.7068075036 volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [i_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [A]... >= 9.55*i0_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4789059732 ampere but the right hand side evaluated to 576.554650629 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [v_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [V]... >= Kv_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.8028090718 volt but the right hand side evaluated to 51.7120763125 volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [i_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [A]... >= 9.55*i0_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4039622102 ampere but the right hand side evaluated to 575.9021274 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [v_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [V]... >= Kv_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.6632160065 volt but the right hand side evaluated to 51.5784567929 volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [i_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [A]... >= 9.55*i0_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.40933071 ampere but the right hand side evaluated to 575.947120765 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [v_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [V]... >= Kv_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.6734725674 volt but the right hand side evaluated to 51.5881235013 volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [i_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [A]... >= 9.55*i0_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.3371668711 ampere but the right hand side evaluated to 575.362559646 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [V]... >= Kv_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.5323683364 volt but the right hand side evaluated to 51.4568165841 volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [i_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [A]... >= 9.55*i0_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.3392744194 ampere but the right hand side evaluated to 575.334298396 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [v_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [V]... >= Kv_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.5434557168 volt but the right hand side evaluated to 51.4634140202 volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [i_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [A]... >= 9.55*i0_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.2597311011 ampere but the right hand side evaluated to 574.64405328 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [V]... >= Kv_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.3950961661 volt but the right hand side evaluated to 51.3215813759 volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [i_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [A]... >= 9.55*i0_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.2690644725 ampere but the right hand side evaluated to 574.722241334 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [V]... >= Kv_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.4129175272 volt but the right hand side evaluated to 51.3383781008 volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [i_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [A]... >= 9.55*i0_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.186568363 ampere but the right hand side evaluated to 574.002282232 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [v_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [V]... >= Kv_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.2597447526 volt but the right hand side evaluated to 51.1915805534 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [A]... >= 9.55*i0_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.1982933246 ampere but the right hand side evaluated to 574.104248104 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [v_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [V]... >= Kv_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.2815680523 volt but the right hand side evaluated to 51.2124654923 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [A]... >= 9.55*i0_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.1132435771 ampere but the right hand side evaluated to 573.361742362 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [v_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [V]... >= Kv_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.1237785069 volt but the right hand side evaluated to 51.0612089293 volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [i_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [A]... >= 9.55*i0_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.1268202083 ampere but the right hand side evaluated to 573.478219255 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [v_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [V]... >= Kv_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 51.1492728679 volt but the right hand side evaluated to 51.085472159 volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [i_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [A]... >= 9.55*i0_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.0392907779 ampere but the right hand side evaluated to 572.714732321 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [V]... >= Kv_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 50.9868676117 volt but the right hand side evaluated to 50.9298360523 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [A]... >= 9.55*i0_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.0550998733 ampere but the right hand side evaluated to 572.852315046 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [V]... >= Kv_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 51.0162402342 volt but the right hand side evaluated to 50.9579585232 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [A]... >= 9.55*i0_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.9647630809 ampere but the right hand side evaluated to 572.062564548 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%)

Warning: Constraint [v_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [V]... >= Kv_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.8489943527 volt but the right hand side evaluated to 50.797518326 volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [i_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [A]... >= 9.55*i0_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.9826046143 ampere but the right hand side evaluated to 572.217855507 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [V]... >= Kv_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.8821220081 volt but the right hand side evaluated to 50.8292403427 volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [i_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [A]... >= 9.55*i0_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8895832115 ampere but the right hand side evaluated to 571.40429109 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%)

Warning: Constraint [v_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [V]... >= Kv_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.7100598589 volt but the right hand side evaluated to 50.6641373036 volt (Allowable error: 0.0001%, Actual error: 0.091%)

Warning: Constraint [i_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [A]... >= 9.55*i0_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.9096480364 ampere but the right hand side evaluated to 571.58055811 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.09%)

Warning: Constraint [v_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [V]... >= Kv_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.7470361851 volt but the right hand side evaluated to 50.6996862083 volt (Allowable error: 0.0001%, Actual error: 0.093%)

Warning: Constraint [i_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [A]... >= 9.55*i0_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8135685677 ampere but the right hand side evaluated to 570.737182821 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%)

Warning: Constraint [v_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [V]... >= Kv_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.5699077614 volt but the right hand side evaluated to 50.5294459137 volt (Allowable error: 0.0001%, Actual error: 0.08%)

Warning: Constraint [i_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [A]... >= 9.55*i0_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8359467349 ampere but the right hand side evaluated to 570.935989211 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.08%)

Warning: Constraint [v_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [V]... >= Kv_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.6107773448 volt but the right hand side evaluated to 50.5689313619 volt (Allowable error: 0.0001%, Actual error: 0.083%)

Warning: Constraint [i_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [A]... >= 9.55*i0_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.7374108468 ampere but the right hand side evaluated to 570.073422694 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%)

Warning: Constraint [v_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [V]... >= Kv_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.428852064 volt but the right hand side evaluated to 50.3942698003 volt (Allowable error: 0.0001%, Actual error: 0.069%)

Warning: Constraint [i_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [A]... >= 9.55*i0_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.7615778669 ampere but the right hand side evaluated to 570.285779487 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.069%)

Warning: Constraint [v_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [V]... >= Kv_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.4733171621 volt but the right hand side evaluated to 50.4370293511 volt (Allowable error: 0.0001%, Actual error: 0.072%)

Warning: Constraint [i_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [A]... >= 9.55*i0_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.660214901 ampere but the right hand side evaluated to 569.398168068 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%)

Warning: Constraint [v_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [V]... >= Kv_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.2863491743 volt but the right hand side evaluated to 50.2574869797 volt (Allowable error: 0.0001%, Actual error: 0.057%)

Warning: Constraint [i_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [A]... >= 9.55*i0_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6862870442 ampere but the right hand side evaluated to 569.626127119 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.059%)

Warning: Constraint [v_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [V]... >= Kv_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.3344844522 volt but the right hand side evaluated to 50.303682748 volt (Allowable error: 0.0001%, Actual error: 0.061%)

Warning: Constraint [i_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [A]... >= 9.55*i0_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5818040561 ampere but the right hand side evaluated to 568.70887114 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.045%)

Warning: Constraint [v_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [V]... >= Kv_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.1422498778 volt but the right hand side evaluated to 50.118869777 volt (Allowable error: 0.0001%, Actual error: 0.047%)

Warning: Constraint [i_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [A]... >= 9.55*i0_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6101981572 ampere but the right hand side evaluated to 568.959441887 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.049%)

Warning: Constraint [v_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [V]... >= Kv_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.1942643877 volt but the right hand side evaluated to 50.1689889875 volt (Allowable error: 0.0001%, Actual error: 0.05%)

Warning: Constraint [i_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [A]... >= 9.55*i0_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.503097168 ampere but the right hand side evaluated to 568.021537314 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.034%)

Warning: Constraint [v_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [V]... >= Kv_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.996965514 volt but the right hand side evaluated to 49.9794908224 volt (Allowable error: 0.0001%, Actual error: 0.035%)

Warning: Constraint [i_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [A]... >= 9.55*i0_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5332998571 ampere but the right hand side evaluated to 568.285986061 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%)

Warning: Constraint [v_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [V]... >= Kv_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.0525930425 volt but the right hand side evaluated to 50.0329175744 volt (Allowable error: 0.0001%, Actual error: 0.039%)

Warning: Constraint [i_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [A]... >= 9.55*i0_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.4232539512 ampere but the right hand side evaluated to 567.322378524 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.023%)

Warning: Constraint [v_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [V]... >= Kv_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.8499921865 volt but the right hand side evaluated to 49.8383182672 volt (Allowable error: 0.0001%, Actual error: 0.023%)

Warning: Constraint [i_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [A]... >= 9.55*i0_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.4555269457 ampere but the right hand side evaluated to 567.605090248 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%)

Warning: Constraint [v_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [V]... >= Kv_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.9093696372 volt but the right hand side evaluated to 49.8953628533 volt (Allowable error: 0.0001%, Actual error: 0.028%)

Warning: Constraint [i_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [A]... >= 9.55*i0_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.3423879262 ampere but the right hand side evaluated to 566.613785058 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%)

Warning: Constraint [v_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [V]... >= Kv_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.7013180899 volt but the right hand side evaluated to 49.6954593721 volt (Allowable error: 0.0001%, Actual error: 0.012%)

Warning: Constraint [i_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [A]... >= 9.55*i0_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.3767292004 ampere but the right hand side evaluated to 566.914667516 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.016%)

Warning: Constraint [v_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [V]... >= Kv_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.7644478537 volt but the right hand side evaluated to 49.7561183936 volt (Allowable error: 0.0001%, Actual error: 0.017%)

Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2395 but bound is 0.1460
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0362 but bound is 0.0500
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0401 but bound is 0.0500
Warning: Constraint [i_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [A]... >= 9.55*i0_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.2969044461 ampere but the right hand side evaluated to 566.215189714 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.005%)

Warning: Constraint [v_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [V]... >= Kv_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.6177497658 volt but the right hand side evaluated to 49.6151507079 volt (Allowable error: 0.0001%, Actual error: 0.0052%)

Using solver 'mosek'
Solving for 4738 variables.
Solving took 0.638 seconds.
Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1350804.7178 but bound is 600000.0000
Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/TailAero.246_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Tail could cause inaccurate result because it is above upper bound. Solution is 1008642.5207 but bound is 1000000.0000
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/TailAero.247_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Tail could cause inaccurate result because it is above upper bound. Solution is 1292032.4332 but bound is 1000000.0000
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.4850831652 ampere but the right hand side evaluated to 734.385479936 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%)

Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.4269319843 ampere but the right hand side evaluated to 734.137719607 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%)

Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.3444447521 ampere but the right hand side evaluated to 733.758465059 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%)

Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.2198444304 ampere but the right hand side evaluated to 733.184380824 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%)

Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.0308211154 ampere but the right hand side evaluated to 732.323549193 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%)

Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 85.0572231972 volt but the right hand side evaluated to 84.4091397813 volt (Allowable error: 0.0001%, Actual error: 0.77%)

Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.9750002042 volt but the right hand side evaluated to 84.3626540077 volt (Allowable error: 0.0001%, Actual error: 0.73%)

Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.8508479081 volt but the right hand side evaluated to 84.2860523858 volt (Allowable error: 0.0001%, Actual error: 0.67%)

Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.6551119176 volt but the right hand side evaluated to 84.1621014005 volt (Allowable error: 0.0001%, Actual error: 0.59%)

Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.3395955732 volt but the right hand side evaluated to 83.9568516261 volt (Allowable error: 0.0001%, Actual error: 0.46%)

Warning: Constraint [i_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [A]... >= 9.55*i0_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.6960931732 ampere but the right hand side evaluated to 625.927938569 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%)

Warning: Constraint [v_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [V]... >= Kv_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 61.275847558 volt but the right hand side evaluated to 61.1323942912 volt (Allowable error: 0.0001%, Actual error: 0.23%)

Warning: Constraint [i_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [A]... >= 9.55*i0_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.6049268827 ampere but the right hand side evaluated to 625.132235268 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [v_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [V]... >= Kv_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 61.0975968447 volt but the right hand side evaluated to 60.9618640561 volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [i_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [A]... >= 9.55*i0_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.5138546039 ampere but the right hand side evaluated to 624.339975894 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [v_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [V]... >= Kv_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.9194879258 volt but the right hand side evaluated to 60.7917117953 volt (Allowable error: 0.0001%, Actual error: 0.21%)

Warning: Constraint [i_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [A]... >= 9.55*i0_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.4219089099 ampere but the right hand side evaluated to 623.532130448 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [v_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [V]... >= Kv_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.7402727238 volt but the right hand side evaluated to 60.6197087949 volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [i_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [A]... >= 9.55*i0_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.3296763367 ampere but the right hand side evaluated to 622.720980228 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [v_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [V]... >= Kv_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.5606085314 volt but the right hand side evaluated to 60.4471824667 volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [i_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [A]... >= 9.55*i0_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.2372264952 ampere but the right hand side evaluated to 621.908688637 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [v_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [V]... >= Kv_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.3805760091 volt but the right hand side evaluated to 60.2743632221 volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [i_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [A]... >= 9.55*i0_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.1449525723 ampere but the right hand side evaluated to 621.102905139 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [v_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [V]... >= Kv_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.2004381111 volt but the right hand side evaluated to 60.1019020923 volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [i_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [A]... >= 9.55*i0_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.0520391234 ampere but the right hand side evaluated to 620.288821137 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [v_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [V]... >= Kv_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.0193678571 volt but the right hand side evaluated to 59.9282708434 volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [i_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [A]... >= 9.55*i0_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.9589067965 ampere but the right hand side evaluated to 619.474985094 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [V]... >= Kv_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.8377275755 volt but the right hand side evaluated to 59.7542833236 volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [i_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [A]... >= 9.55*i0_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.8644114982 ampere but the right hand side evaluated to 618.640133176 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [v_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [V]... >= Kv_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.6543268873 volt but the right hand side evaluated to 59.5777207233 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [A]... >= 9.55*i0_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.7703802198 ampere but the right hand side evaluated to 617.819686965 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [V]... >= Kv_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.4709269147 volt but the right hand side evaluated to 59.4021310591 volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [i_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [A]... >= 9.55*i0_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.6755632625 ampere but the right hand side evaluated to 616.990456595 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [V]... >= Kv_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.2862436518 volt but the right hand side evaluated to 59.2251105997 volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [i_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [A]... >= 9.55*i0_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.5798172048 ampere but the right hand side evaluated to 616.150186449 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%)

Warning: Constraint [v_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [V]... >= Kv_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.1000568606 volt but the right hand side evaluated to 59.0463515886 volt (Allowable error: 0.0001%, Actual error: 0.091%)

Warning: Constraint [i_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [A]... >= 9.55*i0_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.4835800653 ampere but the right hand side evaluated to 615.307908589 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.....076%)

Warning: Constraint [v_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [V]... >= Kv_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.9127539782 volt but the right hand side evaluated to 58.8667215584 volt (Allowable error: 0.0001%, Actual error: 0.078%)

Warning: Constraint [i_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [A]... >= 9.55*i0_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.3863993082 ampere but the right hand side evaluated to 614.455768497 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%)

Warning: Constraint [v_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [V]... >= Kv_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.7238588027 volt but the right hand side evaluated to 58.6853940248 volt (Allowable error: 0.0001%, Actual error: 0.066%)

Warning: Constraint [i_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [A]... >= 9.55*i0_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.2883257876 ampere but the right hand side evaluated to 613.59536851 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%)

Warning: Constraint [v_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [V]... >= Kv_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.5333570681 volt but the right hand side evaluated to 58.5024648612 volt (Allowable error: 0.0001%, Actual error: 0.053%)

Warning: Constraint [i_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [A]... >= 9.55*i0_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.1894287943 ampere but the right hand side evaluated to 612.728584716 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%)

Warning: Constraint [v_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [V]... >= Kv_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.34122998 volt but the right hand side evaluated to 58.3180344411 volt (Allowable error: 0.0001%, Actual error: 0.04%)

Warning: Constraint [i_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [A]... >= 9.55*i0_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.0894710108 ampere but the right hand side evaluated to 611.851750501 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [v_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [V]... >= Kv_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.1472124301 volt but the right hand side evaluated to 58.1316988809 volt (Allowable error: 0.0001%, Actual error: 0.027%)

Warning: Constraint [i_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [A]... >= 9.55*i0_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 63.9884701057 ampere but the right hand side evaluated to 610.965859479 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [V]... >= Kv_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 57.9512410147 volt but the right hand side evaluated to 57.9434753394 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Using solver 'mosek'
Solving for 577 variables.
Solving took 0.0797 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1350804.6900 but bound is 600000.0000
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero_(0,), Re_Mission/Climb/AircraftDrag/TailAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1008642.4804 but bound is 1000000.0000
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1292032.3843 but bound is 1000000.0000
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 77.4846363322 ampere but the right hand side evaluated to 734.381249951 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 77.426506811 ampere but the right hand side evaluated to 734.133687543 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 77.344048942 ampere but the right hand side evaluated to 733.754703267 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 77.2194939759 ampere but the right hand side evaluated to 733.181039757 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 77.0305428479 ampere but the right hand side evaluated to 732.32088486 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 85.0577040288 volt but the right hand side evaluated to 84.4096225669 volt (Allowable error: 0.0001%, Actual error: 0.77%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 84.9754590237 volt but the right hand side evaluated to 84.3631139896 volt (Allowable error: 0.0001%, Actual error: 0.73%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 84.8512764234 volt but the right hand side evaluated to 84.2864811907 volt (Allowable error: 0.0001%, Actual error: 0.67%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 84.6554929271 volt but the right hand side evaluated to 84.1624816739 volt (Allowable error: 0.0001%, Actual error: 0.59%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 84.3398995074 volt but the right hand side evaluated to 83.9571538917 volt (Allowable error: 0.0001%, Actual error: 0.46%)

Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Using solver 'mosek'
Solving for 577 variables.
Solving took 0.0813 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1350804.6900 but bound is 600000.0000
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero_(0,), Re_Mission/Climb/AircraftDrag/TailAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1008642.4804 but bound is 1000000.0000
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1292032.3843 but bound is 1000000.0000
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 77.4846363322 ampere but the right hand side evaluated to 734.381249951 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 77.426506811 ampere but the right hand side evaluated to 734.133687543 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 77.344048942 ampere but the right hand side evaluated to 733.754703267 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 77.2194939759 ampere but the right hand side evaluated to 733.181039757 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 77.0305428479 ampere but the right hand side evaluated to 732.32088486 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 85.0577040288 volt but the right hand side evaluated to 84.4096225669 volt (Allowable error: 0.0001%, Actual error: 0.77%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 84.9754590237 volt but the right hand side evaluated to 84.3631139896 volt (Allowable error: 0.0001%, Actual error: 0.73%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 84.8512764234 volt but the right hand side evaluated to 84.2864811907 volt (Allowable error: 0.0001%, Actual error: 0.67%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 84.6554929271 volt but the right hand side evaluated to 84.1624816739 volt (Allowable error: 0.0001%, Actual error: 0.59%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 84.3398995074 volt but the right hand side evaluated to 83.9571538917 volt (Allowable error: 0.0001%, Actual error: 0.46%)

Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Using solver 'mosek'
Solving for 4738 variables.
Solving took 0.683 seconds.
Allowing negative dual variable(s) as small as -8.97488979118022e-13.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1350804.7006 but bound is 600000.0000
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero_(0,), Re_Mission/Climb/AircraftDrag/TailAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1008642.4963 but bound is 1000000.0000
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1292032.4035 but bound is 1000000.0000
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 77.4850673786 ampere but the right hand side evaluated to 734.385382206 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 77.4269196774 ampere but the right hand side evaluated to 734.13764252 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 77.3444365619 ampere but the right hand side evaluated to 733.758412344 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 77.2198413713 ampere but the right hand side evaluated to 733.184358383 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 77.0308234573 ampere but the right hand side evaluated to 732.323558455 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 85.0572261421 volt but the right hand side evaluated to 84.4091488104 volt (Allowable error: 0.0001%, Actual error: 0.77%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 84.9750022562 volt but the right hand side evaluated to 84.3626607068 volt (Allowable error: 0.0001%, Actual error: 0.73%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 84.8508489213 volt but the right hand side evaluated to 84.2860563349 volt (Allowable error: 0.0001%, Actual error: 0.67%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 84.655111672 volt but the right hand side evaluated to 84.1621019373 volt (Allowable error: 0.0001%, Actual error: 0.59%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 84.3395940621 volt but the right hand side evaluated to 83.9568485974 volt (Allowable error: 0.0001%, Actual error: 0.46%)

Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 65.6958115371 ampere but the right hand side evaluated to 625.921971636 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%)

Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 61.2754428029 volt but the right hand side evaluated to 61.1316604384 volt (Allowable error: 0.0001%, Actual error: 0.24%)

Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.6049807696 ampere but the right hand side evaluated to 625.133020661 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 61.0976029842 volt but the right hand side evaluated to 60.9618972989 volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.5133978139 ampere but the right hand side evaluated to 624.330680335 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.9189103075 volt but the right hand side evaluated to 60.7906398936 volt (Allowable error: 0.0001%, Actual error: 0.21%)

Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.4217990447 ampere but the right hand side evaluated to 623.52977182 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.740109512 volt but the right hand side evaluated to 60.6194144943 volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.3297045661 ampere but the right hand side evaluated to 622.7214058 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.5606143029 volt but the right hand side evaluated to 60.4472037784 volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.2371541313 ampere but the right hand side evaluated to 621.907182202 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.3804781752 volt but the right hand side evaluated to 60.274183928 volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.1450268076 ampere but the right hand side evaluated to 621.104336762 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.2005152688 volt but the right hand side evaluated to 60.102051276 volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.0520085123 ampere but the right hand side evaluated to 620.288230439 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.0193356436 volt but the right hand side evaluated to 59.9282088624 volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 64.9586498193 ampere but the right hand side evaluated to 619.470181537 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 59.8374911783 volt but the right hand side evaluated to 59.7538130973 volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 64.8640750948 ampere but the right hand side evaluated to 618.633992621 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 59.6540476804 volt but the right hand side evaluated to 59.5771504713 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.7729167546 ampere but the right hand side evaluated to 617.867016934 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.4732269481 volt but the right hand side evaluated to 59.4067249774 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.6753614874 ampere but the right hand side evaluated to 616.986674902 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.2860567221 volt but the right hand side evaluated to 59.2247397494 volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.5798918625 ampere but the right hand side evaluated to 616.151855812 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%)

Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.1001783154 volt but the right hand side evaluated to 59.0465677201 volt (Allowable error: 0.0001%, Actual error: 0.091%)

Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.4835894824 ampere but the right hand side evaluated to 615.308187545 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%)

Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.9127818479 volt but the right hand side evaluated to 58.8667681057 volt (Allowable error: 0.0001%, Actual error: 0.078%)

Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.3863828148 ampere but the right hand side evaluated to 614.455578241 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%)

Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.7238660666 volt but the right hand side evaluated to 58.6853980399 volt (Allowable error: 0.0001%, Actual error: 0.066%)

Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.2883012716 ampere but the right hand side evaluated to 613.595064585 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%)

Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.5333641996 volt but the right hand side evaluated to 58.5024650952 volt (Allowable error: 0.0001%, Actual error: 0.053%)

Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.1894150011 ampere but the right hand side evaluated to 612.728429271 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%)

Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.3412364354 volt but the right hand side evaluated to 58.3180385531 volt (Allowable error: 0.0001%, Actual error: 0.04%)

Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.0894618314 ampere but the right hand side evaluated to 611.851653325 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.1472174624 volt but the right hand side evaluated to 58.131702974 volt (Allowable error: 0.0001%, Actual error: 0.027%)

Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 63.9884652267 ampere but the right hand side evaluated to 610.965811203 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 57.9512436529 volt but the right hand side evaluated to 57.9434778114 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.737386186483651e-12.
Allowing negative dual variable(s) as small as -1.6288982252959932e-11.
Allowing negative dual variable(s) as small as -4.10112871271003e-12.
Allowing negative dual variable(s) as small as -3.4796176369186454e-12.
Solving took 4 GP solves and 5.72 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), CL_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1644 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 1233794.1053 but bound is 600000.0000
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2427 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0274 but bound is 0.0500
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/TailAero.43_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/TailAer could cause inaccurate result because it is above upper bound. Solution is 1218667.7655 but bound is 1000000.0000
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0428 but bound is 0.0500
Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.9288267219 ampere but the right hand side evaluated to 687.184289798 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.8564982362 ampere but the right hand side evaluated to 686.996700725 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.7565918644 ampere but the right hand side evaluated to 686.713125437 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.6078857792 ampere but the right hand side evaluated to 686.308476226 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.3875268377 ampere but the right hand side evaluated to 685.771837678 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.8%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.4571505058 volt but the right hand side evaluated to 74.4435381984 volt (Allowable error: 0.0001%, Actual error: 1.4%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.3584466501 volt but the right hand side evaluated to 74.399640175 volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.2133449388 volt but the right hand side evaluated to 74.3277299643 volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 74.9840240739 volt but the right hand side evaluated to 74.2094477368 volt (Allowable error: 0.0001%, Actual error: 1%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 74.6107903113 volt but the right hand side evaluated to 74.0080279298 volt (Allowable error: 0.0001%, Actual error: 0.81%)

Warning: Constraint [i_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.8806947816 ampere but the right hand side evaluated to 589.548559161 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%)

Warning: Constraint [v_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.3129630984 volt but the right hand side evaluated to 54.1828821581 volt (Allowable error: 0.0001%, Actual error: 0.24%)

Warning: Constraint [i_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.7954770313 ampere but the right hand side evaluated to 588.809705692 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [v_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.1518933692 volt but the right hand side evaluated to 54.029100008 volt (Allowable error: 0.0001%, Actual error: 0.23%)

Warning: Constraint [i_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.7095208175 ampere but the right hand side evaluated to 588.058741267 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.21%)

Warning: Constraint [v_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.9902346671 volt but the right hand side evaluated to 53.8742317312 volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [i_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.6233871855 ampere but the right hand side evaluated to 587.306122976 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [v_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.8283352184 volt but the right hand side evaluated to 53.7191089299 volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [i_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.5370288723 ampere but the right hand side evaluated to 586.55146534 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [v_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.6661071844 volt but the right hand side evaluated to 53.5636499392 volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [i_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.4501432965 ampere but the right hand side evaluated to 585.789872967 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [v_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.5032889591 volt but the right hand side evaluated to 53.4074040881 volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [i_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.3634322745 ampere but the right hand side evaluated to 585.034170167 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [v_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.3402937919 volt but the right hand side evaluated to 53.2513613093 volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [i_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.2760736801 ampere but the right hand side evaluated to 584.270318821 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [v_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.1765120998 volt but the right hand side evaluated to 53.0943289745 volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [i_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.1882491398 ampere but the right hand side evaluated to 583.501980622 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.0120064621 volt but the right hand side evaluated to 52.9365511335 volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [i_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.0990026204 ampere but the right hand side evaluated to 582.71291988 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [v_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.8461098705 volt but the right hand side evaluated to 52.7766945988 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.0110735813 ampere but the right hand side evaluated to 581.951460349 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.6804961632 volt but the right hand side evaluated to 52.6185103331 volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [i_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.9214892778 ampere but the right hand side evaluated to 581.166165107 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.5132194543 volt but the right hand side evaluated to 52.4578920212 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.8317197265 ampere but the right hand side evaluated to 580.383145098 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.089%)

Warning: Constraint [v_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.3451328604 volt but the right hand side evaluated to 52.2968226718 volt (Allowable error: 0.0001%, Actual error: 0.092%)

Warning: Constraint [i_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.7410719053 ampere but the right hand side evaluated to 579.590848083 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%)

Warning: Constraint [v_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.1757411064 volt but the right hand side evaluated to 52.1343452053 volt (Allowable error: 0.0001%, Actual error: 0.079%)

Warning: Constraint [i_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.6494896957 ampere but the right hand side evaluated to 578.788831472 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%)

Warning: Constraint [v_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.0049441141 volt but the right hand side evaluated to 51.9703682899 volt (Allowable error: 0.0001%, Actual error: 0.067%)

Warning: Constraint [i_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.5570277108 ampere but the right hand side evaluated to 577.978570002 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%)

Warning: Constraint [v_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.832702738 volt but the right hand side evaluated to 51.8049414032 volt (Allowable error: 0.0001%, Actual error: 0.054%)

Warning: Constraint [i_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.4637667256 ampere but the right hand side evaluated to 577.16201246 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.039%)

Warning: Constraint [v_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.6589910479 volt but the right hand side evaluated to 51.6381475263 volt (Allowable error: 0.0001%, Actual error: 0.04%)

Warning: Constraint [i_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [A]... >= 9.55*i0_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.3694733391 ampere but the right hand side evaluated to 576.335683987 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [v_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [V]... >= Kv_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.4835929054 volt but the right hand side evaluated to 51.4696541047 volt (Allowable error: 0.0001%, Actual error: 0.027%)

Warning: Constraint [i_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.2741726972 ampere but the right hand side evaluated to 575.50058953 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.3064398726 volt but the right hand side evaluated to 51.2994630506 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2427 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0274 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0428 but bound is 0.0500
Using solver 'mosek_cli'
Solving for 4738 variables.
Solving took 0.811 seconds.
Allowing negative dual variable(s) as small as -8.97489e-13.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1350803.2858 but bound is 600000.0000
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero_(0,), Re_Mission/Climb/AircraftDrag/TailAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1008646.6099 but bound is 1000000.0000
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1292036.2239 but bound is 1000000.0000
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 77.4850488745 ampere but the right hand side evaluated to 734.385298061 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 77.4269568751 ampere but the right hand side evaluated to 734.137125177 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 77.3444637157 ampere but the right hand side evaluated to 733.758470359 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 77.2198076579 ampere but the right hand side evaluated to 733.183974901 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%)

Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 77.0308506959 ampere but the right hand side evaluated to 732.323127431 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 85.0572024374 volt but the right hand side evaluated to 84.4091098586 volt (Allowable error: 0.0001%, Actual error: 0.77%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 84.9749918779 volt but the right hand side evaluated to 84.3626773877 volt (Allowable error: 0.0001%, Actual error: 0.73%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 84.8508492102 volt but the right hand side evaluated to 84.2860344713 volt (Allowable error: 0.0001%, Actual error: 0.67%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 84.6550699606 volt but the right hand side evaluated to 84.1621054377 volt (Allowable error: 0.0001%, Actual error: 0.59%)

Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 84.339557358 volt but the right hand side evaluated to 83.9568933953 volt (Allowable error: 0.0001%, Actual error: 0.46%)

Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 65.6958002295 ampere but the right hand side evaluated to 625.922173108 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%)

Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 61.2754332517 volt but the right hand side evaluated to 61.1316613.
----------------------------------------------------------------------
Ran 6 tests in 190.256s

OK

Generating XML reports...
886 volt (Allowable error: 0.0001%, Actual error: 0.24%)

Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.6050057367 ampere but the right hand side evaluated to 625.132810313 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 61.0976253227 volt but the right hand side evaluated to 60.9619162 volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.5134195315 ampere but the right hand side evaluated to 624.331144963 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.918932202 volt but the right hand side evaluated to 60.7906230409 volt (Allowable error: 0.0001%, Actual error: 0.21%)

Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.4218303392 ampere but the right hand side evaluated to 623.529422431 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.7400935629 volt but the right hand side evaluated to 60.6194605926 volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.3297158901 ampere but the right hand side evaluated to 622.72126872 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.5606292744 volt but the right hand side evaluated to 60.447247421 volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.2371440019 ampere but the right hand side evaluated to 621.907292718 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.380487614 volt but the right hand side evaluated to 60.2741719023 volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.145029012 ampere but the right hand side evaluated to 621.104287716 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.2005205929 volt but the right hand side evaluated to 60.1020709834 volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.0520032483 ampere but the right hand side evaluated to 620.288540745 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.019349386 volt but the right hand side evaluated to 59.9281782464 volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 64.9586556113 ampere but the right hand side evaluated to 619.470485794 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 59.837466807 volt but the right hand side evaluated to 59.7537990321 volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 64.8640797653 ampere but the right hand side evaluated to 618.634017176 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 59.6540474767 volt but the right hand side evaluated to 59.5771875316 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.7729449519 ampere but the right hand side evaluated to 617.866595808 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.473212435 volt but the right hand side evaluated to 59.4067668929 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.6753409628 ampere but the right hand side evaluated to 616.986531336 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.2860479955 volt but the right hand side evaluated to 59.2247446877 volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.5798859951 ampere but the right hand side evaluated to 616.151947259 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%)

Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.1001817675 volt but the right hand side evaluated to 59.0465957272 volt (Allowable error: 0.0001%, Actual error: 0.091%)

Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.4836046489 ampere but the right hand side evaluated to 615.308274471 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%)

Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.912777346 volt but the right hand side evaluated to 58.8667998022 volt (Allowable error: 0.0001%, Actual error: 0.078%)

Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.3863722698 ampere but the right hand side evaluated to 614.455556698 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%)

Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.7238530799 volt but the right hand side evaluated to 58.6853712273 volt (Allowable error: 0.0001%, Actual error: 0.066%)

Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.2883221716 ampere but the right hand side evaluated to 613.594979337 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%)

Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.5333688904 volt but the right hand side evaluated to 58.5024457164 volt (Allowable error: 0.0001%, Actual error: 0.053%)

Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.1893943494 ampere but the right hand side evaluated to 612.728860763 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%)

Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.3412272275 volt but the right hand side evaluated to 58.3180388762 volt (Allowable error: 0.0001%, Actual error: 0.04%)

Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.0894651381 ampere but the right hand side evaluated to 611.851541334 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.1472159049 volt but the right hand side evaluated to 58.131716177 volt (Allowable error: 0.0001%, Actual error: 0.027%)

Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 63.9884757027 ampere but the right hand side evaluated to 610.965348838 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 57.9512418942 volt but the right hand side evaluated to 57.9434978888 volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.737386e-12.
Allowing negative dual variable(s) as small as -1.660105e-11.
Allowing negative dual variable(s) as small as -5.264452e-12.
Allowing negative dual variable(s) as small as -6.406306e-12.
Solving took 4 GP solves and 7.04 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), CL_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1644 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 1233788.4076 but bound is 600000.0000
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2427 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0274 but bound is 0.0500
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/TailAero.43_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/TailAer could cause inaccurate result because it is above upper bound. Solution is 1218669.1980 but bound is 1000000.0000
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0428 but bound is 0.0500
Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.9277335899 ampere but the right hand side evaluated to 687.17425883 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.8554251491 ampere but the right hand side evaluated to 686.987467213 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.7556088009 ampere but the right hand side evaluated to 686.704162667 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.6070482172 ampere but the right hand side evaluated to 686.300669005 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%)

Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.386802727 ampere but the right hand side evaluated to 685.764999224 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.8%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.4581350641 volt but the right hand side evaluated to 74.4446326597 volt (Allowable error: 0.0001%, Actual error: 1.4%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.3594249852 volt but the right hand side evaluated to 74.4006205382 volt (Allowable error: 0.0001%, Actual error: 1.3%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.2142719863 volt but the right hand side evaluated to 74.3286747933 volt (Allowable error: 0.0001%, Actual error: 1.2%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 74.9849180014 volt but the right hand side evaluated to 74.2102880125 volt (Allowable error: 0.0001%, Actual error: 1%)

Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 74.6115260525 volt but the right hand side evaluated to 74.0088099865 volt (Allowable error: 0.0001%, Actual error: 0.81%)

Warning: Constraint [i_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.8804934514 ampere but the right hand side evaluated to 589.544902407 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%)

Warning: Constraint [v_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.3129126122 volt but the right hand side evaluated to 54.1827649492 volt (Allowable error: 0.0001%, Actual error: 0.24%)

Warning: Constraint [i_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.7952808563 ampere but the right hand side evaluated to 588.805889101 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [v_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.1518425692 volt but the right hand side evaluated to 54.0289639184 volt (Allowable error: 0.0001%, Actual error: 0.23%)

Warning: Constraint [i_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.7093216669 ampere but the right hand side evaluated to 588.05533794 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.21%)

Warning: Constraint [v_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.9901703803 volt but the right hand side evaluated to 53.8741240073 volt (Allowable error: 0.0001%, Actual error: 0.22%)

Warning: Constraint [i_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.6231739327 ampere but the right hand side evaluated to 587.303641495 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [v_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.828281097 volt but the right hand side evaluated to 53.7189470024 volt (Allowable error: 0.0001%, Actual error: 0.2%)

Warning: Constraint [i_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.5368387779 ampere but the right hand side evaluated to 586.549176621 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [v_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.666072241 volt but the right hand side evaluated to 53.5635415418 volt (Allowable error: 0.0001%, Actual error: 0.19%)

Warning: Constraint [i_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.4500100771 ampere but the right hand side evaluated to 585.788157983 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [v_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.5032821169 volt but the right hand side evaluated to 53.407285583 volt (Allowable error: 0.0001%, Actual error: 0.18%)

Warning: Constraint [i_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.3633038918 ampere but the right hand side evaluated to 585.031999194 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [v_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.3402923705 volt but the right hand side evaluated to 53.2512853383 volt (Allowable error: 0.0001%, Actual error: 0.17%)

Warning: Constraint [i_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.2759234571 ampere but the right hand side evaluated to 584.26877424 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [v_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.176522896 volt but the right hand side evaluated to 53.0942381681 volt (Allowable error: 0.0001%, Actual error: 0.15%)

Warning: Constraint [i_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.1881167553 ampere but the right hand side evaluated to 583.500678063 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [v_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.0119839364 volt but the right hand side evaluated to 52.9364697703 volt (Allowable error: 0.0001%, Actual error: 0.14%)

Warning: Constraint [i_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.0987250899 ampere but the right hand side evaluated to 582.708843335 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [v_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.8459987556 volt but the right hand side evaluated to 52.7764283374 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.0109892752 ampere but the right hand side evaluated to 581.949967358 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.6804806084 volt but the right hand side evaluated to 52.6184443408 volt (Allowable error: 0.0001%, Actual error: 0.12%)

Warning: Constraint [i_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.921369008 ampere but the right hand side evaluated to 581.164709833 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.513222761 volt but the right hand side evaluated to 52.4577946188 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.8316370588 ampere but the right hand side evaluated to 580.382208607 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.089%)

Warning: Constraint [v_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.3451349576 volt but the right hand side evaluated to 52.296827965 volt (Allowable error: 0.0001%, Actual error: 0.092%)

Warning: Constraint [i_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.7410046711 ampere but the right hand side evaluated to 579.590649238 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%)

Warning: Constraint [v_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.1757589972 volt but the right hand side evaluated to 52.1343212485 volt (Allowable error: 0.0001%, Actual error: 0.079%)

Warning: Constraint [i_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.6494762659 ampere but the right hand side evaluated to 578.788467673 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%)

Warning: Constraint [v_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.0049548698 volt but the right hand side evaluated to 51.9703421156 volt (Allowable error: 0.0001%, Actual error: 0.067%)

Warning: Constraint [i_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.5569957457 ampere but the right hand side evaluated to 577.977320074 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%)

Warning: Constraint [v_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.8326883777 volt but the right hand side evaluated to 51.8049058823 volt (Allowable error: 0.0001%, Actual error: 0.054%)

Warning: Constraint [i_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.4637492801 ampere but the right hand side evaluated to 577.161524313 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.039%)

Warning: Constraint [v_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.6589777792 volt but the right hand side evaluated to 51.6381352559 volt (Allowable error: 0.0001%, Actual error: 0.04%)

Warning: Constraint [i_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [A]... >= 9.55*i0_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.3694389958 ampere but the right hand side evaluated to 576.335238384 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [v_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [V]... >= Kv_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.4835840219 volt but the right hand side evaluated to 51.4696904586 volt (Allowable error: 0.0001%, Actual error: 0.027%)

Warning: Constraint [i_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.2741908698 ampere but the right hand side evaluated to 575.500644951 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%)

Warning: Constraint [v_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.3064256157 volt but the right hand side evaluated to 51.2994476997 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2427 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0274 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0428 but bound is 0.0500
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0)
Collecting git+https://github.com/hoburg/gpfit.git
  Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-X2dw_j
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-KjUjTB/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gplibrary
Requirement already satisfied: numpy>=1.12 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.8.1)
Building wheels for collected packages: gpkitmodels
  Running setup.py bdist_wheel for gpkitmodels: started
  Running setup.py bdist_wheel for gpkitmodels: finished with status 'done'
  Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-QTJ7AH/wheels/89/83/63/5c5e519ca7ad1fa93cf087f53642d88b5b0eb066ca83d4bb19
Successfully built gpkitmodels
Installing collected packages: gpkitmodels
  Found existing installation: gpkitmodels 0.0.0.0
    Uninstalling gpkitmodels-0.0.0.0:
      Successfully uninstalled gpkitmodels-0.0.0.0
Successfully installed gpkitmodels-0.0.0.0

Running tests...
----------------------------------------------------------------------
..........
----------------------------------------------------------------------
Ran 10 tests in 2.759s

OK

Generating XML reports...
adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py'
adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py'
adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py'
adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py'
adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.0121 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.0312 seconds.
Using solver 'mosek'
Solving for 8 variables.
Solving took 0.0149 seconds.
Using solver 'mosek'
Solving for 24 variables.
Solving took 0.0133 seconds.
Using solver 'mosek'
Solving for 24 variables.
Solving took 0.00947 seconds.
Using solver 'mosek_cli'
Solving for 8 variables.
Solving took 0.0303 seconds.
Using solver 'mosek_cli'
Solving for 24 variables.
Solving took 0.0305 seconds.
Using solver 'mosek_cli'
Solving for 24 variables.
Solving took 0.0313 seconds.
Using solver 'mosek'
Solving for 13 variables.
Solving took 0.0103 seconds.
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.0304 seconds.
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3838 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9776 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3883 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9590 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.6332 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.1579 but bound is 700000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Cloning into 'eVTOL'...

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 1.107s

OK

Generating XML reports...
adding test for 'aircraft_models.py'
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {})

calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {})

[Execution node] check if [macys] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/Users/jenkins/workspace/gplibrary_PR_Models/mosek' for the testing framework 'JUnit'.
[xUnit] [INFO] - Check 'Failed Tests' threshold.
[xUnit] [INFO] - Check 'Skipped Tests' threshold.
[xUnit] [INFO] - Setting the build status to SUCCESS
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: SUCCESS