Started by upstream project "gplibrary_PR_Models" build number 82 originally caused by: GitHub pull request #163 of commit 6bafbd37f740ef7d21bbc2bb53616c9907a54f86, no merge conflicts. Building remotely on macys_VM 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 8fdf4f479dee43fdda2db43d2466ee60671af827 (refs/remotes/origin/pr/163/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 8fdf4f479dee43fdda2db43d2466ee60671af827 # 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/outboardloads 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/163/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 199 remote branches > git show-ref --tags -d # timeout=10 Checking out Revision 8fdf4f479dee43fdda2db43d2466ee60671af827 (origin/pr/163/merge, origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f 8fdf4f479dee43fdda2db43d2466ee60671af827 # timeout=3 Commit message: "Merge 6bafbd37f740ef7d21bbc2bb53616c9907a54f86 into 37b19bb4ed498761eb51296a13946b1a52fa40aa" 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: PR 163: allow for outboard loads on wing as signomial model [Execution node] check if [macys_VM] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] enabling perform for step [Execute shell] [mosek] $ /bin/bash -xe /var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/jenkins3010117196740432217.sh + [[ macys_VM == *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_VM == *reynolds* ]] + [[ macys_VM == *macys* ]] + [[ mosek == mosek ]] + [[ macys_VM == 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/7/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/7/tools/platform/osx64x86/bin + export DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin + DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin + python /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/setup.py install running install running build running build_py running install_lib creating /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib/mosek/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib/mosek/array.py -> /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/mosek/fusion/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib/mosek/fusion/SolverInfo.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib/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/array.py to array.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/SolverInfo.py to SolverInfo.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_data copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosek64.7.1.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosekglb64.7.1.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libiomp5.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosekxx7_1.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../../../../license.pdf -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek running install_egg_info Writing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/Mosek-7.1.28-py2.7.egg-info Please review the MOSEK license conditions in license.pdf + [[ mosek == mosek ]] + python -c '__import__("mosek").Env()' + msktestlic Computer Platform : MACOSX/64-X86 Cores : 4 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. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator - tries : 0 time : 0.00 Eliminator - elim's : 0 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.01 ************************************ 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 pytz>=2011k (from pandas) Using cached https://files.pythonhosted.org/packages/dc/83/15f7833b70d3e067ca91467ca245bae0f6fe56ddc7451aa0dc5606b120f2/pytz-2018.4-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 python-dateutil (from pandas) Using cached https://files.pythonhosted.org/packages/0c/57/19f3a65bcf6d5be570ee8c35a5398496e10a0ddcbc95393b2d17f86aaaf8/python_dateutil-2.7.2-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: pytz, six, python-dateutil, 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 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: six>=1.10 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.11.0) Requirement not upgraded as not directly required: pytz in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2018.4) Collecting subprocess32 (from matplotlib) 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 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 Requirement not upgraded as not directly required: python-dateutil>=2.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2.7.2) 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: numpy>=1.7.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.14.2) 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: backports.functools-lru-cache, subprocess32, cycler, kiwisolver, 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/7/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 + 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 0.580s OK Generating XML reports... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.0202 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.0294 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.233 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: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) 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: 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: 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-jw_y6n 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-KraTQN/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: 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: 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: 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-tqmmXv/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 30.938s 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 0.437 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 1.06 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 1.1 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 1.1 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 0.437 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1496 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 131552.1345 but bound is 150000.0000 Beginning signomial solve. Solving took 4 GP solves and 2.07 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0581 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 134553.9086 but bound is 150000.0000 Using solver 'mosek_cli' Solving for 1250 variables. Solving took 0.292 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 2.32 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: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) 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: 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: 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-SN59Mk 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-nUtx9N/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Running tests... ---------------------------------------------------------------------- ..EE ====================================================================== ERROR [2.511s]: test_model_print_perf_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "print_perf.py", line 194, in test File "print_perf.py", line 42, in jho_subs File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/prog_factories.py", line 117, in solvefn self.program, progsolve = genfunction(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/prog_factories.py", line 74, in programify prog = program(self.cost, self, constants, **kwargs) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/sgp.py", line 64, in __init__ self._gp = self.init_gp(self.substitutions) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/sgp.py", line 185, in init_gp gp = GeometricProgram(self.cost, [gpconstrs, spapproxs], substitutions) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/gp.py", line 72, in __init__ self.posynomials.extend(self.as_posyslt1(self.substitutions)) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 254, in as_posyslt1 posys = constraint.as_posyslt1(substitutions) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 254, in as_posyslt1 posys = constraint.as_posyslt1(substitutions) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/nomials/math.py", line 471, in as_posyslt1 hmap = self._simplify_posy_ineq(hmap, self.pmap) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/nomials/math.py", line 428, in _simplify_posy_ineq scaled = hmap/coeff File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/small_classes.py", line 242, in __div__ def __div__(self, other): return self * other**-1 ZeroDivisionError: 0.0 cannot be raised to a negative power ====================================================================== ERROR [2.050s]: test_model_print_perf_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "print_perf.py", line 194, in test File "print_perf.py", line 42, in jho_subs File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/prog_factories.py", line 117, in solvefn self.program, progsolve = genfunction(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/prog_factories.py", line 74, in programify prog = program(self.cost, self, constants, **kwargs) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/sgp.py", line 64, in __init__ self._gp = self.init_gp(self.substitutions) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/sgp.py", line 185, in init_gp gp = GeometricProgram(self.cost, [gpconstrs, spapproxs], substitutions) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/gp.py", line 72, in __init__ self.posynomials.extend(self.as_posyslt1(self.substitutions)) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 254, in as_posyslt1 posys = constraint.as_posyslt1(substitutions) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 254, in as_posyslt1 posys = constraint.as_posyslt1(substitutions) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/nomials/math.py", line 471, in as_posyslt1 hmap = self._simplify_posy_ineq(hmap, self.pmap) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/nomials/math.py", line 428, in _simplify_posy_ineq scaled = hmap/coeff File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/small_classes.py", line 242, in __div__ def __div__(self, other): return self * other**-1 ZeroDivisionError: 0.0 cannot be raised to a negative power ---------------------------------------------------------------------- Ran 4 tests in 14.661s FAILED (errors=2) 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 -5.056415355864097e-14. Allowing negative dual variable(s) as small as -7.420149564230094e-14. Allowing negative dual variable(s) as small as -1.516178675664559e-13. Allowing negative dual variable(s) as small as -1.4828025959867652e-13. Solving took 4 GP solves and 1.71 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.1619732793772855e-14. Allowing negative dual variable(s) as small as -7.752349109879653e-14. Allowing negative dual variable(s) as small as -1.5216647386573356e-13. Allowing negative dual variable(s) as small as -1.4806818965373836e-13. Solving took 4 GP solves and 3.27 seconds. 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-It3k9e/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 2.085s 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 24184.7528315 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 26232.8485055 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Cloning into 'SPaircraft'... Checking out files: 50% (1740/3413) Checking out files: 51% (1741/3413) Checking out files: 52% (1775/3413) Checking out files: 53% (1809/3413) Checking out files: 54% (1844/3413) Checking out files: 55% (1878/3413) Checking out files: 56% (1912/3413) Checking out files: 57% (1946/3413) Checking out files: 58% (1980/3413) Checking out files: 59% (2014/3413) Checking out files: 60% (2048/3413) Checking out files: 61% (2082/3413) Checking out files: 62% (2117/3413) Checking out files: 63% (2151/3413) Checking out files: 64% (2185/3413) Checking out files: 65% (2219/3413) Checking out files: 66% (2253/3413) Checking out files: 67% (2287/3413) Checking out files: 68% (2321/3413) Checking out files: 69% (2355/3413) Checking out files: 70% (2390/3413) Checking out files: 71% (2424/3413) Checking out files: 72% (2458/3413) Checking out files: 73% (2492/3413) Checking out files: 74% (2526/3413) Checking out files: 75% (2560/3413) Checking out files: 76% (2594/3413) Checking out files: 77% (2629/3413) Checking out files: 78% (2663/3413) Checking out files: 79% (2697/3413) Checking out files: 80% (2731/3413) Checking out files: 81% (2765/3413) Checking out files: 82% (2799/3413) Checking out files: 83% (2833/3413) Checking out files: 84% (2867/3413) Checking out files: 85% (2902/3413) Checking out files: 86% (2936/3413) Checking out files: 87% (2970/3413) Checking out files: 88% (3004/3413) Checking out files: 89% (3038/3413) Checking out files: 90% (3072/3413) Checking out files: 91% (3106/3413) Checking out files: 92% (3140/3413) Checking out files: 93% (3175/3413) Checking out files: 94% (3209/3413) Checking out files: 95% (3243/3413) Checking out files: 96% (3277/3413) Checking out files: 97% (3311/3413) Checking out files: 98% (3345/3413) Checking out files: 99% (3379/3413) Checking out files: 100% (3413/3413) Checking out files: 100% (3413/3413), done. Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-_aFiUS 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-lpEItd/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 2519606.56222 force_pound * meter but the right hand side evaluated to 2468461.33701 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 32774.4756117 force_pound but the right hand side evaluated to 32399.9999975 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 2.21510116759 meter but the right hand side evaluated to 1.96396132332 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 48608.8413881 newton but the right hand side evaluated to 48529.6815143 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 49704.4438105 newton but the right hand side evaluated to 49411.2033392 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 18949.0365967 newton but the right hand side evaluated to 18923.0397308 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 16591.9652456 newton but the right hand side evaluated to 16565.7582438 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 1002815.08261 joule / kilogram but the right hand side evaluated to 1.15242976163 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 895044.579083 joule / kilogram but the right hand side evaluated to 0.897473435667 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 1072947.54364 joule / kilogram but the right hand side evaluated to 1.19571102416 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 596870.810348 joule / kilogram but the right hand side evaluated to 0.615557272354 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 786925.258516 joule / kilogram but the right hand side evaluated to 0.790364247369 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 18.346557348 meter but the right hand side evaluated to 16.3967795403 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 11.085407863900851 but the right hand side evaluated to 4.680789336285214 (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 9.791743186042297 but the right hand side evaluated to 4.680789326408168 (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 8.22913036771388 but the right hand side evaluated to 4.68078933924853 (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 18.4249289907 meter but the right hand side evaluated to 18.165987701 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 18.4249289907 meter but the right hand side evaluated to 18.2854627019 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 0.31012116523321875 but the right hand side evaluated to 0.19292691729434272 (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 0.2413401869468812 but the right hand side evaluated to 0.17650059118698422 (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 7.27504020974297 but the right hand side evaluated to 4.615986187530306 (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 7.453672108398209 but the right hand side evaluated to 4.646344842558556 (Allowable error: 0.1%, Actual error: 38%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, 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 2504976.75083 force_pound * meter but the right hand side evaluated to 2454470.89462 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 32774.4783745 force_pound but the right hand side evaluated to 32399.9999989 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 1.96383063148 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 982256.832234 joule / kilogram but the right hand side evaluated to 1.20547045144 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 1151137.28447 joule / kilogram but the right hand side evaluated to 1.88379405777 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 18.4111621663 meter but the right hand side evaluated to 16.4524816299 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 11.0893102979549 but the right hand side evaluated to 4.73132123921327 (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 9.749134518648415 but the right hand side evaluated to 4.731321232783405 (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 8.197834219487715 but the right hand side evaluated to 4.731321241514801 (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 18.4749969095 meter but the right hand side evaluated to 18.2223424735 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 18.4749969095 meter but the right hand side evaluated to 18.3384474228 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 0.3092783444797256 but the right hand side evaluated to 0.1927373490895374 (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 0.24173087287522588 but the right hand side evaluated to 0.17660065971822123 (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 7.430222937943862 but the right hand side evaluated to 4.666980951319695 (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 7.495475509880335 but the right hand side evaluated to 4.696716951940968 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, 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 2481461.51054 force_pound * meter but the right hand side evaluated to 2426090.61143 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 32774.4091412 force_pound but the right hand side evaluated to 32399.999997 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 2.21510116707 meter but the right hand side evaluated to 1.83120391143 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 1203378.23693 joule / kilogram but the right hand side evaluated to 1.66380050972 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 18.4693761959 meter but the right hand side evaluated to 16.6431978333 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 11.04730498884324 but the right hand side evaluated to 4.801803566087215 (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 9.670705909557114 but the right hand side evaluated to 4.80180354531174 (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 8.221371713796733 but the right hand side evaluated to 4.801803572204604 (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 18.6280035479 meter but the right hand side evaluated to 18.3449809689 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 18.6280035479 meter but the right hand side evaluated to 18.474386395 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 0.32683244548894397 but the right hand side evaluated to 0.19660245937319898 (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 0.2527498394985086 but the right hand side evaluated to 0.17938776363286904 (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 7.455615367301998 but the right hand side evaluated to 4.729216256770905 (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 7.548871651032211 but the right hand side evaluated to 4.76257613028213 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, 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 2455568.19465 force_pound * meter but the right hand side evaluated to 2407712.19525 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 32774.4966674 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 2.21510116797 meter but the right hand side evaluated to 1.99552199589 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 1227633.95227 joule / kilogram but the right hand side evaluated to 1.7235977753 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 677538.879785 joule / kilogram but the right hand side evaluated to 0.679181892338 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 18.4156358458 meter but the right hand side evaluated to 16.4239724483 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 10.97496954481445 but the right hand side evaluated to 4.762554466176616 (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 9.752896284190143 but the right hand side evaluated to 4.762554458860579 (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 8.158718141958266 but the right hand side evaluated to 4.762554468277634 (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 18.4488724557 meter but the right hand side evaluated to 18.2046630379 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 18.4488724557 meter but the right hand side evaluated to 18.3176180665 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 0.30594651836530584 but the right hand side evaluated to 0.19198931056149063 (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 0.23933836127973596 but the right hand side evaluated to 0.17598581422782253 (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 7.504818966330191 but the right hand side evaluated to 4.699783251052042 (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 7.527658763069801 but the right hand side evaluated to 4.728944139680945 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, 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 2436784.1609 force_pound * meter but the right hand side evaluated to 2390898.57208 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 32774.4741047 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 2.21510116784 meter but the right hand side evaluated to 2.03200908366 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 1233974.86293 joule / kilogram but the right hand side evaluated to 1.62325437459 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 18.4095785527 meter but the right hand side evaluated to 16.3813542463 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 10.931049014591634 but the right hand side evaluated to 4.787719068020463 (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 9.873362086811458 but the right hand side evaluated to 4.787719057277042 (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 8.154647809695605 but the right hand side evaluated to 4.787719070832131 (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 18.4102738788 meter but the right hand side evaluated to 18.1746831248 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 18.4102738788 meter but the right hand side evaluated to 18.283935351 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 0.3020986209705674 but the right hand side evaluated to 0.19112006217677308 (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 0.23685672975785454 but the right hand side evaluated to 0.175345522106162 (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 7.5364847541487165 but the right hand side evaluated to 4.726722915156063 (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 7.551398048753193 but the right hand side evaluated to 4.7551363404634195 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, 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 2418322.87599 force_pound * meter but the right hand side evaluated to 2374882.80455 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 32774.5084544 force_pound but the right hand side evaluated to 32399.9999986 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 2.21510116794 meter but the right hand side evaluated to 2.08236023975 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 1244507.18286 joule / kilogram but the right hand side evaluated to 1.55927511186 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 664750.47317 joule / kilogram but the right hand side evaluated to 0.667401941093 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 18.4000456011 meter but the right hand side evaluated to 16.3223714557 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 10.904037371503438 but the right hand side evaluated to 4.78950132922429 (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 10.025979467462061 but the right hand side evaluated to 4.7895013210165684 (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 8.145554220610295 but the right hand side evaluated to 4.789501331461809 (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 18.3617938272 meter but the right hand side evaluated to 18.1374255955 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 18.3617938272 meter but the right hand side evaluated to 18.2416829548 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 0.2959606150547378 but the right hand side evaluated to 0.18972165985521183 (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 0.23297745066179854 but the right hand side evaluated to 0.17433530042523207 (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 7.565345546865313 but the right hand side evaluated to 4.731316270081677 (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 7.583815800371385 but the right hand side evaluated to 4.758512772558373 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, 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 2405739.63372 force_pound * meter but the right hand side evaluated to 2358168.95232 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 32774.4119756 force_pound but the right hand side evaluated to 32399.999999 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 2.21510116804 meter but the right hand side evaluated to 1.97488690017 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 1245746.8916 joule / kilogram but the right hand side evaluated to 1.35772679887 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 18.4441416281 meter but the right hand side evaluated to 16.4750075361 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 10.933120269654632 but the right hand side evaluated to 4.831718244294948 (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 10.192142764582261 but the right hand side evaluated to 4.831718222339775 (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 8.195663667288033 but the right hand side evaluated to 4.831718248685207 (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 18.4861550353 meter but the right hand side evaluated to 18.2368701895 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 18.4861550353 meter but the right hand side evaluated to 18.35188597 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 0.31020514694112666 but the right hand side evaluated to 0.19294249082643777 (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 0.2419170658417853 but the right hand side evaluated to 0.17664717524222398 (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 7.54212841135738 but the right hand side evaluated to 4.766977618497954 (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 7.597030205610187 but the right hand side evaluated to 4.7970418590223725 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, 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 2391779.51268 force_pound * meter but the right hand side evaluated to 2346059.55829 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 32774.4434296 force_pound but the right hand side evaluated to 32399.9999982 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 2.21510116791 meter but the right hand side evaluated to 2.01208169978 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 1263254.66348 joule / kilogram but the right hand side evaluated to 1.32933804756 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 643003.223572 joule / kilogram but the right hand side evaluated to 0.644587831314 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 18.4391893726 meter but the right hand side evaluated to 16.4333028118 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 10.927057883629846 but the right hand side evaluated to 4.82709667414511 (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 10.332848249835624 but the right hand side evaluated to 4.827096635059693 (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 8.188196474665526 but the right hand side evaluated to 4.827096683625121 (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 18.4531710491 meter but the right hand side evaluated to 18.2123800026 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 18.4531710491 meter but the right hand side evaluated to 18.323733798 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 0.30544736957250507 but the right hand side evaluated to 0.19187568202687236 (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 0.23886134947182036 but the right hand side evaluated to 0.1758633652918478 (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 7.554288638982111 but the right hand side evaluated to 4.764561587837514 (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. ---------------------------------------------------------------------- Ran 1 test in 105.912s OK Generating XML reports... **-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.617831508091317 but the right hand side evaluated to 4.793692981752532 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, 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 2376282.43517 force_pound * meter but the right hand side evaluated to 2334599.94935 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 32774.5308674 force_pound but the right hand side evaluated to 32399.9999973 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 2.21510116784 meter but the right hand side evaluated to 2.09817119365 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 1283641.37455 joule / kilogram but the right hand side evaluated to 1.28936178741 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.24%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.414602487 meter but the right hand side evaluated to 16.3183436598 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 10.93746451216431 but the right hand side evaluated to 4.824378739604941 (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 10.571345714697655 but the right hand side evaluated to 4.824378722248551 (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 8.193851420982073 but the right hand side evaluated to 4.824378744168766 (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 18.3565607078 meter but the right hand side evaluated to 18.1377569313 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 18.3565607078 meter but the right hand side evaluated to 18.2401787874 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 0.29417355639424336 but the right hand side evaluated to 0.18931107841489261 (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 0.23165736112078594 but the right hand side evaluated to 0.17398933627492538 (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 7.620070880953319 but the right hand side evaluated to 4.767019838578083 (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 7.689392199536182 but the right hand side evaluated to 4.793938658918669 (Allowable error: 0.1%, Actual error: 38%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Sweeping took 101 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: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) 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: 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: 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-WYPSRP 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-SRtSbr/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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-JJPq1T 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: 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: 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: 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-VKEH86/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: 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: 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: 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-haj8fg/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 9073 variables. Solving took 0.999 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 1.3000 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 796269.5142 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 0.1885 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 0.0315 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 0.0352 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 65.7609017096 ampere but the right hand side evaluated to 616.348263251 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 65.6904109454 ampere but the right hand side evaluated to 616.348264004 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 65.5943357688 ampere but the right hand side evaluated to 616.348264697 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) 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 65.4468190006 ampere but the right hand side evaluated to 616.348265441 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 65.2157690776 ampere but the right hand side evaluated to 616.348266444 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 40.8361586359 volt but the right hand side evaluated to 40.0442879191 volt (Allowable error: 0.0001%, Actual error: 2%) 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 40.7564348896 volt but the right hand side evaluated to 40.0109036572 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 40.635781141 volt but the right hand side evaluated to 39.9534918093 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 40.448554609 volt but the right hand side evaluated to 39.8631073942 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 40.1471961073 volt but the right hand side evaluated to 39.7128060087 volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 48.4046154955 ampere but the right hand side evaluated to 462.161167206 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 32.6524096128 volt but the right hand side evaluated to 32.6473080451 volt (Allowable error: 0.0001%, Actual error: 0.016%) 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 48.3769642648 ampere but the right hand side evaluated to 461.909921942 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 32.63575881 volt but the right hand side evaluated to 32.631605509 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 48.4032795244 ampere but the right hand side evaluated to 462.149017024 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 32.6515910647 volt but the right hand side evaluated to 32.6465344771 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 48.3789832811 ampere but the right hand side evaluated to 461.928266061 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 32.6369786775 volt but the right hand side evaluated to 32.6327560477 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 48.4012498113 ampere but the right hand side evaluated to 462.130568614 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) 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 32.6503642976 volt but the right hand side evaluated to 32.6453768616 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 48.3803082032 ampere but the right hand side evaluated to 461.940308259 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 32.6377856227 volt but the right hand side evaluated to 32.6335178201 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 48.3985172409 ampere but the right hand side evaluated to 462.105746036 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 32.6487339683 volt but the right hand side evaluated to 32.6438406903 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 48.380939144 ampere but the right hand side evaluated to 461.946048328 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6381782987 volt but the right hand side evaluated to 32.6338893895 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 48.3950984445 ampere but the right hand side evaluated to 462.074682548 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 32.6466805936 volt but the right hand side evaluated to 32.6419045909 volt (Allowable error: 0.0001%, Actual error: 0.015%) 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 48.380898589 ampere but the right hand side evaluated to 461.945667591 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6381342527 volt but the right hand side evaluated to 32.6338458175 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 48.3909894762 ampere but the right hand side evaluated to 462.03734337 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) 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 32.6442015642 volt but the right hand side evaluated to 32.6395661565 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 48.3801489446 ampere but the right hand side evaluated to 461.938857184 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 32.6376827447 volt but the right hand side evaluated to 32.6334200878 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 48.386167682 ampere but the right hand side evaluated to 461.993540229 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 32.6413095277 volt but the right hand side evaluated to 32.6368401305 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 48.3786947387 ampere but the right hand side evaluated to 461.925650979 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 32.6368145644 volt but the right hand side evaluated to 32.6326022911 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 48.3806474169 ampere but the right hand side evaluated to 461.943386112 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6379829398 volt but the right hand side evaluated to 32.633703178 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 48.3765501383 ampere but the right hand side evaluated to 461.906160766 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 32.6355106244 volt but the right hand side evaluated to 32.6313715967 volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 48.3744178693 ampere but the right hand side evaluated to 461.886788132 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 32.6342211792 volt but the right hand side evaluated to 32.6301554488 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 48.3736856142 ampere but the right hand side evaluated to 461.880141361 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 32.6337890345 volt but the right hand side evaluated to 32.6297488579 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 48.3674731487 ampere but the right hand side evaluated to 461.823692832 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 32.6300178149 volt but the right hand side evaluated to 32.6261907229 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 48.3701154061 ampere but the right hand side evaluated to 461.847704047 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 32.6316278792 volt but the right hand side evaluated to 32.6277103152 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 48.3597952396 ampere but the right hand side evaluated to 461.753947187 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 32.6253756156 volt but the right hand side evaluated to 32.6218131759 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 48.3658282205 ampere but the right hand side evaluated to 461.808750818 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 32.6290263126 volt but the right hand side evaluated to 32.6252558569 volt (Allowable error: 0.0001%, Actual error: 0.012%) 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 48.3513933167 ampere but the right hand side evaluated to 461.677619476 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0096%) 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 32.6202720845 volt but the right hand side evaluated to 32.6169988935 volt (Allowable error: 0.0001%, Actual error: 0.01%) 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 48.3608116927 ampere but the right hand side evaluated to 461.763174784 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) 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 32.6259830461 volt but the right hand side evaluated to 32.622385052 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 48.3422496438 ampere but the right hand side evaluated to 461.594557363 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 32.6147065655 volt but the right hand side evaluated to 32.6117484806 volt (Allowable error: 0.0001%, Actual error: 0.0091%) 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 48.3550606921 ampere but the right hand side evaluated to 461.710926977 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0099%) 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 32.6224887738 volt but the right hand side evaluated to 32.6190885543 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 48.3323632402 ampere but the right hand side evaluated to 461.504744829 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0077%) 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 32.608662283 volt but the right hand side evaluated to 32.6060446681 volt (Allowable error: 0.0001%, Actual error: 0.008%) 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 48.3485650602 ampere but the right hand side evaluated to 461.651916772 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0093%) 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 32.6185371573 volt but the right hand side evaluated to 32.615360529 volt (Allowable error: 0.0001%, Actual error: 0.0097%) 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 48.3217179594 ampere but the right hand side evaluated to 461.408041642 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0066%) 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 32.602134073 volt but the right hand side evaluated to 32.5998833559 volt (Allowable error: 0.0001%, Actual error: 0.0069%) 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 48.3413166213 ampere but the right hand side evaluated to 461.586069215 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%) 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 32.6141185152 volt but the right hand side evaluated to 32.6111915285 volt (Allowable error: 0.0001%, Actual error: 0.009%) 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 48.3103027869 ampere but the right hand side evaluated to 461.304348367 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 32.5951105442 volt but the right hand side evaluated to 32.5932535604 volt (Allowable error: 0.0001%, Actual error: 0.0057%) 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 48.3333047086 ampere but the right hand side evaluated to 461.513288146 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0078%) 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 32.6092236529 volt but the right hand side evaluated to 32.6065727894 volt (Allowable error: 0.0001%, Actual error: 0.0081%) 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 48.2980788001 ampere but the right hand side evaluated to 461.193337383 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 32.5876030595 volt but the right hand side evaluated to 32.5861699036 volt (Allowable error: 0.0001%, Actual error: 0.0044%) 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 48.3245093367 ampere but the right hand side evaluated to 461.433400089 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0069%) 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 32.6038496534 volt but the right hand side evaluated to 32.6015026779 volt (Allowable error: 0.0001%, Actual error: 0.0072%) 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 48.2850814122 ampere but the right hand side evaluated to 461.07528607 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 32.5795555717 volt but the right hand side evaluated to 32.5785718481 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 48.3149458936 ampere but the right hand side evaluated to 461.346520539 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0059%) 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 32.5979611413 volt but the right hand side evaluated to 32.5959435181 volt (Allowable error: 0.0001%, Actual error: 0.0062%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 but bound is 0.1460 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 48.2712742759 ampere but the right hand side evaluated to 460.949885971 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 32.5709732914 volt but the right hand side evaluated to 32.5704674369 volt (Allowable error: 0.0001%, Actual error: 0.0016%) 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 48.304560003 ampere but the right hand side evaluated to 461.252193227 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0049%) 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 32.5915815395 volt but the right hand side evaluated to 32.5899233561 volt (Allowable error: 0.0001%, Actual error: 0.0051%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 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 0.0315 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 0.0352 but bound is 0.0500 Warning: Constraint [i_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.2933619936 ampere but the right hand side evaluated to 461.150490077 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0037%) Warning: Constraint [v_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5846757674 volt but the right hand side evaluated to 32.5834051401 volt (Allowable error: 0.0001%, Actual error: 0.0039%) Using solver 'mosek' Solving for 9073 variables. Solving took 1 seconds. 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 1.2824 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 882794.0257 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 0.1991 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 0.0328 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 0.0367 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 83.6080372155 ampere but the right hand side evaluated to 779.784421877 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.4%) 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 83.5014388249 ampere but the right hand side evaluated to 779.784421879 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.3%) 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 83.3556258341 ampere but the right hand side evaluated to 779.784421882 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.1%) 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 83.131017899 ampere but the right hand side evaluated to 779.784421884 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 82.7772083695 ampere but the right hand side evaluated to 779.784421887 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 38.5656642153 volt but the right hand side evaluated to 37.5903670752 volt (Allowable error: 0.0001%, Actual error: 2.6%) 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 38.4803274104 volt but the right hand side evaluated to 37.5596507386 volt (Allowable error: 0.0001%, Actual error: 2.5%) 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 38.352203609 volt but the right hand side evaluated to 37.506247986 volt (Allowable error: 0.0001%, Actual error: 2.3%) 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 38.1536494194 volt but the right hand side evaluated to 37.422231691 volt (Allowable error: 0.0001%, Actual error: 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 37.8404936935 volt but the right hand side evaluated to 37.2880133319 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 55.5628688524 ampere but the right hand side evaluated to 529.982815235 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 34.8025361253 volt but the right hand side evaluated to 34.7608973997 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 55.5201182228 ampere but the right hand side evaluated to 529.58274074 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 34.8073529866 volt but the right hand side evaluated to 34.7662418453 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 55.4304651415 ampere but the right hand side evaluated to 528.741145265 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 34.813319591 volt but the right hand side evaluated to 34.7731432105 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 55.3851023681 ampere but the right hand side evaluated to 528.320762202 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 34.8260335791 volt but the right hand side evaluated to 34.7866978695 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 55.2808645004 ampere but the right hand side evaluated to 527.343085046 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 34.8352980497 volt but the right hand side evaluated to 34.7971111932 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 55.2476782594 ampere but the right hand side evaluated to 527.035753509 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) 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 34.8455229011 volt but the right hand side evaluated to 34.8079681394 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 55.1184390112 ampere but the right hand side evaluated to 525.827357423 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) 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 34.8653662944 volt but the right hand side evaluated to 34.8294999564 volt (Allowable error: 0.0001%, Actual error: 0.1%) 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 55.1068943845 ampere but the right hand side evaluated to 525.719015308 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) 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 34.86645136 volt but the right hand side evaluated to 34.8307091973 volt (Allowable error: 0.0001%, Actual error: 0.1%) 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 54.9630144135 ampere but the right hand side evaluated to 524.373339609 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 34.8896176137 volt but the right hand side evaluated to 34.8557390751 volt (Allowable error: 0.0001%, Actual error: 0.097%) 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 54.9614373307 ampere but the right hand side evaluated to 524.358498001 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 34.8897010772 volt but the right hand side evaluated to 34.8558367963 volt (Allowable error: 0.0001%, Actual error: 0.097%) 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 54.8028331569 ampere but the right hand side evaluated to 522.87448891 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) 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 34.9162372887 volt but the right hand side evaluated to 34.8843967611 volt (Allowable error: 0.0001%, Actual error: 0.091%) 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 54.8140304315 ampere but the right hand side evaluated to 522.978795707 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) 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 34.9133304441 volt but the right hand side evaluated to 34.8813150612 volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 54.6389979629 ampere but the right hand side evaluated to 521.340661529 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 34.944414427 volt but the right hand side evaluated to 34.9146173732 volt (Allowable error: 0.0001%, Actual error: 0.085%) 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 54.6606000956 ampere but the right hand side evaluated to 521.542718457 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.082%) 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 34.9401492967 volt but the right hand side evaluated to 34.910069561 volt (Allowable error: 0.0001%, Actual error: 0.086%) 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 54.4703608938 ampere but the right hand side evaluated to 519.761221983 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 34.9749102114 volt but the right hand side evaluated to 34.9471847378 volt (Allowable error: 0.0001%, Actual error: 0.079%) 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 54.5043507523 ampere but the right hand side evaluated to 520.07928812 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%) 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 34.9678789429 volt but the right hand side evaluated to 34.9397155846 volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 54.2965318489 ampere but the right hand side evaluated to 518.132391598 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.07%) 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 35.0079557764 volt but the right hand side evaluated to 34.9823271014 volt (Allowable error: 0.0001%, Actual error: 0.073%) 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 54.3429213758 ampere but the right hand side evaluated to 518.566800222 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.071%) 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 34.9981297954 volt but the right hand side evaluated to 34.9719211346 volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 54.1167841487 ampere but the right hand side evaluated to 516.447268853 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%) 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 35.0440169255 volt but the right hand side evaluated to 35.0205136758 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 54.175163943 ampere but the right hand side evaluated to 516.994503529 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%) 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 35.0316636982 volt but the right hand side evaluated to 35.0074634787 volt (Allowable error: 0.0001%, Actual error: 0.069%) 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 53.9297957258 ampere but the right hand side evaluated to 514.693409433 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.058%) 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 35.0839754731 volt but the right hand side evaluated to 35.0626397295 volt (Allowable error: 0.0001%, Actual error: 0.061%) 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 54.0017238808 ampere but the right hand side evaluated to 515.368052004 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.06%) 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 35.0679888391 volt but the right hand side evaluated to 35.045816835 volt (Allowable error: 0.0001%, Actual error: 0.063%) 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 53.7347583805 ampere but the right hand side evaluated to 512.862995037 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%) 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 35.1283548142 volt but the right hand side evaluated to 35.1092229771 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 53.8210919437 ampere but the right hand side evaluated to 513.673286154 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%) 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 35.1081190104 volt but the right hand side evaluated to 35.0880133437 volt (Allowable error: 0.0001%, Actual error: 0.057%) 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 53.5310556616 ampere but the right hand side evaluated to 510.949906026 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.046%) 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 35.1775456556 volt but the right hand side evaluated to 35.1606391926 volt (Allowable error: 0.0001%, Actual error: 0.048%) 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 53.6327587841 ampere but the right hand side evaluated to 511.905158744 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.049%) 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 35.1523696628 volt but the right hand side evaluated to 35.1343568655 volt (Allowable error: 0.0001%, Actual error: 0.051%) 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 53.3149899689 ampere but the right hand side evaluated to 508.919369274 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.04%) 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 35.2340962431 volt but the right hand side evaluated to 35.2194758085 volt (Allowable error: 0.0001%, Actual error: 0.042%) 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 53.4345890131 ampere but the right hand side evaluated to 510.043508821 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.043%) 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 35.2021943806 volt but the right hand side evaluated to 35.186318369 volt (Allowable error: 0.0001%, Actual error: 0.045%) 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 53.0851278449 ampere but the right hand side evaluated to 506.757294723 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 35.298977821 volt but the right hand side evaluated to 35.2866779904 volt (Allowable error: 0.0001%, Actual error: 0.035%) 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 53.2248050406 ampere but the right hand side evaluated to 508.071294126 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 35.2587999977 volt but the right hand side evaluated to 35.245101642 volt (Allowable error: 0.0001%, Actual error: 0.039%) 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 52.8369670464 ampere but the right hand side evaluated to 504.420770161 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%) 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 35.3753203217 volt but the right hand side evaluated to 35.3653838851 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 53.0005053035 ampere but the right hand side evaluated to 505.960814231 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 35.3241860382 volt but the right hand side evaluated to 35.3127087493 volt (Allowable error: 0.0001%, Actual error: 0.033%) 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 52.5632836852 ampere but the right hand side evaluated to 501.840827179 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 35.4681843338 volt but the right hand side evaluated to 35.4606585279 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 52.7576495222 ampere but the right hand side evaluated to 503.673399263 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 35.4011612 volt but the right hand side evaluated to 35.3919446141 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 52.2506648943 ampere but the right hand side evaluated to 498.88928597 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) 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 35.5870251383 volt but the right hand side evaluated to 35.5819550902 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 52.4886908764 ampere but the right hand side evaluated to 501.136999856 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.019%) 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 35.4950156461 volt but the right hand side evaluated to 35.4881039244 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 51.8637384454 ampere but the right hand side evaluated to 495.228311707 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 35.7568825314 volt but the right hand side evaluated to 35.7543173931 volt (Allowable error: 0.0001%, Actual error: 0.0072%) 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 52.1782945094 ampere but the right hand side evaluated to 498.205220675 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 35.6165612887 volt but the right hand side evaluated to 35.6120065154 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 0.1991 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 0.0328 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 0.0367 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 0.1991 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 0.0328 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 0.0367 but bound is 0.0500 Using solver 'mosek' Solving for 9073 variables. Solving took 1.34 seconds. 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 1.2351 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 988744.2777 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 0.2106 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 0.0340 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 0.0369 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 99.8053540779 ampere but the right hand side evaluated to 936.51344194 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 99.7125486648 ampere but the right hand side evaluated to 936.513441944 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 99.5866017827 ampere but the right hand side evaluated to 936.513441948 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 99.393966426 ampere but the right hand side evaluated to 936.513441951 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_(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 99.0931198106 ampere but the right hand side evaluated to 936.513441957 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 38.2500456818 volt but the right hand side evaluated to 37.5140776605 volt (Allowable error: 0.0001%, Actual error: 2%) 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 38.1813199969 volt but the right hand side evaluated to 37.4858746086 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 38.0772405805 volt but the right hand side evaluated to 37.4367683767 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 37.9163431908 volt but the right hand side evaluated to 37.3595020972 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 37.6635826988 volt but the right hand side evaluated to 37.2361682408 volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 65.8563782068 ampere but the right hand side evaluated to 627.639745018 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 35.0192122559 volt but the right hand side evaluated to 34.9457457739 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 65.8481441844 ampere but the right hand side evaluated to 627.560050003 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 35.017843742 volt but the right hand side evaluated to 34.9443083468 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 65.5672930912 ampere but the right hand side evaluated to 624.94645497 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 35.0396440362 volt but the right hand side evaluated to 34.9698307724 volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 65.5697093222 ampere but the right hand side evaluated to 624.964253894 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 35.0363415016 volt but the right hand side evaluated to 34.9662235214 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 65.2735233524 ampere but the right hand side evaluated to 622.210963091 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 35.0629121004 volt but the right hand side evaluated to 34.9969280472 volt (Allowable error: 0.0001%, Actual error: 0.19%) 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 65.2863965493 ampere but the right hand side evaluated to 622.324921222 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 35.0577684995 volt but the right hand side evaluated to 34.9912703385 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 64.9803461322 ampere but the right hand side evaluated to 619.476482101 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 35.0852782644 volt but the right hand side evaluated to 35.022883974 volt (Allowable error: 0.0001%, Actual error: 0.18%) 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 65.0010349203 ampere but the right hand side evaluated to 619.664281146 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 35.0799970549 volt but the right hand side evaluated to 35.0170447717 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 64.6877736423 ampere but the right hand side evaluated to 616.744353966 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 35.106796224 volt but the right hand side evaluated to 35.0478221245 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 64.7130619122 ampere but the right hand side evaluated to 616.978755994 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 35.103489926 volt but the right hand side evaluated to 35.0441161602 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 64.38525422 ampere but the right hand side evaluated to 613.923905838 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 35.1343488895 volt but the right hand side evaluated to 35.0792150822 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 64.4227214695 ampere but the right hand side evaluated to 614.269428774 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 35.127909586 volt but the right hand side evaluated to 35.0720730519 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 64.0818756658 ampere but the right hand side evaluated to 611.092058793 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 35.161777708 volt but the right hand side evaluated to 35.1103288462 volt (Allowable error: 0.0001%, Actual error: 0.15%) 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 64.1264221239 ampere but the right hand side evaluated to 611.505296991 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 35.1555649338 volt but the right hand side evaluated to 35.1034190104 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 63.7763469156 ampere but the right hand side evaluated to 608.237766568 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 35.1898728886 volt but the right hand side evaluated to 35.1420280734 volt (Allowable error: 0.0001%, Actual error: 0.14%) 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 63.8268254331 ampere but the right hand side evaluated to 608.708787563 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 35.1846038234 volt but the right hand side evaluated to 35.1361277298 volt (Allowable error: 0.0001%, Actual error: 0.14%) 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 63.4630127188 ampere but the right hand side evaluated to 605.311664189 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 35.2222739796 volt but the right hand side evaluated to 35.1782289784 volt (Allowable error: 0.0001%, Actual error: 0.13%) 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 63.5247002325 ampere but the right hand side evaluated to 605.886304888 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 35.2144334959 volt but the right hand side evaluated to 35.1695506845 volt (Allowable error: 0.0001%, Actual error: 0.13%) 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 63.1455122176 ampere but the right hand side evaluated to 602.344766113 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 35.2564860933 volt but the right hand side evaluated to 35.2162162632 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 63.2148261046 ampere but the right hand side evaluated to 602.992086415 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 35.2484044248 volt but the right hand side evaluated to 35.2072835827 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 62.8221042063 ampere but the right hand side evaluated to 599.321435791 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 35.2935627419 volt but the right hand side evaluated to 35.2571039558 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 62.9011789286 ampere but the right hand side evaluated to 600.060261852 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 35.2838073677 volt but the right hand side evaluated to 35.2463889879 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 62.49258235 ampere but the right hand side evaluated to 596.239334544 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 35.3335466353 volt but the right hand side evaluated to 35.3009140917 volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 62.5797175049 ampere but the right hand side evaluated to 597.054947796 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 35.3232069464 volt but the right hand side evaluated to 35.2895964737 volt (Allowable error: 0.0001%, Actual error: 0.095%) 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 62.1578714444 ampere but the right hand side evaluated to 593.106144896 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 35.3757402277 volt but the right hand side evaluated to 35.3468798826 volt (Allowable error: 0.0001%, Actual error: 0.082%) 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 62.2517755114 ampere but the right hand side evaluated to 593.98722725 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 35.3656332554 volt but the right hand side evaluated to 35.3358380058 volt (Allowable error: 0.0001%, Actual error: 0.084%) 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 61.8068082003 ampere but the right hand side evaluated to 589.821942023 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 35.4273431972 volt but the right hand side evaluated to 35.4026162798 volt (Allowable error: 0.0001%, Actual error: 0.07%) 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 61.9157603925 ampere but the right hand side evaluated to 590.842384316 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 35.4120357241 volt but the right hand side evaluated to 35.3860950574 volt (Allowable error: 0.0001%, Actual error: 0.073%) 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 61.4495518327 ampere but the right hand side evaluated to 586.475982378 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 35.4816170808 volt but the right hand side evaluated to 35.4609094058 volt (Allowable error: 0.0001%, Actual error: 0.058%) 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 61.5712689781 ampere but the right hand side evaluated to 587.616101199 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 35.4625835563 volt but the right hand side evaluated to 35.4405101838 volt (Allowable error: 0.0001%, Actual error: 0.062%) 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 61.0866128746 ampere but the right hand side evaluated to 583.072399236 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 35.5381394514 volt but the right hand side evaluated to 35.5212889738 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 61.2164443739 ampere but the right hand side evaluated to 584.290944973 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.048%) 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 35.5183935631 volt but the right hand side evaluated to 35.5002213618 volt (Allowable error: 0.0001%, Actual error: 0.051%) 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 60.7005659501 ampere but the right hand side evaluated to 579.45311831 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 35.6081656985 volt but the right hand side evaluated to 35.5955412047 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 60.8482256065 ampere but the right hand side evaluated to 580.838302787 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 35.5813633608 volt but the right hand side evaluated to 35.5671689232 volt (Allowable error: 0.0001%, Actual error: 0.04%) 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 60.3007073661 ampere but the right hand side evaluated to 575.699953345 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.022%) 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 35.6855316311 volt but the right hand side evaluated to 35.6770669851 volt (Allowable error: 0.0001%, Actual error: 0.024%) 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 60.4639038598 ampere but the right hand side evaluated to 577.232196746 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 35.6531538015 volt but the right hand side evaluated to 35.643012074 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 59.8791523546 ampere but the right hand side evaluated to 571.739186273 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 35.7752543114 volt but the right hand side evaluated to 35.77098963 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 60.0608406577 ampere but the right hand side evaluated to 573.446732587 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 35.7353723558 volt but the right hand side evaluated to 35.7293194771 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 0.2106 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 0.0340 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 0.0369 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 59.6316108267 ampere but the right hand side evaluated to 569.411378994 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 35.8327102812 volt but the right hand side evaluated to 35.8308145469 volt (Allowable error: 0.0001%, Actual error: 0.0053%) Using solver 'mosek' Solving for 4713 variables. Solving took 0.446 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 1.2058 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 1064456.8435 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 0.2186 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 0.0349 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 0.0382 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 111.917810937 ampere but the right hand side evaluated to 1056.06638275 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.846541433 ampere but the right hand side evaluated to 1056.06638277 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.750519171 ampere but the right hand side evaluated to 1056.06638278 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 111.604592316 ampere but the right hand side evaluated to 1056.0663828 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.378510914 ampere but the right hand side evaluated to 1056.06638281 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.2100219601 volt but the right hand side evaluated to 37.7037019608 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1552399723 volt but the right hand side evaluated to 37.6768755119 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.0707772069 volt but the right hand side evaluated to 37.6300627082 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.9401426021 volt but the right hand side evaluated to 37.5563497155 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7350477719 volt but the right hand side evaluated to 37.4386740011 volt (Allowable error: 0.0001%, Actual error: 0.79%) 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 73.3931430751 ampere but the right hand side evaluated to 699.262983075 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 35.247563952 volt but the right hand side evaluated to 35.16204285 volt (Allowable error: 0.0001%, Actual error: 0.24%) 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 73.0289068891 ampere but the right hand side evaluated to 695.876997884 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 35.2658447159 volt but the right hand side evaluated to 35.1848752097 volt (Allowable error: 0.0001%, Actual error: 0.23%) 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 72.6669905258 ampere but the right hand side evaluated to 692.506062974 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 35.2825858447 volt but the right hand side evaluated to 35.2058333424 volt (Allowable error: 0.0001%, Actual error: 0.22%) 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 72.3031334661 ampere but the right hand side evaluated to 689.116222419 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 35.3004820476 volt but the right hand side evaluated to 35.227964567 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 71.9369652958 ampere but the right hand side evaluated to 685.704039443 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 35.3196517642 volt but the right hand side evaluated to 35.251393353 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 71.569997088 ampere but the right hand side evaluated to 682.281353568 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 35.3389916788 volt but the right hand side evaluated to 35.2748777676 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 71.1963091918 ampere but the right hand side evaluated to 678.799486996 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 35.3622193191 volt but the right hand side evaluated to 35.3025589872 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 70.8211724755 ampere but the right hand side evaluated to 675.300821735 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 35.3857902154 volt but the right hand side evaluated to 35.3304654653 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 70.4426773243 ampere but the right hand side evaluated to 671.769310418 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 35.4108202302 volt but the right hand side evaluated to 35.3598315209 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 70.0648674858 ampere but the right hand side evaluated to 668.23828204 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 35.4345997987 volt but the right hand side evaluated to 35.38765626 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 69.6718345636 ampere but the right hand side evaluated to 664.574168494 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 35.4671819173 volt but the right hand side evaluated to 35.4250082557 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 69.2794492444 ampere but the right hand side evaluated to 660.909012207 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 35.4982832073 volt but the right hand side evaluated to 35.4605270982 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 68.878042071 ampere but the right hand side evaluated to 657.160739807 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 35.5339389167 volt but the right hand side evaluated to 35.5008211305 volt (Allowable error: 0.0001%, Actual error: 0.093%) 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 68.4705016658 ampere but the right hand side evaluated to 653.352900063 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 35.5721735618 volt but the right hand side evaluated to 35.5436916442 volt (Allowable error: 0.0001%, Actual error: 0.08%) 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 68.0565750787 ampere but the right hand side evaluated to 649.482599734 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 35.6130141248 volt but the right hand side evaluated to 35.5891397816 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 67.6342939677 ampere but the right hand side evaluated to 645.532014831 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 35.6575621426 volt but the right hand side evaluated to 35.6383246323 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 67.200805066 ampere but the right hand side evaluated to 641.47514902 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 35.7074556431 volt but the right hand side evaluated to 35.6929605102 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/Motor.Perf.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 66.7560126045 ampere but the right hand side evaluated to 637.309633024 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 35.7625871432 volt but the right hand side evaluated to 35.7528598949 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 66.2964788284 ampere but the right hand side evaluated to 633.003357927 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 35.8249152341 volt but the right hand side evaluated to 35.820028868 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 9073 variables. Solving took 1.02 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 1.3000 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 796269.5175 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 0.1885 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 0.0315 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 0.0352 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 65.7609003964 ampere but the right hand side evaluated to 616.348263327 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 65.6904098813 ampere but the right hand side evaluated to 616.348264085 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 65.594335013 ampere but the right hand side evaluated to 616.348264783 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) 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 65.446818646 ampere but the right hand side evaluated to 616.348265532 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 65.2157691701 ampere but the right hand side evaluated to 616.348266541 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 40.8361575855 volt but the right hand side evaluated to 40.0442876971 volt (Allowable error: 0.0001%, Actual error: 2%) 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 40.7564340094 volt but the right hand side evaluated to 40.0109034438 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 40.6357804706 volt but the right hand side evaluated to 39.9534916067 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 40.4485542108 volt but the right hand side evaluated to 39.8631072064 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 40.1471960078 volt but the right hand side evaluated to 39.7128058368 volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 48.4046127652 ampere but the right hand side evaluated to 462.161140919 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 32.6524117033 volt but the right hand side evaluated to 32.6473101264 volt (Allowable error: 0.0001%, Actual error: 0.016%) 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 48.3769621121 ampere but the right hand side evaluated to 461.909901224 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 32.6357605132 volt but the right hand side evaluated to 32.631607204 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 48.4032768374 ampere but the right hand side evaluated to 462.148991141 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 32.6515931302 volt but the right hand side evaluated to 32.6465365342 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 48.3789810826 ampere but the right hand side evaluated to 461.928244907 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 32.6369804115 volt but the right hand side evaluated to 32.6327577733 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 48.4012471756 ampere but the right hand side evaluated to 462.130543219 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) 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 32.650366332 volt but the right hand side evaluated to 32.6453788881 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 48.3803059775 ampere but the right hand side evaluated to 461.940286842 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 32.6377873747 volt but the right hand side evaluated to 32.6335195635 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 48.3985146785 ampere but the right hand side evaluated to 462.105721333 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 32.6487359598 volt but the right hand side evaluated to 32.6438426744 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 48.3809369239 ampere but the right hand side evaluated to 461.946026943 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6381800464 volt but the right hand side evaluated to 32.6338911289 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 48.3950959618 ampere but the right hand side evaluated to 462.074658605 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 32.6466825352 volt but the right hand side evaluated to 32.6419065256 volt (Allowable error: 0.0001%, Actual error: 0.015%) 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 48.38089637 ampere but the right hand side evaluated to 461.945646219 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.638136 volt but the right hand side evaluated to 32.6338475566 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 48.3909870827 ampere but the right hand side evaluated to 462.037320284 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) 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 32.6442034456 volt but the right hand side evaluated to 32.6395680313 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 48.3801467451 ampere but the right hand side evaluated to 461.938835996 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 32.6376844791 volt but the right hand side evaluated to 32.6334218139 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 48.3861654003 ampere but the right hand side evaluated to 461.99351821 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 32.6413113386 volt but the right hand side evaluated to 32.6368419352 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 48.3786925777 ampere but the right hand side evaluated to 461.925630152 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 32.636816273 volt but the right hand side evaluated to 32.6326039914 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 48.3806452581 ampere but the right hand side evaluated to 461.943365269 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6379846685 volt but the right hand side evaluated to 32.6337049009 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 48.3765480203 ampere but the right hand side evaluated to 461.906140356 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 32.635512304 volt but the right hand side evaluated to 32.631373268 volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 48.3744158485 ampere but the right hand side evaluated to 461.886768612 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 32.6342228141 volt but the right hand side evaluated to 32.630157078 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 48.3736835629 ampere but the right hand side evaluated to 461.880121584 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 32.6337906694 volt but the right hand side evaluated to 32.6297504845 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 48.3674712777 ampere but the right hand side evaluated to 461.823674749 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 32.6300193448 volt but the right hand side evaluated to 32.6261922473 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 48.3701134331 ampere but the right hand side evaluated to 461.847685015 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 32.6316294623 volt but the right hand side evaluated to 32.6277118902 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 48.359793516 ampere but the right hand side evaluated to 461.753930528 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 32.6253770324 volt but the right hand side evaluated to 32.6218145861 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 48.3658263233 ampere but the right hand side evaluated to 461.80873252 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 32.6290278419 volt but the right hand side evaluated to 32.6252573766 volt (Allowable error: 0.0001%, Actual error: 0.012%) 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 48.3513917775 ampere but the right hand side evaluated to 461.677604587 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0096%) 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 32.6202733778 volt but the right hand side evaluated to 32.6170001807 volt (Allowable error: 0.0001%, Actual error: 0.01%) 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 48.3608099161 ampere but the right hand side evaluated to 461.76315763 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) 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 32.6259845005 volt but the right hand side evaluated to 32.622386499 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 48.3422482654 ampere but the right hand side evaluated to 461.594544052 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 32.6147077485 volt but the right hand side evaluated to 32.6117496566 volt (Allowable error: 0.0001%, Actual error: 0.0091%) 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 48.3550590328 ampere but the right hand side evaluated to 461.710910942 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0099%) 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 32.6224901474 volt but the right hand side evaluated to 32.6190899192 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 48.3323620225 ampere but the right hand side evaluated to 461.504733106 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0077%) 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 32.6086633667 volt but the right hand side evaluated to 32.6060457445 volt (Allowable error: 0.0001%, Actual error: 0.008%) 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 48.3485635437 ampere but the right hand side evaluated to 461.6519021 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0093%) 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 32.6185384368 volt but the right hand side evaluated to 32.6153618001 volt (Allowable error: 0.0001%, Actual error: 0.0097%) 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 48.3217169408 ampere but the right hand side evaluated to 461.408031785 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0066%) 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 32.6021350195 volt but the right hand side evaluated to 32.5998842937 volt (Allowable error: 0.0001%, Actual error: 0.0069%) 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 48.3413152785 ampere but the right hand side evaluated to 461.586056192 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%) 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 32.614119682 volt but the right hand side evaluated to 32.6111926879 volt (Allowable error: 0.0001%, Actual error: 0.009%) 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 48.3103020051 ampere but the right hand side evaluated to 461.304340735 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 32.595111326 volt but the right hand side evaluated to 32.5932543332 volt (Allowable error: 0.0001%, Actual error: 0.0057%) 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 48.333303569 ampere but the right hand side evaluated to 461.513277045 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0078%) 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 32.6092246899 volt but the right hand side evaluated to 32.6065738203 volt (Allowable error: 0.0001%, Actual error: 0.0081%) 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 48.2980783015 ampere but the right hand side evaluated to 461.193332497 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 32.5876036569 volt but the right hand side evaluated to 32.5861704967 volt (Allowable error: 0.0001%, Actual error: 0.0044%) 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 48.3245083974 ampere but the right hand side evaluated to 461.433390923 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0069%) 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 32.6038505608 volt but the right hand side evaluated to 32.6015035814 volt (Allowable error: 0.0001%, Actual error: 0.0072%) 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 48.2850812049 ampere but the right hand side evaluated to 461.075283984 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 32.5795559782 volt but the right hand side evaluated to 32.5785722509 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 48.3149451941 ampere but the right hand side evaluated to 461.346513618 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0059%) 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 32.5979619 volt but the right hand side evaluated to 32.595944272 volt (Allowable error: 0.0001%, Actual error: 0.0062%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 but bound is 0.1460 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 48.2712744096 ampere but the right hand side evaluated to 460.949887129 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 32.5709734614 volt but the right hand side evaluated to 32.5704676034 volt (Allowable error: 0.0001%, Actual error: 0.0016%) 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 48.3045595354 ampere but the right hand side evaluated to 461.252188556 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0049%) 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 32.5915821508 volt but the right hand side evaluated to 32.5899239645 volt (Allowable error: 0.0001%, Actual error: 0.0051%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 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 0.0315 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 0.0352 but bound is 0.0500 Warning: Constraint [i_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.2933617417 ampere but the right hand side evaluated to 461.150487498 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0037%) Warning: Constraint [v_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5846762251 volt but the right hand side evaluated to 32.5834055958 volt (Allowable error: 0.0001%, Actual error: 0.0039%) Using solver 'mosek' Solving for 9073 variables. Solving took 1.03 seconds. 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 1.2824 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 882794.0248 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 0.1991 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 0.0328 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 0.0367 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 83.6079561755 ampere but the right hand side evaluated to 779.784420593 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.4%) 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 83.5013759181 ampere but the right hand side evaluated to 779.784420593 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.3%) 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 83.3555852952 ampere but the right hand side evaluated to 779.784420593 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.1%) 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 83.131006234 ampere but the right hand side evaluated to 779.784420593 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 82.7772281643 ampere but the right hand side evaluated to 779.784420594 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 38.5656204092 volt but the right hand side evaluated to 37.5903643543 volt (Allowable error: 0.0001%, Actual error: 2.6%) 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 38.4802934679 volt but the right hand side evaluated to 37.5596486161 volt (Allowable error: 0.0001%, Actual error: 2.5%) 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 38.3521817961 volt but the right hand side evaluated to 37.5062466016 volt (Allowable error: 0.0001%, Actual error: 2.3%) 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 38.153643171 volt but the right hand side evaluated to 37.4222312594 volt (Allowable error: 0.0001%, Actual error: 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 37.8405042252 volt but the right hand side evaluated to 37.2880139386 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 55.562112521 ampere but the right hand side evaluated to 529.97551143 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 34.8029979493 volt but the right hand side evaluated to 34.7613525113 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 55.5193700682 ampere but the right hand side evaluated to 529.575516476 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 34.8078103162 volt but the right hand side evaluated to 34.766692583 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 55.4305726795 ampere but the right hand side evaluated to 528.741638109 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 34.8131782558 volt but the right hand side evaluated to 34.7729652022 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 55.3843738988 ampere but the right hand side evaluated to 528.313735694 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 34.8264812831 volt but the right hand side evaluated to 34.787139712 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 55.280911865 ampere but the right hand side evaluated to 527.343073546 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 34.8352038634 volt but the right hand side evaluated to 34.7969849834 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 55.2470351518 ampere but the right hand side evaluated to 527.029517483 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) 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 34.8459147977 volt but the right hand side evaluated to 34.8083526144 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 55.1178499939 ampere but the right hand side evaluated to 525.821632681 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) 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 34.8657244504 volt but the right hand side evaluated to 34.8298504049 volt (Allowable error: 0.0001%, Actual error: 0.1%) 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 55.1062495296 ampere but the right hand side evaluated to 525.712784826 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) 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 34.8668487131 volt but the right hand side evaluated to 34.8311006849 volt (Allowable error: 0.0001%, Actual error: 0.1%) 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 54.962419246 ampere but the right hand side evaluated to 524.367579126 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 34.8899841654 volt but the right hand side evaluated to 34.8560995368 volt (Allowable error: 0.0001%, Actual error: 0.097%) 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 54.9608450044 ampere but the right hand side evaluated to 524.352763419 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 34.8900656647 volt but the right hand side evaluated to 34.8561952117 volt (Allowable error: 0.0001%, Actual error: 0.097%) 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 54.8022555101 ampere but the right hand side evaluated to 522.868910053 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) 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 34.9165960689 volt but the right hand side evaluated to 34.8847504909 volt (Allowable error: 0.0001%, Actual error: 0.091%) 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 54.813437286 ampere but the right hand side evaluated to 522.973074035 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) 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 34.9136997052 volt but the right hand side evaluated to 34.8816796147 volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 54.6384509524 ampere but the right hand side evaluated to 521.335382419 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 34.944756033 volt but the right hand side evaluated to 34.9149544905 volt (Allowable error: 0.0001%, Actual error: 0.085%) 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 54.6600450293 ampere but the right hand side evaluated to 521.537363063 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.082%) 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 34.9404959559 volt but the right hand side evaluated to 34.9104117647 volt (Allowable error: 0.0001%, Actual error: 0.086%) 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 54.4698698779 ampere but the right hand side evaluated to 519.756474275 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) 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 34.9752168084 volt but the right hand side evaluated to 34.9474866928 volt (Allowable error: 0.0001%, Actual error: 0.079%) 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 54.5038189922 ampere but the right hand side evaluated to 520.074164119 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%) 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 34.9682132004 volt but the right hand side evaluated to 34.9400460554 volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 54.2960655631 ampere but the right hand side evaluated to 518.127890297 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.07%) 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 35.0082491877 volt but the right hand side evaluated to 34.982616638 volt (Allowable error: 0.0001%, Actual error: 0.073%) 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 54.3424153544 ampere but the right hand side evaluated to 518.561929881 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.071%) 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 34.998449909 volt but the right hand side evaluated to 34.9722380662 volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 54.116327568 ampere but the right hand side evaluated to 516.442875882 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%) 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 35.0443075827 volt but the right hand side evaluated to 35.0208015991 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 54.1746939713 ampere but the right hand side evaluated to 516.989981558 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%) 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 35.0319624245 volt but the right hand side evaluated to 35.0077593719 volt (Allowable error: 0.0001%, Actual error: 0.069%) 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 53.9293744032 ampere but the right hand side evaluated to 514.689358897 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.058%) 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 35.0842453915 volt but the right hand side evaluated to 35.062907376 volt (Allowable error: 0.0001%, Actual error: 0.061%) 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 54.0012864359 ampere but the right hand side evaluated to 515.363846204 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.06%) 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 35.0682685421 volt but the right hand side evaluated to 35.046094151 volt (Allowable error: 0.0001%, Actual error: 0.063%) 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 53.7344083697 ampere but the right hand side evaluated to 512.859619458 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%) 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 35.1285786206 volt but the right hand side evaluated to 35.1094441529 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 53.820690325 ampere but the right hand side evaluated to 513.669427047 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%) 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 35.1083772941 volt but the right hand side evaluated to 35.0882696174 volt (Allowable error: 0.0001%, Actual error: 0.057%) 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 53.5308123667 ampere but the right hand side evaluated to 510.947534083 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.046%) 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 35.1776983313 volt but the right hand side evaluated to 35.1607882078 volt (Allowable error: 0.0001%, Actual error: 0.048%) 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 53.6323899977 ampere but the right hand side evaluated to 511.901618772 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.049%) 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 35.1526084996 volt but the right hand side evaluated to 35.1345941393 volt (Allowable error: 0.0001%, Actual error: 0.051%) 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 53.3146964646 ampere but the right hand side evaluated to 508.916550455 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.04%) 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 35.234287692 volt but the right hand side evaluated to 35.2196659333 volt (Allowable error: 0.0001%, Actual error: 0.042%) 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 53.4342803936 ampere but the right hand side evaluated to 510.040540775 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.043%) 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 35.2023944639 volt but the right hand side evaluated to 35.1865167569 volt (Allowable error: 0.0001%, Actual error: 0.045%) 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 53.0848755343 ampere but the right hand side evaluated to 506.754873799 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 35.2991437486 volt but the right hand side evaluated to 35.2868429603 volt (Allowable error: 0.0001%, Actual error: 0.035%) 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 53.2245277989 ampere but the right hand side evaluated to 508.068632466 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 35.2589814132 volt but the right hand side evaluated to 35.2452818842 volt (Allowable error: 0.0001%, Actual error: 0.039%) 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 52.8367588832 ampere but the right hand side evaluated to 504.418774587 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%) 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 35.3754584104 volt but the right hand side evaluated to 35.3655213257 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 53.0002698388 ampere but the right hand side evaluated to 505.958555168 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 35.3243412756 volt but the right hand side evaluated to 35.3128631148 volt (Allowable error: 0.0001%, Actual error: 0.033%) 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 52.5631227052 ampere but the right hand side evaluated to 501.839285258 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 35.4682921452 volt but the right hand side evaluated to 35.4607659471 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 52.7574559533 ampere but the right hand side evaluated to 503.6715439 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 35.4012899347 volt but the right hand side evaluated to 35.3920727725 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 52.2505535654 ampere but the right hand side evaluated to 498.888220675 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) 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 35.5871005299 volt but the right hand side evaluated to 35.5820302972 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 52.4885408771 ampere but the right hand side evaluated to 501.135563701 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.019%) 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 35.4951164053 volt but the right hand side evaluated to 35.4882043648 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 51.8636804322 ampere but the right hand side evaluated to 495.227757218 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 35.7569223555 volt but the right hand side evaluated to 35.7543571729 volt (Allowable error: 0.0001%, Actual error: 0.0072%) 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 52.1781932208 ampere but the right hand side evaluated to 498.204251771 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 35.6166300737 volt but the right hand side evaluated to 35.6120751577 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 0.1991 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 0.0328 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 0.0367 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 0.1991 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 0.0328 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 0.0367 but bound is 0.0500 Using solver 'mosek' Solving for 9073 variables. Solving took 1.26 seconds. 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 1.2351 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 988744.2620 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 0.2106 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 0.0340 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 0.0369 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 99.8053624219 ampere but the right hand side evaluated to 936.51347212 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 99.712539337 ampere but the right hand side evaluated to 936.513472126 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 99.5865958655 ampere but the right hand side evaluated to 936.513472132 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 99.3939650574 ampere but the right hand side evaluated to 936.513472137 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_(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 99.0931238145 ampere but the right hand side evaluated to 936.513472145 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 38.2500479164 volt but the right hand side evaluated to 37.5140776917 volt (Allowable error: 0.0001%, Actual error: 2%) 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 38.1813138383 volt but the right hand side evaluated to 37.485874058 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 38.0772360953 volt but the right hand side evaluated to 37.4367679417 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 37.9163409134 volt but the right hand side evaluated to 37.3595018173 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 37.6635829807 volt but the right hand side evaluated to 37.2361681462 volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 65.8563147688 ampere but the right hand side evaluated to 627.639155091 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 35.0192497575 volt but the right hand side evaluated to 34.9457840718 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 65.8480786504 ampere but the right hand side evaluated to 627.559423375 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 35.0178803522 volt but the right hand side evaluated to 34.9443447545 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 65.5672945648 ampere but the right hand side evaluated to 624.946414192 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 35.0396386462 volt but the right hand side evaluated to 34.9698221325 volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 65.5697435045 ampere but the right hand side evaluated to 624.964497419 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 35.0363153469 volt but the right hand side evaluated to 34.966192527 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 65.2732238363 ampere but the right hand side evaluated to 622.20803645 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 35.0630663757 volt but the right hand side evaluated to 34.9970777971 volt (Allowable error: 0.0001%, Actual error: 0.19%) 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 65.2860508754 ampere but the right hand side evaluated to 622.321577687 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 35.0579503044 volt but the right hand side evaluated to 34.9914489379 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 64.9804137826 ampere but the right hand side evaluated to 619.477084506 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 35.085238457 volt but the right hand side evaluated to 35.0228416554 volt (Allowable error: 0.0001%, Actual error: 0.18%) 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 65.0011128537 ampere but the right hand side evaluated to 619.664988062 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 35.0799525086 volt but the right hand side evaluated to 35.0169981154 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 64.6877941262 ampere but the right hand side evaluated to 616.744587258 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 35.1067915745 volt but the right hand side evaluated to 35.0478197583 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 64.7129078942 ampere but the right hand side evaluated to 616.977348119 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 35.1035825957 volt but the right hand side evaluated to 35.0442121071 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 64.3852082285 ampere but the right hand side evaluated to 613.923428356 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 35.1343709812 volt but the right hand side evaluated to 35.079234615 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 64.4226692383 ampere but the right hand side evaluated to 614.2689048 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 35.1279366406 volt but the right hand side evaluated to 35.0720982899 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 64.081809824 ampere but the right hand side evaluated to 611.09141555 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 35.1618136871 volt but the right hand side evaluated to 35.1103636995 volt (Allowable error: 0.0001%, Actual error: 0.15%) 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 64.1263515405 ampere but the right hand side evaluated to 611.504617984 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 35.1556046334 volt but the right hand side evaluated to 35.1034581239 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 63.7762861783 ampere but the right hand side evaluated to 608.237179518 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 35.1899071568 volt but the right hand side evaluated to 35.1420616844 volt (Allowable error: 0.0001%, Actual error: 0.14%) 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 63.8267792758 ampere but the right hand side evaluated to 608.708326095 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 35.1846283644 volt but the right hand side evaluated to 35.1361507982 volt (Allowable error: 0.0001%, Actual error: 0.14%) 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 63.4629798527 ampere but the right hand side evaluated to 605.311321825 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 35.2222903512 volt but the right hand side evaluated to 35.1782434629 volt (Allowable error: 0.0001%, Actual error: 0.13%) 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 63.5246324679 ampere but the right hand side evaluated to 605.885662887 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 35.2144733016 volt but the right hand side evaluated to 35.1695905864 volt (Allowable error: 0.0001%, Actual error: 0.13%) 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 63.1454614583 ampere but the right hand side evaluated to 602.344270064 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 35.2565146589 volt but the right hand side evaluated to 35.2162439973 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 63.2147629608 ampere but the right hand side evaluated to 602.99148691 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 35.2484416793 volt but the right hand side evaluated to 35.207320875 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 62.8220319485 ampere but the right hand side evaluated to 599.320755393 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 35.2936061513 volt but the right hand side evaluated to 35.2571478351 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 62.9011401311 ampere but the right hand side evaluated to 600.05988324 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 35.2838297511 volt but the right hand side evaluated to 35.2464107419 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 62.4925841508 ampere but the right hand side evaluated to 596.239309878 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 35.3335420317 volt but the right hand side evaluated to 35.3009068561 volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 62.5796735422 ampere but the right hand side evaluated to 597.054528058 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 35.3232333982 volt but the right hand side evaluated to 35.2896228234 volt (Allowable error: 0.0001%, Actual error: 0.095%) 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 62.1579040885 ampere but the right hand side evaluated to 593.106384732 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 35.3757142692 volt but the right hand side evaluated to 35.3468494818 volt (Allowable error: 0.0001%, Actual error: 0.082%) 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 62.2517334388 ampere but the right hand side evaluated to 593.986827374 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 35.3656590245 volt but the right hand side evaluated to 35.335863813 volt (Allowable error: 0.0001%, Actual error: 0.084%) 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 61.8067692629 ampere but the right hand side evaluated to 589.821575336 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 35.4273677999 volt but the right hand side evaluated to 35.4026411529 volt (Allowable error: 0.0001%, Actual error: 0.07%) 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 61.9157403131 ampere but the right hand side evaluated to 590.842184995 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 35.4120478874 volt but the right hand side evaluated to 35.3861066958 volt (Allowable error: 0.0001%, Actual error: 0.073%) 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 61.449543612 ampere but the right hand side evaluated to 586.475895248 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 35.4816223667 volt but the right hand side evaluated to 35.4609141191 volt (Allowable error: 0.0001%, Actual error: 0.058%) 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 61.5712534767 ampere but the right hand side evaluated to 587.615947312 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 35.4625933771 volt but the right hand side evaluated to 35.4405196014 volt (Allowable error: 0.0001%, Actual error: 0.062%) 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 61.0866609394 ampere but the right hand side evaluated to 583.072808697 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 35.5381067816 volt but the right hand side evaluated to 35.5212531834 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 61.216438315 ampere but the right hand side evaluated to 584.290880399 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.048%) 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 35.5183978579 volt but the right hand side evaluated to 35.5002252094 volt (Allowable error: 0.0001%, Actual error: 0.051%) 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 60.7005595085 ampere but the right hand side evaluated to 579.4530553 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 35.6081709252 volt but the right hand side evaluated to 35.5955463266 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 60.8482201915 ampere but the right hand side evaluated to 580.838247724 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 35.5813677355 volt but the right hand side evaluated to 35.567173072 volt (Allowable error: 0.0001%, Actual error: 0.04%) 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 60.3007099836 ampere but the right hand side evaluated to 575.699975547 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.022%) 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 35.6855313609 volt but the right hand side evaluated to 35.6770665309 volt (Allowable error: 0.0001%, Actual error: 0.024%) 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 60.4638991945 ampere but the right hand side evaluated to 577.232151628 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 35.6531581215 volt but the right hand side evaluated to 35.6430163524 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 59.8791569299 ampere but the right hand side evaluated to 571.739228349 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 35.7752530113 volt but the right hand side evaluated to 35.7709882238 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 60.0608417498 ampere but the right hand side evaluated to 573.446742192 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 35.7353732428 volt but the right hand side evaluated to 35.7293203092 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 0.2106 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 0.0340 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 0.0369 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 59.631613628 ampere but the right hand side evaluated to 569.41140563 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 35.8327102316 volt but the right hand side evaluated to 35.8308144898 volt (Allowable error: 0.0001%, Actual error: 0.0053%) Using solver 'mosek' Solving for 4713 variables. Solving took 0.898 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 1.2058 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 1064456.8431 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 0.2186 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 0.0349 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 0.0382 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 111.917770226 ampere but the right hand side evaluated to 1056.06638261 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.846508798 ampere but the right hand side evaluated to 1056.06638263 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.750496787 ampere but the right hand side evaluated to 1056.06638264 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 111.604583519 ampere but the right hand side evaluated to 1056.06638265 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.378520102 ampere but the right hand side evaluated to 1056.06638267 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.210005133 volt but the right hand side evaluated to 37.7037005948 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1552267402 volt but the right hand side evaluated to 37.6768744126 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.0707684081 volt but the right hand side evaluated to 37.6300619471 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.9401395797 volt but the right hand side evaluated to 37.5563494027 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7350514617 volt but the right hand side evaluated to 37.4386742818 volt (Allowable error: 0.0001%, Actual error: 0.79%) 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 73.3928823216 ampere but the right hand side evaluated to 699.259454477 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 35.2475793823 volt but the right hand side evaluated to 35.1620020849 volt (Allowable error: 0.0001%, Actual error: 0.24%) 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 73.028781032 ampere but the right hand side evaluated to 695.874674382 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 35.265786034 volt but the right hand side evaluated to 35.1847558735 volt (Allowable error: 0.0001%, Actual error: 0.23%) 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 72.6668715908 ampere but the right hand side evaluated to 692.503921893 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 35.282536004 volt but the right hand side evaluated to 35.2057288571 volt (Allowable error: 0.0001%, Actual error: 0.22%) 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 72.3030186089 ampere but the right hand side evaluated to 689.114234801 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 35.3004423278 volt but the right hand side evaluated to 35.2278761673 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 71.9368576529 ampere but the right hand side evaluated to 685.702224341 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 35.319619536 volt but the right hand side evaluated to 35.2513178781 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 71.5698260074 ampere but the right hand side evaluated to 682.279126706 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 35.3390118557 volt but the right hand side evaluated to 35.274865042 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 71.1962380408 ampere but the right hand side evaluated to 678.79817986 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 35.362186068 volt but the right hand side evaluated to 35.302490913 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 70.8211300453 ampere but the right hand side evaluated to 675.299847665 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 35.3857488725 volt but the right hand side evaluated to 35.3303924214 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 70.4425569401 ampere but the right hand side evaluated to 671.767779582 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 35.4108387328 volt but the right hand side evaluated to 35.3598285372 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 70.0657066163 ampere but the right hand side evaluated to 668.244838931 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 35.4340121212 volt but the right hand side evaluated to 35.3869876714 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 69.6718388387 ampere but the right hand side evaluated to 664.573838463 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 35.4671382048 volt but the right hand side evaluated to 35.4249435514 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 69.279642726 ampere but the right hand side evaluated to 660.910355453 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 35.4981269724 volt but the right hand side evaluated to 35.4603423191 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 68.8779738337 ampere but the right hand side evaluated to 657.159930685 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 35.5339563443 volt but the right hand side evaluated to 35.5008294687 volt (Allowable error: 0.0001%, Actual error: 0.093%) 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 68.47045714 ampere but the right hand side evaluated to 653.35234871 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 35.57218234 volt but the right hand side evaluated to 35.5436931089 volt (Allowable error: 0.0001%, Actual error: 0.08%) 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 68.0565413946 ampere but the right hand side evaluated to 649.48218895 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/Air....craftDrag.138/MotorPerf.138**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.6130215353 volt but the right hand side evaluated to 35.5891419947 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 67.634264336 ampere but the right hand side evaluated to 645.531678494 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 35.6575716036 volt but the right hand side evaluated to 35.638330961 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 67.2007895204 ampere but the right hand side evaluated to 641.474966622 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 35.7074599381 volt but the right hand side evaluated to 35.6929628074 volt (Allowable error: 0.0001%, Actual error: 0.041%) 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 66.7560033687 ampere but the right hand side evaluated to 637.309530345 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 35.7625903707 volt but the right hand side evaluated to 35.7528622645 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 66.2964767623 ampere but the right hand side evaluated to 633.003334243 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 35.8249158526 volt but the right hand side evaluated to 35.8200292506 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 571 variables. Solving took 0.259 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 1.2058 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 1064456.8406 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 0.2186 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 0.0349 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 0.0382 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 111.920982541 ampere but the right hand side evaluated to 1056.06637512 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.849323437 ampere but the right hand side evaluated to 1056.06637514 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.752850219 ampere but the right hand side evaluated to 1056.06637515 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.606364684 ampere but the right hand side evaluated to 1056.06637517 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.379914651 ampere but the right hand side evaluated to 1056.0663752 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.2086428786 volt but the right hand side evaluated to 37.7038065451 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.153679337 volt but the right hand side evaluated to 37.6769672402 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.0690627461 volt but the right hand side evaluated to 37.6301395552 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.938354044 volt but the right hand side evaluated to 37.5564081264 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7337083369 volt but the right hand side evaluated to 37.4387202454 volt (Allowable error: 0.0001%, Actual error: 0.79%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 571 variables. Solving took 0.136 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 1.2058 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 1064456.8405 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 0.2186 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 0.0349 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 0.0382 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 111.920983251 ampere but the right hand side evaluated to 1056.06637508 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.849324008 ampere but the right hand side evaluated to 1056.0663751 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.752850626 ampere but the right hand side evaluated to 1056.06637511 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.60636488 ampere but the right hand side evaluated to 1056.06637513 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.379914709 ampere but the right hand side evaluated to 1056.06637516 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.208642692 volt but the right hand side evaluated to 37.7038065678 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1536790984 volt but the right hand side evaluated to 37.6769672583 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.0690624496 volt but the right hand side evaluated to 37.630139568 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.9383536892 volt but the right hand side evaluated to 37.5564081322 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7337080468 volt but the right hand side evaluated to 37.4387202467 volt (Allowable error: 0.0001%, Actual error: 0.79%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 4713 variables. Solving took 1.29 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 1.2058 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 1064456.8435 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 0.2186 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 0.0349 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 0.0382 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 111.917810931 ampere but the right hand side evaluated to 1056.06638279 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.846541429 ampere but the right hand side evaluated to 1056.06638281 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.750519169 ampere but the right hand side evaluated to 1056.06638282 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 111.604592318 ampere but the right hand side evaluated to 1056.06638283 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.378510923 ampere but the right hand side evaluated to 1056.06638285 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.2100219553 volt but the right hand side evaluated to 37.7037019608 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1552399681 volt but the right hand side evaluated to 37.676875512 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.0707772038 volt but the right hand side evaluated to 37.6300627084 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.9401426006 volt but the right hand side evaluated to 37.5563497157 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7350477729 volt but the right hand side evaluated to 37.4386740016 volt (Allowable error: 0.0001%, Actual error: 0.79%) 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 73.3931429341 ampere but the right hand side evaluated to 699.262981664 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 35.2475640137 volt but the right hand side evaluated to 35.1620429074 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 73.0289067566 ampere but the right hand side evaluated to 695.876996517 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 35.2658447701 volt but the right hand side evaluated to 35.184875258 volt (Allowable error: 0.0001%, Actual error: 0.23%) 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 72.6669904068 ampere but the right hand side evaluated to 692.506061745 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 35.2825858935 volt but the right hand side evaluated to 35.2058333857 volt (Allowable error: 0.0001%, Actual error: 0.22%) 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 72.3031333602 ampere but the right hand side evaluated to 689.116221323 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 35.3004820913 volt but the right hand side evaluated to 35.2279646057 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 71.9369652022 ampere but the right hand side evaluated to 685.704038472 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 35.3196518029 volt but the right hand side evaluated to 35.2513933871 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 71.5699970079 ampere but the right hand side evaluated to 682.281352753 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 35.3389917141 volt but the right hand side evaluated to 35.2748777999 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 71.1963091206 ampere but the right hand side evaluated to 678.79948625 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 35.3622193481 volt but the right hand side evaluated to 35.3025590122 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 70.8211724146 ampere but the right hand side evaluated to 675.300821086 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 35.3857902397 volt but the right hand side evaluated to 35.3304654857 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 70.4426772744 ampere but the right hand side evaluated to 671.769309904 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 35.4108202524 volt but the right hand side evaluated to 35.3598315407 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 70.0648674373 ampere but the right hand side evaluated to 668.238281309 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 35.4345997948 volt but the right hand side evaluated to 35.3876562417 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 69.6718345305 ampere but the right hand side evaluated to 664.574168125 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 35.4671819297 volt but the right hand side evaluated to 35.4250082651 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 69.2794492211 ampere but the right hand side evaluated to 660.909011901 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 35.498283211 volt but the right hand side evaluated to 35.4605270971 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 68.8780420514 ampere but the right hand side evaluated to 657.160739602 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 35.533938926 volt but the right hand side evaluated to 35.5008211387 volt (Allowable error: 0.0001%, Actual error: 0.093%) 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 68.4705016523 ampere but the right hand side evaluated to 653.352899917 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 35.5721735682 volt but the right hand side evaluated to 35.5436916496 volt (Allowable error: 0.0001%, Actual error: 0.08%) 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 68.05657507 ampere but the right hand side evaluated to 649.482599638 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 35.6130141293 volt but the right hand side evaluated to 35.5891397854 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 67.6342939628 ampere but the right hand side evaluated to 645.532014778 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 35.6575621457 volt but the right hand side evaluated to 35.6383246349 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 67.200805065 ampere but the right hand side evaluated to 641.475149005 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 35.7074556444 volt but the right hand side evaluated to 35.6929605112 volt (Allowable error: 0.0001%, Actual error: 0.041%) 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 66.7560126031 ampere but the right hand side evaluated to 637.309633009 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 35.762587145 volt but the right hand side evaluated to 35.7528598966 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 66.2964788304 ampere but the right hand side evaluated to 633.003357947 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 35.8249152343 volt but the right hand side evaluated to 35.8200288682 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Beginning signomial solve. Solving took 4 GP solves and 7.59 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 1.2115 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 1024485.2888 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 0.2113 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 0.0257 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 0.0393 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 103.179814784 ampere but the right hand side evaluated to 968.100181935 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 103.085208959 ampere but the right hand side evaluated to 968.100181951 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 102.957004143 ampere but the right hand side evaluated to 968.100181965 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) 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 102.761152771 ampere but the right hand side evaluated to 968.100181983 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 102.455547269 ampere but the right hand side evaluated to 968.100182006 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 37.9241426988 volt but the right hand side evaluated to 37.1871323012 volt (Allowable error: 0.0001%, Actual error: 2%) 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 37.8574933262 volt but the right hand side evaluated to 37.1603690013 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 37.7564751324 volt but the right hand side evaluated to 37.1133815899 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 37.6004312216 volt but the right hand side evaluated to 37.0394299652 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 37.355451498 volt but the right hand side evaluated to 36.9213697851 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 68.3444859608 ampere but the right hand side evaluated to 651.134951411 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 34.691175185 volt but the right hand side evaluated to 34.6058513247 volt (Allowable error: 0.0001%, Actual error: 0.25%) 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 67.9966328641 ampere but the right hand side evaluated to 647.901222949 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 34.7122255071 volt but the right hand side evaluated to 34.6314587303 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 67.6513933624 ampere but the right hand side evaluated to 644.685554333 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 34.7315375578 volt but the right hand side evaluated to 34.654987929 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 67.3038758796 ampere but the right hand side evaluated to 641.4477409 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 34.75225971 volt but the right hand side evaluated to 34.6799441473 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 66.9536731634 ampere but the right hand side evaluated to 638.18398319 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 34.7745451035 volt but the right hand side evaluated to 34.7064862658 volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 66.6025514031 ampere but the right hand side evaluated to 634.908663534 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 34.7971179812 volt but the right hand side evaluated to 34.7331992979 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 66.2436665123 ampere but the right hand side evaluated to 631.563924174 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 34.8243603575 volt but the right hand side evaluated to 34.7648894422 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 65.8831222593 ampere but the right hand side evaluated to 628.200445757 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 34.8521451449 volt but the right hand side evaluated to 34.7970015037 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 65.5186334617 ampere but the right hand side evaluated to 624.798563394 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 34.8818587337 volt but the right hand side evaluated to 34.8310443946 volt (Allowable error: 0.0001%, Actual error: 0.15%) 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 65.1558620376 ampere but the right hand side evaluated to 621.406431951 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 34.9097081778 volt but the right hand side evaluated to 34.8628830324 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 64.7736746078 ampere but the right hand side evaluated to 617.841973404 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 34.9493129623 volt but the right hand side evaluated to 34.9072837194 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 64.3930912302 ampere but the right hand side evaluated to 614.285063729 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 34.9868933506 volt but the right hand side evaluated to 34.9492580847 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 64.0013027812 ampere but the right hand side evaluated to 610.624292556 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 35.0306359753 volt but the right hand side evaluated to 34.9976327398 volt (Allowable error: 0.0001%, Actual error: 0.094%) 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 63.602194919 ampere but the right hand side evaluated to 606.89240709 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 35.077901871 volt but the right hand side evaluated to 35.0495152853 volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 63.1950602544 ampere but the right hand side evaluated to 603.082379811 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 35.1290282003 volt but the right hand side evaluated to 35.1052281116 volt (Allowable error: 0.0001%, Actual error: 0.068%) 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 62.7771829451 ampere but the right hand side evaluated to 599.169218092 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 35.1856398265 volt but the right hand side evaluated to 35.1664553444 volt (Allowable error: 0.0001%, Actual error: 0.055%) 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 62.3444969741 ampere but the right hand side evaluated to 595.115296331 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 35.2502144325 volt but the right hand side evaluated to 35.2357530497 volt (Allowable error: 0.0001%, Actual error: 0.041%) 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 61.8960303792 ampere but the right hand side evaluated to 590.90994637 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 35.3232320568 volt but the right hand side evaluated to 35.3135222243 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 61.4259177473 ampere but the right hand side evaluated to 586.49783307 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 35.4082839241 volt but the right hand side evaluated to 35.4034035766 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 0.2113 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 0.0257 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 0.0393 but bound is 0.0500 Using solver 'mosek_cli' Solving for 4713 variables. Solving took 1.49 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 1.2058 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 1064461.9306 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 0.2186 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 0.0349 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 0.0382 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 111.91772465 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.84645576 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.750532658 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 111.604570119 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.378465399 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.2099900097 volt but the right hand side evaluated to 37.7037124356 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1552361519 volt but the right hand side evaluated to 37.6768818679 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.070777763 volt but the right hand side evaluated to 37.6300725084 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.9401531069 volt but the right hand side evaluated to 37.5563550079 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7350360091 volt but the right hand side evaluated to 37.4386798186 volt (Allowable error: 0.0001%, Actual error: 0.79%) 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 73.3928852703 ampere but the right hand side evaluated to 699.259252504 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 35.2475844264 volt but the right hand side evaluated to 35.1620175348 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 73.0288084791 ampere but the right hand side evaluated to 695.875002379 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 35.2657768732 volt but the right hand side evaluated to 35.1847586308 volt (Allowable error: 0.0001%, Actual error: 0.23%) 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 72.6669010809 ampere but the right hand side evaluated to 692.504306469 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 35.2825320963 volt but the right hand side evaluated to 35.2057381181 volt (Allowable error: 0.0001%, Actual error: 0.22%) 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 72.3030273248 ampere but the right hand side evaluated to 689.114181043 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 35.3004601759 volt but the right hand side evaluated to 35.2278680724 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 71.9368751189 ampere but the right hand side evaluated to 685.702542038 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 35.3196335309 volt but the right hand side evaluated to 35.2513063048 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 71.5698574506 amp. ---------------------------------------------------------------------- Ran 6 tests in 215.339s OK Generating XML reports... ere but the right hand side evaluated to 682.279507696 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 35.3389939944 volt but the right hand side evaluated to 35.2748531353 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 71.196239428 ampere but the right hand side evaluated to 678.798399874 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 35.3621839799 volt but the right hand side evaluated to 35.302504444 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 70.8211014944 ampere but the right hand side evaluated to 675.299571033 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 35.3857430387 volt but the right hand side evaluated to 35.3303851139 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 70.4425863487 ampere but the right hand side evaluated to 671.76780333 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 35.4108404265 volt but the right hand side evaluated to 35.3598222095 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 70.0656738448 ampere but the right hand side evaluated to 668.244506754 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 35.4340421247 volt but the right hand side evaluated to 35.3870170771 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 69.6718247479 ampere but the right hand side evaluated to 664.573718666 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 35.4671529804 volt but the right hand side evaluated to 35.4249283144 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 69.2796352934 ampere but the right hand side evaluated to 660.910267925 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 35.4981293242 volt but the right hand side evaluated to 35.4603518177 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 68.8779432657 ampere but the right hand side evaluated to 657.159687095 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 35.5339650128 volt but the right hand side evaluated to 35.5008151603 volt (Allowable error: 0.0001%, Actual error: 0.093%) 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 68.4704318325 ampere but the right hand side evaluated to 653.35251579 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 35.5721845645 volt but the right hand side evaluated to 35.5437029519 volt (Allowable error: 0.0001%, Actual error: 0.08%) 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 68.0565515503 ampere but the right hand side evaluated to 649.482206845 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 35.6130092687 volt but the right hand side evaluated to 35.5891434405 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 67.6342830362 ampere but the right hand side evaluated to 645.531584282 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 35.6575890221 volt but the right hand side evaluated to 35.6383203702 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 67.2007897707 ampere but the right hand side evaluated to 641.475009679 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 35.7074731924 volt but the right hand side evaluated to 35.6929701349 volt (Allowable error: 0.0001%, Actual error: 0.041%) 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 66.7559879251 ampere but the right hand side evaluated to 637.309625955 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 35.7625765899 volt but the right hand side evaluated to 35.7528572379 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 66.2964930089 ampere but the right hand side evaluated to 633.003278394 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 35.8249292918 volt but the right hand side evaluated to 35.8200255905 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Beginning signomial solve. Solving took 4 GP solves and 12.6 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 1.2115 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 1024484.3799 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 0.2113 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 0.0257 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 0.0393 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 103.179996304 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 103.085320531 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 102.957059166 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) 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 102.761215428 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 102.455545289 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 37.9241836643 volt but the right hand side evaluated to 37.1871443682 volt (Allowable error: 0.0001%, Actual error: 2%) 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 37.8575336611 volt but the right hand side evaluated to 37.1603807992 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 37.7565133544 volt but the right hand side evaluated to 37.1134031567 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 37.6004493078 volt but the right hand side evaluated to 37.0394414661 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 37.3554568011 volt but the right hand side evaluated to 36.9213822508 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 68.3448354525 ampere but the right hand side evaluated to 651.14024235 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 34.6911634881 volt but the right hand side evaluated to 34.6059019965 volt (Allowable error: 0.0001%, Actual error: 0.25%) 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 67.9968241222 ampere but the right hand side evaluated to 647.904303437 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 34.7122968411 volt but the right hand side evaluated to 34.6316421233 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 67.6515996291 ampere but the right hand side evaluated to 644.688590865 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 34.7316022445 volt but the right hand side evaluated to 34.655150109 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 67.3040221936 ampere but the right hand side evaluated to 641.450471552 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 34.7523084493 volt but the right hand side evaluated to 34.6800786797 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 66.9538114289 ampere but the right hand side evaluated to 638.186921044 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 34.7745918201 volt but the right hand side evaluated to 34.7065860277 volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 66.6028253953 ampere but the right hand side evaluated to 634.912161143 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 34.797098261 volt but the right hand side evaluated to 34.733210035 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 66.243808242 ampere but the right hand side evaluated to 631.565945243 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 34.8244247074 volt but the right hand side evaluated to 34.7649890168 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 65.8832344376 ampere but the right hand side evaluated to 628.201774725 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 34.8522256894 volt but the right hand side evaluated to 34.7971013557 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 65.518857371 ampere but the right hand side evaluated to 624.800974192 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 34.8818277933 volt but the right hand side evaluated to 34.8310423847 volt (Allowable error: 0.0001%, Actual error: 0.15%) 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 65.1546711898 ampere but the right hand side evaluated to 621.396798421 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 34.9105473541 volt but the right hand side evaluated to 34.8638440471 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 64.7737222319 ampere but the right hand side evaluated to 617.84292787 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 34.949389475 volt but the right hand side evaluated to 34.9073921623 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 64.3928756218 ampere but the right hand side evaluated to 614.283468853 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 34.9871202183 volt but the right hand side evaluated to 34.9495299614 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 64.0014666818 ampere but the right hand side evaluated to 610.625693746 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 35.0306012177 volt but the right hand side evaluated to 34.9976253157 volt (Allowable error: 0.0001%, Actual error: 0.094%) 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 63.6023233284 ampere but the right hand side evaluated to 606.893770305 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 35.0778893875 volt but the right hand side evaluated to 35.0494997294 volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 63.1951779511 ampere but the right hand side evaluated to 603.083311633 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 35.1289999939 volt but the right hand side evaluated to 35.1052008681 volt (Allowable error: 0.0001%, Actual error: 0.068%) 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 62.7772659018 ampere but the right hand side evaluated to 599.170103847 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 35.1856032373 volt but the right hand side evaluated to 35.1664497638 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 62.3445962271 ampere but the right hand side evaluated to 595.115806014 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 35.2501928442 volt but the right hand side evaluated to 35.2357420881 volt (Allowable error: 0.0001%, Actual error: 0.041%) 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 61.8960893007 ampere but the right hand side evaluated to 590.910759624 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 35.3232009941 volt but the right hand side evaluated to 35.3135051811 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 61.4259878198 ampere but the right hand side evaluated to 586.497990346 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 35.4082909378 volt but the right hand side evaluated to 35.4033944035 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 0.2113 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 0.0257 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 0.0393 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: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) 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: 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: 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-HvnWZm 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-Wt5XKX/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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-184ZVC/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 6.314s 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 0.022 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.246 seconds. Using solver 'mosek' Solving for 8 variables. Solving took 0.092 seconds. Using solver 'mosek' Solving for 24 variables. Solving took 0.0545 seconds. Using solver 'mosek' Solving for 24 variables. Solving took 0.0121 seconds. Using solver 'mosek_cli' Solving for 8 variables. Solving took 0.237 seconds. Using solver 'mosek_cli' Solving for 24 variables. Solving took 0.232 seconds. Using solver 'mosek_cli' Solving for 24 variables. Solving took 0.228 seconds. Using solver 'mosek' Solving for 13 variables. Solving took 0.0115 seconds. Using solver 'mosek_cli' Solving for 13 variables. Solving took 0.231 seconds. Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3481 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9721 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3856 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9562 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 1884891.4063 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.2552 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 1.726s 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(, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 SETTINGS defaultdict(, {'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(, {'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(, {'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(, {'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(, {'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(, {'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(, {}) [Execution node] check if [macys_VM] is in [[windows10x64, windows7x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] Build step 'Console output (build log) parsing' changed build result to FAILURE [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 FAILURE [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: FAILURE