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originally caused by:
 GitHub pull request #161 of commit c8273ac60c8b8208547e2de4a4c7a9024c3ccaaa, no merge conflicts.
Building remotely on macys_VM in workspace /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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 d2aa5c2802ceac0493de82c20e4664802e2e8d59 (refs/remotes/origin/pr/161/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 d2aa5c2802ceac0493de82c20e4664802e2e8d59 # timeout=10
 > git rev-parse HEAD^{commit} # timeout=10
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 > git show-ref --tags -d # timeout=10
Checking out Revision d2aa5c2802ceac0493de82c20e4664802e2e8d59 (origin/pr/161/merge, origin/master)
 > git config core.sparsecheckout # timeout=10
 > git checkout -f d2aa5c2802ceac0493de82c20e4664802e2e8d59 # timeout=3
Commit message: "Merge c8273ac60c8b8208547e2de4a4c7a9024c3ccaaa into 3824690dad9dd0d95323d63fb2ed01740e732e4c"
Using 'Changelog to branch' strategy.
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[description-setter] Description set: <a title="Actuator updates" href="https://github.com/convexengineering/gplibrary/pull/161">PR 161</a>: Actuator updates
[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/jenkins3115695347880332594.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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit
New python executable in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/python
Installing setuptools, pip, wheel...done.
+ . /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip
+ PIP=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip
+ python /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade pip
Requirement already up-to-date: pip in ./venv2_gpkit/lib/python2.7/site-packages (10.0.0)
+ [[ macys_VM == *reynolds* ]]
+ [[ macys_VM == *macys* ]]
+ [[ mosek == mosek ]]
+ [[ macys_VM == macys ]]
+ export PATH=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying build/lib/mosek/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying build/lib/mosek/array.py -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
creating /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
copying build/lib/mosek/fusion/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
copying build/lib/mosek/fusion/SolverInfo.py -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
copying build/lib/mosek/fusion/Utils.py -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/__init__.py to __init__.pyc
byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/array.py to array.pyc
byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/__init__.py to __init__.pyc
byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/SolverInfo.py to SolverInfo.pyc
byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
running install_egg_info
Writing /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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: 0.02    
************************************
A license was checked out correctly.
************************************
+ export 'GPKITSOLVERS=mosek, mosek_cli'
+ GPKITSOLVERS='mosek, mosek_cli'
+ [[ mosek == cvxopt ]]
+ python /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/build_gpkit
+ GPKITBUILD=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/gpkit
Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek
Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/build_gpkit
expopt.so
+ python -c 'from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)'
Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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 0.605s

OK

Generating XML reports...
adding test for 'test.py'
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0131 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0104 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.337 seconds.
Cloning into 'gassolar'...
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Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-ByH3Vr
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-l47JZS/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
Installing collected packages: gpfit
Successfully installed gpfit-0.1
Processing /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/gassolar
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-4EOkin/wheels/b0/64/83/52ddaf6fb632d8fe28aa5873a810aecc9a7d7320dc6bf6ee3a
Successfully built gassolar
Installing collected packages: gassolar
Successfully installed gassolar-0.0.0.0

Running tests...
----------------------------------------------------------------------
../Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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 35.126s

OK

Generating XML reports...
adding test for 'gassolar/gas/gas.py'
adding test for 'gassolar/solar/solar.py'
Using solver 'mosek'
Solving for 609 variables.
Solving took 0.106 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 1.46 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 609 variables.
Solving took 0.124 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 1.5 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 1437 variables.
Solving took 0.229 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1925 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 131552.1335 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 2.67 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0986 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 134553.9076 but bound is 150000.0000
Using solver 'mosek_cli'
Solving for 1437 variables.
Solving took 0.515 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 4.04 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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-B6E6nz
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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-delH_q/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit

Running tests...
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....
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Ran 4 tests in 40.815s

OK

Generating XML reports...
adding test for 'model/jho.py'
adding test for 'model/print_perf.py'
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.207670654236665e-14.
Allowing negative dual variable(s) as small as -8.188935640696116e-14.
Allowing negative dual variable(s) as small as -1.524097688332393e-13.
Allowing negative dual variable(s) as small as -1.5012600537711585e-13.
Solving took 4 GP solves and 2.08 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.939829349545846e-14.
Allowing negative dual variable(s) as small as -8.09807949864183e-14.
Allowing negative dual variable(s) as small as -1.5093438651692104e-13.
Allowing negative dual variable(s) as small as -1.500917445884653e-13.
Solving took 4 GP solves and 2.13 seconds.
Allowing negative dual variable(s) as small as -5.23197804525033e-13.
Allowing negative dual variable(s) as small as -5.141859160673334e-13.
Allowing negative dual variable(s) as small as -5.130357944027608e-13.
Allowing negative dual variable(s) as small as -5.157332894079047e-13.
Allowing negative dual variable(s) as small as -2.3984156674594637e-13.
Allowing negative dual variable(s) as small as -1.8391321451871612e-14.
Allowing negative dual variable(s) as small as -1.2592575636752312e-12.
Allowing negative dual variable(s) as small as -1.2592448785098131e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.588356182691264e-14.
Allowing negative dual variable(s) as small as -1.133602760272634e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.434121819968534e-11.
Allowing negative dual variable(s) as small as -6.449526823967958e-12.
Allowing negative dual variable(s) as small as -1.933927654586184e-11.
Allowing negative dual variable(s) as small as -1.9354577237980317e-11.
Solving took 4 GP solves and 1.89 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.43 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.226652444179081e-13.
Allowing negative dual variable(s) as small as -5.107650413727072e-13.
Allowing negative dual variable(s) as small as -5.175044420768771e-13.
Allowing negative dual variable(s) as small as -5.131103875122278e-13.
Allowing negative dual variable(s) as small as -2.3814674190991703e-13.
Allowing negative dual variable(s) as small as -1.8455180959831008e-14.
Allowing negative dual variable(s) as small as -1.2588036082256115e-12.
Allowing negative dual variable(s) as small as -1.2610094175455333e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.6986412276764895e-14.
Allowing negative dual variable(s) as small as -1.1471032457244235e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.4341232006534136e-11.
Allowing negative dual variable(s) as small as -6.449675653983068e-12.
Allowing negative dual variable(s) as small as -1.933919207356888e-11.
Allowing negative dual variable(s) as small as -1.935455715805845e-11.
Solving took 4 GP solves and 1.95 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.87 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Cloning into 'turbofan'...
Processing /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/turbofan
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-EhMrdQ/wheels/bb/fc/4f/4d8fc3d9a877e197055fb41353396df25fa1b083450275d76f
Successfully built turbofan
Installing collected packages: turbofan
Successfully installed turbofan-0.0.0.0

Running tests...
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.
----------------------------------------------------------------------
Ran 1 test in 1.296s

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'...
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-RAXmDy
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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-cukGU8/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 2519607.85783 force_pound * meter but the right hand side evaluated to 2468463.75038 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 32774.4767708 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 2.21510116795 meter but the right hand side evaluated to 1.9639615988 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 48608.9395605 newton but the right hand side evaluated to 48529.7572849 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 49704.3710251 newton but the right hand side evaluated to 49411.0876612 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 18949.0883798 newton but the right hand side evaluated to 18923.0900357 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 16591.9863256 newton but the right hand side evaluated to 16565.7862786 newton (Allowable error: 0.1%, Actual error: 0.16%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1002807.16787 joule / kilogram but the right hand side evaluated to 1.15238790786 megajoule / kilogram (Allowable error: 0.1%, Actual error: 7.1%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 895037.190291 joule / kilogram but the right hand side evaluated to 0.897466347153 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 1072947.06205 joule / kilogram but the right hand side evaluated to 1.19569619038 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 596870.463325 joule / kilogram but the right hand side evaluated to 0.615557029614 megajoule / kilogram (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 786921.755792 joule / kilogram but the right hand side evaluated to 0.790360523486 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 18.346553451 meter but the right hand side evaluated to 16.3967757121 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 11.085406592589855 but the right hand side evaluated to 4.6807857965184345 (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 9.791743087697956 but the right hand side evaluated to 4.680785791905234 (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 8.229124024795148 but the right hand side evaluated to 4.6807857978453455 (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 18.4249255648 meter but the right hand side evaluated to 18.1659842819 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 18.4249255648 meter but the right hand side evaluated to 18.2854592552 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 0.3101211421164374 but the right hand side evaluated to 0.19292693596977523 (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 0.24134173384978652 but the right hand side evaluated to 0.17650128793006437 (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 7.275033677766071 but the right hand side evaluated to 4.615982690995383 (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 7.45366740700679 but the right hand side evaluated to 4.646341321722644 (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 2504976.84929 force_pound * meter but the right hand side evaluated to 2454470.95579 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 32774.4791742 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 2.21510116798 meter but the right hand side evaluated to 1.9638302882 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 982256.654819 joule / kilogram but the right hand side evaluated to 1.20546999087 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 1151137.27952 joule / kilogram but the right hand side evaluated to 1.88379372617 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 18.4111623027 meter but the right hand side evaluated to 16.4524821355 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 11.08931046761834 but the right hand side evaluated to 4.731321035771215 (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 9.749134133481242 but the right hand side evaluated to 4.731321029363463 (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 8.197834085644152 but the right hand side evaluated to 4.73132103806879 (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 18.4749973754 meter but the right hand side evaluated to 18.2223428226 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 18.4749973754 meter but the right hand side evaluated to 18.3384476999 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 0.30927837535228875 but the right hand side evaluated to 0.19273735259135072 (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 0.24173082661437562 but the right hand side evaluated to 0.17660062024980439 (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 7.430221978542619 but the right hand side evaluated to 4.666980724437886 (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 7.49547543212434 but the right hand side evaluated to 4.696716704572758 (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 2481458.80514 force_pound * meter but the right hand side evaluated to 2426089.95035 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 32774.3963932 force_pound but the right hand side evaluated to 32399.9999993 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 2.21510116802 meter but the right hand side evaluated to 1.83119931854 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 1203384.14401 joule / kilogram but the right hand side evaluated to 1.66383377265 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 18.4693769113 meter but the right hand side evaluated to 16.6432032196 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 11.047309473002242 but the right hand side evaluated to 4.801812718943481 (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 9.670710571574924 but the right hand side evaluated to 4.80181271471173 (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 8.221376685769343 but the right hand side evaluated to 4.801812720203433 (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 18.6280064463 meter but the right hand side evaluated to 18.3449863287 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 18.6280064463 meter but the right hand side evaluated to 18.474391872 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 0.32683411638417414 but the right hand side evaluated to 0.19660332574140757 (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 0.2527548383991274 but the right hand side evaluated to 0.17939017864624823 (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 7.455618958042141 but the right hand side evaluated to 4.7292258519724735 (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 7.5488750743215975 but the right hand side evaluated to 4.762585813630804 (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 2455569.18685 force_pound * meter but the right hand side evaluated to 2407712.52042 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 32774.4913265 force_pound but the right hand side evaluated to 32399.9999974 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 2.21510116763 meter but the right hand side evaluated to 1.99552156051 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 1227634.02165 joule / kilogram but the right hand side evaluated to 1.72359797784 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 677538.896697 joule / kilogram but the right hand side evaluated to 0.679181908741 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 18.4156371076 meter but the right hand side evaluated to 16.4239741799 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 10.974969120901777 but the right hand side evaluated to 4.7625542545649 (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 9.752894930207322 but the right hand side evaluated to 4.7625542389414175 (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 8.158717910330562 but the right hand side evaluated to 4.762554259021844 (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 18.4488742292 meter but the right hand side evaluated to 18.2046646696 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 18.4488742292 meter but the right hand side evaluated to 18.3176207225 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 0.30594658165821986 but the right hand side evaluated to 0.19198932475779276 (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 0.23933762901536415 but the right hand side evaluated to 0.17598559398433125 (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 7.50481891799817 but the right hand side evaluated to 4.699783041776793 (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 7.527659678284997 but the right hand side evaluated to 4.728944190943273 (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 2436786.37263 force_pound * meter but the right hand side evaluated to 2390898.72079 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 32774.4573522 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 2.21510116779 meter but the right hand side evaluated to 2.03201114236 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 1233975.43229 joule / kilogram but the right hand side evaluated to 1.62326175727 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 18.4095782885 meter but the right hand side evaluated to 16.3813520493 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 10.931049826624736 but the right hand side evaluated to 4.787717960045892 (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 9.873361714300493 but the right hand side evaluated to 4.787717947951635 (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 8.154647078389733 but the right hand side evaluated to 4.78771796320733 (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 18.4102723048 meter but the right hand side evaluated to 18.1746830502 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 18.4102723048 meter but the right hand side evaluated to 18.2839337645 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 0.3020986408628694 but the right hand side evaluated to 0.19112023139042567 (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 0.23685256184997616 but the right hand side evaluated to 0.17534369132653296 (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 7.536485238125241 but the right hand side evaluated to 4.726722219623846 (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 7.551401280099832 but the right hand side evaluated to 4.755135247640426 (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 2418323.59635 force_pound * meter but the right hand side evaluated to 2374882.72634 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 32774.4615307 force_pound but the right hand side evaluated to 32399.9999997 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 2.2151011681 meter but the right hand side evaluated to 2.08235854102 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 1244507.0209 joule / kilogram but the right hand side evaluated to 1.55927364174 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 664750.506802 joule / kilogram but the right hand side evaluated to 0.66740195071 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 18.4000455549 meter but the right hand side evaluated to 16.3223729972 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 10.90403832724449 but the right hand side evaluated to 4.7895019398330945 (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 10.025980375212445 but the right hand side evaluated to 4.789501935417018 (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 8.145555025787662 but the right hand side evaluated to 4.789501940884043 (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 18.3617948769 meter but the right hand side evaluated to 18.1374262841 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 18.3617948769 meter but the right hand side evaluated to 18.2416855738 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 0.2959608197337138 but the right hand side evaluated to 0.18972170220944604 (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 0.23297658739074212 but the right hand side evaluated to 0.17433509615866635 (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 7.565345374011845 but the right hand side evaluated to 4.731316762535067 (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 7.583817038693815 but the right hand side evaluated to 4.758513770390953 (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 2405738.01818 force_pound * meter but the right hand side evaluated to 2358168.34992 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 32774.4205402 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 2.21510116806 meter but the right hand side evaluated to 1.97490826737 meter (Allowable error: 0.1%, Actual error: 11%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1245747.21498 joule / kilogram but the right hand side evaluated to 1.357728868 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 18.444134383 meter but the right hand side evaluated to 16.4749800468 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 10.93310834385472 but the right hand side evaluated to 4.831717230069513 (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 10.192137907210045 but the right hand side evaluated to 4.831717209589433 (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 8.195656676828303 but the right hand side evaluated to 4.831717234190611 (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 18.4861321722 meter but the right hand side evaluated to 18.2368517033 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 18.4861321722 meter but the right hand side evaluated to 18.3518648192 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 0.310202666340456 but the right hand side evaluated to 0.1929419387246267 (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 0.2419155868033247 but the right hand side evaluated to 0.1766467420511594 (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 7.542128559077057 but the right hand side evaluated to 4.766977754898232 (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 7.597028891124651 but the right hand side evaluated to 4.797041330227309 (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 2391781.65425 force_pound * meter but the right hand side evaluated to 2346059.44284 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 32774.4065459 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 2.21510116802 meter but the right hand side evaluated to 2.01208176102 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 1263254.53855 joule / kilogram but the right hand side evaluated to 1.329337453 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 643003.200212 joule / kilogram but the right hand side evaluated to 0.644587801934 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 18.4391888545 meter but the right hand side evaluated to 16.4333021829 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 10.927058041225497 but the right hand side evaluated to 4.827096677910439 (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 10.332848779072133 but the right hand side evaluated to 4.827096654785315 (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 8.188196534278614 but the right hand side evaluated to 4.827096683603648 (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 18.4531703904 meter but the right hand side evaluated to 18.2123794727 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 18.4531703904 meter but the right hand side evaluated to 18.3237330754 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 0.30544737812145506 but the right hand side evaluated to 0.19187569551606895 (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 0.2388569453604239 but the right hand side evaluated to 0.17586142186386494 (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 7.554288706690349 but the right hand side evaluated to 4.764561603798662 (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/WingNoSt.
----------------------------------------------------------------------
Ran 1 test in 184.287s

OK

Generating XML reports...
ruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.617835846363629 but the right hand side evaluated to 4.793692948254549 (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 2376282.67177 force_pound * meter but the right hand side evaluated to 2334599.953 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 32774.5120109 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 2.21510116784 meter but the right hand side evaluated to 2.09817278146 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 1283641.40728 joule / kilogram but the right hand side evaluated to 1.28936197376 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 18.4146018644 meter but the right hand side evaluated to 16.3183414535 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 10.937463512880736 but the right hand side evaluated to 4.824379007576681 (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 10.571344663927368 but the right hand side evaluated to 4.8243789899948615 (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 8.193850969573035 but the right hand side evaluated to 4.824379012189718 (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 18.3565587891 meter but the right hand side evaluated to 18.1377553229 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 18.3565587891 meter but the right hand side evaluated to 18.2401778584 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 0.29417335805744216 but the right hand side evaluated to 0.1893110256457486 (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 0.23165686485295023 but the right hand side evaluated to 0.17398922949739076 (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 7.620071731589894 but the right hand side evaluated to 4.767020179706166 (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 7.689393446854206 but the right hand side evaluated to 4.793939182908527 (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 180 seconds.
Cloning into 'solar'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-hBelVY
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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-TEpSS3/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-HtJQU3
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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-pzT7pk/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
Processing /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/solar
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-65FJUJ/wheels/e6/64/44/feccaa8126c1cff55951fef02ce14d920ab588ce556b200a54
Successfully built solar
Installing collected packages: solar
Successfully installed solar-0.0.0.0

Running tests...
----------------------------------------------------------------------
/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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)
......
----------------------------------------------------------------------
Ran 6 tests in 261.120s

OK

Generating XML reports...
adding test for 'solar/solar.py'
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 1.77 seconds.
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 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 0.0339 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 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 0.0339 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 1.69 seconds.
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 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 0.0320 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 0.0346 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 0.1666 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 0.0320 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 0.0346 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 0.1666 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 0.0320 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 0.0346 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(0,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(3,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(4,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(2,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(1,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 1.6 seconds.
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 625493.9730 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 0.1713 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 0.0324 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 0.0352 but bound is 0.0500
Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 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 0.0324 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 0.0352 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(3,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(1,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(2,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(4,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(0,).
Using solver 'mosek'
Solving for 4707 variables.
Solving took 0.861 seconds.
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 642574.9339 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 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 1.65 seconds.
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 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 0.0339 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 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 0.0339 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 1.14 seconds.
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 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 0.0320 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 0.0346 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 0.1666 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 0.0320 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 0.0346 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 0.1666 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 0.0320 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 0.0346 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(0,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(3,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(4,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(2,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(1,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 1.15 seconds.
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 625493.9003 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 0.1713 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 0.0324 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 0.0352 but bound is 0.0500
Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 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 0.0324 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 0.0352 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(3,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(1,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(2,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(4,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(0,).
Using solver 'mosek'
Solving for 4707 variables.
Solving took 1.49 seconds.
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 642574.9337 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 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Using solver 'mosek'
Solving for 489 variables.
Solving took 0.676 seconds.
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 642574.3920 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 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Using solver 'mosek'
Solving for 489 variables.
Solving took 0.638 seconds.
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 642574.3919 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 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Using solver 'mosek'
Solving for 4707 variables.
Solving took 1.61 seconds.
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 642574.9341 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 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,).
Beginning signomial solve.
Solving took 4 GP solves and 14.8 seconds.
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 641279.3642 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 0.1713 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 0.0251 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 0.0368 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 0.1713 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 0.0251 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 0.0368 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Using solver 'mosek_cli'
Solving for 4707 variables.
Solving took 1.71 seconds.
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 642575.7579 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 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 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 0.0330 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 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,).
Beginning signomial solve.
Solving took 4 GP solves and 22.4 seconds.
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 641279.0650 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 0.1713 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 0.0251 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 0.0368 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 0.1713 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 0.0251 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 0.0368 but bound is 0.0500
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-0Vq1ab
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/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-g60Sa8/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
Processing /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/gplibrary
Requirement already satisfied: numpy>=1.12 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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/buildnode/macys_VM/optimizer/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-dmMgWw/wheels/7a/92/a8/fdca76a4db1a215e99bae5cd742ce73eb444ece71eebba5ed0
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 8 tests in 5.065s

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'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.019 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.254 seconds.
Using solver 'mosek'
Solving for 5 variables.
Solving took 0.0374 seconds.
Using solver 'mosek_cli'
Solving for 5 variables.
Solving took 0.244 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 1.831s

OK

Generating XML reports...
adding test for 'aircraft_models.py'
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {})

calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'})

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {})

[Execution node] check if [macys_VM] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys_VM/optimizer/mosek' for the testing framework 'JUnit'.
[xUnit] [INFO] - Check 'Failed Tests' threshold.
[xUnit] [INFO] - Check 'Skipped Tests' threshold.
[xUnit] [INFO] - Setting the build status to SUCCESS
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: SUCCESS