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Started by upstream project "gplibrary_PR_Models" build number 80 originally caused by: GitHub pull request #162 of commit 13dacb519885471caf91ec4a014c83481c27125f, no merge conflicts. Building remotely on windows7x64 in workspace D:\jenkins\workspace\gplibrary_PR_Models\mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > git init D:\jenkins\workspace\gplibrary_PR_Models\mosek # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git --version # timeout=10 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 > git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10 > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master Merging Revision a1ac50e04a1cd7750304771d1a478fe308de892d (refs/remotes/origin/pr/162/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 a1ac50e04a1cd7750304771d1a478fe308de892d # timeout=10 > git rev-parse "HEAD^{commit}" # timeout=10 Seen branch in repository origin/1682literate Seen branch in repository origin/1682master Seen branch in repository origin/Breakdown Seen branch in repository origin/SPaircraft Seen branch in repository origin/add_init Seen branch in repository origin/aerosurf Seen branch in repository origin/atmosphere Seen branch in repository origin/bounds5 Seen branch in repository origin/boxspar Seen branch in repository origin/breguet_range Seen branch in repository origin/breguetsetup Seen branch in repository origin/climb Seen branch in repository origin/commercial_sizing Seen branch in repository origin/d8 Seen 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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="Added __init__.py to git tracking" href="https://github.com/convexengineering/gplibrary/pull/162">PR 162</a>: Added __init__.py to git tracking [Execution node] check if [windows7x64] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [windows7x64] is in [[windows10x64, windows7x64]] Run condition [Execution node ] enabling perform for step [Execute Windows batch command] [mosek] $ cmd /c call C:\Users\jenkins\AppData\Local\Temp\jenkins7509284415086504689.bat D:\jenkins\workspace\gplibrary_PR_Models\mosek>echo C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM turn on the anaconda console D:\jenkins\workspace\gplibrary_PR_Models\mosek>call activate.bat || exit /b 666 (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM Create a virtualenv to install everything into (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>SET VENV=D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>virtualenv --system-site-packages D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit || exit /b 666 New python executable in D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts\python.exe Installing setuptools, pip, wheel...done. (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>call D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts\activate.bat || exit /b 666 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>set PATH=C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts;D:\Anaconda2;D:\Anaconda2\Library\mingw-w64\bin;D:\Anaconda2\Library\usr\bin;D:\Anaconda2\Library\bin;D:\Anaconda2\Scripts;D:\Anaconda2\bin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM set PATH=C:\mingw-w64\x86_64-7.3.0-posix-seh-rt_v5-rev0\mingw64\bin;C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts;D:\Anaconda2;D:\Anaconda2\Library\mingw-w64\bin;D:\Anaconda2\Library\usr\bin;D:\Anaconda2\Library\bin;D:\Anaconda2\Scripts;D:\Anaconda2\bin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>gcc --version || exit /b 666 gcc (x86_64-posix-seh-rev0, Built by MinGW-W64 project) 6.4.0 Copyright (C) 2017 Free Software Foundation, Inc. This is free software; see the source for copying conditions. There is NO warranty; not even for MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM upgdade pip (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>python -m pip install --upgrade pip || exit /b 666 Requirement already up-to-date: pip in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (10.0.1) grin 1.2.1 requires argparse>=1.1, which is not installed. (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM Install coverage into the virtualenv to the coverage command blow uses the virtualenv python (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>pip install --upgrade coverage || exit /b 666 Collecting coverage Using cached https://files.pythonhosted.org/packages/a6/2c/39d7da4ea22cf32fd43a72732a4009891d17f237a0ac24bb99ed88e3a86b/coverage-4.5.1-cp27-cp27m-win_amd64.whl grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: coverage Successfully installed coverage-4.5.1 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>SET GPKITBUILD=D:\jenkins\workspace\gplibrary_PR_Models\mosek\build_gpkit (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>if mosek == cvxopt ( pip install --upgrade cvxopt || exit /b 666 set GPKITSOLVERS=cvxopt ) (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>if mosek == mosek ( msktestlic || exit /b 666 python -c "__import__('mosek').Env()" || exit /b 666 set GPKITSOLVERS=mosek, mosek_cli ) Computer Platform : Windows/64-X86 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: 0.09 ************************************ A license was checked out correctly. ************************************ (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>dir D:\jenkins\workspace\gplibrary_PR_Models\mosek\build_gpkit Volume in drive D is Home Volume Serial Number is EA39-7CA0 Directory of D:\jenkins\workspace\gplibrary_PR_Models\mosek File Not Found (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import scipy; print scipy.__version__" || exit /b 666 1.0.1 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import numpy; print numpy.__version__" || exit /b 666 1.14.2 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import pint; print pint.__version__" || exit /b 666 0.8.1 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM Install gpkit to run the documentation examples (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>git clone --depth 1 https://github.com/convexengineering/gpkit.git || exit /b 666 Cloning into 'gpkit'... 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(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>pip install -e D:\jenkins\workspace\gplibrary_PR_Models\mosek\gpkit || exit /b 666 Obtaining file:///D:/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit Requirement already satisfied: numpy>=1.12.1 in d:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.14.2) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (0.8.1) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.0.1) Collecting ad (from gpkit==0.7.0.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: ad, gpkit Running setup.py develop for gpkit Successfully installed ad-1.3.2 gpkit (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>pip install -e D:\jenkins\workspace\gplibrary_PR_Models\mosek || exit /b 666 Obtaining file:///D:/jenkins/workspace/gplibrary_PR_Models/mosek Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1) grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gpkitmodels Running setup.py develop for gpkitmodels Successfully installed gpkitmodels (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM Show the settings file (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>type D:\jenkins\workspace\gplibrary_PR_Models\mosek\gpkit\gpkit\env\settings installed_solvers : mosek, mosek_cli mosek_bin_dir : C:\Program Files\Mosek\7\tools\platform\win64x86\bin (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM Limit number of threads mosek can use (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>set MSK_IPAR_NUM_THREADS=2 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)" Obtaining file:///D:/jenkins/workspace/gplibrary_PR_Models/mosek Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Cloning into 'shopping'... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 2.92 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.455 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 3.78 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 10.468s OK Generating XML reports... Cloning into 'gassolar'... 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Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-t9qsti Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-3darix\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gpfit Successfully installed gpfit-0.1 Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gassolar Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\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: still running... Running setup.py bdist_wheel for gassolar: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-9gm64q\wheels\08\33\b8\d36cec4e8239569444cd725d0dbfe83a0cfc534951775e5535 Successfully built gassolar grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gassolar Successfully installed gassolar-0.0.0.0 adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 609 variables. Solving took 0.138 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 11 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 8.52 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 7.79 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 4.94 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1924 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 10.4 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0985 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 5.43 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 14.9 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 Running tests... ---------------------------------------------------------------------- ..D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 4 tests in 174.007s OK Generating XML reports... Cloning into 'jho'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-lapdid Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-lxzpye\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -8.070757603895196e-14. Allowing negative dual variable(s) as small as -8.167338333420204e-14. Allowing negative dual variable(s) as small as -1.5013294427101975e-13. Allowing negative dual variable(s) as small as -1.498523527487805e-13. Solving took 4 GP solves and 22.7 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -8.092615119692503e-14. Allowing negative dual variable(s) as small as -8.331313069986912e-14. Allowing negative dual variable(s) as small as -1.4854827437571494e-13. Allowing negative dual variable(s) as small as -1.5035585623768277e-13. Solving took 4 GP solves and 25.9 seconds. Allowing negative dual variable(s) as small as -5.245769096884345e-13. Allowing negative dual variable(s) as small as -5.133411057345327e-13. Allowing negative dual variable(s) as small as -5.157489019191885e-13. Allowing negative dual variable(s) as small as -5.160958466143839e-13. Allowing negative dual variable(s) as small as -2.3804786267178635e-13. Allowing negative dual variable(s) as small as -1.9255647423777056e-14. Allowing negative dual variable(s) as small as -1.2582259453081113e-12. Allowing negative dual variable(s) as small as -1.2602281414600403e-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 -1.975806671050684e-14. Allowing negative dual variable(s) as small as -1.134721656914639e-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 -5.434126862779185e-11. Allowing negative dual variable(s) as small as -6.449560335688316e-12. Allowing negative dual variable(s) as small as -1.933920869309646e-11. Allowing negative dual variable(s) as small as -1.9354706988948867e-11. Solving took 4 GP solves and 10.3 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 9.58 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.238101619120528e-13. Allowing negative dual variable(s) as small as -5.126749719197576e-13. Allowing negative dual variable(s) as small as -5.146594955762751e-13. Allowing negative dual variable(s) as small as -5.169441263941366e-13. Allowing negative dual variable(s) as small as -2.3776987323476106e-13. Allowing negative dual variable(s) as small as -1.8218933306446417e-14. Allowing negative dual variable(s) as small as -1.2604569081184347e-12. Allowing negative dual variable(s) as small as -1.259798363718867e-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 -2.3087434741775326e-14. Allowing negative dual variable(s) as small as -1.1394617888127456e-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 -5.4341336308265437e-11. Allowing negative dual variable(s) as small as -6.449682554310503e-12. Allowing negative dual variable(s) as small as -1.9339259673706685e-11. Allowing negative dual variable(s) as small as -1.9354613560738328e-11. Solving took 4 GP solves and 17.2 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 5.48 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 270.736s OK Generating XML reports... Cloning into 'turbofan'... Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\turbofan Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-1os6rm\wheels\e5\cb\a8\3b11c975e79b3f632de8c1b88ce438a834a6b07b3850d6b107 Successfully built turbofan grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: turbofan Successfully installed turbofan-0.0.0.0 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%) Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 29.212s OK Generating XML reports... 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Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to c:\users\jenkins\appdata\local\temp\pip-req-build-wljgjz Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-fuvamz\wheels\49\e6\3a\5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5 Successfully built turbofan grin 1.2.1 requires argparse>=1.1, which is not installed. 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 2519603.95969 force_pound * meter but the right hand side evaluated to 2468460.60417 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 32774.4141117 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 2.21510116804 meter but the right hand side evaluated to 1.96396107319 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 48608.8188243 newton but the right hand side evaluated to 48529.6612775 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 49704.4426537 newton but the right hand side evaluated to 49411.2065223 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 18949.0266704 newton but the right hand side evaluated to 18923.0298776 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 16591.9590429 newton but the right hand side evaluated to 16565.7513459 newton (Allowable error: 0.1%, Actual error: 0.16%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1002815.94364 joule / kilogram but the right hand side evaluated to 1.1524342056 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 895045.449698 joule / kilogram but the right hand side evaluated to 0.897474268685 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 1072947.60152 joule / kilogram but the right hand side evaluated to 1.1957125741 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 596870.863374 joule / kilogram but the right hand side evaluated to 0.61555731595 megajoule / kilogram (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 786925.618718 joule / kilogram but the right hand side evaluated to 0.790364629068 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 18.3465563238 meter but the right hand side evaluated to 16.3967787164 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 11.08540901095908 but the right hand side evaluated to 4.68079002834237 (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 9.79174494645969 but the right hand side evaluated to 4.68079002502152 (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 8.229131630581385 but the right hand side evaluated to 4.680790029290953 (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 18.4249278879 meter but the right hand side evaluated to 18.1659872842 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 18.4249278879 meter but the right hand side evaluated to 18.285466507 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 0.31012135271803043 but the right hand side evaluated to 0.19292705760356585 (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 0.24134453893771202 but the right hand side evaluated to 0.17650303933498424 (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 7.275041079892281 but the right hand side evaluated to 4.615987012580594 (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 7.453669479695587 but the right hand side evaluated to 4.646346746532252 (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 2504976.82928 force_pound * meter but the right hand side evaluated to 2454470.90385 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 32774.4886928 force_pound but the right hand side evaluated to 32399.9999988 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 2.21510116796 meter but the right hand side evaluated to 1.96383091669 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 982256.847174 joule / kilogram but the right hand side evaluated to 1.20547041387 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 1151137.28385 joule / kilogram but the right hand side evaluated to 1.88379396364 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 18.4111621228 meter but the right hand side evaluated to 16.4524813164 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 11.08931024295829 but the right hand side evaluated to 4.731321114437365 (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 9.749134588768381 but the right hand side evaluated to 4.731321107555414 (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 8.19783413650153 but the right hand side evaluated to 4.731321116784794 (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 18.4749966789 meter but the right hand side evaluated to 18.2223419336 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 18.4749966789 meter but the right hand side evaluated to 18.338446447 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 0.30927821036603476 but the right hand side evaluated to 0.19273726537173738 (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 0.2417305161769825 but the right hand side evaluated to 0.1766004211372523 (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 7.430222930137697 but the right hand side evaluated to 4.666980750368579 (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 7.4954755679127985 but the right hand side evaluated to 4.69671663893166 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2481461.4626 force_pound * meter but the right hand side evaluated to 2426090.85609 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 32774.4313037 force_pound but the right hand side evaluated to 32399.999997 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116712 meter but the right hand side evaluated to 1.83120289394 meter (Allowable error: 0.1%, Actual error: 17%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1203378.52247 joule / kilogram but the right hand side evaluated to 1.66380513697 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 18.4693766079 meter but the right hand side evaluated to 16.6431991927 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 11.047306077558838 but the right hand side evaluated to 4.801805728674114 (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 9.67070801766922 but the right hand side evaluated to 4.801805708871408 (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 8.221372652368029 but the right hand side evaluated to 4.801805734508672 (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 18.6280043637 meter but the right hand side evaluated to 18.3449807516 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 18.6280043637 meter but the right hand side evaluated to 18.4743844817 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 0.3268324020253752 but the right hand side evaluated to 0.196602326982677 (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 0.25274985731680655 but the right hand side evaluated to 0.1793874600305886 (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 7.455615465527894 but the right hand side evaluated to 4.729218113398977 (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 7.548872789795769 but the right hand side evaluated to 4.762577563207992 (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 2455569.31212 force_pound * meter but the right hand side evaluated to 2407712.43634 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 32774.4503161 force_pound but the right hand side evaluated to 32399.9999985 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116778 meter but the right hand side evaluated to 1.99552062726 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 1227634.05261 joule / kilogram but the right hand side evaluated to 1.72359796565 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 677538.914016 joule / kilogram but the right hand side evaluated to 0.679181926131 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 18.4156368364 meter but the right hand side evaluated to 16.4239747921 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 10.97496968310333 but the right hand side evaluated to 4.762555299853518 (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 9.7528957849113 but the right hand side evaluated to 4.762555287049334 (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 8.15871865283404 but the right hand side evaluated to 4.762555303338547 (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 18.4488744469 meter but the right hand side evaluated to 18.2046648322 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 18.4488744469 meter but the right hand side evaluated to 18.3176226028 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 0.3059467542061567 but the right hand side evaluated to 0.1919893835007872 (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 0.2393377629239115 but the right hand side evaluated to 0.17598583799754774 (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 7.504819456570612 but the right hand side evaluated to 4.69978404539361 (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 7.527660837824618 but the right hand side evaluated to 4.728945643966491 (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 2436786.59978 force_pound * meter but the right hand side evaluated to 2390898.81664 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 32774.4729179 force_pound but the right hand side evaluated to 32399.9999977 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 2.21510116761 meter but the right hand side evaluated to 2.03201036115 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 1233975.20584 joule / kilogram but the right hand side evaluated to 1.62325857833 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 18.4095790279 meter but the right hand side evaluated to 16.3813535355 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 10.931049346424732 but the right hand side evaluated to 4.78771805744195 (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 9.873361551914304 but the right hand side evaluated to 4.78771804123026 (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 8.154647187498638 but the right hand side evaluated to 4.787718061857711 (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 18.4102736569 meter but the right hand side evaluated to 18.1746843971 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 18.4102736569 meter but the right hand side evaluated to 18.2839342813 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 0.3020987852483268 but the right hand side evaluated to 0.19112028759735633 (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 0.23685232682103674 but the right hand side evaluated to 0.17534349021683743 (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 7.536484913246574 but the right hand side evaluated to 4.726722329230757 (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 7.551401624001962 but the right hand side evaluated to 4.7551351399124755 (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 2418323.31997 force_pound * meter but the right hand side evaluated to 2374882.93362 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 32774.4913283 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116794 meter but the right hand side evaluated to 2.08235680501 meter (Allowable error: 0.1%, Actual error: 6%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1244506.9807 joule / kilogram but the right hand side evaluated to 1.55927311024 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 664750.403866 joule / kilogram but the right hand side evaluated to 0.667401844305 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 18.4000466435 meter but the right hand side evaluated to 16.3223757559 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 10.904038707595356 but the right hand side evaluated to 4.789502539242626 (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 10.02598019888318 but the right hand side evaluated to 4.789502531006663 (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 8.145555584724628 but the right hand side evaluated to 4.789502541400189 (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 18.3617972249 meter but the right hand side evaluated to 18.1374281764 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 18.3617972249 meter but the right hand side evaluated to 18.2416869069 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 0.29596101730167046 but the right hand side evaluated to 0.18972173291676037 (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 0.23297762871606764 but the right hand side evaluated to 0.17433543667678292 (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 7.565345957788949 but the right hand side evaluated to 4.731317249540295 (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 7.583816350983631 but the right hand side evaluated to 4.75851411149791 (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 2405737.98364 force_pound * meter but the right hand side evaluated to 2358168.33371 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 32774.4146854 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 2.21510116801 meter but the right hand side evaluated to 1.97491276643 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 1245747.44828 joule / kilogram but the right hand side evaluated to 1.35773096645 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 18.4441331755 meter but the right hand side evaluated to 16.4749746363 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 10.933105905648256 but the right hand side evaluated to 4.831717003088023 (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 10.192137878650591 but the right hand side evaluated to 4.831716979069152 (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 8.195655136007263 but the right hand side evaluated to 4.831717008028678 (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 18.4861277663 meter but the right hand side evaluated to 18.2368481701 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 18.4861277663 meter but the right hand side evaluated to 18.3518614646 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 0.3102021501047689 but the right hand side evaluated to 0.19294182222920905 (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 0.24191513903948714 but the right hand side evaluated to 0.17664667200697162 (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 7.54212823746992 but the right hand side evaluated to 4.766977773552252 (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 7.597028828648068 but the right hand side evaluated to 4.797041401516232 (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 2391781.28207 force_pound * meter but the right hand side evaluated to 2346059.7902 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 32774.3758532 force_pound but the right hand side evaluated to 32399.9999977 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 2.21510116775 meter but the right hand side evaluated to 2.01208139148 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 1263254.79559 joule / kilogram but the right hand side evaluated to 1.329338295 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 643003.295365 joule / kilogram but the right hand side evaluated to 0.644587900082 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 18.4391901405 meter but the right hand side evaluated to 16.4333039324 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 10.927057482280002 but the right hand side evaluated to 4.827096496974664 (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 10.33284614644894 but the right hand side evaluated to 4.827096448636168 (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 8.188196229148135 but the right hand side evaluated to 4.827096508863237 (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 18.4531721985 meter but the right hand side evaluated to 18.2123809959 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 18.4531721985 meter but the right hand side evaluated to 18.3237391539 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 0.3054474094144082 but the right hand side evaluated to 0.19187568542278866 (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 0.23885969469387014 but the right hand side evaluated to 0.17586312329941317 (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 7.55428854399053 but the right hand side evaluated to 4.764561409578844 (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 7.617834205898077 but the right hand side evaluated to 4.793693942121613 (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 2376282.66924 force_pound * meter but the right hand side evaluated to 2334599.67255 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 32774.4595357 force_pound but the right hand side evaluated to 32399.9999995 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 2.09817217167 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 1283640.74713 joule / kilogram but the right hand side evaluated to 1.28935944788 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 18.4146008737 meter but the right hand side evaluated to 16.318341013 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 10.937464333564606 but the right hand side evaluated to 4.824379093653517 (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 10.571347673194762 but the right hand side evaluated to 4.82437908578113 (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 8.193851527992576 but the right hand side evaluated to 4.824379095585631 (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 18.3565581168 meter but the right hand side evaluated to 18.1377541052 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 18.3565581168 meter but the right hand side evaluated to 18.2401789184 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 0.2941733119820551 but the right hand side evaluated to 0.1893109499762609 (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 0.23165673061620762 but the right hand side evaluated to 0.17398937341863424 (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 7.620071012778696 but the right hand side evaluated to 4.767020067871863 (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 7.689393401938558 but the right hand side evaluated to 4.793939670895413 (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 455 seconds. Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 479.379s OK Generating XML reports... Cloning into 'solar'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-opu0vn Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-h5jqwm\wheels\d5\94\ac\b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12 Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/convexengineering/gassolar.git Cloning https://github.com/convexengineering/gassolar.git to c:\users\jenkins\appdata\local\temp\pip-req-build-gn3v_h Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-gqox_p\wheels\fe\11\0a\2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e Successfully built gassolar grin 1.2.1 requires argparse>=1.1, which is not installed. Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\solar Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1) Requirement already satisfied: gpkitmodels in d:\jenkins\workspace\gplibrary_pr_models\mosek (from solar==0.0.0.0) (0.0.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-sjngmv\wheels\9f\ae\a9\52e286ff9ea1428d6dd1e8c6df0d12b22c44363d9dcc1dd331 Successfully built solar grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: solar Successfully installed solar-0.0.0.0 adding test for 'solar/solar.py' adding test for 'solar/sens_chart.py' adding test for 'solar/season.py' Using solver 'mosek' Solving for 9147 variables. Solving took 2.21 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 Using solver 'mosek' Solving for 9147 variables. Solving took 2.14 seconds. Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 622825.3313 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 0.1665 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 0.1665 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 0.1665 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 Using solver 'mosek' Solving for 9147 variables. Solving took 2.16 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 649649.6903 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 Using solver 'mosek' Solving for 4707 variables. Solving took 1.38 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 667434.8026 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 0.1740 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 0.1740 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 Using solver 'mosek' Solving for 9147 variables. Solving took 2.4 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 Using solver 'mosek' Solving for 9147 variables. Solving took 2.26 seconds. Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 622825.2882 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 0.1665 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 0.1665 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 0.1665 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 Using solver 'mosek' Solving for 9147 variables. Solving took 2.63 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 649652.1055 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 Using solver 'mosek' Solving for 4707 variables. Solving took 1.37 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 667434.8030 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 0.1740 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 0.1740 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 Using solver 'mosek' Solving for 489 variables. Solving took 0.185 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 667434.0884 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 0.1740 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 0.1740 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 Using solver 'mosek' Solving for 489 variables. Solving took 0.213 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 667434.0885 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 0.1740 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 0.1740 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 Using solver 'mosek' Solving for 4707 variables. Solving took 1.41 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 667434.8025 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 0.1740 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 0.1740 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 Beginning signomial solve. Solving took 4 GP solves and 11.7 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 666163.9468 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 0.0367 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 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 0.0367 but bound is 0.0500 Using solver 'mosek_cli' Solving for 4707 variables. Solving took 1.83 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 667436.8113 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 0.1740 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 0.1740 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 Beginning signomial solve. Solving took 4 GP solves and 34.2 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 666163.2236 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 0.0367 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 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 0.0367 but bound is 0.0500 Running tests... ---------------------------------------------------------------------- D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\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 459.961s OK Generating XML reports... Cloning into 'gplibrary'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-ujhghz Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-e2zh0g\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gplibrary Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-taekj4\wheels\4a\da\60\bea5372bf288606a399bdc749979f532f5aff24f4c362a9887 Successfully built gpkitmodels grin 1.2.1 requires argparse>=1.1, which is not installed. 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 adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py' adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py' adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py' adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py' adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py' Using solver 'mosek' Solving for 11 variables. Solving took 0.033 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.113 seconds. Using solver 'mosek' Solving for 8 variables. Solving took 0.02 seconds. Using solver 'mosek' Solving for 24 variables. Solving took 0.02 seconds. Using solver 'mosek' Solving for 24 variables. Solving took 0.031 seconds. Using solver 'mosek_cli' Solving for 8 variables. Solving took 0.096 seconds. Using solver 'mosek_cli' Solving for 24 variables. Solving took 0.08 seconds. Using solver 'mosek_cli' Solving for 24 variables. Solving took 0.127 seconds. Using solver 'mosek' Solving for 13 variables. Solving took 0.038 seconds. Using solver 'mosek_cli' Solving for 13 variables. Solving took 0.103 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 Running tests... ---------------------------------------------------------------------- .......... ---------------------------------------------------------------------- Ran 10 tests in 6.856s OK Generating XML reports... Cloning into 'eVTOL'... 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USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY calling ['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 ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['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 ['pip', 'install', 'pandas'] attempt 1 calling ['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 ['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 ['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 ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['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 ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>exit 0 [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 'D:\jenkins\workspace\gplibrary_PR_Models\mosek' for the testing framework 'JUnit'. [xUnit] [INFO] - Check 'Failed Tests' threshold. [xUnit] [INFO] - Check 'Skipped Tests' threshold. [xUnit] [INFO] - Setting the build status to SUCCESS [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: SUCCESS