Started by upstream project "gplibrary_PR_Models" build number 71 originally caused by: GitHub pull request #158 of commit f28591b4b0076aa61ad8b3d63c4daa9322fc3408, no merge conflicts. Building remotely on windows7x64 in workspace D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\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\buildnode\windows7x64\optimizer\mosek # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git --version # timeout=10 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 > git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10 > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master Merging Revision 34a4748c5d33aa3e90a704092bc0232a5a842082 (refs/remotes/origin/pr/158/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 34a4748c5d33aa3e90a704092bc0232a5a842082 # timeout=10 > git rev-parse "HEAD^{commit}" # timeout=10 Seen branch in repository origin/1682literate Seen branch in repository origin/1682master Seen branch in repository origin/Breakdown Seen branch in repository origin/SPaircraft Seen branch in repository origin/aerosurf Seen branch in repository origin/atmosphere Seen branch in repository origin/bounds5 Seen branch in repository origin/boxspar Seen branch in repository origin/breguet_range Seen branch in repository origin/breguetsetup Seen branch in repository origin/climb Seen branch in repository origin/commercial_sizing Seen branch in repository origin/cosminus1 Seen 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branch in repository origin/troposphere Seen branch in repository origin/vectorizeplanform Seen branch in repository origin/wide_body Seen branch in repository origin/wvl Seen 195 remote branches > git show-ref --tags -d # timeout=10 Checking out Revision 34a4748c5d33aa3e90a704092bc0232a5a842082 (origin/pr/158/merge, origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f 34a4748c5d33aa3e90a704092bc0232a5a842082 # timeout=3 Commit message: "Merge f28591b4b0076aa61ad8b3d63c4daa9322fc3408 into 7acc2f8a183ff6438fe0f5a2592cb3dede6d24e6" Using 'Changelog to branch' strategy. Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [description-setter] Description set: PR 158: fix auto-diff for cosminus1 in gust loading [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\jenkins1609605307985605846.bat D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>echo 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\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;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;D:\Git\cmd 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\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;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;D:\Git\cmd D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>REM turn on the anaconda console D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>call activate.bat || exit /b 666 (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>REM Create a virtualenv to install everything into (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>SET VENV=D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>virtualenv --system-site-packages D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit New python executable in D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\Scripts\python.exe Installing setuptools, pip, wheel...done. (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>call D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\Scripts\activate.bat (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>REM Install coverage into the virtualenv to the coverage command blow uses the virtualenv python (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>pip install coverage Collecting coverage Using cached coverage-4.5.1-cp27-cp27m-win_amd64.whl Installing collected packages: coverage The scripts coverage-2.7.exe, coverage.exe and coverage2.exe are installed in 'd:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\Scripts' which is not on PATH. Consider adding this directory to PATH or, if you prefer to suppress this warning, use --no-warn-script-location. Successfully installed coverage-4.5.1 (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>if mosek == mosek msktestlic || exit /b 666 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: 0.02 Interior-point optimizer terminated. Time: 0.02. Optimizer terminated. Time: 0.44 ************************************ A license was checked out correctly. ************************************ (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>SET GPKITBUILD=D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\build_gpkit (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>gcc --version || exit /b 666 gcc (x86_64-posix-seh-rev1, Built by MinGW-W64 project) 6.3.0 Copyright (C) 2016 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) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>if mosek == cvxopt set GPKITSOLVERS=cvxopt (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>if mosek == mosek set GPKITSOLVERS=mosek, mosek_cli (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>dir D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\build_gpkit Volume in drive D is Home Volume Serial Number is EA39-7CA0 Directory of D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek File Not Found (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>python -c "import scipy; print scipy.__version__" 0.19.0 (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>python -c "import numpy; print numpy.__version__" 1.13.3 (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>python -c "import pint; print pint.__version__" 0.7.2 (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>REM Install gpkit to run the documentation examples (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>git clone --depth 1 https://github.com/convexengineering/gpkit.git Cloning into 'gpkit'... 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(venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>pip install -e D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\gpkit | exit /b 666 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 329 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 214 gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file __init__.py, line 30 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_install.py, line 893 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file install.py, line 354 (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>pip install -e D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek | exit /b 666 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 329 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file __init__.py, line 30 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_install.py, line 893 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file install.py, line 354 (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>REM Show the settings file (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>type D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\env\settings installed_solvers : mosek, mosek_cli mosek_bin_dir : C:\Program Files\Mosek\7\tools\platform\win64x86\bin (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\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/buildnode/windows7x64/optimizer/mosek Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Cloning into 'shopping'... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 1.03 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.561 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 13.1 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 17.333s OK Generating XML reports... Cloning into 'gassolar'... 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Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.20.1) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2016.10) Requirement already satisfied: numpy>=1.7.0 in d:\anaconda2\lib\site-packages (from pandas) (1.13.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.10.0) gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, 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-vqudls Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.13.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (0.19.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (0.7.2) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, which is not installed. Installing collected packages: gpfit Running setup.py install for gpfit: started Running setup.py install for gpfit: finished with status 'done' Successfully installed gpfit-0.1 Processing d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gassolar Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.13.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.19.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (0.20.1) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (0.7.2) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (2.6.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2016.10) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.10.0) 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-akmrji\wheels\27\2e\a1\4da6c2a362dd12f22914b14a911a1d857b1a34a0ded2fc094b Successfully built gassolar gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, 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 2.26 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 143 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 2.17 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 33 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 2.41 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1925 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.1335 but bound is 150000.0000 Beginning signomial solve. Solving took 4 GP solves and 64.9 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0986 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.9076 but bound is 150000.0000 Using solver 'mosek_cli' Solving for 1437 variables. Solving took 35 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 11.3 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\buildnode\windows7x64\optimizer\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 337.631s OK Generating XML reports... Cloning into 'jho'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.20.1) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2016.10) Requirement already satisfied: numpy>=1.7.0 in d:\anaconda2\lib\site-packages (from pandas) (1.13.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.10.0) gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, 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-hrevrm 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\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.13.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (0.19.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (0.7.2) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, 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 -7.86662401886e-14. Allowing negative dual variable(s) as small as -8.30429475185e-14. Allowing negative dual variable(s) as small as -1.5260275682e-13. Allowing negative dual variable(s) as small as -1.49674543592e-13. Solving took 4 GP solves and 13.7 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -8.14899363266e-14. Allowing negative dual variable(s) as small as -8.14842984753e-14. Allowing negative dual variable(s) as small as -1.50783031894e-13. Allowing negative dual variable(s) as small as -1.53209476356e-13. Solving took 4 GP solves and 8.56 seconds. Allowing negative dual variable(s) as small as -5.23601995095e-13. Allowing negative dual variable(s) as small as -5.1328385986e-13. Allowing negative dual variable(s) as small as -5.14793069284e-13. Allowing negative dual variable(s) as small as -5.14246631389e-13. Allowing negative dual variable(s) as small as -2.35874687837e-13. Allowing negative dual variable(s) as small as -1.83882856858e-14. Allowing negative dual variable(s) as small as -1.25902706229e-12. Allowing negative dual variable(s) as small as -1.26011852862e-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 -2.32925657928e-14. Allowing negative dual variable(s) as small as -1.13845348079e-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 -5.43412008022e-11. Allowing negative dual variable(s) as small as -6.44964609518e-12. Allowing negative dual variable(s) as small as -1.933928113e-11. Allowing negative dual variable(s) as small as -1.93544883916e-11. Solving took 4 GP solves and 9.2 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 25.6 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.24042614858e-13. Allowing negative dual variable(s) as small as -5.12017511722e-13. Allowing negative dual variable(s) as small as -5.16064621592e-13. Allowing negative dual variable(s) as small as -5.13849379713e-13. Allowing negative dual variable(s) as small as -2.38577820694e-13. Allowing negative dual variable(s) as small as -1.97746550037e-14. Allowing negative dual variable(s) as small as -1.25993551529e-12. Allowing negative dual variable(s) as small as -1.25922807338e-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 -2.1173167386e-14. Allowing negative dual variable(s) as small as -1.14869702292e-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 -5.43413274937e-11. Allowing negative dual variable(s) as small as -6.44969835232e-12. Allowing negative dual variable(s) as small as -1.93392439115e-11. Allowing negative dual variable(s) as small as -1.93546414307e-11. Solving took 4 GP solves and 363 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 68.2 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 574.593s OK Generating XML reports... Cloning into 'turbofan'... Processing d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\turbofan Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.13.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.19.0) Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.7.2) 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-dywzck\wheels\dd\4b\7e\92f7e903621e519a129c420d5ea6a42fdf8b25b6fdfc976a15 Successfully built turbofan gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires numpy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, 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 52.700s 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-it9nsi 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\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.13.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.19.0) Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.7.2) gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires numpy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, 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 2519606.47531 force_pound * meter but the right hand side evaluated to 2468461.52459 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 32774.4771235 force_pound but the right hand side evaluated to 32399.9999974 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116759 meter but the right hand side evaluated to 1.96396142373 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 48608.8489469 newton but the right hand side evaluated to 48529.6873163 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 49704.4388777 newton but the right hand side evaluated to 49411.1950495 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 18949.0400949 newton but the right hand side evaluated to 18923.0431358 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 16591.9668705 newton but the right hand side evaluated to 16565.760391 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 1002814.52409 joule / kilogram but the right hand side evaluated to 1.15242676377 megajoule / kilogram (Allowable error: 0.1%, Actual error: 7.1%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 895044.025708 joule / kilogram but the right hand side evaluated to 0.897472904602 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 1072947.50609 joule / kilogram but the right hand side evaluated to 1.19570990857 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 596870.846578 joule / kilogram but the right hand side evaluated to 0.615557304065 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 786925.016855 joule / kilogram but the right hand side evaluated to 0.790363989338 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 18.3465571428 meter but the right hand side evaluated to 16.3967792497 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 11.0854077197 but the right hand side evaluated to 4.68078908555 (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 9.79174324012 but the right hand side evaluated to 4.68078907579 (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 8.22912990096 but the right hand side evaluated to 4.68078908851 (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 18.4249287523 meter but the right hand side evaluated to 18.1659875221 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 18.4249287523 meter but the right hand side evaluated to 18.285462676 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 0.310121161893 but the right hand side evaluated to 0.192926923315 (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 0.241340692315 but the right hand side evaluated to 0.176500837503 (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 7.27503982032 but the right hand side evaluated to 4.61598595526 (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 7.45367143606 but the right hand side evaluated to 4.64634464794 (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 2504976.8886 force_pound * meter but the right hand side evaluated to 2454470.88726 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 32774.475379 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 2.21510116796 meter but the right hand side evaluated to 1.96383084357 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 982256.880439 joule / kilogram but the right hand side evaluated to 1.20547055551 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 1151137.29043 joule / kilogram but the right hand side evaluated to 1.88379423855 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 18.4111621027 meter but the right hand side evaluated to 16.4524813546 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 11.0893102187 but the right hand side evaluated to 4.73132120374 (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 9.74913478708 but the right hand side evaluated to 4.73132119702 (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 8.19783419709 but the right hand side evaluated to 4.73132120613 (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 18.4749966859 meter but the right hand side evaluated to 18.2223422677 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 18.4749966859 meter but the right hand side evaluated to 18.3384472983 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 0.309278312077 but the right hand side evaluated to 0.19273733762 (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 0.241730601959 but the right hand side evaluated to 0.176600552063 (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 7.4302230401 but the right hand side evaluated to 4.66698092093 (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 7.49547578507 but the right hand side evaluated to 4.6967169425 (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 2481459.44526 force_pound * meter but the right hand side evaluated to 2426090.44121 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 32774.4225976 force_pound but the right hand side evaluated to 32399.9999972 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 2.21510116711 meter but the right hand side evaluated to 1.83120442154 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 1203378.8769 joule / kilogram but the right hand side evaluated to 1.66380266247 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 18.4693759576 meter but the right hand side evaluated to 16.6431971188 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 11.0473046065 but the right hand side evaluated to 4.80180354667 (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 9.67070457276 but the right hand side evaluated to 4.8018035266 (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 8.22137159054 but the right hand side evaluated to 4.80180355256 (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 18.6280029359 meter but the right hand side evaluated to 18.3449833528 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 18.6280029359 meter but the right hand side evaluated to 18.4743880413 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 0.326833132239 but the right hand side evaluated to 0.19660302985 (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 0.252753753015 but the right hand side evaluated to 0.179389703977 (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 7.45561566733 but the right hand side evaluated to 4.72921700766 (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 7.54886827472 but the right hand side evaluated to 4.762576692 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2455568.61541 force_pound * meter but the right hand side evaluated to 2407712.32625 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 32774.4700885 force_pound but the right hand side evaluated to 32399.9999987 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116788 meter but the right hand side evaluated to 1.99552087206 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 1227634.0193 joule / kilogram but the right hand side evaluated to 1.72359791152 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 677538.889433 joule / kilogram but the right hand side evaluated to 0.679181903711 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 18.4156364599 meter but the right hand side evaluated to 16.4239741572 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 10.9749697764 but the right hand side evaluated to 4.76255526708 (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 9.75289622148 but the right hand side evaluated to 4.76255525708 (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 8.15871866563 but the right hand side evaluated to 4.76255526984 (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 18.4488738371 meter but the right hand side evaluated to 18.2046643011 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 18.4488738371 meter but the right hand side evaluated to 18.31762083 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 0.305946716167 but the right hand side evaluated to 0.191989375373 (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 0.239338438529 but the right hand side evaluated to 0.175986002541 (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 7.50481934213 but the right hand side evaluated to 4.69978402129 (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 7.52765978958 but the right hand side evaluated to 4.7289453 (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 2436785.62237 force_pound * meter but the right hand side evaluated to 2390898.55032 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 32774.4866533 force_pound but the right hand side evaluated to 32399.9999989 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116797 meter but the right hand side evaluated to 2.03201090387 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 1233975.11965 joule / kilogram but the right hand side evaluated to 1.62325951086 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 18.4095778123 meter but the right hand side evaluated to 16.3813517527 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 10.9310499904 but the right hand side evaluated to 4.7877184023 (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 9.87336377409 but the right hand side evaluated to 4.78771839497 (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 8.15464743597 but the right hand side evaluated to 4.78771840421 (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 18.4102718403 meter but the right hand side evaluated to 18.174682175 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 18.4102718403 meter but the right hand side evaluated to 18.2839316808 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 0.302098560112 but the right hand side evaluated to 0.191120152423 (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 0.236853174126 but the right hand side evaluated to 0.175343772566 (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 7.53648473911 but the right hand side evaluated to 4.72672252873 (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 7.55140036889 but the right hand side evaluated to 4.75513524568 (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 2418324.32625 force_pound * meter but the right hand side evaluated to 2374883.04474 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 32774.470114 force_pound but the right hand side evaluated to 32399.9999987 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116784 meter but the right hand side evaluated to 2.08235777027 meter (Allowable error: 0.1%, Actual error: 6%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1244507.20711 joule / kilogram but the right hand side evaluated to 1.55927598852 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 664750.555758 joule / kilogram but the right hand side evaluated to 0.667402034486 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 18.4000466737 meter but the right hand side evaluated to 16.3223749075 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 10.9040385668 but the right hand side evaluated to 4.7895023087 (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 10.0259804754 but the right hand side evaluated to 4.78950229749 (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 8.14555519828 but the right hand side evaluated to 4.78950231154 (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 18.361796643 meter but the right hand side evaluated to 18.1374280176 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 18.361796643 meter but the right hand side evaluated to 18.2416872255 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 0.295960974923 but the right hand side evaluated to 0.189721762502 (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 0.232976064311 but the right hand side evaluated to 0.174334850873 (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 7.56534608226 but the right hand side evaluated to 4.7313171455 (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 7.5838183521 but the right hand side evaluated to 4.7585141316 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2405739.12856 force_pound * meter but the right hand side evaluated to 2358168.71603 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 32774.3998145 force_pound but the right hand side evaluated to 32399.999998 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.2151011678 meter but the right hand side evaluated to 1.97490833534 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 1245747.46566 joule / kilogram but the right hand side evaluated to 1.35773097194 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 18.444135454 meter but the right hand side evaluated to 16.4749811597 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 10.9331079283 but the right hand side evaluated to 4.83171702951 (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 10.1921369429 but the right hand side evaluated to 4.83171698699 (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 8.19565628455 but the right hand side evaluated to 4.83171703829 (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 18.4861334325 meter but the right hand side evaluated to 18.2368528916 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 18.4861334325 meter but the right hand side evaluated to 18.351868134 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 0.310202676313 but the right hand side evaluated to 0.192941941886 (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 0.24191488244 but the right hand side evaluated to 0.17664667247 (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 7.54212824775 but the right hand side evaluated to 4.7669775914 (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 7.59702999728 but the right hand side evaluated to 4.79704171959 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2391779.33725 force_pound * meter but the right hand side evaluated to 2346059.3395 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 32774.4225458 force_pound but the right hand side evaluated to 32399.9999991 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 2.21510116809 meter but the right hand side evaluated to 2.0120819977 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 1263254.55374 joule / kilogram but the right hand side evaluated to 1.32933772155 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 643003.170168 joule / kilogram but the right hand side evaluated to 0.644587781095 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 18.4391885129 meter but the right hand side evaluated to 16.4333016073 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 10.9270581489 but the right hand side evaluated to 4.82709674307 (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 10.3328495033 but the right hand side evaluated to 4.8270967246 (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 8.18819658571 but the right hand side evaluated to 4.82709674757 (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 18.4531698278 meter but the right hand side evaluated to 18.2123788675 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 18.4531698278 meter but the right hand side evaluated to 18.3237332883 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 0.305447318797 but the right hand side evaluated to 0.191875666024 (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 0.238861275532 but the right hand side evaluated to 0.175863412758 (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 7.55428858402 but the right hand side evaluated to 4.76456164263 (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 7.61783172046 but the right hand side evaluated to 4.79369320232 (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 2376284.34377 force_pound * meter but the right hand side evaluated to 2334599.99931 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 32774.4170688 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 2.21510116785 meter but the right hand side evaluated to 2.09817090279 meter (Allowable error: 0.1%, Actual error: 5.3%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1283641.58251 joule / kilogram but the right hand side evaluated to 1.28936257384 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 18.414602325 meter but the right hand side evaluated to 16.3183438122 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 10.9374642354 but the right hand side evaluated to 4.8243789059 (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 10.5713450753 but the right hand side evaluated to 4.8243788864 (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 8.19385130411 but the right hand side evaluated to 4.82437891067 (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 18.3565607748 meter but the right hand side evaluated to 18.1377565741 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 18.3565607748 meter but the right hand side evaluated to 18.2401836504 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 0.29417353457 but the right hand side evaluated to 0.189311027005 (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 0.231655094104 but the right hand side evaluated to 0.173988893697 (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 7.62007113177 but the right hand side evaluated to 4.76701990415 (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 7.68939574806 but the right hand side evaluated to 4.79394009735 (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 953 seconds. Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 958.545s OK Generating XML reports... Cloning into 'solar'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.20.1) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2016.10) Requirement already satisfied: numpy>=1.7.0 in d:\anaconda2\lib\site-packages (from pandas) (1.13.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.10.0) gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires numpy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, 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-fyrkjo 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\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.13.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (0.19.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (0.7.2) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires numpy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, 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-umdyzf 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\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.13.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.19.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (0.20.1) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (0.7.2) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (2.6.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2016.10) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.10.0) gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires numpy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, which is not installed. Processing d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\solar Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.13.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.19.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (0.20.1) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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\buildnode\windows7x64\optimizer\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) (0.7.2) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (2.6.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2016.10) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.10.0) 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-5w9x9b\wheels\09\7a\4a\77e70a4d3b01c71b043502f2bf60681f14786c725c35efc56c Successfully built solar gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, which is not installed. gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. solar 0.0.0.0 requires numpy, which is not installed. solar 0.0.0.0 requires pandas, which is not installed. solar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires numpy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, 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' Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Using solver 'mosek' Solving for 9147 variables. Solving took 10.9 seconds. Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,). Using solver 'mosek' Solving for 9147 variables. Solving took 6.44 seconds. Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(0,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(3,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(4,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(2,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(1,). Using solver 'mosek' Solving for 9147 variables. Solving took 8.18 seconds. Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 625493.9618 but bound is 600000.0000 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(3,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(1,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(2,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(4,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(0,). Using solver 'mosek' Solving for 4707 variables. Solving took 14.2 seconds. Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 642574.9348 but bound is 600000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Using solver 'mosek' Solving for 9147 variables. Solving took 128 seconds. Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,). Using solver 'mosek' Solving for 9147 variables. Solving took 46.8 seconds. Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(0,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(3,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(4,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(2,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(1,). Using solver 'mosek' Solving for 9147 variables. Solving took 2.82 seconds. Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 625493.9636 but bound is 600000.0000 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(3,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(1,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(2,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(4,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(0,). Using solver 'mosek' Solving for 4707 variables. Solving took 2.52 seconds. Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 642574.9340 but bound is 600000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Using solver 'mosek' Solving for 489 variables. Solving took 1.02 seconds. Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642574.3920 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Using solver 'mosek' Solving for 489 variables. Solving took 0.399 seconds. Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642574.3920 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Using solver 'mosek' Solving for 4707 variables. Solving took 3.85 seconds. Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642574.9349 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,). Beginning signomial solve. Solving took 4 GP solves and 59.3 seconds. Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 641279.3491 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Using solver 'mosek_cli' Solving for 4707 variables. Solving took 3.17 seconds. Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642575.7579 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,). Beginning signomial solve. Solving took 4 GP solves and 154 seconds. Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 641279.0650 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500 Running tests... ---------------------------------------------------------------------- D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\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\buildnode\windows7x64\optimizer\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 755.785s OK Generating XML reports... Cloning into 'gplibrary'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.20.1) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2016.10) Requirement already satisfied: numpy>=1.7.0 in d:\anaconda2\lib\site-packages (from pandas) (1.13.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.10.0) gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, which is not installed. gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. solar 0.0.0.0 requires numpy, which is not installed. solar 0.0.0.0 requires pandas, which is not installed. solar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires numpy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, 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-berekn 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\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.13.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (0.19.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\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) (0.7.2) Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, which is not installed. gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. solar 0.0.0.0 requires numpy, which is not installed. solar 0.0.0.0 requires pandas, which is not installed. solar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires numpy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. Processing d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gplibrary Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.13.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.19.0) Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.7.2) 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-vluw5l\wheels\92\ce\06\ec49b09e82f01f946f52378df5a542ddac6d03b78d4466cd8e Successfully built gpkitmodels gpfit 0.1 requires numpy, which is not installed. gpfit 0.1 requires scipy, which is not installed. gassolar 0.0.0.0 requires numpy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires numpy>=1.12, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. solar 0.0.0.0 requires numpy, which is not installed. solar 0.0.0.0 requires pandas, which is not installed. solar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires numpy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires numpy>=1.12.1, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, 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 Running tests... ---------------------------------------------------------------------- ..EEEE ====================================================================== ERROR [0.051s]: test_gpkitmodels_GP_aircraft_tail_tail_tests_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "tail_tests.py", line 117, in test File "tail_tests.py", line 20, in test_htail File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\tail\tail_aero.py", line 44, in setup fd = pd.read_csv(path + os.sep + "tail_dragfit.csv").to_dict( File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 655, in parser_f return _read(filepath_or_buffer, kwds) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 405, in _read parser = TextFileReader(filepath_or_buffer, **kwds) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 762, in __init__ self._make_engine(self.engine) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 966, in _make_engine self._engine = CParserWrapper(self.f, **self.options) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 1582, in __init__ self._reader = parsers.TextReader(src, **kwds) File "pandas\_libs\parsers.pyx", line 394, in pandas._libs.parsers.TextReader.__cinit__ (pandas\_libs\parsers.c:4209) File "pandas\_libs\parsers.pyx", line 710, in pandas._libs.parsers.TextReader._setup_parser_source (pandas\_libs\parsers.c:8873) IOError: File D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\tail\tail_dragfit.csv does not exist ====================================================================== ERROR [0.035s]: test_gpkitmodels_GP_aircraft_tail_tail_tests_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "tail_tests.py", line 117, in test File "tail_tests.py", line 20, in test_htail File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\tail\tail_aero.py", line 44, in setup fd = pd.read_csv(path + os.sep + "tail_dragfit.csv").to_dict( File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 655, in parser_f return _read(filepath_or_buffer, kwds) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 405, in _read parser = TextFileReader(filepath_or_buffer, **kwds) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 762, in __init__ self._make_engine(self.engine) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 966, in _make_engine self._engine = CParserWrapper(self.f, **self.options) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 1582, in __init__ self._reader = parsers.TextReader(src, **kwds) File "pandas\_libs\parsers.pyx", line 394, in pandas._libs.parsers.TextReader.__cinit__ (pandas\_libs\parsers.c:4209) File "pandas\_libs\parsers.pyx", line 710, in pandas._libs.parsers.TextReader._setup_parser_source (pandas\_libs\parsers.c:8873) IOError: File D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\tail\tail_dragfit.csv does not exist ====================================================================== ERROR [0.080s]: test_gpkitmodels_GP_aircraft_wing_wing_test_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "wing_test.py", line 85, in test File "wing_test.py", line 33, in wing_test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\wing\wing.py", line 123, in setup df = pd.read_csv(fitdata) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 655, in parser_f return _read(filepath_or_buffer, kwds) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 405, in _read parser = TextFileReader(filepath_or_buffer, **kwds) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 762, in __init__ self._make_engine(self.engine) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 966, in _make_engine self._engine = CParserWrapper(self.f, **self.options) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 1582, in __init__ self._reader = parsers.TextReader(src, **kwds) File "pandas\_libs\parsers.pyx", line 394, in pandas._libs.parsers.TextReader.__cinit__ (pandas\_libs\parsers.c:4209) File "pandas\_libs\parsers.pyx", line 710, in pandas._libs.parsers.TextReader._setup_parser_source (pandas\_libs\parsers.c:8873) IOError: File D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\wing\jho_fitdata.csv does not exist ====================================================================== ERROR [0.072s]: test_gpkitmodels_GP_aircraft_wing_wing_test_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "d:\jenkins\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' Using solver 'mosek' Solving for 11 variables. Solving took 10.6 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 5.51 seconds. workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "wing_test.py", line 85, in test File "wing_test.py", line 33, in wing_test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\wing\wing.py", line 123, in setup df = pd.read_csv(fitdata) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 655, in parser_f return _read(filepath_or_buffer, kwds) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 405, in _read parser = TextFileReader(filepath_or_buffer, **kwds) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 762, in __init__ self._make_engine(self.engine) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 966, in _make_engine self._engine = CParserWrapper(self.f, **self.options) File "D:\Anaconda2\lib\site-packages\pandas\io\parsers.py", line 1582, in __init__ self._reader = parsers.TextReader(src, **kwds) File "pandas\_libs\parsers.pyx", line 394, in pandas._libs.parsers.TextReader.__cinit__ (pandas\_libs\parsers.c:4209) File "pandas\_libs\parsers.pyx", line 710, in pandas._libs.parsers.TextReader._setup_parser_source (pandas\_libs\parsers.c:8873) IOError: File D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\wing\jho_fitdata.csv does not exist ---------------------------------------------------------------------- Ran 6 tests in 17.449s FAILED (errors=4) Generating XML reports... Cloning into 'eVTOL'... Checking out files: 93% (87/93) Checking out files: 94% (88/93) Checking out files: 95% (89/93) Checking out files: 96% (90/93) Checking out files: 97% (91/93) Checking out files: 98% (92/93) Checking out files: 100% (93/93) Checking out files: 100% (93/93), done. adding test for 'aircraft_models.py' Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 95.277s OK Generating XML reports... 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(, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 SETTINGS defaultdict(, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['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(, {'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(, {'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(, {'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(, {'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(, {'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(, {}) (venv2_gpkit) (root) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>exit 0 Build step 'Console output (build log) parsing' changed build result to FAILURE [xUnit] [INFO] - Starting to record. [xUnit] [INFO] - Processing JUnit [xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek' for the testing framework 'JUnit'. [xUnit] [INFO] - Check 'Failed Tests' threshold. [xUnit] [INFO] - Check 'Skipped Tests' threshold. [xUnit] [INFO] - Setting the build status to FAILURE [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: FAILURE