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Started by upstream project "gplibrary_PR_Models" build number 63 originally caused by: GitHub pull request #146 of commit 6a04d7a8531e7ba8ef06aa8f9881443b92d069c7, 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 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 (refs/remotes/origin/pr/146/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 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 # 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/boombeam Seen branch in repository origin/boxspar Seen branch in repository origin/breguet_range Seen branch in repository origin/breguetsetup Seen branch in repository origin/climb Seen branch in repository origin/commercial_sizing Seen branch in repository origin/d8 Seen branch 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rev-parse "refs/tags/pshaft^{commit}" # timeout=10 > git rev-parse "refs/tags/solarmd^{commit}" # timeout=10 > git rev-parse "refs/tags/climb^{commit}" # timeout=10 > git rev-parse "refs/tags/fuse^{commit}" # timeout=10 > git rev-parse "refs/tags/mission^{commit}" # timeout=10 > git rev-parse "refs/tags/discret^{commit}" # timeout=10 > git rev-parse "refs/tags/plot^{commit}" # timeout=10 > git rev-parse "refs/tags/md^{commit}" # timeout=10 > git rev-parse "refs/tags/atm^{commit}" # timeout=10 > git rev-parse "refs/tags/make^{commit}" # timeout=10 > git rev-parse "refs/tags/eng^{commit}" # timeout=10 Checking out Revision 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 (origin/pr/146/merge, origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 # timeout=3 Commit message: "Merge 6ef200c93b75c6359f18295b5a541fc98586263d into 62026ae2ee1965aa7005a73cc1f60d704fd1c8b0" Using 'Changelog to branch' strategy. Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [description-setter] Description set: <a title="allow for different spar in tailboom bending and flex models" href="https://github.com/convexengineering/gplibrary/pull/146">PR 146</a>: allow for different spar in tailboom bending and flex models [Execution node] check if [windows7x64] is in [[macys, macys_Sierra, 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\jenkins4716541949095614471.bat D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek>echo C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Program Files (x86)\NVIDIA Corporation\PhysX\Common;D:\Compilers\Intel\Compiler\11.1\048\lib\Intel64;D:\Compilers\Intel\Compiler\11.1\048\lib\ia32;D:\Compilers\Intel\Compiler\11.1\048\mkl\em64t\bin;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;D:\Git\cmd;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:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Program Files (x86)\NVIDIA Corporation\PhysX\Common;D:\Compilers\Intel\Compiler\11.1\048\lib\Intel64;D:\Compilers\Intel\Compiler\11.1\048\lib\ia32;D:\Compilers\Intel\Compiler\11.1\048\mkl\em64t\bin;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;D:\Git\cmd;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\ 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-4.4.2-cp27-cp27m-win_amd64.whl Installing collected packages: coverage Successfully installed coverage-4.4.2 (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: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.02 ************************************ 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'... (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 req_set.py, line 480 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_set.py, line 496 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_set.py, line 496 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_set.py, line 496 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_set.py, line 767 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 985 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 369 (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 req_set.py, line 480 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_set.py, line 496 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_set.py, line 496 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_set.py, line 496 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_set.py, line 767 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 985 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 369 (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 0.657 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.406 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.438 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 2.191s OK Generating XML reports... Cloning into 'gassolar'... 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Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: numpy>=1.7.0 in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-b1ew7y-build Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) 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) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gassolar==0.0.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) 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) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) Installing collected packages: gassolar Running setup.py install for gassolar: started Running setup.py install for gassolar: finished with status 'done' Successfully installed gassolar-0.0.0.0 Running tests... ---------------------------------------------------------------------- EED:\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) EE ====================================================================== ERROR [13.290s]: test_gassolar_gas_gas_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> 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 "gas.py", line 209, in test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 166, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 51, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [6.792s]: test_gassolar_gas_gas_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> 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 "gas.py", line 209, in test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 166, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 51, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [4.406s]: test_gassolar_solar_solar_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", lineadding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 593 variables. Solving took 9.97 seconds. Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2090 but bound is 0.2955 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 Using solver 'mosek' Solving for 593 variables. Solving took 4.88 seconds. Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2090 but bound is 0.2955 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 Using solver 'mosek' Solving for 1206 variables. Solving took 0.956 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 97517.0236 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 97518.5695 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 3 is a constraining latitude 4 is a constraining latitude 5 is a constraining latitude 6 is a constraining latitude 7 is a constraining latitude 8 is a constraining latitude 9 is a constraining latitude 10 is a constraining latitude 11 is a constraining latitude Using solver 'mosek_cli' Solving for 1206 variables. Solving took 0.466 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 97516.8049 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 97518.7552 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 3 is a constraining latitude 4 is a constraining latitude 5 is a constraining latitude 6 is a constraining latitude 7 is a constraining latitude 8 is a constraining latitude 9 is a constraining latitude 10 is a constraining latitude 11 is a constraining latitude 50, in <lambda> 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 "solar.py", line 359, in test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 309, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 49, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [4.223s]: test_gassolar_solar_solar_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> 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 "solar.py", line 359, in test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 309, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 49, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ---------------------------------------------------------------------- Ran 4 tests in 28.711s FAILED (errors=4) Generating XML reports... Cloning into 'jho'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: numpy>=1.7.0 in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-sma2hz-build 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) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) Running tests... ---------------------------------------------------------------------- EEEE ====================================================================== ERROR [1.299s]: test_model_jho_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> 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 "jho.py", line 355, in test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ====================================================================== ERROR [0.201s]: test_model_jho_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> 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 "jho.py", line 355, in test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ====================================================================== ERROR [0.209s]: test_model_print_perf_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 50adding test for 'model/jho.py' adding test for 'model/print_perf.py' , in <lambda> 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 "print_perf.py", line 192, in test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ====================================================================== ERROR [0.201s]: test_model_print_perf_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> 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 "print_perf.py", line 192, in test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ---------------------------------------------------------------------- Ran 4 tests in 1.910s FAILED (errors=4) 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) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) Installing collected packages: turbofan Running setup.py install for turbofan: started Running setup.py install for turbofan: finished with status 'done' 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 12.235s OK Generating XML reports... Cloning into 'SPaircraft'... 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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-5y3oc9-build 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) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) 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 2519608.37591 force_pound * meter but the right hand side evaluated to 2468463.79722 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 32774.4714871 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116795 meter but the right hand side evaluated to 1.9639613538 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 48608.9407301 newton but the right hand side evaluated to 48529.7580867 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 49704.36918 newton but the right hand side evaluated to 49411.0850856 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 18949.0888153 newton but the right hand side evaluated to 18923.0904681 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 16591.9866263 newton but the right hand side evaluated to 16565.7866559 newton (Allowable error: 0.1%, Actual error: 0.16%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1002807.08031 joule / kilogram but the right hand side evaluated to 1.15238742762 megajoule / kilogram (Allowable error: 0.1%, Actual error: 7.1%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 895037.084476 joule / kilogram but the right hand side evaluated to 0.897466245783 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 1072947.0546 joule / kilogram but the right hand side evaluated to 1.19569599237 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 596870.47307 joule / kilogram but the right hand side evaluated to 0.615557037678 megajoule / kilogram (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 786921.741004 joule / kilogram but the right hand side evaluated to 0.790360505989 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 18.3465535368 meter but the right hand side evaluated to 16.3967760129 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 11.085406724 but the right hand side evaluated to 4.68078583053 (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 9.79174299058 but the right hand side evaluated to 4.68078582586 (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 8.22912407368 but the right hand side evaluated to 4.68078583189 (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 18.4249258096 meter but the right hand side evaluated to 18.1659843987 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 18.4249258096 meter but the right hand side evaluated to 18.2854594729 meter (Allowable error: 0.1%, Actual error: 0.76%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.49878846872 but the right hand side evaluated to 4.615982691 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.58150133955 but the right hand side evaluated to 4.6463413472 (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 7.2750336767 but the right hand side evaluated to 4.615982691 (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 7.45366822477 but the right hand side evaluated to 4.6463413472 (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 2504976.88842 force_pound * meter but the right hand side evaluated to 2454470.92541 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 32774.485219 force_pound but the right hand side evaluated to 32399.9999989 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116795 meter but the right hand side evaluated to 1.96383086086 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 982256.80093 joule / kilogram but the right hand side evaluated to 1.20547031296 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 1151137.28147 joule / kilogram but the right hand side evaluated to 1.88379385864 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 18.4111621467 meter but the right hand side evaluated to 16.4524814053 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 11.0893101627 but the right hand side evaluated to 4.73132105408 (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 9.74913418967 but the right hand side evaluated to 4.731321047 (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 8.19783403674 but the right hand side evaluated to 4.73132105648 (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 18.474996767 meter but the right hand side evaluated to 18.2223420405 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 18.474996767 meter but the right hand side evaluated to 18.3384468386 meter (Allowable error: 0.1%, Actual error: 0.74%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.55043974489 but the right hand side evaluated to 4.6669806972 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.63158658386 but the right hand side evaluated to 4.69671665816 (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 7.43022265888 but the right hand side evaluated to 4.6669806972 (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 7.49547557416 but the right hand side evaluated to 4.69671665816 (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 2481460.40781 force_pound * meter but the right hand side evaluated to 2426090.19136 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 32774.43044 force_pound but the right hand side evaluated to 32399.9999982 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116755 meter but the right hand side evaluated to 1.83120202173 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 1203380.54281 joule / kilogram but the right hand side evaluated to 1.66381255281 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 18.4693762569 meter but the right hand side evaluated to 16.6431998955 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 11.047306847 but the right hand side evaluated to 4.80180669565 (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 9.67070700752 but the right hand side evaluated to 4.80180668313 (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 8.22137367179 but the right hand side evaluated to 4.80180669933 (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 18.6280046641 meter but the right hand side evaluated to 18.3449808998 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 18.6280046641 meter but the right hand side evaluated to 18.4743841068 meter (Allowable error: 0.1%, Actual error: 0.82%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.59898882577 but the right hand side evaluated to 4.72921901105 (Allowable error: 0.1%, Actual error: 2.8%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.68921553908 but the right hand side evaluated to 4.76257833205 (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 7.45561684045 but the right hand side evaluated to 4.72921901105 (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 7.54887282141 but the right hand side evaluated to 4.76257833205 (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 2455568.40546 force_pound * meter but the right hand side evaluated to 2407712.24073 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 32774.4822466 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116795 meter but the right hand side evaluated to 1.9955208724 meter (Allowable error: 0.1%, Actual error: 9.9%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1227633.97243 joule / kilogram but the right hand side evaluated to 1.72359784568 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 677538.864228 joule / kilogram but the right hand side evaluated to 0.679181880136 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 18.4156362926 meter but the right hand side evaluated to 16.4239739998 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 10.9749700775 but the right hand side evaluated to 4.76255511343 (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 9.75289658746 but the right hand side evaluated to 4.76255510547 (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 8.15871872978 but the right hand side evaluated to 4.76255511565 (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 18.4488736837 meter but the right hand side evaluated to 18.2046640158 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 18.4488736837 meter but the right hand side evaluated to 18.3176200687 meter (Allowable error: 0.1%, Actual error: 0.71%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.58582650291 but the right hand side evaluated to 4.69978382973 (Allowable error: 0.1%, Actual error: 2.4%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.66559245745 but the right hand side evaluated to 4.72894498484 (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 7.50481939875 but the right hand side evaluated to 4.69978382973 (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 7.52765944252 but the right hand side evaluated to 4.72894498484 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2436786.23081 force_pound * meter but the right hand side evaluated to 2390898.60074 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 32774.4722123 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116789 meter but the right hand side evaluated to 2.03201041398 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 1233975.19203 joule / kilogram but the right hand side evaluated to 1.62325921629 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 18.4095781323 meter but the right hand side evaluated to 16.3813525648 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 10.9310496874 but the right hand side evaluated to 4.78771843419 (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 9.87336242472 but the right hand side evaluated to 4.78771842476 (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 8.15464741202 but the right hand side evaluated to 4.78771843661 (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 18.4102725645 meter but the right hand side evaluated to 18.1746828163 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 18.4102725645 meter but the right hand side evaluated to 18.2839332026 meter (Allowable error: 0.1%, Actual error: 0.69%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.6157440867 but the right hand side evaluated to 4.72672254765 (Allowable error: 0.1%, Actual error: 2.3%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.69362657741 but the right hand side evaluated to 4.75513549272 (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 7.53648506615 but the right hand side evaluated to 4.72672254765 (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 7.55140143821 but the right hand side evaluated to 4.75513549272 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2418323.93148 force_pound * meter but the right hand side evaluated to 2374882.84034 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 32774.4632343 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116784 meter but the right hand side evaluated to 2.08235931418 meter (Allowable error: 0.1%, Actual error: 6%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1244506.89431 joule / kilogram but the right hand side evaluated to 1.55927086196 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 664750.338367 joule / kilogram but the right hand side evaluated to 0.667401744201 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 18.4000459585 meter but the right hand side evaluated to 16.3223727331 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 10.9040369149 but the right hand side evaluated to 4.78950113736 (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 10.0259774583 but the right hand side evaluated to 4.78950112623 (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 8.14555422832 but the right hand side evaluated to 4.78950114023 (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 18.3617949589 meter but the right hand side evaluated to 18.1374264551 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 18.3617949589 meter but the right hand side evaluated to 18.2416861656 meter (Allowable error: 0.1%, Actual error: 0.65%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.6250769767 but the right hand side evaluated to 4.73131602158 (Allowable error: 0.1%, Actual error: 2.2%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.69987187268 but the right hand side evaluated to 4.75851313469 (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 7.56534485023 but the right hand side evaluated to 4.73131602158 (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 7.58381668871 but the right hand side evaluated to 4.75851313469 (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 2405736.61336 force_pound * meter but the right hand side evaluated to 2358168.59898 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 32774.3955689 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 2.21510116786 meter but the right hand side evaluated to 1.97490900323 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 1245747.36088 joule / kilogram but the right hand side evaluated to 1.35773002771 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 18.444135006 meter but the right hand side evaluated to 16.4749800535 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 10.9331076338 but the right hand side evaluated to 4.83171712821 (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 10.1921366346 but the right hand side evaluated to 4.83171708474 (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 8.19565622996 but the right hand side evaluated to 4.83171713685 (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 18.486132428 meter but the right hand side evaluated to 18.2368520559 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 18.486132428 meter but the right hand side evaluated to 18.3518702173 meter (Allowable error: 0.1%, Actual error: 0.73%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.64971704854 but the right hand side evaluated to 4.76697771914 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.73177183312 but the right hand side evaluated to 4.79704261253 (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 7.54212864156 but the right hand side evaluated to 4.76697771914 (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 7.59702562604 but the right hand side evaluated to 4.79704261253 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2391781.71952 force_pound * meter but the right hand side evaluated to 2346059.89001 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 32774.3612666 force_pound but the right hand side evaluated to 32399.9999975 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116769 meter but the right hand side evaluated to 2.0120812051 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 1263254.80888 joule / kilogram but the right hand side evaluated to 1.32933855251 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 643003.297444 joule / kilogram but the right hand side evaluated to 0.64458790208 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 18.4391904217 meter but the right hand side evaluated to 16.4333043948 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 10.9270574056 but the right hand side evaluated to 4.8270964957 (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 10.3328456541 but the right hand side evaluated to 4.82709644309 (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 8.18819618897 but the right hand side evaluated to 4.82709650845 (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 18.4531726441 meter but the right hand side evaluated to 18.212381383 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 18.4531726441 meter but the right hand side evaluated to 18.3237405977 meter (Allowable error: 0.1%, Actual error: 0.7%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.6509896608 but the right hand side evaluated to 4.76456140428 (Allowable error: 0.1%, Actual error: 2.4%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.73069792995 but the right hand side evaluated to 4.79369421262 (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 7.55428869636 but the right hand side evaluated to 4.76456140428 (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 7.61783476215 but the right hand side evaluated to 4.79369421262 (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 2376284.6497 force_pound * meter but the right hand side evaluated to 2334600.04722 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 32774.40509 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.2151011678 meter but the right hand side evaluated to 2.09817260583 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 1283641.70722 joule / kilogram but the right hand side evaluated to 1.28936314781 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 18.4146018271 meter but the right hand side evaluated to 16.3183416173 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 10.9374630655 but the right hand side evaluated to 4.82437911843 (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 10.5713435004 but the right hand side evaluated to 4.82437909707 (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 8.19385072424 but the right hand side evaluated to 4.82437912365 (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 18.3565589132 meter but the right hand side evaluated to 18.1377551067 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 18.3565589132 meter but the right hand side evaluated to 18.2401826279 meter (Allowable error: 0.1%, Actual error: 0.63%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.66215786648 but the right hand side evaluated to 4.76702022041 (Allowable error: 0.1%, Actual error: 2.2%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.73627475508 but the right hand side evaluated to 4.79394053454 (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 7.62007183522 but the right hand side evaluated to 4.76702022041 (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 7.68939715986 but the right hand side evaluated to 4.79394053454 (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 432 seconds. Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 436.070s OK Generating XML reports... Cloning into 'solar'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: numpy>=1.7.0 in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-jy64h1-build 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) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) Collecting git+https://github.com/convexengineering/gassolar.git Cloning https://github.com/convexengineering/gassolar.git to c:\users\jenkins\appdata\local\temp\pip-ysfraw-build 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) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gassolar==0.0.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) 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) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) 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) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from solar==0.0.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) 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) Requirement already satisfied: gpkitmodels in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek (from solar==0.0.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->solar==0.0.0.0) Installing collected packages: solar Running setup.py install for solar: started Running setup.py install for solar: finished with status 'done' Successfully installed solar-0.0.0.0 adding test for 'solar/solar.py' adding test for 'solar/sens_chart.py' adding test for 'solar/season.py' Using solver 'mosek' Solving for 5670 variables. Solving took 1.41 seconds. Warning: Variable Re_Mission/FlightSegment.38/AircraftPerf.38/WingAero.38 could cause inaccurate result because it is below lower bound. Solution is 120042.1846 but bound is 125000.0000 Warning: Variable Re_Mission/FlightSegment.39/AircraftPerf.39/WingAero.39 could cause inaccurate result because it is below lower bound. Solution is 121471.1981 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 1.71 seconds. Warning: Variable Re_Mission.1/FlightSegment.78/AircraftPerf.78/WingAero.78 could cause inaccurate result because it is below lower bound. Solution is 122823.1089 but bound is 125000.0000 Warning: Variable Re_Mission.1/FlightSegment.79/AircraftPerf.79/WingAero.79 could cause inaccurate result because it is below lower bound. Solution is 123244.6837 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 9.03 seconds. Using solver 'mosek' Solving for 2910 variables. Solving took 0.626 seconds. Using solver 'mosek' Solving for 5670 variables. Solving took 2.77 seconds. Warning: Variable Re_Mission/FlightSegment.38/AircraftPerf.38/WingAero.38 could cause inaccurate result because it is below lower bound. Solution is 120042.1846 but bound is 125000.0000 Warning: Variable Re_Mission/FlightSegment.39/AircraftPerf.39/WingAero.39 could cause inaccurate result because it is below lower bound. Solution is 121471.1982 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 6.13 seconds. Warning: Variable Re_Mission.1/FlightSegment.78/AircraftPerf.78/WingAero.78 could cause inaccurate result because it is below lower bound. Solution is 122823.1089 but bound is 125000.0000 Warning: Variable Re_Mission.1/FlightSegment.79/AircraftPerf.79/WingAero.79 could cause inaccurate result because it is below lower bound. Solution is 123244.6837 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 10.6 seconds. Using solver 'mosek' Solving for 2910 variables. Solving took 1.66 seconds. Using solver 'mosek' Solving for 288 variables. Solving took 0.095 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 122179.8905 but bound is 125000.0000 Using solver 'mosek' Solving for 288 variables. Solving took 0.076 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 122179.8905 but bound is 125000.0000 Using solver 'mosek' Solving for 2910 variables. Solving took 18.4 seconds. Using solver 'mosek_cli' Solving for 2910 variables. Solving took 5.62 seconds. 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) ....EE ====================================================================== ERROR [25.157s]: test_solar_solar_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> 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 "solar.py", line 486, in test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 467, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 85, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [17.972s]: test_solar_solar_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> 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 "solar.py", line 486, in test File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 467, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 85, in setup File "d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ---------------------------------------------------------------------- Ran 6 tests in 205.940s FAILED (errors=2) Generating XML reports... Cloning into 'gplibrary'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: numpy>=1.7.0 in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-uiieda-build 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) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) Processing d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gplibrary Requirement already satisfied (use --upgrade to upgrade): gpkitmodels==0.0.0.0 from file:///D:/jenkins/workspace/gplibrary_PR_Models/buildnode/windows7x64/optimizer/mosek/gplibrary in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py' adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py' Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3642 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9486 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2262061.5401 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2262061.2755 but bound is 1000000.0000 Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2262068.0066 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2262068.0066 but bound is 1000000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 2147759.9054 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 2232694.7572 but bound is 700000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 2232695.1475 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 2232695.1475 but bound is 700000.0000 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 10.993s 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(<type 'str'>, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'git+https://github.com/hoburg/turbofan.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 (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] - 7 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