Started by upstream project "gplibrary_PR_Models" build number 71 originally caused by: GitHub pull request #158 of commit f28591b4b0076aa61ad8b3d63c4daa9322fc3408, no merge conflicts. Building remotely on windows10x64 in workspace C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > C:\Program Files\Git\cmd\git init C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > C:\Program Files\Git\cmd\git --version # timeout=10 > C:\Program Files\Git\cmd\git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* > C:\Program Files\Git\cmd\git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 > C:\Program Files\Git\cmd\git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10 > C:\Program Files\Git\cmd\git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > C:\Program Files\Git\cmd\git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master Merging Revision 34a4748c5d33aa3e90a704092bc0232a5a842082 (refs/remotes/origin/pr/158/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='default', fastForwardMode='--ff'} > C:\Program Files\Git\cmd\git rev-parse "origin/master^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git config core.sparsecheckout # timeout=10 > C:\Program Files\Git\cmd\git checkout -f origin/master # timeout=3 > C:\Program Files\Git\cmd\git merge --ff 34a4748c5d33aa3e90a704092bc0232a5a842082 # timeout=10 > C:\Program Files\Git\cmd\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 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Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [description-setter] Description set: <a title="fix auto-diff for cosminus1 in gust loading" href="https://github.com/convexengineering/gplibrary/pull/158">PR 158</a>: fix auto-diff for cosminus1 in gust loading [Execution node] check if [windows10x64] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [windows10x64] 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\jenkins8127264320706667468.bat C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>echo C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Git\cmd;C:\Program Files\mingw-w64\x86_64-5.3.0-posix-seh-rt_v4-rev0\mingw64\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Git\cmd;C:\Program Files\mingw-w64\x86_64-5.3.0-posix-seh-rt_v4-rev0\mingw64\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>REM turn on the anaconda console C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>call activate.bat || exit /b 666 (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Create a virtualenv to install everything into (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>SET VENV=C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>virtualenv --system-site-packages C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit New python executable in C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts\python.exe Installing setuptools, pip, wheel...done. (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>call C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts\activate.bat (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Install coverage into the virtualenv to the coverage command blow uses the virtualenv python (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>pip install coverage Collecting coverage Using cached coverage-4.5.1-cp27-cp27m-win_amd64.whl Installing collected packages: coverage The scripts coverage-2.7.exe, coverage.exe and coverage2.exe are installed in 'c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts' which is not on PATH. Consider adding this directory to PATH or, if you prefer to suppress this warning, use --no-warn-script-location. Successfully installed coverage-4.5.1 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>if mosek == mosek msktestlic || exit /b 666 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. Mosek license manager: License path: C:\Users\jenkins\mosek\mosek.lic Mosek license manager: Checkout license feature 'PTS' from flexlm. Mosek license manager: Checkout time 0.03. r: 0 status: 0 Interior-point optimizer started. Presolve started. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 1 time : 0.00 Lin. dep. - tries : 0 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.27 ************************************ A license was checked out correctly. ************************************ (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>SET GPKITBUILD=C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\build_gpkit (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>gcc --version || exit /b 666 gcc (x86_64-posix-seh-rev0, Built by MinGW-W64 project) 5.3.0 Copyright (C) 2015 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) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>if mosek == cvxopt set GPKITSOLVERS=cvxopt (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>if mosek == mosek set GPKITSOLVERS=mosek, mosek_cli (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>dir C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\build_gpkit Volume in drive C has no label. Volume Serial Number is C4C9-8F11 Directory of C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek File Not Found (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "import scipy; print scipy.__version__" 0.18.1 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "import numpy; print numpy.__version__" 1.11.3 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "import pint; print pint.__version__" 0.7.2 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Install gpkit to run the documentation examples (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>git clone --depth 1 https://github.com/convexengineering/gpkit.git Cloning into 'gpkit'... (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>pip install -e C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\gpkit | exit /b 666 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 329 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 214 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 download.py, line 605 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 214 gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file __init__.py, line 30 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file __init__.py, line 38 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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_uninstall.py, line 281 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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_uninstall.py, line 202 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_install.py, line 893 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file install.py, line 354 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>pip install -e C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek | exit /b 666 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 329 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file prepare.py, line 360 gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file __init__.py, line 30 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_install.py, line 893 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\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 "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file install.py, line 354 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Show the settings file (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>type C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\env\settings installed_solvers : mosek, mosek_cli mosek_bin_dir : C:\Program Files\Mosek\8\tools\platform\win64x86\bin (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)" Obtaining file:///C:/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/windows10x64/optimizer/mosek Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Cloning into 'shopping'... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 1.44 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.279 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.378 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 3.286s OK Generating XML reports... Cloning into 'gassolar'... 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Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.19.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.0) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2016.10) Requirement already satisfied: numpy>=1.7.0 in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.10.0) gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-mkja1e Requirement already satisfied: numpy in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (0.18.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.7.2) Requirement already satisfied: ad in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires scipy, which is not installed. Installing collected packages: gpfit Running setup.py install for gpfit: started Running setup.py install for gpfit: finished with status 'done' Successfully installed gpfit-0.1 Processing c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gassolar Requirement already satisfied: numpy in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.18.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.19.2) Requirement already satisfied: gpfit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.7.2) Requirement already satisfied: ad in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.0) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2016.10) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.10.0) Building wheels for collected packages: gassolar Running setup.py bdist_wheel for gassolar: started Running setup.py bdist_wheel for gassolar: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-tpynfi\wheels\9d\25\b2\b7ad5efb66502051059ff6ad9e8c681be9a7b78e83fc845a7a Successfully built gassolar gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires scipy, which is not installed. Installing collected packages: gassolar Successfully installed gassolar-0.0.0.0 adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 609 variables. Solving took 7.46 seconds. Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Beginning signomial solve. Solving took 4 GP solves and 16.4 seconds. Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 609 variables. Solving took 10.2 seconds. Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Beginning signomial solve. Solving took 4 GP solves and 23.7 seconds. Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 1437 variables. Solving took 30.6 seconds. Allowing negative dual variable(s) as small as -1.2047116003085308e-11. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1904 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.1338 but bound is 150000.0000 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.744078639846066e-13. Allowing negative dual variable(s) as small as -1.2083110815243205e-11. Allowing negative dual variable(s) as small as -3.746688633035315e-13. Allowing negative dual variable(s) as small as -4.469011768035925e-12. Solving took 4 GP solves and 72.2 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0972 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.9073 but bound is 150000.0000 Using solver 'mosek_cli' Solving for 1437 variables. Solving took 54.8 seconds. Allowing negative dual variable(s) as small as -1.108507e-11. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.0147 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.3302 but bound is 150000.0000 Beginning signomial solve. Allowing negative dual variable(s) as small as -8.02651e-13. Allowing negative dual variable(s) as small as -1.208277e-11. Allowing negative dual variable(s) as small as -3.391054e-13. Allowing negative dual variable(s) as small as -4.523065e-12. Solving took 4 GP solves and 106 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134552.5355 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.8810 but bound is 150000.0000 Running tests... ---------------------------------------------------------------------- ..C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 4 tests in 351.356s OK Generating XML reports... Cloning into 'jho'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.19.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.0) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2016.10) Requirement already satisfied: numpy>=1.7.0 in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.10.0) gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires scipy, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-3a3yej Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (0.18.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.7.2) Requirement already satisfied: ad in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires scipy, which is not installed. adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -2.7092737775458176e-13. Allowing negative dual variable(s) as small as -5.725060182870667e-13. Allowing negative dual variable(s) as small as -1.0140195974561728e-13. Allowing negative dual variable(s) as small as -7.875297636239509e-14. Solving took 4 GP solves and 232 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.0850261661365934e-14. Allowing negative dual variable(s) as small as -3.7704648431224896e-14. Allowing negative dual variable(s) as small as -1.1461144533431167e-13. Allowing negative dual variable(s) as small as -8.74131496353403e-14. Solving took 4 GP solves and 525 seconds. Allowing negative dual variable(s) as small as -1.189395804068738e-12. Allowing negative dual variable(s) as small as -1.459336124165489e-12. Allowing negative dual variable(s) as small as -1.4619867816367815e-12. Allowing negative dual variable(s) as small as -2.5631450087382213e-13. Allowing negative dual variable(s) as small as -1.3358344378572307e-12. Allowing negative dual variable(s) as small as -1.2354805763517551e-12. Allowing negative dual variable(s) as small as -1.2351390526674222e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -3.687328220536301e-14. Allowing negative dual variable(s) as small as -2.0206883041828938e-13. Allowing negative dual variable(s) as small as -2.0298454757317064e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -8.729262256441841e-15. Allowing negative dual variable(s) as small as -4.073174943198486e-12. Allowing negative dual variable(s) as small as -2.2201976550571146e-11. Allowing negative dual variable(s) as small as -2.2195827426746187e-11. Solving took 4 GP solves and 69.6 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 143 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -1.1897913210212607e-12. Allowing negative dual variable(s) as small as -1.4605382875343409e-12. Allowing negative dual variable(s) as small as -1.4617768800961883e-12. Allowing negative dual variable(s) as small as -2.601989804174032e-13. Allowing negative dual variable(s) as small as -1.3358278242239785e-12. Allowing negative dual variable(s) as small as -1.2349080091844655e-12. Allowing negative dual variable(s) as small as -1.2351663745621688e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -3.838726211902177e-14. Allowing negative dual variable(s) as small as -2.0351472243551605e-13. Allowing negative dual variable(s) as small as -2.0347200486992012e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -7.984269674277372e-15. Allowing negative dual variable(s) as small as -4.073246431826322e-12. Allowing negative dual variable(s) as small as -2.2202138797958717e-11. Allowing negative dual variable(s) as small as -2.219593309479457e-11. Solving took 4 GP solves and 31.8 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 31.8 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 1929.315s OK Generating XML reports... Cloning into 'turbofan'... Processing c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\turbofan Requirement already satisfied: numpy in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from turbofan==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.18.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.7.2) Building wheels for collected packages: turbofan Running setup.py bdist_wheel for turbofan: started Running setup.py bdist_wheel for turbofan: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-qgyoll\wheels\50\36\cf\e4b389dca40a9f3faac4f973a941139376b6bd6f2dd9a6d923 Successfully built turbofan gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires scipy, which is not installed. Installing collected packages: turbofan Successfully installed turbofan-0.0.0.0 adding test for 'turbofan/engine_validation.py' Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528316 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 26232.8485057 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 11.755s 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-req-build-gw9sue Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from turbofan==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.18.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.7.2) gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires scipy, which is not installed. adding test for 'SP_aircraft.py' Solving over 9 passes. Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2519607.08447 force_pound * meter but the right hand side evaluated to 2468463.10962 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 32774.4497416 force_pound but the right hand side evaluated to 32399.9999973 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116762 meter but the right hand side evaluated to 1.96396117373 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 48608.9103053 newton but the right hand side evaluated to 48529.7357509 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 49704.4010335 newton but the right hand side evaluated to 49411.1332645 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 18949.0726616 newton but the right hand side evaluated to 18923.0748718 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 16591.9804833 newton but the right hand side evaluated to 16565.7780127 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 1002809.7972 joule / kilogram but the right hand side evaluated to 1.15240192043 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 895039.839387 joule / kilogram but the right hand side evaluated to 0.897468889684 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 1072947.23223 joule / kilogram but the right hand side evaluated to 1.19570137553 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 596870.414801 joule / kilogram but the right hand side evaluated to 0.615556973251 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 786922.98132 joule / kilogram but the right hand side evaluated to 0.790361831414 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 18.3465553868 meter but the right hand side evaluated to 16.3967779646 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 11.085406998040199 but the right hand side evaluated to 4.680786937106711 (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 9.79174233210136 but the right hand side evaluated to 4.680786927822266 (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 8.22912609404957 but the right hand side evaluated to 4.68078693975965 (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 18.4249276717 meter but the right hand side evaluated to 18.1659866082 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 18.4249276717 meter but the right hand side evaluated to 18.2854635623 meter (Allowable error: 0.1%, Actual error: 0.76%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3101212804964417 but the right hand side evaluated to 0.1929270057736646 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2413427959650427 but the right hand side evaluated to 0.17650198752891746 (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 7.275035743438705 but the right hand side evaluated to 4.615983888010577 (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 7.453667984914703 but the right hand side evaluated to 4.646343026059043 (Allowable error: 0.1%, Actual error: 38%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, 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 2504974.1234 force_pound * meter but the right hand side evaluated to 2454470.88237 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 32774.5133762 force_pound but the right hand side evaluated to 32399.999999 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116804 meter but the right hand side evaluated to 1.96383008606 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 982256.654997 joule / kilogram but the right hand side evaluated to 1.20546998252 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 1151137.26644 joule / kilogram but the right hand side evaluated to 1.88379339279 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 18.4111621685 meter but the right hand side evaluated to 16.4524821931 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 11.089310578520188 but the right hand side evaluated to 4.7313212165373555 (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 9.74913407373437 but the right hand side evaluated to 4.731321211955737 (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 8.197834206440744 but the right hand side evaluated to 4.731321218187922 (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 18.4749973435 meter but the right hand side evaluated to 18.2223434539 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 18.4749973435 meter but the right hand side evaluated to 18.3384477013 meter (Allowable error: 0.1%, Actual error: 0.74%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3092785733274468 but the right hand side evaluated to 0.1927375004562347 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.24173555828115756 but the right hand side evaluated to 0.17660269425781336 (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 7.430222485354896 but the right hand side evaluated to 4.666981066730552 (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 7.495470746755604 but the right hand side evaluated to 4.696716886691007 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission final status of solver 'mosek' was 'NEAR_DUAL_FEAS', not 'optimal'. Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2481458.39778 force_pound * meter but the right hand side evaluated to 2426090.82694 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 32774.4446206 force_pound but the right hand side evaluated to 32399.9999971 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 2.21510116747 meter but the right hand side evaluated to 1.83120052262 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 1203381.5755 joule / kilogram but the right hand side evaluated to 1.66382540875 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 18.4693776207 meter but the right hand side evaluated to 16.6432024871 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 11.047308867550594 but the right hand side evaluated to 4.8018116370661605 (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 9.670712400515033 but the right hand side evaluated to 4.801811623902718 (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 8.221375475085104 but the right hand side evaluated to 4.801811641085479 (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 18.6280062311 meter but the right hand side evaluated to 18.3449868408 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 18.6280062311 meter but the right hand side evaluated to 18.4743897441 meter (Allowable error: 0.1%, Actual error: 0.82%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3268340239843077 but the right hand side evaluated to 0.19660335670486917 (Allowable error: 0.1%, Actual error: 2.8%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.25275664811755494 but the right hand side evaluated to 0.17939074718364978 (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 7.455617208632008 but the right hand side evaluated to 4.72922499175572 (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 7.54887190932776 but the right hand side evaluated to 4.76258426584892 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2455569.18158 force_pound * meter but the right hand side evaluated to 2407712.00184 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 32774.4557996 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 2.21510116801 meter but the right hand side evaluated to 1.99551684227 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 1227633.61418 joule / kilogram but the right hand side evaluated to 1.7235961365 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 677538.059466 joule / kilogram but the right hand side evaluated to 0.679181139186 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 18.415637482 meter but the right hand side evaluated to 16.4239791315 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 10.974970992149107 but the right hand side evaluated to 4.762555039311344 (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 9.752898681556395 but the right hand side evaluated to 4.762555033281843 (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 8.158719623914722 but the right hand side evaluated to 4.7625550411956175 (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 18.4488779665 meter but the right hand side evaluated to 18.2046678564 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 18.4488779665 meter but the right hand side evaluated to 18.3176247466 meter (Allowable error: 0.1%, Actual error: 0.71%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.305947251130247 but the right hand side evaluated to 0.1919895398868301 (Allowable error: 0.1%, Actual error: 2.4%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23933741641172457 but the right hand side evaluated to 0.17598553136581668 (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 7.504819518489688 but the right hand side evaluated to 4.699783644603554 (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 7.527660693152377 but the right hand side evaluated to 4.728945008566443 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2436784.80447 force_pound * meter but the right hand side evaluated to 2390898.24483 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 32774.5255715 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 2.03200543956 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 1233973.61317 joule / kilogram but the right hand side evaluated to 1.62323703523 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 18.4095790685 meter but the right hand side evaluated to 16.3813581289 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 10.931046459027023 but the right hand side evaluated to 4.787720915948654 (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 9.873362830354907 but the right hand side evaluated to 4.787720907059444 (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 8.154648884056947 but the right hand side evaluated to 4.787720918775876 (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 18.4102766825 meter but the right hand side evaluated to 18.1746862045 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 18.4102766825 meter but the right hand side evaluated to 18.2839343899 meter (Allowable error: 0.1%, Actual error: 0.69%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3020993402382963 but the right hand side evaluated to 0.19112037059886372 (Allowable error: 0.1%, Actual error: 2.3%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23685457755304107 but the right hand side evaluated to 0.17534413079187777 (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 7.536483065452208 but the right hand side evaluated to 4.726724795562806 (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 7.551400799819455 but the right hand side evaluated to 4.755137176442591 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, 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 2418327.72188 force_pound * meter but the right hand side evaluated to 2374880.065 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 32774.29911 force_pound but the right hand side evaluated to 32399.9999969 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 2.21510116728 meter but the right hand side evaluated to 2.08230466355 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 1244494.26554 joule / kilogram but the right hand side evaluated to 1.55907155353 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 664738.221856 joule / kilogram but the right hand side evaluated to 0.667387023027 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 18.4000580441 meter but the right hand side evaluated to 16.322437016 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 10.904021424450022 but the right hand side evaluated to 4.7895042493865025 (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 10.025896838899317 but the right hand side evaluated to 4.789504223392421 (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 8.145565119146925 but the right hand side evaluated to 4.78950425561934 (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 18.361847194 meter but the right hand side evaluated to 18.1374681242 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 18.361847194 meter but the right hand side evaluated to 18.241739878 meter (Allowable error: 0.1%, Actual error: 0.65%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.29596760632787067 but the right hand side evaluated to 0.18972338047256834 (Allowable error: 0.1%, Actual error: 2.2%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23297421633149273 but the right hand side evaluated to 0.17433422850412567 (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 7.565332803735263 but the right hand side evaluated to 4.731316364309318 (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 7.583799993081915 but the right hand side evaluated to 4.758516558487425 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, 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 2405735.39596 force_pound * meter but the right hand side evaluated to 2358168.44786 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 32774.4178073 force_pound but the right hand side evaluated to 32399.9999989 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116801 meter but the right hand side evaluated to 1.97491276676 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 1245747.62052 joule / kilogram but the right hand side evaluated to 1.35773385204 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 18.4441332017 meter but the right hand side evaluated to 16.4749746518 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 10.933106407164079 but the right hand side evaluated to 4.8317171537616845 (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 10.192140171169218 but the right hand side evaluated to 4.831717142378198 (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 8.195655194552945 but the right hand side evaluated to 4.831717156187895 (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 18.4861277623 meter but the right hand side evaluated to 18.2368480931 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 18.4861277623 meter but the right hand side evaluated to 18.3518650601 meter (Allowable error: 0.1%, Actual error: 0.73%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3102021385117224 but the right hand side evaluated to 0.1929418066652377 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.24192119525271671 but the right hand side evaluated to 0.1766497312384858 (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 7.542128272732468 but the right hand side evaluated to 4.766977905196433 (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 7.597023420772049 but the right hand side evaluated to 4.797042494086645 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, 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 2391780.64051 force_pound * meter but the right hand side evaluated to 2346059.87996 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 32774.5338662 force_pound but the right hand side evaluated to 32399.9999966 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 2.21510116777 meter but the right hand side evaluated to 2.01208013273 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 1263254.04845 joule / kilogram but the right hand side evaluated to 1.32933656209 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 643003.157719 joule / kilogram but the right hand side evaluated to 0.64458771182 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 18.4391902365 meter but the right hand side evaluated to 16.4333050027 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 10.927058748799338 but the right hand side evaluated to 4.827097510408855 (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 10.332848352245765 but the right hand side evaluated to 4.827097490002345 (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 8.188197321016395 but the right hand side evaluated to 4.827097515397117 (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 18.4531728146 meter but the right hand side evaluated to 18.2123814184 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 18.4531728146 meter but the right hand side evaluated to 18.3237288537 meter (Allowable error: 0.1%, Actual error: 0.7%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.30544752434819156 but the right hand side evaluated to 0.19187570350873634 (Allowable error: 0.1%, Actual error: 2.4%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23885841531648921 but the right hand side evaluated to 0.17586129403717576 (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 7.554292086554423 but the right hand side evaluated to 4.764562324012101 (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 7.617832343617409 but the right hand side evaluated to 4.793692056301662 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, 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 2376284.37667 force_pound * meter but the right hand side evaluated to 2334600.33837 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 32774.3365419 force_pound but the right hand side evaluated to 32399.9999962 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 2.09816957635 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 1283642.3668 joule / kilogram but the right hand side evaluated to 1.28936540652 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 18.4146039581 meter but the right hand side evaluated to 16.3183468022 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 10.9374645902631 but the right hand side evaluated to 4.824379286302794 (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 10.57134324767793 but the right hand side evaluated to 4.824379256969726 (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 8.193851582224173 but the right hand side evaluated to 4.824379293569733 (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 18.3565635269 meter but the right hand side evaluated to 18.1377571413 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 18.3565635269 meter but the right hand side evaluated to 18.2401912066 meter (Allowable error: 0.1%, Actual error: 0.63%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.29417322414784763 but the right hand side evaluated to 0.18931066680611683 (Allowable error: 0.1%, Actual error: 2.2%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2316573844748957 but the right hand side evaluated to 0.1739904592623837 (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 7.620073009202368 but the right hand side evaluated to 4.7670197661758245 (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 7.689394939420791 but the right hand side evaluated to 4.7939417946442635 (Allowable error: 0.1%, Actual error: 38%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission Sweeping took 334 seconds. Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 339.172s OK Generating XML reports... Cloning into 'solar'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.19.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.0) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2016.10) Requirement already satisfied: numpy>=1.7.0 in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.10.0) gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires scipy, which is not installed. Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-kwkjsl Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (0.18.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.7.2) Requirement already satisfied: ad in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires scipy, which is not installed. Collecting git+https://github.com/convexengineering/gassolar.git Cloning https://github.com/convexengineering/gassolar.git to c:\users\jenkins\appdata\local\temp\pip-req-build-wqniei Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.18.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.19.2) Requirement already satisfied: gpfit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.7.2) Requirement already satisfied: ad in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.0) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2016.10) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.10.0) gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. gpfit 0.1 requires scipy, which is not installed. Processing c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\solar Requirement already satisfied: numpy in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.18.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.19.2) Requirement already satisfied: gpfit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1) Requirement already satisfied: gpkitmodels in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek (from solar==0.0.0.0) (0.0.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.7.2) Requirement already satisfied: ad in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.6.0) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2016.10) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.10.0) Building wheels for collected packages: solar Running setup.py bdist_wheel for solar: started Running setup.py bdist_wheel for solar: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-znhhgw\wheels\77\2f\d5\7b6dcae48ee017565219d8f7ea2e8fb7a02bf3c5f61fd8733c Successfully built solar gpfit 0.1 requires scipy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. solar 0.0.0.0 requires pandas, which is not installed. solar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. Installing collected packages: solar Successfully installed solar-0.0.0.0 adding test for 'solar/solar.py' adding test for 'solar/sens_chart.py' adding test for 'solar/season.py' Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Using solver 'mosek' Solving for 9147 variables. Solving took 9.87 seconds. Allowing negative dual variable(s) as small as -1.1670194512774796e-11. Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,). Using solver 'mosek' Solving for 9147 variables. Solving took 3.84 seconds. Allowing negative dual variable(s) as small as -9.751111265990294e-11. Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(0,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(3,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(4,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(2,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(1,). Using solver 'mosek' Solving for 9147 variables. Solving took 4.58 seconds. Allowing negative dual variable(s) as small as -4.126411339422189e-09. Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 625489.6104 but bound is 600000.0000 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(3,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(1,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(2,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(4,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(0,). Using solver 'mosek' Solving for 4707 variables. Solving took 3.24 seconds. Allowing negative dual variable(s) as small as -5.216146878601522e-11. Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 642574.9402 but bound is 600000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Using solver 'mosek' Solving for 9147 variables. Solving took 4.31 seconds. Allowing negative dual variable(s) as small as -1.0290406859902235e-12. Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,). Using solver 'mosek' Solving for 9147 variables. Solving took 4.07 seconds. Allowing negative dual variable(s) as small as -9.727995999692859e-11. Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(0,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(3,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(4,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(2,). Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(1,). Using solver 'mosek' Solving for 9147 variables. Solving took 3.92 seconds. Allowing negative dual variable(s) as small as -2.286568669552153e-09. Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 625491.4872 but bound is 600000.0000 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(3,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(1,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(2,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(4,). Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(0,). Using solver 'mosek' Solving for 4707 variables. Solving took 1.53 seconds. Allowing negative dual variable(s) as small as -5.152949915703545e-11. Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 642574.9419 but bound is 600000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Using solver 'mosek' Solving for 489 variables. Solving took 1.5 seconds. Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642575.0575 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Using solver 'mosek' Solving for 489 variables. Solving took 1.21 seconds. Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642575.0575 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Using solver 'mosek' Solving for 4707 variables. Solving took 6.29 seconds. Allowing negative dual variable(s) as small as -5.481199236825347e-11. Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642574.9370 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,). Beginning signomial solve. Allowing negative dual variable(s) as small as -4.354201675105278e-12. Allowing negative dual variable(s) as small as -2.136259116013787e-11. Allowing negative dual variable(s) as small as -1.6234432329734753e-12. Allowing negative dual variable(s) as small as -2.3138188058989834e-11. Solving took 4 GP solves and 58.9 seconds. Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 641279.3638 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,). Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,). Using solver 'mosek_cli' Solving for 4707 variables. Solving took 11.5 seconds. Allowing negative dual variable(s) as small as -2.973864e-12. Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642575.7579 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500 Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,). Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,). Beginning signomial solve. Allowing negative dual variable(s) as small as -4.37547e-12. Allowing negative dual variable(s) as small as -8.382024e-12. Allowing negative dual variable(s) as small as -2.157718e-11. Allowing negative dual variable(s) as small as -2.1138e-11. Solving took 4 GP solves and 49.6 seconds. Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 641279.0650 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500 Running tests... ---------------------------------------------------------------------- C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun) ...... ---------------------------------------------------------------------- Ran 6 tests in 464.638s OK Generating XML reports... Cloning into 'gplibrary'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.19.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.0) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2016.10) Requirement already satisfied: numpy>=1.7.0 in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.10.0) gpfit 0.1 requires scipy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. solar 0.0.0.0 requires pandas, which is not installed. solar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-zyctdj Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (0.18.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.7.2) Requirement already satisfied: ad in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) gpfit 0.1 requires scipy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. solar 0.0.0.0 requires pandas, which is not installed. solar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. Processing c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gplibrary Requirement already satisfied: numpy>=1.12 in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.18.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.7.2) Building wheels for collected packages: gpkitmodels Running setup.py bdist_wheel for gpkitmodels: started Running setup.py bdist_wheel for gpkitmodels: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-r25s6a\wheels\64\59\cd\9f5c1e641342ef4e9c4e9116148e9f1aa9d75e061ed37a17ad Successfully built gpkitmodels gpfit 0.1 requires scipy, which is not installed. gassolar 0.0.0.0 requires pandas, which is not installed. gassolar 0.0.0.0 requires scipy, which is not installed. gpkitmodels 0.0.0.0 requires pint, which is not installed. gpkitmodels 0.0.0.0 requires scipy, which is not installed. solar 0.0.0.0 requires pandas, which is not installed. solar 0.0.0.0 requires scipy, which is not installed. turbofan 0.0.0.0 requires pint, which is not installed. turbofan 0.0.0.0 requires scipy, which is not installed. gpkit 0.7.0.0 requires pint>=0.7, which is not installed. gpkit 0.7.0.0 requires scipy, which is not installed. Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Successfully installed gpkitmodels-0.0.0.0 Running tests... ---------------------------------------------------------------------- ..EEEE ====================================================================== ERROR [0.050s]: test_gpkitmodels_GP_aircraft_tail_tail_tests_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "tail_tests.py", line 117, in test File "tail_tests.py", line 20, in test_htail File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\tail\tail_aero.py", line 44, in setup fd = pd.read_csv(path + os.sep + "tail_dragfit.csv").to_dict( File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 646, in parser_f return _read(filepath_or_buffer, kwds) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 389, in _read parser = TextFileReader(filepath_or_buffer, **kwds) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 730, in __init__ self._make_engine(self.engine) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 923, in _make_engine self._engine = CParserWrapper(self.f, **self.options) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 1390, in __init__ self._reader = _parser.TextReader(src, **kwds) File "pandas\parser.pyx", line 373, in pandas.parser.TextReader.__cinit__ (pandas\parser.c:4184) File "pandas\parser.pyx", line 667, in pandas.parser.TextReader._setup_parser_source (pandas\parser.c:8449) IOError: File C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\tail\tail_dragfit.csv does not exist ====================================================================== ERROR [0.037s]: test_gpkitmodels_GP_aircraft_tail_tail_tests_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "tail_tests.py", line 117, in test File "tail_tests.py", line 20, in test_htail File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\tail\tail_aero.py", line 44, in setup fd = pd.read_csv(path + os.sep + "tail_dragfit.csv").to_dict( File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 646, in parser_f return _read(filepath_or_buffer, kwds) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 389, in _read parser = TextFileReader(filepath_or_buffer, **kwds) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 730, in __init__ self._make_engine(self.engine) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 923, in _make_engine self._engine = CParserWrapper(self.f, **self.options) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 1390, in __init__ self._reader = _parser.TextReader(src, **kwds) File "pandas\parser.pyx", line 373, in pandas.parser.TextReader.__cinit__ (pandas\parser.c:4184) File "pandas\parser.pyx", line 667, in pandas.parser.TextReader._setup_parser_source (pandas\parser.c:8449) IOError: File C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\tail\tail_dragfit.csv does not exist ====================================================================== ERROR [0.093s]: test_gpkitmodels_GP_aircraft_wing_wing_test_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "wing_test.py", line 85, in test File "wing_test.py", line 33, in wing_test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\wing\wing.py", line 123, in setup df = pd.read_csv(fitdata) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 646, in parser_f return _read(filepath_or_buffer, kwds) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 389, in _read parser = TextFileReader(filepath_or_buffer, **kwds) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 730, in __init__ self._make_engine(self.engine) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 923, in _make_engine self._engine = CParserWrapper(self.f, **self.options) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 1390, in __init__ self._reader = _parser.TextReader(src, **kwds) File "pandas\parser.pyx", line 373, in pandas.parser.TextReader.__cinit__ (pandas\parser.c:4184) File "pandas\parser.pyx", line 667, in pandas.parser.TextReader._setup_parser_source (pandas\parser.c:8449) IOError: File C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\wing\jho_fitdata.csv does not exist ====================================================================== ERROR [0.082s]: test_gpkitmodels_GP_aircraft_wing_wing_test_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable Filadding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py' adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py' adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py' Using solver 'mosek' Solving for 11 variables. Solving took 0.885 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.502 seconds. e "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "wing_test.py", line 85, in test File "wing_test.py", line 33, in wing_test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\wing\wing.py", line 123, in setup df = pd.read_csv(fitdata) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 646, in parser_f return _read(filepath_or_buffer, kwds) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 389, in _read parser = TextFileReader(filepath_or_buffer, **kwds) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 730, in __init__ self._make_engine(self.engine) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 923, in _make_engine self._engine = CParserWrapper(self.f, **self.options) File "c:\anaconda2\lib\site-packages\pandas\io\parsers.py", line 1390, in __init__ self._reader = _parser.TextReader(src, **kwds) File "pandas\parser.pyx", line 373, in pandas.parser.TextReader.__cinit__ (pandas\parser.c:4184) File "pandas\parser.pyx", line 667, in pandas.parser.TextReader._setup_parser_source (pandas\parser.c:8449) IOError: File C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gpkitmodels\GP\aircraft\wing\jho_fitdata.csv does not exist ---------------------------------------------------------------------- Ran 6 tests in 11.187s FAILED (errors=4) Generating XML reports... Cloning into 'eVTOL'... adding test for 'aircraft_models.py' Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 48.389s 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 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) (venv2_gpkit) (root) C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\optimizer\mosek>exit 0 Build step 'Console output (build log) parsing' changed build result to FAILURE [xUnit] [INFO] - Starting to record. [xUnit] [INFO] - Processing JUnit [xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'C:\Users\jenkins\workspace\gplibrary_PR_Models\buildnode\windows10x64\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