Started by upstream project "gplibrary_PR_Models" build number 63 originally caused by: GitHub pull request #146 of commit 6a04d7a8531e7ba8ef06aa8f9881443b92d069c7, no merge conflicts. Building remotely on 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 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 (refs/remotes/origin/pr/146/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 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 # 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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C:\Program Files\Git\cmd\git rev-parse "refs/tags/linking^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/csv^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/start^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/pay^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/sum^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/clean^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/sys^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/pshaft^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/solarmd^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/climb^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/fuse^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/mission^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/discret^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/plot^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/md^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/atm^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/make^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/eng^{commit}" # timeout=10 Checking out Revision 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 (origin/pr/146/merge, origin/master) > C:\Program Files\Git\cmd\git config core.sparsecheckout # timeout=10 > C:\Program Files\Git\cmd\git checkout -f 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 # timeout=3 Commit message: "Merge 6ef200c93b75c6359f18295b5a541fc98586263d into 62026ae2ee1965aa7005a73cc1f60d704fd1c8b0" Using 'Changelog to branch' strategy. Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [description-setter] Description set: <a title="allow for different spar in tailboom bending and flex models" href="https://github.com/convexengineering/gplibrary/pull/146">PR 146</a>: allow for different spar in tailboom bending and flex models [Execution node] check if [windows10x64] is in [[macys, macys_Sierra, 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\jenkins8896936422285662299.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:\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:\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-4.4.2-cp27-cp27m-win_amd64.whl Installing collected packages: coverage Successfully installed coverage-4.4.2 (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 0.02. 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: 0.02 ************************************ 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 req_set.py, line 480 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_set.py, line 503 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 590 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_set.py, line 496 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_set.py, line 496 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_set.py, line 767 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_set.py, line 775 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 619 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 985 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 369 (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 req_set.py, line 480 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_set.py, line 496 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_set.py, line 496 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_set.py, line 496 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_set.py, line 767 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 985 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 369 (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 4.27 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.03 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 1.97 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 6.696s OK Generating XML reports... Cloning into 'gassolar'... 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Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) 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) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-sbwjmm-build 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) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) Installing collected packages: gpfit Running setup.py install for gpfit: started Running setup.py install for gpfit: finished with status 'done' Successfully installed gpfit-0.1 Processing 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) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gassolar==0.0.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) 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) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) Installing collected packages: gassolar Running setup.py install for gassolar: started Running setup.py install for gassolar: finished with status 'done' Successfully installed gassolar-0.0.0.0 Running tests... ---------------------------------------------------------------------- EEC:\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) EE ====================================================================== ERROR [3.531s]: test_gassolar_gas_gas_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 "gas.py", line 209, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 166, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 51, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [2.422s]: test_gassolar_gas_gas_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 "gas.py", line 209, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 166, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 51, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [4.151s]: test_gassolar_solar_solar_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\woradding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 593 variables. Solving took 0.143 seconds. Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2090 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 593 variables. Solving took 0.174 seconds. Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2090 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 1206 variables. Solving took 0.371 seconds. Allowing negative dual variable(s) as small as -1.55664907287e-13. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 97517.0232 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 97518.5695 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 3 is a constraining latitude 4 is a constraining latitude 5 is a constraining latitude 6 is a constraining latitude 7 is a constraining latitude 8 is a constraining latitude 9 is a constraining latitude 10 is a constraining latitude 11 is a constraining latitude Using solver 'mosek_cli' Solving for 1206 variables. Solving took 2.81 seconds. Allowing negative dual variable(s) as small as -1.521817e-13. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 97516.8049 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 97518.7552 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 3 is a constraining latitude 4 is a constraining latitude 5 is a constraining latitude 6 is a constraining latitude 7 is a constraining latitude 8 is a constraining latitude 9 is a constraining latitude 10 is a constraining latitude 11 is a constraining latitude kspace\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 "solar.py", line 359, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 309, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 49, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [6.277s]: test_gassolar_solar_solar_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 "solar.py", line 359, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 309, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 49, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ---------------------------------------------------------------------- Ran 4 tests in 16.381s FAILED (errors=4) Generating XML reports... Cloning into 'jho'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) 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) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-frmep1-build 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) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) Running tests... ---------------------------------------------------------------------- EEEE ====================================================================== ERROR [1.289s]: test_model_jho_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 "jho.py", line 355, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ====================================================================== ERROR [0.311s]: test_model_jho_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 "jho.py", line 355, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ====================================================================== ERROR [0.296s]: test_model_print_perf_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\jenkinadding test for 'model/jho.py' adding test for 'model/print_perf.py' s\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 "print_perf.py", line 192, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ====================================================================== ERROR [0.245s]: test_model_print_perf_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 "print_perf.py", line 192, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ---------------------------------------------------------------------- Ran 4 tests in 2.141s FAILED (errors=4) 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) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) Installing collected packages: turbofan Running setup.py install for turbofan: started Running setup.py install for turbofan: finished with status 'done' Successfully installed turbofan-0.0.0.0 adding test for 'turbofan/engine_validation.py' Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528315 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%) Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485056 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 1.948s OK Generating XML reports... 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Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to c:\users\jenkins\appdata\local\temp\pip-yd5usz-build 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) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) adding test for 'SP_aircraft.py' Solving over 9 passes. Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2519606.97211 force_pound * meter but the right hand side evaluated to 2468463.49191 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 32774.4651227 force_pound but the right hand side evaluated to 32399.999996 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 2.21510116733 meter but the right hand side evaluated to 1.96396127826 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 48608.9213409 newton but the right hand side evaluated to 48529.7459721 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 49704.4038192 newton but the right hand side evaluated to 49411.1346435 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 18949.0774642 newton but the right hand side evaluated to 18923.0796667 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 16591.9836816 newton but the right hand side evaluated to 16565.781452 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 1002809.46296 joule / kilogram but the right hand side evaluated to 1.15240022647 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 895039.523501 joule / kilogram but the right hand side evaluated to 0.897468588156 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 1072947.21007 joule / kilogram but the right hand side evaluated to 1.19570081543 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 596870.364088 joule / kilogram but the right hand side evaluated to 0.615556931058 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 786922.851203 joule / kilogram but the right hand side evaluated to 0.790361694107 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 18.3465561104 meter but the right hand side evaluated to 16.3967786088 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 11.0854063668 but the right hand side evaluated to 4.68078664886 (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 9.79174121963 but the right hand side evaluated to 4.68078663558 (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 8.22912550941 but the right hand side evaluated to 4.68078665269 (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 18.4249284585 meter but the right hand side evaluated to 18.1659874985 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 18.4249284585 meter but the right hand side evaluated to 18.2854648819 meter (Allowable error: 0.1%, Actual error: 0.76%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.49878937217 but the right hand side evaluated to 4.61598364953 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.58150152162 but the right hand side evaluated to 4.64634289359 (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 7.27503538628 but the right hand side evaluated to 4.61598364953 (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 7.45366683182 but the right hand side evaluated to 4.64634289359 (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 2504977.05484 force_pound * meter but the right hand side evaluated to 2454470.73525 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 32774.4986806 force_pound but the right hand side evaluated to 32399.9999998 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 2.21510116821 meter but the right hand side evaluated to 1.96383028627 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 982256.649826 joule / kilogram but the right hand side evaluated to 1.20546986482 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 1151137.27093 joule / kilogram but the right hand side evaluated to 1.88379337 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 18.4111616084 meter but the right hand side evaluated to 16.4524814453 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 11.0893110254 but the right hand side evaluated to 4.73132116241 (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 9.74913460777 but the right hand side evaluated to 4.73132116133 (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 8.1978343575 but the right hand side evaluated to 4.73132116279 (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 18.4749966012 meter but the right hand side evaluated to 18.2223414827 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 18.4749966012 meter but the right hand side evaluated to 18.3384444752 meter (Allowable error: 0.1%, Actual error: 0.74%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.55043970198 but the right hand side evaluated to 4.66698068727 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.63158654387 but the right hand side evaluated to 4.69671618663 (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 7.43022259744 but the right hand side evaluated to 4.66698068727 (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 7.49547630411 but the right hand side evaluated to 4.69671618663 (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 2481462.96903 force_pound * meter but the right hand side evaluated to 2426089.25982 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 32774.228189 force_pound but the right hand side evaluated to 32399.9999991 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116794 meter but the right hand side evaluated to 1.83120073421 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 1203383.40361 joule / kilogram but the right hand side evaluated to 1.66382090324 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 18.4693761001 meter but the right hand side evaluated to 16.6432011917 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 11.0473069419 but the right hand side evaluated to 4.80180785135 (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 9.67070473444 but the right hand side evaluated to 4.80180784578 (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 8.22137489695 but the right hand side evaluated to 4.80180785288 (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 18.6280054484 meter but the right hand side evaluated to 18.3449860123 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 18.6280054484 meter but the right hand side evaluated to 18.4744028375 meter (Allowable error: 0.1%, Actual error: 0.82%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.59899065851 but the right hand side evaluated to 4.72922125226 (Allowable error: 0.1%, Actual error: 2.8%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.68922420243 but the right hand side evaluated to 4.76258409047 (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 7.45561874846 but the right hand side evaluated to 4.72922125226 (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 7.54888001912 but the right hand side evaluated to 4.76258409047 (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 2455568.03593 force_pound * meter but the right hand side evaluated to 2407712.0543 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 32774.5065722 force_pound but the right hand side evaluated to 32399.9999986 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116797 meter but the right hand side evaluated to 1.99551624401 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 1227633.62572 joule / kilogram but the right hand side evaluated to 1.72359591654 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 677538.018931 joule / kilogram but the right hand side evaluated to 0.679181102338 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 18.4156378157 meter but the right hand side evaluated to 16.4239800392 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 10.9749710169 but the right hand side evaluated to 4.76255540167 (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 9.75289879201 but the right hand side evaluated to 4.76255539476 (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 8.15871986245 but the right hand side evaluated to 4.76255540373 (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 18.4488787072 meter but the right hand side evaluated to 18.2046683736 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 18.4488787072 meter but the right hand side evaluated to 18.3176231277 meter (Allowable error: 0.1%, Actual error: 0.71%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.58582617972 but the right hand side evaluated to 4.69978394799 (Allowable error: 0.1%, Actual error: 2.4%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.66559164555 but the right hand side evaluated to 4.72894476154 (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 7.50481973064 but the right hand side evaluated to 4.69978394799 (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 7.52765870787 but the right hand side evaluated to 4.72894476154 (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 2436784.29766 force_pound * meter but the right hand side evaluated to 2390898.73131 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 32774.5832901 force_pound but the right hand side evaluated to 32399.9999967 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 2.21510116766 meter but the right hand side evaluated to 2.03201077536 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 1233974.74828 joule / kilogram but the right hand side evaluated to 1.62325571521 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 18.4095787258 meter but the right hand side evaluated to 16.381352768 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 10.9310493515 but the right hand side evaluated to 4.78771807385 (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 9.87336290913 but the right hand side evaluated to 4.78771806103 (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 8.15464728028 but the right hand side evaluated to 4.78771807802 (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 18.4102729467 meter but the right hand side evaluated to 18.1746837288 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 18.4102729467 meter but the right hand side evaluated to 18.2839285196 meter (Allowable error: 0.1%, Actual error: 0.69%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.61574390414 but the right hand side evaluated to 4.72672234031 (Allowable error: 0.1%, Actual error: 2.3%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.69362289421 but the right hand side evaluated to 4.75513382747 (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 7.53648462491 but the right hand side evaluated to 4.72672234031 (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 7.55139742793 but the right hand side evaluated to 4.75513382747 (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 2418322.98351 force_pound * meter but the right hand side evaluated to 2374882.63527 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 32774.5144057 force_pound but the right hand side evaluated to 32399.9999987 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116795 meter but the right hand side evaluated to 2.08235263481 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 1244505.64767 joule / kilogram but the right hand side evaluated to 1.5592532751 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 664749.45563 joule / kilogram but the right hand side evaluated to 0.667400634129 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 18.4000472828 meter but the right hand side evaluated to 16.3223803903 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 10.9040374263 but the right hand side evaluated to 4.78950272226 (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 10.0259733665 but the right hand side evaluated to 4.78950271435 (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 8.14555654623 but the right hand side evaluated to 4.78950272423 (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 18.3618009294 meter but the right hand side evaluated to 18.1374314282 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 18.3618009294 meter but the right hand side evaluated to 18.2416891277 meter (Allowable error: 0.1%, Actual error: 0.65%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.6250776109 but the right hand side evaluated to 4.73131730985 (Allowable error: 0.1%, Actual error: 2.2%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.69987129972 but the right hand side evaluated to 4.75851389831 (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 7.56534501566 but the right hand side evaluated to 4.73131730985 (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 7.58381273232 but the right hand side evaluated to 4.75851389831 (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 2405738.32729 force_pound * meter but the right hand side evaluated to 2358168.7639 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 32774.4758797 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 2.21510116771 meter but the right hand side evaluated to 1.97490653813 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 1245747.14297 joule / kilogram but the right hand side evaluated to 1.3577266556 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 18.4441361895 meter but the right hand side evaluated to 16.4749836018 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 10.9331075667 but the right hand side evaluated to 4.83171702336 (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 10.1921344423 but the right hand side evaluated to 4.83171700149 (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 8.19565640869 but the right hand side evaluated to 4.83171702812 (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 18.4861355153 meter but the right hand side evaluated to 18.2368549131 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 18.4861355153 meter but the right hand side evaluated to 18.3518668896 meter (Allowable error: 0.1%, Actual error: 0.73%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.64971665889 but the right hand side evaluated to 4.76697758047 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.73177163611 but the right hand side evaluated to 4.79704085161 (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 7.54212787993 but the right hand side evaluated to 4.76697758047 (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 7.59702858155 but the right hand side evaluated to 4.79704085161 (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 2391782.9185 force_pound * meter but the right hand side evaluated to 2346060.05692 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 32774.4388132 force_pound but the right hand side evaluated to 32399.9999975 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116779 meter but the right hand side evaluated to 2.01207937633 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 1263253.58845 joule / kilogram but the right hand side evaluated to 1.32933565278 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 643003.068958 joule / kilogram but the right hand side evaluated to 0.644587597572 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 18.4391902499 meter but the right hand side evaluated to 16.4333056866 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 10.9270587078 but the right hand side evaluated to 4.82709805813 (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 10.3328482589 but the right hand side evaluated to 4.82709803548 (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 8.1881975458 but the right hand side evaluated to 4.82709806288 (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 18.4531732595 meter but the right hand side evaluated to 18.2123822554 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 18.4531732595 meter but the right hand side evaluated to 18.3237342442 meter (Allowable error: 0.1%, Actual error: 0.7%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.65099102076 but the right hand side evaluated to 4.76456297072 (Allowable error: 0.1%, Actual error: 2.4%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.73069878961 but the right hand side evaluated to 4.79369389687 (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 7.55429366134 but the right hand side evaluated to 4.76456297072 (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 7.61783606421 but the right hand side evaluated to 4.79369389687 (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 2376282.18216 force_pound * meter but the right hand side evaluated to 2334599.76525 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 32774.3722475 force_pound but the right hand side evaluated to 32399.9999994 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 2.21510116812 meter but the right hand side evaluated to 2.09817228182 meter (Allowable error: 0.1%, Actual error: 5.3%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1283640.76751 joule / kilogram but the right hand side evaluated to 1.28935945341 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 18.414600592 meter but the right hand side evaluated to 16.3183404618 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 10.9374647969 but the right hand side evaluated to 4.82438055082 (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 10.5713483838 but the right hand side evaluated to 4.82438054397 (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 8.19385237739 but the right hand side evaluated to 4.82438055251 (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 18.3565573539 meter but the right hand side evaluated to 18.1377516362 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 18.3565573539 meter but the right hand side evaluated to 18.2401825953 meter (Allowable error: 0.1%, Actual error: 0.63%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.66215876028 but the right hand side evaluated to 4.76702103874 (Allowable error: 0.1%, Actual error: 2.2%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.7362741766 but the right hand side evaluated to 4.79394226619 (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 7.62007526706 but the right hand side evaluated to 4.76702103874 (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 7.68939298504 but the right hand side evaluated to 4.79394226619 (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 142 seconds. Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 146.825s OK Generating XML reports... Cloning into 'solar'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) 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) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-xvleiy-build 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) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) Collecting git+https://github.com/convexengineering/gassolar.git Cloning https://github.com/convexengineering/gassolar.git to c:\users\jenkins\appdata\local\temp\pip-cricad-build 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) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gassolar==0.0.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) 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) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) 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) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from solar==0.0.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) 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) Requirement already satisfied: gpkitmodels in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek (from solar==0.0.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->solar==0.0.0.0) Installing collected packages: solar Running setup.py install for solar: started Running setup.py install for solar: finished with status 'done' Successfully installed solar-0.0.0.0 adding test for 'solar/solar.py' adding test for 'solar/sens_chart.py' adding test for 'solar/season.py' Using solver 'mosek' Solving for 5670 variables. Solving took 1.63 seconds. Allowing negative dual variable(s) as small as -5.06703237335e-14. Warning: Variable Re_Mission/FlightSegment.38/AircraftPerf.38/WingAero.38 could cause inaccurate result because it is below lower bound. Solution is 120042.1834 but bound is 125000.0000 Warning: Variable Re_Mission/FlightSegment.39/AircraftPerf.39/WingAero.39 could cause inaccurate result because it is below lower bound. Solution is 121471.1792 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 1.55 seconds. Allowing negative dual variable(s) as small as -6.83580961206e-12. Warning: Variable Re_Mission.1/FlightSegment.78/AircraftPerf.78/WingAero.78 could cause inaccurate result because it is below lower bound. Solution is 122823.1054 but bound is 125000.0000 Warning: Variable Re_Mission.1/FlightSegment.79/AircraftPerf.79/WingAero.79 could cause inaccurate result because it is below lower bound. Solution is 123244.7114 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 1.23 seconds. Allowing negative dual variable(s) as small as -2.8892419405e-10. Using solver 'mosek' Solving for 2910 variables. Solving took 0.658 seconds. Allowing negative dual variable(s) as small as -2.76720125842e-12. Using solver 'mosek' Solving for 5670 variables. Solving took 1.76 seconds. Allowing negative dual variable(s) as small as -8.98514330538e-14. Warning: Variable Re_Mission/FlightSegment.38/AircraftPerf.38/WingAero.38 could cause inaccurate result because it is below lower bound. Solution is 120042.1834 but bound is 125000.0000 Warning: Variable Re_Mission/FlightSegment.39/AircraftPerf.39/WingAero.39 could cause inaccurate result because it is below lower bound. Solution is 121471.1792 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 1.53 seconds. Allowing negative dual variable(s) as small as -6.84063436778e-12. Warning: Variable Re_Mission.1/FlightSegment.78/AircraftPerf.78/WingAero.78 could cause inaccurate result because it is below lower bound. Solution is 122823.1054 but bound is 125000.0000 Warning: Variable Re_Mission.1/FlightSegment.79/AircraftPerf.79/WingAero.79 could cause inaccurate result because it is below lower bound. Solution is 123244.7114 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 1.27 seconds. Allowing negative dual variable(s) as small as -2.85684046811e-10. Using solver 'mosek' Solving for 2910 variables. Solving took 0.548 seconds. Allowing negative dual variable(s) as small as -2.62842317583e-12. Using solver 'mosek' Solving for 288 variables. Solving took 0.075 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 122179.8905 but bound is 125000.0000 Using solver 'mosek' Solving for 288 variables. Solving took 0.058 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 122179.8905 but bound is 125000.0000 Using solver 'mosek' Solving for 2910 variables. Solving took 0.624 seconds. Allowing negative dual variable(s) as small as -2.62949260198e-12. Using solver 'mosek_cli' Solving for 2910 variables. Solving took 0.728 seconds. Allowing negative dual variable(s) as small as -2.766245e-12. 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) ....EE ====================================================================== ERROR [7.453s]: test_solar_solar_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 "solar.py", line 486, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 467, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 85, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [13.306s]: test_solar_solar_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 "solar.py", line 486, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 467, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 85, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\constraints\model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ---------------------------------------------------------------------- Ran 6 tests in 159.722s FAILED (errors=2) Generating XML reports... Cloning into 'gplibrary'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) 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) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-mztvx7-build 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) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) Processing c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek\gplibrary Requirement already satisfied (use --upgrade to upgrade): gpkitmodels==0.0.0.0 from file:///C:/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/windows10x64/optimizer/mosek/gplibrary in c:\users\jenkins\workspace\gplibrary_pr_models\buildnode\windows10x64\optimizer\mosek 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) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py' adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py' Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3838 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9775 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2262061.5401 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2262061.2755 but bound is 1000000.0000 Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2262068.0066 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2262068.0066 but bound is 1000000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 2147759.9054 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 2232694.7572 but bound is 700000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 2232695.1475 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 2232695.1475 but bound is 700000.0000 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 2.959s OK Generating XML reports... USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'git+https://github.com/hoburg/turbofan.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 (venv2_gpkit) (root) 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] - 7 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