![[Jenkins]](/csi/static/a404d988/images/svgs/logo.svg){kind=logo}
Started by upstream project "gplibrary_PR_Models" build number 62 originally caused by: GitHub pull request #146 of commit 560722b70fba2d2bfb3ff96ffbf2205b114fea58, 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 2ba6ebdb13fdf0f30a372e0c041f3cdbe9ccbe10 (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 2ba6ebdb13fdf0f30a372e0c041f3cdbe9ccbe10 # 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 Seen branch in repository origin/boombeam Seen branch in repository origin/boxspar Seen branch in repository origin/breguet_range Seen branch in repository origin/breguetsetup Seen branch in repository origin/climb Seen branch in repository origin/commercial_sizing Seen branch in repository origin/d8 Seen branch in repository origin/d8fuselage Seen branch in repository origin/electric_motor Seen branch in repository origin/fits Seen branch in repository origin/flightsegments Seen branch in repository origin/hx Seen branch in repository origin/hx_onbuild Seen branch in repository origin/interactive_simpleflight Seen branch in repository origin/master Seen branch in repository origin/materials Seen branch in repository origin/md_template Seen branch in repository origin/performance Seen branch in repository origin/pr/10/head Seen branch in repository origin/pr/100/head Seen branch in repository origin/pr/103/head Seen branch in repository origin/pr/105/head Seen branch in repository origin/pr/105/merge Seen branch in repository origin/pr/107/head Seen branch in repository origin/pr/109/head Seen branch in repository origin/pr/11/head Seen branch in repository origin/pr/11/merge Seen branch in repository origin/pr/110/head Seen branch in repository origin/pr/112/head Seen branch in repository origin/pr/113/head Seen branch in repository origin/pr/113/merge Seen branch in repository origin/pr/114/head Seen branch in repository origin/pr/115/head Seen branch in repository origin/pr/115/merge Seen branch in repository origin/pr/116/head Seen branch in repository origin/pr/118/head Seen branch in repository origin/pr/119/head Seen branch in repository origin/pr/119/merge Seen branch in repository origin/pr/12/head Seen branch in repository origin/pr/120/head Seen branch in repository origin/pr/121/head Seen branch in repository origin/pr/121/merge Seen branch in repository origin/pr/122/head Seen branch in repository origin/pr/123/head Seen branch in repository origin/pr/124/head Seen branch in repository origin/pr/125/head Seen branch in repository origin/pr/127/head Seen branch in repository origin/pr/128/head Seen branch in repository origin/pr/129/head Seen branch in repository origin/pr/13/head Seen branch in repository origin/pr/13/merge Seen branch in repository origin/pr/131/head Seen branch in repository origin/pr/132/head Seen branch in repository origin/pr/133/head Seen branch in repository origin/pr/134/head Seen branch in repository origin/pr/135/head Seen branch in repository origin/pr/136/head Seen branch in repository origin/pr/137/head Seen branch in repository origin/pr/138/head Seen branch in repository origin/pr/139/head Seen branch in repository origin/pr/14/head Seen branch in repository origin/pr/14/merge Seen branch in repository origin/pr/141/head Seen branch in repository origin/pr/143/head Seen branch in repository origin/pr/144/head Seen branch in repository origin/pr/144/merge Seen branch in repository origin/pr/145/head Seen branch in repository origin/pr/145/merge Seen branch in repository origin/pr/146/head Seen branch in repository origin/pr/146/merge Seen branch in repository origin/pr/15/head Seen branch in repository origin/pr/16/head Seen branch in repository origin/pr/17/head Seen branch in repository origin/pr/17/merge Seen branch in repository origin/pr/19/head Seen branch in repository origin/pr/19/merge Seen branch in repository origin/pr/20/head Seen branch in repository origin/pr/22/head Seen branch in repository origin/pr/22/merge Seen branch in repository origin/pr/23/head Seen branch in repository origin/pr/23/merge Seen branch in repository origin/pr/24/head Seen branch in repository origin/pr/25/head Seen branch in repository origin/pr/26/head Seen branch in repository origin/pr/26/merge Seen branch in repository origin/pr/27/head Seen branch in repository origin/pr/29/head Seen branch in repository origin/pr/30/head Seen branch in repository origin/pr/31/head Seen branch in repository origin/pr/33/head Seen branch in repository origin/pr/34/head Seen branch in repository origin/pr/35/head Seen branch in repository origin/pr/36/head Seen branch in repository origin/pr/37/head Seen branch in repository origin/pr/38/head Seen branch in repository origin/pr/39/head Seen branch in repository origin/pr/40/head Seen branch in repository origin/pr/40/merge Seen branch in repository origin/pr/42/head Seen branch in repository origin/pr/42/merge Seen branch in repository origin/pr/43/head Seen branch in repository origin/pr/44/head Seen branch in repository origin/pr/44/merge Seen branch in repository origin/pr/45/head Seen branch in repository origin/pr/46/head Seen branch in repository origin/pr/46/merge Seen branch in repository origin/pr/47/head Seen branch in repository origin/pr/47/merge Seen branch in repository origin/pr/5/head Seen branch in repository origin/pr/54/head Seen branch in repository origin/pr/54/merge Seen branch in repository origin/pr/55/head Seen branch in repository origin/pr/57/head Seen branch in repository origin/pr/58/head Seen branch in repository origin/pr/60/head Seen branch in repository origin/pr/61/head Seen branch in repository origin/pr/62/head Seen branch in repository origin/pr/63/head Seen branch in repository origin/pr/63/merge Seen branch in repository origin/pr/64/head Seen branch in repository origin/pr/69/head Seen branch in repository origin/pr/70/head Seen branch in repository origin/pr/70/merge Seen branch in repository origin/pr/71/head Seen branch in repository origin/pr/72/head Seen branch in repository origin/pr/72/merge Seen branch in repository origin/pr/73/head Seen branch in repository origin/pr/73/merge Seen branch in repository origin/pr/75/head Seen branch in repository origin/pr/75/merge Seen branch in repository origin/pr/77/head Seen branch in repository origin/pr/77/merge Seen branch in repository origin/pr/78/head Seen branch in repository origin/pr/78/merge Seen branch in repository origin/pr/80/head Seen branch in repository origin/pr/82/head Seen branch in repository origin/pr/82/merge Seen branch in repository origin/pr/83/head Seen branch in repository origin/pr/83/merge Seen branch in repository origin/pr/85/head Seen branch in repository origin/pr/85/merge Seen branch in repository origin/pr/86/head Seen branch in repository origin/pr/88/head Seen branch in repository origin/pr/88/merge Seen branch in repository origin/pr/89/head Seen branch in repository origin/pr/89/merge Seen branch in repository origin/pr/9/head Seen branch in repository origin/pr/90/head Seen branch in repository origin/pr/90/merge Seen branch in repository origin/pr/91/head Seen branch in repository origin/pr/91/merge Seen branch in repository origin/pr/92/head Seen branch in repository origin/pr/92/merge Seen branch in repository origin/pr/94/head Seen branch in repository origin/pr/96/head Seen branch in repository origin/pr/96/merge Seen branch in repository origin/pr/97/head Seen branch in repository origin/pr/97/merge Seen branch in repository origin/pr/98/head Seen branch in repository origin/pr/99/head Seen branch in repository origin/qstr Seen branch in repository origin/quadrotor Seen branch in repository origin/revert-120-SPaircraft Seen branch in repository origin/rockets Seen branch in repository origin/sigeq_paper Seen branch in repository origin/simple_HT_sizing Seen branch in repository origin/simple_flight_profile Seen branch in repository origin/standard_atmosphere Seen branch in repository origin/sutherland Seen branch in repository origin/troposphere Seen branch in repository origin/vectorizeplanform Seen branch in repository origin/wide_body Seen branch in repository origin/wvl Seen 179 remote branches > C:\Program Files\Git\cmd\git tag -l # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/include^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/DF70^{commit}" # timeout=10 > 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 2ba6ebdb13fdf0f30a372e0c041f3cdbe9ccbe10 (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 2ba6ebdb13fdf0f30a372e0c041f3cdbe9ccbe10 # timeout=3 Commit message: "Merge 560722b70fba2d2bfb3ff96ffbf2205b114fea58 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\jenkins3359269162012339616.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 1.36 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.084 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.062 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 4.920s OK Generating XML reports... Cloning into 'gassolar'... Checking out files: 43% (913/2110) Checking out files: 44% (929/2110) Checking out files: 45% (950/2110) Checking out files: 46% (971/2110) Checking out files: 47% (992/2110) Checking out files: 48% (1013/2110) Checking out files: 49% (1034/2110) Checking out files: 50% (1055/2110) Checking out files: 51% (1077/2110) Checking out files: 52% (1098/2110) Checking out files: 53% (1119/2110) Checking out files: 54% (1140/2110) Checking out files: 55% (1161/2110) Checking out files: 56% (1182/2110) Checking out files: 57% (1203/2110) Checking out files: 58% (1224/2110) Checking out files: 59% (1245/2110) Checking out files: 60% (1266/2110) Checking out files: 61% (1288/2110) Checking out files: 62% (1309/2110) Checking out files: 63% (1330/2110) Checking out files: 64% (1351/2110) Checking out files: 65% (1372/2110) Checking out files: 66% (1393/2110) Checking out files: 66% (1394/2110) Checking out files: 67% (1414/2110) Checking out files: 68% (1435/2110) Checking out files: 69% (1456/2110) Checking out files: 70% (1477/2110) Checking out files: 71% (1499/2110) Checking out files: 72% (1520/2110) Checking out files: 73% (1541/2110) Checking out files: 74% (1562/2110) Checking out files: 75% (1583/2110) Checking out files: 76% (1604/2110) Checking out files: 77% (1625/2110) Checking out files: 78% (1646/2110) Checking out files: 79% (1667/2110) Checking out files: 80% (1688/2110) Checking out files: 81% (1710/2110) Checking out files: 82% (1731/2110) Checking out files: 83% (1752/2110) Checking out files: 84% (1773/2110) Checking out files: 85% (1794/2110) Checking out files: 86% (1815/2110) Checking out files: 87% (1836/2110) Checking out files: 88% (1857/2110) Checking out files: 89% (1878/2110) Checking out files: 90% (1899/2110) Checking out files: 91% (1921/2110) Checking out files: 92% (1942/2110) Checking out files: 93% (1963/2110) Checking out files: 93% (1976/2110) Checking out files: 94% (1984/2110) Checking out files: 95% (2005/2110) Checking out files: 96% (2026/2110) Checking out files: 97% (2047/2110) Checking out files: 98% (2068/2110) Checking out files: 99% (2089/2110) Checking out files: 100% (2110/2110) Checking out files: 100% (2110/2110), done. 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-fs9a38-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 [3.076s]: 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 [2.126s]: 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 [3.844s]: 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 0.148 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 0.109 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 0.381 seconds. Allowing negative dual variable(s) as small as -1.52372280197e-13. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 97517.0233 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 2.84 seconds. Allowing negative dual variable(s) as small as -1.532644e-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 [6.491s]: 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 15.537s 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-hzoibq-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 [1.075s]: 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 [0.344s]: 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 [0.357s]: 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 [0.385s]: 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 2.161s 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 24184.7528318 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%) Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485057 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 2.896s OK Generating XML reports... Cloning into 'SPaircraft'... Checking out files: 29% (1003/3413) Checking out files: 30% (1024/3413) Checking out files: 31% (1059/3413) Checking out files: 32% (1093/3413) Checking out files: 33% (1127/3413) Checking out files: 34% (1161/3413) Checking out files: 35% (1195/3413) Checking out files: 36% (1229/3413) Checking out files: 37% (1263/3413) Checking out files: 38% (1297/3413) Checking out files: 39% (1332/3413) Checking out files: 40% (1366/3413) Checking out files: 41% (1400/3413) Checking out files: 42% (1434/3413) Checking out files: 43% (1468/3413) Checking out files: 44% (1502/3413) Checking out files: 45% (1536/3413) Checking out files: 46% (1570/3413) Checking out files: 47% (1605/3413) Checking out files: 48% (1639/3413) Checking out files: 49% (1673/3413) Checking out files: 50% (1707/3413) Checking out files: 51% (1741/3413) Checking out files: 52% (1775/3413) Checking out files: 53% (1809/3413) Checking out files: 54% (1844/3413) Checking out files: 55% (1878/3413) Checking out files: 55% (1890/3413) Checking out files: 56% (1912/3413) Checking out files: 57% (1946/3413) Checking out files: 58% (1980/3413) Checking out files: 59% (2014/3413) Checking out files: 60% (2048/3413) Checking out files: 61% (2082/3413) Checking out files: 62% (2117/3413) Checking out files: 63% (2151/3413) Checking out files: 64% (2185/3413) Checking out files: 65% (2219/3413) Checking out files: 66% (2253/3413) Checking out files: 67% (2287/3413) Checking out files: 68% (2321/3413) Checking out files: 69% (2355/3413) Checking out files: 70% (2390/3413) Checking out files: 71% (2424/3413) Checking out files: 72% (2458/3413) Checking out files: 73% (2492/3413) Checking out files: 74% (2526/3413) Checking out files: 75% (2560/3413) Checking out files: 76% (2594/3413) Checking out files: 77% (2629/3413) Checking out files: 78% (2663/3413) Checking out files: 79% (2697/3413) Checking out files: 79% (2703/3413) Checking out files: 80% (2731/3413) Checking out files: 81% (2765/3413) Checking out files: 82% (2799/3413) Checking out files: 83% (2833/3413) Checking out files: 84% (2867/3413) Checking out files: 85% (2902/3413) Checking out files: 86% (2936/3413) Checking out files: 87% (2970/3413) Checking out files: 88% (3004/3413) Checking out files: 89% (3038/3413) Checking out files: 90% (3072/3413) Checking out files: 91% (3106/3413) Checking out files: 91% (3123/3413) Checking out files: 92% (3140/3413) Checking out files: 93% (3175/3413) Checking out files: 94% (3209/3413) Checking out files: 95% (3243/3413) Checking out files: 96% (3277/3413) Checking out files: 97% (3311/3413) Checking out files: 98% (3345/3413) Checking out files: 99% (3379/3413) Checking out files: 100% (3413/3413) Checking out files: 100% (3413/3413), done. Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to c:\users\jenkins\appdata\local\temp\pip-_fge8r-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 2519608.18895 force_pound * meter but the right hand side evaluated to 2468464.06375 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 32774.5113273 force_pound but the right hand side evaluated to 32399.9999971 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116761 meter but the right hand side evaluated to 1.96396134049 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 48608.9470448 newton but the right hand side evaluated to 48529.7648632 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 49704.3801465 newton but the right hand side evaluated to 49411.097846 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 18949.0917099 newton but the right hand side evaluated to 18923.0934014 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 16591.9887289 newton but the right hand side evaluated to 16565.7886653 newton (Allowable error: 0.1%, Actual error: 0.16%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1002807.08292 joule / kilogram but the right hand side evaluated to 1.15238754071 megajoule / kilogram (Allowable error: 0.1%, Actual error: 7.1%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 895037.344257 joule / kilogram but the right hand side evaluated to 0.897466496888 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 1072947.06672 joule / kilogram but the right hand side evaluated to 1.19569627958 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 596870.318966 joule / kilogram but the right hand side evaluated to 0.615556911205 megajoule / kilogram (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 786921.749687 joule / kilogram but the right hand side evaluated to 0.790360523077 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 18.3465545269 meter but the right hand side evaluated to 16.3967770585 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 11.0854063332 but the right hand side evaluated to 4.68078557422 (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 9.79174204358 but the right hand side evaluated to 4.68078556507 (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 8.22912373735 but the right hand side evaluated to 4.68078557695 (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 18.4249269815 meter but the right hand side evaluated to 18.1659855689 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 18.4249269815 meter but the right hand side evaluated to 18.2854584246 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 4.49878822702 but the right hand side evaluated to 4.61598246102 (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 4.58150008347 but the right hand side evaluated to 4.64634055001 (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 7.27503338511 but the right hand side evaluated to 4.61598246102 (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 7.45366715341 but the right hand side evaluated to 4.64634055001 (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 2504978.86142 force_pound * meter but the right hand side evaluated to 2454471.7311 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 32774.4782023 force_pound but the right hand side evaluated to 32399.9999957 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 2.21510116721 meter but the right hand side evaluated to 1.96382970731 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 982256.575739 joule / kilogram but the right hand side evaluated to 1.20547043731 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 1151137.23779 joule / kilogram but the right hand side evaluated to 1.8837929101 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 18.4111645083 meter but the right hand side evaluated to 16.4524848809 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 11.0893090844 but the right hand side evaluated to 4.73132109879 (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 9.74913123736 but the right hand side evaluated to 4.7313210766 (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 8.19783347972 but the right hand side evaluated to 4.73132110658 (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 18.4750001816 meter but the right hand side evaluated to 18.2223453086 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 18.4750001816 meter but the right hand side evaluated to 18.338451297 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 4.55043967351 but the right hand side evaluated to 4.66698075503 (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 4.63158777564 but the right hand side evaluated to 4.69671701589 (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 7.43022191518 but the right hand side evaluated to 4.66698075503 (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 7.49547698747 but the right hand side evaluated to 4.69671701589 (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 2481467.36886 force_pound * meter but the right hand side evaluated to 2426090.12831 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 32774.1936696 force_pound but the right hand side evaluated to 32399.9999985 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116774 meter but the right hand side evaluated to 1.83120021509 meter (Allowable error: 0.1%, Actual error: 17%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1203381.87763 joule / kilogram but the right hand side evaluated to 1.66382055049 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 18.469376661 meter but the right hand side evaluated to 16.643202047 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 11.0473079049 but the right hand side evaluated to 4.80180969709 (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 9.67070923635 but the right hand side evaluated to 4.80180968786 (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 8.22137517039 but the right hand side evaluated to 4.80180969957 (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 18.6280059541 meter but the right hand side evaluated to 18.3449819391 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 18.6280059541 meter but the right hand side evaluated to 18.4744010704 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 4.59899146795 but the right hand side evaluated to 4.72922188867 (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 4.68922905911 but the right hand side evaluated to 4.76258533329 (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 7.45561753696 but the right hand side evaluated to 4.72922188867 (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 7.54888787803 but the right hand side evaluated to 4.76258533329 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2455569.09902 force_pound * meter but the right hand side evaluated to 2407712.08364 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 32774.4701813 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 2.21510116808 meter but the right hand side evaluated to 1.99552088205 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 1227633.90908 joule / kilogram but the right hand side evaluated to 1.72359767517 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 677538.80927 joule / kilogram but the right hand side evaluated to 0.679181829291 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 18.4156357914 meter but the right hand side evaluated to 16.4239734936 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 10.9749703416 but the right hand side evaluated to 4.76255494908 (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 9.75289713768 but the right hand side evaluated to 4.76255494427 (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 8.15871877106 but the right hand side evaluated to 4.76255495038 (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 18.4488731626 meter but the right hand side evaluated to 18.2046638888 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 18.4488731626 meter but the right hand side evaluated to 18.3176193634 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 4.58582641684 but the right hand side evaluated to 4.69978375735 (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 4.66559316001 but the right hand side evaluated to 4.72894476291 (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 7.50481946396 but the right hand side evaluated to 4.69978375735 (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 7.52766089635 but the right hand side evaluated to 4.72894476291 (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 2436786.78567 force_pound * meter but the right hand side evaluated to 2390898.70379 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 32774.4465836 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116786 meter but the right hand side evaluated to 2.03201158062 meter (Allowable error: 0.1%, Actual error: 8.3%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1233975.56472 joule / kilogram but the right hand side evaluated to 1.62326440488 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 18.4095779248 meter but the right hand side evaluated to 16.3813512939 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 10.9310504793 but the right hand side evaluated to 4.78771753095 (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 9.87336217918 but the right hand side evaluated to 4.78771752026 (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 8.15464694182 but the right hand side evaluated to 4.78771753358 (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 18.4102716882 meter but the right hand side evaluated to 18.1746823596 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 18.4102716882 meter but the right hand side evaluated to 18.283934025 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 4.61574341867 but the right hand side evaluated to 4.72672177351 (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 4.69362666674 but the right hand side evaluated to 4.75513504729 (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 7.53648537493 but the right hand side evaluated to 4.72672177351 (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 7.55140174663 but the right hand side evaluated to 4.75513504729 (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 2418323.5093 force_pound * meter but the right hand side evaluated to 2374882.7219 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 32774.4982041 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 2.21510116791 meter but the right hand side evaluated to 2.08235637579 meter (Allowable error: 0.1%, Actual error: 6%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1244506.57715 joule / kilogram but the right hand side evaluated to 1.55926566872 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 664749.972619 joule / kilogram but the right hand side evaluated to 0.667401311998 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 18.4000465621 meter but the right hand side evaluated to 16.3223761329 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 10.9040373975 but the right hand side evaluated to 4.78950207101 (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 10.025976838 but the right hand side evaluated to 4.78950206221 (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 8.14555535301 but the right hand side evaluated to 4.78950207321 (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 18.3617975771 meter but the right hand side evaluated to 18.1374290135 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 18.3617975771 meter but the right hand side evaluated to 18.2416868196 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 4.62507756402 but the right hand side evaluated to 4.73131691832 (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 4.69987173203 but the right hand side evaluated to 4.75851353595 (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 7.56534504128 but the right hand side evaluated to 4.73131691832 (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 7.58381544417 but the right hand side evaluated to 4.75851353595 (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 2405738.08598 force_pound * meter but the right hand side evaluated to 2358168.58006 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 32774.4304555 force_pound but the right hand side evaluated to 32399.9999978 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 2.21510116783 meter but the right hand side evaluated to 1.9749124293 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 1245747.46227 joule / kilogram but the right hand side evaluated to 1.35773088465 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 18.4441339466 meter but the right hand side evaluated to 16.4749757614 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 10.9331054479 but the right hand side evaluated to 4.83171687712 (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 10.1921366076 but the right hand side evaluated to 4.83171685886 (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 8.19565485175 but the right hand side evaluated to 4.83171688112 (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 18.4861289028 meter but the right hand side evaluated to 18.2368494316 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 18.4861289028 meter but the right hand side evaluated to 18.351862856 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 4.64971733131 but the right hand side evaluated to 4.76697771519 (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 4.73177264965 but the right hand side evaluated to 4.79704137467 (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 7.54212799149 but the right hand side evaluated to 4.76697771519 (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 7.59702841393 but the right hand side evaluated to 4.79704137467 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, MaxClimbDistance_Mission, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2391780.99072 force_pound * meter but the right hand side evaluated to 2346059.90436 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 32774.4177152 force_pound but the right hand side evaluated to 32399.9999979 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 2.01208313426 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 1263255.20327 joule / kilogram but the right hand side evaluated to 1.32934387553 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 643003.052038 joule / kilogram but the right hand side evaluated to 0.644587737329 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 18.4391892779 meter but the right hand side evaluated to 16.4333013483 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 10.9270563394 but the right hand side evaluated to 4.82709767968 (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 10.3328456014 but the right hand side evaluated to 4.82709765586 (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 8.18819577758 but the right hand side evaluated to 4.82709768459 (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 18.4531697871 meter but the right hand side evaluated to 18.2123791267 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 18.4531697871 meter but the right hand side evaluated to 18.3237343833 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 4.65099110333 but the right hand side evaluated to 4.764562707 (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 4.73069774888 but the right hand side evaluated to 4.79369449145 (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 7.55428962784 but the right hand side evaluated to 4.764562707 (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 7.61783414132 but the right hand side evaluated to 4.79369449145 (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 2376281.4096 force_pound * meter but the right hand side evaluated to 2334599.84127 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 32774.4060907 force_pound but the right hand side evaluated to 32399.9999985 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116802 meter but the right hand side evaluated to 2.09817122759 meter (Allowable error: 0.1%, Actual error: 5.3%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1283641.07743 joule / kilogram but the right hand side evaluated to 1.28936033659 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 18.4146015212 meter but the right hand side evaluated to 16.3183424853 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 10.9374655023 but the right hand side evaluated to 4.82438035731 (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 10.5713485506 but the right hand side evaluated to 4.82438034788 (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 8.19385266456 but the right hand side evaluated to 4.82438035988 (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 18.3565592238 meter but the right hand side evaluated to 18.1377529142 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 18.3565592238 meter but the right hand side evaluated to 18.2401831318 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 4.66215835795 but the right hand side evaluated to 4.76702071489 (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 4.7362726327 but the right hand side evaluated to 4.79394174373 (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 7.6200761563 but the right hand side evaluated to 4.76702071489 (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 7.68939043937 but the right hand side evaluated to 4.79394174373 (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 324 seconds. Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 329.262s 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-ycutqo-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-fjjok0-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 1.48 seconds. Allowing negative dual variable(s) as small as -1.51858678632e-10. Warning: Variable Re_Mission/FlightSegment.38/AircraftPerf.38/WingAero.38 could cause inaccurate result because it is below lower bound. Solution is 120042.1842 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 121471.1932 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 2.03 seconds. Allowing negative dual variable(s) as small as -1.50439240959e-10. Warning: Variable Re_Mission.1/FlightSegment.78/AircraftPerf.78/WingAero.78 could cause inaccurate result because it is below lower bound. Solution is 122823.1065 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 123244.7221 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 1.18 seconds. Allowing negative dual variable(s) as small as -2.85909904511e-10. Using solver 'mosek' Solving for 2910 variables. Solving took 0.644 seconds. Allowing negative dual variable(s) as small as -2.76680822133e-12. Using solver 'mosek' Solving for 5670 variables. Solving took 1.8 seconds. Allowing negative dual variable(s) as small as -1.51872426829e-10. Warning: Variable Re_Mission/FlightSegment.38/AircraftPerf.38/WingAero.38 could cause inaccurate result because it is below lower bound. Solution is 120042.1842 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 121471.1932 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 2.22 seconds. Allowing negative dual variable(s) as small as -9.66462122775e-15. 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 123244.7110 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 1.46 seconds. Allowing negative dual variable(s) as small as -2.83166660758e-10. Using solver 'mosek' Solving for 2910 variables. Solving took 0.633 seconds. Allowing negative dual variable(s) as small as -2.76548230897e-12. Using solver 'mosek' Solving for 288 variables. Solving took 1.5 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 0.064 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 1.13 seconds. Allowing negative dual variable(s) as small as -2.76612247234e-12. Using solver 'mosek_cli' Solving for 2910 variables. Solving took 0.612 seconds. Allowing negative dual variable(s) as small as -2.766088e-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 [9.355s]: 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 [11.614s]: 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 159.078s 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-pwgkr_-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 16.561s 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