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Started by upstream project "gpkit_commons_PR_Models" build number 19 originally caused by: GitHub pull request #120 of commit 20b9a911e7dd76930a874b07fd34e2bd2ce9db23, no merge conflicts. Building remotely on windows10x64 in workspace C:\Users\jenkins\workspace\gpkit_commons_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\gpkit_commons_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 5208c8532cc1f370d4be014731ed4cd76f40e5de (refs/remotes/origin/pr/120/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 5208c8532cc1f370d4be014731ed4cd76f40e5de # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "HEAD^{commit}" # timeout=10 Seen branch in repository origin/1682literate Seen branch in repository origin/1682master Seen branch in repository origin/Breakdown Seen branch in repository origin/SPaircraft Seen branch in repository origin/aerosurf Seen branch in repository origin/atmosphere 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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/quadrotor 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/tailfoam Seen branch in repository origin/troposphere Seen branch in repository origin/wide_body Seen 153 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 5208c8532cc1f370d4be014731ed4cd76f40e5de (origin/pr/120/merge, origin/master) > C:\Program Files\Git\cmd\git config core.sparsecheckout # timeout=10 > C:\Program Files\Git\cmd\git checkout -f 5208c8532cc1f370d4be014731ed4cd76f40e5de # timeout=3 Commit message: "Merge 20b9a911e7dd76930a874b07fd34e2bd2ce9db23 into 662ac9f55e6990e08a236d1fb87442c7d54c6596" 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="Merging SimPleAC to master pt. 3 " href="https://github.com/convexengineering/gplibrary/pull/120">PR 120</a>: Merging SimPleAC to master pt. 3 [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\jenkins790719041570138232.bat C:\Users\jenkins\workspace\gpkit_commons_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\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>REM turn on the anaconda console C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>call activate.bat || exit /b 666 (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Create a virtualenv to install everything into (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>SET VENV=C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>virtualenv --system-site-packages C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit New python executable in C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts\python.exe Installing setuptools, pip, wheel...done. (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>call C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts\activate.bat (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_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\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>pip install coverage Collecting coverage Using cached coverage-4.4.1-cp27-cp27m-win_amd64.whl Installing collected packages: coverage Successfully installed coverage-4.4.1 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>if mosek == mosek msktestlic || exit /b 666 Problem Name : Objective sense : min Type : LO (linear optimization problem) Constraints : 1 Cones : 0 Scalar variables : 5000 Matrix variables : 0 Integer variables : 0 Optimizer started. Mosek license manager: License path: C:\Users\jenkins\mosek\mosek.lic Mosek license manager: Checkout license feature 'PTS' from flexlm. Mosek license manager: Checkout time 0.03. r: 0 status: 0 Interior-point optimizer started. Presolve started. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 1 time : 0.00 Lin. dep. - tries : 0 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.03 ************************************ A license was checked out correctly. ************************************ (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>SET GPKITBUILD=C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\build_gpkit (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_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\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>if mosek == cvxopt set GPKITSOLVERS=cvxopt (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>if mosek == mosek set GPKITSOLVERS=mosek, mosek_cli (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>dir C:\Users\jenkins\workspace\gpkit_commons_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\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek File Not Found (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "import scipy; print scipy.__version__" 0.18.1 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "import numpy; print numpy.__version__" 1.11.3 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "import pint; print pint.__version__" 0.7.2 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Install gpkit to run the documentation examples (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_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\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>pip install -e C:\Users\jenkins\workspace\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>pip install -e C:\Users\jenkins\workspace\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_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\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Show the settings file (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>type C:\Users\jenkins\workspace\gpkit_commons_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\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True)" Cloning into 'gpkit-models'... Cloning into 'shopping'... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 5.56 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.03 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.072 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 6.523s OK Generating XML reports... Cloning into 'jho'... From https://github.com/convexengineering/gpkit-models * branch master -> FETCH_HEAD Note: checking out 'FETCH_HEAD'. You are in 'detached HEAD' state. You can look around, make experimental changes and commit them, and you can discard any commits you make in this state without impacting any branches by performing another checkout. If you want to create a new branch to retain commits you create, you may do so (now or later) by using -b with the checkout command again. Example: git checkout -b <new-branch-name> HEAD is now at 662ac9f... add readme with build status Cannot uninstall requirement gpkit-models, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/gpkit-models 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 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:\anaconda2\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-xpxfdx-build Requirement already satisfied: numpy in c:\anaconda2\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\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint 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 adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -2.07997156824e-11. Allowing negative dual variable(s) as small as -1.60152793804e-12. Allowing negative dual variable(s) as small as -1.69474764083e-12. Allowing negative dual variable(s) as small as -2.24482286058e-11. Solving took 4 GP solves and 1.32 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -2.0958317113e-11. Allowing negative dual variable(s) as small as -1.44199669566e-12. Allowing negative dual variable(s) as small as -1.63676537601e-12. Allowing negative dual variable(s) as small as -1.62887498628e-12. Solving took 4 GP solves and 1.24 seconds. Allowing negative dual variable(s) as small as -7.74424274708e-12. Allowing negative dual variable(s) as small as -3.41600706055e-11. Allowing negative dual variable(s) as small as -2.08748643371e-11. Allowing negative dual variable(s) as small as -2.112797437e-11. Allowing negative dual variable(s) as small as -2.13846509944e-11. Allowing negative dual variable(s) as small as -4.88693157122e-12. Allowing negative dual variable(s) as small as -1.04705577975e-11. Allowing negative dual variable(s) as small as -5.89819599411e-12. Allowing negative dual variable(s) as small as -1.10752449963e-11. MTOW [lbs] = 141.59 Zero fuel weight [lbs] = 53.63 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.75761705137e-12. Allowing negative dual variable(s) as small as -7.11270950991e-12. Allowing negative dual variable(s) as small as -1.34973838746e-11. Allowing negative dual variable(s) as small as -1.37366241429e-11. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.42441630667e-11. Allowing negative dual variable(s) as small as -3.57327052526e-11. Allowing negative dual variable(s) as small as -3.97165477056e-13. Allowing negative dual variable(s) as small as -5.6708001202e-11. Solving took 4 GP solves and 1.95 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.01989639492e-13. Allowing negative dual variable(s) as small as -1.8056133845e-11. Allowing negative dual variable(s) as small as -7.28747353261e-11. Allowing negative dual variable(s) as small as -1.43036637222e-11. Solving took 4 GP solves and 1.74 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -7.73682506949e-12. Allowing negative dual variable(s) as small as -3.41888878319e-11. Allowing negative dual variable(s) as small as -2.08928152556e-11. Allowing negative dual variable(s) as small as -2.11521286597e-11. Allowing negative dual variable(s) as small as -2.14118306419e-11. Allowing negative dual variable(s) as small as -4.89125211688e-12. Allowing negative dual variable(s) as small as -1.04706990691e-11. Allowing negative dual variable(s) as small as -5.89447999959e-12. Allowing negative dual variable(s) as small as -1.10742932836e-11. MTOW [lbs] = 141.59 Zero fuel weight [lbs] = 53.63 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.78553135419e-12. Allowing negative dual variable(s) as small as -7.11447383211e-12. Allowing negative dual variable(s) as small as -1.34976065698e-11. Allowing negative dual variable(s) as small as -1.37369743402e-11. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.42467928677e-11. Allowing negative dual variable(s) as small as -3.57339089807e-11. Allowing negative dual variable(s) as small as -3.98204636769e-13. Allowing negative dual variable(s) as small as -5.67072790622e-11. Solving took 4 GP solves and 1.96 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.07465294144e-13. Allowing negative dual variable(s) as small as -1.80554221747e-11. Allowing negative dual variable(s) as small as -7.28732968067e-11. Allowing negative dual variable(s) as small as -1.42998707493e-11. Solving took 4 GP solves and 2.54 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 106.925s OK Generating XML reports... Cloning into 'turbofan'... Cannot uninstall requirement turbofan, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/turbofan Installing collected packages: turbofan Running setup.py develop for turbofan Successfully installed turbofan From https://github.com/convexengineering/gpkit-models * branch master -> FETCH_HEAD HEAD is now at 662ac9f... add readme with build status Cannot uninstall requirement gpkit-models, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/gpkit-models 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 adding test for 'turbofan/engine_validation.py' adding test for 'turbofan/engine_flight_profile_fleet.py' T_{t_{4.1_{max}}}_FleetMission/Aircraft/Engine has no upper bound Beginning signomial solve. Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 746 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 7 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.02 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 2 Optimizer - solved problem : the primal Optimizer - Constraints : 366 Optimizer - Cones : 0 Optimizer - Scalar variables : 1075 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.01 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 5857 after factor : 1.07e+004 Factor - dense dim. : 0 flops : 1.01e+005 Factor - GP saved nzs : 1.05e+004 GP saved flops : 1.12e+005 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.2e+003 4.3e+003 2.0e+004 0.00e+000 -2.004159770e+004 1.023181539e-012 1.0e+000 0.03 1 8.0e+002 2.8e+003 1.3e+004 -9.19e-002 -1.644778994e+004 3.599090741e+000 6.6e-001 0.03 2 4.4e+002 1.5e+003 7.2e+003 7.81e-002 -1.282480446e+004 7.951285033e+000 3.7e-001 0.03 3 2.2e+002 7.9e+002 3.7e+003 4.64e-001 -6.928443334e+003 1.273155424e+001 1.9e-001 0.03 4 8.8e+001 3.1e+002 1.4e+003 1.09e+000 -2.505365849e+003 1.564423771e+001 8.1e-002 0.05 5 4.8e+001 1.7e+002 8.0e+002 1.61e+000 -1.120898167e+003 1.604580993e+001 4.5e-002 0.05 6 3.1e+001 1.1e+002 5.2e+002 1.58e+000 -6.245323152e+002 1.590158365e+001 3.0e-002 0.05 7 1.8e+001 6.1e+001 2.9e+002 1.43e+000 -3.009850958e+002 1.563100638e+001 1.7e-002 0.05 8 5.7e+000 1.6e+001 9.4e+001 1.30e+000 -7.742059796e+001 1.507588726e+001 5.6e-003 0.05 9 2.5e+000 8.1e+000 4.2e+001 9.35e-001 -3.190851607e+001 1.446074473e+001 2.7e-003 0.05 10 1.8e+000 1.2e+001 2.9e+001 5.30e-001 -2.568066342e+001 1.419467053e+001 1.9e-003 0.05 11 4.7e-001 4.5e+000 8.0e+000 5.33e-001 -9.790481936e-001 1.342837965e+001 6.2e-004 0.06 12 2.0e-001 5.8e+000 3.4e+000 5.08e-001 5.514857126e+000 1.305073779e+001 2.8e-004 0.06 13 1.2e-001 3.6e+000 2.1e+000 7.05e-001 7.947354057e+000 1.288349579e+001 1.8e-004 0.06 14 6.0e-002 2.5e+000 1.0e+000 7.78e-001 1.015098672e+001 1.271873581e+001 9.1e-005 0.06 15 1.9e-002 1.8e+000 3.2e-001 8.75e-001 1.174860944e+001 1.258137131e+001 3.1e-005 0.06 16 6.8e-003 1.3e+000 1.2e-001 9.77e-001 1.223381009e+001 1.253865821e+001 1.2e-005 0.06 17 2.3e-003 1.3e+000 4.0e-002 1.01e+000 1.241854407e+001 1.252155679e+001 4.2e-006 0.08 18 7.1e-004 1.2e+000 1.3e-002 9.98e-001 1.248380839e+001 1.251587414e+001 1.3e-006 0.08 19 6.4e-004 1.1e+000 1.1e-002 9.92e-001 1.248676084e+001 1.251569617e+001 1.2e-006 0.08 20 5.7e-004 1.0e+000 1.0e-002 9.94e-001 1.248942742e+001 1.251548155e+001 1.1e-006 0.08 21 5.2e-004 9.3e-001 9.1e-003 9.94e-001 1.249182213e+001 1.251527753e+001 9.7e-007 0.08 22 4.7e-004 8.4e-001 8.2e-003 9.95e-001 1.249398158e+001 1.251509668e+001 8.8e-007 0.08 23 4.2e-004 7.7e-001 7.4e-003 9.95e-001 1.249592721e+001 1.251493529e+001 7.9e-007 0.09 24 3.8e-004 7.0e-001 6.7e-003 9.95e-001 1.249767989e+001 1.251479096e+001 7.1e-007 0.09 25 3.4e-004 6.4e-001 6.0e-003 9.96e-001 1.249925875e+001 1.251466193e+001 6.4e-007 0.09 26 3.1e-004 5.9e-001 5.4e-003 9.96e-001 1.250068096e+001 1.251454656e+001 5.8e-007 0.09 27 2.7e-004 5.4e-001 4.8e-003 9.96e-001 1.250196202e+001 1.251444336e+001 5.2e-007 0.09 28 2.5e-004 4.9e-001 4.4e-003 9.96e-001 1.250311589e+001 1.251435104e+001 4.7e-007 0.09 29 2.2e-004 4.5e-001 3.9e-003 9.97e-001 1.250415514e+001 1.251426841e+001 4.2e-007 0.11 30 2.0e-004 4.2e-001 3.5e-003 9.97e-001 1.250509111e+001 1.251419443e+001 3.8e-007 0.11 31 1.8e-004 3.8e-001 3.2e-003 9.97e-001 1.250593404e+001 1.251412817e+001 3.4e-007 0.11 32 1.6e-004 3.6e-001 2.9e-003 9.97e-001 1.250669313e+001 1.251406880e+001 3.1e-007 0.11 33 1.5e-004 3.3e-001 2.6e-003 9.98e-001 1.250737669e+001 1.251401559e+001 2.8e-007 0.11 34 1.3e-004 3.1e-001 2.3e-003 9.98e-001 1.250799220e+001 1.251396788e+001 2.5e-007 0.11 35 1.2e-004 2.8e-001 2.1e-003 9.98e-001 1.250854643e+001 1.251392510e+001 2.2e-007 0.11 36 1.1e-004 2.7e-001 1.9e-003 9.98e-001 1.250904544e+001 1.251388671e+001 2.0e-007 0.13 37 9.6e-005 2.5e-001 1.7e-003 9.98e-001 1.250949474e+001 1.251385226e+001 1.8e-007 0.13 38 8.6e-005 2.3e-001 1.5e-003 9.98e-001 1.250989925e+001 1.251382133e+001 1.6e-007 0.13 39 7.8e-005 2.2e-001 1.4e-003 9.99e-001 1.251026343e+001 1.251379357e+001 1.5e-007 0.13 40 7.0e-005 2.1e-001 1.2e-003 9.99e-001 1.251059130e+001 1.251376863e+001 1.3e-007 0.13 41 6.3e-005 1.9e-001 1.1e-003 9.99e-001 1.251088646e+001 1.251374624e+001 1.2e-007 0.13 42 5.7e-005 1.8e-001 1.0e-003 9.99e-001 1.251115217e+001 1.251372612e+001 1.1e-007 0.13 43 5.1e-005 1.8e-001 9.0e-004 9.99e-001 1.251139136e+001 1.251370804e+001 9.6e-008 0.13 44 4.6e-005 1.7e-001 8.1e-004 9.99e-001 1.251160668e+001 1.251369180e+001 8.6e-008 0.14 45 4.1e-005 1.6e-001 7.3e-004 9.99e-001 1.251180051e+001 1.251367719e+001 7.8e-008 0.14 46 3.7e-005 1.5e-001 6.6e-004 9.99e-001 1.251197499e+001 1.251366407e+001 7.0e-008 0.14 47 3.3e-005 1.5e-001 5.9e-004 9.99e-001 1.251213204e+001 1.251365227e+001 6.3e-008 0.14 48 3.0e-005 1.4e-001 5.3e-004 9.99e-001 1.251227340e+001 1.251364166e+001 5.7e-008 0.14 49 2.7e-005 1.4e-001 4.8e-004 9.99e-001 1.251240065e+001 1.251363212e+001 5.1e-008 0.14 50 2.4e-005 1.3e-001 4.3e-004 9.99e-001 1.251251518e+001 1.251362354e+001 4.6e-008 0.14 51 2.2e-005 1.3e-001 3.9e-004 9.99e-001 1.251261828e+001 1.251361583e+001 4.1e-008 0.16 52 2.0e-005 1.3e-001 3.5e-004 1.00e+000 1.251271107e+001 1.251360889e+001 3.7e-008 0.16 53 1.8e-005 1.2e-001 3.1e-004 1.00e+000 1.251279459e+001 1.251360264e+001 3.3e-008 0.16 54 1.6e-005 1.2e-001 2.8e-004 1.00e+000 1.251286977e+001 1.251359703e+001 3.0e-008 0.16 55 1.4e-005 1.2e-001 2.5e-004 1.00e+000 1.251293743e+001 1.251359198e+001 2.7e-008 0.16 56 1.3e-005 1.2e-001 2.3e-004 1.00e+000 1.251299833e+001 1.251358743e+001 2.4e-008 0.16 57 1.2e-005 1.1e-001 2.1e-004 1.00e+000 1.251305315e+001 1.251358334e+001 2.2e-008 0.16 58 1.0e-005 1.1e-001 1.9e-004 1.00e+000 1.251310248e+001 1.251357966e+001 2.0e-008 0.16 59 9.4e-006 1.1e-001 1.7e-004 1.00e+000 1.251314689e+001 1.251357635e+001 1.8e-008 0.17 60 8.5e-006 1.1e-001 1.5e-004 1.00e+000 1.251318685e+001 1.251357337e+001 1.6e-008 0.17 61 7.6e-006 1.1e-001 1.3e-004 1.00e+000 1.251322282e+001 1.251357069e+001 1.4e-008 0.17 62 6.9e-006 1.1e-001 1.2e-004 1.00e+000 1.251325519e+001 1.251356828e+001 1.3e-008 0.17 63 6.2e-006 1.0e-001 1.1e-004 1.00e+000 1.251328433e+001 1.251356611e+001 1.2e-008 0.17 64 5.6e-006 1.0e-001 9.8e-005 1.00e+000 1.251331055e+001 1.251356416e+001 1.1e-008 0.19 65 5.0e-006 1.0e-001 8.9e-005 1.00e+000 1.251333416e+001 1.251356240e+001 9.5e-009 0.19 66 4.5e-006 1.0e-001 8.0e-005 1.00e+000 1.251335540e+001 1.251356081e+001 8.5e-009 0.19 67 4.1e-006 1.0e-001 7.2e-005 1.00e+000 1.251337452e+001 1.251355939e+001 7.7e-009 0.19 68 3.7e-006 1.0e-001 6.5e-005 1.00e+000 1.251339172e+001 1.251355811e+001 6.9e-009 0.19 69 3.3e-006 1.0e-001 5.8e-005 1.00e+000 1.251340721e+001 1.251355696e+001 6.2e-009 0.19 70 3.0e-006 1.0e-001 5.2e-005 1.00e+000 1.251342114e+001 1.251355592e+001 5.6e-009 0.20 71 2.7e-006 9.9e-002 4.7e-005 1.00e+000 1.251343368e+001 1.251355498e+001 5.0e-009 0.20 72 2.4e-006 9.9e-002 4.2e-005 1.00e+000 1.251344498e+001 1.251355414e+001 4.5e-009 0.20 73 2.2e-006 9.8e-002 3.8e-005 1.00e+000 1.251345513e+001 1.251355339e+001 4.1e-009 0.20 74 1.9e-006 9.8e-002 3.4e-005 1.00e+000 1.251346428e+001 1.251355271e+001 3.7e-009 0.20 75 1.7e-006 9.8e-002 3.1e-005 1.00e+000 1.251347251e+001 1.251355209e+001 3.3e-009 0.20 76 1.6e-006 9.7e-002 2.8e-005 1.00e+000 1.251347992e+001 1.251355154e+001 3.0e-009 0.22 77 1.4e-006 9.7e-002 2.5e-005 1.00e+000 1.251348658e+001 1.251355104e+001 2.7e-009 0.22 78 1.3e-006 9.7e-002 2.2e-005 1.00e+000 1.251349258e+001 1.251355060e+001 2.4e-009 0.22 79 1.1e-006 9.7e-002 2.0e-005 1.00e+000 1.251349798e+001 1.251355019e+001 2.2e-009 0.22 80 1.0e-006 9.7e-002 1.8e-005 1.00e+000 1.251350284e+001 1.251354983e+001 1.9e-009 0.22 81 9.3e-007 9.6e-002 1.6e-005 9.99e-001 1.251350721e+001 1.251354951e+001 1.8e-009 0.22 82 8.4e-007 9.6e-002 1.5e-005 1.00e+000 1.251351115e+001 1.251354921e+001 1.6e-009 0.23 83 7.5e-007 9.6e-002 1.3e-005 1.00e+000 1.251351471e+001 1.251354895e+001 1.4e-009 0.23 84 7.7e-008 9.8e-003 1.4e-006 9.99e-001 1.251354331e+001 1.251354682e+001 1.5e-010 0.23 85 4.2e-009 5.4e-004 7.5e-008 9.99e-001 1.251354639e+001 1.251354658e+001 8.3e-012 0.23 86 2.8e-010 3.6e-005 5.0e-009 1.02e+000 1.251354656e+001 1.251354657e+001 4.9e-013 0.23 Interior-point optimizer terminated. Time: 0.23. Optimizer terminated. Time: 0.25 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.2513546558e+001 nrm: 1e+001 Viol. con: 2e-010 var: 0e+000 Dual. obj: 1.2513546570e+001 nrm: 9e+001 Viol. con: 0e+000 var: 2e-005 * End solution on dual form. * Transforming to primal solution. Solving took 0.29 seconds. result packing took 68% of solve time solution checking took 26% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 771 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 3 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.02 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 2 Optimizer - solved problem : the primal Optimizer - Constraints : 345 Optimizer - Cones : 0 Optimizer - Scalar variables : 1054 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 5894 after factor : 1.09e+004 Factor - dense dim. : 0 flops : 1.08e+005 Factor - GP saved nzs : 1.06e+004 GP saved flops : 1.18e+005 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.2e+003 4.0e+003 2.3e+004 0.00e+000 -2.313089885e+004 1.023181539e-012 1.0e+000 0.05 1 6.5e+002 2.1e+003 1.2e+004 2.59e-002 -1.531524442e+004 6.000661052e+000 5.4e-001 0.05 2 4.2e+002 1.4e+003 8.0e+003 7.75e-001 -9.393417668e+003 9.614365598e+000 3.6e-001 0.06 3 1.1e+002 3.7e+002 2.2e+003 1.10e+000 -2.279498448e+003 1.395778984e+001 1.1e-001 0.06 4 4.9e+001 1.6e+002 9.3e+002 1.74e+000 -7.571301446e+002 1.377098733e+001 4.7e-002 0.06 5 1.3e+001 4.4e+001 2.5e+002 1.40e+000 -1.651972951e+002 1.254361037e+001 1.3e-002 0.06 6 3.7e+000 1.4e+001 7.1e+001 1.13e+000 -3.756113508e+001 1.118113217e+001 4.3e-003 0.06 7 9.8e-001 9.3e+000 1.9e+001 1.04e+000 -2.048781949e+000 1.065205256e+001 1.3e-003 0.06 8 9.0e-001 1.1e+001 1.7e+001 7.91e-001 -1.456094642e+000 1.063799971e+001 1.2e-003 0.08 9 4.0e-001 1.1e+001 7.7e+000 7.32e-001 3.780601755e+000 1.050672836e+001 5.5e-004 0.08 10 3.2e-001 8.9e+000 6.2e+000 3.11e-001 4.368799746e+000 1.047713321e+001 4.5e-004 0.08 11 1.1e-001 3.2e+000 2.1e+000 4.12e-001 7.529581040e+000 1.033494919e+001 1.8e-004 0.08 12 2.4e-002 3.7e+000 4.8e-001 7.14e-001 9.493551613e+000 1.024454347e+001 5.0e-005 0.09 13 6.8e-003 3.5e+000 1.4e-001 9.11e-001 9.997494319e+000 1.021637518e+001 1.5e-005 0.09 14 2.1e-003 3.1e+000 4.3e-002 9.74e-001 1.013845333e+001 1.020775130e+001 5.0e-006 0.09 15 6.6e-004 3.0e+000 1.3e-002 9.92e-001 1.018326966e+001 1.020498358e+001 1.6e-006 0.09 16 2.1e-004 2.9e+000 4.1e-003 9.98e-001 1.019734873e+001 1.020409885e+001 5.0e-007 0.09 17 8.0e-005 2.6e+000 1.6e-003 9.99e-001 1.020123890e+001 1.020386508e+001 1.9e-007 0.09 18 7.2e-005 2.4e+000 1.4e-003 1.00e+000 1.020147936e+001 1.020384731e+001 1.7e-007 0.11 19 6.5e-005 2.2e+000 1.3e-003 1.00e+000 1.020170127e+001 1.020383281e+001 1.6e-007 0.11 20 5.8e-005 2.0e+000 1.2e-003 1.00e+000 1.020190171e+001 1.020382014e+001 1.4e-007 0.11 21 5.2e-005 1.8e+000 1.1e-003 1.00e+000 1.020208218e+001 1.020380878e+001 1.3e-007 0.11 22 4.7e-005 1.6e+000 9.5e-004 1.00e+000 1.020224464e+001 1.020379859e+001 1.1e-007 0.11 23 4.2e-005 1.5e+000 8.5e-004 1.00e+000 1.020239089e+001 1.020378945e+001 1.0e-007 0.11 24 3.8e-005 1.4e+000 7.7e-004 1.00e+000 1.020252253e+001 1.020378125e+001 9.3e-008 0.13 25 3.4e-005 1.2e+000 6.9e-004 1.00e+000 1.020264103e+001 1.020377388e+001 8.4e-008 0.13 26 3.1e-005 1.1e+000 6.2e-004 1.00e+000 1.020274770e+001 1.020376727e+001 7.5e-008 0.13 27 2.8e-005 1.0e+000 5.6e-004 1.00e+000 1.020284371e+001 1.020376133e+001 6.8e-008 0.13 28 2.5e-005 9.5e-001 5.0e-004 1.00e+000 1.020293013e+001 1.020375600e+001 6.1e-008 0.13 29 2.3e-005 8.7e-001 4.5e-004 1.00e+000 1.020300792e+001 1.020375121e+001 5.5e-008 0.13 30 2.0e-005 8.0e-001 4.1e-004 1.00e+000 1.020307794e+001 1.020374690e+001 4.9e-008 0.14 31 1.8e-005 7.4e-001 3.7e-004 1.00e+000 1.020314097e+001 1.020374303e+001 4.4e-008 0.14 32 1.6e-005 6.8e-001 3.3e-004 1.00e+000 1.020319770e+001 1.020373956e+001 4.0e-008 0.14 33 1.5e-005 6.3e-001 3.0e-004 1.00e+000 1.020324876e+001 1.020373644e+001 3.6e-008 0.14 34 1.3e-005 5.8e-001 2.7e-004 1.00e+000 1.020329472e+001 1.020373363e+001 3.2e-008 0.14 35 1.2e-005 5.4e-001 2.4e-004 1.00e+000 1.020333609e+001 1.020373111e+001 2.9e-008 0.14 36 1.1e-005 5.1e-001 2.2e-004 1.00e+000 1.020337332e+001 1.020372884e+001 2.6e-008 0.14 37 9.7e-006 4.7e-001 2.0e-004 1.00e+000 1.020340683e+001 1.020372681e+001 2.4e-008 0.16 38 8.7e-006 4.4e-001 1.8e-004 1.00e+000 1.020343700e+001 1.020372497e+001 2.1e-008 0.16 39 7.9e-006 4.2e-001 1.6e-004 1.00e+000 1.020346415e+001 1.020372333e+001 1.9e-008 0.16 40 7.1e-006 3.9e-001 1.4e-004 1.00e+000 1.020348859e+001 1.020372185e+001 1.7e-008 0.16 41 6.4e-006 3.7e-001 1.3e-004 1.00e+000 1.020351058e+001 1.020372052e+001 1.5e-008 0.16 42 5.7e-006 3.5e-001 1.2e-004 1.00e+000 1.020353038e+001 1.020371932e+001 1.4e-008 0.16 43 5.2e-006 3.3e-001 1.0e-004 1.00e+000 1.020354820e+001 1.020371824e+001 1.3e-008 0.16 44 5.5e-007 3.6e-002 1.1e-005 1.00e+000 1.020369151e+001 1.020370964e+001 1.3e-009 0.17 45 3.0e-008 2.0e-003 6.1e-007 1.00e+000 1.020370765e+001 1.020370866e+001 7.6e-011 0.17 46 2.6e-010 1.1e-005 3.5e-009 9.99e-001 1.020370860e+001 1.020370860e+001 6.4e-013 0.17 Interior-point optimizer terminated. Time: 0.17. Optimizer terminated. Time: 0.19 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0203708596e+001 nrm: 8e+000 Viol. con: 2e-010 var: 0e+000 Dual. obj: 1.0203708602e+001 nrm: 5e+001 Viol. con: 0e+000 var: 4e-006 * End solution on dual form. * Transforming to primal solution. Solving took 0.217 seconds. result packing took 64% of solve time solution checking took 24% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 771 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 3 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.02 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 2 Optimizer - solved problem : the primal Optimizer - Constraints : 345 Optimizer - Cones : 0 Optimizer - Scalar variables : 1054 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.01 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 5894 after factor : 1.09e+004 Factor - dense dim. : 0 flops : 1.08e+005 Factor - GP saved nzs : 1.06e+004 GP saved flops : 1.18e+005 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.9e+003 4.0e+003 2.3e+004 0.00e+000 -2.318780673e+004 1.023181539e-012 1.0e+000 0.03 1 9.3e+002 2.0e+003 1.1e+004 -3.82e-002 -1.483657985e+004 6.469408367e+000 5.0e-001 0.03 2 7.6e+002 1.6e+003 9.2e+003 8.17e-001 -1.141808522e+004 8.509785565e+000 4.1e-001 0.03 3 4.0e+002 8.6e+002 4.9e+003 1.00e+000 -5.789693727e+003 1.205240773e+001 2.2e-001 0.03 4 1.2e+002 2.5e+002 1.4e+003 1.51e+000 -1.284860586e+003 1.412957537e+001 7.1e-002 0.05 5 3.7e+001 7.8e+001 4.5e+002 1.59e+000 -3.103551445e+002 1.328306779e+001 2.3e-002 0.05 6 1.1e+001 2.6e+001 1.4e+002 1.17e+000 -8.241026576e+001 1.173817747e+001 7.8e-003 0.05 7 2.7e+000 9.7e+000 3.3e+001 1.05e+000 -1.111925119e+001 1.080625548e+001 2.1e-003 0.05 8 1.4e+000 1.3e+001 1.8e+001 9.25e-001 -1.883018131e+000 1.065948056e+001 1.2e-003 0.05 9 1.3e+000 1.4e+001 1.6e+001 6.48e-001 -1.331317323e+000 1.064014764e+001 1.1e-003 0.05 10 5.2e-001 8.3e+000 6.5e+000 5.96e-001 3.816869391e+000 1.047811828e+001 4.8e-004 0.06 11 3.1e-001 9.6e+000 3.9e+000 5.19e-001 5.727934158e+000 1.040073444e+001 3.0e-004 0.06 12 9.5e-002 4.5e+000 1.2e+000 5.35e-001 8.508151142e+000 1.028245289e+001 1.1e-004 0.06 13 1.8e-002 4.3e+000 2.3e-001 8.08e-001 9.838171166e+000 1.021326599e+001 2.6e-005 0.06 14 4.4e-003 3.9e+000 5.7e-002 9.65e-001 1.010294749e+001 1.019682039e+001 7.1e-006 0.06 15 1.4e-003 3.2e+000 1.9e-002 9.94e-001 1.016254678e+001 1.019304437e+001 2.4e-006 0.06 16 4.4e-004 2.8e+000 5.7e-003 9.98e-001 1.018235914e+001 1.019171837e+001 7.3e-007 0.06 17 1.5e-004 2.4e+000 2.0e-003 9.99e-001 1.018811978e+001 1.019134320e+001 2.5e-007 0.08 18 5.0e-005 2.3e+000 6.6e-004 1.00e+000 1.019013131e+001 1.019121454e+001 8.5e-008 0.08 19 1.7e-005 2.2e+000 2.3e-004 1.00e+000 1.019080234e+001 1.019117362e+001 2.9e-008 0.08 20 1.6e-005 2.0e+000 2.0e-004 1.00e+000 1.019083626e+001 1.019117114e+001 2.6e-008 0.08 21 1.4e-005 1.8e+000 1.8e-004 1.00e+000 1.019086771e+001 1.019116916e+001 2.4e-008 0.08 22 1.3e-005 1.7e+000 1.6e-004 1.00e+000 1.019089609e+001 1.019116740e+001 2.1e-008 0.08 23 1.1e-005 1.5e+000 1.5e-004 1.00e+000 1.019092164e+001 1.019116581e+001 1.9e-008 0.09 24 1.0e-005 1.4e+000 1.3e-004 1.00e+000 1.019094464e+001 1.019116439e+001 1.7e-008 0.09 25 9.2e-006 1.3e+000 1.2e-004 1.00e+000 1.019096534e+001 1.019116312e+001 1.6e-008 0.09 26 8.2e-006 1.1e+000 1.1e-004 1.00e+000 1.019098397e+001 1.019116197e+001 1.4e-008 0.09 27 7.4e-006 1.0e+000 9.7e-005 1.00e+000 1.019100074e+001 1.019116094e+001 1.3e-008 0.09 28 6.7e-006 9.6e-001 8.7e-005 1.00e+000 1.019101583e+001 1.019116001e+001 1.1e-008 0.09 29 6.0e-006 8.8e-001 7.9e-005 1.00e+000 1.019102942e+001 1.019115918e+001 1.0e-008 0.11 30 5.4e-006 8.1e-001 7.1e-005 1.00e+000 1.019104165e+001 1.019115843e+001 9.2e-009 0.11 31 4.9e-006 7.4e-001 6.4e-005 1.00e+000 1.019105265e+001 1.019115775e+001 8.3e-009 0.11 32 4.4e-006 6.9e-001 5.7e-005 1.00e+000 1.019106256e+001 1.019115715e+001 7.5e-009 0.11 33 3.9e-006 6.3e-001 5.2e-005 1.00e+000 1.019107147e+001 1.019115661e+001 6.7e-009 0.11 34 3.5e-006 5.9e-001 4.6e-005 1.00e+000 1.019107950e+001 1.019115612e+001 6.0e-009 0.11 35 3.2e-006 5.5e-001 4.2e-005 9.99e-001 1.019108672e+001 1.019115568e+001 5.4e-009 0.11 36 2.9e-006 5.1e-001 3.8e-005 9.99e-001 1.019109322e+001 1.019115528e+001 4.9e-009 0.13 37 2.6e-006 4.7e-001 3.4e-005 1.00e+000 1.019109907e+001 1.019115493e+001 4.4e-009 0.13 38 2.3e-006 4.4e-001 3.0e-005 1.00e+000 1.019110434e+001 1.019115461e+001 4.0e-009 0.13 39 2.1e-006 4.2e-001 2.7e-005 9.99e-001 1.019110908e+001 1.019115432e+001 3.6e-009 0.13 40 1.9e-006 3.9e-001 2.5e-005 1.00e+000 1.019111334e+001 1.019115406e+001 3.2e-009 0.13 41 1.7e-006 3.7e-001 2.2e-005 9.99e-001 1.019111718e+001 1.019115383e+001 2.9e-009 0.13 42 1.5e-006 3.5e-001 2.0e-005 9.97e-001 1.019112063e+001 1.019115362e+001 2.6e-009 0.14 43 1.4e-006 3.3e-001 1.8e-005 1.00e+000 1.019112374e+001 1.019115343e+001 2.3e-009 0.14 44 1.2e-006 3.1e-001 1.6e-005 1.00e+000 1.019112654e+001 1.019115326e+001 2.1e-009 0.14 45 1.1e-006 3.0e-001 1.5e-005 1.00e+000 1.019112905e+001 1.019115311e+001 1.9e-009 0.14 46 1.0e-006 2.9e-001 1.3e-005 1.00e+000 1.019113132e+001 1.019115297e+001 1.7e-009 0.14 47 9.0e-007 2.7e-001 1.2e-005 1.00e+000 1.019113334e+001 1.019115285e+001 1.5e-009 0.14 48 8.1e-007 2.6e-001 1.1e-005 9.98e-001 1.019113518e+001 1.019115274e+001 1.4e-009 0.14 49 7.3e-007 2.5e-001 9.6e-006 1.00e+000 1.019113683e+001 1.019115264e+001 1.2e-009 0.16 50 6.6e-007 2.4e-001 8.6e-006 9.92e-001 1.019113832e+001 1.019115255e+001 1.1e-009 0.16 51 5.9e-007 2.4e-001 7.7e-006 1.00e+000 1.019113967e+001 1.019115247e+001 1.0e-009 0.16 52 5.3e-007 2.3e-001 7.0e-006 9.91e-001 1.019114087e+001 1.019115240e+001 9.1e-010 0.16 53 4.8e-007 2.2e-001 6.3e-006 9.98e-001 1.019114195e+001 1.019115233e+001 8.2e-010 0.16 54 4.3e-007 2.2e-001 5.6e-006 9.95e-001 1.019114293e+001 1.019115227e+001 7.4e-010 0.16 55 3.9e-007 2.1e-001 5.1e-006 9.89e-001 1.019114381e+001 1.019115222e+001 6.6e-010 0.16 56 3.5e-007 2.1e-001 4.6e-006 1.00e+000 1.019114460e+001 1.019115217e+001 6.0e-010 0.16 57 3.1e-007 2.0e-001 4.1e-006 9.96e-001 1.019114532e+001 1.019115213e+001 5.4e-010 0.17 58 2.8e-007 2.0e-001 3.7e-006 1.01e+000 1.019114597e+001 1.019115209e+001 4.8e-010 0.17 59 2.5e-007 2.0e-001 3.3e-006 1.01e+000 1.019114657e+001 1.019115205e+001 4.4e-010 0.17 60 2.3e-007 2.0e-001 3.0e-006 9.88e-001 1.019114709e+001 1.019115202e+001 3.9e-010 0.17 61 2.1e-007 1.9e-001 2.7e-006 9.83e-001 1.019114755e+001 1.019115200e+001 3.5e-010 0.17 62 1.9e-007 1.7e-001 2.4e-006 1.01e+000 1.019114799e+001 1.019115197e+001 3.2e-010 0.17 63 1.7e-007 1.7e-001 2.2e-006 9.89e-001 1.019114836e+001 1.019115195e+001 2.9e-010 0.17 64 1.5e-007 1.5e-001 2.0e-006 1.03e+000 1.019114874e+001 1.019115192e+001 2.6e-010 0.19 65 1.4e-007 1.4e-001 1.8e-006 9.90e-001 1.019114904e+001 1.019115190e+001 2.4e-010 0.19 66 1.2e-007 1.3e-001 1.6e-006 1.03e+000 1.019114934e+001 1.019115189e+001 2.2e-010 0.19 67 1.1e-007 1.1e-001 1.4e-006 9.98e-001 1.019114958e+001 1.019115187e+001 1.9e-010 0.19 68 9.9e-008 1.0e-001 1.3e-006 1.02e+000 1.019114981e+001 1.019115186e+001 1.8e-010 0.19 69 6.7e-009 6.3e-003 8.1e-008 9.30e-001 1.019115162e+001 1.019115176e+001 1.7e-011 0.19 70 6.1e-009 5.8e-003 7.4e-008 9.50e-001 1.019115163e+001 1.019115176e+001 1.5e-011 0.19 71 1.3e-009 1.0e-003 1.3e-008 1.08e+000 1.019115172e+001 1.019115174e+001 1.2e-012 0.20 72 1.5e-010 6.5e-006 8.4e-011 9.91e-001 1.019115174e+001 1.019115174e+001 1.9e-014 0.20 Interior-point optimizer terminated. Time: 0.20. Optimizer terminated. Time: 0.22 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0191151741e+001 nrm: 9e+000 Viol. con: 1e-010 var: 0e+000 Dual. obj: 1.0191151741e+001 nrm: 6e+001 Viol. con: 0e+000 var: 2e-006 * End solution on dual form. * Transforming to primal solution. Solving took 0.253 seconds. result packing took 55% of solve time solution checking took 21% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 771 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 3 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.03 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 2 Optimizer - solved problem : the primal Optimizer - Constraints : 345 Optimizer - Cones : 0 Optimizer - Scalar variables : 1054 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 5894 after factor : 1.09e+004 Factor - dense dim. : 0 flops : 1.08e+005 Factor - GP saved nzs : 1.06e+004 GP saved flops : 1.18e+005 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.9e+003 4.0e+003 2.3e+004 0.00e+000 -2.319472415e+004 1.023181539e-012 1.0e+000 0.05 1 9.6e+002 2.0e+003 1.2e+004 -4.04e-002 -1.526860993e+004 6.135820917e+000 5.2e-001 0.05 2 7.8e+002 1.7e+003 9.5e+003 7.69e-001 -1.183085357e+004 8.225115928e+000 4.2e-001 0.05 3 3.9e+002 8.2e+002 4.7e+003 9.59e-001 -5.587185913e+003 1.220730235e+001 2.2e-001 0.05 4 1.4e+002 3.0e+002 1.7e+003 1.57e+000 -1.517850489e+003 1.397244536e+001 8.2e-002 0.06 5 3.7e+001 8.0e+001 4.6e+002 1.60e+000 -3.085327189e+002 1.331757308e+001 2.3e-002 0.06 6 1.1e+001 2.4e+001 1.3e+002 1.14e+000 -7.794940325e+001 1.165767501e+001 7.5e-003 0.06 7 2.4e+000 1.0e+001 3.0e+001 1.04e+000 -9.314075527e+000 1.074098163e+001 2.0e-003 0.06 8 1.4e+000 1.6e+001 1.7e+001 8.97e-001 -1.324243483e+000 1.061030910e+001 1.1e-003 0.06 9 1.1e+000 1.8e+001 1.4e+001 6.19e-001 -1.810298381e-001 1.057130815e+001 9.2e-004 0.06 10 4.0e-001 9.2e+000 4.9e+000 5.48e-001 5.033978068e+000 1.040348276e+001 3.8e-004 0.08 11 2.3e-001 9.6e+000 2.9e+000 5.64e-001 6.655518362e+000 1.033842349e+001 2.4e-004 0.08 12 5.6e-002 4.4e+000 7.1e-001 6.08e-001 9.154717138e+000 1.022979665e+001 7.1e-005 0.08 13 1.8e-002 3.2e+000 2.4e-001 8.61e-001 9.819003765e+000 1.019154529e+001 2.5e-005 0.08 14 1.1e-002 3.0e+000 1.4e-001 9.60e-001 9.967714356e+000 1.018351959e+001 1.5e-005 0.08 15 2.8e-003 2.9e+000 3.5e-002 9.74e-001 1.011654832e+001 1.017372520e+001 4.1e-006 0.08 16 7.8e-004 2.8e+000 1.0e-002 9.95e-001 1.015489733e+001 1.017122500e+001 1.2e-006 0.08 17 2.8e-004 2.6e+000 3.6e-003 9.99e-001 1.016485127e+001 1.017060321e+001 4.2e-007 0.08 18 1.1e-004 2.1e+000 1.5e-003 1.00e+000 1.016801730e+001 1.017040589e+001 1.7e-007 0.09 19 1.0e-004 2.0e+000 1.3e-003 1.00e+000 1.016824059e+001 1.017039405e+001 1.6e-007 0.09 20 9.3e-005 1.8e+000 1.2e-003 1.00e+000 1.016844242e+001 1.017038082e+001 1.4e-007 0.09 21 8.3e-005 1.7e+000 1.1e-003 1.00e+000 1.016862462e+001 1.017036923e+001 1.3e-007 0.09 22 7.5e-005 1.5e+000 9.7e-004 1.00e+000 1.016878862e+001 1.017035879e+001 1.1e-007 0.09 23 6.8e-005 1.4e+000 8.7e-004 1.00e+000 1.016893625e+001 1.017034942e+001 1.0e-007 0.09 24 6.1e-005 1.3e+000 7.9e-004 1.00e+000 1.016906914e+001 1.017034100e+001 9.3e-008 0.11 25 5.5e-005 1.2e+000 7.1e-004 1.00e+000 1.016918875e+001 1.017033344e+001 8.3e-008 0.11 26 4.9e-005 1.1e+000 6.4e-004 1.00e+000 1.016929642e+001 1.017032666e+001 7.5e-008 0.11 27 4.4e-005 9.7e-001 5.7e-004 1.00e+000 1.016939334e+001 1.017032056e+001 6.8e-008 0.11 28 4.0e-005 8.9e-001 5.2e-004 1.00e+000 1.016948057e+001 1.017031508e+001 6.1e-008 0.11 29 3.6e-005 8.2e-001 4.6e-004 1.00e+000 1.016955909e+001 1.017031016e+001 5.5e-008 0.11 30 3.2e-005 7.6e-001 4.2e-004 1.00e+000 1.016962977e+001 1.017030573e+001 4.9e-008 0.11 31 2.9e-005 7.0e-001 3.8e-004 1.00e+000 1.016969338e+001 1.017030176e+001 4.4e-008 0.11 32 2.6e-005 6.5e-001 3.4e-004 1.00e+000 1.016975064e+001 1.017029818e+001 4.0e-008 0.13 33 2.4e-005 6.0e-001 3.0e-004 1.00e+000 1.016980218e+001 1.017029497e+001 3.6e-008 0.13 34 2.1e-005 5.6e-001 2.7e-004 1.00e+000 1.016984857e+001 1.017029209e+001 3.2e-008 0.13 35 1.9e-005 5.2e-001 2.5e-004 1.00e+000 1.016989032e+001 1.017028949e+001 2.9e-008 0.13 36 1.7e-005 4.8e-001 2.2e-004 1.00e+000 1.016992790e+001 1.017028716e+001 2.6e-008 0.13 37 1.5e-005 4.5e-001 2.0e-004 1.00e+000 1.016996173e+001 1.017028506e+001 2.4e-008 0.13 38 1.4e-005 4.3e-001 1.8e-004 1.00e+000 1.016999217e+001 1.017028317e+001 2.1e-008 0.13 39 1.3e-005 4.0e-001 1.6e-004 1.00e+000 1.017001957e+001 1.017028147e+001 1.9e-008 0.13 40 1.1e-005 3.8e-001 1.5e-004 1.00e+000 1.017004423e+001 1.017027995e+001 1.7e-008 0.13 41 1.0e-005 3.6e-001 1.3e-004 1.00e+000 1.017006643e+001 1.017027857e+001 1.5e-008 0.14 42 9.1e-006 3.4e-001 1.2e-004 1.00e+000 1.017008640e+001 1.017027734e+001 1.4e-008 0.14 43 8.2e-006 3.2e-001 1.1e-004 1.00e+000 1.017010438e+001 1.017027623e+001 1.3e-008 0.14 44 7.4e-006 3.1e-001 9.5e-005 1.00e+000 1.017012057e+001 1.017027523e+001 1.1e-008 0.14 45 6.6e-006 3.0e-001 8.6e-005 1.00e+000 1.017013513e+001 1.017027432e+001 1.0e-008 0.14 46 6.0e-006 2.8e-001 7.7e-005 1.00e+000 1.017014824e+001 1.017027351e+001 9.1e-009 0.14 47 5.4e-006 2.7e-001 7.0e-005 1.00e+000 1.017016004e+001 1.017027279e+001 8.2e-009 0.14 48 4.8e-006 2.6e-001 6.3e-005 1.00e+000 1.017017066e+001 1.017027213e+001 7.4e-009 0.14 49 4.4e-006 2.5e-001 5.6e-005 1.00e+000 1.017018021e+001 1.017027154e+001 6.7e-009 0.14 50 3.9e-006 2.5e-001 5.1e-005 1.00e+000 1.017018882e+001 1.017027101e+001 6.0e-009 0.16 51 3.5e-006 2.4e-001 4.6e-005 1.00e+000 1.017019656e+001 1.017027053e+001 5.4e-009 0.16 52 3.2e-006 2.3e-001 4.1e-005 1.00e+000 1.017020352e+001 1.017027010e+001 4.9e-009 0.16 53 2.9e-006 2.3e-001 3.7e-005 1.00e+000 1.017020979e+001 1.017026971e+001 4.4e-009 0.16 54 2.6e-006 2.2e-001 3.3e-005 1.00e+000 1.017021544e+001 1.017026937e+001 3.9e-009 0.16 55 2.3e-006 2.2e-001 3.0e-005 9.99e-001 1.017022051e+001 1.017026905e+001 3.5e-009 0.16 56 2.1e-006 2.1e-001 2.7e-005 1.00e+000 1.017022508e+001 1.017026877e+001 3.2e-009 0.16 57 1.9e-006 2.1e-001 2.4e-005 9.99e-001 1.017022919e+001 1.017026852e+001 2.9e-009 0.16 58 1.7e-006 2.1e-001 2.2e-005 1.00e+000 1.017023290e+001 1.017026829e+001 2.6e-009 0.16 59 1.5e-006 2.0e-001 2.0e-005 1.00e+000 1.017023623e+001 1.017026808e+001 2.3e-009 0.17 60 1.4e-006 2.0e-001 1.8e-005 1.00e+000 1.017023924e+001 1.017026789e+001 2.1e-009 0.17 61 1.2e-006 2.0e-001 1.6e-005 9.96e-001 1.017024192e+001 1.017026773e+001 1.9e-009 0.17 62 1.1e-006 2.0e-001 1.4e-005 9.98e-001 1.017024435e+001 1.017026758e+001 1.7e-009 0.17 63 1.0e-006 2.0e-001 1.3e-005 1.00e+000 1.017024654e+001 1.017026744e+001 1.5e-009 0.17 64 9.0e-007 1.9e-001 1.2e-005 1.01e+000 1.017024855e+001 1.017026732e+001 1.4e-009 0.17 65 8.1e-007 1.9e-001 1.0e-005 9.99e-001 1.017025031e+001 1.017026721e+001 1.2e-009 0.17 66 7.3e-007 1.9e-001 9.4e-006 1.00e+000 1.017025191e+001 1.017026711e+001 1.1e-009 0.17 67 6.5e-007 1.9e-001 8.5e-006 1.00e+000 1.017025334e+001 1.017026702e+001 1.0e-009 0.19 68 5.9e-007 1.9e-001 7.6e-006 9.98e-001 1.017025462e+001 1.017026694e+001 9.0e-010 0.19 69 5.3e-007 1.9e-001 6.9e-006 9.97e-001 1.017025579e+001 1.017026687e+001 8.1e-010 0.19 70 4.8e-007 1.9e-001 6.2e-006 1.01e+000 1.017025684e+001 1.017026680e+001 7.3e-010 0.19 71 4.3e-007 1.9e-001 5.6e-006 9.97e-001 1.017025778e+001 1.017026675e+001 6.6e-010 0.19 72 3.9e-007 1.7e-001 5.0e-006 1.01e+000 1.017025867e+001 1.017026669e+001 6.0e-010 0.19 73 3.5e-007 1.5e-001 4.5e-006 9.99e-001 1.017025942e+001 1.017026664e+001 5.4e-010 0.19 74 3.1e-007 1.4e-001 4.0e-006 9.97e-001 1.017026010e+001 1.017026660e+001 4.8e-010 0.19 75 2.8e-007 1.2e-001 3.6e-006 9.95e-001 1.017026071e+001 1.017026656e+001 4.3e-010 0.19 76 2.5e-007 1.1e-001 3.3e-006 9.93e-001 1.017026126e+001 1.017026653e+001 3.9e-010 0.20 77 2.3e-007 9.9e-002 3.0e-006 9.98e-001 1.017026176e+001 1.017026650e+001 3.5e-010 0.20 78 2.1e-007 8.9e-002 2.7e-006 9.76e-001 1.017026220e+001 1.017026647e+001 3.2e-010 0.20 79 1.9e-007 8.0e-002 2.4e-006 9.98e-001 1.017026260e+001 1.017026645e+001 2.8e-010 0.20 80 1.7e-007 7.2e-002 2.2e-006 1.01e+000 1.017026297e+001 1.017026642e+001 2.6e-010 0.20 81 1.5e-007 6.5e-002 1.9e-006 1.02e+000 1.017026333e+001 1.017026640e+001 2.3e-010 0.20 82 3.0e-008 1.3e-002 3.9e-007 1.01e+000 1.017026564e+001 1.017026626e+001 4.8e-011 0.20 83 4.4e-009 1.8e-003 5.3e-008 9.41e-001 1.017026614e+001 1.017026622e+001 4.7e-012 0.20 84 4.0e-009 1.6e-003 4.8e-008 8.93e-001 1.017026615e+001 1.017026622e+001 4.2e-012 0.20 85 3.6e-009 1.4e-003 4.3e-008 1.40e+000 1.017026616e+001 1.017026622e+001 3.8e-012 0.22 86 3.2e-009 1.3e-003 3.9e-008 1.34e+000 1.017026616e+001 1.017026622e+001 3.5e-012 0.22 87 3.8e-010 1.6e-004 4.7e-009 1.11e+000 1.017026621e+001 1.017026622e+001 3.9e-013 0.22 Interior-point optimizer terminated. Time: 0.22. Optimizer terminated. Time: 0.25 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0170266213e+001 nrm: 6e+000 Viol. con: 1e-010 var: 0e+000 Dual. obj: 1.0170266220e+001 nrm: 6e+001 Viol. con: 0e+000 var: 4e-005 * End solution on dual form. * Transforming to primal solution. Solving took 0.283 seconds. result packing took 48% of solve time solution checking took 19% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 770 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 3 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.01 Lin. dep. - number : 0 Presolve terminated. Time: 0.03 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 2 Optimizer - solved problem : the primal Optimizer - Constraints : 346 Optimizer - Cones : 0 Optimizer - Scalar variables : 1055 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 5889 after factor : 1.09e+004 Factor - dense dim. : 0 flops : 1.09e+005 Factor - GP saved nzs : 1.06e+004 GP saved flops : 1.18e+005 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.9e+003 4.0e+003 2.3e+004 0.00e+000 -2.322140343e+004 1.023181539e-012 1.0e+000 0.06 1 9.7e+002 2.0e+003 1.2e+004 -4.21e-002 -1.529869847e+004 6.125183807e+000 5.2e-001 0.06 2 7.8e+002 1.7e+003 9.5e+003 7.67e-001 -1.176094173e+004 8.277598549e+000 4.2e-001 0.06 3 3.9e+002 8.1e+002 4.7e+003 9.66e-001 -5.502163907e+003 1.225856930e+001 2.1e-001 0.08 4 1.4e+002 3.0e+002 1.7e+003 1.57e+000 -1.538217709e+003 1.394920379e+001 8.3e-002 0.08 5 3.8e+001 8.0e+001 4.6e+002 1.60e+000 -3.103675602e+002 1.331916735e+001 2.3e-002 0.08 6 1.1e+001 2.5e+001 1.4e+002 1.14e+000 -7.990129325e+001 1.166605796e+001 7.6e-003 0.08 7 2.5e+000 9.9e+000 3.1e+001 1.04e+000 -9.814585495e+000 1.074416031e+001 2.0e-003 0.08 8 1.4e+000 1.5e+001 1.7e+001 9.02e-001 -1.461035277e+000 1.060986641e+001 1.1e-003 0.08 9 1.1e+000 1.7e+001 1.4e+001 6.29e-001 -1.998297041e-001 1.056867585e+001 9.2e-004 0.09 10 4.0e-001 8.9e+000 5.0e+000 5.48e-001 4.981391139e+000 1.040299346e+001 3.8e-004 0.09 11 2.4e-001 9.6e+000 2.9e+000 5.64e-001 6.634138423e+000 1.033781948e+001 2.4e-004 0.09 12 5.7e-002 4.4e+000 7.2e-001 6.06e-001 9.139868939e+000 1.023012625e+001 7.1e-005 0.09 13 1.7e-002 3.3e+000 2.2e-001 8.59e-001 9.840850056e+000 1.019008169e+001 2.4e-005 0.09 14 1.0e-002 3.0e+000 1.3e-001 9.63e-001 9.974287580e+000 1.018293613e+001 1.4e-005 0.09 15 2.7e-003 2.9e+000 3.4e-002 9.75e-001 1.011824860e+001 1.017347105e+001 3.9e-006 0.11 16 7.6e-004 2.8e+000 9.7e-003 9.95e-001 1.015529736e+001 1.017106257e+001 1.1e-006 0.11 17 2.4e-004 2.7e+000 3.1e-003 9.99e-001 1.016538752e+001 1.017042707e+001 3.7e-007 0.11 18 1.0e-004 2.2e+000 1.3e-003 1.00e+000 1.016816320e+001 1.017025349e+001 1.5e-007 0.11 19 9.0e-005 2.1e+000 1.2e-003 1.00e+000 1.016835832e+001 1.017024300e+001 1.4e-007 0.11 20 8.1e-005 1.9e+000 1.0e-003 1.00e+000 1.016853493e+001 1.017023141e+001 1.2e-007 0.11 21 7.3e-005 1.7e+000 9.4e-004 1.00e+000 1.016869436e+001 1.017022125e+001 1.1e-007 0.13 22 6.6e-005 1.5e+000 8.5e-004 1.00e+000 1.016883788e+001 1.017021210e+001 1.0e-007 0.13 23 5.9e-005 1.4e+000 7.6e-004 1.00e+000 1.016896707e+001 1.017020388e+001 9.0e-008 0.13 24 5.3e-005 1.3e+000 6.9e-004 1.00e+000 1.016908335e+001 1.017019650e+001 8.1e-008 0.13 25 4.8e-005 1.2e+000 6.2e-004 1.00e+000 1.016918803e+001 1.017018987e+001 7.3e-008 0.13 26 4.3e-005 1.1e+000 5.5e-004 1.00e+000 1.016928224e+001 1.017018391e+001 6.6e-008 0.13 27 3.9e-005 9.8e-001 5.0e-004 1.00e+000 1.016936705e+001 1.017017856e+001 5.9e-008 0.13 28 3.5e-005 9.0e-001 4.5e-004 1.00e+000 1.016944338e+001 1.017017375e+001 5.3e-008 0.14 29 3.2e-005 8.3e-001 4.0e-004 1.00e+000 1.016951209e+001 1.017016942e+001 4.8e-008 0.14 30 2.8e-005 7.6e-001 3.6e-004 1.00e+000 1.016957393e+001 1.017016554e+001 4.3e-008 0.14 31 2.6e-005 7.0e-001 3.3e-004 1.00e+000 1.016962960e+001 1.017016205e+001 3.9e-008 0.14 32 2.3e-005 6.5e-001 2.9e-004 1.00e+000 1.016967970e+001 1.017015891e+001 3.5e-008 0.14 33 2.1e-005 6.0e-001 2.7e-004 1.00e+000 1.016972479e+001 1.017015609e+001 3.2e-008 0.14 34 1.9e-005 5.6e-001 2.4e-004 1.00e+000 1.016976538e+001 1.017015355e+001 2.8e-008 0.14 35 1.7e-005 5.2e-001 2.1e-004 1.00e+000 1.016980191e+001 1.017015127e+001 2.6e-008 0.14 36 1.5e-005 4.9e-001 1.9e-004 1.00e+000 1.016983479e+001 1.017014922e+001 2.3e-008 0.16 37 1.4e-005 4.6e-001 1.7e-004 1.00e+000 1.016986439e+001 1.017014737e+001 2.1e-008 0.16 38 1.2e-005 4.3e-001 1.6e-004 1.00e+000 1.016989102e+001 1.017014571e+001 1.9e-008 0.16 39 1.1e-005 4.0e-001 1.4e-004 1.00e+000 1.016991500e+001 1.017014422e+001 1.7e-008 0.16 40 9.9e-006 3.8e-001 1.3e-004 1.00e+000 1.016993658e+001 1.017014287e+001 1.5e-008 0.16 41 8.9e-006 3.6e-001 1.1e-004 1.00e+000 1.016995600e+001 1.017014166e+001 1.4e-008 0.16 42 8.0e-006 3.4e-001 1.0e-004 1.00e+000 1.016997348e+001 1.017014058e+001 1.2e-008 0.16 43 7.2e-006 3.3e-001 9.3e-005 1.00e+000 1.016998921e+001 1.017013960e+001 1.1e-008 0.16 44 6.5e-006 3.1e-001 8.3e-005 1.00e+000 1.017000337e+001 1.017013872e+001 9.9e-009 0.17 45 5.8e-006 3.0e-001 7.5e-005 1.00e+000 1.017001611e+001 1.017013792e+001 8.9e-009 0.17 46 5.3e-006 2.8e-001 6.7e-005 1.00e+000 1.017002758e+001 1.017013721e+001 8.0e-009 0.17 47 4.7e-006 2.7e-001 6.1e-005 1.00e+000 1.017003790e+001 1.017013657e+001 7.2e-009 0.17 48 4.3e-006 2.6e-001 5.5e-005 9.99e-001 1.017004719e+001 1.017013599e+001 6.5e-009 0.17 49 3.8e-006 2.6e-001 4.9e-005 1.00e+000 1.017005555e+001 1.017013547e+001 5.8e-009 0.17 50 3.5e-006 2.5e-001 4.4e-005 1.00e+000 1.017006307e+001 1.017013500e+001 5.3e-009 0.17 51 3.1e-006 2.4e-001 4.0e-005 9.99e-001 1.017006984e+001 1.017013458e+001 4.7e-009 0.17 52 2.8e-006 2.3e-001 3.6e-005 1.00e+000 1.017007594e+001 1.017013420e+001 4.3e-009 0.19 53 2.5e-006 2.3e-001 3.2e-005 1.00e+000 1.017008143e+001 1.017013386e+001 3.8e-009 0.19 54 2.3e-006 2.2e-001 2.9e-005 1.00e+000 1.017008636e+001 1.017013355e+001 3.5e-009 0.19 55 2.0e-006 2.2e-001 2.6e-005 9.99e-001 1.017009080e+001 1.017013328e+001 3.1e-009 0.19 56 1.8e-006 2.1e-001 2.4e-005 9.99e-001 1.017009480e+001 1.017013303e+001 2.8e-009 0.19 57 1.7e-006 2.1e-001 2.1e-005 1.00e+000 1.017009840e+001 1.017013281e+001 2.5e-009 0.19 58 1.5e-006 2.1e-001 1.9e-005 9.98e-001 1.017010163e+001 1.017013260e+001 2.3e-009 0.19 59 1.3e-006 2.0e-001 1.7e-005 1.00e+000 1.017010455e+001 1.017013242e+001 2.0e-009 0.19 60 1.2e-006 2.0e-001 1.5e-005 1.00e+000 1.017010717e+001 1.017013226e+001 1.8e-009 0.19 61 1.1e-006 2.0e-001 1.4e-005 1.00e+000 1.017010953e+001 1.017013211e+001 1.7e-009 0.20 62 9.7e-007 2.0e-001 1.3e-005 1.00e+000 1.017011165e+001 1.017013198e+001 1.5e-009 0.20 63 8.8e-007 1.9e-001 1.1e-005 1.00e+000 1.017011355e+001 1.017013186e+001 1.3e-009 0.20 64 7.9e-007 1.9e-001 1.0e-005 9.96e-001 1.017011527e+001 1.017013176e+001 1.2e-009 0.20 65 7.1e-007 1.9e-001 9.1e-006 9.99e-001 1.017011683e+001 1.017013166e+001 1.1e-009 0.20 66 6.4e-007 1.9e-001 8.2e-006 9.98e-001 1.017011822e+001 1.017013157e+001 9.8e-010 0.20 67 5.8e-007 1.9e-001 7.4e-006 1.00e+000 1.017011948e+001 1.017013149e+001 8.8e-010 0.20 68 5.2e-007 1.9e-001 6.6e-006 9.97e-001 1.017012061e+001 1.017013142e+001 7.9e-010 0.20 69 4.7e-007 1.7e-001 6.0e-006 1.01e+000 1.017012165e+001 1.017013136e+001 7.1e-010 0.20 70 4.2e-007 1.5e-001 5.4e-006 1.01e+000 1.017012261e+001 1.017013130e+001 6.5e-010 0.20 71 3.8e-007 1.4e-001 4.8e-006 1.01e+000 1.017012345e+001 1.017013124e+001 5.8e-010 0.22 72 3.4e-007 1.2e-001 4.4e-006 1.00e+000 1.017012418e+001 1.017013120e+001 5.2e-010 0.22 73 3.1e-007 1.1e-001 3.9e-006 9.99e-001 1.017012484e+001 1.017013116e+001 4.7e-010 0.22 74 2.8e-007 9.9e-002 3.5e-006 1.00e+000 1.017012543e+001 1.017013112e+001 4.2e-010 0.22 75 2.5e-007 9.0e-002 3.2e-006 9.83e-001 1.017012596e+001 1.017013109e+001 3.8e-010 0.22 76 2.2e-007 8.1e-002 2.9e-006 1.01e+000 1.017012647e+001 1.017013105e+001 3.5e-010 0.22 77 2.0e-007 7.3e-002 2.6e-006 9.97e-001 1.017012690e+001 1.017013103e+001 3.1e-010 0.22 78 1.8e-007 6.5e-002 2.3e-006 9.65e-001 1.017012728e+001 1.017013100e+001 2.8e-010 0.22 79 1.6e-007 5.9e-002 2.1e-006 9.94e-001 1.017012763e+001 1.017013098e+001 2.5e-010 0.23 80 1.5e-007 5.3e-002 1.9e-006 9.93e-001 1.017012795e+001 1.017013096e+001 2.3e-010 0.23 81 1.3e-007 4.8e-002 1.7e-006 9.70e-001 1.017012823e+001 1.017013094e+001 2.0e-010 0.23 82 1.2e-007 4.3e-002 1.5e-006 9.97e-001 1.017012848e+001 1.017013093e+001 1.8e-010 0.23 83 1.1e-007 3.9e-002 1.4e-006 9.47e-001 1.017012871e+001 1.017013091e+001 1.7e-010 0.23 84 9.6e-008 3.5e-002 1.2e-006 9.84e-001 1.017012892e+001 1.017013090e+001 1.5e-010 0.23 85 8.6e-008 3.1e-002 1.1e-006 1.03e+000 1.017012913e+001 1.017013089e+001 1.4e-010 0.23 86 7.8e-008 2.8e-002 1.0e-006 1.05e+000 1.017012934e+001 1.017013087e+001 1.3e-010 0.23 87 7.0e-008 2.5e-002 9.0e-007 9.84e-001 1.017012948e+001 1.017013086e+001 1.1e-010 0.23 88 6.3e-008 2.3e-002 8.1e-007 9.73e-001 1.017012961e+001 1.017013086e+001 1.0e-010 0.25 89 5.7e-008 2.0e-002 7.3e-007 9.75e-001 1.017012972e+001 1.017013085e+001 9.2e-011 0.25 90 4.2e-009 1.3e-003 4.6e-008 9.44e-001 1.017013072e+001 1.017013079e+001 9.0e-012 0.25 91 2.9e-010 7.7e-005 2.8e-009 9.50e-001 1.017013078e+001 1.017013078e+001 7.9e-013 0.25 Interior-point optimizer terminated. Time: 0.25. Optimizer terminated. Time: 0.27 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0170130779e+001 nrm: 9e+000 Viol. con: 3e-010 var: 0e+000 Dual. obj: 1.0170130783e+001 nrm: 6e+001 Viol. con: 0e+000 var: 2e-005 * End solution on dual form. * Transforming to primal solution. Solving took 0.297 seconds. result packing took 2.4e+02% of solve time solution checking took 18% of solve time Solving took 5 GP solves and 5.11 seconds. Warning: Constraint [W_{total}_FleetMission_(0,) [N]... >= W_{dry}_FleetMission_(0,) + W_{f_{total}}_FleetMission_(0,) [N]...] is not tight because the left hand side evaluated to 366641.68011 newton but the right hand side evaluated to 366630.068284 newton (Allowable error: 0.0001%, Actual error: 0.0032%) Warning: Constraint [W_{total}_FleetMission_(1,) [N]... >= W_{dry}_FleetMission_(1,) + W_{f_{total}}_FleetMission_(1,) [N]...] is not tight because the left hand side evaluated to 377162.194107 newton but the right hand side evaluated to 377115.443361 newton (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [W_{total}_FleetMission_(2,) [N]... >= W_{dry}_FleetMission_(2,) + W_{f_{total}}_FleetMission_(2,) [N]...] is not tight because the left hand side evaluated to 388105.092591 newton but the right hand side evaluated to 387998.862059 newton (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [W_{total}_FleetMission_(3,) [N]... >= W_{dry}_FleetMission_(3,) + W_{f_{total}}_FleetMission_(3,) [N]...] is not tight because the left hand side evaluated to 399470.246683 newton but the right hand side evaluated to 399279.095298 newton (Allowable error: 0.0001%, Actual error: 0.048%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 361212.196356 newton but the right hand side evaluated to 361206.371724 newton (Allowable error: 0.0001%, Actual error: 0.0016%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 1) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 1) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 371522.142922 newton but the right hand side evaluated to 371498.546408 newton (Allowable error: 0.0001%, Actual error: 0.0064%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 2) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 2) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 382190.308533 newton but the right hand side evaluated to 382135.97016 newton (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 3) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 3) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 393255.645285 newton but the right hand side evaluated to 393156.48009 newton (Allowable error: 0.0001%, Actual error: 0.025%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 356181.888903 newton but the right hand side evaluated to 356176.101781 newton (Allowable error: 0.0001%, Actual error: 0.0016%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 1) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 1) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 361243.205811 newton but the right hand side evaluated to 361220.051646 newton (Allowable error: 0.0001%, Actual error: 0.0064%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 2) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 2) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 366354.227328 newton but the right hand side evaluated to 366302.335362 newton (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 3) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 3) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 371535.457173 newton but the right hand side evaluated to 371443.471164 newton (Allowable error: 0.0001%, Actual error: 0.025%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) [N]...] is not tight because the left hand side evaluated to 18366.9603608 newton but the right hand side evaluated to 18366.7175501 newton (Allowable error: 0.0001%, Actual error: 0.0013%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 1) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 1) [N]...] is not tight because the left hand side evaluated to 18344.4542914 newton but the right hand side evaluated to 18344.2049502 newton (Allowable error: 0.0001%, Actual error: 0.0014%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 2) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 2) [N]...] is not tight because the left hand side evaluated to 18344.454213 newton but the right hand side evaluated to 18344.2048419 newton (Allowable error: 0.0001%, Actual error: 0.0014%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 3) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 3) [N]...] is not tight because the left hand side evaluated to 18344.454242 newton but the right hand side evaluated to 18344.2048694 newton (Allowable error: 0.0001%, Actual error: 0.0014%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) [N]...] is not tight because the left hand side evaluated to 18924.2856477 newton but the right hand side evaluated to 18924.2651601 newton (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 2) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 2) [N]...] is not tight because the left hand side evaluated to 8445.89963773 newton but the right hand side evaluated to 8445.84800394 newton (Allowable error: 0.0001%, Actual error: 0.00061%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 3) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 3) [N]...] is not tight because the left hand side evaluated to 8626.29336595 newton but the right hand side evaluated to 8626.24784664 newton (Allowable error: 0.0001%, Actual error: 0.00053%) 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 24184.7528322 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 26232.8485062 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 15.397s OK Generating XML reports... Cloning into 'gassolar'... 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Cannot uninstall requirement gassolar, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/gassolar Installing collected packages: gassolar Running setup.py develop for gassolar Successfully installed gassolar From https://github.com/convexengineering/gpkit-models * branch tailfoam -> FETCH_HEAD Previous HEAD position was 662ac9f... add readme with build status HEAD is now at 2605db2... move cmac calc to different line Cannot uninstall requirement gpkit-models, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/gpkit-models 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 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:\anaconda2\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-mzukuv-build Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\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\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/gas/gas_simple/gassimple.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 564 variables. Solving took 0.125 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 0.2682 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 564 variables. Solving took 0.121 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 0.2682 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 564 variables. Solving took 0.15 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 0.2682 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_cli' Solving for 564 variables. Solving took 0.266 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 0.2682 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 79 variables. Solving took 0.04 seconds. Using solver 'mosek_cli' Solving for 79 variables. Solving took 0.067 seconds. Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(0,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(0,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.214978984961 but the right hand side evaluated to 0.214980454496 (Allowable error: 0.0001%, Actual error: 0.00068%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(1,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(1,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.201771179179 but the right hand side evaluated to 0.201763680631 (Allowable error: 0.0001%, Actual error: 0.0037%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(2,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(2,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.197670060366 but the right hand side evaluated to 0.197659749313 (Allowable error: 0.0001%, Actual error: 0.0052%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(3,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(3,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.201771179179 but the right hand side evaluated to 0.201763680631 (Allowable error: 0.0001%, Actual error: 0.0037%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(4,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(4,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.214978984961 but the right hand side evaluated to 0.214980454496 (Allowable error: 0.0001%, Actual error: 0.00068%) Using solver 'mosek' Solving for 1067 variables. Solving took 0.539 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 134070.2901 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 134071.9051 but bound is 150000.0000 1 is a constraining latitude 11 is a constraining latitude Beginning signomial solve. Solving took 4 GP solves and 2.43 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 136276.7371 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 136278.3664 but bound is 150000.0000 1 is a constraining latitude 11 is a constraining latitude Using solver 'mosek_cli' Solving for 1067 variables. Solving took 0.643 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 134070.3579 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 134071.6986 but bound is 150000.0000 1 is a constraining latitude 11 is a constraining latitude Beginning signomial solve. Solving took 4 GP solves and 2.95 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 136276.3380 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 136277.7007 but bound is 150000.0000 1 is a constraining latitude 11 is a constraining latitude Running tests... ---------------------------------------------------------------------- ....c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\gassolar\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 6 tests in 31.474s OK Generating XML reports... Cloning into 'SPaircraft'... 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From https://github.com/convexengineering/gpkit-models * branch master -> FETCH_HEAD Warning: you are leaving 1 commit behind, not connected to any of your branches: 2605db2 move cmac calc to different line If you want to keep it by creating a new branch, this may be a good time to do so with: git branch <new-branch-name> 2605db2 HEAD is now at 662ac9f... add readme with build status Cannot uninstall requirement gpkit-models, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/gpkit-models 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 Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to c:\users\jenkins\appdata\local\temp\pip-js6zxe-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\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\turbofan Requirement already satisfied: numpy in c:\anaconda2\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' Beginning signomial solve. Solving took 7 GP solves and 7.83 seconds. 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 2427091.85981 force_pound * meter but the right hand side evaluated to 2397885.90144 force_pound * meter (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 2.21510116713 meter but the right hand side evaluated to 1.96470877865 meter (Allowable error: 0.1%, Actual error: 11%) 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 17472.5956929 newton but the right hand side evaluated to 17443.2611004 newton (Allowable error: 0.1%, Actual error: 0.17%) 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 1242113.51232 joule / kilogram but the right hand side evaluated to 1.481323689 megajoule / kilogram (Allowable error: 0.1%, Actual error: 9.5%) 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 642470.702049 joule / kilogram but the right hand side evaluated to 0.643954903842 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.1%) Warning: Constraint [W_{lg}_Mission/Aircraft/LandingGear*x_{CG_{lg}}_Mission/Aircraft/LandingGear [N*m]... >= W_{mg}_Mission/Aircraft/LandingGear*x_m_Mission/Aircraft/LandingGear + W_{ng}_Mission/Aircraft/Landi...] is not tight because the left hand side evaluated to 271789.77817 meter * newton but the right hand side evaluated to 263034.946839 meter * newton (Allowable error: 1.0%, Actual error: 3.3%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.5759806369 meter but the right hand side evaluated to 16.6120443238 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 10.9551724251 but the right hand side evaluated to 4.85819009907 (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 10.0069241739 but the right hand side evaluated to 4.85820032213 (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 8.21524855375 but the right hand side evaluated to 4.85820039676 (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 18.6219984919 meter but the right hand side evaluated to 18.3758647678 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 18.6219984919 meter but the right hand side evaluated to 18.4513421121 meter (Allowable error: 0.1%, Actual error: 0.92%) 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 4.67771495028 but the right hand side evaluated to 4.79404361453 (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 4.73115251145 but the right hand side evaluated to 4.81373475207 (Allowable error: 0.1%, Actual error: 1.7%) 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 7.60828704516 but the right hand side evaluated to 4.79404361453 (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 7.57972229752 but the right hand side evaluated to 4.81373475207 (Allowable error: 0.1%, Actual error: 36%) Solves with these variables bounded: value near lower bound: [CruiseAlt_Mission] value near upper bound: [TotalTime_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission] Checking for relaxed constants... WEIGHT DIFFERENCES Total Fuel Weight Percent Diff: [-6.974511] Total Aircraft Weight Percent Diff: [-4.95040632] Engine Weight Percent Diff: -8.23491296731 Fuselage Weight Percent Diff: -10.954183999 Payload Weight Percent Diff: [-0.04003556] VT Weight Percent Diff: -24.5189197889 HT Weight Percent Diff: -85.1524642817 Wing Weight Percent Diff: 0.426055038685 WING DIFFERENCES Wing Span Percent Diff: 0.92160714659 Wing Area Percent Diff: -6.86178864998 HORIZONTAL TAIL DIFFERENCES HT Area Percent Diff: -54.618442108 VERTICAL TAIL DIFFERENCES VT Span Percent Diff: -16.3231876887 VT Area Percent Diff: -29.9969617604 CRUISE SEGMENT 1 DRAG DIFFERENCES Overall Cd Percent Diff: [-0.13097824] Nacelle Cd Percent Diff: [ 23.80939266] HT Cd Percent Diff: [-63.50965072] dimensionless Fuselage Cd Percent Diff: [ 45.32349081] VT Cd Percent Diff: [ 60.36863942] dimensionless Induced Drag Cd Percent Diff: [ 1.0635387] Wing Profile Cd Percent Diff: [-15.69404962] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [ 2.99115911] FUSELAGE DIFFERENCES Fan Propulsive Efficiency in Cruise Segment 1 --------------------- 0.790004809152 Beginning signomial solve. Solving took 7 GP solves and 9.54 seconds. 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 2427110.46813 force_pound * meter but the right hand side evaluated to 2397879.59156 force_pound * meter (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 2.2151026307 meter but the right hand side evaluated to 1.96463858069 meter (Allowable error: 0.1%, Actual error: 11%) 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 17472.6096941 newton but the right hand side evaluated to 17443.2668622 newton (Allowable error: 0.1%, Actual error: 0.17%) 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 1242089.58173 joule / kilogram but the right hand side evaluated to 1.48110933844 megajoule / kilogram (Allowable error: 0.1%, Actual error: 9.5%) 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 642468.482114 joule / kilogram but the right hand side evaluated to 0.643951001757 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.1%) Warning: Constraint [W_{lg}_Mission/Aircraft/LandingGear*x_{CG_{lg}}_Mission/Aircraft/LandingGear [N*m]... >= W_{mg}_Mission/Aircraft/LandingGear*x_m_Mission/Aircraft/LandingGear + W_{ng}_Mission/Aircraft/Landi...] is not tight because the left hand side evaluated to 271790.00319 meter * newton but the right hand side evaluated to 263035.234242 meter * newton (Allowable error: 1.0%, Actual error: 3.3%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.576010682 meter but the right hand side evaluated to 16.612144097 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 10.9551811851 but the right hand side evaluated to 4.8581805724 (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 10.0069446021 but the right hand side evaluated to 4.85819028877 (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 8.21526262845 but the right hand side evaluated to 4.85819028877 (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 18.6220848341 meter but the right hand side evaluated to 18.3759363202 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 18.6220848341 meter but the right hand side evaluated to 18.4514323201 meter (Allowable error: 0.1%, Actual error: 0.92%) 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 4.67769548154 but the right hand side evaluated to 4.79403290607 (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 4.73115391837 but the right hand side evaluated to 4.81372878996 (Allowable error: 0.1%, Actual error: 1.7%) 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 7.60828467118 but the right hand side evaluated to 4.79403290607 (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 7.57972986055 but the right hand side evaluated to 4.81372878996 (Allowable error: 0.1%, Actual error: 36%) Solves with these variables bounded: value near lower bound: [CruiseAlt_Mission] value near upper bound: [TotalTime_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission] Checking for relaxed constants... WEIGHT DIFFERENCES Total Fuel Weight Percent Diff: [-6.97422995] Total Aircraft Weight Percent Diff: [-4.95044675] Engine Weight Percent Diff: -8.23523451512 Fuselage Weight Percent Diff: -10.954618425 Payload Weight Percent Diff: [-0.04052335] VT Weight Percent Diff: -24.5186291271 HT Weight Percent Diff: -85.1522421315 Wing Weight Percent Diff: 0.425462741526 WING DIFFERENCES Wing Span Percent Diff: 0.921619801497 Wing Area Percent Diff: -6.86125473922 HORIZONTAL TAIL DIFFERENCES HT Area Percent Diff: -54.6177482454 VERTICAL TAIL DIFFERENCES VT Span Percent Diff: -16.3230602377 VT Area Percent Diff: -29.9968058767 CRUISE SEGMENT 1 DRAG DIFFERENCES Overall Cd Percent Diff: [-0.13148046] Nacelle Cd Percent Diff: [ 23.80877311] HT Cd Percent Diff: [-63.50920274] dimensionless Fuselage Cd Percent Diff: [ 45.32347143] VT Cd Percent Diff: [ 60.36804424] dimensionless Induced Drag Cd Percent Diff: [ 1.0628754] Wing Profile Cd Percent Diff: [-15.6945082] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [ 2.99160433] FUSELAGE DIFFERENCES Fan Propulsive Efficiency in Cruise Segment 1 --------------------- 0.790003964601 Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 34.597s OK Generating XML reports... calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gpkit-models.git'] 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/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 ['git', 'fetch', '--depth', '1', 'origin', 'master'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 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 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'turbofan'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'master'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gassolar'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'tailfoam'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'tailfoam'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 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/SPaircraft.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'master'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/turbofan.git'] attempt 1 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>exit 0 [xUnit] [INFO] - Starting to record. [xUnit] [INFO] - Processing JUnit [xUnit] [INFO] - [JUnit] - 5 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'C:\Users\jenkins\workspace\gpkit_commons_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 SUCCESS [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: SUCCESS