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Started by upstream project "gpkit_commons_PR_Models" build number 16 originally caused by: GitHub pull request #123 of commit 238e02f31062b9197e4b2a4d47181e33ca099d6a, no merge conflicts. Building remotely on windows7x64 in workspace D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > git init D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git --version # timeout=10 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 > git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10 > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master Merging Revision 9a9531c5d88de00e8825c434df4d40f160cb13e5 (refs/remotes/origin/pr/123/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='default', fastForwardMode='--ff'} > git rev-parse "origin/master^{commit}" # timeout=10 > git config core.sparsecheckout # timeout=10 > git checkout -f origin/master # timeout=3 > git merge --ff 9a9531c5d88de00e8825c434df4d40f160cb13e5 # timeout=10 > git rev-parse "HEAD^{commit}" # timeout=10 Seen branch in repository origin/1682literate Seen branch in repository origin/1682master Seen branch in repository origin/Breakdown Seen branch in repository origin/SPaircraft Seen branch in repository origin/aerosurf Seen branch in repository origin/atmosphere Seen branch in repository origin/boxspar Seen branch in repository origin/breguet_range Seen branch in repository origin/breguetsetup Seen branch in repository origin/climb Seen branch in repository origin/commercial_sizing Seen branch in repository origin/d8 Seen branch in repository origin/d8fuselage Seen 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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 > git tag -l # timeout=10 > git rev-parse "refs/tags/include^{commit}" # timeout=10 > git rev-parse "refs/tags/DF70^{commit}" # timeout=10 > git rev-parse "refs/tags/linking^{commit}" # timeout=10 > git rev-parse "refs/tags/csv^{commit}" # timeout=10 > git rev-parse "refs/tags/start^{commit}" # timeout=10 > git rev-parse "refs/tags/pay^{commit}" # timeout=10 > git rev-parse "refs/tags/sum^{commit}" # timeout=10 > git rev-parse "refs/tags/clean^{commit}" # timeout=10 > git rev-parse "refs/tags/sys^{commit}" # timeout=10 > git rev-parse "refs/tags/pshaft^{commit}" # timeout=10 > git rev-parse "refs/tags/solarmd^{commit}" # timeout=10 > git rev-parse "refs/tags/climb^{commit}" # timeout=10 > git rev-parse "refs/tags/fuse^{commit}" # timeout=10 > git rev-parse "refs/tags/mission^{commit}" # timeout=10 > git rev-parse "refs/tags/discret^{commit}" # timeout=10 > git rev-parse "refs/tags/plot^{commit}" # timeout=10 > git rev-parse "refs/tags/md^{commit}" # timeout=10 > git rev-parse "refs/tags/atm^{commit}" # timeout=10 > git rev-parse "refs/tags/make^{commit}" # timeout=10 > git rev-parse "refs/tags/eng^{commit}" # timeout=10 Checking out Revision 9a9531c5d88de00e8825c434df4d40f160cb13e5 (origin/pr/123/merge, origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f 9a9531c5d88de00e8825c434df4d40f160cb13e5 # timeout=3 Commit message: "Merge 238e02f31062b9197e4b2a4d47181e33ca099d6a 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="explicitly add wing interior to v-h tails" href="https://github.com/convexengineering/gplibrary/pull/123">PR 123</a>: explicitly add wing interior to v-h tails [Execution node] check if [windows7x64] is in [[macys, macys_Sierra, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [windows7x64] is in [[windows10x64, windows7x64]] Run condition [Execution node ] enabling perform for step [Execute Windows batch command] [mosek] $ cmd /c call C:\Users\jenkins\AppData\Local\Temp\jenkins2452801850394681216.bat D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>echo C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Program Files (x86)\NVIDIA Corporation\PhysX\Common;D:\Compilers\Intel\Compiler\11.1\048\lib\Intel64;D:\Compilers\Intel\Compiler\11.1\048\lib\ia32;D:\Compilers\Intel\Compiler\11.1\048\mkl\em64t\bin;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\ C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Program Files (x86)\NVIDIA Corporation\PhysX\Common;D:\Compilers\Intel\Compiler\11.1\048\lib\Intel64;D:\Compilers\Intel\Compiler\11.1\048\lib\ia32;D:\Compilers\Intel\Compiler\11.1\048\mkl\em64t\bin;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\ D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>REM turn on the anaconda console D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>call activate.bat || exit /b 666 (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>REM Create a virtualenv to install everything into (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>SET VENV=D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>virtualenv --system-site-packages D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit New python executable in D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\Scripts\python.exe Installing setuptools, pip, wheel...done. (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>call D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\Scripts\activate.bat (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>REM Install coverage into the virtualenv to the coverage command blow uses the virtualenv python (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\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) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>if mosek == mosek msktestlic || exit /b 666 Computer Platform : Windows/64-X86 Problem Name : Objective sense : min Type : LO (linear optimization problem) Constraints : 1 Cones : 0 Scalar variables : 5000 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator - tries : 0 time : 0.00 Eliminator - elim's : 0 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.03 ************************************ A license was checked out correctly. ************************************ (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>SET GPKITBUILD=D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek\build_gpkit (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>gcc --version || exit /b 666 gcc (x86_64-posix-seh-rev1, Built by MinGW-W64 project) 6.3.0 Copyright (C) 2016 Free Software Foundation, Inc. This is free software; see the source for copying conditions. There is NO warranty; not even for MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>if mosek == cvxopt set GPKITSOLVERS=cvxopt (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>if mosek == mosek set GPKITSOLVERS=mosek, mosek_cli (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>dir D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek\build_gpkit Volume in drive D is Home Volume Serial Number is EA39-7CA0 Directory of D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek File Not Found (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>python -c "import scipy; print scipy.__version__" 0.19.0 (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>python -c "import numpy; print numpy.__version__" 1.12.1 (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>python -c "import pint; print pint.__version__" 0.7.2 (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>REM Install gpkit to run the documentation examples (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>git clone --depth 1 https://github.com/convexengineering/gpkit.git Cloning into 'gpkit'... (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>pip install -e D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek\gpkit | exit /b 666 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 480 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 767 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_install.py, line 985 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file install.py, line 369 (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>pip install -e D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek | exit /b 666 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 480 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 767 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_install.py, line 985 Traceback (most recent call last): File "D:\Anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file install.py, line 369 (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>REM Show the settings file (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek>type D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\env\settings installed_solvers : mosek, mosek_cli mosek_bin_dir : C:\Program Files\Mosek\7\tools\platform\win64x86\bin (venv2_gpkit) (root) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\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 0.025 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.02 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.066 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 0.576s 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:///D:/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows7x64/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 d:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: numpy>=1.7.0 in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-lq5375-build Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) Installing collected packages: gpfit Running setup.py install for gpfit: started Running setup.py install for gpfit: finished with status 'done' Successfully installed gpfit-0.1 adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -9.54887210969e-14. Allowing negative dual variable(s) as small as -1.17742100791e-12. Allowing negative dual variable(s) as small as -1.14131100404e-12. Allowing negative dual variable(s) as small as -1.14081183736e-12. Solving took 4 GP solves and 5.21 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.01646122075e-13. Allowing negative dual variable(s) as small as -1.17227625177e-12. Allowing negative dual variable(s) as small as -1.1354112095e-12. Allowing negative dual variable(s) as small as -1.12470406252e-12. Solving took 4 GP solves and 2.01 seconds. Allowing negative dual variable(s) as small as -1.56934534812e-12. Allowing negative dual variable(s) as small as -3.9608871738e-12. Allowing negative dual variable(s) as small as -1.78670012813e-12. Allowing negative dual variable(s) as small as -2.08236899946e-12. Allowing negative dual variable(s) as small as -2.08074529828e-12. Allowing negative dual variable(s) as small as -4.72235098248e-13. Allowing negative dual variable(s) as small as -8.93242728048e-13. Allowing negative dual variable(s) as small as -9.4073923998e-13. Allowing negative dual variable(s) as small as -9.44143309541e-13. 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 -2.28685343232e-13. Allowing negative dual variable(s) as small as -9.27694336281e-14. Allowing negative dual variable(s) as small as -1.19352986695e-13. Allowing negative dual variable(s) as small as -1.20252115557e-13. 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 -9.61398786492e-13. Allowing negative dual variable(s) as small as -2.01783224596e-12. Allowing negative dual variable(s) as small as -1.27258002355e-14. Allowing negative dual variable(s) as small as -1.76552011693e-14. Solving took 4 GP solves and 3.12 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 1021559.0193 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Solving took 4 GP solves and 4.31 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -1.56981459082e-12. Allowing negative dual variable(s) as small as -3.96070242575e-12. Allowing negative dual variable(s) as small as -1.78650670646e-12. Allowing negative dual variable(s) as small as -2.08240716337e-12. Allowing negative dual variable(s) as small as -2.08098815957e-12. Allowing negative dual variable(s) as small as -4.72637554094e-13. Allowing negative dual variable(s) as small as -8.93307563338e-13. Allowing negative dual variable(s) as small as -9.41251200245e-13. Allowing negative dual variable(s) as small as -9.43594594821e-13. 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 -2.37099619452e-13. Allowing negative dual variable(s) as small as -9.19345979553e-14. Allowing negative dual variable(s) as small as -1.19538168426e-13. Allowing negative dual variable(s) as small as -1.20402494398e-13. 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 -9.61399790861e-13. Allowing negative dual variable(s) as small as -2.01627488438e-12. Allowing negative dual variable(s) as small as -1.32873863089e-14. Allowing negative dual variable(s) as small as -1.76514913238e-14. Solving took 4 GP solves and 22.8 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 1021559.0193 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Solving took 4 GP solves and 5.68 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 201.251s OK Generating XML reports... Cloning into 'turbofan'... Cannot uninstall requirement turbofan, not installed Obtaining file:///D:/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows7x64/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:///D:/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows7x64/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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 987 Eliminator terminated. Eliminator started. Total number of eliminations : 990 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 990 Lin. dep. - tries : 1 time : 0.02 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 : 329 Optimizer - Cones : 0 Optimizer - Scalar variables : 1038 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.06 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 6388 after factor : 1.11e+004 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.2e+003 1.8e+004 2.1e+004 0.00e+000 -2.068680080e+004 1.023181539e-012 1.0e+000 0.09 1 9.0e+002 1.3e+004 1.5e+004 -1.09e-001 -1.772328772e+004 2.816143901e+000 7.3e-001 0.20 2 3.6e+002 5.2e+003 6.0e+003 4.01e-002 -1.101718517e+004 1.002493482e+001 3.0e-001 0.31 3 1.9e+002 2.7e+003 3.1e+003 6.47e-001 -5.771883838e+003 1.375649323e+001 1.7e-001 0.42 4 5.8e+001 8.4e+002 9.8e+002 1.20e+000 -1.605000052e+003 1.625567831e+001 5.7e-002 0.48 5 3.1e+001 4.5e+002 5.2e+002 1.69e+000 -6.745231482e+002 1.621109938e+001 3.1e-002 0.66 6 1.0e+001 1.4e+002 1.7e+002 1.50e+000 -1.671132385e+002 1.570777420e+001 1.0e-002 0.73 7 4.4e+000 6.5e+001 7.4e+001 1.15e+000 -6.553631853e+001 1.497843205e+001 4.8e-003 0.87 8 2.1e+000 3.2e+001 3.6e+001 8.76e-001 -3.007576931e+001 1.440762897e+001 2.4e-003 0.98 9 9.9e-001 1.8e+001 1.7e+001 5.55e-001 -1.319811678e+001 1.384703499e+001 1.2e-003 1.12 10 3.3e-001 6.3e+000 5.6e+000 5.48e-001 1.823337596e+000 1.321186566e+001 4.6e-004 1.33 11 1.5e-001 3.2e+000 2.6e+000 6.35e-001 7.019656333e+000 1.295307474e+001 2.2e-004 1.36 12 9.8e-002 2.5e+000 1.7e+000 7.48e-001 8.809112745e+000 1.282120596e+001 1.4e-004 1.53 13 2.3e-002 1.5e+000 4.1e-001 8.18e-001 1.155746091e+001 1.259123248e+001 4.1e-005 1.56 14 7.4e-003 1.5e+000 1.3e-001 9.41e-001 1.219953216e+001 1.254375298e+001 1.5e-005 1.64 15 2.0e-003 1.5e+000 3.7e-002 9.82e-001 1.242496775e+001 1.252086493e+001 4.4e-006 1.76 16 6.0e-004 1.3e+000 1.1e-002 9.93e-001 1.248678478e+001 1.251548966e+001 1.3e-006 1.92 17 2.3e-004 1.0e+000 4.3e-003 9.69e-001 1.250291333e+001 1.251431905e+001 5.4e-007 1.92 18 2.1e-004 9.4e-001 3.9e-003 9.74e-001 1.250394691e+001 1.251423010e+001 4.8e-007 2.01 19 1.9e-004 8.6e-001 3.5e-003 9.55e-001 1.250488688e+001 1.251416524e+001 4.3e-007 2.11 20 1.7e-004 7.8e-001 3.2e-003 8.89e-001 1.250572265e+001 1.251410451e+001 3.9e-007 2.12 21 1.5e-004 7.1e-001 2.9e-003 9.68e-001 1.250651822e+001 1.251404538e+001 3.5e-007 2.17 22 1.4e-004 6.5e-001 2.6e-003 9.96e-001 1.250722158e+001 1.251399378e+001 3.2e-007 2.31 23 1.2e-004 5.9e-001 2.3e-003 9.74e-001 1.250785475e+001 1.251394604e+001 2.9e-007 2.39 24 1.1e-004 5.4e-001 2.1e-003 9.84e-001 1.250840727e+001 1.251390902e+001 2.6e-007 2.40 25 1.0e-004 5.0e-001 1.9e-003 9.05e-001 1.250890955e+001 1.251387277e+001 2.3e-007 2.42 26 9.1e-005 4.6e-001 1.7e-003 1.01e+000 1.250937263e+001 1.251384241e+001 2.1e-007 2.42 27 8.2e-005 4.2e-001 1.5e-003 9.94e-001 1.250979396e+001 1.251381064e+001 1.9e-007 2.51 28 7.4e-005 3.9e-001 1.4e-003 9.94e-001 1.251017550e+001 1.251378176e+001 1.7e-007 2.67 29 6.6e-005 3.6e-001 1.2e-003 9.70e-001 1.251050054e+001 1.251376051e+001 1.5e-007 2.70 30 6.0e-005 3.3e-001 1.1e-003 1.03e+000 1.251084613e+001 1.251373599e+001 1.4e-007 2.87 31 5.4e-005 3.1e-001 1.0e-003 9.48e-001 1.251112677e+001 1.251371314e+001 1.2e-007 2.98 32 4.8e-005 2.9e-001 9.0e-004 8.79e-001 1.251135331e+001 1.251369973e+001 1.1e-007 3.12 33 4.4e-005 2.8e-001 8.1e-004 1.11e+000 1.251166800e+001 1.251367930e+001 1.1e-007 3.26 34 3.9e-005 2.6e-001 7.3e-004 9.20e-001 1.251183553e+001 1.251367034e+001 9.6e-008 3.34 35 3.5e-005 2.3e-001 6.5e-004 7.74e-001 1.251198074e+001 1.251366423e+001 8.7e-008 3.48 36 3.2e-005 2.1e-001 5.9e-004 1.19e+000 1.251225680e+001 1.251364719e+001 8.6e-008 3.60 37 2.9e-005 2.0e-001 5.3e-004 9.03e-001 1.251237760e+001 1.251363851e+001 7.8e-008 3.67 38 2.6e-005 1.8e-001 4.8e-004 1.08e+000 1.251254000e+001 1.251362482e+001 7.2e-008 3.79 39 2.3e-005 1.7e-001 4.3e-004 1.08e+000 1.251266577e+001 1.251361651e+001 6.8e-008 3.90 40 2.1e-005 1.6e-001 3.9e-004 8.63e-001 1.251274131e+001 1.251361270e+001 6.1e-008 3.90 41 1.9e-005 1.5e-001 3.5e-004 7.87e-001 1.251282178e+001 1.251360593e+001 5.5e-008 3.90 42 1.7e-005 1.4e-001 3.1e-004 1.32e+000 1.251288744e+001 1.251360218e+001 4.9e-008 3.90 43 1.0e-005 8.6e-002 1.9e-004 3.43e-001 1.251315722e+001 1.251357634e+001 2.9e-008 3.90 44 9.1e-006 7.8e-002 1.7e-004 1.65e+000 1.251319978e+001 1.251357252e+001 2.6e-008 3.90 45 8.2e-006 7.7e-002 1.5e-004 1.26e+000 1.251323189e+001 1.251357066e+001 2.4e-008 3.92 46 7.4e-006 6.9e-002 1.4e-004 9.98e-001 1.251326175e+001 1.251356870e+001 2.1e-008 3.92 47 6.7e-006 6.2e-002 1.2e-004 6.27e+000 1.251332243e+001 1.251355729e+001 1.8e-008 3.92 48 6.0e-006 5.6e-002 1.1e-004 1.00e+000 1.251334552e+001 1.251355624e+001 1.6e-008 3.92 49 1.3e-006 7.2e-003 1.4e-005 5.77e-001 1.251352040e+001 1.251355067e+001 3.4e-009 3.92 50 1.2e-006 6.5e-003 1.2e-005 1.00e+000 1.251352493e+001 1.251355024e+001 3.0e-009 3.92 51 1.2e-006 6.3e-003 1.1e-005 1.72e+000 1.251352629e+001 1.251355037e+001 2.7e-009 3.92 52 1.5e-006 5.7e-003 1.1e-005 1.00e+000 1.251352408e+001 1.251354999e+001 2.5e-009 3.92 53 1.9e-006 5.1e-003 1.0e-005 -1.32e+000 1.251352442e+001 1.251355064e+001 2.2e-009 3.93 54 2.4e-006 4.6e-003 1.9e-005 1.00e+000 1.251350316e+001 1.251355023e+001 2.0e-009 3.93 55 1.2e-005 3.9e-003 1.6e-005 -2.02e-001 1.251351937e+001 1.251354718e+001 1.2e-009 3.93 56 4.9e-006 2.2e-004 4.2e-005 1.00e+000 1.251362079e+001 1.251354660e+001 6.6e-011 3.93 57 7.2e-006 1.9e-004 3.8e-005 2.77e+000 1.251360324e+001 1.251354658e+001 5.6e-011 3.93 58 1.1e-005 9.9e-007 4.3e-005 1.00e+000 1.251348313e+001 1.251354657e+001 3.0e-013 3.93 59 1.1e-005 9.0e-007 3.9e-005 -7.93e-001 1.251348139e+001 1.251354657e+001 2.7e-013 3.93 60 9.0e-006 8.1e-007 4.6e-005 1.00e+000 1.251346866e+001 1.251354657e+001 2.5e-013 3.93 61 7.8e-006 7.3e-007 4.2e-005 -5.29e+000 1.251345396e+001 1.251354657e+001 2.1e-013 3.93 62 6.7e-006 6.8e-007 3.9e-005 -2.44e+001 1.251348068e+001 1.251354657e+001 1.7e-013 3.95 63 6.1e-006 6.1e-007 3.5e-005 1.11e+000 1.251348521e+001 1.251354657e+001 1.7e-013 3.95 64 5.4e-006 5.5e-007 3.2e-005 -1.64e+000 1.251348428e+001 1.251354657e+001 1.5e-013 3.95 65 6.2e-006 5.0e-007 1.1e-005 1.00e+000 1.251352426e+001 1.251354657e+001 1.4e-013 3.95 66 5.6e-006 4.5e-007 1.0e-005 -1.25e+000 1.251352555e+001 1.251354657e+001 1.3e-013 3.95 67 5.2e-006 4.2e-007 1.2e-005 1.00e+000 1.251352268e+001 1.251354657e+001 1.2e-013 3.95 68 4.3e-006 3.8e-007 1.0e-005 1.45e+000 1.251352447e+001 1.251354657e+001 1.0e-013 3.95 69 4.2e-006 3.7e-007 1.1e-005 1.00e+000 1.251352299e+001 1.251354657e+001 1.0e-013 3.95 70 4.1e-006 3.6e-007 1.1e-005 5.69e-001 1.251352311e+001 1.251354657e+001 1.0e-013 3.96 71 4.1e-006 1.7e-005 9.8e-006 -1.52e+000 1.251352437e+001 1.251354657e+001 9.1e-014 3.96 72 6.2e-006 1.6e-005 4.8e-006 1.00e+000 1.251355739e+001 1.251354657e+001 8.5e-014 3.96 Interior-point optimizer terminated. Time: 3.98. Optimizer terminated. Time: 4.01 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.2513557388e+001 Viol. con: 8e-006 var: 0e+000 Dual. obj: 1.2513546570e+001 Viol. con: 0e+000 var: 9e-006 * End solution on dual form. * Transforming to primal solution. Solving took 4.06 seconds. result packing took 8.5% of solve time solution checking took 2.5% 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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 1029 Eliminator terminated. Eliminator started. Total number of eliminations : 1046 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1046 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 : 283 Optimizer - Cones : 0 Optimizer - Scalar variables : 992 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 : 0.00 Factor - nonzeros before factor : 6516 after factor : 1.06e+004 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.8e+003 7.6e+003 0.00e+000 -7.644377855e+003 1.023181539e-012 1.0e+000 0.05 1 7.5e+002 1.2e+003 2.5e+003 9.80e-002 -3.407479490e+003 9.786322781e+000 3.5e-001 0.16 2 3.9e+002 6.4e+002 1.3e+003 1.32e+000 -1.482252780e+003 1.282296595e+001 1.9e-001 0.22 3 2.8e+002 4.6e+002 9.5e+002 1.54e+000 -9.489377563e+002 1.334845838e+001 1.4e-001 0.23 4 8.5e+001 1.4e+002 2.9e+002 1.50e+000 -2.206898694e+002 1.377114935e+001 4.5e-002 0.37 5 2.7e+001 4.7e+001 9.4e+001 1.38e+000 -5.391233010e+001 1.255159156e+001 1.5e-002 0.44 6 7.2e+000 1.8e+001 2.5e+001 1.15e+000 -5.358283062e+000 1.118506736e+001 4.6e-003 0.47 7 1.9e+000 1.3e+001 6.8e+000 1.04e+000 6.211168094e+000 1.065374643e+001 1.4e-003 0.48 8 1.8e+000 1.2e+001 6.3e+000 8.06e-001 6.408062636e+000 1.064029175e+001 1.3e-003 0.62 9 8.0e-001 1.2e+001 2.8e+000 7.51e-001 8.166277151e+000 1.051014264e+001 6.0e-004 0.76 10 6.7e-001 9.7e+000 2.3e+000 3.05e-001 8.319313990e+000 1.048321199e+001 5.1e-004 0.87 11 2.1e-001 3.5e+000 7.8e-001 3.97e-001 9.318875654e+000 1.033893763e+001 2.0e-004 1.08 12 5.1e-002 3.6e+000 1.9e-001 7.03e-001 9.955777771e+000 1.024572658e+001 5.8e-005 1.22 13 1.6e-002 3.3e+000 6.2e-002 9.10e-001 1.012192801e+001 1.021849637e+001 2.0e-005 1.25 14 6.8e-003 2.6e+000 2.7e-002 9.70e-001 1.016844975e+001 1.021016384e+001 8.6e-006 1.29 15 3.1e-003 2.2e+000 1.2e-002 9.87e-001 1.018781555e+001 1.020660618e+001 3.9e-006 1.37 16 1.4e-003 2.0e+000 5.4e-003 9.94e-001 1.019655547e+001 1.020501152e+001 1.7e-006 1.54 17 5.1e-004 7.6e-001 2.0e-003 9.98e-001 1.020101403e+001 1.020419652e+001 6.6e-007 1.67 18 4.6e-004 6.9e-001 1.8e-003 9.99e-001 1.020130729e+001 1.020417886e+001 5.9e-007 1.69 19 4.2e-004 6.3e-001 1.6e-003 9.99e-001 1.020154344e+001 1.020412868e+001 5.3e-007 1.79 20 1.6e-004 2.5e-001 6.4e-004 9.99e-001 1.020285712e+001 1.020387174e+001 2.1e-007 1.86 21 1.5e-004 2.4e-001 5.8e-004 9.99e-001 1.020294071e+001 1.020385389e+001 1.9e-007 1.93 22 5.6e-005 9.0e-002 2.2e-004 9.99e-001 1.020341681e+001 1.020376350e+001 7.2e-008 2.00 23 5.0e-005 8.1e-002 2.0e-004 1.00e+000 1.020344540e+001 1.020375742e+001 6.4e-008 2.12 24 4.5e-005 7.3e-002 1.8e-004 1.00e+000 1.020347166e+001 1.020375248e+001 5.8e-008 2.23 25 4.1e-005 6.5e-002 1.6e-004 1.00e+000 1.020349530e+001 1.020374805e+001 5.2e-008 2.28 26 3.7e-005 5.9e-002 1.4e-004 1.00e+000 1.020351659e+001 1.020374406e+001 4.7e-008 2.31 27 3.3e-005 5.3e-002 1.3e-004 1.00e+000 1.020353575e+001 1.020374048e+001 4.2e-008 2.40 28 3.0e-005 4.8e-002 1.2e-004 1.00e+000 1.020355300e+001 1.020373726e+001 3.8e-008 2.43 29 2.7e-005 4.3e-002 1.1e-004 1.00e+000 1.020356853e+001 1.020373437e+001 3.4e-008 2.43 30 2.4e-005 3.9e-002 9.5e-005 1.00e+000 1.020358251e+001 1.020373177e+001 3.1e-008 2.43 31 2.2e-005 3.5e-002 8.5e-005 1.00e+000 1.020359510e+001 1.020372943e+001 2.8e-008 2.43 32 1.9e-005 3.1e-002 7.7e-005 1.00e+000 1.020360643e+001 1.020372733e+001 2.5e-008 2.43 33 3.9e-006 6.2e-003 1.5e-005 1.00e+000 1.020368827e+001 1.020371228e+001 5.0e-009 2.51 34 2.2e-007 3.5e-004 8.6e-007 1.00e+000 1.020370740e+001 1.020370875e+001 2.8e-010 2.71 35 1.2e-009 2.0e-006 5.2e-009 9.99e-001 1.020370853e+001 1.020370854e+001 1.9e-012 2.75 Interior-point optimizer terminated. Time: 2.75. Optimizer terminated. Time: 2.76 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0203708529e+001 Viol. con: 1e-009 var: 0e+000 Dual. obj: 1.0203708537e+001 Viol. con: 0e+000 var: 6e-007 * End solution on dual form. * Transforming to primal solution. Solving took 2.83 seconds. result packing took 7.2% of solve time solution checking took 2.7% 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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 1026 Eliminator terminated. Eliminator started. Total number of eliminations : 1043 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1043 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 : 286 Optimizer - Cones : 0 Optimizer - Scalar variables : 995 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 : 0.00 Factor - nonzeros before factor : 6557 after factor : 1.08e+004 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.5e+003 3.8e+003 7.6e+003 0.00e+000 -7.646714862e+003 1.023181539e-012 1.0e+000 0.03 1 7.9e+002 1.2e+003 2.4e+003 4.43e-003 -3.439952575e+003 9.865562227e+000 3.4e-001 0.08 2 5.5e+002 8.3e+002 1.7e+003 1.39e+000 -2.072270701e+003 1.199515898e+001 2.4e-001 0.08 3 2.4e+002 3.6e+002 7.4e+002 1.50e+000 -7.271016325e+002 1.390012391e+001 1.1e-001 0.09 4 7.2e+001 1.1e+002 2.2e+002 1.65e+000 -1.536459383e+002 1.372034682e+001 3.4e-002 0.13 5 1.9e+001 3.1e+001 5.8e+001 1.27e+000 -2.763449326e+001 1.211216782e+001 9.8e-003 0.28 6 4.5e+000 1.2e+001 1.4e+001 1.05e+000 1.436241441e+000 1.092816723e+001 2.7e-003 0.38 7 2.1e+000 1.1e+001 6.5e+000 9.71e-001 6.193049363e+000 1.068618402e+001 1.3e-003 0.42 8 1.9e+000 9.6e+000 5.9e+000 7.00e-001 6.369624443e+000 1.066665778e+001 1.2e-003 0.53 9 7.5e-001 7.8e+000 2.4e+000 6.46e-001 8.110266509e+000 1.049629801e+001 5.4e-004 0.59 10 6.1e-001 6.3e+000 1.9e+000 5.13e-001 8.387127068e+000 1.045979738e+001 4.3e-004 0.73 11 1.9e-001 3.0e+000 6.4e-001 5.08e-001 9.417596456e+000 1.031757308e+001 1.6e-004 0.83 12 8.2e-002 3.1e+000 2.7e-001 7.46e-001 9.843807193e+000 1.025740524e+001 7.4e-005 0.86 13 7.4e-002 2.8e+000 2.5e-001 8.54e-001 9.883252334e+000 1.025562207e+001 6.6e-005 0.91 14 6.6e-002 2.6e+000 2.2e-001 8.50e-001 9.912634735e+000 1.025014228e+001 6.0e-005 0.91 15 6.0e-002 2.3e+000 2.0e-001 8.61e-001 9.939032191e+000 1.024491251e+001 5.4e-005 0.92 16 5.4e-002 2.1e+000 1.8e-001 8.72e-001 9.963014707e+000 1.024007336e+001 4.8e-005 0.95 17 4.8e-002 1.9e+000 1.6e-001 8.83e-001 9.984805103e+000 1.023562274e+001 4.4e-005 0.98 18 4.4e-002 1.8e+000 1.5e-001 8.93e-001 1.000459315e+001 1.023153905e+001 3.9e-005 1.00 19 3.9e-002 1.6e+000 1.3e-001 9.03e-001 1.002254923e+001 1.022779861e+001 3.5e-005 1.00 20 3.5e-002 1.5e+000 1.2e-001 9.12e-001 1.003883134e+001 1.022437779e+001 3.2e-005 1.00 21 3.2e-002 1.3e+000 1.1e-001 9.20e-001 1.005358583e+001 1.022125374e+001 2.9e-005 1.01 22 2.9e-002 1.2e+000 9.6e-002 9.27e-001 1.006694796e+001 1.021840448e+001 2.6e-005 1.03 23 2.6e-002 1.1e+000 8.6e-002 9.34e-001 1.007904246e+001 1.021580901e+001 2.3e-005 1.04 24 2.3e-002 1.0e+000 7.8e-002 9.40e-001 1.008998405e+001 1.021344739e+001 2.1e-005 1.04 25 2.1e-002 9.6e-001 7.0e-002 9.45e-001 1.009987804e+001 1.021130074e+001 1.9e-005 1.06 26 1.9e-002 8.8e-001 6.3e-002 9.51e-001 1.010882094e+001 1.020935131e+001 1.7e-005 1.08 27 1.7e-002 8.1e-001 5.7e-002 9.55e-001 1.011690101e+001 1.020758249e+001 1.5e-005 1.08 28 1.5e-002 7.5e-001 5.1e-002 9.60e-001 1.012419893e+001 1.020597879e+001 1.4e-005 1.09 29 1.4e-002 7.0e-001 4.6e-002 9.64e-001 1.013078829e+001 1.020452587e+001 1.2e-005 1.11 30 1.2e-002 6.5e-001 4.1e-002 9.67e-001 1.013673619e+001 1.020321045e+001 1.1e-005 1.12 31 1.1e-002 6.0e-001 3.7e-002 9.70e-001 1.014210369e+001 1.020202031e+001 1.0e-005 1.12 32 1.0e-002 5.6e-001 3.3e-002 9.73e-001 1.014694632e+001 1.020094419e+001 9.1e-006 1.16 33 9.0e-003 5.2e-001 3.0e-002 9.76e-001 1.015131455e+001 1.019997176e+001 8.2e-006 1.19 34 8.1e-003 4.9e-001 2.7e-002 9.79e-001 1.015525414e+001 1.019909353e+001 7.3e-006 1.22 35 7.3e-003 4.6e-001 2.4e-002 9.81e-001 1.015880661e+001 1.019830080e+001 6.6e-006 1.23 36 6.5e-003 4.3e-001 2.2e-002 9.83e-001 1.016200956e+001 1.019758563e+001 5.9e-006 1.25 37 5.9e-003 4.1e-001 2.0e-002 9.85e-001 1.016489702e+001 1.019694074e+001 5.4e-006 1.26 38 5.3e-003 3.8e-001 1.8e-002 9.86e-001 1.016749981e+001 1.019635950e+001 4.8e-006 1.28 39 4.8e-003 3.6e-001 1.6e-002 9.88e-001 1.016984575e+001 1.019583583e+001 4.3e-006 1.29 40 4.3e-003 3.5e-001 1.4e-002 9.89e-001 1.017196002e+001 1.019536423e+001 3.9e-006 1.34 41 3.9e-003 3.3e-001 1.3e-002 9.90e-001 1.017386533e+001 1.019493965e+001 3.5e-006 1.36 42 3.5e-003 3.1e-001 1.2e-002 9.91e-001 1.017558223e+001 1.019455753e+001 3.2e-006 1.37 43 3.1e-003 3.0e-001 1.1e-002 9.92e-001 1.017712921e+001 1.019421371e+001 2.8e-006 1.39 44 2.8e-003 2.9e-001 9.5e-003 9.93e-001 1.017852301e+001 1.019390440e+001 2.6e-006 1.40 45 2.5e-003 2.8e-001 8.5e-003 9.94e-001 1.017977869e+001 1.019362619e+001 2.3e-006 1.40 46 2.3e-003 2.7e-001 7.7e-003 9.95e-001 1.018090986e+001 1.019337598e+001 2.1e-006 1.40 47 2.1e-003 2.6e-001 6.9e-003 9.95e-001 1.018192881e+001 1.019315097e+001 1.9e-006 1.40 48 1.8e-003 2.5e-001 6.2e-003 9.96e-001 1.018284659e+001 1.019294863e+001 1.7e-006 1.42 49 1.7e-003 2.4e-001 5.6e-003 9.96e-001 1.018367322e+001 1.019276668e+001 1.5e-006 1.42 50 1.5e-003 2.4e-001 5.0e-003 9.97e-001 1.018441768e+001 1.019260308e+001 1.4e-006 1.76 51 1.3e-003 2.3e-001 4.5e-003 9.97e-001 1.018508813e+001 1.019245598e+001 1.2e-006 1.98 52 1.2e-003 2.3e-001 4.1e-003 9.98e-001 1.018569189e+001 1.019232373e+001 1.1e-006 1.98 53 1.1e-003 2.2e-001 3.7e-003 9.98e-001 1.018623558e+001 1.019220482e+001 9.9e-007 1.98 54 9.8e-004 2.2e-001 3.3e-003 9.98e-001 1.018672516e+001 1.019209793e+001 8.9e-007 1.98 55 8.8e-004 2.1e-001 3.0e-003 9.98e-001 1.018716601e+001 1.019200184e+001 8.1e-007 2.00 56 7.9e-004 2.1e-001 2.7e-003 9.99e-001 1.018756297e+001 1.019191547e+001 7.2e-007 2.00 57 7.2e-004 2.1e-001 2.4e-003 9.99e-001 1.018792040e+001 1.019183784e+001 6.5e-007 2.00 58 6.4e-004 2.0e-001 2.2e-003 9.99e-001 1.018824225e+001 1.019176809e+001 5.9e-007 2.01 59 5.8e-004 2.0e-001 1.9e-003 9.99e-001 1.018853206e+001 1.019170541e+001 5.3e-007 2.01 60 5.2e-004 2.0e-001 1.8e-003 1.00e+000 1.018879302e+001 1.019164910e+001 4.8e-007 2.01 61 4.7e-004 2.0e-001 1.6e-003 1.00e+000 1.018902799e+001 1.019159851e+001 4.3e-007 2.01 62 4.2e-004 1.9e-001 1.4e-003 1.00e+000 1.018923958e+001 1.019155307e+001 3.9e-007 2.01 63 3.8e-004 1.9e-001 1.3e-003 1.00e+000 1.018943010e+001 1.019151226e+001 3.5e-007 2.01 64 3.4e-004 1.9e-001 1.2e-003 1.00e+000 1.018960165e+001 1.019147560e+001 3.1e-007 2.01 65 3.1e-004 1.9e-001 1.0e-003 1.00e+000 1.018975612e+001 1.019144267e+001 2.8e-007 2.01 66 2.8e-004 1.9e-001 9.3e-004 1.00e+000 1.018989520e+001 1.019141310e+001 2.5e-007 2.03 67 2.5e-004 1.9e-001 8.4e-004 1.00e+000 1.019002042e+001 1.019138652e+001 2.3e-007 2.03 68 2.2e-004 1.8e-001 7.6e-004 1.00e+000 1.019013317e+001 1.019136265e+001 2.0e-007 2.03 69 2.0e-004 1.8e-001 6.8e-004 1.00e+000 1.019023469e+001 1.019134121e+001 1.8e-007 2.03 70 1.8e-004 1.8e-001 6.1e-004 1.00e+000 1.019032609e+001 1.019132195e+001 1.7e-007 2.03 71 1.6e-004 1.8e-001 5.5e-004 1.00e+000 1.019040838e+001 1.019130464e+001 1.5e-007 2.03 72 1.5e-004 1.8e-001 5.0e-004 1.00e+000 1.019048247e+001 1.019128910e+001 1.3e-007 2.03 73 1.3e-004 1.8e-001 4.5e-004 1.00e+000 1.019054918e+001 1.019127513e+001 1.2e-007 2.04 74 1.2e-004 1.8e-001 4.0e-004 1.00e+000 1.019060924e+001 1.019126259e+001 1.1e-007 2.04 75 1.1e-004 1.8e-001 3.6e-004 1.00e+000 1.019066331e+001 1.019125132e+001 9.8e-008 2.04 76 9.7e-005 1.8e-001 3.3e-004 1.00e+000 1.019071200e+001 1.019124120e+001 8.8e-008 2.04 77 8.7e-005 1.8e-001 2.9e-004 1.00e+000 1.019075584e+001 1.019123212e+001 7.9e-008 2.04 78 7.8e-005 1.8e-001 2.6e-004 1.00e+000 1.019079531e+001 1.019122395e+001 7.1e-008 2.04 79 7.0e-005 1.8e-001 2.4e-004 1.00e+000 1.019083085e+001 1.019121662e+001 6.4e-008 2.04 80 6.3e-005 1.8e-001 2.1e-004 1.00e+000 1.019086285e+001 1.019121004e+001 5.8e-008 2.04 81 5.7e-005 1.8e-001 1.9e-004 1.00e+000 1.019089166e+001 1.019120413e+001 5.2e-008 2.04 82 5.1e-005 1.8e-001 1.7e-004 1.00e+000 1.019091760e+001 1.019119882e+001 4.7e-008 2.06 83 4.6e-005 1.8e-001 1.6e-004 1.00e+000 1.019094096e+001 1.019119405e+001 4.2e-008 2.06 84 4.2e-005 1.8e-001 1.4e-004 1.00e+000 1.019096199e+001 1.019118977e+001 3.8e-008 2.06 85 3.7e-005 1.8e-001 1.3e-004 1.00e+000 1.019098092e+001 1.019118592e+001 3.4e-008 2.06 86 3.4e-005 1.8e-001 1.1e-004 1.00e+000 1.019099797e+001 1.019118247e+001 3.1e-008 2.06 87 3.0e-005 1.7e-001 1.0e-004 1.00e+000 1.019101332e+001 1.019117936e+001 2.8e-008 2.06 88 2.7e-005 1.7e-001 9.2e-005 1.00e+000 1.019102713e+001 1.019117657e+001 2.5e-008 2.06 89 2.5e-005 1.7e-001 8.3e-005 1.00e+000 1.019103957e+001 1.019117407e+001 2.2e-008 2.08 90 2.2e-005 1.7e-001 7.4e-005 1.00e+000 1.019105077e+001 1.019117181e+001 2.0e-008 2.08 91 2.0e-005 1.7e-001 6.7e-005 1.00e+000 1.019106084e+001 1.019116979e+001 1.8e-008 2.08 92 1.8e-005 1.7e-001 6.0e-005 1.00e+000 1.019106992e+001 1.019116796e+001 1.6e-008 2.08 93 1.6e-005 1.7e-001 5.4e-005 1.00e+000 1.019107809e+001 1.019116633e+001 1.5e-008 2.08 94 1.4e-005 1.7e-001 4.9e-005 1.00e+000 1.019108544e+001 1.019116485e+001 1.3e-008 2.08 95 1.3e-005 1.7e-001 4.4e-005 1.00e+000 1.019109206e+001 1.019116353e+001 1.2e-008 2.08 96 1.2e-005 1.7e-001 4.0e-005 1.00e+000 1.019109801e+001 1.019116234e+001 1.1e-008 2.09 97 1.1e-005 1.7e-001 3.6e-005 1.00e+000 1.019110338e+001 1.019116127e+001 9.7e-009 2.09 98 9.5e-006 1.7e-001 3.2e-005 1.00e+000 1.019110820e+001 1.019116031e+001 8.7e-009 2.09 99 8.6e-006 1.7e-001 2.9e-005 1.00e+000 1.019111255e+001 1.019115944e+001 7.8e-009 2.09 100 7.7e-006 1.7e-001 2.6e-005 1.00e+000 1.019111646e+001 1.019115866e+001 7.0e-009 2.09 101 6.9e-006 1.7e-001 2.3e-005 1.00e+000 1.019111998e+001 1.019115796e+001 6.3e-009 2.11 102 6.2e-006 1.7e-001 2.1e-005 1.00e+000 1.019112315e+001 1.019115733e+001 5.7e-009 2.11 103 5.6e-006 1.7e-001 1.9e-005 1.00e+000 1.019112600e+001 1.019115677e+001 5.1e-009 2.11 104 5.1e-006 1.7e-001 1.7e-005 1.00e+000 1.019112857e+001 1.019115626e+001 4.6e-009 2.11 105 4.5e-006 1.7e-001 1.5e-005 1.00e+000 1.019113088e+001 1.019115580e+001 4.2e-009 2.11 106 4.1e-006 1.7e-001 1.4e-005 1.00e+000 1.019113296e+001 1.019115539e+001 3.7e-009 2.11 107 3.7e-006 1.7e-001 1.2e-005 1.00e+000 1.019113483e+001 1.019115501e+001 3.4e-009 2.11 108 3.3e-006 1.7e-001 1.1e-005 1.00e+000 1.019113651e+001 1.019115468e+001 3.0e-009 2.11 109 3.0e-006 1.7e-001 1.0e-005 1.00e+000 1.019113803e+001 1.019115438e+001 2.7e-009 2.12 110 2.7e-006 1.7e-001 9.0e-006 1.00e+000 1.019113940e+001 1.019115411e+001 2.5e-009 2.12 111 2.4e-006 1.7e-001 8.1e-006 1.00e+000 1.019114062e+001 1.019115387e+001 2.2e-009 2.12 112 2.2e-006 1.7e-001 7.3e-006 1.00e+000 1.019114173e+001 1.019115365e+001 2.0e-009 2.12 113 2.0e-006 1.7e-001 6.6e-006 9.99e-001 1.019114273e+001 1.019115345e+001 1.8e-009 2.12 114 1.8e-006 1.7e-001 5.9e-006 1.00e+000 1.019114362e+001 1.019115328e+001 1.6e-009 2.12 115 1.6e-006 1.7e-001 5.3e-006 1.00e+000 1.019114443e+001 1.019115312e+001 1.4e-009 2.12 116 1.4e-006 1.5e-001 4.8e-006 1.00e+000 1.019114515e+001 1.019115297e+001 1.3e-009 2.12 117 1.3e-006 1.4e-001 4.3e-006 1.00e+000 1.019114581e+001 1.019115284e+001 1.2e-009 2.14 118 1.2e-006 1.3e-001 3.9e-006 1.00e+000 1.019114639e+001 1.019115273e+001 1.1e-009 2.14 119 1.0e-006 1.1e-001 3.5e-006 1.00e+000 1.019114692e+001 1.019115262e+001 9.5e-010 2.14 120 9.4e-007 1.0e-001 3.2e-006 1.00e+000 1.019114740e+001 1.019115253e+001 8.6e-010 2.14 121 8.4e-007 9.1e-002 2.8e-006 1.00e+000 1.019114783e+001 1.019115245e+001 7.7e-010 2.14 122 7.6e-007 8.2e-002 2.6e-006 1.00e+000 1.019114821e+001 1.019115237e+001 6.9e-010 2.14 123 6.8e-007 7.4e-002 2.3e-006 1.00e+000 1.019114856e+001 1.019115230e+001 6.2e-010 2.14 124 6.1e-007 6.7e-002 2.1e-006 1.00e+000 1.019114888e+001 1.019115224e+001 5.6e-010 2.14 125 5.5e-007 6.0e-002 1.9e-006 9.99e-001 1.019114916e+001 1.019115218e+001 5.1e-010 2.15 126 5.0e-007 5.4e-002 1.7e-006 1.00e+000 1.019114941e+001 1.019115213e+001 4.6e-010 2.15 127 4.5e-007 4.9e-002 1.5e-006 1.00e+000 1.019114964e+001 1.019115209e+001 4.1e-010 2.15 128 4.0e-007 4.4e-002 1.4e-006 1.00e+000 1.019114984e+001 1.019115205e+001 3.7e-010 2.15 129 3.6e-007 3.9e-002 1.2e-006 9.98e-001 1.019115003e+001 1.019115201e+001 3.3e-010 2.15 130 3.3e-007 3.5e-002 1.1e-006 1.00e+000 1.019115020e+001 1.019115198e+001 3.0e-010 2.15 131 2.9e-007 3.2e-002 9.9e-007 9.93e-001 1.019115034e+001 1.019115195e+001 2.7e-010 2.15 132 2.6e-007 2.9e-002 8.9e-007 1.00e+000 1.019115048e+001 1.019115192e+001 2.4e-010 2.15 133 2.4e-007 2.6e-002 8.0e-007 1.01e+000 1.019115061e+001 1.019115190e+001 2.2e-010 2.17 134 2.1e-007 2.3e-002 7.2e-007 1.01e+000 1.019115072e+001 1.019115188e+001 2.0e-010 2.17 135 1.9e-007 2.1e-002 6.5e-007 1.00e+000 1.019115081e+001 1.019115186e+001 1.8e-010 2.17 136 1.7e-007 1.9e-002 5.8e-007 9.95e-001 1.019115090e+001 1.019115184e+001 1.6e-010 2.17 137 1.6e-007 1.7e-002 5.3e-007 9.90e-001 1.019115098e+001 1.019115183e+001 1.4e-010 2.17 138 1.4e-007 1.5e-002 4.7e-007 1.01e+000 1.019115105e+001 1.019115181e+001 1.3e-010 2.17 139 1.3e-007 1.4e-002 4.3e-007 9.98e-001 1.019115112e+001 1.019115180e+001 1.2e-010 2.17 140 7.3e-009 7.8e-004 2.4e-008 9.86e-001 1.019115165e+001 1.019115169e+001 7.8e-012 2.18 141 1.0e-009 7.1e-005 2.2e-009 1.03e+000 1.019115168e+001 1.019115169e+001 4.9e-013 2.18 Interior-point optimizer terminated. Time: 2.18. Optimizer terminated. Time: 2.21 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0191151683e+001 Viol. con: 9e-010 var: 0e+000 Dual. obj: 1.0191151687e+001 Viol. con: 0e+000 var: 2e-005 * End solution on dual form. * Transforming to primal solution. Solving took 2.25 seconds. result packing took 6.4% of solve time solution checking took 2.8% 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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 1026 Eliminator terminated. Eliminator started. Total number of eliminations : 1041 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1041 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 : 286 Optimizer - Cones : 0 Optimizer - Scalar variables : 995 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 : 6535 after factor : 1.08e+004 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.7e+003 3.7e+003 5.3e+003 0.00e+000 -5.296203327e+003 1.023181539e-012 1.0e+000 0.05 1 8.5e+002 1.2e+003 1.7e+003 1.11e-003 -2.376466465e+003 9.885579008e+000 3.4e-001 0.06 2 5.9e+002 8.0e+002 1.1e+003 1.39e+000 -1.418154302e+003 1.205994462e+001 2.3e-001 0.06 3 2.2e+002 3.0e+002 4.4e+002 1.52e+000 -4.109293410e+002 1.409921579e+001 9.3e-002 0.06 4 6.6e+001 9.0e+001 1.3e+002 1.67e+000 -8.391618411e+001 1.359200781e+001 2.9e-002 0.06 5 1.6e+001 2.6e+001 3.3e+001 1.21e+000 -1.082885659e+001 1.187819345e+001 8.2e-003 0.06 6 5.3e+000 1.6e+001 1.1e+001 1.04e+000 3.446469530e+000 1.095661017e+001 2.9e-003 0.08 7 2.2e+000 1.3e+001 4.5e+000 9.90e-001 7.495553694e+000 1.065234054e+001 1.3e-003 0.08 8 2.0e+000 1.2e+001 4.1e+000 7.11e-001 7.616682164e+000 1.063384177e+001 1.2e-003 0.08 9 7.6e-001 9.1e+000 1.6e+000 6.62e-001 8.866438864e+000 1.045993682e+001 5.1e-004 0.08 10 5.3e-001 8.9e+000 1.1e+000 5.22e-001 9.162400212e+000 1.040172459e+001 3.6e-004 0.08 11 1.8e-001 3.8e+000 4.0e-001 5.32e-001 9.723482693e+000 1.028165187e+001 1.4e-004 0.08 12 6.7e-002 3.7e+000 1.5e-001 7.74e-001 9.991214908e+000 1.022240937e+001 5.8e-005 0.09 13 1.4e-002 3.4e+000 3.5e-002 8.82e-001 1.012712623e+001 1.018244533e+001 1.5e-005 0.09 14 5.6e-003 3.0e+000 1.4e-002 9.81e-001 1.015355874e+001 1.017529210e+001 5.9e-006 0.09 15 1.8e-003 2.6e+000 4.4e-003 9.93e-001 1.016475454e+001 1.017187031e+001 1.9e-006 0.09 16 6.2e-004 2.4e+000 1.5e-003 9.98e-001 1.016836776e+001 1.017080165e+001 6.7e-007 0.09 17 2.8e-004 2.0e+000 6.9e-004 1.00e+000 1.016940727e+001 1.017050966e+001 3.0e-007 0.09 18 1.1e-004 1.9e+000 2.8e-004 1.00e+000 1.016991435e+001 1.017036554e+001 1.2e-007 0.11 19 1.0e-004 1.8e+000 2.5e-004 1.00e+000 1.016994971e+001 1.017035650e+001 1.1e-007 0.11 20 9.3e-005 1.7e+000 2.3e-004 1.00e+000 1.016998105e+001 1.017034723e+001 1.0e-007 0.11 21 8.3e-005 1.5e+000 2.1e-004 1.00e+000 1.017000949e+001 1.017033905e+001 9.1e-008 0.11 22 7.5e-005 1.4e+000 1.8e-004 1.00e+000 1.017003509e+001 1.017033169e+001 8.2e-008 0.13 23 6.7e-005 1.3e+000 1.7e-004 1.00e+000 1.017005814e+001 1.017032508e+001 7.3e-008 0.13 24 6.1e-005 1.2e+000 1.5e-004 1.00e+000 1.017007890e+001 1.017031914e+001 6.6e-008 0.13 25 5.5e-005 1.1e+000 1.3e-004 1.00e+000 1.017009760e+001 1.017031381e+001 5.9e-008 0.13 26 4.9e-005 9.7e-001 1.2e-004 1.00e+000 1.017011443e+001 1.017030902e+001 5.4e-008 0.13 27 4.4e-005 8.9e-001 1.1e-004 1.00e+000 1.017012958e+001 1.017030471e+001 4.8e-008 0.14 28 4.0e-005 8.2e-001 9.8e-005 1.00e+000 1.017014322e+001 1.017030084e+001 4.3e-008 0.14 29 3.6e-005 7.6e-001 8.8e-005 1.00e+000 1.017015550e+001 1.017029736e+001 3.9e-008 0.14 30 3.2e-005 7.0e-001 8.0e-005 1.00e+000 1.017016656e+001 1.017029423e+001 3.5e-008 0.14 31 2.9e-005 6.5e-001 7.2e-005 1.00e+000 1.017017652e+001 1.017029142e+001 3.2e-008 0.14 32 2.6e-005 6.0e-001 6.4e-005 1.00e+000 1.017018548e+001 1.017028889e+001 2.8e-008 0.16 33 2.4e-005 5.6e-001 5.8e-005 1.00e+000 1.017019354e+001 1.017028661e+001 2.6e-008 0.16 34 2.1e-005 5.2e-001 5.2e-005 1.00e+000 1.017020081e+001 1.017028457e+001 2.3e-008 0.16 35 1.9e-005 4.9e-001 4.7e-005 1.00e+000 1.017020734e+001 1.017028273e+001 2.1e-008 0.16 36 1.7e-005 4.5e-001 4.2e-005 1.00e+000 1.017021323e+001 1.017028108e+001 1.9e-008 0.17 37 1.5e-005 4.3e-001 3.8e-005 1.00e+000 1.017021853e+001 1.017027959e+001 1.7e-008 0.17 38 1.4e-005 4.0e-001 3.4e-005 1.00e+000 1.017022329e+001 1.017027825e+001 1.5e-008 0.17 39 1.3e-005 3.8e-001 3.1e-005 1.00e+000 1.017022759e+001 1.017027705e+001 1.4e-008 0.17 40 1.1e-005 3.6e-001 2.8e-005 1.00e+000 1.017023145e+001 1.017027596e+001 1.2e-008 0.17 41 1.0e-005 3.4e-001 2.5e-005 1.00e+000 1.017023493e+001 1.017027499e+001 1.1e-008 0.19 42 9.1e-006 3.2e-001 2.2e-005 1.00e+000 1.017023806e+001 1.017027411e+001 9.9e-009 0.19 43 8.2e-006 3.1e-001 2.0e-005 1.00e+000 1.017024087e+001 1.017027332e+001 8.9e-009 0.19 44 7.4e-006 3.0e-001 1.8e-005 1.00e+000 1.017024341e+001 1.017027261e+001 8.0e-009 0.19 45 6.6e-006 2.9e-001 1.6e-005 1.00e+000 1.017024569e+001 1.017027198e+001 7.2e-009 0.19 46 6.0e-006 2.7e-001 1.5e-005 1.00e+000 1.017024774e+001 1.017027140e+001 6.5e-009 0.19 47 5.4e-006 2.7e-001 1.3e-005 1.00e+000 1.017024959e+001 1.017027088e+001 5.9e-009 0.20 48 4.8e-006 2.6e-001 1.2e-005 1.00e+000 1.017025125e+001 1.017027042e+001 5.3e-009 0.20 49 4.4e-006 2.5e-001 1.1e-005 1.00e+000 1.017025275e+001 1.017027000e+001 4.7e-009 0.20 50 3.9e-006 2.4e-001 9.7e-006 1.00e+000 1.017025410e+001 1.017026962e+001 4.3e-009 0.20 51 3.5e-006 2.4e-001 8.7e-006 1.00e+000 1.017025531e+001 1.017026928e+001 3.8e-009 0.20 52 3.2e-006 2.3e-001 7.8e-006 1.00e+000 1.017025640e+001 1.017026898e+001 3.5e-009 0.20 53 2.9e-006 2.2e-001 7.0e-006 1.00e+000 1.017025739e+001 1.017026870e+001 3.1e-009 0.22 54 2.6e-006 2.2e-001 6.3e-006 9.99e-001 1.017025827e+001 1.017026845e+001 2.8e-009 0.22 55 2.3e-006 2.2e-001 5.7e-006 1.00e+000 1.017025906e+001 1.017026823e+001 2.5e-009 0.22 56 2.1e-006 2.1e-001 5.1e-006 9.99e-001 1.017025978e+001 1.017026803e+001 2.3e-009 0.22 57 1.9e-006 2.1e-001 4.6e-006 1.00e+000 1.017026042e+001 1.017026785e+001 2.0e-009 0.22 58 1.7e-006 2.1e-001 4.2e-006 1.00e+000 1.017026100e+001 1.017026769e+001 1.8e-009 0.22 59 1.5e-006 2.0e-001 3.7e-006 1.00e+000 1.017026153e+001 1.017026754e+001 1.7e-009 0.22 60 1.4e-006 2.0e-001 3.4e-006 1.00e+000 1.017026200e+001 1.017026741e+001 1.5e-009 0.23 61 1.2e-006 2.0e-001 3.0e-006 9.98e-001 1.017026242e+001 1.017026729e+001 1.3e-009 0.23 62 1.1e-006 2.0e-001 2.7e-006 1.00e+000 1.017026280e+001 1.017026718e+001 1.2e-009 0.23 63 1.0e-006 2.0e-001 2.5e-006 1.00e+000 1.017026314e+001 1.017026709e+001 1.1e-009 0.23 64 9.0e-007 1.9e-001 2.2e-006 9.99e-001 1.017026345e+001 1.017026700e+001 9.8e-010 0.23 65 8.1e-007 1.9e-001 2.0e-006 1.00e+000 1.017026372e+001 1.017026692e+001 8.8e-010 0.23 66 7.3e-007 1.9e-001 1.8e-006 1.00e+000 1.017026397e+001 1.017026685e+001 7.9e-010 0.23 67 6.5e-007 1.9e-001 1.6e-006 1.00e+000 1.017026420e+001 1.017026679e+001 7.1e-010 0.25 68 5.9e-007 1.9e-001 1.5e-006 1.00e+000 1.017026440e+001 1.017026673e+001 6.4e-010 0.25 69 5.3e-007 1.9e-001 1.3e-006 1.00e+000 1.017026458e+001 1.017026668e+001 5.8e-010 0.25 70 4.8e-007 1.9e-001 1.2e-006 9.99e-001 1.017026475e+001 1.017026663e+001 5.2e-010 0.25 71 4.3e-007 1.9e-001 1.1e-006 1.00e+000 1.017026489e+001 1.017026659e+001 4.7e-010 0.25 72 3.9e-007 1.9e-001 9.5e-007 9.95e-001 1.017026503e+001 1.017026655e+001 4.2e-010 0.25 73 3.5e-007 1.7e-001 8.6e-007 1.01e+000 1.017026515e+001 1.017026652e+001 3.8e-010 0.25 74 3.1e-007 1.5e-001 7.7e-007 9.96e-001 1.017026526e+001 1.017026649e+001 3.4e-010 0.27 75 2.8e-007 1.4e-001 6.9e-007 1.01e+000 1.017026536e+001 1.017026646e+001 3.1e-010 0.27 76 2.5e-007 1.2e-001 6.2e-007 1.01e+000 1.017026545e+001 1.017026644e+001 2.8e-010 0.27 77 2.3e-007 1.1e-001 5.6e-007 1.01e+000 1.017026553e+001 1.017026641e+001 2.5e-010 0.27 78 4.6e-008 2.2e-002 1.1e-007 9.96e-001 1.017026608e+001 1.017026626e+001 5.1e-011 0.27 79 7.1e-009 3.4e-003 1.7e-008 1.10e+000 1.017026620e+001 1.017026622e+001 6.2e-012 0.27 80 4.3e-010 2.0e-004 1.0e-009 9.52e-001 1.017026622e+001 1.017026622e+001 5.3e-013 0.27 Interior-point optimizer terminated. Time: 0.28. Optimizer terminated. Time: 0.31 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0170266217e+001 Viol. con: 4e-010 var: 0e+000 Dual. obj: 1.0170266218e+001 Viol. con: 0e+000 var: 5e-005 * End solution on dual form. * Transforming to primal solution. Solving took 0.331 seconds. result packing took 45% 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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 1026 Eliminator terminated. Eliminator started. Total number of eliminations : 1039 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1039 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 : 286 Optimizer - Cones : 0 Optimizer - Scalar variables : 995 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 : 6535 after factor : 1.08e+004 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.7e+003 3.8e+003 5.1e+003 0.00e+000 -5.147026235e+003 1.023181539e-012 1.0e+000 0.05 1 8.5e+002 1.2e+003 1.6e+003 7.47e-004 -2.308564063e+003 9.891749917e+000 3.4e-001 0.06 2 3.9e+002 5.3e+002 7.4e+002 1.39e+000 -8.486137036e+002 1.339127375e+001 1.6e-001 0.06 3 8.7e+001 1.2e+002 1.7e+002 1.69e+000 -1.251202023e+002 1.420957845e+001 3.9e-002 0.06 4 2.9e+001 4.0e+001 5.7e+001 1.26e+000 -3.003042283e+001 1.274778969e+001 1.4e-002 0.06 5 7.7e+000 1.5e+001 1.6e+001 1.11e+000 -1.140988973e-001 1.127786265e+001 4.3e-003 0.06 6 3.0e+000 7.8e+000 6.1e+000 1.00e+000 6.305847140e+000 1.079857353e+001 1.8e-003 0.08 7 1.4e+000 9.5e+000 2.8e+000 9.00e-001 8.318995878e+000 1.059239760e+001 8.6e-004 0.08 8 1.2e+000 8.6e+000 2.5e+000 5.16e-001 8.389418060e+000 1.057149654e+001 7.8e-004 0.08 9 1.2e+000 8.0e+000 2.4e+000 5.12e-001 8.271488089e+000 1.055681824e+001 7.3e-004 0.08 10 3.7e-001 7.3e+000 7.9e-001 5.85e-001 9.398191453e+000 1.036554987e+001 2.7e-004 0.08 11 2.8e-001 5.6e+000 6.1e-001 5.74e-001 9.538777897e+000 1.033335844e+001 2.1e-004 0.09 12 5.5e-002 3.7e+000 1.3e-001 6.40e-001 1.001181175e+001 1.021636790e+001 5.6e-005 0.09 13 1.9e-002 3.2e+000 4.6e-002 9.09e-001 1.011275545e+001 1.018712174e+001 2.0e-005 0.11 14 8.6e-003 3.2e+000 2.1e-002 9.74e-001 1.014424368e+001 1.017849761e+001 9.5e-006 0.11 15 2.5e-003 2.7e+000 6.2e-003 9.87e-001 1.016233738e+001 1.017251252e+001 2.9e-006 0.11 16 7.4e-004 2.6e+000 1.8e-003 9.96e-001 1.016776309e+001 1.017077423e+001 8.5e-007 0.11 17 2.4e-004 2.5e+000 6.1e-004 9.98e-001 1.016930441e+001 1.017030515e+001 2.8e-007 0.11 18 7.4e-005 2.5e+000 1.9e-004 9.97e-001 1.016983904e+001 1.017014294e+001 8.7e-008 0.11 19 5.6e-005 1.9e+000 1.4e-004 9.49e-001 1.016988826e+001 1.017013795e+001 6.6e-008 0.13 20 5.6e-005 1.9e+000 1.4e-004 -4.05e-001 1.016988615e+001 1.017014314e+001 6.6e-008 0.13 21 5.3e-005 1.9e+000 1.3e-004 -2.34e-001 1.016988079e+001 1.017016844e+001 6.3e-008 0.13 22 4.8e-005 1.9e+000 1.2e-004 9.62e-001 1.016991484e+001 1.017014862e+001 5.7e-008 0.13 23 2.5e-005 1.3e+000 6.7e-005 5.25e-001 1.017001256e+001 1.017015601e+001 3.0e-008 0.13 24 2.5e-005 1.3e+000 6.7e-005 -9.93e-002 1.017001261e+001 1.017015590e+001 3.0e-008 0.13 25 2.5e-005 1.3e+000 6.7e-005 -9.67e-002 1.017001266e+001 1.017015578e+001 3.0e-008 0.14 26 2.5e-005 1.3e+000 6.7e-005 -9.42e-002 1.017001270e+001 1.017015567e+001 3.0e-008 0.14 27 2.5e-005 1.3e+000 6.7e-005 -9.19e-002 1.017001275e+001 1.017015556e+001 3.0e-008 0.14 28 2.5e-005 1.3e+000 6.7e-005 -8.97e-002 1.017001280e+001 1.017015545e+001 3.0e-008 0.14 29 2.5e-005 1.3e+000 6.7e-005 -8.76e-002 1.017001285e+001 1.017015534e+001 3.0e-008 0.14 30 2.5e-005 1.3e+000 6.7e-005 -8.55e-002 1.017001289e+001 1.017015523e+001 3.0e-008 0.16 31 2.5e-005 1.3e+000 6.7e-005 -8.36e-002 1.017001294e+001 1.017015512e+001 3.0e-008 0.16 32 2.5e-005 1.3e+000 6.7e-005 -8.18e-002 1.017001299e+001 1.017015501e+001 3.0e-008 0.16 33 2.5e-005 1.3e+000 6.7e-005 -8.00e-002 1.017001303e+001 1.017015490e+001 3.0e-008 0.16 34 2.5e-005 1.3e+000 6.7e-005 -7.83e-002 1.017001308e+001 1.017015479e+001 3.0e-008 0.16 35 2.5e-005 1.3e+000 6.7e-005 -7.67e-002 1.017001313e+001 1.017015469e+001 3.0e-008 0.17 36 2.5e-005 1.3e+000 6.7e-005 -7.51e-002 1.017001318e+001 1.017015458e+001 3.0e-008 0.17 37 2.5e-005 1.3e+000 6.6e-005 -7.36e-002 1.017001439e+001 1.017015188e+001 3.0e-008 0.17 38 2.5e-005 1.3e+000 6.6e-005 -5.68e-002 1.017001560e+001 1.017014983e+001 3.0e-008 0.17 39 2.4e-005 1.3e+000 6.3e-005 -3.78e-002 1.017002178e+001 1.017014193e+001 2.8e-008 0.17 40 9.4e-006 9.1e-001 2.7e-005 -3.06e-003 1.017007505e+001 1.017013246e+001 1.4e-008 0.17 41 5.3e-007 4.3e-001 1.4e-005 4.88e-001 1.017010185e+001 1.017014026e+001 3.4e-009 0.19 42 2.1e-007 1.8e-001 6.1e-006 -3.79e-001 1.017011491e+001 1.017014342e+001 1.5e-009 0.19 43 1.9e-007 1.8e-001 5.7e-006 9.51e-001 1.017011751e+001 1.017014211e+001 1.4e-009 0.19 44 1.7e-007 1.7e-001 5.1e-006 1.03e+000 1.017011916e+001 1.017014069e+001 1.3e-009 0.19 45 1.5e-007 1.6e-001 4.6e-006 1.02e+000 1.017012039e+001 1.017013963e+001 1.1e-009 0.19 46 1.4e-007 1.6e-001 4.2e-006 1.06e+000 1.017012168e+001 1.017013846e+001 1.1e-009 0.19 47 1.3e-007 1.5e-001 3.7e-006 9.57e-001 1.017012258e+001 1.017013772e+001 9.6e-010 0.19 48 1.1e-007 1.4e-001 3.4e-006 1.00e+000 1.017012341e+001 1.017013702e+001 8.6e-010 0.19 49 1.0e-007 1.4e-001 3.0e-006 1.04e+000 1.017012424e+001 1.017013629e+001 7.9e-010 0.20 50 9.1e-008 1.3e-001 2.7e-006 1.00e+000 1.017012490e+001 1.017013575e+001 7.1e-010 0.20 51 8.3e-008 1.3e-001 2.5e-006 1.02e+000 1.017012553e+001 1.017013521e+001 6.4e-010 0.20 52 7.4e-008 1.2e-001 2.2e-006 1.00e+000 1.017012606e+001 1.017013478e+001 5.8e-010 0.20 53 6.7e-008 1.2e-001 2.0e-006 1.00e+000 1.017012653e+001 1.017013439e+001 5.2e-010 0.20 54 6.0e-008 1.0e-001 1.8e-006 1.13e+000 1.017012720e+001 1.017013375e+001 5.0e-010 0.20 55 6.1e-008 9.4e-002 1.6e-006 1.15e+000 1.017012778e+001 1.017013321e+001 4.8e-010 0.20 56 5.5e-008 9.1e-002 1.5e-006 9.82e-001 1.017012808e+001 1.017013297e+001 4.3e-010 0.22 57 5.0e-008 9.0e-002 1.3e-006 9.82e-001 1.017012835e+001 1.017013276e+001 3.9e-010 0.22 58 4.5e-008 8.7e-002 1.2e-006 8.73e-001 1.017012859e+001 1.017013258e+001 3.5e-010 0.22 59 4.1e-008 8.6e-002 1.1e-006 9.66e-001 1.017012881e+001 1.017013242e+001 3.2e-010 0.22 60 3.7e-008 8.6e-002 9.5e-007 9.26e-001 1.017012901e+001 1.017013225e+001 2.8e-010 0.22 61 3.3e-008 7.7e-002 8.6e-007 1.02e+000 1.017012920e+001 1.017013209e+001 2.6e-010 0.22 62 2.9e-008 7.0e-002 7.7e-007 9.92e-001 1.017012936e+001 1.017013195e+001 2.3e-010 0.22 63 2.7e-008 6.9e-002 6.9e-007 8.94e-001 1.017012950e+001 1.017013185e+001 2.1e-010 0.23 64 2.5e-008 6.8e-002 6.2e-007 8.22e-001 1.017012963e+001 1.017013176e+001 1.9e-010 0.23 65 2.3e-008 6.1e-002 5.6e-007 9.61e-001 1.017012974e+001 1.017013166e+001 1.7e-010 0.23 66 2.0e-008 5.5e-002 5.1e-007 9.10e-001 1.017012985e+001 1.017013157e+001 1.5e-010 0.23 67 1.8e-008 4.9e-002 4.6e-007 1.03e+000 1.017012996e+001 1.017013148e+001 1.4e-010 0.23 68 1.6e-008 4.4e-002 4.1e-007 1.02e+000 1.017013005e+001 1.017013140e+001 1.3e-010 0.23 69 1.5e-008 4.0e-002 3.7e-007 9.65e-001 1.017013012e+001 1.017013134e+001 1.1e-010 0.25 70 1.4e-008 3.6e-002 3.3e-007 9.25e-001 1.017013019e+001 1.017013129e+001 1.0e-010 0.25 71 1.2e-008 3.2e-002 3.0e-007 1.00e+000 1.017013025e+001 1.017013124e+001 9.3e-011 0.25 72 1.1e-008 2.9e-002 2.7e-007 1.10e+000 1.017013032e+001 1.017013116e+001 8.8e-011 0.25 73 1.1e-008 2.6e-002 2.4e-007 9.14e-001 1.017013037e+001 1.017013113e+001 7.9e-011 0.25 74 1.2e-008 2.4e-002 2.2e-007 1.14e+000 1.017013043e+001 1.017013107e+001 7.6e-011 0.25 75 9.7e-009 2.1e-002 2.0e-007 9.72e-001 1.017013047e+001 1.017013104e+001 6.8e-011 0.25 76 9.8e-009 1.9e-002 1.8e-007 8.76e-001 1.017013050e+001 1.017013102e+001 6.1e-011 0.25 77 8.9e-009 1.7e-002 1.6e-007 1.02e+000 1.017013053e+001 1.017013099e+001 5.6e-011 0.27 78 8.6e-009 1.5e-002 1.4e-007 1.36e+000 1.017013055e+001 1.017013096e+001 5.0e-011 0.27 79 6.8e-009 1.4e-002 1.3e-007 1.12e+000 1.017013059e+001 1.017013093e+001 4.8e-011 0.27 80 6.5e-009 1.3e-002 1.2e-007 9.47e-001 1.017013061e+001 1.017013092e+001 4.3e-011 0.27 81 5.3e-009 1.1e-002 1.0e-007 7.15e-001 1.017013062e+001 1.017013091e+001 3.8e-011 0.27 82 4.8e-009 1.0e-002 9.4e-008 1.23e+000 1.017013064e+001 1.017013089e+001 3.4e-011 0.28 83 4.9e-009 9.1e-003 8.4e-008 9.71e-001 1.017013065e+001 1.017013088e+001 3.1e-011 0.28 84 4.6e-009 8.2e-003 7.6e-008 8.13e-001 1.017013067e+001 1.017013087e+001 2.8e-011 0.28 85 4.2e-009 7.4e-003 6.8e-008 9.50e-001 1.017013068e+001 1.017013087e+001 2.5e-011 0.28 86 3.8e-009 6.7e-003 6.2e-008 7.95e-001 1.017013069e+001 1.017013086e+001 2.2e-011 0.28 87 4.2e-009 6.0e-003 5.5e-008 1.07e+000 1.017013070e+001 1.017013085e+001 2.1e-011 0.28 88 3.7e-009 5.4e-003 5.0e-008 1.02e+000 1.017013071e+001 1.017013084e+001 1.9e-011 0.28 89 3.9e-009 4.9e-003 4.5e-008 1.21e+000 1.017013072e+001 1.017013083e+001 1.9e-011 0.30 90 3.6e-009 4.4e-003 4.0e-008 1.38e+000 1.017013073e+001 1.017013082e+001 1.7e-011 0.30 91 3.8e-009 3.9e-003 3.6e-008 1.13e+000 1.017013074e+001 1.017013082e+001 1.6e-011 0.30 92 3.3e-009 3.5e-003 3.3e-008 9.42e-001 1.017013074e+001 1.017013081e+001 1.5e-011 0.30 93 3.5e-009 3.2e-003 2.9e-008 1.16e+000 1.017013075e+001 1.017013081e+001 1.4e-011 0.30 94 2.5e-009 6.0e-004 5.6e-009 9.92e-001 1.017013078e+001 1.017013079e+001 2.8e-012 0.30 95 2.3e-009 5.4e-004 5.0e-009 1.12e+000 1.017013078e+001 1.017013079e+001 2.7e-012 0.31 96 2.0e-009 4.9e-004 4.5e-009 1.77e+000 1.017013078e+001 1.017013078e+001 2.4e-012 0.31 97 1.8e-009 4.4e-004 4.1e-009 1.05e+000 1.017013078e+001 1.017013078e+001 2.2e-012 0.31 98 1.6e-009 4.0e-004 3.7e-009 1.62e+000 1.017013078e+001 1.017013078e+001 2.0e-012 0.31 99 1.5e-009 3.6e-004 3.3e-009 9.86e-001 1.017013078e+001 1.017013078e+001 1.7e-012 0.31 100 1.3e-009 3.2e-004 3.0e-009 1.13e+000 1.017013078e+001 1.017013078e+001 1.7e-012 0.33 101 1.2e-009 2.9e-004 2.7e-009 1.36e+000 1.017013078e+001 1.017013078e+001 1.5e-012 0.33 102 1.1e-009 2.6e-004 2.4e-009 1.39e+000 1.017013078e+001 1.017013078e+001 1.3e-012 0.33 103 1.0e-009 2.3e-004 2.2e-009 8.40e-001 1.017013078e+001 1.017013078e+001 1.2e-012 0.33 104 9.3e-010 2.1e-004 2.0e-009 9.12e-001 1.017013078e+001 1.017013078e+001 1.1e-012 0.33 105 8.5e-010 1.9e-004 1.8e-009 1.10e+000 1.017013078e+001 1.017013078e+001 1.0e-012 0.33 106 8.5e-010 1.9e-004 1.8e-009 1.18e+000 1.017013078e+001 1.017013078e+001 1.0e-012 0.34 107 7.6e-010 1.7e-004 1.6e-009 1.01e+000 1.017013078e+001 1.017013078e+001 9.0e-013 0.34 Interior-point optimizer terminated. Time: 0.34. Optimizer terminated. Time: 0.36 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0170130780e+001 Viol. con: 8e-010 var: 0e+000 Dual. obj: 1.0170130782e+001 Viol. con: 0e+000 var: 5e-005 * End solution on dual form. * Transforming to primal solution. Solving took 0.393 seconds. result packing took 38% of solve time solution checking took 16% of solve time Solving took 5 GP solves and 13.8 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 366641.674293 newton but the right hand side evaluated to 366630.062468 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 377162.188142 newton but the right hand side evaluated to 377115.437398 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 388105.086612 newton but the right hand side evaluated to 387998.856084 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 399470.240713 newton but the right hand side evaluated to 399279.089406 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 361212.19029 newton but the right hand side evaluated to 361206.365657 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 371522.136704 newton but the right hand side evaluated to 371498.54019 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 382190.30228 newton but the right hand side evaluated to 382135.963907 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 393255.63901 newton but the right hand side evaluated to 393156.473813 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 356181.882924 newton but the right hand side evaluated to 356176.095803 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 361243.199753 newton but the right hand side evaluated to 361220.04559 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 366354.221181 newton but the right hand side evaluated to 366302.329217 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 371535.450867 newton but the right hand side evaluated to 371443.464936 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 18366.9596924 newton but the right hand side evaluated to 18366.7168854 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 18344.453621 newton but the right hand side evaluated to 18344.2042843 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 18344.453547 newton but the right hand side evaluated to 18344.2041803 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 18344.4535752 newton but the right hand side evaluated to 18344.2042071 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 18924.2848439 newton but the right hand side evaluated to 18924.2643569 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 8445.89963446 newton but the right hand side evaluated to 8445.84800432 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 8626.29336426 newton but the right hand side evaluated to 8626.24784807 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 24184.7528315 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%) Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485055 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 29.946s OK Generating XML reports... Cloning into 'gassolar'... 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Cannot uninstall requirement gassolar, not installed Obtaining file:///D:/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows7x64/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 238e02f... explicitly add wing interior to v-h tails Cannot uninstall requirement gpkit-models, not installed Obtaining file:///D:/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows7x64/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 d:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: numpy>=1.7.0 in d:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-lezama-build Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint in d:\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 6.57 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 4.96 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 5.66 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 0.545 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 0.037 seconds. Using solver 'mosek_cli' Solving for 79 variables. Solving took 0.079 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 0.214969920711 (Allowable error: 0.0001%, Actual error: 0.0042%) 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 0.201773970842 (Allowable error: 0.0001%, Actual error: 0.0014%) 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 0.197670258036 but the right hand side evaluated to 0.197669830217 (Allowable error: 0.0001%, Actual error: 0.00022%) 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 0.20177138095 but the right hand side evaluated to 0.201773970842 (Allowable error: 0.0001%, Actual error: 0.0013%) 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 0.21497919994 but the right hand side evaluated to 0.214991418778 (Allowable error: 0.0001%, Actual error: 0.0057%) Using solver 'mosek' Solving for 1067 variables. Solving took 1.78 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 134065.0319 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.1/AircraftPerf.1/WingAero.1 could cause inaccurate result because it is below lower bound. Solution is 132709.8902 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 134071.9969 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 11 is a constraining latitude Beginning signomial solve. Solving took 4 GP solves and 18.2 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 136276.7307 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 136278.3666 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 0.82 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 134064.9952 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.1/AircraftPerf.1/WingAero.1 could cause inaccurate result because it is below lower bound. Solution is 132709.7909 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 2 is a constraining latitude 11 is a constraining latitude Beginning signomial solve. Solving took 4 GP solves and 10.7 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... ---------------------------------------------------------------------- ....d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\gassolar\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 6 tests in 77.356s 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: 238e02f explicitly add wing interior to v-h tails If you want to keep them by creating a new branch, this may be a good time to do so with: git branch new_branch_name 238e02f HEAD is now at 662ac9f... add readme with build status Cannot uninstall requirement gpkit-models, not installed Obtaining file:///D:/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows7x64/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-bg5wrs-build Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in d:\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows7x64\optimizer\mosek\turbofan Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) adding test for 'SP_aircraft.py' Beginning signomial solve. Solving took 7 GP solves and 31.2 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 2427079.05341 force_pound * meter but the right hand side evaluated to 2397885.60935 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 2.21510116744 meter but the right hand side evaluated to 1.96470305248 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 17472.5843457 newton but the right hand side evaluated to 17443.2514001 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 1242117.48852 joule / kilogram but the right hand side evaluated to 1.48135621057 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 642471.430057 joule / kilogram but the right hand side evaluated to 0.64395594674 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 271789.798363 meter * newton but the right hand side evaluated to 263034.92027 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 18.5759827201 meter but the right hand side evaluated to 16.6120518295 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 10.9551780441 but the right hand side evaluated to 4.85819494985 (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 10.0069397588 but the right hand side evaluated to 4.85820517362 (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 8.21525230325 but the right hand side evaluated to 4.85820523006 (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 18.6220040522 meter but the right hand side evaluated to 18.3758687213 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 18.6220040522 meter but the right hand side evaluated to 18.451319281 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 4.67771867533 but the right hand side evaluated to 4.79404794419 (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 4.73113698617 but the right hand side evaluated to 4.8137321075 (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 7.60828606842 but the right hand side evaluated to 4.79404794419 (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 7.57970215372 but the right hand side evaluated to 4.8137321075 (Allowable error: 0.1%, Actual error: 36%) Solves with these variables bounded: value near lower bound: [MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, CruiseAlt_Mission, ClimbDistance_Mission] value near upper bound: [TotalTime_Mission, A_{tri}_Mission/Aircraft/Wing/WingNoStruct] Checking for relaxed constants... WEIGHT DIFFERENCES Total Fuel Weight Percent Diff: [-6.97453438] Total Aircraft Weight Percent Diff: [-4.95042979] Engine Weight Percent Diff: -8.23500415796 Fuselage Weight Percent Diff: -10.9542159667 Payload Weight Percent Diff: [-0.04003558] VT Weight Percent Diff: -24.5189510456 HT Weight Percent Diff: -85.1525152147 Wing Weight Percent Diff: 0.426088647416 WING DIFFERENCES Wing Span Percent Diff: 0.921607240519 Wing Area Percent Diff: -6.86185076619 HORIZONTAL TAIL DIFFERENCES HT Area Percent Diff: -54.6184798626 VERTICAL TAIL DIFFERENCES VT Span Percent Diff: -16.3231941378 VT Area Percent Diff: -29.9969725511 CRUISE SEGMENT 1 DRAG DIFFERENCES Overall Cd Percent Diff: [-0.13085823] Nacelle Cd Percent Diff: [ 23.80937862] HT Cd Percent Diff: [-63.50965746] dimensionless Fuselage Cd Percent Diff: [ 45.32349081] VT Cd Percent Diff: [ 60.36869804] dimensionless Induced Drag Cd Percent Diff: [ 1.06377352] Wing Profile Cd Percent Diff: [-15.69394141] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [ 2.99108567] FUSELAGE DIFFERENCES Fan Propulsive Efficiency in Cruise Segment 1 --------------------- 0.790004734279 Beginning signomial solve. Solving took 7 GP solves and 11.6 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 2427086.19714 force_pound * meter but the right hand side evaluated to 2397878.88462 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 2.2151029155 meter but the right hand side evaluated to 1.96470832659 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 17472.4999511 newton but the right hand side evaluated to 17443.2145325 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 1242107.88076 joule / kilogram but the right hand side evaluated to 1.48150781044 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 642492.385771 joule / kilogram but the right hand side evaluated to 0.643976760313 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 263034.971207 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 18.575992106 meter but the right hand side evaluated to 16.6120610364 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 10.9552358245 but the right hand side evaluated to 4.85818543058 (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 10.0071246438 but the right hand side evaluated to 4.85819514696 (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 8.21526226574 but the right hand side evaluated to 4.85819514696 (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 18.6220164763 meter but the right hand side evaluated to 18.3758811924 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 18.6220164763 meter but the right hand side evaluated to 18.4513400632 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 4.67770662453 but the right hand side evaluated to 4.79403770011 (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 4.73113191581 but the right hand side evaluated to 4.81372397623 (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 7.60820130775 but the right hand side evaluated to 4.79403770011 (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 7.57969984142 but the right hand side evaluated to 4.81372397623 (Allowable error: 0.1%, Actual error: 36%) Solves with these variables bounded: value near lower bound: [MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, CruiseAlt_Mission, ClimbDistance_Mission] value near upper bound: [TotalTime_Mission, A_{tri}_Mission/Aircraft/Wing/WingNoStruct] Checking for relaxed constants... WEIGHT DIFFERENCES Total Fuel Weight Percent Diff: [-6.97422995] Total Aircraft Weight Percent Diff: [-4.95044675] Engine Weight Percent Diff: -8.23468392487 Fuselage Weight Percent Diff: -10.954618425 Payload Weight Percent Diff: [-0.04052335] VT Weight Percent Diff: -24.5185536457 HT Weight Percent Diff: -85.152583626 Wing Weight Percent Diff: 0.425462741526 WING DIFFERENCES Wing Span Percent Diff: 0.921619801497 Wing Area Percent Diff: -6.86162729346 HORIZONTAL TAIL DIFFERENCES HT Area Percent Diff: -54.6182474474 VERTICAL TAIL DIFFERENCES VT Span Percent Diff: -16.3230602377 VT Area Percent Diff: -29.9967358734 CRUISE SEGMENT 1 DRAG DIFFERENCES Overall Cd Percent Diff: [-0.12888384] Nacelle Cd Percent Diff: [ 23.80939215] HT Cd Percent Diff: [-63.50956764] dimensionless Fuselage Cd Percent Diff: [ 45.32347143] VT Cd Percent Diff: [ 60.36836498] dimensionless Induced Drag Cd Percent Diff: [ 1.06873722] Wing Profile Cd Percent Diff: [-15.69240054] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [ 2.99029634] FUSELAGE DIFFERENCES Fan Propulsive Efficiency in Cruise Segment 1 --------------------- 0.790005398454 Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 63.422s 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) D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\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 'D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek' for the testing framework 'JUnit'. [xUnit] [INFO] - Check 'Failed Tests' threshold. [xUnit] [INFO] - Check 'Skipped Tests' threshold. [xUnit] [INFO] - Setting the build status to SUCCESS [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: SUCCESS