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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 windows10x64 in workspace C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > C:\Program Files\Git\cmd\git init C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > C:\Program Files\Git\cmd\git --version # timeout=10 > C:\Program Files\Git\cmd\git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* > C:\Program Files\Git\cmd\git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 > C:\Program Files\Git\cmd\git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10 > C:\Program Files\Git\cmd\git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > C:\Program Files\Git\cmd\git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master Merging Revision 9a9531c5d88de00e8825c434df4d40f160cb13e5 (refs/remotes/origin/pr/123/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='default', fastForwardMode='--ff'} > C:\Program Files\Git\cmd\git rev-parse "origin/master^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git config core.sparsecheckout # timeout=10 > C:\Program Files\Git\cmd\git checkout -f origin/master # timeout=3 > C:\Program Files\Git\cmd\git merge --ff 9a9531c5d88de00e8825c434df4d40f160cb13e5 # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "HEAD^{commit}" # timeout=10 Seen branch in repository origin/1682literate Seen branch in repository origin/1682master Seen branch in repository origin/Breakdown Seen branch in repository origin/SPaircraft Seen branch in repository origin/aerosurf Seen branch in repository origin/atmosphere 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branch in repository origin/pr/97/merge Seen branch in repository origin/pr/98/head Seen branch in repository origin/pr/99/head Seen branch in repository origin/quadrotor Seen branch in repository origin/rockets Seen branch in repository origin/sigeq_paper Seen branch in repository origin/simple_HT_sizing Seen branch in repository origin/simple_flight_profile Seen branch in repository origin/standard_atmosphere Seen branch in repository origin/sutherland Seen branch in repository origin/tailfoam Seen branch in repository origin/troposphere Seen branch in repository origin/wide_body Seen 153 remote branches > C:\Program Files\Git\cmd\git tag -l # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/include^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/DF70^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/linking^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/csv^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/start^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/pay^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/sum^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/clean^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/sys^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/pshaft^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/solarmd^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/climb^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/fuse^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/mission^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/discret^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/plot^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/md^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/atm^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/make^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "refs/tags/eng^{commit}" # timeout=10 Checking out Revision 9a9531c5d88de00e8825c434df4d40f160cb13e5 (origin/pr/123/merge, origin/master) > C:\Program Files\Git\cmd\git config core.sparsecheckout # timeout=10 > C:\Program Files\Git\cmd\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 [windows10x64] is in [[macys, macys_Sierra, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [windows10x64] is in [[windows10x64, windows7x64]] Run condition [Execution node ] enabling perform for step [Execute Windows batch command] [mosek] $ cmd /c call C:\Users\jenkins\AppData\Local\Temp\jenkins3863322997831196448.bat C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>echo C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Git\cmd;C:\Program Files\mingw-w64\x86_64-5.3.0-posix-seh-rt_v4-rev0\mingw64\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Git\cmd;C:\Program Files\mingw-w64\x86_64-5.3.0-posix-seh-rt_v4-rev0\mingw64\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>REM turn on the anaconda console C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>call activate.bat || exit /b 666 (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Create a virtualenv to install everything into (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>SET VENV=C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>virtualenv --system-site-packages C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit New python executable in C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts\python.exe Installing setuptools, pip, wheel...done. (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>call C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts\activate.bat (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Install coverage into the virtualenv to the coverage command blow uses the virtualenv python (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>pip install coverage Collecting coverage Using cached coverage-4.4.1-cp27-cp27m-win_amd64.whl Installing collected packages: coverage Successfully installed coverage-4.4.1 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>if mosek == mosek msktestlic || exit /b 666 Problem Name : Objective sense : min Type : LO (linear optimization problem) Constraints : 1 Cones : 0 Scalar variables : 5000 Matrix variables : 0 Integer variables : 0 Optimizer started. Mosek license manager: License path: C:\Users\jenkins\mosek\mosek.lic Mosek license manager: Checkout license feature 'PTS' from flexlm. Mosek license manager: Checkout time 0.02. r: 0 status: 0 Interior-point optimizer started. Presolve started. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 1 time : 0.00 Lin. dep. - tries : 0 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.01. Optimizer terminated. Time: 0.03 ************************************ A license was checked out correctly. ************************************ (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>SET GPKITBUILD=C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\build_gpkit (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>gcc --version || exit /b 666 gcc (x86_64-posix-seh-rev0, Built by MinGW-W64 project) 5.3.0 Copyright (C) 2015 Free Software Foundation, Inc. This is free software; see the source for copying conditions. There is NO warranty; not even for MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>if mosek == cvxopt set GPKITSOLVERS=cvxopt (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>if mosek == mosek set GPKITSOLVERS=mosek, mosek_cli (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>dir C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\build_gpkit Volume in drive C has no label. Volume Serial Number is C4C9-8F11 Directory of C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek File Not Found (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "import scipy; print scipy.__version__" 0.18.1 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "import numpy; print numpy.__version__" 1.11.3 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "import pint; print pint.__version__" 0.7.2 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Install gpkit to run the documentation examples (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>git clone --depth 1 https://github.com/convexengineering/gpkit.git Cloning into 'gpkit'... (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>pip install -e C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\gpkit | exit /b 666 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 480 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 767 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_install.py, line 985 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file install.py, line 369 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>pip install -e C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek | exit /b 666 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 480 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 496 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_set.py, line 767 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file req_install.py, line 985 Traceback (most recent call last): File "c:\anaconda2\Lib\logging\__init__.py", line 882, in emit stream.write(fs % msg) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 141, in write self.write_and_convert(text) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 169, in write_and_convert self.write_plain_text(text, cursor, len(text)) File "c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\pip\_vendor\colorama\ansitowin32.py", line 175, in write_plain_text self.wrapped.flush() IOError: [Errno 22] Invalid argument Logged from file install.py, line 369 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>REM Show the settings file (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>type C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\env\settings installed_solvers : mosek, mosek_cli mosek_bin_dir : C:\Program Files\Mosek\8\tools\platform\win64x86\bin (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True)" Cloning into 'gpkit-models'... Cloning into 'shopping'... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 2.18 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 1.2 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.072 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 3.791s OK Generating XML reports... Cloning into 'jho'... From https://github.com/convexengineering/gpkit-models * branch master -> FETCH_HEAD Note: checking out 'FETCH_HEAD'. You are in 'detached HEAD' state. You can look around, make experimental changes and commit them, and you can discard any commits you make in this state without impacting any branches by performing another checkout. If you want to create a new branch to retain commits you create, you may do so (now or later) by using -b with the checkout command again. Example: git checkout -b <new-branch-name> HEAD is now at 662ac9f... add readme with build status Cannot uninstall requirement gpkit-models, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/gpkit-models Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: numpy>=1.7.0 in c:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-c4edzd-build Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) Installing collected packages: gpfit Running setup.py install for gpfit: started Running setup.py install for gpfit: finished with status 'done' Successfully installed gpfit-0.1 adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -1.10731155148e-11. Allowing negative dual variable(s) as small as -1.60386461057e-12. Allowing negative dual variable(s) as small as -2.16796528646e-11. Allowing negative dual variable(s) as small as -1.52839329734e-12. Solving took 4 GP solves and 1.23 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -9.62326138915e-12. Allowing negative dual variable(s) as small as -1.60251369466e-12. Allowing negative dual variable(s) as small as -1.62081242525e-12. Allowing negative dual variable(s) as small as -1.52599330741e-12. Solving took 4 GP solves and 4.8 seconds. Allowing negative dual variable(s) as small as -7.74469377518e-12. Allowing negative dual variable(s) as small as -3.41680919669e-11. Allowing negative dual variable(s) as small as -2.09158662612e-11. Allowing negative dual variable(s) as small as -2.11292650043e-11. Allowing negative dual variable(s) as small as -2.14083681338e-11. Allowing negative dual variable(s) as small as -4.94407856669e-12. Allowing negative dual variable(s) as small as -1.04706506052e-11. Allowing negative dual variable(s) as small as -5.89564681797e-12. Allowing negative dual variable(s) as small as -1.10750192654e-11. MTOW [lbs] = 141.59 Zero fuel weight [lbs] = 53.63 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.74901152189e-12. Allowing negative dual variable(s) as small as -7.1149467611e-12. Allowing negative dual variable(s) as small as -1.34979809448e-11. Allowing negative dual variable(s) as small as -1.3736824395e-11. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.42476286503e-11. Allowing negative dual variable(s) as small as -3.57309260077e-11. Allowing negative dual variable(s) as small as -3.97672524319e-13. Allowing negative dual variable(s) as small as -5.67089819052e-11. Solving took 4 GP solves and 1.91 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.05680697368e-13. Allowing negative dual variable(s) as small as -1.80572896046e-11. Allowing negative dual variable(s) as small as -7.28713187882e-11. Allowing negative dual variable(s) as small as -1.43015703447e-11. Solving took 4 GP solves and 1.78 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -7.73321684466e-12. Allowing negative dual variable(s) as small as -3.41736500209e-11. Allowing negative dual variable(s) as small as -2.09340184076e-11. Allowing negative dual variable(s) as small as -2.11171011233e-11. Allowing negative dual variable(s) as small as -2.14180131963e-11. Allowing negative dual variable(s) as small as -4.88942913934e-12. Allowing negative dual variable(s) as small as -1.047098519e-11. Allowing negative dual variable(s) as small as -5.89334538201e-12. Allowing negative dual variable(s) as small as -1.10736954545e-11. MTOW [lbs] = 141.59 Zero fuel weight [lbs] = 53.63 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.75411616256e-12. Allowing negative dual variable(s) as small as -7.1127947282e-12. Allowing negative dual variable(s) as small as -1.34966698191e-11. Allowing negative dual variable(s) as small as -1.3740172845e-11. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.42480184744e-11. Allowing negative dual variable(s) as small as -3.57313447169e-11. Allowing negative dual variable(s) as small as -3.97821681738e-13. Allowing negative dual variable(s) as small as -5.67073676267e-11. Solving took 4 GP solves and 2.04 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.06213691156e-13. Allowing negative dual variable(s) as small as -1.80545405015e-11. Allowing negative dual variable(s) as small as -7.287456966e-11. Allowing negative dual variable(s) as small as -1.43018019302e-11. Solving took 4 GP solves and 18.3 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 173.925s OK Generating XML reports... Cloning into 'turbofan'... Cannot uninstall requirement turbofan, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/turbofan Installing collected packages: turbofan Running setup.py develop for turbofan Successfully installed turbofan From https://github.com/convexengineering/gpkit-models * branch master -> FETCH_HEAD HEAD is now at 662ac9f... add readme with build status Cannot uninstall requirement gpkit-models, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/gpkit-models Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels adding test for 'turbofan/engine_validation.py' adding test for 'turbofan/engine_flight_profile_fleet.py' T_{t_{4.1_{max}}}_FleetMission/Aircraft/Engine has no upper bound Beginning signomial solve. Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 746 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 7 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.02 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 2 Optimizer - solved problem : the primal Optimizer - Constraints : 366 Optimizer - Cones : 0 Optimizer - Scalar variables : 1075 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.00 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.00 Factor - nonzeros before factor : 5857 after factor : 1.07e+004 Factor - dense dim. : 0 flops : 1.01e+005 Factor - GP saved nzs : 1.05e+004 GP saved flops : 1.12e+005 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.2e+003 4.3e+003 2.0e+004 0.00e+000 -2.004159770e+004 1.023181539e-012 1.0e+000 0.02 1 8.0e+002 2.8e+003 1.3e+004 -9.19e-002 -1.644778994e+004 3.599090741e+000 6.6e-001 0.53 2 4.4e+002 1.5e+003 7.2e+003 7.81e-002 -1.282460784e+004 7.951485611e+000 3.7e-001 0.58 3 2.2e+002 7.9e+002 3.7e+003 4.64e-001 -6.928674912e+003 1.273134154e+001 1.9e-001 0.63 4 8.8e+001 3.1e+002 1.4e+003 1.09e+000 -2.493194390e+003 1.565269744e+001 8.0e-002 0.67 5 4.8e+001 1.7e+002 7.9e+002 1.61e+000 -1.112541302e+003 1.604885507e+001 4.5e-002 0.67 6 3.1e+001 1.1e+002 5.1e+002 1.58e+000 -6.178130552e+002 1.590105852e+001 2.9e-002 0.83 7 1.7e+001 6.0e+001 2.9e+002 1.43e+000 -2.984952244e+002 1.562817861e+001 1.7e-002 0.83 8 5.6e+000 1.6e+001 9.2e+001 1.30e+000 -7.551622698e+001 1.506809630e+001 5.5e-003 0.83 9 2.5e+000 8.0e+000 4.1e+001 9.26e-001 -3.122683429e+001 1.444951916e+001 2.7e-003 0.83 10 1.7e+000 1.2e+001 2.9e+001 5.19e-001 -2.502154152e+001 1.418384811e+001 1.9e-003 0.84 11 4.6e-001 4.5e+000 7.9e+000 5.27e-001 -8.912243347e-001 1.342130163e+001 6.1e-004 0.84 12 2.0e-001 5.9e+000 3.4e+000 5.13e-001 5.534323567e+000 1.305030357e+001 2.8e-004 0.84 13 1.2e-001 3.6e+000 2.1e+000 7.05e-001 7.974950032e+000 1.288236196e+001 1.8e-004 0.84 14 5.9e-002 2.5e+000 1.0e+000 7.78e-001 1.019984196e+001 1.271463281e+001 8.9e-005 0.84 15 1.9e-002 1.8e+000 3.2e-001 8.78e-001 1.174966832e+001 1.258159676e+001 3.1e-005 0.86 16 6.7e-003 1.3e+000 1.2e-001 9.77e-001 1.223575557e+001 1.253849051e+001 1.2e-005 0.86 17 2.3e-003 1.3e+000 4.0e-002 1.01e+000 1.241931212e+001 1.252149371e+001 4.2e-006 0.88 18 7.0e-004 1.2e+000 1.2e-002 9.98e-001 1.248404800e+001 1.251586182e+001 1.3e-006 0.88 19 6.3e-004 1.1e+000 1.1e-002 9.92e-001 1.248697427e+001 1.251567987e+001 1.2e-006 0.88 20 5.7e-004 1.0e+000 1.0e-002 9.94e-001 1.248961971e+001 1.251546691e+001 1.1e-006 0.88 21 5.1e-004 9.3e-001 9.1e-003 9.94e-001 1.249199556e+001 1.251526468e+001 9.6e-007 0.88 22 4.6e-004 8.4e-001 8.2e-003 9.95e-001 1.249413788e+001 1.251508529e+001 8.7e-007 0.89 23 4.2e-004 7.7e-001 7.3e-003 9.95e-001 1.249606807e+001 1.251492519e+001 7.8e-007 0.89 24 3.7e-004 7.0e-001 6.6e-003 9.95e-001 1.249780683e+001 1.251478201e+001 7.0e-007 0.89 25 3.4e-004 6.4e-001 5.9e-003 9.96e-001 1.249937314e+001 1.251465399e+001 6.3e-007 0.89 26 3.0e-004 5.9e-001 5.4e-003 9.96e-001 1.250078404e+001 1.251453950e+001 5.7e-007 1.05 27 2.7e-004 5.4e-001 4.8e-003 9.96e-001 1.250205490e+001 1.251443709e+001 5.1e-007 1.05 28 2.5e-004 4.9e-001 4.3e-003 9.96e-001 1.250319957e+001 1.251434546e+001 4.6e-007 1.05 29 2.2e-004 4.5e-001 3.9e-003 9.97e-001 1.250423053e+001 1.251426345e+001 4.2e-007 1.05 30 2.0e-004 4.2e-001 3.5e-003 9.97e-001 1.250515903e+001 1.251419001e+001 3.7e-007 1.05 31 1.8e-004 3.8e-001 3.2e-003 9.97e-001 1.250599522e+001 1.251412423e+001 3.4e-007 1.06 32 1.6e-004 3.6e-001 2.8e-003 9.97e-001 1.250674823e+001 1.251406529e+001 3.0e-007 1.06 33 1.5e-004 3.3e-001 2.6e-003 9.98e-001 1.250742631e+001 1.251401245e+001 2.7e-007 1.06 34 1.3e-004 3.1e-001 2.3e-003 9.98e-001 1.250803690e+001 1.251396508e+001 2.5e-007 1.06 35 1.2e-004 2.8e-001 2.1e-003 9.98e-001 1.250858667e+001 1.251392259e+001 2.2e-007 1.06 36 1.1e-004 2.7e-001 1.9e-003 9.98e-001 1.250908169e+001 1.251388446e+001 2.0e-007 1.06 37 9.5e-005 2.5e-001 1.7e-003 9.98e-001 1.250952738e+001 1.251385025e+001 1.8e-007 1.06 38 8.6e-005 2.3e-001 1.5e-003 9.98e-001 1.250992864e+001 1.251381953e+001 1.6e-007 1.08 39 7.7e-005 2.2e-001 1.4e-003 9.99e-001 1.251028990e+001 1.251379196e+001 1.4e-007 1.08 40 6.9e-005 2.1e-001 1.2e-003 9.99e-001 1.251061512e+001 1.251376719e+001 1.3e-007 1.08 41 6.2e-005 1.9e-001 1.1e-003 9.99e-001 1.251090791e+001 1.251374494e+001 1.2e-007 1.08 42 5.6e-005 1.8e-001 9.9e-004 9.99e-001 1.251117148e+001 1.251372496e+001 1.1e-007 1.08 43 5.1e-005 1.8e-001 8.9e-004 9.99e-001 1.251140875e+001 1.251370700e+001 9.5e-008 1.08 44 4.6e-005 1.7e-001 8.0e-004 9.99e-001 1.251162234e+001 1.251369086e+001 8.6e-008 1.08 45 4.1e-005 1.6e-001 7.2e-004 9.99e-001 1.251181460e+001 1.251367635e+001 7.7e-008 1.09 46 3.7e-005 1.5e-001 6.5e-004 9.99e-001 1.251198767e+001 1.251366332e+001 6.9e-008 1.09 47 3.3e-005 1.5e-001 5.9e-004 9.99e-001 1.251214345e+001 1.251365159e+001 6.2e-008 1.09 48 3.0e-005 1.4e-001 5.3e-004 9.99e-001 1.251228368e+001 1.251364105e+001 5.6e-008 1.09 49 2.7e-005 1.4e-001 4.7e-004 9.99e-001 1.251240990e+001 1.251363157e+001 5.1e-008 1.09 50 2.4e-005 1.3e-001 4.3e-004 9.99e-001 1.251252351e+001 1.251362305e+001 4.5e-008 1.09 51 2.2e-005 1.3e-001 3.8e-004 1.00e+000 1.251262578e+001 1.251361538e+001 4.1e-008 1.09 52 2.0e-005 1.3e-001 3.5e-004 1.00e+000 1.251271782e+001 1.251360849e+001 3.7e-008 1.11 53 1.8e-005 1.2e-001 3.1e-004 1.00e+000 1.251280067e+001 1.251360229e+001 3.3e-008 1.11 54 1.6e-005 1.2e-001 2.8e-004 1.00e+000 1.251287524e+001 1.251359671e+001 3.0e-008 1.11 55 1.4e-005 1.2e-001 2.5e-004 1.00e+000 1.251294235e+001 1.251359169e+001 2.7e-008 1.11 56 1.3e-005 1.2e-001 2.3e-004 1.00e+000 1.251300276e+001 1.251358717e+001 2.4e-008 1.11 57 1.2e-005 1.1e-001 2.0e-004 1.00e+000 1.251305713e+001 1.251358311e+001 2.2e-008 1.11 58 1.0e-005 1.1e-001 1.8e-004 1.00e+000 1.251310607e+001 1.251357945e+001 2.0e-008 1.11 59 9.4e-006 1.1e-001 1.7e-004 1.00e+000 1.251315011e+001 1.251357616e+001 1.8e-008 1.13 60 8.4e-006 1.1e-001 1.5e-004 1.00e+000 1.251318975e+001 1.251357320e+001 1.6e-008 1.13 61 7.6e-006 1.1e-001 1.3e-004 1.00e+000 1.251322543e+001 1.251357054e+001 1.4e-008 1.13 62 6.8e-006 1.1e-001 1.2e-004 1.00e+000 1.251325754e+001 1.251356814e+001 1.3e-008 1.13 63 6.2e-006 1.0e-001 1.1e-004 1.00e+000 1.251328644e+001 1.251356599e+001 1.2e-008 1.13 64 5.5e-006 1.0e-001 9.8e-005 1.00e+000 1.251331245e+001 1.251356405e+001 1.0e-008 1.13 65 5.0e-006 1.0e-001 8.8e-005 1.00e+000 1.251333587e+001 1.251356230e+001 9.4e-009 1.13 66 4.5e-006 1.0e-001 7.9e-005 1.00e+000 1.251335694e+001 1.251356073e+001 8.4e-009 1.14 67 4.0e-006 1.0e-001 7.1e-005 1.00e+000 1.251337590e+001 1.251355931e+001 7.6e-009 1.14 68 3.6e-006 1.0e-001 6.4e-005 1.00e+000 1.251339297e+001 1.251355804e+001 6.8e-009 1.14 69 3.3e-006 1.0e-001 5.8e-005 1.00e+000 1.251340833e+001 1.251355689e+001 6.1e-009 1.14 70 2.9e-006 1.0e-001 5.2e-005 1.00e+000 1.251342215e+001 1.251355586e+001 5.5e-009 1.14 71 2.6e-006 9.9e-002 4.7e-005 1.00e+000 1.251343460e+001 1.251355493e+001 5.0e-009 1.14 72 2.4e-006 9.9e-002 4.2e-005 1.00e+000 1.251344581e+001 1.251355409e+001 4.5e-009 1.14 73 2.1e-006 9.8e-002 3.8e-005 9.99e-001 1.251345588e+001 1.251355334e+001 4.0e-009 1.16 74 1.9e-006 9.8e-002 3.4e-005 1.00e+000 1.251346495e+001 1.251355267e+001 3.6e-009 1.16 75 1.7e-006 9.8e-002 3.1e-005 1.00e+000 1.251347311e+001 1.251355206e+001 3.3e-009 1.16 76 1.6e-006 9.8e-002 2.8e-005 1.00e+000 1.251348046e+001 1.251355151e+001 2.9e-009 1.16 77 1.4e-006 9.7e-002 2.5e-005 1.00e+000 1.251348707e+001 1.251355101e+001 2.6e-009 1.16 78 1.3e-006 9.7e-002 2.2e-005 1.00e+000 1.251349302e+001 1.251355057e+001 2.4e-009 1.17 79 1.1e-006 9.6e-002 2.0e-005 9.99e-001 1.251349828e+001 1.251355019e+001 2.1e-009 1.17 80 1.0e-006 9.6e-002 1.8e-005 1.00e+000 1.251350311e+001 1.251354983e+001 1.9e-009 1.17 81 9.2e-007 9.6e-002 1.6e-005 1.00e+000 1.251350746e+001 1.251354950e+001 1.7e-009 1.17 82 8.3e-007 9.6e-002 1.5e-005 9.99e-001 1.251351137e+001 1.251354921e+001 1.6e-009 1.17 83 7.5e-007 9.6e-002 1.3e-005 9.99e-001 1.251351489e+001 1.251354895e+001 1.4e-009 1.17 84 7.6e-008 9.8e-003 1.3e-006 1.00e+000 1.251354333e+001 1.251354681e+001 1.4e-010 1.19 85 4.6e-010 5.4e-005 7.6e-009 9.91e-001 1.251354655e+001 1.251354657e+001 1.3e-012 1.19 86 4.1e-010 4.9e-005 6.9e-009 1.04e+000 1.251354655e+001 1.251354657e+001 1.2e-012 1.19 87 3.9e-010 4.6e-005 6.4e-009 9.24e-001 1.251354656e+001 1.251354657e+001 1.1e-012 1.19 88 3.8e-010 4.6e-005 6.4e-009 8.50e-001 1.251354656e+001 1.251354657e+001 1.1e-012 1.19 89 3.5e-010 4.1e-005 5.8e-009 9.83e-001 1.251354656e+001 1.251354657e+001 1.0e-012 1.19 Interior-point optimizer terminated. Time: 1.20. Optimizer terminated. Time: 1.31 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.2513546557e+001 nrm: 1e+001 Viol. con: 2e-010 var: 0e+000 Dual. obj: 1.2513546572e+001 nrm: 9e+001 Viol. con: 0e+000 var: 2e-005 * End solution on dual form. * Transforming to primal solution. Solving took 1.33 seconds. result packing took 12% of solve time solution checking took 11% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 771 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 3 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.02 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 2 Optimizer - solved problem : the primal Optimizer - Constraints : 345 Optimizer - Cones : 0 Optimizer - Scalar variables : 1054 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.00 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.00 Factor - nonzeros before factor : 5894 after factor : 1.09e+004 Factor - dense dim. : 0 flops : 1.08e+005 Factor - GP saved nzs : 1.06e+004 GP saved flops : 1.18e+005 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.2e+003 4.0e+003 2.3e+004 0.00e+000 -2.313089756e+004 1.023181539e-012 1.0e+000 0.03 1 6.5e+002 2.1e+003 1.2e+004 2.59e-002 -1.531524357e+004 6.000660881e+000 5.4e-001 1.16 2 4.2e+002 1.4e+003 8.0e+003 7.75e-001 -9.393417252e+003 9.614365311e+000 3.6e-001 1.95 3 1.1e+002 3.7e+002 2.2e+003 1.10e+000 -2.279498501e+003 1.395778948e+001 1.1e-001 2.22 4 4.9e+001 1.6e+002 9.3e+002 1.74e+000 -7.571291598e+002 1.377098723e+001 4.7e-002 2.28 5 1.3e+001 4.4e+001 2.5e+002 1.40e+000 -1.651969057e+002 1.254360851e+001 1.3e-002 2.30 6 3.7e+000 1.4e+001 7.1e+001 1.13e+000 -3.756103941e+001 1.118113086e+001 4.3e-003 2.31 7 9.8e-001 9.3e+000 1.9e+001 1.04e+000 -2.048780333e+000 1.065205247e+001 1.3e-003 2.39 8 9.0e-001 1.1e+001 1.7e+001 7.91e-001 -1.456092312e+000 1.063799961e+001 1.2e-003 2.52 9 4.0e-001 1.1e+001 7.7e+000 7.32e-001 3.780602146e+000 1.050672845e+001 5.5e-004 2.55 10 3.2e-001 8.9e+000 6.2e+000 3.11e-001 4.368799450e+000 1.047713316e+001 4.5e-004 2.67 11 1.1e-001 3.2e+000 2.1e+000 4.12e-001 7.529575436e+000 1.033494958e+001 1.8e-004 2.80 12 2.4e-002 3.7e+000 4.8e-001 7.14e-001 9.493561020e+000 1.024454304e+001 5.0e-005 2.81 13 6.8e-003 3.5e+000 1.4e-001 9.11e-001 9.997497406e+000 1.021637510e+001 1.5e-005 2.91 14 2.1e-003 3.1e+000 4.3e-002 9.74e-001 1.013845413e+001 1.020775137e+001 5.0e-006 2.92 15 6.6e-004 3.0e+000 1.3e-002 9.92e-001 1.018326997e+001 1.020498367e+001 1.6e-006 3.06 16 2.1e-004 2.9e+000 4.1e-003 9.98e-001 1.019734893e+001 1.020409895e+001 5.0e-007 3.08 17 8.0e-005 2.6e+000 1.6e-003 9.99e-001 1.020123903e+001 1.020386519e+001 1.9e-007 3.09 18 7.2e-005 2.4e+000 1.4e-003 1.00e+000 1.020147949e+001 1.020384741e+001 1.7e-007 4.42 19 6.5e-005 2.2e+000 1.3e-003 1.00e+000 1.020170140e+001 1.020383292e+001 1.6e-007 4.45 20 5.8e-005 2.0e+000 1.2e-003 1.00e+000 1.020190184e+001 1.020382025e+001 1.4e-007 4.47 21 5.2e-005 1.8e+000 1.1e-003 1.00e+000 1.020208230e+001 1.020380889e+001 1.3e-007 4.47 22 4.7e-005 1.6e+000 9.5e-004 1.00e+000 1.020224477e+001 1.020379870e+001 1.1e-007 4.47 23 4.2e-005 1.5e+000 8.5e-004 1.00e+000 1.020239101e+001 1.020378956e+001 1.0e-007 4.47 24 3.8e-005 1.4e+000 7.7e-004 1.00e+000 1.020252265e+001 1.020378136e+001 9.3e-008 4.47 25 3.4e-005 1.2e+000 6.9e-004 1.00e+000 1.020264115e+001 1.020377399e+001 8.4e-008 4.47 26 3.1e-005 1.1e+000 6.2e-004 1.00e+000 1.020274782e+001 1.020376738e+001 7.5e-008 4.47 27 2.8e-005 1.0e+000 5.6e-004 1.00e+000 1.020284383e+001 1.020376144e+001 6.8e-008 4.48 28 2.5e-005 9.5e-001 5.0e-004 1.00e+000 1.020293025e+001 1.020375610e+001 6.1e-008 4.48 29 2.3e-005 8.7e-001 4.5e-004 1.00e+000 1.020300804e+001 1.020375131e+001 5.5e-008 4.50 30 2.0e-005 8.0e-001 4.1e-004 1.00e+000 1.020307806e+001 1.020374701e+001 4.9e-008 4.50 31 1.8e-005 7.4e-001 3.7e-004 1.00e+000 1.020314108e+001 1.020374314e+001 4.4e-008 4.50 32 1.6e-005 6.8e-001 3.3e-004 1.00e+000 1.020319781e+001 1.020373967e+001 4.0e-008 4.50 33 1.5e-005 6.3e-001 3.0e-004 1.00e+000 1.020324887e+001 1.020373654e+001 3.6e-008 4.50 34 1.3e-005 5.8e-001 2.7e-004 1.00e+000 1.020329483e+001 1.020373374e+001 3.2e-008 4.50 35 1.2e-005 5.4e-001 2.4e-004 1.00e+000 1.020333620e+001 1.020373122e+001 2.9e-008 4.50 36 1.1e-005 5.1e-001 2.2e-004 1.00e+000 1.020337343e+001 1.020372895e+001 2.6e-008 4.50 37 9.7e-006 4.7e-001 2.0e-004 1.00e+000 1.020340695e+001 1.020372691e+001 2.4e-008 4.50 38 8.7e-006 4.4e-001 1.8e-004 1.00e+000 1.020343711e+001 1.020372508e+001 2.1e-008 4.50 39 7.9e-006 4.2e-001 1.6e-004 1.00e+000 1.020346426e+001 1.020372344e+001 1.9e-008 4.50 40 7.1e-006 3.9e-001 1.4e-004 1.00e+000 1.020348870e+001 1.020372196e+001 1.7e-008 4.52 41 6.4e-006 3.7e-001 1.3e-004 1.00e+000 1.020351069e+001 1.020372062e+001 1.5e-008 4.52 42 5.7e-006 3.5e-001 1.2e-004 1.00e+000 1.020353049e+001 1.020371943e+001 1.4e-008 4.52 43 5.2e-006 3.3e-001 1.0e-004 1.00e+000 1.020354831e+001 1.020371835e+001 1.3e-008 4.52 44 5.5e-007 3.6e-002 1.1e-005 1.00e+000 1.020369162e+001 1.020370975e+001 1.3e-009 4.52 45 3.0e-008 2.0e-003 6.1e-007 1.00e+000 1.020370776e+001 1.020370877e+001 7.5e-011 4.52 46 3.7e-010 1.7e-005 5.5e-009 9.97e-001 1.020370870e+001 1.020370871e+001 5.6e-013 4.52 Interior-point optimizer terminated. Time: 4.52. Optimizer terminated. Time: 4.59 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0203708701e+001 nrm: 8e+000 Viol. con: 2e-010 var: 0e+000 Dual. obj: 1.0203708710e+001 nrm: 5e+001 Viol. con: 0e+000 var: 6e-006 * End solution on dual form. * Transforming to primal solution. Solving took 4.63 seconds. result packing took 4.2% of solve time solution checking took 1.1% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 771 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 3 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.03 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 2 Optimizer - solved problem : the primal Optimizer - Constraints : 345 Optimizer - Cones : 0 Optimizer - Scalar variables : 1054 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 5894 after factor : 1.09e+004 Factor - dense dim. : 0 flops : 1.08e+005 Factor - GP saved nzs : 1.06e+004 GP saved flops : 1.18e+005 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.9e+003 4.0e+003 2.3e+004 0.00e+000 -2.318780625e+004 1.023181539e-012 1.0e+000 0.05 1 9.3e+002 2.0e+003 1.1e+004 -3.82e-002 -1.486259405e+004 6.449434567e+000 5.0e-001 1.34 2 7.6e+002 1.6e+003 9.3e+003 8.13e-001 -1.147556012e+004 8.473072341e+000 4.1e-001 2.80 3 4.0e+002 8.6e+002 4.9e+003 9.96e-001 -5.785428842e+003 1.205881614e+001 2.2e-001 3.36 4 1.2e+002 2.5e+002 1.5e+003 1.51e+000 -1.302194664e+003 1.412028616e+001 7.2e-002 4.22 5 3.7e+001 7.8e+001 4.5e+002 1.59e+000 -3.102918143e+002 1.328592694e+001 2.3e-002 4.27 6 1.1e+001 2.6e+001 1.4e+002 1.16e+000 -8.203050647e+001 1.173299850e+001 7.8e-003 4.39 7 2.6e+000 9.8e+000 3.3e+001 1.05e+000 -1.099723812e+001 1.080415150e+001 2.1e-003 4.52 8 1.4e+000 1.3e+001 1.8e+001 9.24e-001 -1.866295237e+000 1.065887325e+001 1.2e-003 4.55 9 1.3e+000 1.4e+001 1.6e+001 6.47e-001 -1.309206269e+000 1.063938178e+001 1.1e-003 4.63 10 5.2e-001 8.3e+000 6.5e+000 5.94e-001 3.823146097e+000 1.047743821e+001 4.8e-004 4.66 11 3.1e-001 9.5e+000 3.9e+000 5.20e-001 5.730524261e+000 1.040036620e+001 3.0e-004 4.67 12 9.4e-002 4.5e+000 1.2e+000 5.36e-001 8.519937702e+000 1.028187367e+001 1.1e-004 4.75 13 1.8e-002 4.4e+000 2.3e-001 8.09e-001 9.842804571e+000 1.021297482e+001 2.6e-005 4.88 14 3.8e-003 4.3e+000 5.0e-002 9.66e-001 1.011470740e+001 1.019608888e+001 6.3e-006 4.91 15 1.4e-003 3.1e+000 1.9e-002 9.95e-001 1.016249705e+001 1.019305035e+001 2.4e-006 4.92 16 4.3e-004 2.7e+000 5.7e-003 9.98e-001 1.018241238e+001 1.019171451e+001 7.4e-007 4.92 17 1.2e-004 2.7e+000 1.6e-003 9.99e-001 1.018871041e+001 1.019130441e+001 2.1e-007 5.55 18 3.9e-005 2.4e+000 5.1e-004 1.00e+000 1.019036740e+001 1.019119980e+001 6.7e-008 6.38 19 1.2e-005 2.3e+000 1.6e-004 1.00e+000 1.019090465e+001 1.019116684e+001 2.1e-008 6.39 20 1.1e-005 2.1e+000 1.4e-004 1.00e+000 1.019092875e+001 1.019116527e+001 1.9e-008 7.36 21 9.8e-006 1.9e+000 1.3e-004 1.00e+000 1.019095097e+001 1.019116390e+001 1.7e-008 8.70 22 8.9e-006 1.7e+000 1.2e-004 1.00e+000 1.019097103e+001 1.019116266e+001 1.5e-008 9.89 23 8.0e-006 1.6e+000 1.0e-004 1.00e+000 1.019098909e+001 1.019116155e+001 1.4e-008 10.28 24 7.2e-006 1.4e+000 9.4e-005 1.00e+000 1.019100534e+001 1.019116056e+001 1.2e-008 10.30 25 6.5e-006 1.3e+000 8.5e-005 1.00e+000 1.019101997e+001 1.019115966e+001 1.1e-008 10.31 26 5.8e-006 1.2e+000 7.6e-005 1.00e+000 1.019103313e+001 1.019115885e+001 1.0e-008 11.14 27 5.2e-006 1.1e+000 6.9e-005 1.00e+000 1.019104498e+001 1.019115813e+001 9.1e-009 11.55 28 4.7e-006 1.0e+000 6.2e-005 1.00e+000 1.019105565e+001 1.019115748e+001 8.2e-009 11.59 29 4.2e-006 9.2e-001 5.6e-005 1.00e+000 1.019106525e+001 1.019115689e+001 7.4e-009 11.64 30 3.8e-006 8.5e-001 5.0e-005 1.00e+000 1.019107388e+001 1.019115637e+001 6.6e-009 11.84 31 3.4e-006 7.8e-001 4.5e-005 1.00e+000 1.019108166e+001 1.019115589e+001 6.0e-009 11.89 32 3.1e-006 7.2e-001 4.0e-005 1.00e+000 1.019108866e+001 1.019115547e+001 5.4e-009 11.91 33 2.8e-006 6.6e-001 3.6e-005 1.00e+000 1.019109496e+001 1.019115508e+001 4.8e-009 11.91 34 2.5e-006 6.1e-001 3.3e-005 1.00e+000 1.019110063e+001 1.019115474e+001 4.3e-009 11.91 35 2.3e-006 5.7e-001 3.0e-005 1.00e+000 1.019110573e+001 1.019115443e+001 3.9e-009 11.92 36 2.0e-006 5.3e-001 2.7e-005 9.99e-001 1.019111032e+001 1.019115415e+001 3.5e-009 12.00 37 1.8e-006 4.9e-001 2.4e-005 1.00e+000 1.019111446e+001 1.019115390e+001 3.2e-009 12.02 38 1.6e-006 4.6e-001 2.2e-005 9.98e-001 1.019111817e+001 1.019115368e+001 2.9e-009 12.03 39 1.5e-006 4.3e-001 1.9e-005 9.99e-001 1.019112152e+001 1.019115348e+001 2.6e-009 12.03 40 1.3e-006 4.0e-001 1.7e-005 1.00e+000 1.019112454e+001 1.019115329e+001 2.3e-009 12.03 41 1.2e-006 3.8e-001 1.6e-005 9.99e-001 1.019112725e+001 1.019115313e+001 2.1e-009 12.03 42 1.1e-006 3.6e-001 1.4e-005 1.00e+000 1.019112969e+001 1.019115298e+001 1.9e-009 12.03 43 9.7e-007 3.4e-001 1.3e-005 9.97e-001 1.019113189e+001 1.019115285e+001 1.7e-009 12.03 44 8.7e-007 3.2e-001 1.1e-005 1.00e+000 1.019113387e+001 1.019115273e+001 1.5e-009 12.05 45 7.9e-007 3.1e-001 1.0e-005 1.00e+000 1.019113564e+001 1.019115263e+001 1.4e-009 12.05 46 7.1e-007 2.9e-001 9.3e-006 1.00e+000 1.019113724e+001 1.019115253e+001 1.2e-009 12.05 47 6.4e-007 2.8e-001 8.3e-006 1.00e+000 1.019113868e+001 1.019115244e+001 1.1e-009 12.05 48 5.7e-007 2.7e-001 7.5e-006 1.00e+000 1.019113999e+001 1.019115236e+001 1.0e-009 12.05 49 5.2e-007 2.6e-001 6.8e-006 1.00e+000 1.019114116e+001 1.019115229e+001 9.0e-010 12.05 50 4.6e-007 2.5e-001 6.1e-006 9.95e-001 1.019114220e+001 1.019115223e+001 8.1e-010 12.06 51 4.2e-007 2.4e-001 5.5e-006 1.00e+000 1.019114315e+001 1.019115217e+001 7.3e-010 12.06 52 3.8e-007 2.4e-001 4.9e-006 1.01e+000 1.019114404e+001 1.019115212e+001 6.6e-010 12.06 53 3.4e-007 2.3e-001 4.4e-006 1.02e+000 1.019114485e+001 1.019115207e+001 5.9e-010 12.06 54 3.0e-007 2.3e-001 4.0e-006 9.99e-001 1.019114553e+001 1.019115203e+001 5.4e-010 12.06 55 2.7e-007 2.2e-001 3.6e-006 9.98e-001 1.019114614e+001 1.019115199e+001 4.8e-010 12.08 56 2.5e-007 2.1e-001 3.2e-006 9.94e-001 1.019114669e+001 1.019115196e+001 4.3e-010 12.08 57 2.2e-007 1.9e-001 2.9e-006 1.05e+000 1.019114730e+001 1.019115192e+001 4.0e-010 12.08 58 2.0e-007 1.7e-001 2.6e-006 1.03e+000 1.019114779e+001 1.019115189e+001 3.6e-010 12.08 59 1.8e-007 1.6e-001 2.4e-006 1.01e+000 1.019114818e+001 1.019115187e+001 3.3e-010 12.08 60 1.6e-007 1.4e-001 2.1e-006 1.01e+000 1.019114853e+001 1.019115185e+001 3.0e-010 12.09 61 1.5e-007 1.3e-001 1.9e-006 1.04e+000 1.019114891e+001 1.019115183e+001 2.7e-010 12.17 62 1.3e-007 1.1e-001 1.7e-006 1.02e+000 1.019114921e+001 1.019115181e+001 2.5e-010 12.19 63 1.2e-007 1.0e-001 1.5e-006 1.07e+000 1.019114954e+001 1.019115179e+001 2.3e-010 12.20 64 1.1e-007 9.2e-002 1.4e-006 1.03e+000 1.019114978e+001 1.019115177e+001 2.1e-010 12.33 65 9.6e-008 8.3e-002 1.3e-006 9.77e-001 1.019114997e+001 1.019115176e+001 1.9e-010 12.34 66 8.6e-008 7.5e-002 1.1e-006 1.01e+000 1.019115015e+001 1.019115175e+001 1.7e-010 12.36 67 7.7e-008 6.7e-002 1.0e-006 1.05e+000 1.019115034e+001 1.019115174e+001 1.6e-010 12.39 68 7.0e-008 6.1e-002 9.1e-007 1.07e+000 1.019115051e+001 1.019115173e+001 1.5e-010 12.41 69 8.7e-009 6.9e-003 1.0e-007 1.07e+000 1.019115154e+001 1.019115167e+001 1.6e-011 12.42 70 5.9e-010 3.8e-004 5.8e-009 9.93e-001 1.019115166e+001 1.019115166e+001 9.4e-013 12.44 Interior-point optimizer terminated. Time: 12.44. Optimizer terminated. Time: 12.77 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0191151655e+001 nrm: 8e+000 Viol. con: 3e-010 var: 0e+000 Dual. obj: 1.0191151663e+001 nrm: 6e+001 Viol. con: 0e+000 var: 9e-005 * End solution on dual form. * Transforming to primal solution. Solving took 12.8 seconds. result packing took 1.2% of solve time solution checking took 0.43% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 771 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 3 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.05 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 2 Optimizer - solved problem : the primal Optimizer - Constraints : 345 Optimizer - Cones : 0 Optimizer - Scalar variables : 1054 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 5894 after factor : 1.09e+004 Factor - dense dim. : 0 flops : 1.08e+005 Factor - GP saved nzs : 1.06e+004 GP saved flops : 1.18e+005 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.9e+003 4.0e+003 2.3e+004 0.00e+000 -2.319472374e+004 1.023181539e-012 1.0e+000 0.06 1 9.6e+002 2.0e+003 1.2e+004 -4.04e-002 -1.524651211e+004 6.152724343e+000 5.2e-001 0.06 2 7.8e+002 1.7e+003 9.5e+003 7.71e-001 -1.178116294e+004 8.257345261e+000 4.2e-001 0.09 3 3.9e+002 8.2e+002 4.7e+003 9.63e-001 -5.579793628e+003 1.220856198e+001 2.2e-001 0.09 4 1.4e+002 2.9e+002 1.7e+003 1.56e+000 -1.515377565e+003 1.397192810e+001 8.2e-002 0.09 5 3.7e+001 8.0e+001 4.6e+002 1.60e+000 -3.079894803e+002 1.331579286e+001 2.3e-002 0.09 6 1.1e+001 2.4e+001 1.3e+002 1.14e+000 -7.788807779e+001 1.165664941e+001 7.5e-003 0.09 7 2.4e+000 1.0e+001 3.0e+001 1.04e+000 -9.289269188e+000 1.074056165e+001 2.0e-003 0.14 8 1.4e+000 1.6e+001 1.7e+001 8.97e-001 -1.314059805e+000 1.061005911e+001 1.1e-003 0.16 9 1.1e+000 1.8e+001 1.4e+001 6.18e-001 -1.727767435e-001 1.057105316e+001 9.2e-004 0.16 10 3.9e-001 9.2e+000 4.9e+000 5.47e-001 5.042572170e+000 1.040315117e+001 3.8e-004 0.16 11 2.3e-001 9.6e+000 2.9e+000 5.64e-001 6.656685519e+000 1.033835325e+001 2.4e-004 0.16 12 5.6e-002 4.4e+000 7.1e-001 6.08e-001 9.157343594e+000 1.022965037e+001 7.1e-005 0.16 13 1.8e-002 3.2e+000 2.4e-001 8.62e-001 9.819216709e+000 1.019153201e+001 2.5e-005 0.17 14 1.1e-002 3.0e+000 1.4e-001 9.60e-001 9.967999574e+000 1.018350048e+001 1.5e-005 0.17 15 2.8e-003 2.9e+000 3.5e-002 9.74e-001 1.011661896e+001 1.017372046e+001 4.1e-006 0.17 16 7.8e-004 2.8e+000 1.0e-002 9.95e-001 1.015492483e+001 1.017122320e+001 1.2e-006 0.17 17 2.7e-004 2.6e+000 3.5e-003 9.99e-001 1.016486578e+001 1.017060230e+001 4.2e-007 0.17 18 1.1e-004 2.1e+000 1.5e-003 1.00e+000 1.016802392e+001 1.017040547e+001 1.7e-007 0.17 19 1.0e-004 2.0e+000 1.3e-003 1.00e+000 1.016824654e+001 1.017039365e+001 1.6e-007 0.19 20 9.2e-005 1.8e+000 1.2e-003 1.00e+000 1.016844778e+001 1.017038047e+001 1.4e-007 0.19 21 8.3e-005 1.7e+000 1.1e-003 1.00e+000 1.016862944e+001 1.017036892e+001 1.3e-007 0.19 22 7.5e-005 1.5e+000 9.7e-004 1.00e+000 1.016879296e+001 1.017035851e+001 1.1e-007 0.19 23 6.7e-005 1.4e+000 8.7e-004 1.00e+000 1.016894016e+001 1.017034916e+001 1.0e-007 0.19 24 6.1e-005 1.3e+000 7.8e-004 1.00e+000 1.016907265e+001 1.017034077e+001 9.2e-008 0.19 25 5.5e-005 1.2e+000 7.0e-004 1.00e+000 1.016919192e+001 1.017033324e+001 8.3e-008 0.20 26 4.9e-005 1.1e+000 6.3e-004 1.00e+000 1.016929927e+001 1.017032647e+001 7.5e-008 0.20 27 4.4e-005 9.7e-001 5.7e-004 1.00e+000 1.016939590e+001 1.017032039e+001 6.7e-008 0.20 28 4.0e-005 8.9e-001 5.1e-004 1.00e+000 1.016948288e+001 1.017031493e+001 6.1e-008 0.20 29 3.6e-005 8.2e-001 4.6e-004 1.00e+000 1.016956117e+001 1.017031002e+001 5.5e-008 0.20 30 3.2e-005 7.6e-001 4.2e-004 1.00e+000 1.016963164e+001 1.017030561e+001 4.9e-008 0.20 31 2.9e-005 7.0e-001 3.7e-004 1.00e+000 1.016969507e+001 1.017030165e+001 4.4e-008 0.20 32 2.6e-005 6.5e-001 3.4e-004 1.00e+000 1.016975216e+001 1.017029808e+001 4.0e-008 0.22 33 2.3e-005 6.0e-001 3.0e-004 1.00e+000 1.016980355e+001 1.017029488e+001 3.6e-008 0.22 34 2.1e-005 5.6e-001 2.7e-004 1.00e+000 1.016984980e+001 1.017029200e+001 3.2e-008 0.22 35 1.9e-005 5.2e-001 2.5e-004 1.00e+000 1.016989143e+001 1.017028942e+001 2.9e-008 0.22 36 1.7e-005 4.8e-001 2.2e-004 1.00e+000 1.016992890e+001 1.017028709e+001 2.6e-008 0.22 37 1.5e-005 4.5e-001 2.0e-004 1.00e+000 1.016996262e+001 1.017028500e+001 2.3e-008 0.22 38 1.4e-005 4.3e-001 1.8e-004 1.00e+000 1.016999297e+001 1.017028312e+001 2.1e-008 0.23 39 1.2e-005 4.0e-001 1.6e-004 1.00e+000 1.017002029e+001 1.017028142e+001 1.9e-008 0.23 40 1.1e-005 3.8e-001 1.5e-004 1.00e+000 1.017004488e+001 1.017027990e+001 1.7e-008 0.23 41 1.0e-005 3.6e-001 1.3e-004 1.00e+000 1.017006702e+001 1.017027853e+001 1.5e-008 0.23 42 9.1e-006 3.4e-001 1.2e-004 1.00e+000 1.017008693e+001 1.017027730e+001 1.4e-008 0.23 43 8.2e-006 3.2e-001 1.1e-004 1.00e+000 1.017010486e+001 1.017027619e+001 1.2e-008 0.23 44 7.4e-006 3.1e-001 9.5e-005 1.00e+000 1.017012100e+001 1.017027519e+001 1.1e-008 0.23 45 6.6e-006 3.0e-001 8.6e-005 1.00e+000 1.017013552e+001 1.017027430e+001 1.0e-008 0.25 46 6.0e-006 2.8e-001 7.7e-005 1.00e+000 1.017014859e+001 1.017027349e+001 9.1e-009 0.25 47 5.4e-006 2.7e-001 6.9e-005 1.00e+000 1.017016035e+001 1.017027276e+001 8.2e-009 0.25 48 4.8e-006 2.6e-001 6.2e-005 1.00e+000 1.017017094e+001 1.017027211e+001 7.4e-009 0.25 49 4.3e-006 2.5e-001 5.6e-005 1.00e+000 1.017018047e+001 1.017027152e+001 6.6e-009 0.25 50 3.9e-006 2.5e-001 5.1e-005 1.00e+000 1.017018904e+001 1.017027099e+001 6.0e-009 0.25 51 3.5e-006 2.4e-001 4.6e-005 1.00e+000 1.017019676e+001 1.017027051e+001 5.4e-009 0.25 52 3.2e-006 2.3e-001 4.1e-005 1.00e+000 1.017020371e+001 1.017027009e+001 4.8e-009 0.27 53 2.9e-006 2.3e-001 3.7e-005 1.00e+000 1.017020996e+001 1.017026970e+001 4.4e-009 0.27 54 2.6e-006 2.2e-001 3.3e-005 1.00e+000 1.017021558e+001 1.017026935e+001 3.9e-009 0.27 55 2.3e-006 2.2e-001 3.0e-005 1.00e+000 1.017022065e+001 1.017026904e+001 3.5e-009 0.27 56 2.1e-006 2.1e-001 2.7e-005 1.00e+000 1.017022520e+001 1.017026876e+001 3.2e-009 0.27 57 1.9e-006 2.1e-001 2.4e-005 1.00e+000 1.017022931e+001 1.017026850e+001 2.9e-009 0.27 58 1.7e-006 2.1e-001 2.2e-005 1.00e+000 1.017023300e+001 1.017026828e+001 2.6e-009 0.28 59 1.5e-006 2.0e-001 2.0e-005 9.99e-001 1.017023632e+001 1.017026807e+001 2.3e-009 0.28 60 1.4e-006 2.0e-001 1.8e-005 9.98e-001 1.017023931e+001 1.017026789e+001 2.1e-009 0.28 61 1.2e-006 2.0e-001 1.6e-005 9.98e-001 1.017024200e+001 1.017026772e+001 1.9e-009 0.28 62 1.1e-006 2.0e-001 1.4e-005 9.99e-001 1.017024442e+001 1.017026757e+001 1.7e-009 0.28 63 1.0e-006 2.0e-001 1.3e-005 1.00e+000 1.017024660e+001 1.017026743e+001 1.5e-009 0.28 64 9.0e-007 1.9e-001 1.2e-005 9.99e-001 1.017024855e+001 1.017026732e+001 1.4e-009 0.30 65 8.1e-007 1.9e-001 1.0e-005 1.00e+000 1.017025033e+001 1.017026720e+001 1.2e-009 0.30 66 7.3e-007 1.9e-001 9.4e-006 9.99e-001 1.017025193e+001 1.017026710e+001 1.1e-009 0.30 67 6.5e-007 1.9e-001 8.4e-006 1.00e+000 1.017025336e+001 1.017026701e+001 1.0e-009 0.30 68 5.9e-007 1.9e-001 7.6e-006 1.00e+000 1.017025465e+001 1.017026693e+001 9.0e-010 0.30 69 5.3e-007 1.9e-001 6.8e-006 9.99e-001 1.017025580e+001 1.017026686e+001 8.1e-010 0.31 70 4.8e-007 1.9e-001 6.2e-006 1.01e+000 1.017025686e+001 1.017026680e+001 7.3e-010 0.31 71 4.3e-007 1.9e-001 5.5e-006 1.00e+000 1.017025780e+001 1.017026674e+001 6.5e-010 0.31 72 3.9e-007 1.9e-001 5.0e-006 9.93e-001 1.017025864e+001 1.017026669e+001 5.9e-010 0.31 73 3.5e-007 1.8e-001 4.5e-006 1.00e+000 1.017025939e+001 1.017026664e+001 5.3e-010 0.31 74 3.1e-007 1.8e-001 4.0e-006 9.93e-001 1.017026007e+001 1.017026660e+001 4.8e-010 0.31 75 2.8e-007 1.8e-001 3.6e-006 9.93e-001 1.017026069e+001 1.017026656e+001 4.3e-010 0.31 76 2.5e-007 1.8e-001 3.3e-006 9.99e-001 1.017026124e+001 1.017026653e+001 3.9e-010 0.33 77 2.3e-007 1.8e-001 2.9e-006 1.00e+000 1.017026174e+001 1.017026649e+001 3.5e-010 0.33 78 2.1e-007 1.8e-001 2.6e-006 9.83e-001 1.017026219e+001 1.017026647e+001 3.1e-010 0.33 79 1.8e-007 1.8e-001 2.4e-006 9.85e-001 1.017026259e+001 1.017026644e+001 2.8e-010 0.33 80 1.7e-007 1.6e-001 2.1e-006 1.01e+000 1.017026296e+001 1.017026642e+001 2.5e-010 0.33 81 1.5e-007 1.5e-001 1.9e-006 9.93e-001 1.017026328e+001 1.017026640e+001 2.3e-010 0.33 82 3.3e-008 3.2e-002 4.2e-007 1.02e+000 1.017026559e+001 1.017026625e+001 4.8e-011 0.33 83 2.5e-009 2.2e-003 2.9e-008 9.80e-001 1.017026617e+001 1.017026622e+001 4.4e-012 0.34 84 2.7e-010 1.6e-004 2.2e-009 9.96e-001 1.017026621e+001 1.017026622e+001 6.3e-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: 1.0170266213e+001 nrm: 8e+000 Viol. con: 3e-010 var: 0e+000 Dual. obj: 1.0170266217e+001 nrm: 6e+001 Viol. con: 0e+000 var: 5e-005 * End solution on dual form. * Transforming to primal solution. Solving took 0.409 seconds. result packing took 47% of solve time solution checking took 15% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 770 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 3 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 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 : 346 Optimizer - Cones : 0 Optimizer - Scalar variables : 1055 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 5889 after factor : 1.09e+004 Factor - dense dim. : 0 flops : 1.09e+005 Factor - GP saved nzs : 1.06e+004 GP saved flops : 1.18e+005 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 1.9e+003 4.0e+003 2.3e+004 0.00e+000 -2.322140314e+004 1.023181539e-012 1.0e+000 0.06 1 9.7e+002 2.0e+003 1.2e+004 -4.21e-002 -1.528607192e+004 6.134862402e+000 5.2e-001 0.06 2 7.8e+002 1.6e+003 9.5e+003 7.68e-001 -1.171628487e+004 8.305805600e+000 4.2e-001 0.06 3 3.9e+002 8.2e+002 4.7e+003 9.69e-001 -5.544228076e+003 1.222793140e+001 2.1e-001 0.06 4 1.4e+002 2.9e+002 1.7e+003 1.57e+000 -1.509235971e+003 1.396895548e+001 8.1e-002 0.08 5 3.7e+001 7.9e+001 4.5e+002 1.60e+000 -3.045599872e+002 1.330796373e+001 2.3e-002 0.08 6 1.1e+001 2.4e+001 1.3e+002 1.13e+000 -7.757489262e+001 1.165073918e+001 7.5e-003 0.08 7 2.4e+000 1.0e+001 3.0e+001 1.04e+000 -9.074963415e+000 1.073636903e+001 1.9e-003 0.08 8 1.4e+000 1.7e+001 1.7e+001 8.95e-001 -1.181718452e+000 1.060628482e+001 1.1e-003 0.08 9 1.1e+000 1.8e+001 1.4e+001 6.09e-001 -1.023717652e-001 1.056876989e+001 9.2e-004 0.08 10 3.9e-001 9.5e+000 4.8e+000 5.42e-001 5.089854191e+000 1.039995881e+001 3.8e-004 0.09 11 2.3e-001 9.9e+000 2.9e+000 5.69e-001 6.689129745e+000 1.033596820e+001 2.3e-004 0.09 12 5.5e-002 4.5e+000 6.9e-001 6.20e-001 9.192726267e+000 1.022754582e+001 6.9e-005 0.09 13 1.7e-002 3.3e+000 2.2e-001 8.67e-001 9.844836677e+000 1.018991259e+001 2.4e-005 0.09 14 1.0e-002 3.0e+000 1.3e-001 9.63e-001 9.980097016e+000 1.018260322e+001 1.4e-005 0.09 15 2.6e-003 2.9e+000 3.3e-002 9.76e-001 1.011969435e+001 1.017338839e+001 3.9e-006 0.09 16 7.6e-004 2.8e+000 9.7e-003 9.95e-001 1.015545411e+001 1.017105611e+001 1.1e-006 0.11 17 2.4e-004 2.7e+000 3.1e-003 9.99e-001 1.016545582e+001 1.017042376e+001 3.7e-007 0.11 18 1.0e-004 2.2e+000 1.3e-003 1.00e+000 1.016818877e+001 1.017025229e+001 1.5e-007 0.11 19 9.0e-005 2.1e+000 1.2e-003 1.00e+000 1.016838135e+001 1.017024187e+001 1.4e-007 0.11 20 8.1e-005 1.9e+000 1.0e-003 1.00e+000 1.016855566e+001 1.017023040e+001 1.2e-007 0.11 21 7.3e-005 1.7e+000 9.3e-004 1.00e+000 1.016871302e+001 1.017022035e+001 1.1e-007 0.11 22 6.5e-005 1.5e+000 8.4e-004 1.00e+000 1.016885468e+001 1.017021128e+001 1.0e-007 0.13 23 5.9e-005 1.4e+000 7.6e-004 1.00e+000 1.016898219e+001 1.017020315e+001 9.1e-008 0.13 24 5.3e-005 1.3e+000 6.8e-004 1.00e+000 1.016909696e+001 1.017019584e+001 8.1e-008 0.13 25 4.8e-005 1.2e+000 6.1e-004 1.00e+000 1.016920027e+001 1.017018927e+001 7.3e-008 0.13 26 4.3e-005 1.1e+000 5.5e-004 1.00e+000 1.016929327e+001 1.017018338e+001 6.6e-008 0.13 27 3.9e-005 9.9e-001 5.0e-004 1.00e+000 1.016937697e+001 1.017017808e+001 5.9e-008 0.13 28 3.5e-005 9.0e-001 4.5e-004 1.00e+000 1.016945232e+001 1.017017332e+001 5.3e-008 0.13 29 3.1e-005 8.3e-001 4.0e-004 1.00e+000 1.016952013e+001 1.017016904e+001 4.8e-008 0.13 30 2.8e-005 7.7e-001 3.6e-004 1.00e+000 1.016958117e+001 1.017016519e+001 4.3e-008 0.14 31 2.5e-005 7.1e-001 3.3e-004 1.00e+000 1.016963611e+001 1.017016174e+001 3.9e-008 0.14 32 2.3e-005 6.5e-001 2.9e-004 1.00e+000 1.016968556e+001 1.017015863e+001 3.5e-008 0.14 33 2.1e-005 6.1e-001 2.6e-004 1.00e+000 1.016973007e+001 1.017015583e+001 3.2e-008 0.14 34 1.8e-005 5.6e-001 2.4e-004 1.00e+000 1.016977013e+001 1.017015332e+001 2.8e-008 0.14 35 1.7e-005 5.2e-001 2.1e-004 1.00e+000 1.016980619e+001 1.017015106e+001 2.6e-008 0.14 36 1.5e-005 4.9e-001 1.9e-004 1.00e+000 1.016983864e+001 1.017014903e+001 2.3e-008 0.16 37 1.3e-005 4.6e-001 1.7e-004 1.00e+000 1.016986785e+001 1.017014720e+001 2.1e-008 0.16 38 1.2e-005 4.3e-001 1.6e-004 1.00e+000 1.016989414e+001 1.017014556e+001 1.9e-008 0.16 39 1.1e-005 4.0e-001 1.4e-004 1.00e+000 1.016991780e+001 1.017014408e+001 1.7e-008 0.16 40 9.8e-006 3.8e-001 1.3e-004 1.00e+000 1.016993910e+001 1.017014275e+001 1.5e-008 0.16 41 8.8e-006 3.6e-001 1.1e-004 1.00e+000 1.016995827e+001 1.017014155e+001 1.4e-008 0.16 42 7.9e-006 3.4e-001 1.0e-004 1.00e+000 1.016997552e+001 1.017014048e+001 1.2e-008 0.16 43 7.2e-006 3.3e-001 9.2e-005 1.00e+000 1.016999105e+001 1.017013951e+001 1.1e-008 0.16 44 6.4e-006 3.1e-001 8.3e-005 1.00e+000 1.017000502e+001 1.017013864e+001 9.9e-009 0.17 45 5.8e-006 3.0e-001 7.4e-005 1.00e+000 1.017001760e+001 1.017013785e+001 8.9e-009 0.17 46 5.2e-006 2.9e-001 6.7e-005 1.00e+000 1.017002892e+001 1.017013715e+001 8.0e-009 0.17 47 4.7e-006 2.8e-001 6.0e-005 1.00e+000 1.017003911e+001 1.017013651e+001 7.2e-009 0.17 48 4.2e-006 2.7e-001 5.4e-005 1.00e+000 1.017004828e+001 1.017013594e+001 6.5e-009 0.17 49 3.8e-006 2.6e-001 4.9e-005 1.00e+000 1.017005653e+001 1.017013542e+001 5.9e-009 0.17 50 3.4e-006 2.5e-001 4.4e-005 1.00e+000 1.017006395e+001 1.017013496e+001 5.3e-009 0.17 51 3.1e-006 2.4e-001 4.0e-005 1.00e+000 1.017007063e+001 1.017013454e+001 4.7e-009 0.17 52 2.8e-006 2.4e-001 3.6e-005 9.99e-001 1.017007665e+001 1.017013417e+001 4.3e-009 0.19 53 2.5e-006 2.3e-001 3.2e-005 1.00e+000 1.017008206e+001 1.017013383e+001 3.8e-009 0.19 54 2.2e-006 2.2e-001 2.9e-005 9.99e-001 1.017008693e+001 1.017013353e+001 3.5e-009 0.19 55 2.0e-006 2.2e-001 2.6e-005 1.00e+000 1.017009132e+001 1.017013325e+001 3.1e-009 0.19 56 1.8e-006 2.2e-001 2.3e-005 1.00e+000 1.017009526e+001 1.017013301e+001 2.8e-009 0.19 57 1.6e-006 2.1e-001 2.1e-005 1.00e+000 1.017009881e+001 1.017013279e+001 2.5e-009 0.19 58 1.5e-006 2.1e-001 1.9e-005 1.00e+000 1.017010201e+001 1.017013259e+001 2.3e-009 0.19 59 1.3e-006 2.1e-001 1.7e-005 9.98e-001 1.017010488e+001 1.017013241e+001 2.0e-009 0.19 60 1.2e-006 2.0e-001 1.5e-005 9.99e-001 1.017010747e+001 1.017013224e+001 1.8e-009 0.19 61 1.1e-006 2.0e-001 1.4e-005 1.00e+000 1.017010980e+001 1.017013210e+001 1.7e-009 0.20 62 9.7e-007 2.0e-001 1.2e-005 1.00e+000 1.017011190e+001 1.017013197e+001 1.5e-009 0.20 63 8.7e-007 2.0e-001 1.1e-005 1.00e+000 1.017011380e+001 1.017013185e+001 1.3e-009 0.20 64 7.8e-007 2.0e-001 1.0e-005 1.00e+000 1.017011551e+001 1.017013174e+001 1.2e-009 0.20 65 7.0e-007 1.9e-001 9.0e-006 1.00e+000 1.017011704e+001 1.017013164e+001 1.1e-009 0.20 66 6.3e-007 1.9e-001 8.1e-006 1.00e+000 1.017011841e+001 1.017013156e+001 9.8e-010 0.20 67 5.7e-007 1.9e-001 7.3e-006 1.00e+000 1.017011966e+001 1.017013148e+001 8.8e-010 0.20 68 5.1e-007 1.7e-001 6.6e-006 1.01e+000 1.017012080e+001 1.017013141e+001 7.9e-010 0.20 69 4.6e-007 1.5e-001 5.9e-006 1.00e+000 1.017012180e+001 1.017013134e+001 7.1e-010 0.20 70 4.2e-007 1.4e-001 5.3e-006 1.01e+000 1.017012273e+001 1.017013129e+001 6.4e-010 0.20 71 3.7e-007 1.3e-001 4.8e-006 1.01e+000 1.017012355e+001 1.017013123e+001 5.8e-010 0.22 72 3.4e-007 1.1e-001 4.3e-006 1.00e+000 1.017012428e+001 1.017013119e+001 5.2e-010 0.22 73 3.0e-007 1.0e-001 3.9e-006 9.98e-001 1.017012493e+001 1.017013115e+001 4.7e-010 0.22 74 2.7e-007 9.1e-002 3.5e-006 1.00e+000 1.017012551e+001 1.017013111e+001 4.2e-010 0.22 75 2.5e-007 8.2e-002 3.2e-006 1.02e+000 1.017012607e+001 1.017013108e+001 3.8e-010 0.22 76 2.2e-007 7.4e-002 2.8e-006 9.96e-001 1.017012654e+001 1.017013105e+001 3.5e-010 0.22 77 2.0e-007 6.7e-002 2.6e-006 1.01e+000 1.017012697e+001 1.017013102e+001 3.1e-010 0.22 78 1.8e-007 6.0e-002 2.3e-006 9.81e-001 1.017012735e+001 1.017013100e+001 2.8e-010 0.22 79 1.6e-007 5.4e-002 2.1e-006 1.02e+000 1.017012771e+001 1.017013097e+001 2.5e-010 0.23 80 1.5e-007 4.9e-002 1.9e-006 1.01e+000 1.017012803e+001 1.017013095e+001 2.3e-010 0.23 81 1.3e-007 4.4e-002 1.7e-006 1.01e+000 1.017012831e+001 1.017013094e+001 2.1e-010 0.23 82 1.2e-007 3.9e-002 1.5e-006 1.01e+000 1.017012857e+001 1.017013092e+001 1.9e-010 0.23 83 1.1e-007 3.5e-002 1.4e-006 9.82e-001 1.017012880e+001 1.017013090e+001 1.7e-010 0.23 84 9.5e-008 3.2e-002 1.2e-006 1.01e+000 1.017012900e+001 1.017013089e+001 1.5e-010 0.23 85 8.6e-008 2.9e-002 1.1e-006 9.64e-001 1.017012918e+001 1.017013088e+001 1.4e-010 0.23 86 7.7e-008 2.6e-002 9.9e-007 1.01e+000 1.017012935e+001 1.017013087e+001 1.2e-010 0.25 87 6.9e-008 2.3e-002 8.9e-007 1.02e+000 1.017012950e+001 1.017013086e+001 1.1e-010 0.25 88 6.2e-008 2.1e-002 8.0e-007 1.08e+000 1.017012968e+001 1.017013085e+001 1.0e-010 0.25 89 6.6e-009 2.2e-003 8.3e-008 9.34e-001 1.017013067e+001 1.017013079e+001 1.1e-011 0.25 90 5.2e-010 1.6e-004 6.0e-009 1.01e+000 1.017013077e+001 1.017013078e+001 7.6e-013 0.25 Interior-point optimizer terminated. Time: 0.25. Optimizer terminated. Time: 0.27 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0170130772e+001 nrm: 8e+000 Viol. con: 3e-010 var: 0e+000 Dual. obj: 1.0170130781e+001 nrm: 6e+001 Viol. con: 0e+000 var: 4e-005 * End solution on dual form. * Transforming to primal solution. Solving took 0.322 seconds. result packing took 2.9e+02% of solve time solution checking took 18% of solve time Solving took 5 GP solves and 23.9 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 366641.668662 newton but the right hand side evaluated to 366630.056872 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 377162.182377 newton but the right hand side evaluated to 377115.431664 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 388105.080786 newton but the right hand side evaluated to 387998.850338 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 399470.235072 newton but the right hand side evaluated to 399279.083762 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 361212.184427 newton but the right hand side evaluated to 361206.359801 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 371522.130737 newton but the right hand side evaluated to 371498.534228 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 382190.296275 newton but the right hand side evaluated to 382135.957911 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 393255.633156 newton but the right hand side evaluated to 393156.467965 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 356181.877158 newton but the right hand side evaluated to 356176.090039 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 361243.193939 newton but the right hand side evaluated to 361220.039776 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 366354.215283 newton but the right hand side evaluated to 366302.323322 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 371535.44497 newton but the right hand side evaluated to 371443.458967 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 18366.9591341 newton but the right hand side evaluated to 18366.7163334 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 18344.453045 newton but the right hand side evaluated to 18344.2037166 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 18344.4529775 newton but the right hand side evaluated to 18344.2036189 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 18344.4530038 newton but the right hand side evaluated to 18344.2036438 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 18924.2840279 newton but the right hand side evaluated to 18924.2635416 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 8445.89962967 newton but the right hand side evaluated to 8445.8480032 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 8626.29336539 newton but the right hand side evaluated to 8626.24785229 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 24184.7528314 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 26232.8485054 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 34.475s OK Generating XML reports... Cloning into 'gassolar'... Cannot uninstall requirement gassolar, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/gassolar Installing collected packages: gassolar Running setup.py develop for gassolar Successfully installed gassolar From https://github.com/convexengineering/gpkit-models * branch tailfoam -> FETCH_HEAD Previous HEAD position was 662ac9f... add readme with build status HEAD is now at 238e02f... explicitly add wing interior to v-h tails Cannot uninstall requirement gpkit-models, not installed Obtaining file:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/gpkit-models Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: numpy>=1.7.0 in c:\anaconda2\lib\site-packages (from pandas) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-qkb5ss-build Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\gpkit (from gpfit==0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/gas/gas_simple/gassimple.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 564 variables. Solving took 0.148 seconds. Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 564 variables. Solving took 0.112 seconds. Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 564 variables. Solving took 0.164 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 6.03 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 3.6 seconds. Using solver 'mosek_cli' Solving for 79 variables. Solving took 0.099 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 0.214980669476 (Allowable error: 0.0001%, Actual error: 0.00078%) 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 0.201784059792 (Allowable error: 0.0001%, Actual error: 0.0064%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(2,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(2,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.197670060366 but the right hand side evaluated to 0.197679713956 (Allowable error: 0.0001%, Actual error: 0.0049%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(3,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(3,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.201771179179 but the right hand side evaluated to 0.201784059792 (Allowable error: 0.0001%, Actual error: 0.0064%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(4,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(4,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.214978984961 but the right hand side evaluated to 0.214969920711 (Allowable error: 0.0001%, Actual error: 0.0042%) Using solver 'mosek' Solving for 1067 variables. Solving took 0.661 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 134070.2824 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 134071.9055 but bound is 150000.0000 1 is a constraining latitude 11 is a constraining latitude Beginning signomial solve. Solving took 4 GP solves and 3.85 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 136276.7524 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 136278.3661 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 0.824 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 134070.3579 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 134071.6986 but bound is 150000.0000 1 is a constraining latitude 11 is a constraining latitude Beginning signomial solve. Solving took 4 GP solves and 2.77 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 136276.3380 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 136277.7007 but bound is 150000.0000 1 is a constraining latitude 11 is a constraining latitude Running tests... ---------------------------------------------------------------------- ....c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\gassolar\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 6 tests in 43.189s 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 it 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:///C:/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/windows10x64/optimizer/mosek/gpkit-models Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to c:\users\jenkins\appdata\local\temp\pip-gpxtsr-build Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\turbofan Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) adding test for 'SP_aircraft.py' Beginning signomial solve. Solving took 7 GP solves and 8.4 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 2427078.46878 force_pound * meter but the right hand side evaluated to 2397887.62621 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 2.21510116662 meter but the right hand side evaluated to 1.96468453965 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 17472.6000387 newton but the right hand side evaluated to 17443.2658731 newton (Allowable error: 0.1%, Actual error: 0.17%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1242113.69138 joule / kilogram but the right hand side evaluated to 1.48132365011 megajoule / kilogram (Allowable error: 0.1%, Actual error: 9.5%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 642470.639336 joule / kilogram but the right hand side evaluated to 0.643954787046 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 271790.235801 meter * newton but the right hand side evaluated to 263035.192483 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 18.57599158 meter but the right hand side evaluated to 16.6120802425 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 10.9551818778 but the right hand side evaluated to 4.85819873496 (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 10.0069293811 but the right hand side evaluated to 4.85820896032 (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 8.21525792546 but the right hand side evaluated to 4.85820907032 (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 18.6220282969 meter but the right hand side evaluated to 18.3758893789 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 18.6220282969 meter but the right hand side evaluated to 18.4513332717 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 4.67771975188 but the right hand side evaluated to 4.79405101096 (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 4.73113350584 but the right hand side evaluated to 4.81373342539 (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 7.60828890219 but the right hand side evaluated to 4.79405101096 (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 7.57969753677 but the right hand side evaluated to 4.81373342539 (Allowable error: 0.1%, Actual error: 36%) Solves with these variables bounded: value near lower bound: [CruiseAlt_Mission] value near upper bound: [TotalTime_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission] Checking for relaxed constants... WEIGHT DIFFERENCES Total Fuel Weight Percent Diff: [-6.97448585] Total Aircraft Weight Percent Diff: [-4.95039159] Engine Weight Percent Diff: -8.23496521972 Fuselage Weight Percent Diff: -10.9541956325 Payload Weight Percent Diff: [-0.04003551] VT Weight Percent Diff: -24.5187099138 HT Weight Percent Diff: -85.1524103255 Wing Weight Percent Diff: 0.426133596528 WING DIFFERENCES Wing Span Percent Diff: 0.921606965985 Wing Area Percent Diff: -6.86180861434 HORIZONTAL TAIL DIFFERENCES HT Area Percent Diff: -54.6183721954 VERTICAL TAIL DIFFERENCES VT Span Percent Diff: -16.3231200423 VT Area Percent Diff: -29.9968485758 CRUISE SEGMENT 1 DRAG DIFFERENCES Overall Cd Percent Diff: [-0.13090349] Nacelle Cd Percent Diff: [ 23.80938679] HT Cd Percent Diff: [-63.5095769] dimensionless Fuselage Cd Percent Diff: [ 45.32349081] VT Cd Percent Diff: [ 60.3689529] dimensionless Induced Drag Cd Percent Diff: [ 1.0636524] Wing Profile Cd Percent Diff: [-15.69400458] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [ 2.99116576] FUSELAGE DIFFERENCES Fan Propulsive Efficiency in Cruise Segment 1 --------------------- 0.790004735125 Beginning signomial solve. Solving took 7 GP solves and 9.49 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 2427081.34298 force_pound * meter but the right hand side evaluated to 2397882.79624 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 2.21510126999 meter but the right hand side evaluated to 1.96471461367 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 17472.4969771 newton but the right hand side evaluated to 17443.1796461 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 1242176.44049 joule / kilogram but the right hand side evaluated to 1.48175079765 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 642480.65072 joule / kilogram but the right hand side evaluated to 0.643967744701 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 10.9552545943 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 10.0070081129 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 8.21526823043 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 18.6220178962 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 18.6220178962 meter but the right hand side evaluated to 18.4513216119 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 4.67771110957 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 4.73112391285 but the right hand side evaluated to 4.81371916251 (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 7.6082551416 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 7.57969074629 but the right hand side evaluated to 4.81371916251 (Allowable error: 0.1%, Actual error: 36%) Solves with these variables bounded: value near lower bound: [CruiseAlt_Mission] value near upper bound: [TotalTime_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, A_{tri}_Mission/Aircraft/Wing/WingNoStruct, ClimbDistance_Mission] Checking for relaxed constants... WEIGHT DIFFERENCES Total Fuel Weight Percent Diff: [-6.97422995] Total Aircraft Weight Percent Diff: [-4.95044675] Engine Weight Percent Diff: -8.23560157345 Fuselage Weight Percent Diff: -10.9537279668 Payload Weight Percent Diff: [-0.04052335] VT Weight Percent Diff: -24.5186291271 HT Weight Percent Diff: -85.1524945413 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: -29.9968058767 CRUISE SEGMENT 1 DRAG DIFFERENCES Overall Cd Percent Diff: [-0.1303819] Nacelle Cd Percent Diff: [ 23.80790645] HT Cd Percent Diff: [-63.50953115] dimensionless Fuselage Cd Percent Diff: [ 45.32347143] VT Cd Percent Diff: [ 60.36852535] dimensionless Induced Drag Cd Percent Diff: [ 1.06550307] Wing Profile Cd Percent Diff: [-15.69341222] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [ 2.99019335] FUSELAGE DIFFERENCES Fan Propulsive Efficiency in Cruise Segment 1 --------------------- 0.790005398454 Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 38.056s OK Generating XML reports... calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gpkit-models.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'master'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'turbofan'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'master'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gassolar'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'tailfoam'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'tailfoam'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'master'] attempt 1 calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/turbofan.git'] attempt 1 (venv2_gpkit) (root) C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek>exit 0 [xUnit] [INFO] - Starting to record. [xUnit] [INFO] - Processing JUnit [xUnit] [INFO] - [JUnit] - 5 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'C:\Users\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows10x64\optimizer\mosek' for the testing framework 'JUnit'. [xUnit] [INFO] - Check 'Failed Tests' threshold. [xUnit] [INFO] - Check 'Skipped Tests' threshold. [xUnit] [INFO] - Setting the build status to SUCCESS [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: SUCCESS