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Started by upstream project "gplibrary_PR_Models" build number 89 originally caused by: GitHub pull request #169 of commit ff7fdcd8af9b09c55f17635373c0f374dec05c09, no merge conflicts. Building remotely on windows10x64 in workspace C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > C:\Program Files\Git\cmd\git init C:\Users\jenkins\workspace\gplibrary_PR_Models\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 d45d49ec90ceab5887e9d87dc3b5b2648c07456a (refs/remotes/origin/pr/169/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 d45d49ec90ceab5887e9d87dc3b5b2648c07456a # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "HEAD^{commit}" # timeout=10 Seen branch in repository origin/1682literate Seen branch in repository origin/1682master Seen branch in repository origin/Breakdown Seen branch in repository origin/SPaircraft Seen branch in repository origin/aerosurf Seen branch in repository origin/atmosphere Seen branch in repository origin/boundj Seen 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remote branches > C:\Program Files\Git\cmd\git show-ref --tags -d # timeout=10 Checking out Revision d45d49ec90ceab5887e9d87dc3b5b2648c07456a (origin/pr/169/merge, origin/master) > C:\Program Files\Git\cmd\git config core.sparsecheckout # timeout=10 > C:\Program Files\Git\cmd\git checkout -f d45d49ec90ceab5887e9d87dc3b5b2648c07456a # timeout=3 Commit message: "Merge ff7fdcd8af9b09c55f17635373c0f374dec05c09 into f92158c8230dad6f2a09c90b265a9ce8ff32c7da" 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="move outboard moment and shear equations to aircraft models" href="https://github.com/convexengineering/gplibrary/pull/169">PR 169</a>: move outboard moment and shear equations to aircraft models [Execution node] check if [windows10x64] is in [[macys, macys_VM, 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\jenkins223799346476238187.bat C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>echo C:\Program Files (x86)\Common Files\Oracle\Java\javapath;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\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\cmd;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps C:\Program Files (x86)\Common Files\Oracle\Java\javapath;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\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\cmd;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM turn on the anaconda console C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>call activate.bat || exit /b 666 (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM Create a virtualenv to install everything into (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>SET VENV=C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>virtualenv --system-site-packages C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit || exit /b 666 New python executable in C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts\python.exe Installing setuptools, pip, wheel...done. (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>call C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts\activate.bat || exit /b 666 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set PATH=C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts;C:\Anaconda2;C:\Anaconda2\Library\mingw-w64\bin;C:\Anaconda2\Library\usr\bin;C:\Anaconda2\Library\bin;C:\Anaconda2\Scripts;C:\Anaconda2\bin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;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\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\cmd;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM set PATH=C:\mingw-w64\x86_64-7.3.0-posix-seh-rt_v5-rev0\mingw64\bin;C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts;C:\Anaconda2;C:\Anaconda2\Library\mingw-w64\bin;C:\Anaconda2\Library\usr\bin;C:\Anaconda2\Library\bin;C:\Anaconda2\Scripts;C:\Anaconda2\bin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;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\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\cmd;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>gcc --version || exit /b 666 gcc (x86_64-posix-seh-rev0, Built by MinGW-W64 project) 6.4.0 Copyright (C) 2017 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) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM upgdade pip (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>python -m pip install --upgrade pip || exit /b 666 Requirement already up-to-date: pip in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (10.0.1) gassolar 0.0.0.0 requires gpkit, which is not installed. solar 0.0.0.0 requires gpkit, which is not installed. solar 0.0.0.0 requires gpkitmodels, which is not installed. grin 1.2.1 requires argparse>=1.1, which is not installed. gpfit 0.1 requires gpkit, which is not installed. (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM Install coverage into the virtualenv to the coverage command blow uses the virtualenv python (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>pip install --upgrade coverage || exit /b 666 Requirement already up-to-date: coverage in c:\anaconda2\lib\site-packages (4.5.1) gassolar 0.0.0.0 requires gpkit, which is not installed. solar 0.0.0.0 requires gpkit, which is not installed. solar 0.0.0.0 requires gpkitmodels, which is not installed. grin 1.2.1 requires argparse>=1.1, which is not installed. gpfit 0.1 requires gpkit, which is not installed. (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>SET GPKITBUILD=C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\build_gpkit (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>if mosek == cvxopt ( pip install --upgrade cvxopt || exit /b 666 set GPKITSOLVERS=cvxopt ) (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>if mosek == mosek ( msktestlic || exit /b 666 python -c "__import__('mosek').Env()" || exit /b 666 set GPKITSOLVERS=mosek, mosek_cli ) Problem Name : Objective sense : min Type : LO (linear optimization problem) Constraints : 1 Cones : 0 Scalar variables : 5000 Matrix variables : 0 Integer variables : 0 Optimizer started. Mosek license manager: License path: C:\Users\jenkins\mosek\mosek.lic Mosek license manager: Checkout license feature 'PTS' from flexlm. Mosek license manager: Checkout time 0.02. r: 0 status: 0 Interior-point optimizer started. Presolve started. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 1 time : 0.00 Lin. dep. - tries : 0 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.08 ************************************ A license was checked out correctly. ************************************ (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>dir C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\build_gpkit Volume in drive C has no label. Volume Serial Number is C4C9-8F11 Directory of C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek File Not Found (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import scipy; print scipy.__version__" || exit /b 666 1.0.1 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import numpy; print numpy.__version__" || exit /b 666 1.14.2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import pint; print pint.__version__" || exit /b 666 0.8.1 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM Install gpkit to run the documentation examples (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>git clone --depth 1 https://github.com/convexengineering/gpkit.git || exit /b 666 Cloning into 'gpkit'... (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>pip install -e C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\gpkit || exit /b 666 Obtaining file:///C:/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit Requirement already satisfied: numpy>=1.12.1 in c:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.14.2) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (0.8.1) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.0.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.3.2) solar 0.0.0.0 requires gpkitmodels, which is not installed. grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gpkit Running setup.py develop for gpkit Successfully installed gpkit (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>pip install -e C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek || exit /b 666 Obtaining file:///C:/Users/jenkins/workspace/gplibrary_PR_Models/mosek Requirement already satisfied: numpy>=1.12 in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1) grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gpkitmodels Running setup.py develop for gpkitmodels Successfully installed gpkitmodels (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM Show the settings file (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>type C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\gpkit\gpkit\env\settings installed_solvers : mosek, mosek_cli mosek_bin_dir : C:\Program Files\Mosek\8\tools\platform\win64x86\bin (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM Limit number of threads that be can used (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set MSK_IPAR_NUM_THREADS=2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set MKL_NUM_THREADS=2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set NUMEXPR_NUM_THREADS=2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set OPENBLAS_NUM_THREADS=2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set OMP_NUM_THREADS=2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)" Obtaining file:///C:/Users/jenkins/workspace/gplibrary_PR_Models/mosek Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Cloning into 'shopping'... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.028 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.051 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.089 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 0.747s OK Generating XML reports... Cloning into 'gassolar'... 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Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-qngxmo Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\anaconda2\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-ru4i2g\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gassolar Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0) Building wheels for collected packages: gassolar Running setup.py bdist_wheel for gassolar: started Running setup.py bdist_wheel for gassolar: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-hvu930\wheels\5c\45\ee\a8ea86f24e24acb4b8a5b5ef8c1a921fb70526d25cb0d4c0da Successfully built gassolar grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gassolar Found existing installation: gassolar 0.0.0.0 Not uninstalling gassolar at c:\anaconda2\lib\site-packages, outside environment c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit Can't uninstall 'gassolar'. No files were found to uninstall. Successfully installed gassolar-0.0.0.0 adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 592 variables. Solving took 0.412 seconds. 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 Beginning signomial solve. Solving took 4 GP solves and 3.91 seconds. Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 592 variables. Solving took 0.384 seconds. 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 Beginning signomial solve. Solving took 4 GP solves and 2.3 seconds. Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 1250 variables. Solving took 0.53 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1529 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 131552.1347 but bound is 150000.0000 Beginning signomial solve. Solving took 4 GP solves and 5.47 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0529 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 134553.9089 but bound is 150000.0000 Using solver 'mosek_cli' Solving for 1250 variables. Solving took 0.639 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.0147 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 131552.3302 but bound is 150000.0000 Beginning signomial solve. Solving took 4 GP solves and 5.59 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134552.5355 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 134553.8810 but bound is 150000.0000 Running tests... ---------------------------------------------------------------------- ..C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 4 tests in 68.512s OK Generating XML reports... Cloning into 'jho'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-k7nelc Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\anaconda2\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-soon1j\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -7.117646316084913e-14. Allowing negative dual variable(s) as small as -7.779725214734912e-14. Allowing negative dual variable(s) as small as -1.312812705767108e-13. Allowing negative dual variable(s) as small as -1.2642762271114494e-13. Solving took 4 GP solves and 6.35 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -7.61974034216295e-14. Allowing negative dual variable(s) as small as -6.635599188176133e-14. Allowing negative dual variable(s) as small as -1.3075727566674855e-13. Allowing negative dual variable(s) as small as -1.2881286749061305e-13. Solving took 4 GP solves and 7.62 seconds. Allowing negative dual variable(s) as small as -5.850315891453572e-13. Allowing negative dual variable(s) as small as -3.3793063833331694e-13. Allowing negative dual variable(s) as small as -1.022974240039165e-12. Allowing negative dual variable(s) as small as -1.022076086959478e-12. Allowing negative dual variable(s) as small as -2.7603212684329526e-13. Allowing negative dual variable(s) as small as -1.1550357024991964e-12. Allowing negative dual variable(s) as small as -1.116510828019432e-12. Allowing negative dual variable(s) as small as -1.1161072066556699e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 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 = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -1.2095529113888281e-12. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -6.14544008971425e-11. Allowing negative dual variable(s) as small as -1.4546773045318779e-12. Allowing negative dual variable(s) as small as -6.463349134055873e-12. Allowing negative dual variable(s) as small as -6.468851458228352e-12. Solving took 4 GP solves and 5.89 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 3.3 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.844981616764944e-13. Allowing negative dual variable(s) as small as -3.395027314834209e-13. Allowing negative dual variable(s) as small as -1.0227972982446154e-12. Allowing negative dual variable(s) as small as -1.0221402717280892e-12. Allowing negative dual variable(s) as small as -2.7777937285436427e-13. Allowing negative dual variable(s) as small as -1.1544863101533437e-12. Allowing negative dual variable(s) as small as -1.1161437984789913e-12. Allowing negative dual variable(s) as small as -1.1159076321407696e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 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 = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -1.2093633928490777e-12. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -6.145438748797567e-11. Allowing negative dual variable(s) as small as -1.4546608248573795e-12. Allowing negative dual variable(s) as small as -6.463168154587613e-12. Allowing negative dual variable(s) as small as -6.468772437320328e-12. Solving took 4 GP solves and 5.8 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 3.36 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 91.395s OK Generating XML reports... Cloning into 'turbofan'... Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\turbofan Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.8.1) Building wheels for collected packages: turbofan Running setup.py bdist_wheel for turbofan: started Running setup.py bdist_wheel for turbofan: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-ilr4ov\wheels\3a\4a\df\1e137b486523078491de3a0319a07f314f5e9aa745dfaf6fd5 Successfully built turbofan grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: turbofan Successfully installed turbofan-0.0.0.0 adding test for 'turbofan/engine_validation.py' Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528308 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 26232.8485049 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 2.655s OK Generating XML reports... 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Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to c:\users\jenkins\appdata\local\temp\pip-req-build-7zddyp Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.8.1) Building wheels for collected packages: turbofan Running setup.py bdist_wheel for turbofan: started Running setup.py bdist_wheel for turbofan: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-ira8fr\wheels\49\e6\3a\5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5 Successfully built turbofan grin 1.2.1 requires argparse>=1.1, which is not installed. adding test for 'SP_aircraft.py' Beginning signomial solve. Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * 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 : 1900 Cones : 0 Scalar variables : 6471 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 : 485 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 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 : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3606 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.06 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.52e+004 after factor : 1.75e+005 Factor - dense dim. : 0 flops : 3.95e+007 Factor - GP saved nzs : -1.40e+005 GP saved flops : -3.84e+007 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.5e+003 1.2e+005 0.00e+000 -1.241488813e+005 2.000000000e+000 1.0e+000 0.13 1 1.5e+003 2.3e+003 8.0e+004 -9.71e-001 -1.230687516e+005 2.970987356e+000 6.4e-001 0.30 2 6.4e+002 1.0e+003 3.5e+004 -9.53e-001 -1.192967354e+005 6.579340153e+000 2.8e-001 0.47 3 2.9e+002 4.5e+002 1.6e+004 -8.91e-001 -1.118073907e+005 2.810620976e+001 1.3e-001 0.64 4 2.9e+002 4.5e+002 1.6e+004 -7.65e-001 -1.098742004e+005 1.715053438e+003 1.3e-001 0.83 5 1.0e+002 1.6e+002 5.5e+003 -7.58e-001 -8.114911129e+004 8.829466497e+003 4.5e-002 0.97 6 3.6e+001 5.7e+001 2.0e+003 -3.53e-001 -4.317145151e+004 1.174544900e+004 1.6e-002 1.16 7 1.6e+001 2.6e+001 9.0e+002 2.99e-001 -2.298460899e+004 6.535836542e+003 7.3e-003 1.27 8 8.0e+000 1.2e+001 4.3e+002 6.72e-001 -1.157711675e+004 3.816611718e+003 3.5e-003 1.44 9 3.6e+000 5.5e+000 1.9e+002 8.63e-001 -5.013061690e+003 2.102664920e+003 1.6e-003 1.58 10 1.8e+000 2.8e+000 1.0e+002 9.56e-001 -2.269644083e+003 1.452988731e+003 8.2e-004 1.78 11 6.7e-001 1.0e+000 3.7e+001 9.85e-001 -6.169041418e+002 7.675247964e+002 3.1e-004 1.83 12 5.7e-001 9.2e-001 3.2e+001 9.80e-001 -4.754488783e+002 7.121688414e+002 2.6e-004 1.94 13 4.2e-001 7.3e-001 2.3e+001 9.75e-001 -2.603298963e+002 6.223932253e+002 1.9e-004 2.13 14 2.1e-001 4.5e-001 1.2e+001 9.88e-001 4.312159478e+001 4.907642806e+002 9.7e-005 2.28 15 6.3e-002 1.9e-001 3.6e+000 1.00e+000 2.631300191e+002 3.980771438e+002 3.0e-005 2.36 16 1.9e-002 1.4e-001 1.1e+000 1.00e+000 3.276991459e+002 3.698964737e+002 9.5e-006 2.45 17 4.8e-003 1.4e-001 2.9e-001 1.00e+000 3.497768258e+002 3.605591115e+002 2.5e-006 2.52 18 2.8e-003 1.1e-001 1.7e-001 1.00e+000 3.528642049e+002 3.591637527e+002 1.4e-006 2.56 19 4.6e-004 1.7e-001 2.8e-002 1.00e+000 3.565809519e+002 3.576475141e+002 2.5e-007 2.64 20 1.7e-004 1.1e-001 1.1e-002 9.92e-001 3.570616993e+002 3.574624815e+002 9.3e-008 2.72 21 5.1e-005 1.1e-001 3.1e-003 1.00e+000 3.572639171e+002 3.573824211e+002 2.8e-008 2.84 22 3.1e-005 8.4e-002 1.9e-003 9.82e-001 3.572958347e+002 3.573692277e+002 1.7e-008 2.94 23 1.1e-005 8.2e-002 6.9e-004 9.73e-001 3.573299009e+002 3.573559479e+002 6.0e-009 3.11 24 5.1e-006 7.1e-002 3.2e-004 1.01e+000 3.573399373e+002 3.573520203e+002 2.8e-009 3.25 25 2.2e-006 6.9e-002 1.4e-004 1.00e+000 3.573448652e+002 3.573500931e+002 1.2e-009 3.38 26 2.0e-006 6.8e-002 1.2e-004 1.00e+000 3.573452504e+002 3.573499542e+002 1.1e-009 3.52 27 1.8e-006 6.1e-002 1.1e-004 1.00e+000 3.573455861e+002 3.573498193e+002 9.8e-010 3.63 28 1.6e-006 5.6e-002 1.0e-004 1.00e+000 3.573458891e+002 3.573496990e+002 8.9e-010 3.75 29 1.4e-006 5.1e-002 9.1e-005 1.00e+000 3.573461619e+002 3.573495908e+002 8.0e-010 3.94 30 1.3e-006 4.6e-002 8.2e-005 1.00e+000 3.573464074e+002 3.573494934e+002 7.2e-010 4.09 31 1.2e-006 4.2e-002 7.4e-005 1.00e+000 3.573466283e+002 3.573494057e+002 6.5e-010 4.25 32 1.1e-006 3.9e-002 6.6e-005 1.00e+000 3.573468271e+002 3.573493268e+002 5.8e-010 4.34 33 9.5e-007 3.6e-002 6.0e-005 1.00e+000 3.573470060e+002 3.573492557e+002 5.2e-010 4.53 34 8.5e-007 3.3e-002 5.4e-005 1.00e+000 3.573471670e+002 3.573491918e+002 4.7e-010 4.78 35 7.7e-007 3.0e-002 4.8e-005 1.00e+000 3.573473119e+002 3.573491342e+002 4.2e-010 4.91 36 6.9e-007 2.8e-002 4.3e-005 1.00e+000 3.573474423e+002 3.573490824e+002 3.8e-010 5.03 37 6.7e-007 2.8e-002 4.1e-005 1.00e+000 3.573475190e+002 3.573490511e+002 3.6e-010 5.16 38 6.8e-007 2.7e-002 4.1e-005 9.86e-001 3.573475246e+002 3.573490410e+002 3.6e-010 5.22 39 6.1e-007 2.5e-002 3.6e-005 1.00e+000 3.573476324e+002 3.573490015e+002 3.2e-010 5.30 40 6.0e-007 2.5e-002 3.6e-005 9.88e-001 3.573476333e+002 3.573490018e+002 3.2e-010 5.39 41 5.9e-007 2.5e-002 3.3e-005 1.00e+000 3.573477301e+002 3.573489659e+002 2.9e-010 5.45 42 8.6e-007 2.5e-002 3.2e-005 9.94e-001 3.573477425e+002 3.573489612e+002 2.8e-010 5.53 43 8.0e-007 2.3e-002 2.9e-005 1.00e+000 3.573478307e+002 3.573489230e+002 2.6e-010 5.58 44 6.8e-007 2.2e-002 2.6e-005 1.01e+000 3.573479152e+002 3.573488845e+002 2.3e-010 5.69 45 6.2e-007 2.0e-002 2.4e-005 1.01e+000 3.573479863e+002 3.573488613e+002 2.1e-010 5.78 46 6.9e-007 2.0e-002 2.4e-005 9.70e-001 3.573479784e+002 3.573488833e+002 2.1e-010 5.88 47 1.2e-006 1.9e-002 2.3e-005 1.01e+000 3.573480188e+002 3.573488252e+002 2.0e-010 5.95 48 8.7e-007 1.7e-002 2.0e-005 9.99e-001 3.573480714e+002 3.573488203e+002 1.8e-010 6.03 49 7.5e-007 1.6e-002 1.8e-005 1.00e+000 3.573481258e+002 3.573488001e+002 1.6e-010 6.11 50 5.8e-007 1.5e-002 1.6e-005 9.96e-001 3.573481753e+002 3.573487799e+002 1.4e-010 6.17 51 5.3e-007 1.4e-002 1.5e-005 1.00e+000 3.573482198e+002 3.573487627e+002 1.3e-010 6.24 52 4.8e-007 1.4e-002 1.3e-005 9.91e-001 3.573482592e+002 3.573487480e+002 1.2e-010 6.36 53 4.3e-007 1.3e-002 1.2e-005 9.99e-001 3.573482947e+002 3.573487347e+002 1.1e-010 6.52 54 3.5e-007 1.2e-002 1.1e-005 1.00e+000 3.573483269e+002 3.573487234e+002 9.5e-011 6.61 55 3.1e-007 1.2e-002 9.7e-006 9.93e-001 3.573483557e+002 3.573487125e+002 8.6e-011 6.69 56 4.2e-007 1.2e-002 9.7e-006 1.01e+000 3.573483588e+002 3.573487078e+002 8.5e-011 6.75 57 3.5e-007 1.1e-002 8.7e-006 9.94e-001 3.573483840e+002 3.573486993e+002 7.7e-011 6.83 58 3.2e-007 1.1e-002 7.8e-006 9.97e-001 3.573484070e+002 3.573486910e+002 6.9e-011 6.91 59 5.9e-007 1.1e-002 7.7e-006 9.85e-001 3.573484067e+002 3.573486973e+002 6.8e-011 6.99 60 5.3e-007 1.0e-002 7.0e-006 9.98e-001 3.573484275e+002 3.573486888e+002 6.1e-011 7.06 61 5.5e-007 1.0e-002 7.0e-006 -1.17e-001 3.573484321e+002 3.573486777e+002 6.1e-011 7.17 62 5.5e-007 1.0e-002 6.8e-006 1.00e+000 3.573484367e+002 3.573486777e+002 6.1e-011 7.28 63 5.0e-007 9.3e-003 6.1e-006 9.86e-001 3.573484559e+002 3.573486677e+002 5.5e-011 7.38 64 3.0e-006 9.3e-003 6.1e-006 9.67e-001 3.573484575e+002 3.573486648e+002 5.5e-011 7.45 65 2.9e-006 9.3e-003 6.1e-006 1.09e+000 3.573484629e+002 3.573486560e+002 5.4e-011 7.53 66 2.9e-006 9.3e-003 6.1e-006 1.15e+000 3.573484629e+002 3.573486560e+002 5.4e-011 7.59 67 2.6e-006 8.3e-003 5.5e-006 1.01e+000 3.573484791e+002 3.573486505e+002 4.9e-011 7.69 68 2.6e-006 8.3e-003 5.3e-006 1.00e+000 3.573484851e+002 3.573486483e+002 4.7e-011 7.75 69 3.4e-006 8.1e-003 5.2e-006 9.89e-001 3.573484861e+002 3.573486502e+002 4.6e-011 7.81 70 3.1e-006 7.9e-003 4.7e-006 1.01e+000 3.573484988e+002 3.573486473e+002 4.1e-011 7.91 71 2.8e-006 7.1e-003 4.2e-006 1.00e+000 3.573485091e+002 3.573486440e+002 3.7e-011 8.02 72 2.9e-006 7.1e-003 4.2e-006 9.96e-001 3.573485095e+002 3.573486439e+002 3.7e-011 8.09 73 2.9e-006 7.1e-003 4.1e-006 1.00e+000 3.573485129e+002 3.573486439e+002 3.7e-011 8.19 74 2.9e-006 7.1e-003 3.9e-006 1.00e+000 3.573485180e+002 3.573486439e+002 3.7e-011 8.33 75 2.9e-006 7.1e-003 3.9e-006 1.00e+000 3.573485193e+002 3.573486439e+002 3.7e-011 8.45 76 2.9e-006 7.1e-003 3.9e-006 1.00e+000 3.573485200e+002 3.573486438e+002 3.7e-011 8.59 77 2.7e-006 7.1e-003 4.2e-006 1.00e+000 3.573485088e+002 3.573486438e+002 3.7e-011 8.70 78 2.6e-006 6.9e-003 4.2e-006 1.04e+000 3.573485085e+002 3.573486471e+002 3.6e-011 8.88 79 2.4e-006 6.4e-003 3.8e-006 1.00e+000 3.573485198e+002 3.573486397e+002 3.3e-011 9.03 80 2.2e-006 5.8e-003 3.4e-006 8.58e-001 3.573485279e+002 3.573486392e+002 3.0e-011 9.14 81 2.2e-006 5.8e-003 2.7e-006 1.00e+000 3.573485508e+002 3.573486392e+002 3.0e-011 9.23 82 3.1e-006 5.8e-003 1.6e-006 1.00e+000 3.573485883e+002 3.573486390e+002 3.0e-011 9.36 83 3.0e-006 5.8e-003 1.6e-006 1.01e+000 3.573485883e+002 3.573486385e+002 3.0e-011 9.52 84 3.0e-006 5.7e-003 1.6e-006 1.09e+000 3.573485888e+002 3.573486404e+002 3.0e-011 9.64 85 3.0e-006 5.7e-003 1.6e-006 1.00e+000 3.573485886e+002 3.573486404e+002 3.0e-011 9.78 86 3.0e-006 5.7e-003 1.6e-006 1.00e+000 3.573485886e+002 3.573486404e+002 3.0e-011 9.92 Interior-point optimizer terminated. Time: 9.92. Optimizer terminated. Time: 9.94 solsta = 8, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : NEAR_OPTIMAL Primal. obj: 3.5734858857e+002 nrm: 9e+001 Viol. con: 6e-005 var: 0e+000 Dual. obj: 3.5734864038e+002 nrm: 8e+002 Viol. con: 0e+000 var: 4e-002 * End solution on dual form. * Transforming to primal solution. Solving took 9.99 seconds. final status of solver 'mosek' was 'NEAR_DUAL_FEAS', not 'optimal'. result packing took 5.2% of solve time solution checking took 1.7% of solve time Using solver 'mosek' Solving for 1899 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'. Number of Hessian non-zeros: 1953 * 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 : 1900 Cones : 0 Scalar variables : 6471 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 : 487 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 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 : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3607 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.05 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.53e+004 after factor : 1.76e+005 Factor - dense dim. : 0 flops : 3.97e+007 Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.234758035e+005 2.000000000e+000 1.0e+000 0.09 1 1.5e+003 2.0e+003 8.0e+004 -9.71e-001 -1.224174060e+005 2.927903826e+000 6.5e-001 0.20 2 7.1e+002 9.7e+002 3.8e+004 -9.53e-001 -1.192652447e+005 6.047889938e+000 3.1e-001 0.30 3 2.9e+002 4.0e+002 1.6e+004 -9.01e-001 -1.111484949e+005 2.515365448e+001 1.3e-001 0.39 4 2.9e+002 4.0e+002 1.6e+004 -7.65e-001 -1.092627588e+005 1.672591448e+003 1.3e-001 0.50 5 1.2e+002 1.6e+002 6.4e+003 -7.58e-001 -8.564991791e+004 7.659095908e+003 5.2e-002 0.59 6 3.5e+001 4.8e+001 1.9e+003 -4.31e-001 -4.091381335e+004 1.290802040e+004 1.5e-002 0.73 7 1.5e+001 2.1e+001 8.3e+002 3.29e-001 -2.129514412e+004 6.272280306e+003 6.8e-003 0.83 8 6.9e+000 9.4e+000 3.7e+002 7.04e-001 -1.003204920e+004 3.298432315e+003 3.1e-003 0.89 9 2.8e+000 3.8e+000 1.5e+002 8.93e-001 -3.935729139e+003 1.598485027e+003 1.2e-003 0.97 10 1.2e+000 1.6e+000 6.5e+001 9.75e-001 -1.631239289e+003 7.616896397e+002 5.3e-004 1.05 11 9.1e-001 1.3e+000 5.0e+001 9.87e-001 -1.230601942e+003 6.193610397e+002 4.1e-004 1.13 12 7.2e-001 1.2e+000 3.9e+001 9.70e-001 -9.738090485e+002 5.013885062e+002 3.2e-004 1.22 13 3.7e-001 6.4e-001 2.0e+001 9.91e-001 -4.737154364e+002 2.805103538e+002 1.7e-004 1.31 14 1.2e-001 2.4e-001 6.8e+000 9.98e-001 -1.373846285e+002 1.176219904e+002 5.7e-005 1.44 15 4.1e-002 1.3e-001 2.3e+000 1.00e+000 -2.387366200e+001 6.392407942e+001 2.0e-005 1.51 16 2.5e-002 9.2e-002 1.4e+000 1.00e+000 4.561302744e-002 5.311069584e+001 1.2e-005 1.58 17 1.6e-002 9.0e-002 9.3e-001 1.00e+000 1.225152822e+001 4.734748333e+001 7.9e-006 1.66 18 3.8e-003 1.3e-001 2.2e-001 1.00e+000 3.045532086e+001 3.887121219e+001 1.9e-006 1.72 19 2.1e-003 9.4e-002 1.2e-001 1.00e+000 3.309947114e+001 3.769690820e+001 1.1e-006 1.81 20 7.8e-004 9.4e-002 4.6e-002 1.00e+000 3.505616763e+001 3.679522355e+001 4.0e-007 1.91 21 2.3e-004 1.0e-001 1.4e-002 1.00e+000 3.589055263e+001 3.640904490e+001 1.2e-007 2.03 22 9.2e-005 8.9e-002 5.5e-003 1.00e+000 3.610362695e+001 3.630882323e+001 4.8e-008 2.11 23 8.3e-005 8.0e-002 4.9e-003 1.00e+000 3.611850706e+001 3.630318141e+001 4.3e-008 2.17 24 7.4e-005 7.3e-002 4.4e-003 1.00e+000 3.613099643e+001 3.629719465e+001 3.9e-008 2.25 25 6.7e-005 6.6e-002 4.0e-003 1.00e+000 3.614225807e+001 3.629182967e+001 3.5e-008 2.33 26 6.0e-005 6.1e-002 3.6e-003 1.00e+000 3.615238227e+001 3.628699109e+001 3.1e-008 2.41 27 5.4e-005 5.5e-002 3.2e-003 1.00e+000 3.616149194e+001 3.628263528e+001 2.8e-008 2.52 28 4.9e-005 5.0e-002 2.9e-003 1.00e+000 3.616968808e+001 3.627871334e+001 2.5e-008 2.59 29 4.4e-005 4.6e-002 2.6e-003 1.00e+000 3.617706278e+001 3.627518244e+001 2.3e-008 2.70 30 4.0e-005 4.2e-002 2.4e-003 1.00e+000 3.618369849e+001 3.627200369e+001 2.1e-008 2.78 31 3.6e-005 3.9e-002 2.1e-003 1.00e+000 3.618966944e+001 3.626914208e+001 1.8e-008 2.86 32 3.2e-005 3.6e-002 1.9e-003 1.00e+000 3.619504232e+001 3.626656606e+001 1.7e-008 2.92 33 2.9e-005 3.3e-002 1.7e-003 1.00e+000 3.619987716e+001 3.626424718e+001 1.5e-008 2.98 34 2.6e-005 3.0e-002 1.5e-003 1.00e+000 3.620422791e+001 3.626215985e+001 1.3e-008 3.05 35 2.3e-005 2.8e-002 1.4e-003 1.00e+000 3.620814309e+001 3.626028097e+001 1.2e-008 3.17 36 2.1e-005 2.6e-002 1.3e-003 1.00e+000 3.621166636e+001 3.625858975e+001 1.1e-008 3.27 37 1.9e-005 2.4e-002 1.1e-003 1.00e+000 3.621483699e+001 3.625706748e+001 9.8e-009 3.33 38 1.7e-005 2.2e-002 1.0e-003 1.00e+000 3.621769030e+001 3.625569728e+001 8.8e-009 3.39 39 1.5e-005 2.1e-002 9.1e-004 1.00e+000 3.622025805e+001 3.625446398e+001 8.0e-009 3.52 40 1.4e-005 1.9e-002 8.2e-004 1.00e+000 3.622256885e+001 3.625335390e+001 7.2e-009 3.64 41 1.2e-005 1.8e-002 7.4e-004 1.00e+000 3.622464840e+001 3.625235472e+001 6.5e-009 3.78 42 1.1e-005 1.7e-002 6.7e-004 1.00e+000 3.622651986e+001 3.625145536e+001 5.8e-009 3.84 43 1.0e-005 1.6e-002 6.0e-004 1.00e+000 3.622820404e+001 3.625064586e+001 5.2e-009 3.95 44 9.0e-006 1.5e-002 5.4e-004 1.00e+000 3.622971969e+001 3.624991721e+001 4.7e-009 4.00 45 8.1e-006 1.4e-002 4.9e-004 1.00e+000 3.623108368e+001 3.624926136e+001 4.2e-009 4.08 46 7.3e-006 1.4e-002 4.4e-004 1.00e+000 3.623231117e+001 3.624867101e+001 3.8e-009 4.26 47 6.6e-006 1.3e-002 3.9e-004 1.00e+000 3.623341582e+001 3.624813963e+001 3.4e-009 4.41 48 5.9e-006 1.3e-002 3.5e-004 1.00e+000 3.623440993e+001 3.624766132e+001 3.1e-009 4.50 49 5.3e-006 1.2e-002 3.2e-004 1.00e+000 3.623530456e+001 3.624723078e+001 2.8e-009 4.67 50 4.8e-006 1.2e-002 2.9e-004 1.00e+000 3.623610966e+001 3.624684324e+001 2.5e-009 4.81 51 4.3e-006 1.1e-002 2.6e-004 1.00e+000 3.623683419e+001 3.624649439e+001 2.2e-009 4.92 52 3.9e-006 1.1e-002 2.3e-004 1.00e+000 3.623748621e+001 3.624618038e+001 2.0e-009 5.05 53 3.5e-006 1.0e-002 2.1e-004 1.00e+000 3.623807298e+001 3.624589773e+001 1.8e-009 5.14 54 3.2e-006 1.0e-002 1.9e-004 1.00e+000 3.623860103e+001 3.624564330e+001 1.6e-009 5.23 55 2.8e-006 9.8e-003 1.7e-004 1.00e+000 3.623907623e+001 3.624541427e+001 1.5e-009 5.33 56 2.6e-006 9.6e-003 1.5e-004 1.00e+000 3.623950388e+001 3.624520811e+001 1.3e-009 5.70 57 2.3e-006 9.3e-003 1.4e-004 1.00e+000 3.623988873e+001 3.624502254e+001 1.2e-009 5.83 58 2.1e-006 9.1e-003 1.2e-004 1.00e+000 3.624023507e+001 3.624485550e+001 1.1e-009 5.91 59 1.9e-006 9.0e-003 1.1e-004 1.00e+000 3.624054675e+001 3.624470513e+001 9.7e-010 6.01 60 1.7e-006 8.8e-003 1.0e-004 1.00e+000 3.624082723e+001 3.624456979e+001 8.7e-010 6.11 61 1.5e-006 8.6e-003 9.0e-005 1.00e+000 3.624107965e+001 3.624444795e+001 7.8e-010 6.19 62 1.4e-006 8.5e-003 8.1e-005 1.00e+000 3.624130681e+001 3.624433829e+001 7.1e-010 6.30 63 1.2e-006 8.4e-003 7.3e-005 1.00e+000 3.624151124e+001 3.624423957e+001 6.4e-010 6.39 64 1.1e-006 8.3e-003 6.6e-005 1.00e+000 3.624169521e+001 3.624415071e+001 5.7e-010 6.53 65 9.9e-007 8.2e-003 5.9e-005 1.00e+000 3.624186077e+001 3.624407072e+001 5.1e-010 6.89 66 8.9e-007 8.1e-003 5.3e-005 1.00e+000 3.624200977e+001 3.624399872e+001 4.6e-010 6.98 67 8.0e-007 8.0e-003 4.8e-005 1.00e+000 3.624214385e+001 3.624393392e+001 4.2e-010 7.11 68 7.2e-007 7.9e-003 4.3e-005 1.00e+000 3.624226452e+001 3.624387558e+001 3.8e-010 7.20 69 6.5e-007 7.9e-003 3.9e-005 1.00e+000 3.624237311e+001 3.624382307e+001 3.4e-010 7.53 70 5.8e-007 7.8e-003 3.5e-005 1.00e+000 3.624247084e+001 3.624377581e+001 3.0e-010 7.70 71 5.3e-007 7.7e-003 3.1e-005 1.00e+000 3.624255879e+001 3.624373326e+001 2.7e-010 7.83 72 4.7e-007 7.7e-003 2.8e-005 1.00e+000 3.624263794e+001 3.624369497e+001 2.5e-010 7.95 73 4.3e-007 7.6e-003 2.5e-005 1.00e+000 3.624270917e+001 3.624366049e+001 2.2e-010 8.05 74 3.8e-007 7.6e-003 2.3e-005 1.00e+000 3.624277328e+001 3.624362946e+001 2.0e-010 8.14 75 3.4e-007 7.6e-003 2.1e-005 1.00e+000 3.624283097e+001 3.624360154e+001 1.8e-010 8.28 76 3.1e-007 7.5e-003 1.9e-005 1.00e+000 3.624288289e+001 3.624357640e+001 1.6e-010 8.41 77 2.8e-007 7.5e-003 1.7e-005 1.00e+000 3.624292961e+001 3.624355377e+001 1.5e-010 8.55 78 2.5e-007 7.5e-003 1.5e-005 1.00e+000 3.624297166e+001 3.624353340e+001 1.3e-010 8.64 79 2.3e-007 7.4e-003 1.4e-005 1.00e+000 3.624300950e+001 3.624351507e+001 1.2e-010 8.73 80 2.0e-007 7.4e-003 1.2e-005 1.00e+000 3.624304356e+001 3.624349857e+001 1.1e-010 8.81 81 1.8e-007 7.4e-003 1.1e-005 1.00e+000 3.624307421e+001 3.624348371e+001 9.5e-011 9.17 82 1.6e-007 7.4e-003 9.9e-006 1.00e+000 3.624310179e+001 3.624347035e+001 8.6e-011 9.27 83 1.5e-007 7.3e-003 8.9e-006 1.00e+000 3.624312661e+001 3.624345832e+001 7.7e-011 9.38 84 1.3e-007 7.3e-003 8.0e-006 1.00e+000 3.624314895e+001 3.624344749e+001 7.0e-011 9.47 85 1.2e-007 7.3e-003 7.2e-006 1.00e+000 3.624316905e+001 3.624343774e+001 6.3e-011 9.58 86 1.1e-007 7.3e-003 6.5e-006 1.00e+000 3.624318715e+001 3.624342897e+001 5.6e-011 9.69 87 9.7e-008 7.3e-003 5.8e-006 1.00e+000 3.624320343e+001 3.624342107e+001 5.1e-011 9.80 88 8.8e-008 7.3e-003 5.2e-006 1.00e+000 3.624321809e+001 3.624341396e+001 4.6e-011 10.03 89 7.9e-008 7.3e-003 4.7e-006 1.00e+000 3.624323127e+001 3.624340756e+001 4.1e-011 10.14 90 7.1e-008 7.2e-003 4.2e-006 1.00e+000 3.624324314e+001 3.624340180e+001 3.7e-011 10.22 91 6.4e-008 7.2e-003 3.8e-006 1.00e+000 3.624325383e+001 3.624339662e+001 3.3e-011 10.28 92 5.7e-008 7.2e-003 3.4e-006 1.00e+000 3.624326344e+001 3.624339196e+001 3.0e-011 10.38 93 5.2e-008 7.2e-003 3.1e-006 1.00e+000 3.624327209e+001 3.624338776e+001 2.7e-011 10.48 94 4.7e-008 7.2e-003 2.8e-006 1.00e+000 3.624327988e+001 3.624338398e+001 2.4e-011 10.58 95 4.2e-008 7.2e-003 2.5e-006 1.00e+000 3.624328689e+001 3.624338057e+001 2.2e-011 10.70 96 3.8e-008 7.2e-003 2.3e-006 1.00e+000 3.624329319e+001 3.624337751e+001 2.0e-011 10.83 97 3.4e-008 7.2e-003 2.0e-006 1.00e+000 3.624329887e+001 3.624337475e+001 1.8e-011 10.95 98 3.1e-008 6.5e-003 1.8e-006 1.00e+000 3.624330402e+001 3.624337224e+001 1.6e-011 11.08 99 2.7e-008 5.8e-003 1.6e-006 1.00e+000 3.624330863e+001 3.624337000e+001 1.4e-011 11.22 100 2.5e-008 5.2e-003 1.5e-006 9.97e-001 3.624331276e+001 3.624336800e+001 1.3e-011 11.34 101 2.2e-008 4.7e-003 1.3e-006 1.00e+000 3.624331649e+001 3.624336619e+001 1.2e-011 11.44 102 2.0e-008 4.2e-003 1.2e-006 9.98e-001 3.624331983e+001 3.624336457e+001 1.0e-011 11.59 103 1.8e-008 3.8e-003 1.1e-006 9.97e-001 3.624332284e+001 3.624336311e+001 9.4e-012 11.80 104 1.6e-008 3.4e-003 9.7e-007 1.00e+000 3.624332555e+001 3.624336179e+001 8.5e-012 11.92 105 1.5e-008 3.1e-003 8.7e-007 1.00e+000 3.624332799e+001 3.624336061e+001 7.6e-012 12.02 106 1.3e-008 2.8e-003 7.9e-007 1.00e+000 3.624333018e+001 3.624335954e+001 6.9e-012 12.16 107 1.2e-008 2.5e-003 7.1e-007 1.00e+000 3.624333216e+001 3.624335858e+001 6.2e-012 12.20 108 1.1e-008 2.3e-003 6.4e-007 9.99e-001 3.624333394e+001 3.624335772e+001 5.6e-012 12.30 109 9.6e-009 2.0e-003 5.7e-007 1.00e+000 3.624333554e+001 3.624335694e+001 5.0e-012 12.34 110 8.6e-009 1.8e-003 5.2e-007 9.98e-001 3.624333698e+001 3.624335624e+001 4.5e-012 12.44 111 7.8e-009 1.6e-003 4.6e-007 1.00e+000 3.624333827e+001 3.624335561e+001 4.1e-012 12.50 112 7.0e-009 1.5e-003 4.2e-007 1.00e+000 3.624333944e+001 3.624335504e+001 3.6e-012 12.58 113 6.3e-009 1.3e-003 3.8e-007 1.00e+000 3.624334049e+001 3.624335453e+001 3.3e-012 12.67 114 5.7e-009 1.2e-003 3.4e-007 1.00e+000 3.624334143e+001 3.624335407e+001 3.0e-012 12.78 115 5.1e-009 1.1e-003 3.0e-007 1.00e+000 3.624334229e+001 3.624335365e+001 2.7e-012 12.92 116 4.6e-009 9.7e-004 2.7e-007 1.00e+000 3.624334305e+001 3.624335328e+001 2.4e-012 13.02 117 4.1e-009 8.7e-004 2.5e-007 1.00e+000 3.624334374e+001 3.624335295e+001 2.2e-012 13.08 118 3.7e-009 7.9e-004 2.2e-007 9.99e-001 3.624334436e+001 3.624335264e+001 1.9e-012 13.14 119 3.3e-009 7.1e-004 2.0e-007 1.00e+000 3.624334493e+001 3.624335237e+001 1.7e-012 13.19 120 3.0e-009 6.4e-004 1.8e-007 1.00e+000 3.624334543e+001 3.624335212e+001 1.6e-012 13.25 121 2.7e-009 5.7e-004 1.6e-007 9.98e-001 3.624334588e+001 3.624335190e+001 1.4e-012 13.31 122 2.4e-009 5.2e-004 1.5e-007 1.01e+000 3.624334630e+001 3.624335170e+001 1.3e-012 13.38 123 2.2e-009 4.6e-004 1.3e-007 9.87e-001 3.624334666e+001 3.624335153e+001 1.2e-012 13.41 124 2.0e-009 4.2e-004 1.2e-007 1.01e+000 3.624334700e+001 3.624335136e+001 1.0e-012 13.52 125 1.8e-009 3.8e-004 1.1e-007 9.98e-001 3.624334730e+001 3.624335121e+001 9.4e-013 13.61 Interior-point optimizer terminated. Time: 13.63. Optimizer terminated. Time: 13.70 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 3.6243347297e+001 nrm: 2e+002 Viol. con: 3e-008 var: 0e+000 Dual. obj: 3.6243351214e+001 nrm: 8e+002 Viol. con: 0e+000 var: 3e-003 * End solution on dual form. * Transforming to primal solution. Solving took 13.8 seconds. result packing took 3.3% of solve time solution checking took 0.65% of solve time Using solver 'mosek' Solving for 1899 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'. Number of Hessian non-zeros: 1953 * 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 : 1900 Cones : 0 Scalar variables : 6471 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 : 487 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.02 Lin. dep. - number : 0 Presolve terminated. Time: 0.02 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3607 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 : 0.03 Factor - nonzeros before factor : 1.53e+004 after factor : 1.76e+005 Factor - dense dim. : 0 flops : 3.97e+007 Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.232670642e+005 2.000000000e+000 1.0e+000 0.06 1 1.5e+003 2.1e+003 8.2e+004 -9.71e-001 -1.222858921e+005 2.848124002e+000 6.6e-001 0.17 2 6.9e+002 9.5e+002 3.7e+004 -9.55e-001 -1.189334608e+005 6.009127132e+000 3.0e-001 0.27 3 2.9e+002 3.9e+002 1.6e+004 -8.99e-001 -1.109052028e+005 2.518501256e+001 1.3e-001 0.36 4 2.9e+002 3.9e+002 1.6e+004 -7.64e-001 -1.087669500e+005 1.890337841e+003 1.3e-001 0.45 5 1.1e+002 1.5e+002 6.1e+003 -7.55e-001 -8.412356615e+004 7.783825718e+003 5.0e-002 0.53 6 4.3e+001 5.8e+001 2.3e+003 -4.05e-001 -4.824012559e+004 1.171597883e+004 1.9e-002 0.63 7 2.1e+001 2.8e+001 1.1e+003 2.01e-001 -2.781125767e+004 7.288540579e+003 9.1e-003 0.73 8 8.5e+000 1.2e+001 4.6e+002 5.86e-001 -1.238721603e+004 3.708949148e+003 3.7e-003 0.86 9 3.9e+000 5.3e+000 2.1e+002 8.57e-001 -5.637608012e+003 2.044299155e+003 1.7e-003 1.00 10 2.0e+000 2.8e+000 1.1e+002 9.52e-001 -2.781865865e+003 1.271934844e+003 9.1e-004 1.14 11 9.2e-001 1.2e+000 5.0e+001 9.85e-001 -1.247357556e+003 5.982207759e+002 4.1e-004 1.22 12 8.7e-001 1.3e+000 4.8e+001 9.63e-001 -1.215616937e+003 5.626008702e+002 3.9e-004 1.27 13 4.3e-001 6.3e-001 2.4e+001 9.80e-001 -5.888658100e+002 2.990299278e+002 2.0e-004 1.39 14 1.8e-001 2.7e-001 9.9e+000 1.00e+000 -2.437528373e+002 1.275957367e+002 8.2e-005 1.50 15 8.3e-002 1.5e-001 4.6e+000 1.00e+000 -1.042287248e+002 6.939763676e+001 3.9e-005 1.58 16 3.1e-002 1.0e-001 1.8e+000 1.00e+000 -3.163808195e+001 3.408267804e+001 1.5e-005 1.70 17 1.2e-002 1.0e-001 7.1e-001 1.00e+000 -5.104471616e+000 2.143967521e+001 6.1e-006 1.81 18 1.1e-002 9.1e-002 6.4e-001 1.00e+000 -2.786340395e+000 2.113403223e+001 5.5e-006 1.95 19 6.0e-003 6.7e-002 3.5e-001 1.00e+000 4.844302416e+000 1.776295680e+001 3.0e-006 2.11 20 3.5e-003 5.2e-002 2.0e-001 1.01e+000 8.846789613e+000 1.635871194e+001 1.7e-006 2.16 21 2.7e-003 4.3e-002 1.6e-001 1.02e+000 1.013118000e+001 1.585680334e+001 1.3e-006 2.23 22 2.1e-003 3.7e-002 1.2e-001 1.02e+000 1.111067354e+001 1.551012354e+001 1.0e-006 2.39 23 9.2e-004 4.8e-002 5.4e-002 1.02e+000 1.289742359e+001 1.487655721e+001 4.7e-007 2.53 24 5.1e-004 4.6e-002 3.0e-002 1.02e+000 1.350591699e+001 1.460873478e+001 2.6e-007 2.67 25 3.0e-004 4.5e-002 1.8e-002 1.01e+000 1.383474878e+001 1.447330951e+001 1.5e-007 2.81 26 2.0e-004 4.1e-002 1.2e-002 1.01e+000 1.398081988e+001 1.441221528e+001 1.0e-007 2.89 27 1.8e-004 3.8e-002 1.1e-002 1.01e+000 1.401710204e+001 1.440559783e+001 9.4e-008 3.06 28 1.6e-004 3.5e-002 9.7e-003 1.01e+000 1.404335921e+001 1.439287363e+001 8.4e-008 3.20 29 1.5e-004 3.2e-002 8.7e-003 1.01e+000 1.406784218e+001 1.438232961e+001 7.6e-008 3.36 30 1.3e-004 2.9e-002 7.9e-003 1.01e+000 1.408963337e+001 1.437260656e+001 6.8e-008 3.48 31 1.2e-004 2.7e-002 7.1e-003 1.01e+000 1.410919293e+001 1.436381727e+001 6.2e-008 3.63 32 1.1e-004 2.5e-002 6.4e-003 1.01e+000 1.412673392e+001 1.435585420e+001 5.5e-008 3.75 33 9.6e-005 2.4e-002 5.7e-003 1.00e+000 1.414247185e+001 1.434864681e+001 5.0e-008 3.91 34 8.6e-005 2.2e-002 5.2e-003 1.00e+000 1.415659379e+001 1.434212447e+001 4.5e-008 4.05 35 7.8e-005 2.1e-002 4.6e-003 1.00e+000 1.416926719e+001 1.433622321e+001 4.0e-008 4.20 36 7.0e-005 1.9e-002 4.2e-003 1.00e+000 1.418064146e+001 1.433088452e+001 3.6e-008 4.31 37 6.3e-005 1.8e-002 3.8e-003 1.00e+000 1.419085026e+001 1.432605487e+001 3.3e-008 4.41 38 5.7e-005 1.7e-002 3.4e-003 1.00e+000 1.420001344e+001 1.432168621e+001 2.9e-008 4.52 39 5.1e-005 1.6e-002 3.0e-003 1.00e+000 1.420823848e+001 1.431773456e+001 2.7e-008 4.63 40 4.6e-005 1.5e-002 2.7e-003 1.00e+000 1.421562223e+001 1.431416099e+001 2.4e-008 4.72 41 4.1e-005 1.5e-002 2.5e-003 1.00e+000 1.422225179e+001 1.431093079e+001 2.1e-008 4.83 42 3.7e-005 1.4e-002 2.2e-003 1.00e+000 1.422820554e+001 1.430801198e+001 1.9e-008 4.88 43 3.3e-005 1.3e-002 2.0e-003 1.00e+000 1.423355382e+001 1.430537568e+001 1.7e-008 4.94 44 3.0e-005 1.3e-002 1.8e-003 1.00e+000 1.423835935e+001 1.430299560e+001 1.6e-008 5.02 45 2.7e-005 1.2e-002 1.6e-003 1.00e+000 1.424267801e+001 1.430084800e+001 1.4e-008 5.06 46 2.4e-005 1.2e-002 1.5e-003 1.00e+000 1.424655960e+001 1.429891041e+001 1.3e-008 5.13 47 2.2e-005 1.1e-002 1.3e-003 1.00e+000 1.425004883e+001 1.429716312e+001 1.1e-008 5.22 48 2.0e-005 1.1e-002 1.2e-003 1.00e+000 1.425318568e+001 1.429558735e+001 1.0e-008 5.33 49 1.8e-005 1.1e-002 1.1e-003 1.00e+000 1.425600605e+001 1.429416650e+001 9.3e-009 5.42 50 1.6e-005 1.0e-002 9.6e-004 1.00e+000 1.425854205e+001 1.429288563e+001 8.3e-009 5.55 51 1.4e-005 1.0e-002 8.6e-004 1.00e+000 1.426082247e+001 1.429173114e+001 7.5e-009 5.72 52 1.3e-005 1.0e-002 7.7e-004 1.00e+000 1.426287312e+001 1.429069017e+001 6.7e-009 5.84 53 1.2e-005 9.7e-003 7.0e-004 1.00e+000 1.426471720e+001 1.428975215e+001 6.1e-009 5.97 54 1.0e-005 9.5e-003 6.3e-004 1.00e+000 1.426637542e+001 1.428890666e+001 5.5e-009 6.09 55 9.4e-006 9.4e-003 5.6e-004 1.00e+000 1.426786652e+001 1.428814424e+001 4.9e-009 6.27 56 8.5e-006 9.2e-003 5.1e-004 1.00e+000 1.426920729e+001 1.428745690e+001 4.4e-009 6.44 57 7.7e-006 9.0e-003 4.6e-004 1.00e+000 1.427041286e+001 1.428683694e+001 4.0e-009 6.61 58 6.9e-006 8.9e-003 4.1e-004 1.00e+000 1.427149673e+001 1.428627857e+001 3.6e-009 6.78 59 6.2e-006 8.8e-003 3.7e-004 1.00e+000 1.427247129e+001 1.428577463e+001 3.2e-009 6.94 60 5.6e-006 8.7e-003 3.3e-004 1.00e+000 1.427334761e+001 1.428532044e+001 2.9e-009 7.11 61 5.0e-006 8.6e-003 3.0e-004 1.00e+000 1.427413560e+001 1.428491118e+001 2.6e-009 7.28 62 4.5e-006 8.5e-003 2.7e-004 1.00e+000 1.427484435e+001 1.428454203e+001 2.4e-009 7.44 63 4.1e-006 8.4e-003 2.4e-004 1.00e+000 1.427548178e+001 1.428420987e+001 2.1e-009 7.61 64 3.7e-006 8.3e-003 2.2e-004 1.00e+000 1.427605523e+001 1.428391029e+001 1.9e-009 7.81 65 3.3e-006 8.3e-003 2.0e-004 1.00e+000 1.427657117e+001 1.428364040e+001 1.7e-009 7.98 66 3.0e-006 8.2e-003 1.8e-004 1.00e+000 1.427703528e+001 1.428339766e+001 1.5e-009 8.16 67 2.7e-006 8.1e-003 1.6e-004 1.00e+000 1.427745289e+001 1.428317887e+001 1.4e-009 8.33 68 2.4e-006 8.1e-003 1.4e-004 1.00e+000 1.427782863e+001 1.428298192e+001 1.3e-009 8.50 69 2.2e-006 8.0e-003 1.3e-004 9.99e-001 1.427816665e+001 1.428280493e+001 1.1e-009 8.70 70 1.9e-006 8.0e-003 1.2e-004 9.99e-001 1.427847080e+001 1.428264548e+001 1.0e-009 8.89 71 1.8e-006 7.9e-003 1.0e-004 1.00e+000 1.427874453e+001 1.428250176e+001 9.1e-010 9.06 72 1.6e-006 7.9e-003 9.4e-005 1.00e+000 1.427899085e+001 1.428237230e+001 8.2e-010 9.16 73 1.4e-006 7.9e-003 8.5e-005 1.00e+000 1.427921255e+001 1.428225553e+001 7.4e-010 9.27 74 1.3e-006 7.8e-003 7.6e-005 1.00e+000 1.427941208e+001 1.428215034e+001 6.7e-010 9.34 75 1.1e-006 7.8e-003 6.9e-005 1.00e+000 1.427959158e+001 1.428205580e+001 6.0e-010 9.48 76 1.0e-006 7.8e-003 6.2e-005 1.00e+000 1.427975356e+001 1.428197034e+001 5.4e-010 9.66 77 9.3e-007 7.8e-003 5.6e-005 9.97e-001 1.427989877e+001 1.428189418e+001 4.8e-010 9.70 78 8.4e-007 7.7e-003 5.0e-005 9.98e-001 1.428002947e+001 1.428182547e+001 4.4e-010 9.78 79 7.5e-007 7.0e-003 4.5e-005 1.01e+000 1.428014991e+001 1.428176158e+001 3.9e-010 9.84 80 6.8e-007 6.3e-003 4.1e-005 9.98e-001 1.428025548e+001 1.428170611e+001 3.5e-010 9.97 81 6.1e-007 5.6e-003 3.6e-005 1.00e+000 1.428035049e+001 1.428165605e+001 3.2e-010 10.09 82 5.5e-007 5.1e-003 3.3e-005 1.00e+000 1.428043703e+001 1.428161031e+001 2.9e-010 10.23 83 4.9e-007 4.6e-003 3.0e-005 1.00e+000 1.428051388e+001 1.428156980e+001 2.6e-010 10.38 84 4.4e-007 4.1e-003 2.7e-005 1.01e+000 1.428058440e+001 1.428153243e+001 2.3e-010 10.45 85 4.0e-007 3.7e-003 2.4e-005 1.00e+000 1.428064669e+001 1.428149952e+001 2.1e-010 10.55 86 3.6e-007 3.3e-003 2.2e-005 1.00e+000 1.428070258e+001 1.428147002e+001 1.9e-010 10.59 87 3.2e-007 3.0e-003 1.9e-005 9.98e-001 1.428075284e+001 1.428144356e+001 1.7e-010 10.67 88 2.9e-007 2.7e-003 1.7e-005 1.00e+000 1.428079829e+001 1.428141954e+001 1.5e-010 10.73 89 2.6e-007 2.4e-003 1.6e-005 1.02e+000 1.428084145e+001 1.428139647e+001 1.4e-010 10.78 90 2.4e-007 2.2e-003 1.4e-005 1.01e+000 1.428087980e+001 1.428137602e+001 1.3e-010 10.88 91 2.1e-007 2.0e-003 1.3e-005 9.87e-001 1.428091227e+001 1.428135914e+001 1.1e-010 10.94 92 1.9e-007 1.8e-003 1.1e-005 9.95e-001 1.428094152e+001 1.428134380e+001 1.0e-010 11.02 93 1.7e-007 1.6e-003 1.0e-005 1.04e+000 1.428097232e+001 1.428132700e+001 9.3e-011 11.08 94 1.6e-007 1.4e-003 9.3e-006 1.02e+000 1.428099797e+001 1.428131327e+001 8.5e-011 11.19 95 1.4e-007 1.3e-003 8.3e-006 1.02e+000 1.428102070e+001 1.428130112e+001 7.7e-011 11.28 96 1.3e-007 1.2e-003 7.5e-006 9.96e-001 1.428103912e+001 1.428129154e+001 6.9e-011 11.39 97 1.1e-007 1.0e-003 6.8e-006 9.86e-001 1.428105566e+001 1.428128299e+001 6.3e-011 11.47 98 1.0e-007 9.4e-004 6.1e-006 9.78e-001 1.428107054e+001 1.428127536e+001 5.6e-011 11.56 99 9.2e-008 8.5e-004 5.5e-006 1.09e+000 1.428108950e+001 1.428126458e+001 5.3e-011 11.63 100 8.3e-008 7.6e-004 4.9e-006 9.92e-001 1.428110103e+001 1.428125867e+001 4.8e-011 11.69 101 7.4e-008 6.9e-004 4.4e-006 1.01e+000 1.428111192e+001 1.428125296e+001 4.3e-011 11.78 102 6.7e-008 6.2e-004 4.0e-006 1.00e+000 1.428112130e+001 1.428124810e+001 3.9e-011 11.88 103 6.0e-008 5.6e-004 3.6e-006 9.92e-001 1.428112965e+001 1.428124378e+001 3.5e-011 11.98 104 5.4e-008 5.0e-004 3.2e-006 1.05e+000 1.428113888e+001 1.428123878e+001 3.2e-011 12.08 105 4.9e-008 4.5e-004 2.9e-006 1.01e+000 1.428114572e+001 1.428123523e+001 2.9e-011 12.19 106 4.4e-008 4.0e-004 2.6e-006 8.70e-001 1.428115152e+001 1.428123263e+001 2.6e-011 12.30 107 4.0e-008 3.6e-004 2.4e-006 9.32e-001 1.428115680e+001 1.428123003e+001 2.4e-011 12.39 108 3.6e-008 3.3e-004 2.1e-006 1.00e+000 1.428116160e+001 1.428122751e+001 2.1e-011 12.47 109 3.2e-008 3.0e-004 1.9e-006 9.88e-001 1.428116592e+001 1.428122527e+001 1.9e-011 12.55 110 2.9e-008 2.7e-004 1.7e-006 1.00e+000 1.428116986e+001 1.428122318e+001 1.7e-011 12.61 111 2.6e-008 2.4e-004 1.5e-006 9.91e-001 1.428117335e+001 1.428122137e+001 1.6e-011 12.66 112 2.3e-008 2.2e-004 1.4e-006 9.79e-001 1.428117649e+001 1.428121975e+001 1.4e-011 12.75 113 2.1e-008 1.9e-004 1.3e-006 9.93e-001 1.428117932e+001 1.428121826e+001 1.3e-011 12.86 114 1.9e-008 1.7e-004 1.1e-006 1.02e+000 1.428118206e+001 1.428121678e+001 1.1e-011 12.95 115 1.7e-008 1.6e-004 1.0e-006 9.96e-001 1.428118433e+001 1.428121559e+001 1.0e-011 13.06 116 1.5e-008 1.4e-004 9.1e-007 9.63e-001 1.428118637e+001 1.428121456e+001 9.2e-012 13.14 117 1.4e-008 1.3e-004 8.2e-007 9.95e-001 1.428118821e+001 1.428121359e+001 8.3e-012 13.20 118 1.2e-008 1.1e-004 7.4e-007 1.00e+000 1.428118987e+001 1.428121271e+001 7.5e-012 13.27 119 1.1e-008 1.0e-004 6.7e-007 9.79e-001 1.428119136e+001 1.428121194e+001 6.7e-012 13.34 120 1.0e-008 9.3e-005 6.0e-007 1.03e+000 1.428119285e+001 1.428121112e+001 6.1e-012 13.41 121 9.1e-009 8.3e-005 5.4e-007 1.05e+000 1.428119428e+001 1.428121031e+001 5.7e-012 13.50 122 8.2e-009 7.5e-005 4.9e-007 1.00e+000 1.428119533e+001 1.428120976e+001 5.1e-012 13.63 123 7.3e-009 6.8e-005 4.4e-007 1.00e+000 1.428119628e+001 1.428120926e+001 4.6e-012 13.73 124 6.6e-009 6.1e-005 3.9e-007 1.05e+000 1.428119732e+001 1.428120868e+001 4.2e-012 13.83 125 6.0e-009 5.5e-005 3.5e-007 9.28e-001 1.428119806e+001 1.428120832e+001 3.8e-012 13.94 126 5.4e-009 4.9e-005 3.2e-007 1.04e+000 1.428119885e+001 1.428120788e+001 3.5e-012 14.05 127 4.9e-009 4.4e-005 2.9e-007 1.07e+000 1.428119962e+001 1.428120744e+001 3.3e-012 14.16 128 4.4e-009 4.0e-005 2.6e-007 1.07e+000 1.428120030e+001 1.428120706e+001 3.0e-012 14.23 129 4.0e-009 3.6e-005 2.3e-007 9.71e-001 1.428120075e+001 1.428120684e+001 2.7e-012 14.34 130 3.6e-009 3.2e-005 2.1e-007 1.22e+000 1.428120116e+001 1.428120658e+001 2.5e-012 14.48 131 3.2e-009 2.9e-005 1.9e-007 1.06e+000 1.428120162e+001 1.428120634e+001 2.3e-012 14.53 Interior-point optimizer terminated. Time: 14.55. Optimizer terminated. Time: 14.58 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.4281201621e+001 nrm: 3e+002 Viol. con: 3e-008 var: 0e+000 Dual. obj: 1.4281206339e+001 nrm: 8e+002 Viol. con: 0e+000 var: 1e-004 * End solution on dual form. * Transforming to primal solution. Solving took 14.6 seconds. result packing took 2.2% of solve time solution checking took 0.59% of solve time Using solver 'mosek' Solving for 1899 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6216) of matrix 'A'. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'. Number of Hessian non-zeros: 1953 * 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 : 1900 Cones : 0 Scalar variables : 6471 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 : 487 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 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 : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3607 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 : 1.53e+004 after factor : 1.76e+005 Factor - dense dim. : 0 flops : 3.97e+007 Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.230870188e+005 2.000000000e+000 1.0e+000 0.06 1 1.5e+003 2.1e+003 8.3e+004 -9.71e-001 -1.221562904e+005 2.804524657e+000 6.8e-001 0.17 2 6.7e+002 9.1e+002 3.6e+004 -9.55e-001 -1.185444295e+005 6.126748561e+000 2.9e-001 0.30 3 2.9e+002 3.9e+002 1.5e+004 -8.96e-001 -1.107350441e+005 2.591630622e+001 1.3e-001 0.41 4 2.9e+002 3.9e+002 1.5e+004 -7.64e-001 -1.083959783e+005 2.074738769e+003 1.3e-001 0.50 5 1.1e+002 1.5e+002 5.9e+003 -7.55e-001 -8.304293861e+004 8.001013464e+003 4.8e-002 0.59 6 4.5e+001 6.1e+001 2.4e+003 -3.87e-001 -5.007900790e+004 1.132754358e+004 2.0e-002 0.72 7 2.7e+001 3.7e+001 1.5e+003 1.77e-001 -3.519354404e+004 8.037059052e+003 1.2e-002 0.83 8 1.3e+001 1.8e+001 7.0e+002 4.62e-001 -1.863074082e+004 4.843511534e+003 5.8e-003 0.92 9 5.2e+000 7.0e+000 2.8e+002 7.51e-001 -7.592041561e+003 2.420006575e+003 2.3e-003 1.05 10 3.4e+000 4.7e+000 1.9e+002 9.25e-001 -4.950378075e+003 1.774570335e+003 1.5e-003 1.17 11 1.1e+000 1.5e+000 5.9e+001 9.59e-001 -1.561063642e+003 6.117735815e+002 4.9e-004 1.25 12 9.0e-001 1.4e+000 4.9e+001 9.84e-001 -1.270650577e+003 5.441526164e+002 4.1e-004 1.33 13 6.6e-001 1.1e+000 3.6e+001 9.71e-001 -9.474748999e+002 4.129975928e+002 3.0e-004 1.41 14 3.5e-001 6.0e-001 1.9e+001 9.99e-001 -4.733806301e+002 2.353628223e+002 1.6e-004 1.48 15 1.3e-001 2.5e-001 7.4e+000 9.95e-001 -1.818580117e+002 9.609628437e+001 6.2e-005 1.58 16 7.7e-002 1.6e-001 4.3e+000 1.01e+000 -1.009936739e+002 5.913032376e+001 3.6e-005 1.69 17 2.7e-002 1.1e-001 1.5e+000 1.01e+000 -3.128241268e+001 2.625196085e+001 1.3e-005 1.78 18 1.5e-002 8.9e-002 8.7e-001 1.01e+000 -1.385627201e+001 1.825404626e+001 7.4e-006 1.86 19 1.3e-002 6.6e-002 7.3e-001 1.03e+000 -8.632366276e+000 1.816632692e+001 6.2e-006 1.97 20 4.9e-003 6.5e-002 2.8e-001 1.01e+000 3.613204331e+000 1.391232974e+001 2.4e-006 2.06 21 2.5e-003 5.9e-002 1.5e-001 1.02e+000 7.373997333e+000 1.271678076e+001 1.3e-006 2.14 22 8.2e-004 7.3e-002 5.1e-002 9.89e-001 1.005578056e+001 1.191382486e+001 4.6e-007 2.19 23 2.5e-004 8.7e-002 1.6e-002 9.76e-001 1.099444693e+001 1.160405759e+001 1.5e-007 2.25 24 8.2e-005 8.7e-002 5.6e-003 9.85e-001 1.129692683e+001 1.150645361e+001 5.4e-008 2.30 25 3.2e-005 8.0e-002 2.2e-003 9.94e-001 1.139531565e+001 1.147879347e+001 2.2e-008 2.34 26 1.3e-005 7.6e-002 9.2e-004 9.98e-001 1.143398366e+001 1.146827796e+001 8.9e-009 2.42 27 5.7e-006 7.2e-002 4.0e-004 1.00e+000 1.144918369e+001 1.146406699e+001 3.9e-009 2.48 28 5.1e-006 6.5e-002 3.6e-004 1.00e+000 1.145049614e+001 1.146389183e+001 3.5e-009 2.55 29 4.6e-006 5.9e-002 3.2e-004 1.00e+000 1.145151736e+001 1.146357361e+001 3.1e-009 2.59 30 4.2e-006 5.4e-002 2.9e-004 1.00e+000 1.145243806e+001 1.146328851e+001 2.8e-009 2.66 31 3.7e-006 4.9e-002 2.6e-004 1.00e+000 1.145326534e+001 1.146303053e+001 2.5e-009 2.72 32 3.4e-006 4.5e-002 2.4e-004 1.00e+000 1.145400930e+001 1.146279762e+001 2.3e-009 2.78 33 3.0e-006 4.1e-002 2.1e-004 1.00e+000 1.145467829e+001 1.146258774e+001 2.1e-009 2.83 34 2.7e-006 3.8e-002 1.9e-004 1.00e+000 1.145527996e+001 1.146239855e+001 1.9e-009 2.88 35 2.5e-006 3.5e-002 1.7e-004 1.00e+000 1.145582121e+001 1.146222768e+001 1.7e-009 2.94 36 2.2e-006 3.2e-002 1.5e-004 1.00e+000 1.145630805e+001 1.146207391e+001 1.5e-009 3.00 37 2.0e-006 3.0e-002 1.4e-004 1.00e+000 1.145674600e+001 1.146193532e+001 1.3e-009 3.05 38 1.8e-006 2.7e-002 1.3e-004 1.00e+000 1.145714005e+001 1.146181027e+001 1.2e-009 3.11 39 1.6e-006 2.5e-002 1.1e-004 1.00e+000 1.145749458e+001 1.146169763e+001 1.1e-009 3.16 40 1.4e-006 2.4e-002 1.0e-004 9.98e-001 1.145781345e+001 1.146159657e+001 9.8e-010 3.22 41 1.3e-006 2.2e-002 9.1e-005 1.00e+000 1.145810044e+001 1.146150523e+001 8.9e-010 3.30 42 1.2e-006 2.0e-002 8.2e-005 1.00e+000 1.145835866e+001 1.146142301e+001 8.0e-010 3.36 43 1.1e-006 1.9e-002 7.4e-005 9.97e-001 1.145859092e+001 1.146134934e+001 7.2e-010 3.41 44 9.5e-007 1.8e-002 6.7e-005 1.00e+000 1.145880030e+001 1.146128217e+001 6.5e-010 3.47 45 8.6e-007 1.7e-002 6.0e-005 1.01e+000 1.145899182e+001 1.146122046e+001 5.8e-010 3.53 46 7.7e-007 1.6e-002 5.4e-005 1.00e+000 1.145916084e+001 1.146116639e+001 5.2e-010 3.58 47 6.9e-007 1.5e-002 4.9e-005 1.00e+000 1.145931289e+001 1.146111786e+001 4.7e-010 3.64 48 6.2e-007 1.4e-002 4.4e-005 9.97e-001 1.145944966e+001 1.146107442e+001 4.2e-010 3.69 49 5.6e-007 1.4e-002 3.9e-005 1.00e+000 1.145957375e+001 1.146103477e+001 3.8e-010 3.75 50 5.1e-007 1.3e-002 3.5e-005 9.98e-001 1.145968444e+001 1.146099950e+001 3.4e-010 3.80 51 1.8e-007 4.5e-003 1.2e-005 9.94e-001 1.146033705e+001 1.146079270e+001 1.2e-010 3.84 52 1.6e-007 4.0e-003 1.1e-005 1.02e+000 1.146037404e+001 1.146078039e+001 1.1e-010 3.89 53 6.8e-008 1.4e-003 3.8e-006 9.53e-001 1.146057752e+001 1.146071903e+001 3.8e-011 3.94 54 6.7e-008 1.2e-003 3.4e-006 1.07e+000 1.146059103e+001 1.146071338e+001 3.6e-011 4.00 55 8.4e-008 1.1e-003 3.0e-006 2.14e+000 1.146059818e+001 1.146071920e+001 3.2e-011 4.06 56 7.2e-008 2.1e-005 5.8e-008 7.26e-001 1.146069089e+001 1.146069359e+001 4.7e-012 4.13 Interior-point optimizer terminated. Time: 4.14. Optimizer terminated. Time: 4.16 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1460690889e+001 nrm: 1e+002 Viol. con: 2e-006 var: 0e+000 Dual. obj: 1.1460693590e+001 nrm: 8e+002 Viol. con: 0e+000 var: 2e-004 * End solution on dual form. * Transforming to primal solution. Solving took 4.19 seconds. result packing took 14% of solve time solution checking took 3.3% of solve time Using solver 'mosek' Solving for 1899 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'. Number of Hessian non-zeros: 1953 * 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 : 1900 Cones : 0 Scalar variables : 6471 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 : 487 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 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 : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3607 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.05 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.05 Factor - nonzeros before factor : 1.53e+004 after factor : 1.76e+005 Factor - dense dim. : 0 flops : 3.97e+007 Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.230224434e+005 2.000000000e+000 1.0e+000 0.11 1 1.6e+003 2.1e+003 8.4e+004 -9.71e-001 -1.221078250e+005 2.791154484e+000 6.8e-001 0.19 2 7.0e+002 9.6e+002 3.8e+004 -9.56e-001 -1.187969029e+005 5.799400417e+000 3.1e-001 0.23 3 2.9e+002 3.9e+002 1.5e+004 -9.01e-001 -1.107028731e+005 2.527999472e+001 1.3e-001 0.30 4 2.9e+002 3.9e+002 1.5e+004 -7.65e-001 -1.083499739e+005 2.088232838e+003 1.3e-001 0.38 5 1.4e+002 1.8e+002 7.3e+003 -7.56e-001 -9.013673297e+004 6.370757503e+003 6.0e-002 0.45 6 4.3e+001 5.8e+001 2.3e+003 -4.97e-001 -4.846931821e+004 1.174255219e+004 1.9e-002 0.53 7 2.3e+001 3.2e+001 1.3e+003 2.03e-001 -3.104817568e+004 7.486106444e+003 1.0e-002 0.61 8 1.1e+001 1.5e+001 5.8e+002 5.40e-001 -1.573200993e+004 4.181966197e+003 4.8e-003 0.69 9 4.7e+000 6.4e+000 2.5e+002 8.04e-001 -6.938620631e+003 2.240934011e+003 2.1e-003 0.75 10 2.2e+000 3.0e+000 1.2e+002 9.34e-001 -3.068869138e+003 1.209368851e+003 9.7e-004 0.80 11 1.4e+000 1.9e+000 7.7e+001 9.84e-001 -1.999555552e+003 8.255100905e+002 6.4e-004 0.86 12 9.4e-001 1.3e+000 5.1e+001 9.86e-001 -1.316984913e+003 5.684401213e+002 4.2e-004 0.92 13 7.8e-001 1.2e+000 4.3e+001 9.64e-001 -1.116593437e+003 4.784425275e+002 3.5e-004 0.97 14 3.1e-001 4.9e-001 1.7e+001 9.90e-001 -4.317637135e+002 2.064154795e+002 1.4e-004 1.03 15 1.5e-001 2.5e-001 8.5e+000 1.00e+000 -2.108188011e+002 1.081421538e+002 7.1e-005 1.09 16 4.8e-002 1.5e-001 2.7e+000 1.00e+000 -6.193336183e+001 3.891286204e+001 2.3e-005 1.16 17 3.9e-002 1.3e-001 2.2e+000 1.00e+000 -4.879777072e+001 3.332971043e+001 1.9e-005 1.22 18 2.1e-002 9.0e-002 1.2e+000 1.00e+000 -2.297472686e+001 2.142904986e+001 1.0e-005 1.30 19 1.5e-002 7.0e-002 8.6e-001 1.02e+000 -1.327872082e+001 1.845277539e+001 7.3e-006 1.36 20 7.7e-003 4.8e-002 4.4e-001 1.03e+000 -6.665440276e-001 1.527645752e+001 3.7e-006 1.44 21 2.6e-003 7.3e-002 1.5e-001 1.02e+000 7.285398634e+000 1.268744172e+001 1.3e-006 1.50 22 1.5e-003 5.4e-002 8.9e-002 9.94e-001 8.864089672e+000 1.209399991e+001 7.8e-007 1.55 23 4.9e-004 7.4e-002 3.1e-002 9.81e-001 1.049751812e+001 1.162667840e+001 2.8e-007 1.61 24 1.8e-004 7.3e-002 1.2e-002 9.83e-001 1.101837814e+001 1.145789473e+001 1.1e-007 1.66 25 8.3e-005 6.8e-002 5.5e-003 9.94e-001 1.119790450e+001 1.140058842e+001 5.1e-008 1.72 26 3.9e-005 6.5e-002 2.6e-003 9.98e-001 1.127981370e+001 1.137560754e+001 2.4e-008 1.77 27 3.5e-005 5.9e-002 2.3e-003 9.99e-001 1.128921527e+001 1.137545689e+001 2.2e-008 1.83 28 3.2e-005 5.4e-002 2.1e-003 1.00e+000 1.129561885e+001 1.137324224e+001 2.0e-008 1.88 29 2.8e-005 4.9e-002 1.9e-003 1.00e+000 1.130147717e+001 1.137134632e+001 1.8e-008 1.92 30 2.6e-005 4.5e-002 1.7e-003 1.00e+000 1.130672028e+001 1.136960881e+001 1.6e-008 1.97 31 2.3e-005 4.1e-002 1.5e-003 1.00e+000 1.131142552e+001 1.136803050e+001 1.4e-008 2.02 32 2.1e-005 3.8e-002 1.4e-003 1.00e+000 1.131564806e+001 1.136659698e+001 1.3e-008 2.08 33 1.9e-005 3.5e-002 1.2e-003 1.00e+000 1.131943858e+001 1.136529623e+001 1.2e-008 2.14 34 1.7e-005 3.2e-002 1.1e-003 1.00e+000 1.132284206e+001 1.136411685e+001 1.1e-008 2.17 35 1.5e-005 3.0e-002 1.0e-003 1.00e+000 1.132589868e+001 1.136304849e+001 9.5e-009 2.23 36 1.4e-005 2.7e-002 9.0e-004 1.00e+000 1.132864429e+001 1.136208127e+001 8.5e-009 2.30 37 1.2e-005 2.5e-002 8.1e-004 1.00e+000 1.133111099e+001 1.136120603e+001 7.7e-009 2.41 38 1.1e-005 2.4e-002 7.3e-004 1.00e+000 1.133332753e+001 1.136041455e+001 6.9e-009 2.48 39 9.9e-006 2.2e-002 6.6e-004 1.00e+000 1.133531956e+001 1.135969911e+001 6.2e-009 2.58 40 8.9e-006 2.1e-002 5.9e-004 1.00e+000 1.133711005e+001 1.135905272e+001 5.6e-009 2.67 41 8.0e-006 1.9e-002 5.3e-004 1.00e+000 1.133871959e+001 1.135846878e+001 5.0e-009 2.73 42 7.2e-006 1.8e-002 4.8e-004 1.00e+000 1.134016660e+001 1.135794148e+001 4.5e-009 2.81 43 6.5e-006 1.7e-002 4.3e-004 1.00e+000 1.134146757e+001 1.135746559e+001 4.1e-009 2.89 44 5.9e-006 1.6e-002 3.9e-004 1.00e+000 1.134263729e+001 1.135703595e+001 3.7e-009 2.92 45 5.3e-006 1.5e-002 3.5e-004 1.00e+000 1.134368908e+001 1.135664829e+001 3.3e-009 2.95 46 4.7e-006 1.4e-002 3.2e-004 1.00e+000 1.134463486e+001 1.135629844e+001 3.0e-009 2.97 47 4.3e-006 1.4e-002 2.8e-004 1.00e+000 1.134548533e+001 1.135598299e+001 2.7e-009 2.98 48 3.8e-006 1.3e-002 2.6e-004 1.00e+000 1.134625019e+001 1.135569842e+001 2.4e-009 3.00 49 3.5e-006 1.3e-002 2.3e-004 1.00e+000 1.134693814e+001 1.135544171e+001 2.2e-009 3.02 50 3.1e-006 1.2e-002 2.1e-004 1.00e+000 1.134755692e+001 1.135521045e+001 1.9e-009 3.05 51 2.8e-006 1.2e-002 1.9e-004 1.00e+000 1.134811357e+001 1.135500197e+001 1.8e-009 3.06 52 2.5e-006 1.1e-002 1.7e-004 1.00e+000 1.134861441e+001 1.135481403e+001 1.6e-009 3.08 53 2.3e-006 1.1e-002 1.5e-004 1.00e+000 1.134906501e+001 1.135464479e+001 1.4e-009 3.09 54 2.0e-006 1.0e-002 1.4e-004 1.00e+000 1.134947048e+001 1.135449232e+001 1.3e-009 3.11 55 1.8e-006 1.0e-002 1.2e-004 1.00e+000 1.134983533e+001 1.135435508e+001 1.2e-009 3.13 56 1.7e-006 9.8e-003 1.1e-004 1.00e+000 1.135016366e+001 1.135423150e+001 1.0e-009 3.14 57 1.5e-006 9.6e-003 9.9e-005 1.00e+000 1.135045915e+001 1.135412021e+001 9.3e-010 3.16 58 1.3e-006 9.4e-003 8.9e-005 1.00e+000 1.135072510e+001 1.135401999e+001 8.4e-010 3.19 59 1.2e-006 9.2e-003 8.0e-005 1.00e+000 1.135096443e+001 1.135392982e+001 7.5e-010 3.20 60 1.1e-006 9.0e-003 7.2e-005 1.00e+000 1.135117982e+001 1.135384876e+001 6.8e-010 3.25 61 9.8e-007 8.8e-003 6.5e-005 1.00e+000 1.135137369e+001 1.135377573e+001 6.1e-010 3.28 62 8.8e-007 8.7e-003 5.9e-005 9.98e-001 1.135154813e+001 1.135371018e+001 5.5e-010 3.30 63 7.9e-007 8.5e-003 5.3e-005 1.00e+000 1.135170517e+001 1.135365107e+001 5.0e-010 3.31 64 7.1e-007 8.4e-003 4.7e-005 1.00e+000 1.135184655e+001 1.135359778e+001 4.5e-010 3.33 65 6.4e-007 8.3e-003 4.3e-005 1.00e+000 1.135197377e+001 1.135354987e+001 4.0e-010 3.34 66 5.8e-007 8.2e-003 3.8e-005 9.99e-001 1.135208826e+001 1.135350682e+001 3.6e-010 3.36 67 5.2e-007 8.1e-003 3.5e-005 1.00e+000 1.135219132e+001 1.135346805e+001 3.2e-010 3.38 68 4.7e-007 8.0e-003 3.1e-005 9.96e-001 1.135228404e+001 1.135343331e+001 2.9e-010 3.41 69 4.2e-007 7.9e-003 2.8e-005 9.99e-001 1.135236751e+001 1.135340194e+001 2.6e-010 3.42 70 3.8e-007 7.9e-003 2.5e-005 9.98e-001 1.135244264e+001 1.135337374e+001 2.4e-010 3.45 71 3.4e-007 7.8e-003 2.3e-005 1.00e+000 1.135251027e+001 1.135334828e+001 2.1e-010 3.47 72 3.1e-007 7.8e-003 2.0e-005 9.99e-001 1.135257113e+001 1.135332539e+001 1.9e-010 3.48 73 2.8e-007 7.7e-003 1.8e-005 1.00e+000 1.135262593e+001 1.135330473e+001 1.7e-010 3.50 74 2.5e-007 7.7e-003 1.7e-005 1.00e+000 1.135267523e+001 1.135328616e+001 1.6e-010 3.56 75 2.2e-007 7.6e-003 1.5e-005 1.00e+000 1.135271968e+001 1.135326937e+001 1.4e-010 3.58 76 2.0e-007 6.9e-003 1.3e-005 1.01e+000 1.135276053e+001 1.135325386e+001 1.3e-010 3.61 77 1.8e-007 6.2e-003 1.2e-005 9.97e-001 1.135279636e+001 1.135324045e+001 1.1e-010 3.63 78 1.6e-007 5.6e-003 1.1e-005 9.94e-001 1.135282859e+001 1.135322840e+001 1.0e-010 3.64 79 1.5e-007 5.0e-003 9.8e-006 1.00e+000 1.135285763e+001 1.135321745e+001 9.2e-011 3.66 80 1.3e-007 4.5e-003 8.8e-006 1.00e+000 1.135288389e+001 1.135320760e+001 8.3e-011 3.67 81 1.2e-007 4.1e-003 7.9e-006 1.00e+000 1.135290763e+001 1.135319862e+001 7.5e-011 3.69 82 1.1e-007 3.7e-003 7.1e-006 1.00e+000 1.135292876e+001 1.135319066e+001 6.7e-011 3.70 83 9.6e-008 3.3e-003 6.4e-006 9.89e-001 1.135294775e+001 1.135318359e+001 6.0e-011 3.72 84 8.7e-008 3.0e-003 5.8e-006 1.00e+000 1.135296487e+001 1.135317712e+001 5.4e-011 3.75 85 7.8e-008 2.7e-003 5.2e-006 9.90e-001 1.135298026e+001 1.135317138e+001 4.9e-011 3.77 86 7.0e-008 2.4e-003 4.7e-006 1.00e+000 1.135299425e+001 1.135316607e+001 4.4e-011 3.81 87 6.3e-008 2.2e-003 4.2e-006 1.02e+000 1.135300756e+001 1.135316095e+001 4.0e-011 3.83 88 5.7e-008 1.9e-003 3.8e-006 1.01e+000 1.135301936e+001 1.135315642e+001 3.6e-011 3.84 89 5.1e-008 1.7e-003 3.4e-006 1.02e+000 1.135303018e+001 1.135315225e+001 3.3e-011 3.86 90 4.6e-008 1.6e-003 3.1e-006 9.94e-001 1.135303905e+001 1.135314895e+001 3.0e-011 3.89 91 4.1e-008 1.4e-003 2.8e-006 1.02e+000 1.135304773e+001 1.135314560e+001 2.7e-011 3.91 92 3.7e-008 1.3e-003 2.5e-006 1.00e+000 1.135305485e+001 1.135314294e+001 2.4e-011 3.92 93 3.4e-008 1.1e-003 2.2e-006 9.77e-001 1.135306123e+001 1.135314061e+001 2.2e-011 3.97 94 3.0e-008 1.0e-003 2.0e-006 9.72e-001 1.135306698e+001 1.135313852e+001 2.0e-011 3.98 95 2.7e-008 9.3e-004 1.8e-006 1.03e+000 1.135307283e+001 1.135313620e+001 1.8e-011 4.00 96 2.5e-008 8.4e-004 1.6e-006 1.01e+000 1.135307760e+001 1.135313445e+001 1.6e-011 4.05 97 2.3e-008 7.5e-004 1.5e-006 9.89e-001 1.135308171e+001 1.135313298e+001 1.5e-011 4.06 98 2.1e-008 6.8e-004 1.3e-006 9.79e-001 1.135308542e+001 1.135313160e+001 1.3e-011 4.08 99 1.0e-007 4.1e-004 9.5e-008 9.08e-001 1.135313352e+001 1.135313979e+001 3.8e-012 4.13 100 1.1e-007 4.1e-004 9.5e-008 9.87e-001 1.135313437e+001 1.135314079e+001 3.8e-012 4.16 101 2.7e-007 2.4e-004 5.8e-008 9.07e-001 1.135331764e+001 1.135334430e+001 7.9e-013 4.19 102 2.6e-007 2.2e-004 5.2e-008 9.26e-001 1.135331348e+001 1.135333841e+001 7.1e-013 4.20 103 2.4e-007 2.0e-004 4.7e-008 1.00e+000 1.135331190e+001 1.135333533e+001 6.4e-013 4.24 104 2.2e-007 1.9e-004 4.2e-008 9.20e-001 1.135329416e+001 1.135331534e+001 5.8e-013 4.25 105 2.0e-007 1.7e-004 3.8e-008 1.04e+000 1.135327185e+001 1.135329044e+001 5.3e-013 4.27 106 1.8e-007 1.6e-004 3.4e-008 9.43e-001 1.135325673e+001 1.135327348e+001 4.8e-013 4.28 107 1.6e-007 1.4e-004 3.1e-008 1.13e+000 1.135323557e+001 1.135324973e+001 4.6e-013 4.30 108 1.5e-007 1.3e-004 2.8e-008 9.25e-001 1.135322515e+001 1.135323796e+001 4.1e-013 4.31 109 1.3e-007 1.1e-004 2.5e-008 1.04e+000 1.135321290e+001 1.135322424e+001 3.8e-013 4.33 Interior-point optimizer terminated. Time: 4.34. Optimizer terminated. Time: 4.36 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1353212904e+001 nrm: 4e+001 Viol. con: 3e-005 var: 0e+000 Dual. obj: 1.1353224237e+001 nrm: 8e+002 Viol. con: 0e+000 var: 3e-002 * End solution on dual form. * Transforming to primal solution. Solving took 4.41 seconds. result packing took 6.3% of solve time solution checking took 1.5% of solve time Using solver 'mosek' Solving for 1899 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6216) of matrix 'A'. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'. Number of Hessian non-zeros: 1953 * 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 : 1900 Cones : 0 Scalar variables : 6471 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 : 487 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 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 : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3608 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.05 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 1.53e+004 after factor : 1.76e+005 Factor - dense dim. : 0 flops : 3.97e+007 Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.232389052e+005 2.000000000e+000 1.0e+000 0.09 1 1.6e+003 2.1e+003 8.4e+004 -9.71e-001 -1.223329704e+005 2.782320903e+000 6.8e-001 0.13 2 7.0e+002 9.6e+002 3.8e+004 -9.56e-001 -1.190342852e+005 5.777216904e+000 3.1e-001 0.16 3 3.0e+002 4.0e+002 1.6e+004 -9.02e-001 -1.113435916e+005 2.374527692e+001 1.3e-001 0.20 4 2.9e+002 3.9e+002 1.5e+004 -7.76e-001 -1.085279307e+005 2.132673953e+003 1.3e-001 0.22 5 1.5e+002 2.1e+002 8.2e+003 -7.56e-001 -9.386893641e+004 5.592734311e+003 6.8e-002 0.25 6 4.6e+001 6.3e+001 2.5e+003 -5.50e-001 -5.135599741e+004 1.182882004e+004 2.0e-002 0.28 7 2.2e+001 3.1e+001 1.2e+003 1.49e-001 -2.972303161e+004 7.891100997e+003 9.9e-003 0.30 8 1.1e+001 1.5e+001 5.7e+002 5.63e-001 -1.546607033e+004 4.321095096e+003 4.7e-003 0.31 9 3.9e+000 5.3e+000 2.1e+002 8.11e-001 -5.793212117e+003 1.916643320e+003 1.7e-003 0.34 10 1.8e+000 2.5e+000 1.0e+002 9.51e-001 -2.547314304e+003 1.153456120e+003 8.3e-004 0.36 11 9.8e-001 1.3e+000 5.3e+001 9.87e-001 -1.361269637e+003 6.166844458e+002 4.4e-004 0.38 12 9.0e-001 1.2e+000 4.9e+001 9.73e-001 -1.281020639e+003 5.639239699e+002 4.1e-004 0.39 13 4.8e-001 6.7e-001 2.6e+001 9.82e-001 -6.836689457e+002 3.083519471e+002 2.2e-004 0.42 14 1.9e-001 4.5e-001 1.0e+001 9.98e-001 -2.638116534e+002 1.240002904e+002 8.6e-005 0.45 15 8.8e-002 2.3e-001 4.9e+000 1.01e+000 -1.186364759e+002 6.592278305e+001 4.1e-005 0.48 16 4.8e-002 1.3e-001 2.7e+000 1.01e+000 -6.179591710e+001 3.972665191e+001 2.3e-005 0.53 17 2.2e-002 9.4e-002 1.3e+000 1.01e+000 -2.507328407e+001 2.237194552e+001 1.1e-005 0.56 18 2.1e-002 8.8e-002 1.2e+000 1.02e+000 -2.254271939e+001 2.185654656e+001 1.0e-005 0.61 19 1.1e-002 6.6e-002 6.2e-001 1.02e+000 -6.182846189e+000 1.650026342e+001 5.2e-006 0.64 20 4.3e-003 6.1e-002 2.5e-001 1.03e+000 4.554701468e+000 1.363169644e+001 2.1e-006 0.67 21 1.9e-003 5.9e-002 1.1e-001 1.00e+000 8.283529060e+000 1.230159633e+001 9.6e-007 0.70 22 1.1e-003 4.8e-002 6.6e-002 9.75e-001 9.420511781e+000 1.187318164e+001 5.9e-007 0.78 23 3.4e-004 7.6e-002 2.2e-002 9.73e-001 1.071454154e+001 1.152950530e+001 2.0e-007 0.80 24 1.9e-004 6.1e-002 1.2e-002 9.85e-001 1.098621509e+001 1.143493177e+001 1.1e-007 0.83 25 1.7e-004 5.5e-002 1.1e-002 9.91e-001 1.102378549e+001 1.142774647e+001 9.8e-008 0.84 26 1.5e-004 5.0e-002 9.7e-003 9.91e-001 1.105475753e+001 1.141854508e+001 8.9e-008 0.86 27 1.4e-004 4.6e-002 8.7e-003 9.91e-001 1.108363117e+001 1.141125554e+001 8.0e-008 0.88 28 1.2e-004 4.2e-002 7.9e-003 9.92e-001 1.110951367e+001 1.140455419e+001 7.2e-008 0.91 29 1.1e-004 3.9e-002 7.1e-003 9.93e-001 1.113274259e+001 1.139842812e+001 6.5e-008 0.92 30 9.9e-005 3.6e-002 6.4e-003 9.94e-001 1.115356952e+001 1.139281008e+001 5.8e-008 0.94 31 8.9e-005 3.3e-002 5.7e-003 9.94e-001 1.117224188e+001 1.138766084e+001 5.2e-008 0.98 32 8.0e-005 3.0e-002 5.2e-003 9.95e-001 1.118898039e+001 1.138294229e+001 4.7e-008 1.00 33 7.2e-005 2.8e-002 4.6e-003 9.95e-001 1.120398433e+001 1.137862008e+001 4.2e-008 1.01 34 6.5e-005 2.6e-002 4.2e-003 9.96e-001 1.121743335e+001 1.137466331e+001 3.8e-008 1.03 35 5.8e-005 2.4e-002 3.8e-003 9.96e-001 1.122948893e+001 1.137104355e+001 3.4e-008 1.05 36 5.3e-005 2.2e-002 3.4e-003 9.97e-001 1.124029601e+001 1.136773434e+001 3.1e-008 1.06 37 4.7e-005 2.1e-002 3.1e-003 9.97e-001 1.124998477e+001 1.136471142e+001 2.8e-008 1.08 38 4.3e-005 1.9e-002 2.7e-003 9.97e-001 1.125867166e+001 1.136195197e+001 2.5e-008 1.09 39 3.8e-005 1.8e-002 2.5e-003 9.98e-001 1.126646098e+001 1.135943485e+001 2.3e-008 1.13 40 3.5e-005 1.7e-002 2.2e-003 9.98e-001 1.127344607e+001 1.135714029e+001 2.0e-008 1.14 41 3.1e-005 1.6e-002 2.0e-003 9.98e-001 1.127971068e+001 1.135504994e+001 1.8e-008 1.16 42 2.8e-005 1.5e-002 1.8e-003 9.98e-001 1.128533004e+001 1.135314717e+001 1.6e-008 1.20 43 2.5e-005 1.4e-002 1.6e-003 9.99e-001 1.129037166e+001 1.135141671e+001 1.5e-008 1.23 44 2.3e-005 1.4e-002 1.5e-003 9.99e-001 1.129489594e+001 1.134984436e+001 1.3e-008 1.30 45 2.0e-005 1.3e-002 1.3e-003 9.99e-001 1.129895681e+001 1.134841685e+001 1.2e-008 1.33 46 1.8e-005 1.3e-002 1.2e-003 9.99e-001 1.130260245e+001 1.134712175e+001 1.1e-008 1.34 47 1.7e-005 1.2e-002 1.1e-003 9.99e-001 1.130587594e+001 1.134594748e+001 9.7e-009 1.38 48 1.5e-005 1.2e-002 9.6e-004 9.99e-001 1.130881585e+001 1.134488362e+001 8.8e-009 1.42 49 1.3e-005 1.1e-002 8.6e-004 9.99e-001 1.131145660e+001 1.134392038e+001 7.9e-009 1.47 50 1.2e-005 1.1e-002 7.8e-004 1.00e+000 1.131382900e+001 1.134304862e+001 7.1e-009 1.51 51 1.1e-005 1.0e-002 7.0e-004 1.00e+000 1.131596065e+001 1.134226011e+001 6.4e-009 1.56 52 9.7e-006 1.0e-002 6.3e-004 1.00e+000 1.131787621e+001 1.134154717e+001 5.8e-009 1.58 53 8.8e-006 9.9e-003 5.7e-004 1.00e+000 1.131959779e+001 1.134090285e+001 5.2e-009 1.64 54 7.9e-006 9.6e-003 5.1e-004 1.00e+000 1.132114516e+001 1.134032075e+001 4.7e-009 1.66 55 7.1e-006 9.4e-003 4.6e-004 1.00e+000 1.132253605e+001 1.133979496e+001 4.2e-009 1.67 56 6.4e-006 9.2e-003 4.1e-004 1.00e+000 1.132378637e+001 1.133932012e+001 3.8e-009 1.70 57 5.8e-006 9.0e-003 3.7e-004 1.00e+000 1.132491038e+001 1.133889138e+001 3.4e-009 1.72 58 5.2e-006 8.9e-003 3.3e-004 1.00e+000 1.132592090e+001 1.133850419e+001 3.1e-009 1.73 59 4.7e-006 8.7e-003 3.0e-004 1.00e+000 1.132682943e+001 1.133815471e+001 2.8e-009 1.75 60 4.2e-006 8.6e-003 2.7e-004 1.00e+000 1.132764630e+001 1.133783940e+001 2.5e-009 1.78 61 3.8e-006 8.4e-003 2.4e-004 1.00e+000 1.132838084e+001 1.133755476e+001 2.2e-009 1.84 62 3.4e-006 8.3e-003 2.2e-004 1.00e+000 1.132904138e+001 1.133729818e+001 2.0e-009 1.86 63 3.1e-006 8.2e-003 2.0e-004 1.00e+000 1.132963545e+001 1.133706675e+001 1.8e-009 1.89 64 2.8e-006 8.1e-003 1.8e-004 1.00e+000 1.133016983e+001 1.133685802e+001 1.6e-009 1.92 65 2.5e-006 8.1e-003 1.6e-004 1.00e+000 1.133065051e+001 1.133667003e+001 1.5e-009 1.95 66 2.2e-006 8.0e-003 1.4e-004 1.00e+000 1.133108294e+001 1.133650059e+001 1.3e-009 2.00 67 2.0e-006 7.9e-003 1.3e-004 1.00e+000 1.133147200e+001 1.133634794e+001 1.2e-009 2.05 68 1.8e-006 7.8e-003 1.2e-004 1.00e+000 1.133182204e+001 1.133621047e+001 1.1e-009 2.08 69 1.6e-006 7.8e-003 1.0e-004 1.00e+000 1.133213700e+001 1.133608661e+001 9.6e-010 2.11 70 1.5e-006 7.7e-003 9.4e-005 1.00e+000 1.133242042e+001 1.133597507e+001 8.6e-010 2.16 71 1.3e-006 7.7e-003 8.5e-005 1.00e+000 1.133267544e+001 1.133587465e+001 7.8e-010 2.19 72 1.2e-006 7.6e-003 7.7e-005 1.00e+000 1.133290493e+001 1.133578420e+001 7.0e-010 2.25 73 1.1e-006 7.6e-003 6.9e-005 1.00e+000 1.133311143e+001 1.133570286e+001 6.3e-010 2.33 74 9.6e-007 7.6e-003 6.2e-005 1.00e+000 1.133329728e+001 1.133562951e+001 5.7e-010 2.36 75 8.6e-007 7.5e-003 5.6e-005 9.99e-001 1.133346450e+001 1.133556361e+001 5.1e-010 2.39 76 7.8e-007 7.5e-003 5.0e-005 1.00e+000 1.133361499e+001 1.133550422e+001 4.6e-010 2.44 77 7.0e-007 7.5e-003 4.5e-005 1.00e+000 1.133375043e+001 1.133545076e+001 4.1e-010 2.47 78 6.3e-007 7.4e-003 4.1e-005 1.00e+000 1.133387232e+001 1.133540261e+001 3.7e-010 2.50 79 5.7e-007 7.4e-003 3.7e-005 1.00e+000 1.133398201e+001 1.133535928e+001 3.3e-010 2.52 80 5.1e-007 7.4e-003 3.3e-005 9.99e-001 1.133408071e+001 1.133532031e+001 3.0e-010 2.55 81 4.6e-007 7.4e-003 3.0e-005 1.00e+000 1.133416981e+001 1.133528496e+001 2.7e-010 2.56 82 4.1e-007 7.4e-003 2.7e-005 9.99e-001 1.133424972e+001 1.133525342e+001 2.4e-010 2.58 83 3.7e-007 7.3e-003 2.4e-005 1.00e+000 1.133432165e+001 1.133522498e+001 2.2e-010 2.59 84 3.3e-007 7.3e-003 2.2e-005 9.99e-001 1.133438637e+001 1.133519940e+001 2.0e-010 2.61 85 3.0e-007 7.3e-003 1.9e-005 1.00e+000 1.133444462e+001 1.133517635e+001 1.8e-010 2.63 86 2.7e-007 7.3e-003 1.8e-005 9.99e-001 1.133449704e+001 1.133515561e+001 1.6e-010 2.66 87 2.4e-007 7.3e-003 1.6e-005 9.96e-001 1.133454419e+001 1.133513704e+001 1.4e-010 2.67 88 2.2e-007 7.3e-003 1.4e-005 9.98e-001 1.133458664e+001 1.133512026e+001 1.3e-010 2.69 89 2.0e-007 7.2e-003 1.3e-005 9.99e-001 1.133462484e+001 1.133510514e+001 1.2e-010 2.70 90 1.8e-007 6.5e-003 1.1e-005 1.00e+000 1.133465933e+001 1.133509142e+001 1.1e-010 2.72 91 1.6e-007 5.9e-003 1.0e-005 9.97e-001 1.133469025e+001 1.133507921e+001 9.5e-011 2.77 92 1.4e-007 5.3e-003 9.3e-006 1.00e+000 1.133471834e+001 1.133506801e+001 8.5e-011 2.78 93 1.3e-007 4.7e-003 8.4e-006 9.98e-001 1.133474337e+001 1.133505811e+001 7.7e-011 2.80 94 1.2e-007 4.3e-003 7.5e-006 9.94e-001 1.133476588e+001 1.133504924e+001 6.9e-011 2.83 95 1.1e-007 3.8e-003 6.8e-006 9.96e-001 1.133478614e+001 1.133504122e+001 6.2e-011 2.84 96 9.5e-008 3.5e-003 6.1e-006 1.01e+000 1.133480496e+001 1.133503367e+001 5.6e-011 2.86 97 8.5e-008 3.1e-003 5.5e-006 9.98e-001 1.133482132e+001 1.133502719e+001 5.1e-011 2.92 98 7.7e-008 2.8e-003 4.9e-006 9.97e-001 1.133483604e+001 1.133502135e+001 4.5e-011 2.97 99 6.9e-008 2.5e-003 4.5e-006 1.01e+000 1.133484995e+001 1.133501574e+001 4.1e-011 2.98 100 6.2e-008 2.3e-003 4.0e-006 9.90e-001 1.133486180e+001 1.133501109e+001 3.7e-011 3.00 101 5.6e-008 2.0e-003 3.6e-006 1.01e+000 1.133487302e+001 1.133500655e+001 3.4e-011 3.06 102 5.0e-008 1.8e-003 3.2e-006 9.97e-001 1.133488257e+001 1.133500277e+001 3.0e-011 3.16 103 4.5e-008 1.7e-003 2.9e-006 9.96e-001 1.133489117e+001 1.133499937e+001 2.7e-011 3.20 104 4.1e-008 1.5e-003 2.6e-006 9.94e-001 1.133489890e+001 1.133499631e+001 2.4e-011 3.23 105 3.7e-008 1.3e-003 2.4e-006 1.01e+000 1.133490625e+001 1.133499334e+001 2.2e-011 3.25 106 3.3e-008 1.2e-003 2.1e-006 9.92e-001 1.133491248e+001 1.133499088e+001 2.0e-011 3.27 107 6.8e-009 2.3e-004 4.1e-007 9.79e-001 1.133495802e+001 1.133497316e+001 4.0e-012 3.30 108 5.7e-009 1.4e-005 2.5e-008 9.92e-001 1.133496811e+001 1.133496907e+001 3.6e-013 3.31 Interior-point optimizer terminated. Time: 3.33. Optimizer terminated. Time: 3.34 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1334968109e+001 nrm: 6e+001 Viol. con: 1e-007 var: 0e+000 Dual. obj: 1.1334969069e+001 nrm: 8e+002 Viol. con: 0e+000 var: 1e-004 * End solution on dual form. * Transforming to primal solution. Solving took 3.38 seconds. result packing took 68% of solve time solution checking took 1.9% of solve time Solving took 6 GP solves and 63.1 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 2418979.40198 force_pound * meter but the right hand side evaluated to 2375478.24153 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.3960212 force_pound but the right hand side evaluated to 32399.9999957 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116754 meter but the right hand side evaluated to 2.08122880926 meter (Allowable error: 0.1%, Actual error: 6%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1243567.22287 joule / kilogram but the right hand side evaluated to 1.56100826489 megajoule / kilogram (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 664756.154311 joule / kilogram but the right hand side evaluated to 0.667332864144 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.17%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4000174051 meter but the right hand side evaluated to 16.3233744558 meter (Allowable error: 0.1%, Actual error: 13%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.903786495908673 but the right hand side evaluated to 4.789010148260598 (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 10.01990980908264 but the right hand side evaluated to 4.789010127711618 (Allowable error: 0.1%, Actual error: 52%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.145070797055464 but the right hand side evaluated to 4.789010153262572 (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 18.3626165892 meter but the right hand side evaluated to 18.1380305221 meter (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3626165892 meter but the right hand side evaluated to 18.2424014007 meter (Allowable error: 0.1%, Actual error: 0.65%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.29608215026777174 but the right hand side evaluated to 0.18974961900220483 (Allowable error: 0.1%, Actual error: 2.2%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2330487685457756 but the right hand side evaluated to 0.1743535710036239 (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.563329486730277 but the right hand side evaluated to 4.730769525594513 (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 7.58315126252786 but the right hand side evaluated to 4.7579915865247715 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 77.448s OK Generating XML reports... Cloning into 'solar'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-mehyrp Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in c:\anaconda2\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-d9kvq2\wheels\d5\94\ac\b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12 Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/convexengineering/gassolar.git Cloning https://github.com/convexengineering/gassolar.git to c:\users\jenkins\appdata\local\temp\pip-req-build-zoacgv Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0) Building wheels for collected packages: gassolar Running setup.py bdist_wheel for gassolar: started Running setup.py bdist_wheel for gassolar: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-cvjgeg\wheels\fe\11\0a\2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e Successfully built gassolar grin 1.2.1 requires argparse>=1.1, which is not installed. Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\solar Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.1) Requirement already satisfied: gpkitmodels in c:\users\jenkins\workspace\gplibrary_pr_models\mosek (from solar==0.0.0.0) (0.0.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.11.0) Building wheels for collected packages: solar Running setup.py bdist_wheel for solar: started Running setup.py bdist_wheel for solar: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-xjmiom\wheels\f4\d5\5c\e37fedf74a44fbd5641b13d5622b97d759218ff594b631174a Successfully built solar grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: solar Found existing installation: solar 0.0.0.0 Not uninstalling solar at c:\anaconda2\lib\site-packages, outside environment c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit Can't uninstall 'solar'. No files were found to uninstall. Successfully installed solar-0.0.0.0 adding test for 'solar/solar.py' adding test for 'solar/sens_chart.py' adding test for 'solar/season.py' adding test for 'solar/npod_trade.py' Beginning signomial solve. Solving took 10 GP solves and 10.8 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1372749.6852 but bound is 600000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 79493.7398 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.1182603697 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825742821 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%) Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 1.63010984806 meter ** 2 / second ** 2 but the right hand side evaluated to 1.6301057309 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%) Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985253849 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983804228 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%) Beginning signomial solve. Solving took 10 GP solves and 12.4 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1372726.1620 but bound is 600000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 79493.7398 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.11826031494 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825737342 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%) Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 1.63010984225 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010572504 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%) Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985250604 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983800968 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%) Using solver 'mosek' Solving for 12129 variables. Solving took 4.7 seconds. Allowing negative dual variable(s) as small as -9.358773592755516e-11. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2985 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 720429.8377 but bound is 600000.0000 Using solver 'mosek' Solving for 12129 variables. Solving took 7.65 seconds. Allowing negative dual variable(s) as small as -1.3272762485459973e-10. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2521 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 791679.5168 but bound is 600000.0000 Using solver 'mosek' Solving for 12129 variables. Solving took 4.96 seconds. Allowing negative dual variable(s) as small as -3.4613257017271386e-10. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1920 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 883741.5106 but bound is 600000.0000 Using solver 'mosek' Solving for 6269 variables. Solving took 1.9 seconds. Allowing negative dual variable(s) as small as -9.851046470047377e-12. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.1637 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 933393.0329 but bound is 600000.0000 Using solver 'mosek' Solving for 12129 variables. Solving took 3.72 seconds. Allowing negative dual variable(s) as small as -5.366753759762477e-11. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2985 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 720429.8148 but bound is 600000.0000 Using solver 'mosek' Solving for 12129 variables. Solving took 3.32 seconds. Allowing negative dual variable(s) as small as -6.48037199118196e-11. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2521 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 791679.4767 but bound is 600000.0000 Using solver 'mosek' Solving for 12129 variables. Solving took 4.27 seconds. Allowing negative dual variable(s) as small as -1.3324381530281444e-10. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1920 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 883741.3777 but bound is 600000.0000 Using solver 'mosek' Solving for 6269 variables. Solving took 1.55 seconds. Allowing negative dual variable(s) as small as -2.742651997015427e-11. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.1637 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 933393.0440 but bound is 600000.0000 Beginning signomial solve. Solving took 10 GP solves and 6.75 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1372749.3142 but bound is 600000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 79493.7398 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.11826036081 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825741931 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%) Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 1.63010984333 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010572614 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%) Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985252308 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983802679 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%) Beginning signomial solve. Solving took 10 GP solves and 6.19 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1372724.5345 but bound is 600000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 79493.7398 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.11826031509 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825737361 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%) Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 1.63010984658 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010572942 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%) Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985252979 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983803361 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%) Using solver 'mosek' Solving for 702 variables. Solving took 0.344 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2555 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 773120.5089 but bound is 600000.0000 Beginning signomial solve. Solving took 9 GP solves and 5.19 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.0784 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1002038.1288 but bound is 600000.0000 Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,), could cause inaccurate result because it is below lower bound. Solution is 76735.5640 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(1... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.39813215563 meter ** 2 / second ** 2 but the right hand side evaluated to 1.39812954423 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00019%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.80391902523 meter ** 2 / second ** 2 but the right hand side evaluated to 0.803918043794 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%) Using solver 'mosek_cli' Solving for 702 variables. Solving took 0.516 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2555 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 773120.3442 but bound is 600000.0000 Beginning signomial solve. Solving took 9 GP solves and 7.05 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.0784 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1002041.5231 but bound is 600000.0000 Warning: Constraint [dQ_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,) [N... >= B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,)*G_M...] is not tight because the left hand side evaluated to 0.0359295931977 meter * newton but the right hand side evaluated to 0.0359295529168 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,), could cause inaccurate result because it is below lower bound. Solution is 76735.5213 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(1... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.39813162962 meter ** 2 / second ** 2 but the right hand side evaluated to 1.39812837496 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00023%) Running tests... ---------------------------------------------------------------------- ..C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun) ....EE ====================================================================== ERROR [9.672s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "solar.py", line 654, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 633, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 479, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkitmodels\GP\aircraft\wing\sparloading.py", line 70, in setup constraints.extend([ UnboundLocalError: local variable 'constraints' referenced before assignment ====================================================================== ERROR [11.782s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "solar.py", line 654, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 633, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 479, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkitmodels\GP\aircraft\wing\sparloading.py", line 70, in setup constraints.extend([ UnboundLocalError: local variable 'constraints' referenced before assignment ---------------------------------------------------------------------- Ran 8 tests in 603.895s FAILED (errors=2) Generating XML reports... Cloning into 'gplibrary'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.2) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-hpdjhr Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\anaconda2\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-2zpw2i\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gplibrary Requirement already satisfied: numpy>=1.12 in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1) Building wheels for collected packages: gpkitmodels Running setup.py bdist_wheel for gpkitmodels: started Running setup.py bdist_wheel for gpkitmodels: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-5blhlb\wheels\a3\80\70\6d80d6b876aaa160fc8dda3c238a4f64c571e65f335a009034 Successfully built gpkitmodels grin 1.2.1 requires argparse>=1.1, which is not installed. 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 Successfully installed gpkitmodels-0.0.0.0 adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py' adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py' adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py' adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py' adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py' Using solver 'mosek' Solving for 11 variables. Solving took 0.032 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.078 seconds. Using solver 'mosek' Solving for 9 variables. Solving took 0.031 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.031 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.015 seconds. Beginning signomial solve. Solving took 16 GP solves and 2.66 seconds. Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006556016 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%) Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544378397 meter * revolutions_per_minute but the right hand side evaluated to 103.04141117 meter / second (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585712831 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420572932397 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.003%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.314644960895 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629821892 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0048%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.168936399593 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931565056 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0639642271294 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631270164 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0017%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226356547314 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354017703 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%) Using solver 'mosek_cli' Solving for 9 variables. Solving took 0.094 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.094 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.109 seconds. Beginning signomial solve. Solving took 16 GP solves and 4.25 seconds. Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006568341 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%) Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544519398 meter * revolutions_per_minute but the right hand side evaluated to 103.041408191 meter / second (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [dQ_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [N*m]... >= B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement_...] is not tight because the left hand side evaluated to 74.5041627751 meter * newton but the right hand side evaluated to 74.5040725471 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%) Warning: Constraint [-B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement... >= dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [lbf]...] is not tight because the left hand side evaluated to 134.449579759 kilogram * meter / second ** 2 but the right hand side evaluated to 30.2255018449 force_pound (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585911845 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420572949095 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0031%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.314645033519 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629748579 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0049%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.16893640237 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931506563 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0639640648661 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639629971205 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0017%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226356673111 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226353930664 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0012%) Using solver 'mosek' Solving for 13 variables. Solving took 0.015 seconds. Beginning signomial solve. Solving took 11 GP solves and 1.41 seconds. Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742 Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619897.9847 but bound is 700000.0000 Using solver 'mosek_cli' Solving for 13 variables. Solving took 0.062 seconds. Beginning signomial solve. Solving took 11 GP solves and 2.7 seconds. Warning: Constraint [dQ_BladeElementProp/BladeElementPerf_(0,) [N*m]... >= B_BladeElementProp/BladeElementPerf_(0,)*G_BladeElementProp/BladeElementPerf_(0,)*Wa_BladeElementPro...] is not tight because the left hand side evaluated to 1.9475800463 meter * newton but the right hand side evaluated to 1.94757809539 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0001%) Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742 Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000 Warning: Constraint [-B_BladeElementProp/BladeElementPerf_(1,)*G_BladeElementProp/BladeElementPerf_(1,)*Wa_BladeElementPr... >= dT_BladeElementProp/BladeElementPerf_(1,) [lbf]...] is not tight because the left hand side evaluated to 52.7761427098 kilogram * meter / second ** 2 but the right hand side evaluated to 11.8645623096 force_pound (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [0.151*B_BladeElementProp/BladeElementPerf_(1,)**-2*F_BladeElementProp/BladeElementPerf_(1,)**2*R_Pro... >= 0.00633*B_BladeElementProp/BladeElementPerf_(1,)**2*G_BladeElementProp/BladeElementPerf_(1,)**2*r_Bl...] is not tight because the left hand side evaluated to 3.18328454561 meter ** 2 / second ** 2 but the right hand side evaluated to 3.18327922145 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00017%) Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3838 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9776 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3883 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9590 but bound is 1000000.0000 Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000 Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000 Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.6332 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.1579 but bound is 700000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000 Running tests... ---------------------------------------------------------------------- .......... ---------------------------------------------------------------------- Ran 10 tests in 18.344s OK Generating XML reports... Cloning into 'eVTOL'... adding test for 'aircraft_models.py' Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 2.094s OK Generating XML reports... USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'git+https://github.com/hoburg/turbofan.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>exit 0 Build step 'Console output (build log) parsing' changed build result to FAILURE [xUnit] [INFO] - Starting to record. [xUnit] [INFO] - Processing JUnit [xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek' for the testing framework 'JUnit'. [xUnit] [INFO] - Check 'Failed Tests' threshold. [xUnit] [INFO] - Check 'Skipped Tests' threshold. [xUnit] [INFO] - Setting the build status to FAILURE [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: FAILURE