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Started by upstream project "gplibrary_PR_Models" build number 93 originally caused by: GitHub pull request #169 of commit 35bdbde8eea99bed3162877ee1ca67e2b061a3e5, no merge conflicts. Building remotely on windows7x64 in workspace D:\jenkins\workspace\gplibrary_PR_Models\mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > git init D:\jenkins\workspace\gplibrary_PR_Models\mosek # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git --version # timeout=10 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 > git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10 > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master Merging Revision c93bb9e622d1f8dbc3f0371ffe91258327ee398f (refs/remotes/origin/pr/169/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='default', fastForwardMode='--ff'} > git rev-parse "origin/master^{commit}" # timeout=10 > git config core.sparsecheckout # timeout=10 > git checkout -f origin/master # timeout=3 > git merge --ff c93bb9e622d1f8dbc3f0371ffe91258327ee398f # timeout=10 > git rev-parse "HEAD^{commit}" # timeout=10 Seen branch in repository origin/1682literate Seen branch in repository origin/1682master Seen branch in repository origin/Breakdown Seen branch in repository origin/SPaircraft Seen branch in repository origin/aerosurf Seen branch in repository origin/atmosphere Seen branch in repository origin/boundj Seen branch in repository origin/bounds5 Seen branch in repository origin/boxspar Seen branch in repository origin/breguet_range Seen branch in repository origin/breguetsetup Seen branch in repository origin/climb Seen branch in repository origin/commercial_sizing Seen branch in repository origin/d8 Seen branch 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origin/prop_beta Seen branch in repository origin/qstr Seen branch in repository origin/quadrotor Seen branch in repository origin/revert-120-SPaircraft Seen branch in repository origin/rockets Seen branch in repository origin/sigeq_paper Seen branch in repository origin/simple_HT_sizing Seen branch in repository origin/simple_flight_profile Seen branch in repository origin/sparlS Seen branch in repository origin/standard_atmosphere Seen branch in repository origin/sutherland Seen branch in repository origin/troposphere Seen branch in repository origin/vectorizeplanform Seen branch in repository origin/wide_body Seen branch in repository origin/wvl Seen 207 remote branches > git show-ref --tags -d # timeout=10 Checking out Revision c93bb9e622d1f8dbc3f0371ffe91258327ee398f (origin/pr/169/merge, origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f c93bb9e622d1f8dbc3f0371ffe91258327ee398f # timeout=3 Commit message: "Merge d057fc54b0626b10dd6fdfee52a83746da2e48ee 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 [windows7x64] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [windows7x64] is in [[windows10x64, windows7x64]] Run condition [Execution node ] enabling perform for step [Execute Windows batch command] [mosek] $ cmd /c call C:\Users\jenkins\AppData\Local\Temp\jenkins4066809318834346518.bat D:\jenkins\workspace\gplibrary_PR_Models\mosek>echo C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM turn on the anaconda console D:\jenkins\workspace\gplibrary_PR_Models\mosek>call activate.bat || exit /b 666 (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM Create a virtualenv to install everything into (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>SET VENV=D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>virtualenv --system-site-packages D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit || exit /b 666 New python executable in D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts\python.exe Installing setuptools, pip, wheel...done. (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>call D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts\activate.bat || exit /b 666 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>set PATH=C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts;D:\Anaconda2;D:\Anaconda2\Library\mingw-w64\bin;D:\Anaconda2\Library\usr\bin;D:\Anaconda2\Library\bin;D:\Anaconda2\Scripts;D:\Anaconda2\bin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd (venv2_gpkit) (base) D:\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;D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts;D:\Anaconda2;D:\Anaconda2\Library\mingw-w64\bin;D:\Anaconda2\Library\usr\bin;D:\Anaconda2\Library\bin;D:\Anaconda2\Scripts;D:\Anaconda2\bin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd (venv2_gpkit) (base) D:\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) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM upgdade pip (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>python -m pip install --upgrade pip || exit /b 666 Requirement already up-to-date: pip in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (10.0.1) grin 1.2.1 requires argparse>=1.1, which is not installed. (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM Install coverage into the virtualenv to the coverage command blow uses the virtualenv python (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>pip install --upgrade coverage || exit /b 666 Requirement already up-to-date: coverage in d:\anaconda2\lib\site-packages (4.5.1) grin 1.2.1 requires argparse>=1.1, which is not installed. (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>SET GPKITBUILD=D:\jenkins\workspace\gplibrary_PR_Models\mosek\build_gpkit (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>if mosek == cvxopt ( pip install --upgrade cvxopt || exit /b 666 set GPKITSOLVERS=cvxopt ) (venv2_gpkit) (base) D:\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 ) Computer Platform : Windows/64-X86 Problem Name : Objective sense : min Type : LO (linear optimization problem) Constraints : 1 Cones : 0 Scalar variables : 5000 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator - tries : 0 time : 0.00 Eliminator - elim's : 0 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.17 ************************************ A license was checked out correctly. ************************************ (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>dir D:\jenkins\workspace\gplibrary_PR_Models\mosek\build_gpkit Volume in drive D is Home Volume Serial Number is EA39-7CA0 Directory of D:\jenkins\workspace\gplibrary_PR_Models\mosek File Not Found (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import scipy; print scipy.__version__" || exit /b 666 1.0.1 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import numpy; print numpy.__version__" || exit /b 666 1.14.3 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import pint; print pint.__version__" || exit /b 666 0.8.1 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM Install gpkit to run the documentation examples (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>git clone --depth 1 https://github.com/convexengineering/gpkit.git || exit /b 666 Cloning into 'gpkit'... 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(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>pip install -e D:\jenkins\workspace\gplibrary_PR_Models\mosek\gpkit || exit /b 666 Obtaining file:///D:/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit Requirement already satisfied: numpy>=1.12.1 in d:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.14.3) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (0.8.1) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.0.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.3.2) 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) D:\jenkins\workspace\gplibrary_PR_Models\mosek>pip install -e D:\jenkins\workspace\gplibrary_PR_Models\mosek || exit /b 666 Obtaining file:///D:/jenkins/workspace/gplibrary_PR_Models/mosek Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in d:\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) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM Show the settings file (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>type D:\jenkins\workspace\gplibrary_PR_Models\mosek\gpkit\gpkit\env\settings installed_solvers : mosek, mosek_cli mosek_bin_dir : C:\Program Files\Mosek\7\tools\platform\win64x86\bin (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>REM Limit number of threads that be can used (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>set MSK_IPAR_NUM_THREADS=2 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>set MKL_NUM_THREADS=2 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>set NUMEXPR_NUM_THREADS=2 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>set OPENBLAS_NUM_THREADS=2 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>set OMP_NUM_THREADS=2 (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)" Obtaining file:///D:/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 0.095 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.391 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.345 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 1.598s OK Generating XML reports... Cloning into 'gassolar'... 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Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in d:\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-xabljw Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\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-aeyubl\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gpfit Successfully installed gpfit-0.1 Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gassolar Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in d:\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-amugxp\wheels\08\33\b8\d36cec4e8239569444cd725d0dbfe83a0cfc534951775e5535 Successfully built gassolar grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gassolar Successfully installed gassolar-0.0.0.0 adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Couldn't auto-differentiate linked variable cosminus1_Mission/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 592 variables. Solving took 0.167 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 Couldn't auto-differentiate linked variable cosminus1_Mission.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 4 GP solves and 2.56 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 Couldn't auto-differentiate linked variable cosminus1_Mission/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 592 variables. Solving took 0.174 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 Couldn't auto-differentiate linked variable cosminus1_Mission.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 4 GP solves and 4.33 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 Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 1250 variables. Solving took 0.482 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1496 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 131552.1345 but bound is 150000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.14/GustL.14_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.13/GustL.13_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.19/GustL.19_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.20/GustL.20_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.16/GustL.16_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.15/GustL.15_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.12/GustL.12_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.17/GustL.17_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.18/GustL.18_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.11/GustL.11_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.21/GustL.21_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 4 GP solves and 8.36 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0581 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 134553.9086 but bound is 150000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek_cli' Solving for 1250 variables. Solving took 0.502 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 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.14/GustL.14_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.13/GustL.13_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.19/GustL.19_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.20/GustL.20_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.16/GustL.16_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.15/GustL.15_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.12/GustL.12_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.17/GustL.17_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.18/GustL.18_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.11/GustL.11_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.21/GustL.21_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 4 GP solves and 17 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... ---------------------------------------------------------------------- ..D:\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 74.520s OK Generating XML reports... Cloning into 'jho'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in d:\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-jfkjii Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\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-vnaks5\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 -5.02926693346506e-14. Allowing negative dual variable(s) as small as -7.520373213054654e-14. Allowing negative dual variable(s) as small as -1.513637305772253e-13. Allowing negative dual variable(s) as small as -1.5147041607099787e-13. Solving took 4 GP solves and 6.82 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.454447657426975e-14. Allowing negative dual variable(s) as small as -8.123363093304192e-14. Allowing negative dual variable(s) as small as -1.5141013443020768e-13. Allowing negative dual variable(s) as small as -1.4886139196312875e-13. Solving took 4 GP solves and 23.7 seconds. Allowing negative dual variable(s) as small as -5.176276074436714e-13. Allowing negative dual variable(s) as small as -1.4316863666818946e-12. Allowing negative dual variable(s) as small as -4.424516308887405e-13. Allowing negative dual variable(s) as small as -4.4336929960753224e-13. Allowing negative dual variable(s) as small as -1.2984123325121555e-12. Allowing negative dual variable(s) as small as -1.0922827312770389e-12. Allowing negative dual variable(s) as small as -1.090798350082689e-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 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 -2.423894268164525e-14. Allowing negative dual variable(s) as small as -5.696037278041664e-12. Allowing negative dual variable(s) as small as -2.0879025499564702e-11. Allowing negative dual variable(s) as small as -2.088085637732088e-11. Solving took 4 GP solves and 5.77 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 4.81 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.157107380027171e-13. Allowing negative dual variable(s) as small as -1.4291831607060601e-12. Allowing negative dual variable(s) as small as -4.448542229029684e-13. Allowing negative dual variable(s) as small as -4.433207273502049e-13. Allowing negative dual variable(s) as small as -1.2973334429303152e-12. Allowing negative dual variable(s) as small as -1.0899360840949113e-12. Allowing negative dual variable(s) as small as -1.0909163112790554e-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 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 -2.4951838326702056e-14. Allowing negative dual variable(s) as small as -5.696010269496168e-12. Allowing negative dual variable(s) as small as -2.0879057432918572e-11. Allowing negative dual variable(s) as small as -2.0880778863403582e-11. Solving took 4 GP solves and 2.26 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 6.71 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 131.532s OK Generating XML reports... Cloning into 'turbofan'... Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\turbofan Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in d:\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-bquvsr\wheels\e5\cb\a8\3b11c975e79b3f632de8c1b88ce438a834a6b07b3850d6b107 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 24184.7528315 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%) Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485055 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 4.165s OK Generating XML reports... Cloning into 'SPaircraft'... 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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-i1nxio Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in d:\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-hoib6n\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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 1015 Eliminator terminated. Eliminator started. Total number of eliminations : 1025 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1025 Lin. dep. - tries : 1 time : 0.02 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 : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 826 Optimizer - Cones : 0 Optimizer - Scalar variables : 3575 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 : 1.67e+004 after factor : 1.69e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.290114216e+005 2.000000000e+000 1.0e+000 0.11 1 1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.268199332e+005 3.700570996e+000 4.8e-001 0.16 2 3.9e+002 5.0e+002 2.2e+004 -9.36e-001 -1.196731173e+005 1.153832762e+001 1.7e-001 0.19 3 2.8e+002 3.7e+002 1.6e+004 -8.23e-001 -1.157725499e+005 8.911193657e+001 1.2e-001 0.23 4 2.8e+002 3.6e+002 1.6e+004 -7.55e-001 -1.127836302e+005 2.530618096e+003 1.2e-001 0.27 5 6.9e+001 9.0e+001 3.9e+003 -7.46e-001 -7.044561375e+004 1.168298555e+004 3.1e-002 0.31 6 3.1e+001 4.1e+001 1.8e+003 -1.39e-001 -4.096532654e+004 1.098732371e+004 1.4e-002 0.34 7 1.6e+001 2.1e+001 9.1e+002 3.72e-001 -2.384884033e+004 6.701248905e+003 7.2e-003 0.39 8 7.3e+000 9.5e+000 4.1e+002 6.70e-001 -1.130515668e+004 3.761163374e+003 3.3e-003 0.42 9 3.4e+000 4.4e+000 1.9e+002 8.75e-001 -5.068498667e+003 2.154890886e+003 1.5e-003 0.45 10 1.7e+000 2.2e+000 9.8e+001 9.56e-001 -2.274239213e+003 1.449630149e+003 7.8e-004 0.50 11 6.5e-001 8.4e-001 3.7e+001 9.85e-001 -6.386409604e+002 7.708877882e+002 2.9e-004 0.53 12 5.5e-001 7.6e-001 3.2e+001 9.80e-001 -4.977186201e+002 7.157125316e+002 2.5e-004 0.58 13 3.9e-001 9.4e-001 2.2e+001 9.74e-001 -2.511527669e+002 6.146396419e+002 1.8e-004 0.61 14 2.1e-001 6.0e-001 1.2e+001 9.86e-001 2.118551311e+001 4.971611734e+002 9.8e-005 0.66 15 6.4e-002 2.4e-001 3.8e+000 1.00e+000 2.547904550e+002 4.008091633e+002 3.1e-005 0.69 16 2.0e-002 1.4e-001 1.2e+000 1.00e+000 3.243515273e+002 3.710547149e+002 9.9e-006 0.73 17 4.6e-003 1.5e-001 2.8e-001 1.00e+000 3.496092054e+002 3.605442939e+002 2.4e-006 0.78 18 2.7e-003 1.2e-001 1.7e-001 1.00e+000 3.526527396e+002 3.591730387e+002 1.4e-006 0.83 19 6.5e-004 1.3e-001 4.1e-002 9.94e-001 3.562031755e+002 3.577903301e+002 3.5e-007 0.86 20 2.4e-004 9.9e-002 1.5e-002 9.98e-001 3.569203947e+002 3.575142357e+002 1.3e-007 0.91 21 1.2e-004 7.9e-002 7.5e-003 1.00e+000 3.571413806e+002 3.574309325e+002 6.3e-008 0.94 22 1.1e-004 7.2e-002 6.8e-003 1.00e+000 3.571621286e+002 3.574227098e+002 5.7e-008 0.97 23 9.5e-005 6.6e-002 6.1e-003 1.00e+000 3.571807621e+002 3.574152867e+002 5.1e-008 1.00 24 8.6e-005 6.0e-002 5.5e-003 1.00e+000 3.571975379e+002 3.574086184e+002 4.6e-008 1.04 25 7.7e-005 5.4e-002 4.9e-003 1.00e+000 3.572126371e+002 3.574026145e+002 4.2e-008 1.08 26 7.0e-005 4.9e-002 4.4e-003 1.00e+000 3.572262247e+002 3.573972063e+002 3.7e-008 1.11 27 6.3e-005 4.5e-002 4.0e-003 1.00e+000 3.572384517e+002 3.573923352e+002 3.4e-008 1.15 28 5.6e-005 4.1e-002 3.6e-003 1.00e+000 3.572494550e+002 3.573879494e+002 3.0e-008 1.20 29 5.1e-005 3.8e-002 3.2e-003 1.00e+000 3.572593579e+002 3.573840020e+002 2.7e-008 1.23 30 4.6e-005 3.5e-002 2.9e-003 1.00e+000 3.572682711e+002 3.573804497e+002 2.5e-008 1.26 31 4.1e-005 3.2e-002 2.6e-003 1.00e+000 3.572762938e+002 3.573772537e+002 2.2e-008 1.31 32 3.7e-005 2.9e-002 2.4e-003 1.00e+000 3.572835153e+002 3.573743784e+002 2.0e-008 1.34 33 3.3e-005 2.7e-002 2.1e-003 1.00e+000 3.572900158e+002 3.573717920e+002 1.8e-008 1.37 34 3.0e-005 2.5e-002 1.9e-003 1.00e+000 3.572958675e+002 3.573694654e+002 1.6e-008 1.40 35 2.7e-005 2.3e-002 1.7e-003 1.00e+000 3.573011351e+002 3.573673728e+002 1.4e-008 1.45 36 2.4e-005 2.2e-002 1.5e-003 1.00e+000 3.573058769e+002 3.573654905e+002 1.3e-008 1.48 37 2.2e-005 2.0e-002 1.4e-003 1.00e+000 3.573101455e+002 3.573637976e+002 1.2e-008 1.51 38 2.0e-005 1.9e-002 1.3e-003 1.00e+000 3.573139881e+002 3.573622748e+002 1.1e-008 1.56 39 1.8e-005 1.8e-002 1.1e-003 1.00e+000 3.573174472e+002 3.573609051e+002 9.5e-009 1.59 40 1.6e-005 1.7e-002 1.0e-003 1.00e+000 3.573205611e+002 3.573596730e+002 8.6e-009 1.62 41 1.4e-005 1.6e-002 9.1e-004 1.00e+000 3.573233641e+002 3.573585648e+002 7.7e-009 1.67 42 1.3e-005 1.5e-002 8.2e-004 1.00e+000 3.573258873e+002 3.573575679e+002 6.9e-009 1.70 43 1.2e-005 1.4e-002 7.4e-004 1.00e+000 3.573281586e+002 3.573566712e+002 6.2e-009 1.73 44 1.0e-005 1.3e-002 6.7e-004 1.00e+000 3.573302032e+002 3.573558645e+002 5.6e-009 1.78 45 9.4e-006 1.3e-002 6.0e-004 1.00e+000 3.573320436e+002 3.573551388e+002 5.1e-009 1.81 46 8.5e-006 1.2e-002 5.4e-004 1.00e+000 3.573337002e+002 3.573544859e+002 4.5e-009 1.84 47 7.6e-006 1.2e-002 4.9e-004 1.00e+000 3.573351914e+002 3.573538985e+002 4.1e-009 1.89 48 6.9e-006 1.1e-002 4.4e-004 1.00e+000 3.573365336e+002 3.573533701e+002 3.7e-009 1.92 49 6.2e-006 1.1e-002 3.9e-004 1.00e+000 3.573377417e+002 3.573528946e+002 3.3e-009 1.95 50 5.6e-006 1.0e-002 3.5e-004 1.00e+000 3.573388292e+002 3.573524668e+002 3.0e-009 2.00 51 5.0e-006 1.0e-002 3.2e-004 1.00e+000 3.573398079e+002 3.573520818e+002 2.7e-009 2.03 52 4.5e-006 9.8e-003 2.9e-004 1.00e+000 3.573406889e+002 3.573517354e+002 2.4e-009 2.06 53 4.0e-006 9.5e-003 2.6e-004 1.00e+000 3.573414818e+002 3.573514236e+002 2.2e-009 2.09 54 3.6e-006 9.3e-003 2.3e-004 1.00e+000 3.573421954e+002 3.573511431e+002 2.0e-009 2.12 55 3.3e-006 9.1e-003 2.1e-004 1.00e+000 3.573428376e+002 3.573508906e+002 1.8e-009 2.17 56 3.0e-006 8.9e-003 1.9e-004 1.00e+000 3.573434156e+002 3.573506633e+002 1.6e-009 2.20 57 2.7e-006 8.7e-003 1.7e-004 1.00e+000 3.573439358e+002 3.573504587e+002 1.4e-009 2.23 58 2.4e-006 8.6e-003 1.5e-004 1.00e+000 3.573444040e+002 3.573502746e+002 1.3e-009 2.26 59 2.2e-006 8.5e-003 1.4e-004 1.00e+000 3.573448253e+002 3.573501089e+002 1.2e-009 2.29 60 1.9e-006 8.3e-003 1.2e-004 1.00e+000 3.573452045e+002 3.573499597e+002 1.0e-009 2.32 61 1.7e-006 8.2e-003 1.1e-004 1.00e+000 3.573455458e+002 3.573498255e+002 9.4e-010 2.37 62 1.6e-006 8.1e-003 1.0e-004 1.00e+000 3.573458529e+002 3.573497046e+002 8.4e-010 2.40 63 1.4e-006 8.1e-003 9.0e-005 1.00e+000 3.573461293e+002 3.573495958e+002 7.6e-010 2.43 64 1.3e-006 8.0e-003 8.1e-005 1.00e+000 3.573463780e+002 3.573494979e+002 6.8e-010 2.46 65 1.1e-006 7.9e-003 7.3e-005 1.00e+000 3.573466018e+002 3.573494098e+002 6.1e-010 2.51 66 1.0e-006 7.8e-003 6.6e-005 1.00e+000 3.573468033e+002 3.573493305e+002 5.5e-010 2.54 67 9.3e-007 7.8e-003 5.9e-005 1.00e+000 3.573469846e+002 3.573492590e+002 5.0e-010 2.59 68 8.3e-007 7.7e-003 5.3e-005 1.00e+000 3.573471477e+002 3.573491948e+002 4.5e-010 2.62 69 7.5e-007 7.7e-003 4.8e-005 1.00e+000 3.573472945e+002 3.573491368e+002 4.0e-010 2.65 70 6.8e-007 7.6e-003 4.3e-005 1.00e+000 3.573474267e+002 3.573490848e+002 3.6e-010 2.68 71 6.1e-007 7.6e-003 3.9e-005 1.00e+000 3.573475456e+002 3.573490379e+002 3.3e-010 2.73 72 5.5e-007 7.6e-003 3.5e-005 1.00e+000 3.573476526e+002 3.573489956e+002 2.9e-010 2.76 73 4.9e-007 7.5e-003 3.1e-005 1.00e+000 3.573477489e+002 3.573489576e+002 2.6e-010 2.79 74 4.4e-007 7.5e-003 2.8e-005 1.00e+000 3.573478355e+002 3.573489234e+002 2.4e-010 2.84 75 4.0e-007 7.5e-003 2.5e-005 1.00e+000 3.573479135e+002 3.573488925e+002 2.1e-010 2.87 76 3.6e-007 7.5e-003 2.3e-005 1.00e+000 3.573479836e+002 3.573488648e+002 1.9e-010 2.90 77 3.2e-007 7.4e-003 2.1e-005 1.00e+000 3.573480468e+002 3.573488398e+002 1.7e-010 2.95 78 2.9e-007 7.4e-003 1.9e-005 1.00e+000 3.573481036e+002 3.573488173e+002 1.6e-010 2.98 79 2.6e-007 7.4e-003 1.7e-005 1.00e+000 3.573481547e+002 3.573487970e+002 1.4e-010 3.03 80 2.4e-007 7.4e-003 1.5e-005 1.00e+000 3.573482007e+002 3.573487788e+002 1.3e-010 3.06 81 2.1e-007 7.4e-003 1.3e-005 9.99e-001 3.573482421e+002 3.573487624e+002 1.1e-010 3.09 82 1.9e-007 7.3e-003 1.2e-005 1.00e+000 3.573482793e+002 3.573487476e+002 1.0e-010 3.13 83 1.7e-007 7.3e-003 1.1e-005 9.98e-001 3.573483129e+002 3.573487343e+002 9.2e-011 3.17 84 1.5e-007 7.3e-003 9.8e-006 9.97e-001 3.573483430e+002 3.573487224e+002 8.3e-011 3.20 85 1.4e-007 7.3e-003 8.9e-006 9.98e-001 3.573483701e+002 3.573487116e+002 7.5e-011 3.25 86 1.3e-007 7.3e-003 8.0e-006 1.00e+000 3.573483946e+002 3.573487019e+002 6.7e-011 3.28 87 1.1e-007 7.3e-003 7.2e-006 9.99e-001 3.573484166e+002 3.573486932e+002 6.1e-011 3.31 88 1.0e-007 6.5e-003 6.5e-006 1.00e+000 3.573484364e+002 3.573486853e+002 5.4e-011 3.34 89 9.1e-008 5.9e-003 5.8e-006 1.00e+000 3.573484542e+002 3.573486782e+002 4.9e-011 3.38 90 8.2e-008 5.3e-003 5.2e-006 9.95e-001 3.573484702e+002 3.573486718e+002 4.4e-011 3.42 91 7.4e-008 4.8e-003 4.7e-006 9.99e-001 3.573484847e+002 3.573486661e+002 4.0e-011 3.45 92 6.6e-008 4.3e-003 4.2e-006 1.01e+000 3.573484979e+002 3.573486608e+002 3.6e-011 3.49 93 6.0e-008 3.9e-003 3.8e-006 1.00e+000 3.573485096e+002 3.573486561e+002 3.2e-011 3.52 94 5.4e-008 3.5e-003 3.4e-006 1.00e+000 3.573485203e+002 3.573486518e+002 2.9e-011 3.56 95 1.1e-008 6.7e-004 6.6e-007 9.97e-001 3.573485962e+002 3.573486217e+002 5.7e-012 3.60 96 9.5e-009 6.0e-004 6.0e-007 9.64e-001 3.573485980e+002 3.573486210e+002 5.1e-012 3.63 97 8.5e-009 5.4e-004 5.4e-007 9.88e-001 3.573485997e+002 3.573486203e+002 4.6e-012 3.67 98 7.7e-009 4.9e-004 4.8e-007 9.97e-001 3.573486011e+002 3.573486198e+002 4.1e-012 3.70 99 6.9e-009 4.4e-004 4.4e-007 1.10e+000 3.573486031e+002 3.573486189e+002 3.9e-012 3.79 100 6.2e-009 4.0e-004 3.9e-007 9.82e-001 3.573486042e+002 3.573486184e+002 3.5e-012 3.82 101 5.6e-009 3.6e-004 3.5e-007 9.92e-001 3.573486052e+002 3.573486180e+002 3.2e-012 3.87 102 5.0e-009 3.2e-004 3.2e-007 1.06e+000 3.573486064e+002 3.573486175e+002 2.9e-012 3.90 103 4.5e-009 2.9e-004 2.9e-007 1.00e+000 3.573486072e+002 3.573486172e+002 2.6e-012 3.93 104 4.1e-009 2.6e-004 2.6e-007 9.93e-001 3.573486080e+002 3.573486169e+002 2.4e-012 3.96 105 3.7e-009 2.3e-004 2.3e-007 9.98e-001 3.573486086e+002 3.573486167e+002 2.1e-012 3.99 106 3.3e-009 2.1e-004 2.1e-007 9.92e-001 3.573486092e+002 3.573486164e+002 1.9e-012 4.03 107 3.0e-009 1.9e-004 1.9e-007 9.93e-001 3.573486097e+002 3.573486162e+002 1.7e-012 4.06 108 2.7e-009 1.7e-004 1.7e-007 1.01e+000 3.573486102e+002 3.573486160e+002 1.6e-012 4.10 109 2.4e-009 1.5e-004 1.5e-007 9.88e-001 3.573486106e+002 3.573486159e+002 1.4e-012 4.13 110 2.2e-009 1.4e-004 1.4e-007 1.01e+000 3.573486110e+002 3.573486157e+002 1.3e-012 4.18 111 1.9e-009 1.2e-004 1.2e-007 1.00e+000 3.573486113e+002 3.573486156e+002 1.2e-012 4.21 112 1.8e-009 1.1e-004 1.1e-007 9.79e-001 3.573486117e+002 3.573486155e+002 1.0e-012 4.24 113 1.6e-009 1.0e-004 1.0e-007 1.00e+000 3.573486119e+002 3.573486154e+002 9.4e-013 4.27 Interior-point optimizer terminated. Time: 4.29. Optimizer terminated. Time: 4.31 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 3.5734861193e+002 Viol. con: 2e-008 var: 0e+000 Dual. obj: 3.5734861535e+002 Viol. con: 0e+000 var: 7e-004 * End solution on dual form. * Transforming to primal solution. Solving took 4.32 seconds. result packing took 7.1% of solve time solution checking took 2.7% of solve time 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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 1012 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 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 : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 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 : 1.67e+004 after factor : 1.72e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.289216044e+005 2.000000000e+000 1.0e+000 0.11 1 1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.266775833e+005 3.803741941e+000 4.7e-001 0.12 2 4.4e+002 5.7e+002 2.5e+004 -9.35e-001 -1.207998731e+005 1.084180436e+001 1.9e-001 0.16 3 2.9e+002 3.7e+002 1.6e+004 -8.43e-001 -1.159533006e+005 6.141738706e+001 1.3e-001 0.20 4 2.9e+002 3.7e+002 1.6e+004 -7.60e-001 -1.137614550e+005 1.946615988e+003 1.3e-001 0.23 5 8.6e+001 1.1e+002 4.9e+003 -7.56e-001 -7.873791105e+004 1.029432261e+004 3.8e-002 0.28 6 2.8e+001 3.7e+001 1.6e+003 -2.75e-001 -3.706476018e+004 1.220641362e+004 1.3e-002 0.31 7 1.4e+001 1.8e+001 7.7e+002 4.35e-001 -2.030567980e+004 6.163510231e+003 6.0e-003 0.34 8 7.6e+000 9.8e+000 4.3e+002 7.35e-001 -1.180252616e+004 3.699008339e+003 3.4e-003 0.37 9 2.9e+000 3.7e+000 1.6e+002 8.69e-001 -4.542574263e+003 1.611196614e+003 1.3e-003 0.42 10 1.4e+000 1.8e+000 7.9e+001 9.69e-001 -2.009195307e+003 9.676511769e+002 6.2e-004 0.45 11 9.6e-001 1.2e+000 5.5e+001 9.89e-001 -1.381391303e+003 6.944429121e+002 4.3e-004 0.48 12 8.4e-001 1.1e+000 4.8e+001 9.74e-001 -1.220057855e+003 6.089998967e+002 3.8e-004 0.51 13 3.5e-001 4.5e-001 2.0e+001 9.84e-001 -4.954113131e+002 2.767217263e+002 1.6e-004 0.55 14 1.9e-001 2.6e-001 1.1e+001 1.01e+000 -2.547990479e+002 1.739608308e+002 8.8e-005 0.58 15 7.8e-002 1.3e-001 4.5e+000 9.99e-001 -8.253878908e+001 9.184542776e+001 3.6e-005 0.61 16 2.3e-002 1.1e-001 1.4e+000 1.00e+000 -6.410176310e-001 5.294698129e+001 1.1e-005 0.64 17 1.5e-002 8.3e-002 8.7e-001 1.00e+000 1.306854197e+001 4.649502052e+001 7.1e-006 0.67 18 2.8e-003 1.4e-001 1.7e-001 1.00e+000 3.161975125e+001 3.829726235e+001 1.4e-006 0.70 19 1.4e-003 9.8e-002 8.9e-002 1.00e+000 3.387244786e+001 3.730607056e+001 7.5e-007 0.75 20 4.6e-004 1.0e-001 2.8e-002 1.00e+000 3.549091350e+001 3.658198742e+001 2.4e-007 0.78 21 2.1e-004 7.9e-002 1.3e-002 1.00e+000 3.589091670e+001 3.640150496e+001 1.1e-007 0.81 22 1.9e-004 7.1e-002 1.2e-002 1.00e+000 3.592728077e+001 3.638680158e+001 1.0e-007 0.84 23 1.7e-004 6.5e-002 1.1e-002 1.00e+000 3.595898848e+001 3.637252730e+001 9.1e-008 0.89 24 1.6e-004 5.9e-002 9.7e-003 1.00e+000 3.598755004e+001 3.635971270e+001 8.1e-008 0.92 25 1.4e-004 5.4e-002 8.7e-003 1.00e+000 3.601322434e+001 3.634815202e+001 7.3e-008 0.95 26 1.3e-004 4.9e-002 7.9e-003 1.00e+000 3.603631297e+001 3.633773248e+001 6.6e-008 1.00 27 1.1e-004 4.5e-002 7.1e-003 1.00e+000 3.605707767e+001 3.632834261e+001 5.9e-008 1.04 28 1.0e-004 4.1e-002 6.4e-003 1.00e+000 3.607575382e+001 3.631988191e+001 5.3e-008 1.08 29 9.2e-005 3.8e-002 5.7e-003 1.00e+000 3.609255266e+001 3.631225946e+001 4.8e-008 1.11 30 8.3e-005 3.5e-002 5.2e-003 1.00e+000 3.610766383e+001 3.630539306e+001 4.3e-008 1.14 31 7.4e-005 3.2e-002 4.6e-003 1.00e+000 3.612125765e+001 3.629920834e+001 3.9e-008 1.17 32 6.7e-005 3.0e-002 4.2e-003 1.00e+000 3.613348708e+001 3.629363815e+001 3.5e-008 1.20 33 6.0e-005 2.7e-002 3.8e-003 1.00e+000 3.614448953e+001 3.628862180e+001 3.2e-008 1.23 34 5.4e-005 2.5e-002 3.4e-003 1.00e+000 3.615438848e+001 3.628410454e+001 2.8e-008 1.26 35 4.9e-005 2.3e-002 3.1e-003 1.00e+000 3.616329491e+001 3.628003698e+001 2.6e-008 1.29 36 4.4e-005 2.2e-002 2.7e-003 1.00e+000 3.617130858e+001 3.627637453e+001 2.3e-008 1.33 37 3.9e-005 2.0e-002 2.5e-003 1.00e+000 3.617851919e+001 3.627307700e+001 2.1e-008 1.36 38 3.6e-005 1.9e-002 2.2e-003 1.00e+000 3.618500737e+001 3.627010817e+001 1.9e-008 1.37 39 3.2e-005 1.8e-002 2.0e-003 1.00e+000 3.619084563e+001 3.626743538e+001 1.7e-008 1.40 40 2.9e-005 1.7e-002 1.8e-003 1.00e+000 3.619609919e+001 3.626502920e+001 1.5e-008 1.42 41 2.6e-005 1.6e-002 1.6e-003 1.00e+000 3.620082670e+001 3.626286310e+001 1.4e-008 1.45 42 2.3e-005 1.5e-002 1.5e-003 1.00e+000 3.620508089e+001 3.626091317e+001 1.2e-008 1.47 43 2.1e-005 1.4e-002 1.3e-003 1.00e+000 3.620890920e+001 3.625915789e+001 1.1e-008 1.48 44 1.9e-005 1.3e-002 1.2e-003 1.00e+000 3.621235432e+001 3.625757784e+001 9.9e-009 1.53 45 1.7e-005 1.3e-002 1.1e-003 1.00e+000 3.621545463e+001 3.625615556e+001 8.9e-009 1.54 46 1.5e-005 1.2e-002 9.6e-004 1.00e+000 3.621824465e+001 3.625487531e+001 8.0e-009 1.58 47 1.4e-005 1.2e-002 8.6e-004 1.00e+000 3.622075545e+001 3.625372292e+001 7.2e-009 1.61 48 1.2e-005 1.1e-002 7.8e-004 1.00e+000 3.622301498e+001 3.625268562e+001 6.5e-009 1.64 49 1.1e-005 1.1e-002 7.0e-004 1.00e+000 3.622504841e+001 3.625175190e+001 5.9e-009 1.67 50 1.0e-005 1.1e-002 6.3e-004 1.00e+000 3.622687834e+001 3.625091144e+001 5.3e-009 1.68 51 9.0e-006 1.0e-002 5.7e-004 1.00e+000 3.622852515e+001 3.625015491e+001 4.7e-009 1.72 52 8.1e-006 9.9e-003 5.1e-004 1.00e+000 3.623000717e+001 3.624947392e+001 4.3e-009 1.75 53 7.3e-006 9.6e-003 4.6e-004 1.00e+000 3.623134088e+001 3.624886094e+001 3.8e-009 1.79 54 6.6e-006 9.4e-003 4.1e-004 1.00e+000 3.623254111e+001 3.624830917e+001 3.5e-009 1.84 55 5.9e-006 9.2e-003 3.7e-004 1.00e+000 3.623362124e+001 3.624781248e+001 3.1e-009 1.87 56 5.3e-006 9.0e-003 3.3e-004 1.00e+000 3.623459328e+001 3.624736539e+001 2.8e-009 1.92 57 4.8e-006 8.8e-003 3.0e-004 1.00e+000 3.623546803e+001 3.624696294e+001 2.5e-009 1.95 58 4.3e-006 8.6e-003 2.7e-004 1.00e+000 3.623625525e+001 3.624660066e+001 2.3e-009 1.98 59 3.9e-006 8.5e-003 2.4e-004 1.00e+000 3.623696368e+001 3.624627455e+001 2.0e-009 2.01 60 3.5e-006 8.4e-003 2.2e-004 1.00e+000 3.623760121e+001 3.624598100e+001 1.8e-009 2.06 61 3.1e-006 8.3e-003 2.0e-004 1.00e+000 3.623817494e+001 3.624571676e+001 1.7e-009 2.09 62 2.8e-006 8.1e-003 1.8e-004 1.00e+000 3.623869125e+001 3.624547891e+001 1.5e-009 2.14 63 2.6e-006 8.1e-003 1.6e-004 1.00e+000 3.623915590e+001 3.624526477e+001 1.3e-009 2.17 64 2.3e-006 8.0e-003 1.4e-004 1.00e+000 3.623957404e+001 3.624507204e+001 1.2e-009 2.21 65 2.1e-006 7.9e-003 1.3e-004 1.00e+000 3.623995034e+001 3.624489852e+001 1.1e-009 2.26 66 1.9e-006 7.8e-003 1.2e-004 1.00e+000 3.624028897e+001 3.624474235e+001 9.8e-010 2.29 67 1.7e-006 7.7e-003 1.0e-004 1.00e+000 3.624059372e+001 3.624460177e+001 8.8e-010 2.32 68 1.5e-006 7.7e-003 9.4e-005 1.00e+000 3.624086797e+001 3.624447522e+001 7.9e-010 2.36 69 1.4e-006 7.6e-003 8.5e-005 1.00e+000 3.624111477e+001 3.624436131e+001 7.1e-010 2.40 70 1.2e-006 7.6e-003 7.6e-005 1.00e+000 3.624133688e+001 3.624425877e+001 6.4e-010 2.43 71 1.1e-006 7.5e-003 6.9e-005 1.00e+000 3.624153676e+001 3.624416645e+001 5.8e-010 2.46 72 9.9e-007 7.5e-003 6.2e-005 1.00e+000 3.624171665e+001 3.624408336e+001 5.2e-010 2.51 73 8.9e-007 7.5e-003 5.6e-005 1.00e+000 3.624187852e+001 3.624400857e+001 4.7e-010 2.54 74 8.0e-007 7.4e-003 5.0e-005 1.00e+000 3.624202420e+001 3.624394126e+001 4.2e-010 2.57 75 7.2e-007 7.4e-003 4.5e-005 1.00e+000 3.624215530e+001 3.624388067e+001 3.8e-010 2.62 76 6.5e-007 7.4e-003 4.1e-005 1.00e+000 3.624227329e+001 3.624382612e+001 3.4e-010 2.65 77 5.8e-007 7.3e-003 3.7e-005 1.00e+000 3.624237947e+001 3.624377702e+001 3.1e-010 2.68 78 5.3e-007 7.3e-003 3.3e-005 1.00e+000 3.624247502e+001 3.624373282e+001 2.8e-010 2.73 79 4.7e-007 7.3e-003 3.0e-005 1.00e+000 3.624256102e+001 3.624369303e+001 2.5e-010 2.76 80 4.3e-007 7.3e-003 2.7e-005 1.00e+000 3.624263841e+001 3.624365722e+001 2.2e-010 2.79 81 3.8e-007 7.2e-003 2.4e-005 1.00e+000 3.624270806e+001 3.624362498e+001 2.0e-010 2.82 82 3.4e-007 7.2e-003 2.2e-005 1.00e+000 3.624277073e+001 3.624359597e+001 1.8e-010 2.87 83 3.1e-007 7.2e-003 1.9e-005 1.00e+000 3.624282714e+001 3.624356985e+001 1.6e-010 2.90 84 2.8e-007 7.2e-003 1.7e-005 9.99e-001 3.624287790e+001 3.624354636e+001 1.5e-010 2.93 85 2.5e-007 7.2e-003 1.6e-005 1.00e+000 3.624292359e+001 3.624352519e+001 1.3e-010 2.96 86 2.3e-007 7.2e-003 1.4e-005 1.00e+000 3.624296470e+001 3.624350615e+001 1.2e-010 3.00 87 2.0e-007 7.2e-003 1.3e-005 1.00e+000 3.624300171e+001 3.624348899e+001 1.1e-010 3.03 88 1.8e-007 7.1e-003 1.1e-005 1.00e+000 3.624303500e+001 3.624347356e+001 9.6e-011 3.06 89 1.6e-007 7.1e-003 1.0e-005 1.00e+000 3.624306497e+001 3.624345967e+001 8.7e-011 3.10 90 1.5e-007 7.1e-003 9.3e-006 1.00e+000 3.624309196e+001 3.624344715e+001 7.8e-011 3.13 91 1.3e-007 7.1e-003 8.4e-006 1.00e+000 3.624311623e+001 3.624343590e+001 7.0e-011 3.17 92 1.2e-007 7.1e-003 7.5e-006 1.00e+000 3.624313807e+001 3.624342577e+001 6.3e-011 3.20 93 1.1e-007 7.1e-003 6.8e-006 9.99e-001 3.624315773e+001 3.624341666e+001 5.7e-011 3.23 94 9.7e-008 7.1e-003 6.1e-006 9.99e-001 3.624317541e+001 3.624340847e+001 5.1e-011 3.28 95 8.8e-008 7.1e-003 5.5e-006 9.99e-001 3.624319133e+001 3.624340109e+001 4.6e-011 3.31 96 7.9e-008 7.1e-003 4.9e-006 9.99e-001 3.624320566e+001 3.624339445e+001 4.1e-011 3.34 97 7.1e-008 7.1e-003 4.4e-006 1.00e+000 3.624321856e+001 3.624338846e+001 3.7e-011 3.38 98 6.4e-008 7.0e-003 4.0e-006 1.00e+000 3.624323017e+001 3.624338307e+001 3.4e-011 3.42 99 5.7e-008 6.3e-003 3.6e-006 1.00e+000 3.624324069e+001 3.624337817e+001 3.0e-011 3.45 100 5.2e-008 5.7e-003 3.2e-006 1.00e+000 3.624325008e+001 3.624337382e+001 2.7e-011 3.48 101 4.7e-008 5.1e-003 2.9e-006 9.99e-001 3.624325853e+001 3.624336990e+001 2.4e-011 3.51 102 4.2e-008 4.6e-003 2.6e-006 1.00e+000 3.624326614e+001 3.624336637e+001 2.2e-011 3.56 103 3.8e-008 4.2e-003 2.4e-006 9.97e-001 3.624327298e+001 3.624336320e+001 2.0e-011 3.59 104 3.4e-008 3.7e-003 2.1e-006 1.00e+000 3.624327918e+001 3.624336031e+001 1.8e-011 3.62 105 3.1e-008 3.4e-003 1.9e-006 9.99e-001 3.624328472e+001 3.624335774e+001 1.6e-011 3.65 106 2.7e-008 3.0e-003 1.7e-006 1.00e+000 3.624328971e+001 3.624335543e+001 1.4e-011 3.68 107 2.5e-008 2.7e-003 1.5e-006 9.98e-001 3.624329419e+001 3.624335335e+001 1.3e-011 3.71 108 2.2e-008 2.5e-003 1.4e-006 9.96e-001 3.624329823e+001 3.624335148e+001 1.2e-011 3.74 109 2.0e-008 2.2e-003 1.3e-006 1.00e+000 3.624330189e+001 3.624334977e+001 1.1e-011 3.77 110 1.8e-008 2.0e-003 1.1e-006 1.00e+000 3.624330519e+001 3.624334823e+001 9.5e-012 3.81 111 1.6e-008 1.8e-003 1.0e-006 1.00e+000 3.624330818e+001 3.624334684e+001 8.6e-012 3.84 112 1.5e-008 1.6e-003 9.1e-007 1.01e+000 3.624331088e+001 3.624334558e+001 7.7e-012 3.87 113 1.3e-008 1.5e-003 8.2e-007 9.98e-001 3.624331325e+001 3.624334448e+001 7.0e-012 3.90 114 1.2e-008 1.3e-003 7.4e-007 1.00e+000 3.624331538e+001 3.624334349e+001 6.3e-012 3.93 115 1.1e-008 1.2e-003 6.7e-007 1.00e+000 3.624331730e+001 3.624334260e+001 5.6e-012 3.96 116 9.6e-009 1.1e-003 6.0e-007 1.00e+000 3.624331903e+001 3.624334180e+001 5.1e-012 3.99 117 8.6e-009 9.5e-004 5.4e-007 9.98e-001 3.624332058e+001 3.624334108e+001 4.6e-012 4.03 118 7.8e-009 8.6e-004 4.9e-007 1.00e+000 3.624332198e+001 3.624334043e+001 4.1e-012 4.06 119 7.0e-009 7.7e-004 4.4e-007 1.00e+000 3.624332324e+001 3.624333984e+001 3.7e-012 4.09 120 6.3e-009 6.9e-004 3.9e-007 9.99e-001 3.624332437e+001 3.624333932e+001 3.3e-012 4.12 121 5.7e-009 6.2e-004 3.5e-007 1.00e+000 3.624332540e+001 3.624333884e+001 3.0e-012 4.15 122 5.1e-009 5.6e-004 3.2e-007 1.00e+000 3.624332631e+001 3.624333841e+001 2.7e-012 4.18 123 4.6e-009 5.1e-004 2.9e-007 9.99e-001 3.624332714e+001 3.624333803e+001 2.4e-012 4.21 124 4.1e-009 4.6e-004 2.6e-007 1.00e+000 3.624332788e+001 3.624333768e+001 2.2e-012 4.26 125 3.7e-009 4.1e-004 2.3e-007 1.00e+000 3.624332855e+001 3.624333737e+001 2.0e-012 4.29 126 3.3e-009 3.7e-004 2.1e-007 1.00e+000 3.624332915e+001 3.624333709e+001 1.8e-012 4.34 127 3.0e-009 3.3e-004 1.9e-007 9.97e-001 3.624332970e+001 3.624333684e+001 1.6e-012 4.38 128 2.7e-009 3.0e-004 1.7e-007 1.00e+000 3.624333019e+001 3.624333661e+001 1.4e-012 4.43 129 2.4e-009 2.7e-004 1.5e-007 1.01e+000 3.624333064e+001 3.624333640e+001 1.3e-012 4.46 130 2.2e-009 2.4e-004 1.4e-007 9.97e-001 3.624333103e+001 3.624333622e+001 1.2e-012 4.51 131 2.0e-009 2.2e-004 1.2e-007 1.00e+000 3.624333138e+001 3.624333605e+001 1.0e-012 4.54 132 1.8e-009 2.0e-004 1.1e-007 1.01e+000 3.624333171e+001 3.624333590e+001 9.5e-013 4.59 Interior-point optimizer terminated. Time: 4.59. Optimizer terminated. Time: 4.60 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 3.6243331713e+001 Viol. con: 3e-008 var: 0e+000 Dual. obj: 3.6243335900e+001 Viol. con: 0e+000 var: 1e-003 * End solution on dual form. * Transforming to primal solution. Solving took 4.63 seconds. result packing took 5.6% of solve time solution checking took 1.4% of solve time 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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 1012 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 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 : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 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 : 1.67e+004 after factor : 1.72e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.288863851e+005 2.000000000e+000 1.0e+000 0.08 1 1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.266339057e+005 3.774599270e+000 4.7e-001 0.14 2 4.2e+002 5.5e+002 2.4e+004 -9.35e-001 -1.204516300e+005 1.083248759e+001 1.9e-001 0.17 3 2.8e+002 3.7e+002 1.6e+004 -8.37e-001 -1.157870810e+005 6.665177446e+001 1.3e-001 0.22 4 2.8e+002 3.7e+002 1.6e+004 -7.58e-001 -1.132101896e+005 2.261947307e+003 1.2e-001 0.27 5 7.5e+001 9.8e+001 4.3e+003 -7.51e-001 -7.369911778e+004 1.114794054e+004 3.3e-002 0.30 6 3.0e+001 3.9e+001 1.7e+003 -1.92e-001 -3.984855613e+004 1.107249694e+004 1.3e-002 0.34 7 1.4e+001 1.8e+001 7.8e+002 3.92e-001 -2.070937051e+004 5.965041847e+003 6.1e-003 0.39 8 9.0e+000 1.2e+001 5.1e+002 7.29e-001 -1.410201696e+004 4.103526475e+003 4.0e-003 0.42 9 3.6e+000 4.7e+000 2.1e+002 8.34e-001 -5.837225250e+003 1.819161796e+003 1.6e-003 0.47 10 2.0e+000 2.6e+000 1.1e+002 9.52e-001 -2.940268965e+003 1.325304069e+003 8.9e-004 0.50 11 9.0e-001 1.2e+000 5.1e+001 9.84e-001 -1.324698522e+003 6.203743386e+002 4.1e-004 0.55 12 8.6e-001 1.2e+000 4.9e+001 9.64e-001 -1.286285107e+003 5.821375492e+002 3.9e-004 0.59 13 3.8e-001 5.3e-001 2.2e+001 9.81e-001 -5.626622952e+002 2.744796640e+002 1.7e-004 0.62 14 1.5e-001 2.3e-001 8.6e+000 1.00e+000 -2.179543837e+002 1.114771315e+002 6.9e-005 0.67 15 8.6e-002 1.5e-001 5.0e+000 1.00e+000 -1.179869490e+002 7.375584732e+001 4.0e-005 0.70 16 2.6e-002 1.2e-001 1.6e+000 1.00e+000 -2.807277833e+001 3.131489227e+001 1.3e-005 0.75 17 1.1e-002 9.3e-002 6.9e-001 1.00e+000 -5.276650842e+000 2.122045166e+001 5.7e-006 0.78 18 1.0e-002 8.5e-002 6.3e-001 1.01e+000 -3.410705859e+000 2.059177424e+001 5.2e-006 0.83 19 6.6e-003 6.5e-002 4.0e-001 1.01e+000 2.894599905e+000 1.822581874e+001 3.3e-006 0.86 20 4.5e-003 4.7e-002 2.8e-001 1.01e+000 6.709271993e+000 1.712856187e+001 2.3e-006 0.91 21 1.8e-003 5.9e-002 1.1e-001 1.01e+000 1.119391706e+001 1.545046106e+001 9.4e-007 0.95 22 1.0e-003 4.8e-002 6.2e-002 1.02e+000 1.264898549e+001 1.495383895e+001 5.1e-007 1.00 23 4.6e-004 5.4e-002 2.9e-002 1.02e+000 1.351661242e+001 1.458946314e+001 2.4e-007 1.03 24 2.6e-004 5.0e-002 1.6e-002 1.01e+000 1.385886798e+001 1.445533808e+001 1.4e-007 1.08 25 1.3e-004 5.2e-002 8.5e-003 1.01e+000 1.406164007e+001 1.437394309e+001 7.1e-008 1.11 26 9.0e-005 4.6e-002 5.6e-003 1.01e+000 1.413613414e+001 1.434341617e+001 4.7e-008 1.15 27 8.1e-005 4.2e-002 5.1e-003 1.00e+000 1.415438157e+001 1.434100931e+001 4.3e-008 1.19 28 7.3e-005 3.9e-002 4.6e-003 1.00e+000 1.416703049e+001 1.433496306e+001 3.8e-008 1.22 29 6.5e-005 3.6e-002 4.1e-003 1.00e+000 1.417864773e+001 1.432976687e+001 3.4e-008 1.25 30 5.9e-005 3.3e-002 3.7e-003 1.00e+000 1.418904926e+001 1.432503954e+001 3.1e-008 1.28 31 5.3e-005 3.0e-002 3.3e-003 1.00e+000 1.419838953e+001 1.432076735e+001 2.8e-008 1.31 32 4.8e-005 2.8e-002 3.0e-003 1.00e+000 1.420677443e+001 1.431690351e+001 2.5e-008 1.36 33 4.3e-005 2.6e-002 2.7e-003 1.00e+000 1.421430263e+001 1.431340996e+001 2.3e-008 1.39 34 3.9e-005 2.4e-002 2.4e-003 1.00e+000 1.422106268e+001 1.431025194e+001 2.0e-008 1.42 35 3.5e-005 2.2e-002 2.2e-003 1.00e+000 1.422713437e+001 1.430739887e+001 1.8e-008 1.45 36 3.1e-005 2.1e-002 2.0e-003 1.00e+000 1.423258909e+001 1.430482222e+001 1.7e-008 1.48 37 2.8e-005 2.0e-002 1.8e-003 1.00e+000 1.423749064e+001 1.430249684e+001 1.5e-008 1.51 38 2.5e-005 1.8e-002 1.6e-003 1.00e+000 1.424189578e+001 1.430039832e+001 1.3e-008 1.56 39 2.3e-005 1.7e-002 1.4e-003 1.00e+000 1.424585545e+001 1.429850505e+001 1.2e-008 1.59 40 2.0e-005 1.6e-002 1.3e-003 1.00e+000 1.424941511e+001 1.429679782e+001 1.1e-008 1.62 41 1.8e-005 1.5e-002 1.2e-003 1.00e+000 1.425261543e+001 1.429525814e+001 9.8e-009 1.65 42 1.7e-005 1.5e-002 1.0e-003 1.00e+000 1.425549304e+001 1.429386993e+001 8.8e-009 1.69 43 1.5e-005 1.4e-002 9.4e-004 1.00e+000 1.425808059e+001 1.429261881e+001 7.9e-009 1.72 44 1.3e-005 1.3e-002 8.5e-004 1.00e+000 1.426040741e+001 1.429149100e+001 7.1e-009 1.76 45 1.2e-005 1.3e-002 7.6e-004 1.00e+000 1.426249986e+001 1.429047450e+001 6.4e-009 1.79 46 1.1e-005 1.2e-002 6.9e-004 1.00e+000 1.426438154e+001 1.428955825e+001 5.8e-009 1.83 47 9.8e-006 1.2e-002 6.2e-004 1.00e+000 1.426607367e+001 1.428873230e+001 5.2e-009 1.86 48 8.8e-006 1.1e-002 5.6e-004 1.00e+000 1.426759530e+001 1.428798768e+001 4.7e-009 1.89 49 7.9e-006 1.1e-002 5.0e-004 1.00e+000 1.426896358e+001 1.428731610e+001 4.2e-009 1.93 50 7.1e-006 1.1e-002 4.5e-004 1.00e+000 1.427019388e+001 1.428671078e+001 3.8e-009 1.97 51 6.4e-006 1.0e-002 4.0e-004 1.00e+000 1.427130007e+001 1.428616500e+001 3.4e-009 2.00 52 5.8e-006 1.0e-002 3.6e-004 1.00e+000 1.427229471e+001 1.428567276e+001 3.1e-009 2.03 53 5.2e-006 9.7e-003 3.3e-004 1.00e+000 1.427318906e+001 1.428522922e+001 2.8e-009 2.06 54 4.7e-006 9.5e-003 3.0e-004 1.00e+000 1.427399327e+001 1.428482962e+001 2.5e-009 2.11 55 4.2e-006 9.3e-003 2.7e-004 1.00e+000 1.427471664e+001 1.428446911e+001 2.2e-009 2.14 56 3.8e-006 9.1e-003 2.4e-004 1.00e+000 1.427536730e+001 1.428414445e+001 2.0e-009 2.17 57 3.4e-006 9.0e-003 2.2e-004 1.00e+000 1.427595262e+001 1.428385189e+001 1.8e-009 2.21 58 3.1e-006 8.8e-003 1.9e-004 1.00e+000 1.427647916e+001 1.428358862e+001 1.6e-009 2.25 59 2.8e-006 8.7e-003 1.7e-004 9.99e-001 1.427695283e+001 1.428335173e+001 1.5e-009 2.28 60 2.5e-006 8.5e-003 1.6e-004 1.00e+000 1.427737914e+001 1.428313781e+001 1.3e-009 2.31 61 2.2e-006 8.4e-003 1.4e-004 1.00e+000 1.427776271e+001 1.428294538e+001 1.2e-009 2.34 62 2.0e-006 8.3e-003 1.3e-004 1.00e+000 1.427810784e+001 1.428277203e+001 1.1e-009 2.37 63 1.8e-006 8.2e-003 1.1e-004 9.98e-001 1.427841826e+001 1.428261655e+001 9.6e-010 2.42 64 1.6e-006 8.1e-003 1.0e-004 9.99e-001 1.427869762e+001 1.428247629e+001 8.6e-010 2.45 65 1.5e-006 8.1e-003 9.3e-005 1.00e+000 1.427894911e+001 1.428234962e+001 7.8e-010 2.48 66 1.3e-006 8.0e-003 8.3e-005 9.98e-001 1.427917529e+001 1.428223613e+001 7.0e-010 2.51 67 1.2e-006 7.9e-003 7.5e-005 9.99e-001 1.427937883e+001 1.428213381e+001 6.3e-010 2.54 68 1.1e-006 7.9e-003 6.8e-005 9.95e-001 1.427956192e+001 1.428204201e+001 5.7e-010 2.57 69 9.7e-007 7.8e-003 6.1e-005 1.00e+000 1.427972681e+001 1.428195877e+001 5.1e-010 2.61 70 8.7e-007 7.8e-003 5.5e-005 9.98e-001 1.427987514e+001 1.428188415e+001 4.6e-010 2.64 71 7.8e-007 7.7e-003 4.9e-005 1.00e+000 1.428000869e+001 1.428181660e+001 4.1e-010 2.67 72 7.0e-007 7.7e-003 4.4e-005 1.00e+000 1.428012886e+001 1.428175588e+001 3.7e-010 2.70 73 6.3e-007 7.6e-003 4.0e-005 9.96e-001 1.428023692e+001 1.428170151e+001 3.4e-010 2.75 74 5.7e-007 7.6e-003 3.6e-005 9.93e-001 1.428033412e+001 1.428165272e+001 3.0e-010 2.76 75 5.1e-007 7.6e-003 3.2e-005 9.98e-001 1.428042166e+001 1.428160851e+001 2.7e-010 2.81 76 4.6e-007 7.6e-003 2.9e-005 1.00e+000 1.428050122e+001 1.428156809e+001 2.4e-010 2.84 77 4.2e-007 7.5e-003 2.6e-005 9.97e-001 1.428057203e+001 1.428153234e+001 2.2e-010 2.87 78 3.7e-007 7.5e-003 2.4e-005 1.00e+000 1.428063578e+001 1.428150006e+001 2.0e-010 2.90 79 3.4e-007 6.8e-003 2.1e-005 1.01e+000 1.428069420e+001 1.428147031e+001 1.8e-010 2.93 80 3.0e-007 6.1e-003 1.9e-005 9.95e-001 1.428074569e+001 1.428144436e+001 1.6e-010 2.96 81 2.7e-007 5.5e-003 1.7e-005 9.92e-001 1.428079201e+001 1.428142105e+001 1.4e-010 3.00 82 2.5e-007 4.9e-003 1.5e-005 1.01e+000 1.428083483e+001 1.428139917e+001 1.3e-010 3.03 83 2.2e-007 4.4e-003 1.4e-005 9.94e-001 1.428087225e+001 1.428138030e+001 1.2e-010 3.06 84 2.0e-007 4.0e-003 1.3e-005 1.02e+000 1.428090809e+001 1.428136185e+001 1.1e-010 3.09 85 1.8e-007 3.6e-003 1.1e-005 1.03e+000 1.428094159e+001 1.428134447e+001 9.7e-011 3.12 86 1.6e-007 3.2e-003 1.0e-005 1.01e+000 1.428096932e+001 1.428133034e+001 8.8e-011 3.15 87 1.4e-007 2.9e-003 9.1e-006 9.88e-001 1.428099327e+001 1.428131838e+001 7.9e-011 3.20 88 1.3e-007 2.6e-003 8.2e-006 9.77e-001 1.428101479e+001 1.428130772e+001 7.1e-011 3.23 89 1.2e-007 2.4e-003 7.4e-006 9.98e-001 1.428103421e+001 1.428129789e+001 6.4e-011 3.26 90 1.1e-007 2.1e-003 6.7e-006 1.00e+000 1.428105186e+001 1.428128891e+001 5.8e-011 3.29 91 9.5e-008 1.9e-003 6.0e-006 9.73e-001 1.428106753e+001 1.428128116e+001 5.2e-011 3.32 92 8.6e-008 1.7e-003 5.4e-006 1.00e+000 1.428108189e+001 1.428127382e+001 4.7e-011 3.35 93 7.7e-008 1.5e-003 4.8e-006 1.01e+000 1.428109494e+001 1.428126714e+001 4.2e-011 3.38 94 6.9e-008 1.4e-003 4.4e-006 1.01e+000 1.428110689e+001 1.428126100e+001 3.8e-011 3.42 95 6.2e-008 1.3e-003 3.9e-006 9.89e-001 1.428111709e+001 1.428125587e+001 3.4e-011 3.45 96 5.6e-008 1.1e-003 3.5e-006 1.02e+000 1.428112717e+001 1.428125064e+001 3.1e-011 3.48 97 5.1e-008 1.0e-003 3.2e-006 1.03e+000 1.428113654e+001 1.428124575e+001 2.9e-011 3.51 98 4.6e-008 9.1e-004 2.9e-006 9.01e-001 1.428114369e+001 1.428124247e+001 2.6e-011 3.54 99 4.1e-008 8.2e-004 2.6e-006 1.06e+000 1.428115203e+001 1.428123796e+001 2.4e-011 3.57 100 3.7e-008 7.4e-004 2.3e-006 1.00e+000 1.428115774e+001 1.428123508e+001 2.1e-011 3.62 101 3.3e-008 6.7e-004 2.1e-006 1.00e+000 1.428116287e+001 1.428123247e+001 1.9e-011 3.65 102 3.0e-008 6.0e-004 1.9e-006 8.98e-001 1.428116742e+001 1.428123038e+001 1.7e-011 3.68 103 2.7e-008 5.4e-004 1.7e-006 1.14e+000 1.428117419e+001 1.428122648e+001 1.7e-011 3.71 104 2.5e-008 4.9e-004 1.5e-006 1.00e+000 1.428117772e+001 1.428122471e+001 1.5e-011 3.74 105 2.2e-008 4.4e-004 1.4e-006 9.92e-001 1.428118085e+001 1.428122316e+001 1.4e-011 3.77 106 2.0e-008 3.9e-004 1.2e-006 1.01e+000 1.428118376e+001 1.428122169e+001 1.2e-011 3.81 107 1.8e-008 3.5e-004 1.1e-006 1.01e+000 1.428118638e+001 1.428122036e+001 1.1e-011 3.84 108 1.6e-008 3.2e-004 1.0e-006 1.02e+000 1.428118889e+001 1.428121908e+001 1.0e-011 3.87 109 1.5e-008 2.9e-004 9.0e-007 9.96e-001 1.428119090e+001 1.428121808e+001 9.1e-012 3.88 110 1.3e-008 2.6e-004 8.1e-007 9.75e-001 1.428119271e+001 1.428121720e+001 8.2e-012 3.92 111 1.2e-008 2.3e-004 7.3e-007 1.02e+000 1.428119451e+001 1.428121627e+001 7.4e-012 3.95 112 1.1e-008 2.1e-004 6.6e-007 1.01e+000 1.428119602e+001 1.428121551e+001 6.7e-012 3.98 113 9.6e-009 1.9e-004 5.9e-007 1.00e+000 1.428119734e+001 1.428121485e+001 6.1e-012 4.03 114 8.6e-009 1.7e-004 5.3e-007 9.70e-001 1.428119851e+001 1.428121429e+001 5.5e-012 4.06 115 7.7e-009 1.5e-004 4.8e-007 1.00e+000 1.428119956e+001 1.428121377e+001 4.9e-012 4.10 116 6.9e-009 1.4e-004 4.3e-007 9.98e-001 1.428120051e+001 1.428121329e+001 4.4e-012 4.13 117 6.2e-009 1.2e-004 3.9e-007 9.91e-001 1.428120136e+001 1.428121287e+001 4.0e-012 4.17 118 5.6e-009 1.1e-004 3.5e-007 9.47e-001 1.428120212e+001 1.428121251e+001 3.6e-012 4.20 119 5.0e-009 1.0e-004 3.1e-007 9.48e-001 1.428120281e+001 1.428121219e+001 3.2e-012 4.24 120 4.5e-009 9.0e-005 2.8e-007 1.02e+000 1.428120350e+001 1.428121183e+001 2.9e-012 4.27 121 4.1e-009 8.1e-005 2.5e-007 1.06e+000 1.428120418e+001 1.428121146e+001 2.7e-012 4.32 122 3.7e-009 7.3e-005 2.3e-007 9.65e-001 1.428120467e+001 1.428121123e+001 2.4e-012 4.37 123 3.3e-009 6.6e-005 2.1e-007 1.10e+000 1.428120530e+001 1.428121087e+001 2.3e-012 4.40 124 3.0e-009 5.9e-005 1.9e-007 9.90e-001 1.428120568e+001 1.428121069e+001 2.1e-012 4.43 125 2.7e-009 5.3e-005 1.7e-007 9.60e-001 1.428120601e+001 1.428121053e+001 1.9e-012 4.49 126 2.2e-009 3.1e-006 9.7e-009 8.04e-001 1.428120905e+001 1.428120934e+001 2.6e-013 4.52 Interior-point optimizer terminated. Time: 4.54. Optimizer terminated. Time: 4.55 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.4281209047e+001 Viol. con: 4e-008 var: 0e+000 Dual. obj: 1.4281209335e+001 Viol. con: 0e+000 var: 2e-005 * End solution on dual form. * Transforming to primal solution. Solving took 4.57 seconds. result packing took 6.7% of solve time solution checking took 2.1% of solve time 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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 1010 Eliminator terminated. Eliminator started. Total number of eliminations : 1022 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1022 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 : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 831 Optimizer - Cones : 0 Optimizer - Scalar variables : 3581 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.08 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.06 Factor - nonzeros before factor : 1.67e+004 after factor : 1.72e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.289101986e+005 2.000000000e+000 1.0e+000 0.11 1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.266148481e+005 3.779171618e+000 4.6e-001 0.16 2 4.0e+002 5.1e+002 2.2e+004 -9.34e-001 -1.198563787e+005 1.137215124e+001 1.7e-001 0.19 3 2.8e+002 3.6e+002 1.6e+004 -8.29e-001 -1.157240237e+005 8.367015203e+001 1.2e-001 0.23 4 2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.124198285e+005 2.832600458e+003 1.2e-001 0.27 5 6.3e+001 8.2e+001 3.6e+003 -7.47e-001 -6.640387866e+004 1.269993095e+004 2.8e-002 0.30 6 3.9e+001 5.1e+001 2.2e+003 -7.19e-002 -4.860600692e+004 1.113872250e+004 1.7e-002 0.33 7 2.8e+001 3.7e+001 1.6e+003 2.50e-001 -3.839144233e+004 8.758888391e+003 1.3e-002 0.36 8 1.6e+001 2.1e+001 9.0e+002 4.36e-001 -2.428137334e+004 5.454539791e+003 7.1e-003 0.41 9 6.4e+000 8.3e+000 3.6e+002 6.74e-001 -1.033392090e+004 2.810570912e+003 2.9e-003 0.44 10 3.6e+000 4.7e+000 2.0e+002 8.87e-001 -5.635129586e+003 1.899017961e+003 1.6e-003 0.47 11 1.3e+000 1.7e+000 7.5e+001 9.54e-001 -2.012850000e+003 7.891732150e+002 5.9e-004 0.50 12 1.0e+000 1.3e+000 5.7e+001 9.87e-001 -1.520027719e+003 6.366082891e+002 4.5e-004 0.53 13 8.5e-001 1.5e+000 4.8e+001 9.70e-001 -1.298863315e+003 5.502877421e+002 3.9e-004 0.56 14 2.9e-001 5.1e-001 1.6e+001 9.89e-001 -4.334746822e+002 1.970088633e+002 1.3e-004 0.59 15 1.6e-001 3.0e-001 9.3e+000 1.00e+000 -2.379382790e+002 1.162332356e+002 7.5e-005 0.62 16 7.3e-002 1.6e-001 4.2e+000 1.00e+000 -1.038595138e+002 5.761979623e+001 3.4e-005 0.67 17 3.5e-002 1.0e-001 2.1e+000 1.01e+000 -4.582056537e+001 3.218273637e+001 1.7e-005 0.70 18 1.8e-002 7.9e-002 1.1e+000 1.01e+000 -2.038712715e+001 2.046089104e+001 8.8e-006 0.73 19 1.8e-002 7.6e-002 1.0e+000 1.02e+000 -1.899852130e+001 2.043791705e+001 8.5e-006 0.76 20 9.7e-003 5.8e-002 5.7e-001 1.02e+000 -4.740804072e+000 1.674373134e+001 4.7e-006 0.80 21 4.1e-003 5.8e-002 2.5e-001 1.02e+000 4.583283022e+000 1.368803991e+001 2.0e-006 0.83 22 2.1e-003 5.2e-002 1.3e-001 1.01e+000 7.768931233e+000 1.261358749e+001 1.1e-006 0.87 23 6.0e-004 8.2e-002 3.9e-002 9.87e-001 1.034302451e+001 1.181151718e+001 3.4e-007 0.90 24 1.8e-004 8.8e-002 1.3e-002 9.78e-001 1.109075737e+001 1.156935519e+001 1.1e-007 0.94 25 6.0e-005 8.7e-002 4.3e-003 9.88e-001 1.133248299e+001 1.149489107e+001 3.9e-008 0.97 26 2.2e-005 8.4e-002 1.6e-003 9.96e-001 1.141328756e+001 1.147317424e+001 1.5e-008 1.00 27 8.2e-006 8.1e-002 6.0e-004 9.99e-001 1.144292920e+001 1.146572700e+001 5.6e-009 1.03 28 7.4e-006 7.4e-002 5.4e-004 1.00e+000 1.144485658e+001 1.146537603e+001 5.0e-009 1.06 29 6.7e-006 6.7e-002 4.9e-004 1.00e+000 1.144644876e+001 1.146491665e+001 4.5e-009 1.09 30 6.0e-006 6.1e-002 4.4e-004 1.00e+000 1.144788140e+001 1.146450283e+001 4.1e-009 1.12 31 5.4e-006 5.6e-002 3.9e-004 1.00e+000 1.144916812e+001 1.146412767e+001 3.7e-009 1.15 32 4.9e-006 5.1e-002 3.5e-004 1.00e+000 1.145032498e+001 1.146378879e+001 3.3e-009 1.20 33 4.4e-006 4.6e-002 3.2e-004 1.00e+000 1.145136502e+001 1.146348257e+001 3.0e-009 1.23 34 3.9e-006 4.2e-002 2.9e-004 1.00e+000 1.145230015e+001 1.146320607e+001 2.7e-009 1.26 35 3.5e-006 3.9e-002 2.6e-004 1.00e+000 1.145314102e+001 1.146295644e+001 2.4e-009 1.29 36 3.2e-006 3.6e-002 2.3e-004 1.00e+000 1.145389720e+001 1.146273117e+001 2.2e-009 1.33 37 2.9e-006 3.3e-002 2.1e-004 1.00e+000 1.145457730e+001 1.146252794e+001 1.9e-009 1.36 38 2.6e-006 3.0e-002 1.9e-004 1.00e+000 1.145518902e+001 1.146234466e+001 1.7e-009 1.40 39 2.3e-006 2.8e-002 1.7e-004 1.00e+000 1.145573927e+001 1.146217941e+001 1.6e-009 1.44 40 2.1e-006 2.6e-002 1.5e-004 1.00e+000 1.145623426e+001 1.146203046e+001 1.4e-009 1.47 41 1.9e-006 2.4e-002 1.4e-004 1.00e+000 1.145667959e+001 1.146189616e+001 1.3e-009 1.50 42 1.7e-006 2.2e-002 1.2e-004 1.00e+000 1.145708023e+001 1.146177521e+001 1.1e-009 1.54 43 1.5e-006 2.1e-002 1.1e-004 1.00e+000 1.145744069e+001 1.146166622e+001 1.0e-009 1.58 44 1.4e-006 1.9e-002 1.0e-004 1.00e+000 1.145776504e+001 1.146156800e+001 9.3e-010 1.62 45 1.2e-006 1.8e-002 9.0e-005 1.00e+000 1.145805688e+001 1.146147951e+001 8.4e-010 1.65 46 1.1e-006 1.7e-002 8.1e-005 1.00e+000 1.145831948e+001 1.146139983e+001 7.5e-010 1.68 47 1.0e-006 1.6e-002 7.3e-005 1.00e+000 1.145855577e+001 1.146132811e+001 6.8e-010 1.70 48 9.0e-007 1.5e-002 6.6e-005 1.00e+000 1.145876839e+001 1.146126355e+001 6.1e-010 1.73 49 8.1e-007 1.4e-002 5.9e-005 1.00e+000 1.145895973e+001 1.146120537e+001 5.5e-010 1.76 50 7.3e-007 1.4e-002 5.3e-005 1.00e+000 1.145913192e+001 1.146115299e+001 4.9e-010 1.79 51 6.6e-007 1.3e-002 4.8e-005 1.00e+000 1.145928688e+001 1.146110581e+001 4.4e-010 1.83 52 2.3e-007 4.5e-003 1.7e-005 1.00e+000 1.146019606e+001 1.146082816e+001 1.5e-010 1.86 53 2.1e-007 4.0e-003 1.5e-005 1.00e+000 1.146024491e+001 1.146081372e+001 1.4e-010 1.89 54 7.1e-008 1.4e-003 5.1e-006 1.00e+000 1.146053150e+001 1.146072571e+001 4.7e-011 1.93 55 6.3e-008 1.2e-003 4.6e-006 9.70e-001 1.146054643e+001 1.146072145e+001 4.3e-011 1.97 56 5.7e-008 1.1e-003 4.1e-006 1.03e+000 1.146056187e+001 1.146071645e+001 3.9e-011 2.01 57 5.1e-008 1.0e-003 3.7e-006 1.02e+000 1.146057456e+001 1.146071255e+001 3.5e-011 2.04 58 4.6e-008 9.0e-004 3.4e-006 1.01e+000 1.146058559e+001 1.146070918e+001 3.2e-011 2.07 59 4.2e-008 8.1e-004 3.0e-006 1.04e+000 1.146059689e+001 1.146070556e+001 2.9e-011 2.12 60 1.6e-008 1.6e-004 5.8e-007 9.71e-001 1.146066502e+001 1.146068616e+001 6.0e-012 2.15 61 1.4e-008 1.4e-004 5.2e-007 9.72e-001 1.146066657e+001 1.146068567e+001 5.4e-012 2.18 62 5.8e-009 8.1e-006 3.0e-008 9.58e-001 1.146067995e+001 1.146068109e+001 4.3e-013 2.21 Interior-point optimizer terminated. Time: 2.23. Optimizer terminated. Time: 2.23 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1460679945e+001 Viol. con: 2e-007 var: 0e+000 Dual. obj: 1.1460681085e+001 Viol. con: 0e+000 var: 6e-005 * End solution on dual form. * Transforming to primal solution. Solving took 2.26 seconds. result packing took 13% of solve time solution checking took 3.7% of solve time 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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 1012 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 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 : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 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 : 0.05 Factor - nonzeros before factor : 1.67e+004 after factor : 1.72e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.288303351e+005 2.000000000e+000 1.0e+000 0.11 1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265192771e+005 3.780479854e+000 4.6e-001 0.16 2 3.9e+002 5.0e+002 2.2e+004 -9.34e-001 -1.195799157e+005 1.160516545e+001 1.7e-001 0.20 3 2.8e+002 3.6e+002 1.6e+004 -8.26e-001 -1.156357841e+005 9.406781001e+001 1.2e-001 0.23 4 2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.123238043e+005 2.800934451e+003 1.2e-001 0.28 5 7.8e+001 1.0e+002 4.4e+003 -7.46e-001 -7.498391453e+004 1.053067756e+004 3.5e-002 0.31 6 3.8e+001 4.9e+001 2.1e+003 -2.08e-001 -4.716202121e+004 1.110975420e+004 1.7e-002 0.36 7 2.1e+001 2.8e+001 1.2e+003 2.72e-001 -3.073919504e+004 7.248970455e+003 9.5e-003 0.39 8 9.8e+000 1.3e+001 5.5e+002 5.69e-001 -1.536034849e+004 3.891970581e+003 4.3e-003 0.42 9 4.2e+000 5.5e+000 2.4e+002 8.19e-001 -6.676929582e+003 2.109893022e+003 1.9e-003 0.47 10 2.0e+000 2.6e+000 1.1e+002 9.39e-001 -2.962273675e+003 1.171566214e+003 8.8e-004 0.50 11 1.4e+000 1.8e+000 7.8e+001 9.83e-001 -2.096575009e+003 8.360471154e+002 6.2e-004 0.53 12 9.0e-001 1.2e+000 5.1e+001 9.85e-001 -1.355755905e+003 5.626980397e+002 4.0e-004 0.56 13 7.4e-001 1.1e+000 4.2e+001 9.64e-001 -1.126538147e+003 4.651708815e+002 3.3e-004 0.61 14 2.6e-001 3.9e-001 1.5e+001 9.90e-001 -3.944746202e+002 1.817810166e+002 1.2e-004 0.64 15 1.5e-001 2.3e-001 8.6e+000 1.00e+000 -2.189168180e+002 1.081383764e+002 6.9e-005 0.69 16 4.0e-002 1.5e-001 2.4e+000 1.00e+000 -5.533028505e+001 3.458678931e+001 1.9e-005 0.73 17 3.4e-002 1.3e-001 2.0e+000 1.00e+000 -4.533261194e+001 3.085049303e+001 1.6e-005 0.76 18 2.2e-002 9.8e-002 1.3e+000 1.00e+000 -2.663560875e+001 2.253725602e+001 1.1e-005 0.80 19 1.7e-002 7.9e-002 1.0e+000 1.01e+000 -1.829653412e+001 1.992511463e+001 8.3e-006 0.83 20 1.4e-002 6.7e-002 8.5e-001 1.02e+000 -1.320402192e+001 1.870490002e+001 7.0e-006 0.86 21 5.6e-003 6.1e-002 3.3e-001 1.02e+000 1.873822750e+000 1.418997686e+001 2.7e-006 0.89 22 2.2e-003 6.3e-002 1.4e-001 1.02e+000 7.557518630e+000 1.254469167e+001 1.1e-006 0.92 23 8.1e-004 6.3e-002 5.1e-002 9.85e-001 9.852186839e+000 1.176720121e+001 4.5e-007 0.95 24 3.0e-004 7.5e-002 2.0e-002 9.69e-001 1.075832651e+001 1.152374615e+001 1.8e-007 0.98 25 1.5e-004 5.8e-002 1.0e-002 9.56e-001 1.105384790e+001 1.143573124e+001 8.9e-008 1.00 26 7.1e-005 5.7e-002 5.0e-003 9.86e-001 1.120398083e+001 1.139454036e+001 4.4e-008 1.03 27 6.4e-005 5.2e-002 4.5e-003 9.93e-001 1.122050915e+001 1.139216386e+001 4.0e-008 1.06 28 5.8e-005 4.8e-002 4.0e-003 9.92e-001 1.123375956e+001 1.138832808e+001 3.6e-008 1.09 29 5.2e-005 4.4e-002 3.6e-003 9.93e-001 1.124593056e+001 1.138513225e+001 3.2e-008 1.12 30 4.7e-005 4.0e-002 3.3e-003 9.93e-001 1.125681720e+001 1.138218757e+001 2.9e-008 1.15 31 4.2e-005 3.7e-002 2.9e-003 9.93e-001 1.126657406e+001 1.137949765e+001 2.6e-008 1.19 32 3.8e-005 3.4e-002 2.6e-003 9.92e-001 1.127530756e+001 1.137704145e+001 2.4e-008 1.22 33 3.4e-005 3.1e-002 2.4e-003 9.91e-001 1.128312316e+001 1.137480592e+001 2.1e-008 1.25 34 3.1e-005 2.9e-002 2.1e-003 9.89e-001 1.129012460e+001 1.137278071e+001 1.9e-008 1.28 35 2.8e-005 2.7e-002 1.9e-003 9.88e-001 1.129646134e+001 1.137095314e+001 1.7e-008 1.33 36 2.5e-005 2.5e-002 1.7e-003 9.88e-001 1.130220444e+001 1.136926515e+001 1.6e-008 1.36 37 2.2e-005 2.3e-002 1.6e-003 9.88e-001 1.130732385e+001 1.136773521e+001 1.4e-008 1.39 38 2.0e-005 2.1e-002 1.4e-003 9.88e-001 1.131194971e+001 1.136632941e+001 1.3e-008 1.44 39 1.8e-005 2.0e-002 1.3e-003 9.88e-001 1.131609590e+001 1.136507114e+001 1.1e-008 1.47 40 1.6e-005 1.9e-002 1.1e-003 9.89e-001 1.131981121e+001 1.136390407e+001 1.0e-008 1.50 41 1.5e-005 1.7e-002 1.0e-003 9.89e-001 1.132316883e+001 1.136286263e+001 9.2e-009 1.54 42 1.3e-005 1.6e-002 9.2e-004 9.90e-001 1.132617129e+001 1.136191456e+001 8.3e-009 1.58 43 1.2e-005 1.5e-002 8.3e-004 9.90e-001 1.132886964e+001 1.136104847e+001 7.4e-009 1.61 44 1.1e-005 1.5e-002 7.5e-004 9.90e-001 1.133130220e+001 1.136027066e+001 6.7e-009 1.64 45 9.6e-006 1.4e-002 6.7e-004 9.91e-001 1.133348670e+001 1.135956791e+001 6.0e-009 1.69 46 8.7e-006 1.3e-002 6.1e-004 9.91e-001 1.133544874e+001 1.135893063e+001 5.4e-009 1.72 47 7.8e-006 1.3e-002 5.5e-004 9.92e-001 1.133721413e+001 1.135835530e+001 4.9e-009 1.75 48 7.0e-006 1.2e-002 4.9e-004 9.93e-001 1.133880300e+001 1.135783694e+001 4.4e-009 1.78 49 6.3e-006 1.1e-002 4.4e-004 9.94e-001 1.134023293e+001 1.135736994e+001 4.0e-009 1.81 50 5.7e-006 1.1e-002 4.0e-004 9.94e-001 1.134152016e+001 1.135694928e+001 3.6e-009 1.84 51 5.1e-006 1.1e-002 3.6e-004 9.95e-001 1.134267925e+001 1.135657034e+001 3.2e-009 1.89 52 4.6e-006 1.0e-002 3.2e-004 9.96e-001 1.134372305e+001 1.135622890e+001 2.9e-009 1.92 53 4.2e-006 9.9e-003 2.9e-004 9.97e-001 1.134466291e+001 1.135592109e+001 2.6e-009 1.95 54 3.7e-006 9.6e-003 2.6e-004 9.97e-001 1.134550901e+001 1.135564350e+001 2.3e-009 1.98 55 3.4e-006 9.4e-003 2.3e-004 9.98e-001 1.134627055e+001 1.135539314e+001 2.1e-009 2.03 56 3.0e-006 9.1e-003 2.1e-004 9.98e-001 1.134695588e+001 1.135516738e+001 1.9e-009 2.06 57 2.7e-006 8.9e-003 1.9e-004 9.98e-001 1.134757261e+001 1.135496384e+001 1.7e-009 2.09 58 2.5e-006 8.7e-003 1.7e-004 9.98e-001 1.134812758e+001 1.135478040e+001 1.5e-009 2.12 59 2.2e-006 8.6e-003 1.5e-004 9.99e-001 1.134862701e+001 1.135461511e+001 1.4e-009 2.20 60 2.0e-006 8.4e-003 1.4e-004 9.99e-001 1.134907646e+001 1.135446619e+001 1.2e-009 2.23 61 1.8e-006 8.3e-003 1.2e-004 9.99e-001 1.134948095e+001 1.135433205e+001 1.1e-009 2.26 62 1.6e-006 8.1e-003 1.1e-004 9.99e-001 1.134984499e+001 1.135421128e+001 1.0e-009 2.29 63 1.4e-006 8.0e-003 1.0e-004 9.99e-001 1.135017263e+001 1.135410253e+001 9.0e-010 2.34 64 1.3e-006 7.9e-003 9.1e-005 9.99e-001 1.135046752e+001 1.135400460e+001 8.1e-010 2.37 65 1.2e-006 7.8e-003 8.2e-005 9.99e-001 1.135073294e+001 1.135391646e+001 7.3e-010 2.40 66 1.1e-006 7.7e-003 7.4e-005 9.99e-001 1.135097182e+001 1.135383715e+001 6.6e-010 2.43 67 9.5e-007 7.7e-003 6.6e-005 9.99e-001 1.135118685e+001 1.135376574e+001 5.9e-010 2.46 68 8.6e-007 7.6e-003 6.0e-005 1.00e+000 1.135138038e+001 1.135370148e+001 5.3e-010 2.50 69 7.7e-007 7.5e-003 5.4e-005 1.00e+000 1.135155459e+001 1.135364363e+001 4.8e-010 2.54 70 6.9e-007 7.5e-003 4.8e-005 1.00e+000 1.135171138e+001 1.135359158e+001 4.3e-010 2.57 71 6.2e-007 7.4e-003 4.4e-005 1.00e+000 1.135185251e+001 1.135354474e+001 3.9e-010 2.61 72 5.6e-007 7.4e-003 3.9e-005 1.00e+000 1.135197954e+001 1.135350257e+001 3.5e-010 2.64 73 5.0e-007 7.3e-003 3.5e-005 1.00e+000 1.135209388e+001 1.135346463e+001 3.2e-010 2.67 74 4.5e-007 7.3e-003 3.2e-005 1.00e+000 1.135219679e+001 1.135343048e+001 2.8e-010 2.70 75 4.1e-007 7.3e-003 2.9e-005 1.00e+000 1.135228941e+001 1.135339975e+001 2.6e-010 2.73 76 3.7e-007 7.2e-003 2.6e-005 9.99e-001 1.135237277e+001 1.135337211e+001 2.3e-010 2.78 77 3.3e-007 7.2e-003 2.3e-005 1.00e+000 1.135244780e+001 1.135334722e+001 2.1e-010 2.81 78 3.0e-007 7.2e-003 2.1e-005 1.00e+000 1.135251534e+001 1.135332482e+001 1.9e-010 2.84 79 2.7e-007 7.1e-003 1.9e-005 9.99e-001 1.135257611e+001 1.135330468e+001 1.7e-010 2.87 80 2.4e-007 7.1e-003 1.7e-005 1.00e+000 1.135263081e+001 1.135328654e+001 1.5e-010 2.90 81 2.2e-007 7.1e-003 1.5e-005 1.00e+000 1.135268005e+001 1.135327020e+001 1.4e-010 2.93 82 2.0e-007 7.1e-003 1.4e-005 1.00e+000 1.135272437e+001 1.135325546e+001 1.2e-010 2.96 83 1.8e-007 7.1e-003 1.2e-005 1.00e+000 1.135276425e+001 1.135324222e+001 1.1e-010 3.00 84 1.6e-007 7.0e-003 1.1e-005 1.00e+000 1.135280014e+001 1.135323032e+001 9.9e-011 3.04 85 1.4e-007 7.0e-003 1.0e-005 1.00e+000 1.135283244e+001 1.135321961e+001 8.9e-011 3.07 86 1.3e-007 7.0e-003 9.0e-006 1.00e+000 1.135286151e+001 1.135320996e+001 8.0e-011 3.10 87 1.2e-007 7.0e-003 8.1e-006 1.00e+000 1.135288767e+001 1.135320128e+001 7.2e-011 3.15 88 1.0e-007 7.0e-003 7.3e-006 1.00e+000 1.135291121e+001 1.135319347e+001 6.5e-011 3.18 89 9.4e-008 7.0e-003 6.5e-006 1.00e+000 1.135293240e+001 1.135318643e+001 5.8e-011 3.21 90 8.4e-008 7.0e-003 5.9e-006 1.00e+000 1.135295148e+001 1.135318009e+001 5.3e-011 3.26 91 7.6e-008 7.0e-003 5.3e-006 1.00e+000 1.135296864e+001 1.135317438e+001 4.7e-011 3.29 92 6.8e-008 7.0e-003 4.8e-006 1.00e+000 1.135298409e+001 1.135316925e+001 4.3e-011 3.32 93 6.1e-008 6.9e-003 4.3e-006 9.98e-001 1.135299798e+001 1.135316464e+001 3.8e-011 3.37 94 5.5e-008 6.9e-003 3.9e-006 9.98e-001 1.135301049e+001 1.135316050e+001 3.5e-011 3.40 95 5.0e-008 6.9e-003 3.5e-006 9.97e-001 1.135302174e+001 1.135315677e+001 3.1e-011 3.45 96 4.5e-008 6.9e-003 3.1e-006 9.97e-001 1.135303187e+001 1.135315341e+001 2.8e-011 3.48 97 4.0e-008 6.9e-003 2.8e-006 9.96e-001 1.135304098e+001 1.135315040e+001 2.5e-011 3.51 98 3.6e-008 6.2e-003 2.5e-006 1.01e+000 1.135304938e+001 1.135314758e+001 2.3e-011 3.56 99 3.3e-008 5.6e-003 2.3e-006 9.99e-001 1.135305675e+001 1.135314513e+001 2.0e-011 3.59 100 2.9e-008 5.0e-003 2.1e-006 9.89e-001 1.135306337e+001 1.135314296e+001 1.8e-011 3.62 101 2.6e-008 4.5e-003 1.8e-006 1.00e+000 1.135306943e+001 1.135314092e+001 1.7e-011 3.67 102 2.4e-008 4.1e-003 1.7e-006 1.01e+000 1.135307491e+001 1.135313908e+001 1.5e-011 3.70 103 2.1e-008 3.7e-003 1.5e-006 9.95e-001 1.135307972e+001 1.135313749e+001 1.3e-011 3.73 104 1.9e-008 3.3e-003 1.3e-006 9.87e-001 1.135308405e+001 1.135313607e+001 1.2e-011 3.76 105 1.7e-008 3.0e-003 1.2e-006 9.98e-001 1.135308795e+001 1.135313477e+001 1.1e-011 3.81 106 1.6e-008 2.7e-003 1.1e-006 1.02e+000 1.135309169e+001 1.135313349e+001 9.9e-012 3.84 107 1.4e-008 2.4e-003 9.8e-007 1.00e+000 1.135309483e+001 1.135313244e+001 8.9e-012 3.87 108 1.3e-008 2.2e-003 8.8e-007 9.99e-001 1.135309765e+001 1.135313150e+001 8.0e-012 3.92 109 1.1e-008 1.9e-003 7.9e-007 1.01e+000 1.135310028e+001 1.135313061e+001 7.2e-012 3.95 110 1.6e-009 2.0e-004 8.2e-008 9.96e-001 1.135312071e+001 1.135312383e+001 7.6e-013 3.98 Interior-point optimizer terminated. Time: 3.98. Optimizer terminated. Time: 4.01 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1353120709e+001 Viol. con: 3e-008 var: 0e+000 Dual. obj: 1.1353123831e+001 Viol. con: 0e+000 var: 2e-003 * End solution on dual form. * Transforming to primal solution. Solving took 4.03 seconds. result packing took 6.8% of solve time solution checking took 1.9% of solve time 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. * Computer Platform : Windows/64-X86 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. Total number of eliminations : 1010 Eliminator terminated. Eliminator started. Total number of eliminations : 1022 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1022 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 : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 831 Optimizer - Cones : 0 Optimizer - Scalar variables : 3581 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 : 1.67e+004 after factor : 1.72e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.288985035e+005 2.000000000e+000 1.0e+000 0.11 1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265799433e+005 3.775575030e+000 4.6e-001 0.16 2 3.8e+002 4.9e+002 2.1e+004 -9.34e-001 -1.194833585e+005 1.178222162e+001 1.7e-001 0.20 3 2.8e+002 3.6e+002 1.6e+004 -8.24e-001 -1.156680190e+005 1.068050796e+002 1.2e-001 0.25 4 2.8e+002 3.6e+002 1.5e+004 -7.56e-001 -1.123101100e+005 2.781216341e+003 1.2e-001 0.28 5 7.6e+001 9.8e+001 4.2e+003 -7.45e-001 -7.369370619e+004 1.086779369e+004 3.3e-002 0.34 6 3.6e+001 4.7e+001 2.0e+003 -1.88e-001 -4.546681680e+004 1.112170247e+004 1.6e-002 0.38 7 2.0e+001 2.6e+001 1.1e+003 3.02e-001 -2.909690548e+004 7.248066992e+003 9.0e-003 0.41 8 9.7e+000 1.3e+001 5.4e+002 5.97e-001 -1.524966141e+004 3.925529133e+003 4.3e-003 0.44 9 4.3e+000 5.6e+000 2.4e+002 8.22e-001 -6.824812249e+003 2.126890598e+003 1.9e-003 0.48 10 1.6e+000 2.1e+000 9.0e+001 9.39e-001 -2.382018991e+003 9.940758961e+002 7.2e-004 0.52 11 1.1e+000 1.5e+000 6.3e+001 9.88e-001 -1.660108723e+003 6.956310872e+002 5.0e-004 0.55 12 7.8e-001 1.0e+000 4.4e+001 9.83e-001 -1.186246607e+003 4.998444489e+002 3.5e-004 0.58 13 5.9e-001 7.7e-001 3.3e+001 9.85e-001 -8.730305623e+002 3.883188572e+002 2.6e-004 0.61 14 2.1e-001 2.9e-001 1.2e+001 9.89e-001 -3.245170687e+002 1.424684703e+002 9.8e-005 0.66 15 8.9e-002 1.4e-001 5.1e+000 1.01e+000 -1.284348155e+002 6.667981455e+001 4.2e-005 0.69 16 3.5e-002 9.9e-002 2.1e+000 1.01e+000 -4.749299954e+001 3.075570524e+001 1.7e-005 0.72 17 2.9e-002 8.4e-002 1.7e+000 9.96e-001 -3.703524508e+001 2.753513659e+001 1.4e-005 0.77 18 1.8e-002 6.6e-002 1.0e+000 1.01e+000 -1.901829238e+001 2.024511273e+001 8.5e-006 0.80 19 1.5e-002 5.7e-002 8.8e-001 1.02e+000 -1.416260061e+001 1.901457702e+001 7.2e-006 0.83 20 5.4e-003 6.6e-002 3.2e-001 1.02e+000 2.106659148e+000 1.405586790e+001 2.6e-006 0.86 21 1.8e-003 7.8e-002 1.1e-001 1.02e+000 8.170171793e+000 1.230683790e+001 9.7e-007 0.89 22 1.3e-003 6.0e-002 8.3e-002 9.63e-001 8.936995317e+000 1.202328710e+001 7.2e-007 0.94 23 4.8e-004 6.6e-002 3.1e-002 9.59e-001 1.040638979e+001 1.160345172e+001 2.8e-007 0.97 24 1.9e-004 6.2e-002 1.3e-002 9.58e-001 1.093939121e+001 1.142612395e+001 1.1e-007 1.00 25 1.7e-004 5.7e-002 1.1e-002 9.76e-001 1.097690673e+001 1.141479074e+001 1.0e-007 1.03 26 1.5e-004 5.2e-002 1.0e-002 9.75e-001 1.101084760e+001 1.140546126e+001 9.2e-008 1.08 27 1.4e-004 4.7e-002 9.2e-003 9.76e-001 1.104378850e+001 1.139945345e+001 8.3e-008 1.11 28 1.2e-004 4.3e-002 8.3e-003 9.78e-001 1.107352313e+001 1.139406142e+001 7.5e-008 1.14 29 1.1e-004 3.9e-002 7.5e-003 9.80e-001 1.110028341e+001 1.138913496e+001 6.7e-008 1.17 30 9.9e-005 3.6e-002 6.7e-003 9.82e-001 1.112431784e+001 1.138458868e+001 6.1e-008 1.22 31 8.9e-005 3.3e-002 6.0e-003 9.83e-001 1.114589638e+001 1.138039224e+001 5.5e-008 1.25 32 8.0e-005 3.1e-002 5.4e-003 9.85e-001 1.116526428e+001 1.137651903e+001 4.9e-008 1.28 33 7.2e-005 2.8e-002 4.9e-003 9.86e-001 1.118264432e+001 1.137294586e+001 4.4e-008 1.33 34 6.5e-005 2.6e-002 4.4e-003 9.88e-001 1.119823796e+001 1.136965147e+001 4.0e-008 1.36 35 5.8e-005 2.4e-002 4.0e-003 9.89e-001 1.121222748e+001 1.136661683e+001 3.6e-008 1.39 36 5.2e-005 2.3e-002 3.6e-003 9.90e-001 1.122477718e+001 1.136382403e+001 3.2e-008 1.44 37 4.7e-005 2.1e-002 3.2e-003 9.91e-001 1.123603528e+001 1.136125678e+001 2.9e-008 1.47 38 4.3e-005 2.0e-002 2.9e-003 9.92e-001 1.124613473e+001 1.135889922e+001 2.6e-008 1.48 39 3.8e-005 1.8e-002 2.6e-003 9.92e-001 1.125519512e+001 1.135673666e+001 2.4e-008 1.51 40 3.4e-005 1.7e-002 2.3e-003 9.93e-001 1.126332350e+001 1.135475474e+001 2.1e-008 1.54 41 3.1e-005 1.6e-002 2.1e-003 9.94e-001 1.127061608e+001 1.135294015e+001 1.9e-008 1.58 42 2.8e-005 1.5e-002 1.9e-003 9.94e-001 1.127715917e+001 1.135128024e+001 1.7e-008 1.61 43 2.5e-005 1.5e-002 1.7e-003 9.95e-001 1.128303048e+001 1.134976350e+001 1.5e-008 1.62 44 2.3e-005 1.4e-002 1.5e-003 9.96e-001 1.128829978e+001 1.134837915e+001 1.4e-008 1.65 45 2.0e-005 1.3e-002 1.4e-003 9.96e-001 1.129302968e+001 1.134711718e+001 1.3e-008 1.69 46 1.8e-005 1.3e-002 1.2e-003 9.96e-001 1.129727615e+001 1.134596799e+001 1.1e-008 1.72 47 1.6e-005 1.2e-002 1.1e-003 9.97e-001 1.130108924e+001 1.134492256e+001 1.0e-008 1.73 48 1.5e-005 1.2e-002 1.0e-003 9.97e-001 1.130451373e+001 1.134397243e+001 9.1e-009 1.76 49 1.3e-005 1.1e-002 9.1e-004 9.97e-001 1.130758970e+001 1.134310965e+001 8.2e-009 1.79 50 1.2e-005 1.1e-002 8.2e-004 9.98e-001 1.131035303e+001 1.134232678e+001 7.4e-009 1.83 51 1.1e-005 1.0e-002 7.4e-004 9.98e-001 1.131283587e+001 1.134161695e+001 6.7e-009 1.84 52 9.7e-006 1.0e-002 6.6e-004 9.98e-001 1.131506697e+001 1.134097382e+001 6.0e-009 1.87 53 8.8e-006 9.7e-003 6.0e-004 9.98e-001 1.131707208e+001 1.134039137e+001 5.4e-009 1.90 54 7.9e-006 9.5e-003 5.4e-004 9.99e-001 1.131887429e+001 1.133986423e+001 4.9e-009 1.94 55 7.1e-006 9.2e-003 4.8e-004 9.99e-001 1.132049425e+001 1.133938726e+001 4.4e-009 1.97 56 6.4e-006 9.0e-003 4.4e-004 9.99e-001 1.132195051e+001 1.133895590e+001 3.9e-009 1.98 57 5.7e-006 8.8e-003 3.9e-004 9.99e-001 1.132325966e+001 1.133856592e+001 3.5e-009 2.01 58 5.2e-006 8.7e-003 3.5e-004 9.99e-001 1.132443662e+001 1.133821342e+001 3.2e-009 2.04 59 4.7e-006 8.5e-003 3.2e-004 9.99e-001 1.132549477e+001 1.133789486e+001 2.9e-009 2.08 60 4.2e-006 8.4e-003 2.9e-004 9.99e-001 1.132644617e+001 1.133760698e+001 2.6e-009 2.11 61 3.8e-006 8.2e-003 2.6e-004 9.99e-001 1.132730162e+001 1.133734700e+001 2.3e-009 2.14 62 3.4e-006 8.1e-003 2.3e-004 9.99e-001 1.132807085e+001 1.133711223e+001 2.1e-009 2.17 63 3.1e-006 8.0e-003 2.1e-004 1.00e+000 1.132876264e+001 1.133690029e+001 1.9e-009 2.20 64 2.7e-006 7.9e-003 1.9e-004 1.00e+000 1.132938484e+001 1.133670899e+001 1.7e-009 2.23 65 2.5e-006 7.8e-003 1.7e-004 1.00e+000 1.132994449e+001 1.133653648e+001 1.5e-009 2.26 66 2.2e-006 7.8e-003 1.5e-004 1.00e+000 1.133044793e+001 1.133638091e+001 1.4e-009 2.29 67 2.0e-006 7.7e-003 1.4e-004 9.99e-001 1.133090082e+001 1.133624074e+001 1.2e-009 2.34 68 1.8e-006 7.6e-003 1.2e-004 1.00e+000 1.133130829e+001 1.133611438e+001 1.1e-009 2.37 69 1.6e-006 7.6e-003 1.1e-004 1.00e+000 1.133167491e+001 1.133600051e+001 1.0e-009 2.40 70 1.5e-006 7.5e-003 1.0e-004 1.00e+000 1.133200479e+001 1.133589791e+001 9.0e-010 2.43 71 1.3e-006 7.4e-003 9.0e-005 1.00e+000 1.133230162e+001 1.133580551e+001 8.1e-010 2.46 72 1.2e-006 7.4e-003 8.1e-005 1.00e+000 1.133256873e+001 1.133572226e+001 7.3e-010 2.50 73 1.1e-006 7.4e-003 7.3e-005 1.00e+000 1.133280909e+001 1.133564729e+001 6.6e-010 2.53 74 9.6e-007 7.3e-003 6.5e-005 9.99e-001 1.133302535e+001 1.133557987e+001 5.9e-010 2.56 75 8.6e-007 7.3e-003 5.9e-005 1.00e+000 1.133322000e+001 1.133551907e+001 5.3e-010 2.59 76 7.8e-007 7.2e-003 5.3e-005 1.00e+000 1.133339516e+001 1.133546435e+001 4.8e-010 2.62 77 7.0e-007 7.2e-003 4.8e-005 1.00e+000 1.133355279e+001 1.133541506e+001 4.3e-010 2.65 78 6.3e-007 7.2e-003 4.3e-005 1.00e+000 1.133369464e+001 1.133537070e+001 3.9e-010 2.68 79 5.7e-007 7.2e-003 3.9e-005 1.00e+000 1.133382230e+001 1.133533076e+001 3.5e-010 2.71 80 5.1e-007 7.1e-003 3.5e-005 1.00e+000 1.133393718e+001 1.133529483e+001 3.1e-010 2.76 81 4.6e-007 7.1e-003 3.1e-005 1.00e+000 1.133404058e+001 1.133526242e+001 2.8e-010 2.79 82 4.1e-007 7.1e-003 2.8e-005 1.00e+000 1.133413363e+001 1.133523325e+001 2.5e-010 2.82 83 3.7e-007 7.1e-003 2.5e-005 1.00e+000 1.133421737e+001 1.133520699e+001 2.3e-010 2.86 84 3.3e-007 7.1e-003 2.3e-005 1.00e+000 1.133429272e+001 1.133518338e+001 2.1e-010 2.89 85 3.0e-007 7.0e-003 2.1e-005 9.99e-001 1.133436053e+001 1.133516215e+001 1.9e-010 2.93 86 2.7e-007 7.0e-003 1.8e-005 1.00e+000 1.133442155e+001 1.133514302e+001 1.7e-010 2.96 87 2.4e-007 7.0e-003 1.7e-005 1.00e+000 1.133447647e+001 1.133512580e+001 1.5e-010 3.00 88 2.2e-007 7.0e-003 1.5e-005 1.00e+000 1.133452589e+001 1.133511030e+001 1.4e-010 3.04 89 2.0e-007 7.0e-003 1.3e-005 9.99e-001 1.133457036e+001 1.133509636e+001 1.2e-010 3.07 90 1.8e-007 7.0e-003 1.2e-005 1.00e+000 1.133461039e+001 1.133508376e+001 1.1e-010 3.11 91 1.6e-007 7.0e-003 1.1e-005 1.00e+000 1.133464645e+001 1.133507240e+001 9.9e-011 3.14 92 1.4e-007 7.0e-003 9.8e-006 9.98e-001 1.133467885e+001 1.133506225e+001 8.9e-011 3.17 93 1.3e-007 6.9e-003 8.8e-006 1.00e+000 1.133470802e+001 1.133505308e+001 8.0e-011 3.20 94 1.2e-007 6.2e-003 8.0e-006 1.00e+000 1.133473438e+001 1.133504476e+001 7.2e-011 3.23 95 1.0e-007 5.6e-003 7.2e-006 9.97e-001 1.133475798e+001 1.133503737e+001 6.5e-011 3.25 96 9.4e-008 5.1e-003 6.4e-006 1.00e+000 1.133477923e+001 1.133503068e+001 5.8e-011 3.28 97 8.5e-008 4.6e-003 5.8e-006 1.00e+000 1.133479840e+001 1.133502463e+001 5.3e-011 3.31 98 7.6e-008 4.1e-003 5.2e-006 9.96e-001 1.133481560e+001 1.133501925e+001 4.7e-011 3.34 99 6.9e-008 3.7e-003 4.7e-006 1.00e+000 1.133483108e+001 1.133501437e+001 4.3e-011 3.37 100 6.2e-008 3.3e-003 4.2e-006 1.00e+000 1.133484508e+001 1.133500995e+001 3.8e-011 3.38 101 5.6e-008 3.0e-003 3.8e-006 9.98e-001 1.133485761e+001 1.133500601e+001 3.4e-011 3.42 102 5.0e-008 2.7e-003 3.4e-006 1.00e+000 1.133486895e+001 1.133500242e+001 3.1e-011 3.45 103 4.5e-008 2.4e-003 3.1e-006 1.00e+000 1.133487910e+001 1.133499922e+001 2.8e-011 3.48 104 4.1e-008 2.2e-003 2.8e-006 9.98e-001 1.133488823e+001 1.133499635e+001 2.5e-011 3.50 105 3.7e-008 2.0e-003 2.5e-006 1.01e+000 1.133489660e+001 1.133499369e+001 2.3e-011 3.51 106 3.3e-008 1.8e-003 2.2e-006 1.01e+000 1.133490421e+001 1.133499126e+001 2.0e-011 3.53 107 3.0e-008 1.6e-003 2.0e-006 1.00e+000 1.133491090e+001 1.133498914e+001 1.8e-011 3.54 108 2.7e-008 1.4e-003 1.8e-006 1.02e+000 1.133491729e+001 1.133498708e+001 1.7e-011 3.57 109 6.5e-009 2.7e-004 3.5e-007 9.76e-001 1.133496042e+001 1.133497394e+001 3.3e-012 3.59 110 1.8e-009 1.6e-005 2.0e-008 9.71e-001 1.133496988e+001 1.133497067e+001 2.3e-013 3.62 Interior-point optimizer terminated. Time: 3.62. Optimizer terminated. Time: 3.63 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1334969876e+001 Viol. con: 3e-008 var: 0e+000 Dual. obj: 1.1334970667e+001 Viol. con: 0e+000 var: 1e-004 * End solution on dual form. * Transforming to primal solution. Solving took 3.67 seconds. result packing took 47% of solve time solution checking took 1.9% of solve time Solving took 6 GP solves and 32.1 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 2418947.0039 force_pound * meter but the right hand side evaluated to 2375461.35935 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 32774.3705743 force_pound but the right hand side evaluated to 32399.999997 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116779 meter but the right hand side evaluated to 2.08160516082 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 1243582.02419 joule / kilogram but the right hand side evaluated to 1.56115190103 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 664761.445478 joule / kilogram but the right hand side evaluated to 0.667340201649 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 18.3998921652 meter but the right hand side evaluated to 16.3228924212 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 10.903626505094902 but the right hand side evaluated to 4.788858697202067 (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 10.019808134985984 but the right hand side evaluated to 4.788858683173327 (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 8.1449107530031 but the right hand side evaluated to 4.788858700579637 (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 18.362235801 meter but the right hand side evaluated to 18.1377250839 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 18.362235801 meter but the right hand side evaluated to 18.2420616751 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 0.2960343772447329 but the right hand side evaluated to 0.189738717699852 (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 0.23301904998793432 but the right hand side evaluated to 0.17434597917335243 (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 7.5632495058212985 but the right hand side evaluated to 4.730639831644189 (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 7.583099995521609 but the right hand side evaluated to 4.757852661899832 (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 42.015s OK Generating XML reports... Cloning into 'solar'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in d:\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-gapdnc Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\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-g41phb\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-sbzsl6 Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in d:\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-_ktbzv\wheels\fe\11\0a\2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e Successfully built gassolar grin 1.2.1 requires argparse>=1.1, which is not installed. Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\solar Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1) Requirement already satisfied: gpkitmodels in d:\jenkins\workspace\gplibrary_pr_models\mosek (from solar==0.0.0.0) (0.0.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in d:\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-3c70oc\wheels\9f\ae\a9\52e286ff9ea1428d6dd1e8c6df0d12b22c44363d9dcc1dd331 Successfully built solar grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: solar 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' Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 9 GP solves and 10.6 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 1.0624 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 1388463.0580 but bound is 600000.0000 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1248776.3208 but bound is 1000000.0000 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 82150.9611 but bound is 50000.0000 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 2.29645501 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194389 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 9 GP solves and 7.84 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 1.0624 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 1388463.0328 but bound is 600000.0000 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1248776.2981 but bound is 1000000.0000 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 82150.9611 but bound is 50000.0000 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 2.2964550096 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194348 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 28.2 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 1.2510 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 765970.5416 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.65/GustL.65_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.58/GustL.58_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.69/GustL.69_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.46/GustL.46_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.78/GustL.78_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.48/GustL.48_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.52/GustL.52_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.71/GustL.71_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.75/GustL.75_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.59/GustL.59_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.66/GustL.66_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.49/GustL.49_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.67/GustL.67_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.64/GustL.64_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.40/GustL.40_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.55/GustL.55_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.54/GustL.54_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.53/GustL.53_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.60/GustL.60_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.51/GustL.51_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.41/GustL.41_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.47/GustL.47_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.70/GustL.70_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.50/GustL.50_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.74/GustL.74_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.68/GustL.68_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.76/GustL.76_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.79/GustL.79_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.63/GustL.63_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.44/GustL.44_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.77/GustL.77_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.56/GustL.56_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.57/GustL.57_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.42/GustL.42_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.62/GustL.62_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.61/GustL.61_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.45/GustL.45_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.43/GustL.43_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.72/GustL.72_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.73/GustL.73_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 14.6 seconds. 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 1.1911 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 862671.9762 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.90/GustL.90_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.118/GustL.118_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.119/GustL.119_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.104/GustL.104_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.102/GustL.102_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.93/GustL.93_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.105/GustL.105_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.85/GustL.85_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.106/GustL.106_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.117/GustL.117_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.91/GustL.91_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.109/GustL.109_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.116/GustL.116_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.114/GustL.114_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.96/GustL.96_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.101/GustL.101_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.87/GustL.87_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.100/GustL.100_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.99/GustL.99_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.88/GustL.88_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.98/GustL.98_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.113/GustL.113_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.89/GustL.89_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.81/GustL.81_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.95/GustL.95_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.107/GustL.107_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.94/GustL.94_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.115/GustL.115_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.110/GustL.110_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.84/GustL.84_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.82/GustL.82_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.83/GustL.83_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.97/GustL.97_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.112/GustL.112_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.86/GustL.86_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.92/GustL.92_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.111/GustL.111_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.103/GustL.103_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.108/GustL.108_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.80/GustL.80_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 4.32 seconds. 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 1.1202 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 987087.3039 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 6269 variables. Solving took 6.04 seconds. 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 1.0863 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 1058302.4686 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 4.65 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 1.2510 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 765970.5393 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.65/GustL.65_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.58/GustL.58_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.69/GustL.69_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.46/GustL.46_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.78/GustL.78_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.48/GustL.48_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.52/GustL.52_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.71/GustL.71_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.75/GustL.75_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.59/GustL.59_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.66/GustL.66_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.49/GustL.49_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.67/GustL.67_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.64/GustL.64_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.40/GustL.40_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.55/GustL.55_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.54/GustL.54_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.53/GustL.53_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.60/GustL.60_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.51/GustL.51_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.41/GustL.41_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.47/GustL.47_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.70/GustL.70_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.50/GustL.50_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.74/GustL.74_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.68/GustL.68_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.76/GustL.76_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.79/GustL.79_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.63/GustL.63_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.44/GustL.44_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.77/GustL.77_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.56/GustL.56_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.57/GustL.57_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.42/GustL.42_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.62/GustL.62_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.61/GustL.61_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.45/GustL.45_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.43/GustL.43_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.72/GustL.72_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.73/GustL.73_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 18.3 seconds. 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 1.1911 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 862671.9762 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.90/GustL.90_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.118/GustL.118_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.119/GustL.119_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.104/GustL.104_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.102/GustL.102_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.93/GustL.93_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.105/GustL.105_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.85/GustL.85_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.106/GustL.106_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.117/GustL.117_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.91/GustL.91_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.109/GustL.109_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.116/GustL.116_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.114/GustL.114_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.96/GustL.96_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.101/GustL.101_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.87/GustL.87_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.100/GustL.100_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.99/GustL.99_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.88/GustL.88_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.98/GustL.98_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.113/GustL.113_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.89/GustL.89_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.81/GustL.81_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.95/GustL.95_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.107/GustL.107_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.94/GustL.94_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.115/GustL.115_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.110/GustL.110_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.84/GustL.84_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.82/GustL.82_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.83/GustL.83_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.97/GustL.97_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.112/GustL.112_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.86/GustL.86_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.92/GustL.92_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.111/GustL.111_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.103/GustL.103_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.108/GustL.108_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.80/GustL.80_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 4.4 seconds. 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 1.1202 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 987087.2997 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 6269 variables. Solving took 2.57 seconds. 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 1.0863 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 1058302.4686 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 9 GP solves and 57.4 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 1.0624 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 1388463.0503 but bound is 600000.0000 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1248776.3139 but bound is 1000000.0000 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 82150.9611 but bound is 50000.0000 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 2.29645500986 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194375 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 9 GP solves and 11.3 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 1.0624 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 1388463.0483 but bound is 600000.0000 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1248776.3121 but bound is 1000000.0000 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 82150.9611 but bound is 50000.0000 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 2.29645500987 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194376 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 702 variables. Solving took 1.09 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 1.1958 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 838075.6758 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 8 GP solves and 21.8 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 1.1418 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 1017215.9408 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 78650.4124 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 2.62125883059 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124747973 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00043%) 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 1.95293542213 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215303 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00068%) 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 1.04275941614 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521709 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0004%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(3... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.467698134225 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697003887 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00024%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(4... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.13900679193 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006573775 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%) Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]' Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek_cli' Solving for 702 variables. Solving took 34.9 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 1.1958 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 838072.5912 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 8 GP solves and 52.6 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 1.1418 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 1017215.9574 but bound is 600000.0000 Warning: Constraint [dQ_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2,) [N... >= B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2,)*G_M...] is not tight because the left hand side evaluated to 0.546199983583 meter * newton but the right hand side evaluated to 0.54619937481 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 78650.5577 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 2.62125881924 meter ** 2 / second ** 2 but the right hand side evaluated to 2.6212478085 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00042%) 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 1.9529359766 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292347375 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00064%) 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 1.04275932764 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275522741 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00039%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(3... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.467698058867 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697044815 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00022%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(4... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.13900678254 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006562766 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%) Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monom Running tests... ---------------------------------------------------------------------- ..D:\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) D:\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 [29.168s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "d:\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 "d:\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 "d:\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 "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 83, in __init__ CostedConstraintSet.__init__(self, cost, constraints, substitutions) File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__ ConstraintSet.__init__(self, constraints, subs) File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__ list.__setitem__(self, i, ConstraintSet(constraint)) File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__ raise_elementhasnumpybools(constraint) File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 357, in raise_elementhasnumpybools % (cause, constraint)) ValueError: An ArrayConstraint was created with elements of numpy.bool_ Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])] ====================================================================== ERROR [92.927s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "d:\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 "d:\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 "d:\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 "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 83, in __init__ CostedConstraintSet.__init__(self, cost, ial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]' constraints, substitutions) File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__ ConstraintSet.__init__(self, constraints, subs) File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__ list.__setitem__(self, i, ConstraintSet(constraint)) File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__ raise_elementhasnumpybools(constraint) File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 357, in raise_elementhasnumpybools % (cause, constraint)) ValueError: An ArrayConstraint was created with elements of numpy.bool_ Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])] ---------------------------------------------------------------------- Ran 8 tests in 896.402s FAILED (errors=2) Generating XML reports... Cloning into 'gplibrary'... Checking out files: 93% (124/132) Checking out files: 94% (125/132) Checking out files: 95% (126/132) Checking out files: 96% (127/132) Checking out files: 97% (129/132) Checking out files: 98% (130/132) Checking out files: 99% (131/132) Checking out files: 100% (132/132) Checking out files: 100% (132/132), done. Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in d:\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-nwvbuu Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\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-osgcqj\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gplibrary Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in d:\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-_h_l8f\wheels\4a\da\60\bea5372bf288606a399bdc749979f532f5aff24f4c362a9887 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 0.04 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.296 seconds. Using solver 'mosek' Solving for 9 variables. Solving took 0.051 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.027 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.021 seconds. Beginning signomial solve. Solving took 16 GP solves and 5.62 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 100.006556021 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 985.544371504 meter * revolutions_per_minute but the right hand side evaluated to 103.04140943 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 0.420585924901 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573144841 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 0.314645033948 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629895185 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 0.168936438403 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931603968 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 0.0639642380825 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631379949 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 0.0226356535418 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354005867 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%) Using solver 'mosek_cli' Solving for 9 variables. Solving took 0.122 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.088 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.088 seconds. Beginning signomial solve. Solving took 16 GP solves and 5.52 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 985.544539109 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 0.420585903433 meter ** 2 / second ** 2 but the right hand side evaluated to 0.42057303321 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 0.314644998908 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629685653 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 0.063964051843 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639630073546 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0016%) 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 0.019 seconds. Beginning signomial solve. Solving took 11 GP solves and 2.6 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 1619897.4194 but bound is 700000.0000 Using solver 'mosek_cli' Solving for 13 variables. Solving took 0.098 seconds. Beginning signomial solve. Solving took 11 GP solves and 6.68 seconds. Warning: Constraint [omega_BladeElementProp/BladeElementPerf_(0,)*r_BladeElementProp/BladeElementPerf_(0,) [m*rpm]... >= Wt_BladeElementProp/BladeElementPerf_(0,) + vt_BladeElementProp/BladeElementPerf_(0,) [m/s]...] is not tight because the left hand side evaluated to 147.268875342 meter * revolutions_per_minute but the right hand side evaluated to 15.4219435408 meter / second (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [dQ_BladeElementProp/BladeElementPerf_(3,) [N*m]... >= B_BladeElementProp/BladeElementPerf_(3,)*G_BladeElementProp/BladeElementPerf_(3,)*Wa_BladeElementPro...] is not tight because the left hand side evaluated to 42.7884411703 meter * newton but the right hand side evaluated to 42.7884887635 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%) 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: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3481 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9721 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3856 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9562 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 1884891.2729 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 29.929s OK Generating XML reports... Cloning into 'eVTOL'... adding test for 'aircraft_models.py' Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 3.528s 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) D:\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 'D:\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