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Started by upstream project "gplibrary_PR_Models" build number 94 originally caused by: GitHub pull request #169 of commit d057fc54b0626b10dd6fdfee52a83746da2e48ee, no merge conflicts. GitHub pull request #169 of commit d057fc54b0626b10dd6fdfee52a83746da2e48ee, no merge conflicts. Building remotely on windows10x64 in workspace C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > C:\Program Files\Git\cmd\git init C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > C:\Program Files\Git\cmd\git --version # timeout=10 > C:\Program Files\Git\cmd\git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* > C:\Program Files\Git\cmd\git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 > C:\Program Files\Git\cmd\git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10 > C:\Program Files\Git\cmd\git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > C:\Program Files\Git\cmd\git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master Merging Revision c93bb9e622d1f8dbc3f0371ffe91258327ee398f (refs/remotes/origin/pr/169/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='default', fastForwardMode='--ff'} > C:\Program Files\Git\cmd\git rev-parse "origin/master^{commit}" # timeout=10 > C:\Program Files\Git\cmd\git config core.sparsecheckout # timeout=10 > C:\Program Files\Git\cmd\git checkout -f origin/master # timeout=3 > C:\Program Files\Git\cmd\git merge --ff c93bb9e622d1f8dbc3f0371ffe91258327ee398f # timeout=10 > C:\Program Files\Git\cmd\git rev-parse "HEAD^{commit}" # timeout=10 Seen branch in repository origin/1682literate Seen branch in repository origin/1682master Seen branch in repository origin/Breakdown Seen branch in repository origin/SPaircraft Seen branch in repository origin/aerosurf Seen branch in repository origin/atmosphere Seen branch in repository origin/boundj Seen 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remote branches > C:\Program Files\Git\cmd\git show-ref --tags -d # timeout=10 Checking out Revision c93bb9e622d1f8dbc3f0371ffe91258327ee398f (origin/pr/169/merge, origin/master) > C:\Program Files\Git\cmd\git config core.sparsecheckout # timeout=10 > C:\Program Files\Git\cmd\git checkout -f 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 [windows10x64] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [windows10x64] is in [[windows10x64, windows7x64]] Run condition [Execution node ] enabling perform for step [Execute Windows batch command] [mosek] $ cmd /c call C:\Users\jenkins\AppData\Local\Temp\jenkins2218686175702308949.bat C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>echo C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\cmd;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\cmd;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM turn on the anaconda console C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>call activate.bat || exit /b 666 (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM Create a virtualenv to install everything into (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>SET VENV=C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>virtualenv --system-site-packages C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit || exit /b 666 New python executable in C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts\python.exe Installing setuptools, pip, wheel...done. (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>call C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts\activate.bat || exit /b 666 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set PATH=C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts;C:\Anaconda2;C:\Anaconda2\Library\mingw-w64\bin;C:\Anaconda2\Library\usr\bin;C:\Anaconda2\Library\bin;C:\Anaconda2\Scripts;C:\Anaconda2\bin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\cmd;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM set PATH=C:\mingw-w64\x86_64-7.3.0-posix-seh-rt_v5-rev0\mingw64\bin;C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\Scripts;C:\Anaconda2;C:\Anaconda2\Library\mingw-w64\bin;C:\Anaconda2\Library\usr\bin;C:\Anaconda2\Library\bin;C:\Anaconda2\Scripts;C:\Anaconda2\bin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\cmd;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>gcc --version || exit /b 666 gcc (x86_64-posix-seh-rev0, Built by MinGW-W64 project) 6.4.0 Copyright (C) 2017 Free Software Foundation, Inc. This is free software; see the source for copying conditions. There is NO warranty; not even for MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM upgdade pip (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>python -m pip install --upgrade pip || exit /b 666 Requirement already up-to-date: pip in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (10.0.1) grin 1.2.1 requires argparse>=1.1, which is not installed. (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM Install coverage into the virtualenv to the coverage command blow uses the virtualenv python (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>pip install --upgrade coverage || exit /b 666 Requirement already up-to-date: coverage in c:\anaconda2\lib\site-packages (4.5.1) grin 1.2.1 requires argparse>=1.1, which is not installed. (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>SET GPKITBUILD=C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\build_gpkit (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>if mosek == cvxopt ( pip install --upgrade cvxopt || exit /b 666 set GPKITSOLVERS=cvxopt ) (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>if mosek == mosek ( msktestlic || exit /b 666 python -c "__import__('mosek').Env()" || exit /b 666 set GPKITSOLVERS=mosek, mosek_cli ) Problem Name : Objective sense : min Type : LO (linear optimization problem) Constraints : 1 Cones : 0 Scalar variables : 5000 Matrix variables : 0 Integer variables : 0 Optimizer started. Mosek license manager: License path: C:\Users\jenkins\mosek\mosek.lic Mosek license manager: Checkout license feature 'PTS' from flexlm. Mosek license manager: Checkout time 0.03. r: 0 status: 0 Interior-point optimizer started. Presolve started. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 1 time : 0.00 Lin. dep. - tries : 0 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.03 ************************************ A license was checked out correctly. ************************************ (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>dir C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\build_gpkit Volume in drive C has no label. Volume Serial Number is C4C9-8F11 Directory of C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek File Not Found (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import scipy; print scipy.__version__" || exit /b 666 1.0.1 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import numpy; print numpy.__version__" || exit /b 666 1.14.3 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "import pint; print pint.__version__" || exit /b 666 0.8.1 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM Install gpkit to run the documentation examples (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>git clone --depth 1 https://github.com/convexengineering/gpkit.git || exit /b 666 Cloning into 'gpkit'... (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>pip install -e C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\gpkit || exit /b 666 Obtaining file:///C:/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit Requirement already satisfied: numpy>=1.12.1 in c:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.14.3) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (0.8.1) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.0.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.3.2) grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gpkit Running setup.py develop for gpkit Successfully installed gpkit (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>pip install -e C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek || exit /b 666 Obtaining file:///C:/Users/jenkins/workspace/gplibrary_PR_Models/mosek Requirement already satisfied: numpy>=1.12 in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1) grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gpkitmodels Running setup.py develop for gpkitmodels Successfully installed gpkitmodels (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM Show the settings file (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>type C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\gpkit\gpkit\env\settings installed_solvers : mosek, mosek_cli mosek_bin_dir : C:\Program Files\Mosek\8\tools\platform\win64x86\bin (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>REM Limit number of threads that be can used (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set MSK_IPAR_NUM_THREADS=2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set MKL_NUM_THREADS=2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set NUMEXPR_NUM_THREADS=2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set OPENBLAS_NUM_THREADS=2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>set OMP_NUM_THREADS=2 (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)" Obtaining file:///C:/Users/jenkins/workspace/gplibrary_PR_Models/mosek Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Cloning into 'shopping'... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.065 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.036 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.153 seconds. Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 0.834s OK Generating XML reports... Cloning into 'gassolar'... 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Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-blmgrh Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-re5xi0\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 c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gassolar Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in c:\users\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 c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0) Building wheels for collected packages: gassolar Running setup.py bdist_wheel for gassolar: started Running setup.py bdist_wheel for gassolar: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-4kc_5h\wheels\5c\45\ee\a8ea86f24e24acb4b8a5b5ef8c1a921fb70526d25cb0d4c0da 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 0.593 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 3.52 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 0.389 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 2.09 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 0.467 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1528 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.1347 but bound is 150000.0000 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 5.16 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0523 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.9089 but bound is 150000.0000 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 0.826 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 4.55 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134552.5355 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.8810 but bound is 150000.0000 Running tests... ---------------------------------------------------------------------- ..C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 4 tests in 68.103s OK Generating XML reports... Cloning into 'jho'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-qkkvjt Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-0lt1ig\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -7.870895775419218e-14. Allowing negative dual variable(s) as small as -7.282889569193429e-14. Allowing negative dual variable(s) as small as -1.3029226135496952e-13. Allowing negative dual variable(s) as small as -1.3197808731296723e-13. Solving took 4 GP solves and 4.79 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -7.370525630795433e-14. Allowing negative dual variable(s) as small as -7.875698791043328e-14. Allowing negative dual variable(s) as small as -1.2989978016852977e-13. Allowing negative dual variable(s) as small as -1.2660586554830155e-13. Solving took 4 GP solves and 5.96 seconds. Allowing negative dual variable(s) as small as -5.833194170745681e-13. Allowing negative dual variable(s) as small as -3.4073395147049546e-13. Allowing negative dual variable(s) as small as -1.0226303311100526e-12. Allowing negative dual variable(s) as small as -1.022749159668157e-12. Allowing negative dual variable(s) as small as -2.788347894591703e-13. Allowing negative dual variable(s) as small as -1.1548276169972421e-12. Allowing negative dual variable(s) as small as -1.116416095854611e-12. Allowing negative dual variable(s) as small as -1.1164025704325092e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -1.2092699346218094e-12. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -6.145438394806617e-11. Allowing negative dual variable(s) as small as -1.4547383708692844e-12. Allowing negative dual variable(s) as small as -6.4631940011494886e-12. Allowing negative dual variable(s) as small as -6.4686419617415615e-12. Solving took 4 GP solves and 5.06 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 2.22 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.83105612406154e-13. Allowing negative dual variable(s) as small as -3.3985141090209225e-13. Allowing negative dual variable(s) as small as -1.0221081793437836e-12. Allowing negative dual variable(s) as small as -1.0226264279822317e-12. Allowing negative dual variable(s) as small as -2.7669912801980834e-13. Allowing negative dual variable(s) as small as -1.1548964367301406e-12. Allowing negative dual variable(s) as small as -1.1157224233046548e-12. Allowing negative dual variable(s) as small as -1.116401242284848e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -1.2090882765478095e-12. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -6.145442006433343e-11. Allowing negative dual variable(s) as small as -1.4547318835101158e-12. Allowing negative dual variable(s) as small as -6.46326132831769e-12. Allowing negative dual variable(s) as small as -6.468984787461118e-12. Solving took 4 GP solves and 3.21 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 2.3 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 75.646s OK Generating XML reports... Cloning into 'turbofan'... Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\turbofan Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.8.1) Building wheels for collected packages: turbofan Running setup.py bdist_wheel for turbofan: started Running setup.py bdist_wheel for turbofan: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-b95ezt\wheels\3a\4a\df\1e137b486523078491de3a0319a07f314f5e9aa745dfaf6fd5 Successfully built turbofan grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: turbofan Successfully installed turbofan-0.0.0.0 adding test for 'turbofan/engine_validation.py' Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.752832 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 26232.8485059 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 3.395s 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-_txvzb Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.8.1) Building wheels for collected packages: turbofan Running setup.py bdist_wheel for turbofan: started Running setup.py bdist_wheel for turbofan: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-18gols\wheels\49\e6\3a\5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5 Successfully built turbofan grin 1.2.1 requires argparse>=1.1, which is not installed. adding test for 'SP_aircraft.py' Beginning signomial solve. Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 485 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.03 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3606 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 : 1.52e+004 after factor : 1.75e+005 Factor - dense dim. : 0 flops : 3.95e+007 Factor - GP saved nzs : -1.40e+005 GP saved flops : -3.84e+007 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.5e+003 1.2e+005 0.00e+000 -1.241488813e+005 2.000000000e+000 1.0e+000 0.08 1 1.5e+003 2.3e+003 8.0e+004 -9.71e-001 -1.230686685e+005 2.971062159e+000 6.4e-001 0.16 2 6.4e+002 1.0e+003 3.5e+004 -9.53e-001 -1.193008499e+005 6.575658302e+000 2.8e-001 0.22 3 2.9e+002 4.5e+002 1.6e+004 -8.91e-001 -1.118074281e+005 2.808647532e+001 1.3e-001 0.30 4 2.9e+002 4.5e+002 1.6e+004 -7.65e-001 -1.098743216e+005 1.714956975e+003 1.3e-001 0.36 5 1.0e+002 1.6e+002 5.5e+003 -7.58e-001 -8.115745614e+004 8.827687984e+003 4.5e-002 0.44 6 3.6e+001 5.7e+001 2.0e+003 -3.54e-001 -4.316773054e+004 1.174834799e+004 1.6e-002 0.52 7 1.6e+001 2.6e+001 9.0e+002 2.99e-001 -2.298771694e+004 6.536721980e+003 7.3e-003 0.59 8 8.0e+000 1.2e+001 4.3e+002 6.71e-001 -1.157926456e+004 3.817230704e+003 3.5e-003 0.67 9 3.6e+000 5.5e+000 1.9e+002 8.63e-001 -5.013718748e+003 2.102823988e+003 1.6e-003 0.81 10 1.8e+000 2.8e+000 1.0e+002 9.56e-001 -2.270020370e+003 1.453116933e+003 8.2e-004 0.89 11 6.7e-001 1.0e+000 3.7e+001 9.85e-001 -6.169520663e+002 7.675323015e+002 3.1e-004 0.95 12 5.7e-001 9.2e-001 3.2e+001 9.80e-001 -4.755430548e+002 7.121973807e+002 2.6e-004 1.03 13 4.2e-001 7.3e-001 2.3e+001 9.75e-001 -2.606708303e+002 6.225039195e+002 1.9e-004 1.09 14 2.1e-001 4.5e-001 1.2e+001 9.88e-001 4.354381180e+001 4.905757073e+002 9.7e-005 1.16 15 6.3e-002 1.9e-001 3.6e+000 1.00e+000 2.632162538e+002 3.980309947e+002 3.0e-005 1.22 16 1.9e-002 1.4e-001 1.1e+000 1.00e+000 3.277409384e+002 3.698760819e+002 9.5e-006 1.31 17 4.8e-003 1.4e-001 2.9e-001 1.00e+000 3.497761840e+002 3.605589737e+002 2.5e-006 1.38 18 2.8e-003 1.1e-001 1.7e-001 1.00e+000 3.528660001e+002 3.591632100e+002 1.4e-006 1.44 19 4.6e-004 1.7e-001 2.8e-002 1.00e+000 3.565842649e+002 3.576461463e+002 2.5e-007 1.58 20 1.7e-004 1.1e-001 1.1e-002 9.92e-001 3.570641830e+002 3.574615160e+002 9.2e-008 1.70 21 4.9e-005 1.1e-001 3.1e-003 1.00e+000 3.572657425e+002 3.573816690e+002 2.7e-008 1.78 22 3.1e-005 8.6e-002 2.0e-003 9.82e-001 3.572956725e+002 3.573692800e+002 1.7e-008 1.83 23 1.1e-005 8.1e-002 7.1e-004 9.72e-001 3.573294061e+002 3.573561297e+002 6.2e-009 1.89 24 5.3e-006 7.0e-002 3.3e-004 1.01e+000 3.573396609e+002 3.573521235e+002 2.9e-009 1.95 25 2.3e-006 6.9e-002 1.4e-004 1.00e+000 3.573447422e+002 3.573501395e+002 1.3e-009 2.03 26 2.1e-006 6.8e-002 1.3e-004 1.00e+000 3.573451411e+002 3.573499972e+002 1.1e-009 2.14 27 1.8e-006 6.2e-002 1.2e-004 1.00e+000 3.573454875e+002 3.573498578e+002 1.0e-009 2.20 28 1.7e-006 5.6e-002 1.0e-004 1.00e+000 3.573458004e+002 3.573497337e+002 9.2e-010 2.25 29 1.5e-006 5.1e-002 9.4e-005 1.00e+000 3.573460821e+002 3.573496220e+002 8.2e-010 2.31 30 1.3e-006 4.7e-002 8.4e-005 1.00e+000 3.573463356e+002 3.573495215e+002 7.4e-010 2.39 31 1.2e-006 4.2e-002 7.6e-005 1.00e+000 3.573465637e+002 3.573494310e+002 6.7e-010 2.53 32 1.1e-006 3.9e-002 6.8e-005 1.00e+000 3.573467689e+002 3.573493496e+002 6.0e-010 2.63 33 9.8e-007 3.6e-002 6.2e-005 1.00e+000 3.573469537e+002 3.573492763e+002 5.4e-010 2.67 34 8.8e-007 3.3e-002 5.5e-005 1.00e+000 3.573471199e+002 3.573492102e+002 4.9e-010 2.77 35 7.9e-007 3.0e-002 5.0e-005 1.00e+000 3.573472695e+002 3.573491510e+002 4.4e-010 2.91 36 7.1e-007 2.8e-002 4.5e-005 1.00e+000 3.573474041e+002 3.573490976e+002 3.9e-010 2.97 37 6.4e-007 2.6e-002 4.0e-005 1.00e+000 3.573475252e+002 3.573490494e+002 3.5e-010 3.05 38 5.8e-007 2.4e-002 3.6e-005 1.00e+000 3.573476343e+002 3.573490060e+002 3.2e-010 3.13 39 5.3e-007 2.2e-002 3.3e-005 1.00e+000 3.573477308e+002 3.573489719e+002 2.9e-010 3.19 40 6.6e-007 2.1e-002 3.2e-005 9.93e-001 3.573477611e+002 3.573489599e+002 2.8e-010 3.27 41 5.6e-007 1.9e-002 2.8e-005 9.98e-001 3.573478453e+002 3.573489278e+002 2.5e-010 3.33 42 4.8e-007 1.7e-002 2.6e-005 1.00e+000 3.573479243e+002 3.573488900e+002 2.2e-010 3.39 43 5.0e-007 1.7e-002 2.6e-005 8.36e-001 3.573479153e+002 3.573489127e+002 2.2e-010 3.45 44 4.5e-007 1.6e-002 2.3e-005 1.00e+000 3.573479830e+002 3.573488911e+002 2.0e-010 3.52 45 4.0e-007 1.5e-002 2.1e-005 1.00e+000 3.573480463e+002 3.573488633e+002 1.8e-010 3.58 46 3.6e-007 1.4e-002 1.9e-005 1.00e+000 3.573481031e+002 3.573488384e+002 1.6e-010 3.66 47 3.3e-007 1.3e-002 1.7e-005 1.00e+000 3.573481543e+002 3.573488161e+002 1.5e-010 3.72 48 3.0e-007 1.3e-002 1.7e-005 1.12e+000 3.573481536e+002 3.573488202e+002 1.5e-010 3.80 49 2.6e-007 1.3e-002 1.5e-005 1.00e+000 3.573481995e+002 3.573488000e+002 1.3e-010 3.86 50 2.4e-007 1.2e-002 1.4e-005 9.99e-001 3.573482411e+002 3.573487815e+002 1.2e-010 3.94 51 2.1e-007 1.2e-002 1.2e-005 1.00e+000 3.573482784e+002 3.573487648e+002 1.1e-010 4.00 52 3.0e-007 1.1e-002 1.1e-005 1.35e+000 3.573483038e+002 3.573487604e+002 9.8e-011 4.06 53 3.3e-007 1.0e-002 1.1e-005 9.93e-001 3.573483140e+002 3.573487771e+002 9.3e-011 4.16 54 3.4e-007 9.1e-003 9.6e-006 1.00e+000 3.573483442e+002 3.573487582e+002 8.4e-011 4.28 55 3.0e-007 8.8e-003 8.6e-006 1.00e+000 3.573483713e+002 3.573487436e+002 7.5e-011 4.34 56 2.8e-007 8.7e-003 8.5e-006 9.30e-001 3.573483744e+002 3.573487353e+002 7.5e-011 4.39 57 3.3e-007 8.7e-003 8.5e-006 1.17e+000 3.573483804e+002 3.573487141e+002 7.4e-011 4.47 58 3.3e-007 8.6e-003 8.3e-006 1.01e+000 3.573483848e+002 3.573487183e+002 7.2e-011 4.53 59 2.9e-007 8.4e-003 7.5e-006 1.01e+000 3.573484090e+002 3.573487079e+002 6.6e-011 4.59 60 6.9e-007 8.4e-003 7.5e-006 1.31e+000 3.573484047e+002 3.573487221e+002 6.5e-011 4.66 61 6.0e-007 8.4e-003 7.4e-006 1.45e+000 3.573484006e+002 3.573487429e+002 6.5e-011 4.73 62 5.3e-007 7.6e-003 6.7e-006 1.03e+000 3.573484244e+002 3.573487286e+002 5.9e-011 4.80 63 4.8e-007 7.3e-003 6.0e-006 1.00e+000 3.573484434e+002 3.573487184e+002 5.3e-011 4.84 64 4.3e-007 7.2e-003 5.4e-006 1.01e+000 3.573484609e+002 3.573487077e+002 4.8e-011 4.92 65 6.4e-007 7.0e-003 5.3e-006 8.99e-001 3.573484610e+002 3.573487309e+002 4.7e-011 4.98 66 6.5e-007 7.0e-003 5.3e-006 1.27e+000 3.573484610e+002 3.573487310e+002 4.7e-011 5.03 67 5.9e-007 6.9e-003 4.8e-006 1.00e+000 3.573484763e+002 3.573487195e+002 4.2e-011 5.09 68 5.3e-007 6.8e-003 4.3e-006 9.99e-001 3.573484901e+002 3.573487088e+002 3.8e-011 5.25 69 8.4e-007 6.8e-003 3.7e-006 1.00e+000 3.573485217e+002 3.573487088e+002 3.8e-011 5.33 70 1.2e-006 6.7e-003 6.5e-006 1.00e+000 3.573483781e+002 3.573487075e+002 3.7e-011 5.42 71 1.2e-006 6.7e-003 6.4e-006 1.00e+000 3.573483815e+002 3.573487075e+002 3.7e-011 5.50 72 1.2e-006 6.7e-003 6.4e-006 -4.95e+000 3.573483821e+002 3.573487067e+002 3.7e-011 5.59 73 1.3e-006 6.7e-003 6.4e-006 -3.34e-002 3.573483823e+002 3.573487062e+002 3.7e-011 5.67 74 1.2e-006 6.7e-003 6.4e-006 8.97e-001 3.573483821e+002 3.573487067e+002 3.7e-011 5.73 75 1.2e-006 6.7e-003 6.3e-006 1.06e+000 3.573483853e+002 3.573487121e+002 3.7e-011 5.80 76 2.4e-006 6.6e-003 6.2e-006 -5.74e+000 3.573483745e+002 3.573487378e+002 3.6e-011 5.84 77 2.4e-006 6.6e-003 6.2e-006 2.03e+000 3.573483755e+002 3.573487347e+002 3.6e-011 5.92 78 1.8e-006 6.4e-003 4.6e-006 -1.51e-001 3.573484389e+002 3.573487150e+002 2.7e-011 6.00 79 1.6e-006 6.1e-003 4.1e-006 1.01e+000 3.573484563e+002 3.573487079e+002 2.4e-011 6.11 80 2.3e-006 6.0e-003 4.0e-006 -3.43e+000 3.573484555e+002 3.573487273e+002 2.4e-011 6.20 81 1.6e-006 6.0e-003 4.0e-006 1.03e+000 3.573484576e+002 3.573487205e+002 2.3e-011 6.27 82 1.6e-006 5.9e-003 3.9e-006 1.01e+000 3.573484577e+002 3.573487426e+002 2.3e-011 6.33 83 1.6e-006 5.8e-003 3.9e-006 9.85e-001 3.573484591e+002 3.573487394e+002 2.3e-011 6.42 84 1.6e-006 5.7e-003 3.8e-006 9.69e-001 3.573484621e+002 3.573487525e+002 2.2e-011 6.55 85 1.3e-006 5.1e-003 3.4e-006 9.93e-001 3.573484763e+002 3.573487291e+002 2.0e-011 6.67 86 1.8e-006 5.1e-003 3.4e-006 1.01e+000 3.573484766e+002 3.573487350e+002 2.0e-011 6.78 87 7.1e-007 5.0e-003 3.4e-006 1.03e+000 3.573484797e+002 3.573487397e+002 1.9e-011 6.86 88 6.3e-007 4.5e-003 3.0e-006 1.05e+000 3.573484949e+002 3.573487166e+002 1.8e-011 6.94 89 5.6e-007 4.4e-003 2.7e-006 1.02e+000 3.573485078e+002 3.573487065e+002 1.6e-011 7.02 90 4.4e-007 4.4e-003 2.7e-006 -6.09e-001 3.573485078e+002 3.573487049e+002 1.6e-011 7.08 91 7.5e-007 4.4e-003 2.7e-006 3.83e-001 3.573485078e+002 3.573487042e+002 1.6e-011 7.14 92 7.9e-007 4.4e-003 2.7e-006 -2.66e+000 3.573485079e+002 3.573487001e+002 1.6e-011 7.20 93 8.0e-007 4.4e-003 2.7e-006 -1.25e+001 3.573485084e+002 3.573486935e+002 1.6e-011 7.27 94 8.2e-007 4.4e-003 2.7e-006 -3.50e+000 3.573485084e+002 3.573486936e+002 1.6e-011 7.33 95 7.7e-007 4.1e-003 2.5e-006 1.14e+000 3.573485199e+002 3.573486766e+002 1.6e-011 7.39 96 1.2e-006 3.8e-003 2.3e-006 1.10e+000 3.573485333e+002 3.573486745e+002 1.5e-011 7.45 97 1.2e-006 3.8e-003 2.3e-006 5.90e-001 3.573485341e+002 3.573486641e+002 1.5e-011 7.53 98 1.1e-006 3.4e-003 2.0e-006 1.32e+000 3.573485427e+002 3.573486535e+002 1.3e-011 7.61 99 9.8e-007 3.1e-003 1.8e-006 9.48e-001 3.573485506e+002 3.573486455e+002 1.2e-011 7.69 100 9.9e-007 3.1e-003 1.8e-006 -7.28e+001 3.573485506e+002 3.573486455e+002 1.2e-011 7.73 101 8.9e-007 2.8e-003 1.7e-006 1.04e+000 3.573485583e+002 3.573486408e+002 1.1e-011 7.80 102 1.0e-006 2.5e-003 9.0e-007 1.00e+000 3.573485931e+002 3.573486381e+002 9.6e-012 7.88 103 9.6e-007 2.2e-003 8.1e-007 1.05e+000 3.573485971e+002 3.573486414e+002 8.8e-012 7.94 104 9.6e-007 2.2e-003 8.1e-007 1.12e+000 3.573485971e+002 3.573486414e+002 8.8e-012 7.98 105 8.7e-007 2.0e-003 7.3e-007 1.06e+000 3.573485994e+002 3.573486382e+002 8.2e-012 8.05 106 9.1e-007 2.0e-003 3.5e-007 1.00e+000 3.573486198e+002 3.573486381e+002 8.2e-012 8.14 107 9.0e-007 2.0e-003 3.5e-007 -2.24e+000 3.573486205e+002 3.573486392e+002 8.2e-012 8.20 108 8.3e-007 1.8e-003 3.1e-007 1.00e+000 3.573486190e+002 3.573486354e+002 7.3e-012 8.28 109 1.2e-006 1.8e-003 1.0e-006 1.00e+000 3.573486884e+002 3.573486354e+002 7.3e-012 8.34 110 1.2e-006 1.8e-003 6.7e-007 1.00e+000 3.573486708e+002 3.573486354e+002 7.3e-012 8.48 111 1.1e-006 1.6e-003 6.0e-007 1.01e+000 3.573486650e+002 3.573486332e+002 6.6e-012 8.63 112 1.4e-006 1.6e-003 1.2e-006 1.00e+000 3.573486974e+002 3.573486332e+002 6.6e-012 8.69 113 1.3e-006 1.5e-003 1.0e-006 1.00e+000 3.573486856e+002 3.573486313e+002 6.0e-012 8.75 114 1.0e-006 1.5e-003 1.0e-006 1.25e+000 3.573486856e+002 3.573486313e+002 6.0e-012 8.83 115 1.2e-006 1.5e-003 1.0e-006 -3.82e+000 3.573486855e+002 3.573486313e+002 6.0e-012 8.91 116 1.1e-006 1.3e-003 9.3e-007 1.05e+000 3.573486852e+002 3.573486328e+002 5.5e-012 8.97 117 1.0e-006 1.2e-003 8.4e-007 9.96e-001 3.573486790e+002 3.573486314e+002 5.0e-012 9.05 118 1.2e-005 1.2e-003 8.4e-007 1.78e-001 3.573486790e+002 3.573486314e+002 5.0e-012 9.19 119 1.2e-005 1.2e-003 8.4e-007 -2.20e+000 3.573486790e+002 3.573486314e+002 5.0e-012 9.36 120 1.2e-005 1.2e-003 8.4e-007 1.97e+000 3.573486789e+002 3.573486313e+002 5.0e-012 9.52 121 1.2e-005 1.2e-003 7.3e-007 1.00e+000 3.573486727e+002 3.573486313e+002 5.0e-012 9.66 122 1.2e-005 1.2e-003 7.3e-007 9.09e-001 3.573486727e+002 3.573486313e+002 5.0e-012 9.80 123 1.1e-005 1.1e-003 6.5e-007 1.02e+000 3.573486777e+002 3.573486350e+002 4.5e-012 9.92 124 1.1e-005 1.1e-003 6.5e-007 1.00e+000 3.573486777e+002 3.573486350e+002 4.5e-012 10.05 Interior-point optimizer terminated. Time: 10.05. Optimizer terminated. Time: 10.08 solsta = 8, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : NEAR_OPTIMAL Primal. obj: 3.5734867768e+002 nrm: 9e+001 Viol. con: 5e-004 var: 0e+000 Dual. obj: 3.5734863504e+002 nrm: 8e+002 Viol. con: 0e+000 var: 2e-002 * End solution on dual form. * Transforming to primal solution. Solving took 10.1 seconds. final status of solver 'mosek' was 'NEAR_DUAL_FEAS', not 'optimal'. result packing took 3.8% of solve time solution checking took 1.3% of solve time Using solver 'mosek' Solving for 1899 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 487 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.03 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3607 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.05 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.53e+004 after factor : 1.76e+005 Factor - dense dim. : 0 flops : 3.97e+007 Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.234758051e+005 2.000000000e+000 1.0e+000 0.08 1 1.5e+003 2.0e+003 8.0e+004 -9.71e-001 -1.224173914e+005 2.927914582e+000 6.5e-001 0.16 2 7.1e+002 9.7e+002 3.8e+004 -9.53e-001 -1.192653277e+005 6.047815878e+000 3.1e-001 0.22 3 2.9e+002 4.0e+002 1.6e+004 -9.01e-001 -1.111484986e+005 2.515334720e+001 1.3e-001 0.28 4 2.9e+002 4.0e+002 1.6e+004 -7.65e-001 -1.092627606e+005 1.672591815e+003 1.3e-001 0.36 5 1.2e+002 1.6e+002 6.4e+003 -7.58e-001 -8.565015446e+004 7.659037230e+003 5.2e-002 0.42 6 3.5e+001 4.8e+001 1.9e+003 -4.31e-001 -4.091389451e+004 1.290804782e+004 1.5e-002 0.50 7 1.5e+001 2.1e+001 8.3e+002 3.29e-001 -2.129523539e+004 6.272293000e+003 6.8e-003 0.56 8 6.9e+000 9.4e+000 3.7e+002 7.04e-001 -1.003212542e+004 3.298450575e+003 3.1e-003 0.64 9 2.8e+000 3.8e+000 1.5e+002 8.93e-001 -3.935814771e+003 1.598514853e+003 1.2e-003 0.77 10 1.2e+000 1.6e+000 6.5e+001 9.75e-001 -1.631246894e+003 7.616915366e+002 5.3e-004 0.89 11 9.1e-001 1.3e+000 5.0e+001 9.87e-001 -1.230608704e+003 6.193640813e+002 4.1e-004 0.95 12 7.2e-001 1.2e+000 3.9e+001 9.70e-001 -9.738171406e+002 5.013920813e+002 3.2e-004 1.00 13 3.7e-001 6.4e-001 2.0e+001 9.91e-001 -4.737124511e+002 2.805087155e+002 1.7e-004 1.11 14 1.2e-001 2.4e-001 6.8e+000 9.98e-001 -1.373854541e+002 1.176221895e+002 5.7e-005 1.23 15 4.1e-002 1.3e-001 2.3e+000 1.00e+000 -2.387462325e+001 6.392426662e+001 2.0e-005 1.30 16 2.5e-002 9.2e-002 1.4e+000 1.00e+000 4.484421949e-002 5.311076669e+001 1.2e-005 1.36 17 1.6e-002 9.0e-002 9.3e-001 1.00e+000 1.225129072e+001 4.734729951e+001 7.9e-006 1.42 18 3.8e-003 1.3e-001 2.2e-001 1.00e+000 3.045516378e+001 3.887097545e+001 1.9e-006 1.50 19 2.1e-003 9.4e-002 1.2e-001 1.00e+000 3.309921921e+001 3.769671408e+001 1.1e-006 1.56 20 7.8e-004 9.4e-002 4.6e-002 1.00e+000 3.505592930e+001 3.679502796e+001 4.0e-007 1.63 21 2.3e-004 1.0e-001 1.4e-002 1.00e+000 3.589034343e+001 3.640883635e+001 1.2e-007 1.69 22 9.2e-005 8.9e-002 5.5e-003 1.00e+000 3.610335797e+001 3.630864562e+001 4.8e-008 1.75 23 8.3e-005 8.0e-002 4.9e-003 1.00e+000 3.611824491e+001 3.630300153e+001 4.3e-008 1.84 24 7.4e-005 7.3e-002 4.4e-003 1.00e+000 3.613073997e+001 3.629701223e+001 3.9e-008 1.91 25 6.7e-005 6.6e-002 4.0e-003 1.00e+000 3.614200671e+001 3.629164495e+001 3.5e-008 1.98 26 6.0e-005 6.0e-002 3.6e-003 1.00e+000 3.615213550e+001 3.628680430e+001 3.1e-008 2.05 27 5.4e-005 5.5e-002 3.2e-003 1.00e+000 3.616124930e+001 3.628244663e+001 2.8e-008 2.13 28 4.9e-005 5.0e-002 2.9e-003 1.00e+000 3.616944917e+001 3.627852301e+001 2.5e-008 2.19 29 4.4e-005 4.6e-002 2.6e-003 1.00e+000 3.617682722e+001 3.627499061e+001 2.3e-008 2.27 30 4.0e-005 4.2e-002 2.4e-003 1.00e+000 3.618346595e+001 3.627181051e+001 2.1e-008 2.33 31 3.6e-005 3.9e-002 2.1e-003 1.00e+000 3.618943962e+001 3.626894769e+001 1.9e-008 2.41 32 3.2e-005 3.6e-002 1.9e-003 1.00e+000 3.619481496e+001 3.626637058e+001 1.7e-008 2.48 33 2.9e-005 3.3e-002 1.7e-003 1.00e+000 3.619965201e+001 3.626405073e+001 1.5e-008 2.55 34 2.6e-005 3.0e-002 1.5e-003 1.00e+000 3.620400474e+001 3.626196251e+001 1.3e-008 2.61 35 2.3e-005 2.8e-002 1.4e-003 1.00e+000 3.620792171e+001 3.626008284e+001 1.2e-008 2.69 36 2.1e-005 2.6e-002 1.3e-003 1.00e+000 3.621144660e+001 3.625839091e+001 1.1e-008 2.77 37 1.9e-005 2.4e-002 1.1e-003 1.00e+000 3.621461868e+001 3.625686800e+001 9.8e-009 2.83 38 1.7e-005 2.2e-002 1.0e-003 1.00e+000 3.621747329e+001 3.625549722e+001 8.9e-009 2.89 39 1.5e-005 2.1e-002 9.1e-004 1.00e+000 3.622004222e+001 3.625426340e+001 8.0e-009 2.98 40 1.4e-005 1.9e-002 8.2e-004 1.00e+000 3.622235407e+001 3.625315285e+001 7.2e-009 3.05 41 1.2e-005 1.8e-002 7.4e-004 1.00e+000 3.622443457e+001 3.625215325e+001 6.5e-009 3.11 42 1.1e-005 1.7e-002 6.7e-004 1.00e+000 3.622630688e+001 3.625125351e+001 5.8e-009 3.19 43 1.0e-005 1.6e-002 6.0e-004 1.00e+000 3.622799184e+001 3.625044366e+001 5.2e-009 3.25 44 9.0e-006 1.5e-002 5.4e-004 1.00e+000 3.622950818e+001 3.624971470e+001 4.7e-009 3.30 45 8.1e-006 1.4e-002 4.9e-004 1.00e+000 3.623087278e+001 3.624905857e+001 4.2e-009 3.38 46 7.3e-006 1.4e-002 4.4e-004 1.00e+000 3.623210083e+001 3.624846797e+001 3.8e-009 3.52 47 6.6e-006 1.3e-002 3.9e-004 1.00e+000 3.623320598e+001 3.624793636e+001 3.4e-009 3.67 48 5.9e-006 1.3e-002 3.5e-004 1.00e+000 3.623420054e+001 3.624745784e+001 3.1e-009 3.80 49 5.3e-006 1.2e-002 3.2e-004 1.00e+000 3.623509558e+001 3.624702712e+001 2.8e-009 3.91 50 4.8e-006 1.2e-002 2.9e-004 1.00e+000 3.623590104e+001 3.624663940e+001 2.5e-009 4.03 51 4.3e-006 1.1e-002 2.6e-004 1.00e+000 3.623662589e+001 3.624629040e+001 2.3e-009 4.16 52 3.9e-006 1.1e-002 2.3e-004 1.00e+000 3.623727821e+001 3.624597626e+001 2.0e-009 4.31 53 3.5e-006 1.0e-002 2.1e-004 1.00e+000 3.623786524e+001 3.624569348e+001 1.8e-009 4.38 54 3.2e-006 1.0e-002 1.9e-004 1.00e+000 3.623839353e+001 3.624543894e+001 1.6e-009 4.42 55 2.8e-006 9.8e-003 1.7e-004 1.00e+000 3.623886895e+001 3.624520981e+001 1.5e-009 4.48 56 2.6e-006 9.6e-003 1.5e-004 1.00e+000 3.623929678e+001 3.624500356e+001 1.3e-009 4.53 57 2.3e-006 9.3e-003 1.4e-004 1.00e+000 3.623968181e+001 3.624481791e+001 1.2e-009 4.59 58 2.1e-006 9.1e-003 1.2e-004 1.00e+000 3.624002830e+001 3.624465079e+001 1.1e-009 4.67 59 1.9e-006 9.0e-003 1.1e-004 1.00e+000 3.624034012e+001 3.624450036e+001 9.7e-010 4.73 60 1.7e-006 8.8e-003 1.0e-004 1.00e+000 3.624062073e+001 3.624436495e+001 8.7e-010 4.80 61 1.5e-006 8.6e-003 9.0e-005 1.00e+000 3.624087326e+001 3.624424307e+001 7.8e-010 4.84 62 1.4e-006 8.5e-003 8.1e-005 1.00e+000 3.624110052e+001 3.624413335e+001 7.1e-010 4.91 63 1.2e-006 8.4e-003 7.3e-005 1.00e+000 3.624130504e+001 3.624403459e+001 6.4e-010 4.98 64 1.1e-006 8.3e-003 6.6e-005 1.00e+000 3.624148910e+001 3.624394569e+001 5.7e-010 5.09 65 9.9e-007 8.2e-003 5.9e-005 1.00e+000 3.624165473e+001 3.624386567e+001 5.1e-010 5.16 66 8.9e-007 8.1e-003 5.3e-005 1.00e+000 3.624180379e+001 3.624379364e+001 4.6e-010 5.22 67 8.0e-007 8.0e-003 4.8e-005 1.00e+000 3.624193794e+001 3.624372880e+001 4.2e-010 5.26 68 7.2e-007 7.9e-003 4.3e-005 1.00e+000 3.624205866e+001 3.624367044e+001 3.8e-010 5.33 69 6.5e-007 7.9e-003 3.9e-005 1.00e+000 3.624216730e+001 3.624361791e+001 3.4e-010 5.39 70 5.8e-007 7.8e-003 3.5e-005 1.00e+000 3.624226508e+001 3.624357062e+001 3.0e-010 5.47 71 5.3e-007 7.7e-003 3.1e-005 1.00e+000 3.624235307e+001 3.624352806e+001 2.7e-010 5.53 72 4.7e-007 7.7e-003 2.8e-005 1.00e+000 3.624243225e+001 3.624348974e+001 2.5e-010 5.59 73 4.3e-007 7.6e-003 2.5e-005 1.00e+000 3.624250351e+001 3.624345526e+001 2.2e-010 5.67 74 3.8e-007 7.6e-003 2.3e-005 1.00e+000 3.624256765e+001 3.624342422e+001 2.0e-010 5.75 75 3.4e-007 7.6e-003 2.1e-005 1.00e+000 3.624262536e+001 3.624339628e+001 1.8e-010 5.81 76 3.1e-007 7.5e-003 1.9e-005 1.00e+000 3.624267730e+001 3.624337113e+001 1.6e-010 5.91 77 2.8e-007 7.5e-003 1.7e-005 1.00e+000 3.624272405e+001 3.624334849e+001 1.5e-010 5.95 78 2.5e-007 7.5e-003 1.5e-005 1.00e+000 3.624276612e+001 3.624332811e+001 1.3e-010 6.00 79 2.3e-007 7.4e-003 1.4e-005 1.00e+000 3.624280397e+001 3.624330977e+001 1.2e-010 6.09 80 2.0e-007 7.4e-003 1.2e-005 1.00e+000 3.624283805e+001 3.624329327e+001 1.1e-010 6.17 81 1.8e-007 7.4e-003 1.1e-005 1.00e+000 3.624286871e+001 3.624327841e+001 9.5e-011 6.31 82 1.6e-007 7.4e-003 9.9e-006 1.00e+000 3.624289630e+001 3.624326503e+001 8.6e-011 6.44 83 1.5e-007 7.3e-003 8.9e-006 1.00e+000 3.624292114e+001 3.624325300e+001 7.7e-011 6.55 84 1.3e-007 7.3e-003 8.0e-006 1.00e+000 3.624294349e+001 3.624324216e+001 7.0e-011 6.63 85 1.2e-007 7.3e-003 7.2e-006 1.00e+000 3.624296360e+001 3.624323241e+001 6.3e-011 6.72 86 1.1e-007 7.3e-003 6.5e-006 1.00e+000 3.624298170e+001 3.624322363e+001 5.6e-011 6.80 87 9.7e-008 7.3e-003 5.8e-006 9.99e-001 3.624299799e+001 3.624321573e+001 5.1e-011 6.88 88 8.8e-008 7.3e-003 5.2e-006 1.00e+000 3.624301265e+001 3.624320862e+001 4.6e-011 6.94 89 7.9e-008 7.3e-003 4.7e-006 1.00e+000 3.624302585e+001 3.624320222e+001 4.1e-011 7.00 90 7.1e-008 7.2e-003 4.2e-006 1.00e+000 3.624303772e+001 3.624319645e+001 3.7e-011 7.06 91 6.4e-008 7.2e-003 3.8e-006 1.00e+000 3.624304841e+001 3.624319127e+001 3.3e-011 7.13 92 5.8e-008 7.2e-003 3.4e-006 9.99e-001 3.624305803e+001 3.624318661e+001 3.0e-011 7.20 93 5.2e-008 7.2e-003 3.1e-006 1.00e+000 3.624306668e+001 3.624318240e+001 2.7e-011 7.26 94 4.7e-008 7.2e-003 2.8e-006 1.00e+000 3.624307447e+001 3.624317862e+001 2.4e-011 7.33 95 4.2e-008 7.2e-003 2.5e-006 9.99e-001 3.624308148e+001 3.624317522e+001 2.2e-011 7.39 96 3.8e-008 7.2e-003 2.3e-006 1.00e+000 3.624308779e+001 3.624317215e+001 2.0e-011 7.47 97 3.4e-008 7.2e-003 2.0e-006 1.00e+000 3.624309347e+001 3.624316939e+001 1.8e-011 7.56 98 3.1e-008 7.2e-003 1.8e-006 9.99e-001 3.624309858e+001 3.624316691e+001 1.6e-011 7.63 99 2.8e-008 7.2e-003 1.6e-006 9.97e-001 3.624310318e+001 3.624316469e+001 1.4e-011 7.73 100 2.5e-008 7.1e-003 1.5e-006 9.98e-001 3.624310732e+001 3.624316268e+001 1.3e-011 7.88 101 2.2e-008 6.4e-003 1.3e-006 1.00e+000 3.624311107e+001 3.624316085e+001 1.2e-011 8.02 102 2.0e-008 5.8e-003 1.2e-006 9.99e-001 3.624311441e+001 3.624315923e+001 1.0e-011 8.16 103 1.8e-008 5.2e-003 1.1e-006 1.00e+000 3.624311745e+001 3.624315775e+001 9.4e-012 8.30 104 1.6e-008 4.7e-003 9.7e-007 1.00e+000 3.624312016e+001 3.624315643e+001 8.5e-012 8.42 105 1.5e-008 4.2e-003 8.7e-007 1.00e+000 3.624312260e+001 3.624315524e+001 7.6e-012 8.55 106 1.3e-008 3.8e-003 7.9e-007 1.00e+000 3.624312480e+001 3.624315418e+001 6.9e-012 8.64 107 1.2e-008 3.4e-003 7.1e-007 9.99e-001 3.624312677e+001 3.624315322e+001 6.2e-012 8.80 108 1.1e-008 3.1e-003 6.4e-007 1.00e+000 3.624312855e+001 3.624315235e+001 5.6e-012 8.86 109 9.6e-009 2.8e-003 5.7e-007 1.00e+000 3.624313015e+001 3.624315157e+001 5.0e-012 8.94 110 8.6e-009 2.5e-003 5.2e-007 1.00e+000 3.624313159e+001 3.624315087e+001 4.5e-012 8.98 111 7.8e-009 2.2e-003 4.6e-007 1.00e+000 3.624313289e+001 3.624315024e+001 4.1e-012 9.06 112 7.0e-009 2.0e-003 4.2e-007 1.00e+000 3.624313406e+001 3.624314967e+001 3.6e-012 9.13 113 6.3e-009 1.8e-003 3.8e-007 9.99e-001 3.624313511e+001 3.624314916e+001 3.3e-012 9.19 114 5.7e-009 1.6e-003 3.4e-007 1.00e+000 3.624313605e+001 3.624314870e+001 3.0e-012 9.23 115 5.1e-009 1.5e-003 3.0e-007 1.00e+000 3.624313691e+001 3.624314828e+001 2.7e-012 9.30 116 4.6e-009 1.3e-003 2.7e-007 9.97e-001 3.624313767e+001 3.624314791e+001 2.4e-012 9.38 117 4.1e-009 1.2e-003 2.5e-007 1.00e+000 3.624313837e+001 3.624314757e+001 2.2e-012 9.44 118 3.7e-009 1.1e-003 2.2e-007 1.00e+000 3.624313900e+001 3.624314726e+001 1.9e-012 9.52 119 3.3e-009 9.7e-004 2.0e-007 1.00e+000 3.624313956e+001 3.624314699e+001 1.8e-012 9.67 120 3.0e-009 8.7e-004 1.8e-007 1.00e+000 3.624314006e+001 3.624314675e+001 1.6e-012 9.83 121 2.7e-009 7.8e-004 1.6e-007 9.96e-001 3.624314051e+001 3.624314653e+001 1.4e-012 9.97 122 2.4e-009 7.0e-004 1.5e-007 9.96e-001 3.624314092e+001 3.624314633e+001 1.3e-012 10.13 123 2.2e-009 6.3e-004 1.3e-007 9.98e-001 3.624314128e+001 3.624314616e+001 1.2e-012 10.27 124 2.0e-009 5.7e-004 1.2e-007 9.99e-001 3.624314161e+001 3.624314600e+001 1.0e-012 10.42 125 1.8e-009 5.1e-004 1.1e-007 1.01e+000 3.624314191e+001 3.624314585e+001 9.3e-013 10.63 Interior-point optimizer terminated. Time: 10.63. Optimizer terminated. Time: 10.64 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 3.6243141911e+001 nrm: 2e+002 Viol. con: 3e-008 var: 0e+000 Dual. obj: 3.6243145848e+001 nrm: 8e+002 Viol. con: 0e+000 var: 4e-003 * End solution on dual form. * Transforming to primal solution. Solving took 10.7 seconds. result packing took 3% of solve time solution checking took 0.82% of solve time Using solver 'mosek' Solving for 1899 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6215) of matrix 'A'. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 487 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.03 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3607 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.53e+004 after factor : 1.76e+005 Factor - dense dim. : 0 flops : 3.97e+007 Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.232670624e+005 2.000000000e+000 1.0e+000 0.09 1 1.5e+003 2.1e+003 8.2e+004 -9.71e-001 -1.222858160e+005 2.848188808e+000 6.6e-001 0.19 2 6.9e+002 9.5e+002 3.7e+004 -9.55e-001 -1.189353182e+005 6.007525415e+000 3.0e-001 0.28 3 2.9e+002 3.9e+002 1.6e+004 -8.99e-001 -1.109052009e+005 2.517783774e+001 1.3e-001 0.38 4 2.9e+002 3.9e+002 1.6e+004 -7.64e-001 -1.087669480e+005 1.890324740e+003 1.3e-001 0.44 5 1.1e+002 1.5e+002 6.1e+003 -7.55e-001 -8.412797820e+004 7.782729418e+003 5.0e-002 0.53 6 4.3e+001 5.8e+001 2.3e+003 -4.05e-001 -4.824084944e+004 1.171638585e+004 1.9e-002 0.63 7 2.1e+001 2.8e+001 1.1e+003 2.01e-001 -2.781393721e+004 7.289109176e+003 9.1e-003 0.72 8 8.5e+000 1.2e+001 4.6e+002 5.86e-001 -1.238741532e+004 3.709102071e+003 3.7e-003 0.81 9 3.9e+000 5.3e+000 2.1e+002 8.57e-001 -5.638082637e+003 2.044488043e+003 1.7e-003 0.92 10 2.0e+000 2.8e+000 1.1e+002 9.52e-001 -2.782202103e+003 1.272067222e+003 9.1e-004 1.00 11 9.2e-001 1.2e+000 5.0e+001 9.85e-001 -1.247259590e+003 5.981654295e+002 4.1e-004 1.09 12 8.7e-001 1.3e+000 4.8e+001 9.63e-001 -1.215548496e+003 5.625582907e+002 3.9e-004 1.20 13 4.3e-001 6.3e-001 2.4e+001 9.80e-001 -5.889218178e+002 2.990658887e+002 2.0e-004 1.31 14 1.8e-001 2.7e-001 9.9e+000 1.00e+000 -2.437543082e+002 1.275967960e+002 8.2e-005 1.42 15 8.3e-002 1.5e-001 4.6e+000 1.00e+000 -1.042339599e+002 6.939970950e+001 3.9e-005 1.53 16 3.1e-002 1.0e-001 1.8e+000 1.00e+000 -3.164621977e+001 3.408662039e+001 1.5e-005 1.64 17 1.2e-002 1.0e-001 7.1e-001 1.00e+000 -5.103281541e+000 2.143878192e+001 6.1e-006 1.75 18 1.1e-002 9.1e-002 6.4e-001 1.00e+000 -2.786658786e+000 2.113375415e+001 5.5e-006 1.86 19 6.0e-003 6.7e-002 3.5e-001 1.00e+000 4.844020121e+000 1.776269599e+001 3.0e-006 1.97 20 3.5e-003 5.2e-002 2.0e-001 1.01e+000 8.846944268e+000 1.635839421e+001 1.7e-006 2.06 21 2.7e-003 4.3e-002 1.6e-001 1.02e+000 1.013097138e+001 1.585660386e+001 1.3e-006 2.17 22 2.1e-003 3.7e-002 1.2e-001 1.02e+000 1.111007982e+001 1.551008095e+001 1.0e-006 2.27 23 9.2e-004 4.8e-002 5.4e-002 1.02e+000 1.289782355e+001 1.487618410e+001 4.7e-007 2.34 24 5.1e-004 4.6e-002 3.0e-002 1.02e+000 1.350561772e+001 1.460866851e+001 2.6e-007 2.45 25 3.0e-004 4.5e-002 1.8e-002 1.01e+000 1.383445186e+001 1.447321276e+001 1.5e-007 2.55 26 2.0e-004 4.1e-002 1.2e-002 1.01e+000 1.398057287e+001 1.441209142e+001 1.0e-007 2.67 27 1.8e-004 3.8e-002 1.1e-002 1.01e+000 1.401686021e+001 1.440546620e+001 9.4e-008 2.77 28 1.6e-004 3.4e-002 9.7e-003 1.01e+000 1.404312480e+001 1.439273872e+001 8.4e-008 2.89 29 1.5e-004 3.2e-002 8.7e-003 1.01e+000 1.406761445e+001 1.438219134e+001 7.6e-008 2.98 30 1.3e-004 2.9e-002 7.9e-003 1.01e+000 1.408941206e+001 1.437246597e+001 6.8e-008 3.09 31 1.2e-004 2.7e-002 7.1e-003 1.01e+000 1.410897715e+001 1.436367402e+001 6.2e-008 3.20 32 1.1e-004 2.5e-002 6.4e-003 1.01e+000 1.412652327e+001 1.435570884e+001 5.5e-008 3.31 33 9.6e-005 2.4e-002 5.7e-003 1.00e+000 1.414226573e+001 1.434849912e+001 5.0e-008 3.41 34 8.6e-005 2.2e-002 5.2e-003 1.00e+000 1.415639185e+001 1.434197487e+001 4.5e-008 3.50 35 7.8e-005 2.1e-002 4.6e-003 1.00e+000 1.416906897e+001 1.433607225e+001 4.0e-008 3.63 36 7.0e-005 1.9e-002 4.2e-003 1.00e+000 1.418044647e+001 1.433073193e+001 3.6e-008 3.73 37 6.3e-005 1.8e-002 3.8e-003 1.00e+000 1.419065823e+001 1.432590092e+001 3.3e-008 3.84 38 5.7e-005 1.7e-002 3.4e-003 1.00e+000 1.419982406e+001 1.432153108e+001 2.9e-008 3.95 39 5.1e-005 1.6e-002 3.0e-003 1.00e+000 1.420805146e+001 1.431757872e+001 2.7e-008 4.05 40 4.6e-005 1.5e-002 2.7e-003 1.00e+000 1.421543724e+001 1.431400382e+001 2.4e-008 4.17 41 4.1e-005 1.5e-002 2.5e-003 1.00e+000 1.422206877e+001 1.431077261e+001 2.2e-008 4.30 42 3.7e-005 1.4e-002 2.2e-003 1.00e+000 1.422802425e+001 1.430785284e+001 1.9e-008 4.42 43 3.3e-005 1.3e-002 2.0e-003 1.00e+000 1.423337407e+001 1.430521601e+001 1.7e-008 4.55 44 3.0e-005 1.3e-002 1.8e-003 1.00e+000 1.423818094e+001 1.430283548e+001 1.6e-008 4.66 45 2.7e-005 1.2e-002 1.6e-003 1.00e+000 1.424250076e+001 1.430068748e+001 1.4e-008 4.78 46 2.4e-005 1.2e-002 1.5e-003 1.00e+000 1.424638340e+001 1.429874946e+001 1.3e-008 4.91 47 2.2e-005 1.1e-002 1.3e-003 1.00e+000 1.424987362e+001 1.429700130e+001 1.1e-008 5.03 48 2.0e-005 1.1e-002 1.2e-003 1.00e+000 1.425301141e+001 1.429542527e+001 1.0e-008 5.13 49 1.8e-005 1.1e-002 1.1e-003 1.00e+000 1.425583256e+001 1.429400381e+001 9.3e-009 5.22 50 1.6e-005 1.0e-002 9.6e-004 1.00e+000 1.425836932e+001 1.429272244e+001 8.3e-009 5.31 51 1.4e-005 1.0e-002 8.6e-004 1.00e+000 1.426065040e+001 1.429156775e+001 7.5e-009 5.38 52 1.3e-005 1.0e-002 7.7e-004 1.00e+000 1.426270159e+001 1.429052672e+001 6.8e-009 5.55 53 1.2e-005 9.7e-003 7.0e-004 1.00e+000 1.426454612e+001 1.428958878e+001 6.1e-009 5.59 54 1.0e-005 9.5e-003 6.3e-004 1.00e+000 1.426620482e+001 1.428874253e+001 5.5e-009 5.67 55 9.4e-006 9.4e-003 5.6e-004 1.00e+000 1.426769636e+001 1.428798018e+001 4.9e-009 5.69 56 8.5e-006 9.2e-003 5.1e-004 1.00e+000 1.426903748e+001 1.428729271e+001 4.4e-009 5.70 57 7.7e-006 9.0e-003 4.6e-004 1.00e+000 1.427024332e+001 1.428667304e+001 4.0e-009 5.72 58 6.9e-006 8.9e-003 4.1e-004 1.00e+000 1.427132751e+001 1.428611420e+001 3.6e-009 5.75 59 6.2e-006 8.8e-003 3.7e-004 1.00e+000 1.427230236e+001 1.428561012e+001 3.2e-009 5.77 60 5.6e-006 8.7e-003 3.3e-004 1.00e+000 1.427317891e+001 1.428515584e+001 2.9e-009 5.78 61 5.0e-006 8.6e-003 3.0e-004 1.00e+000 1.427396720e+001 1.428474606e+001 2.6e-009 5.80 62 4.5e-006 8.5e-003 2.7e-004 1.00e+000 1.427467611e+001 1.428437711e+001 2.4e-009 5.81 63 4.1e-006 8.4e-003 2.4e-004 1.00e+000 1.427531378e+001 1.428404447e+001 2.1e-009 5.83 64 3.7e-006 8.3e-003 2.2e-004 1.00e+000 1.427588738e+001 1.428374500e+001 1.9e-009 5.84 65 3.3e-006 8.2e-003 2.0e-004 1.00e+000 1.427640343e+001 1.428347511e+001 1.7e-009 5.88 66 3.0e-006 8.2e-003 1.8e-004 1.00e+000 1.427686766e+001 1.428323235e+001 1.5e-009 5.91 67 2.7e-006 8.1e-003 1.6e-004 1.00e+000 1.427728545e+001 1.428301318e+001 1.4e-009 5.92 68 2.4e-006 8.1e-003 1.4e-004 1.00e+000 1.427766142e+001 1.428281565e+001 1.3e-009 5.94 69 2.2e-006 8.0e-003 1.3e-004 1.00e+000 1.427799962e+001 1.428263824e+001 1.1e-009 5.97 70 1.9e-006 8.0e-003 1.2e-004 1.00e+000 1.427830387e+001 1.428247875e+001 1.0e-009 5.99 71 1.8e-006 7.9e-003 1.0e-004 1.00e+000 1.427857770e+001 1.428233488e+001 9.1e-010 6.00 72 1.6e-006 7.9e-003 9.4e-005 9.99e-001 1.427882403e+001 1.428220570e+001 8.2e-010 6.02 73 1.4e-006 7.9e-003 8.5e-005 9.99e-001 1.427904569e+001 1.428208932e+001 7.4e-010 6.03 74 1.3e-006 7.8e-003 7.6e-005 1.00e+000 1.427924521e+001 1.428198431e+001 6.7e-010 6.06 75 1.1e-006 7.8e-003 6.9e-005 9.98e-001 1.427942467e+001 1.428189013e+001 6.0e-010 6.08 76 1.0e-006 7.8e-003 6.2e-005 1.00e+000 1.427958623e+001 1.428180503e+001 5.4e-010 6.09 77 9.3e-007 7.8e-003 5.6e-005 1.00e+000 1.427973159e+001 1.428172850e+001 4.8e-010 6.11 78 8.4e-007 7.7e-003 5.0e-005 9.95e-001 1.427986233e+001 1.428165995e+001 4.4e-010 6.13 79 7.5e-007 7.7e-003 4.5e-005 9.98e-001 1.427998001e+001 1.428159808e+001 3.9e-010 6.16 80 6.8e-007 7.7e-003 4.1e-005 9.95e-001 1.428008588e+001 1.428154248e+001 3.5e-010 6.17 81 6.1e-007 7.7e-003 3.6e-005 1.00e+000 1.428018138e+001 1.428149198e+001 3.2e-010 6.19 82 5.5e-007 7.6e-003 3.3e-005 9.97e-001 1.428026714e+001 1.428144678e+001 2.9e-010 6.24 83 4.9e-007 6.9e-003 3.0e-005 1.01e+000 1.428034793e+001 1.428140361e+001 2.6e-010 6.27 84 4.5e-007 6.2e-003 2.7e-005 9.96e-001 1.428041701e+001 1.428136732e+001 2.3e-010 6.28 85 4.0e-007 5.6e-003 2.4e-005 1.01e+000 1.428048110e+001 1.428133320e+001 2.1e-010 6.30 86 3.6e-007 5.0e-003 2.2e-005 1.01e+000 1.428053922e+001 1.428130221e+001 1.9e-010 6.33 87 3.2e-007 4.5e-003 1.9e-005 1.01e+000 1.428059114e+001 1.428127459e+001 1.7e-010 6.39 88 2.9e-007 4.1e-003 1.7e-005 9.94e-001 1.428063587e+001 1.428125117e+001 1.5e-010 6.41 89 2.6e-007 3.7e-003 1.6e-005 9.95e-001 1.428067612e+001 1.428123006e+001 1.4e-010 6.42 90 2.4e-007 3.3e-003 1.4e-005 1.01e+000 1.428071380e+001 1.428120998e+001 1.3e-010 6.45 91 2.1e-007 3.0e-003 1.3e-005 1.02e+000 1.428074846e+001 1.428119142e+001 1.1e-010 6.47 92 1.9e-007 2.7e-003 1.1e-005 9.68e-001 1.428077736e+001 1.428117666e+001 1.0e-010 6.50 93 1.7e-007 2.4e-003 1.0e-005 9.76e-001 1.428080340e+001 1.428116321e+001 9.2e-011 6.52 94 1.6e-007 2.2e-003 9.3e-006 1.01e+000 1.428082769e+001 1.428115024e+001 8.4e-011 6.53 95 1.4e-007 1.9e-003 8.3e-006 9.87e-001 1.428084875e+001 1.428113922e+001 7.5e-011 6.55 96 1.3e-007 1.7e-003 7.5e-006 1.01e+000 1.428086814e+001 1.428112887e+001 6.8e-011 6.58 97 1.1e-007 1.6e-003 6.8e-006 9.83e-001 1.428088514e+001 1.428112000e+001 6.1e-011 6.59 98 1.0e-007 1.4e-003 6.1e-006 9.97e-001 1.428090047e+001 1.428111189e+001 5.5e-011 6.61 99 9.2e-008 1.3e-003 5.5e-006 9.67e-001 1.428091422e+001 1.428110481e+001 4.9e-011 6.64 100 8.2e-008 1.1e-003 4.9e-006 1.00e+000 1.428092663e+001 1.428109821e+001 4.5e-011 6.69 101 7.4e-008 1.0e-003 4.4e-006 9.67e-001 1.428093777e+001 1.428109246e+001 4.0e-011 6.72 102 6.7e-008 9.3e-004 4.0e-006 1.01e+000 1.428094820e+001 1.428108686e+001 3.6e-011 6.74 103 6.0e-008 8.4e-004 3.6e-006 1.06e+000 1.428095950e+001 1.428108049e+001 3.3e-011 6.75 104 5.4e-008 7.5e-004 3.2e-006 9.46e-001 1.428096734e+001 1.428107655e+001 3.0e-011 6.77 105 4.9e-008 6.8e-004 2.9e-006 9.32e-001 1.428097439e+001 1.428107301e+001 2.7e-011 6.78 106 4.4e-008 6.1e-004 2.6e-006 1.23e+000 1.428098099e+001 1.428106871e+001 2.4e-011 6.80 107 4.0e-008 5.5e-004 2.4e-006 1.00e+000 1.428098675e+001 1.428106571e+001 2.2e-011 6.83 108 3.6e-008 4.9e-004 2.1e-006 9.99e-001 1.428099193e+001 1.428106299e+001 2.0e-011 6.86 109 3.2e-008 4.4e-004 1.9e-006 1.01e+000 1.428099666e+001 1.428106047e+001 1.8e-011 6.89 110 2.9e-008 4.0e-004 1.7e-006 1.01e+000 1.428100108e+001 1.428105809e+001 1.6e-011 6.92 111 2.6e-008 3.6e-004 1.5e-006 9.75e-001 1.428100481e+001 1.428105618e+001 1.5e-011 6.94 112 2.3e-008 3.2e-004 1.4e-006 9.98e-001 1.428100817e+001 1.428105442e+001 1.3e-011 6.97 113 2.1e-008 2.9e-004 1.3e-006 1.01e+000 1.428101127e+001 1.428105277e+001 1.2e-011 7.00 114 1.9e-008 2.6e-004 1.1e-006 9.81e-001 1.428101398e+001 1.428105137e+001 1.1e-011 7.03 115 1.7e-008 2.4e-004 1.0e-006 9.56e-001 1.428101642e+001 1.428105014e+001 9.6e-012 7.06 116 1.5e-008 2.1e-004 9.1e-007 9.77e-001 1.428101862e+001 1.428104900e+001 8.6e-012 7.11 117 1.4e-008 1.9e-004 8.2e-007 1.00e+000 1.428102060e+001 1.428104795e+001 7.7e-012 7.14 118 1.2e-008 1.7e-004 7.4e-007 9.75e-001 1.428102238e+001 1.428104703e+001 7.0e-012 7.16 119 1.1e-008 1.5e-004 6.7e-007 9.50e-001 1.428102398e+001 1.428104622e+001 6.3e-012 7.19 120 1.0e-008 1.4e-004 6.0e-007 1.00e+000 1.428102545e+001 1.428104543e+001 5.7e-012 7.24 121 9.0e-009 1.3e-004 5.4e-007 9.78e-001 1.428102674e+001 1.428104475e+001 5.1e-012 7.28 122 8.1e-009 1.1e-004 4.9e-007 9.81e-001 1.428102791e+001 1.428104413e+001 4.6e-012 7.31 123 7.3e-009 1.0e-004 4.4e-007 9.77e-001 1.428102896e+001 1.428104358e+001 4.1e-012 7.34 124 6.6e-009 9.1e-005 3.9e-007 1.03e+000 1.428103004e+001 1.428104297e+001 3.8e-012 7.38 125 5.9e-009 8.2e-005 3.5e-007 1.06e+000 1.428103108e+001 1.428104237e+001 3.5e-012 7.41 126 5.3e-009 7.4e-005 3.2e-007 1.12e+000 1.428103218e+001 1.428104168e+001 3.3e-012 7.45 127 4.8e-009 6.7e-005 2.9e-007 9.65e-001 1.428103281e+001 1.428104137e+001 3.0e-012 7.50 128 4.3e-009 6.0e-005 2.6e-007 9.99e-001 1.428103337e+001 1.428104108e+001 2.7e-012 7.53 129 3.9e-009 5.4e-005 2.3e-007 9.61e-001 1.428103388e+001 1.428104083e+001 2.4e-012 7.55 130 3.5e-009 4.9e-005 2.1e-007 1.06e+000 1.428103446e+001 1.428104050e+001 2.3e-012 7.59 131 3.2e-009 4.4e-005 1.9e-007 9.39e-001 1.428103485e+001 1.428104031e+001 2.0e-012 7.64 132 2.9e-009 3.9e-005 1.7e-007 1.08e+000 1.428103534e+001 1.428104002e+001 1.9e-012 7.67 133 2.6e-009 3.5e-005 1.5e-007 9.91e-001 1.428103565e+001 1.428103987e+001 1.7e-012 7.72 134 2.3e-009 3.2e-005 1.4e-007 1.07e+000 1.428103601e+001 1.428103966e+001 1.6e-012 7.75 135 2.1e-009 2.9e-005 1.2e-007 1.05e+000 1.428103630e+001 1.428103950e+001 1.5e-012 7.78 Interior-point optimizer terminated. Time: 7.78. Optimizer terminated. Time: 7.81 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.4281036304e+001 nrm: 3e+002 Viol. con: 2e-008 var: 0e+000 Dual. obj: 1.4281039498e+001 nrm: 8e+002 Viol. con: 0e+000 var: 1e-004 * End solution on dual form. * Transforming to primal solution. Solving took 7.85 seconds. result packing took 4.5% of solve time solution checking took 1.2% of solve time Using solver 'mosek' Solving for 1899 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6215) of matrix 'A'. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 487 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.03 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3607 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.53e+004 after factor : 1.76e+005 Factor - dense dim. : 0 flops : 3.97e+007 Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.233077111e+005 2.000000000e+000 1.0e+000 0.06 1 1.6e+003 2.1e+003 8.4e+004 -9.71e-001 -1.223909672e+005 2.791894501e+000 6.8e-001 0.09 2 6.8e+002 9.4e+002 3.7e+004 -9.56e-001 -1.189136286e+005 5.989386607e+000 3.0e-001 0.11 3 2.9e+002 3.9e+002 1.6e+004 -8.98e-001 -1.109631602e+005 2.525211054e+001 1.3e-001 0.13 4 2.9e+002 3.9e+002 1.5e+004 -7.65e-001 -1.086302791e+005 2.068926820e+003 1.3e-001 0.16 5 1.1e+002 1.5e+002 6.0e+003 -7.55e-001 -8.374365502e+004 7.889430305e+003 4.9e-002 0.17 6 4.5e+001 6.1e+001 2.4e+003 -3.96e-001 -5.019494636e+004 1.143610118e+004 2.0e-002 0.19 7 2.8e+001 3.8e+001 1.5e+003 1.76e-001 -3.558939452e+004 8.115385874e+003 1.2e-002 0.20 8 1.3e+001 1.8e+001 7.1e+002 4.56e-001 -1.881438153e+004 4.885634316e+003 5.8e-003 0.22 9 5.2e+000 7.1e+000 2.8e+002 7.48e-001 -7.630413398e+003 2.426809112e+003 2.3e-003 0.25 10 3.4e+000 4.7e+000 1.9e+002 9.25e-001 -5.001656506e+003 1.788917037e+003 1.5e-003 0.27 11 1.1e+000 1.5e+000 5.9e+001 9.58e-001 -1.556954044e+003 6.120662006e+002 4.9e-004 0.28 12 8.9e-001 1.4e+000 4.9e+001 9.85e-001 -1.268689550e+003 5.446789915e+002 4.0e-004 0.30 13 6.6e-001 1.1e+000 3.6e+001 9.71e-001 -9.473281228e+002 4.133286946e+002 3.0e-004 0.33 14 3.4e-001 5.7e-001 1.9e+001 9.99e-001 -4.716258855e+002 2.344442263e+002 1.6e-004 0.36 15 1.3e-001 2.4e-001 7.4e+000 9.96e-001 -1.823507724e+002 9.633453742e+001 6.2e-005 0.38 16 7.7e-002 1.5e-001 4.3e+000 1.01e+000 -1.013606618e+002 5.928676608e+001 3.6e-005 0.41 17 2.8e-002 1.1e-001 1.6e+000 1.01e+000 -3.170023468e+001 2.645486769e+001 1.3e-005 0.44 18 1.6e-002 8.7e-002 8.9e-001 1.01e+000 -1.443836123e+001 1.849355037e+001 7.5e-006 0.45 19 1.3e-002 6.9e-002 7.7e-001 1.03e+000 -9.873394887e+000 1.835823378e+001 6.5e-006 0.47 20 5.0e-003 6.7e-002 2.9e-001 1.02e+000 3.345494935e+000 1.396912097e+001 2.5e-006 0.52 21 2.5e-003 6.2e-002 1.5e-001 1.02e+000 7.350323693e+000 1.271306853e+001 1.3e-006 0.53 22 8.0e-004 7.4e-002 5.0e-002 9.86e-001 1.007229316e+001 1.189316564e+001 4.5e-007 0.55 23 2.5e-004 8.6e-002 1.6e-002 9.73e-001 1.099667619e+001 1.159975201e+001 1.5e-007 0.58 24 8.3e-005 8.5e-002 5.7e-003 9.83e-001 1.129453792e+001 1.150613656e+001 5.4e-008 0.59 25 3.2e-005 7.9e-002 2.3e-003 9.93e-001 1.139420716e+001 1.147869520e+001 2.2e-008 0.61 26 1.3e-005 7.5e-002 9.3e-004 9.97e-001 1.143329442e+001 1.146830042e+001 9.0e-009 0.63 27 5.9e-006 7.0e-002 4.1e-004 9.99e-001 1.144865207e+001 1.146415943e+001 4.0e-009 0.64 28 5.3e-006 6.4e-002 3.7e-004 1.00e+000 1.145002652e+001 1.146398401e+001 3.6e-009 0.69 29 4.8e-006 5.8e-002 3.4e-004 1.00e+000 1.145109586e+001 1.146365783e+001 3.2e-009 0.70 30 4.3e-006 5.3e-002 3.0e-004 1.00e+000 1.145205996e+001 1.146336615e+001 2.9e-009 0.73 31 3.9e-006 4.8e-002 2.7e-004 1.00e+000 1.145292622e+001 1.146310184e+001 2.6e-009 0.75 32 3.5e-006 4.4e-002 2.4e-004 1.00e+000 1.145370519e+001 1.146286336e+001 2.4e-009 0.77 33 3.1e-006 4.0e-002 2.2e-004 1.00e+000 1.145440572e+001 1.146264797e+001 2.1e-009 0.78 34 2.8e-006 3.7e-002 2.0e-004 1.00e+000 1.145503573e+001 1.146245392e+001 1.9e-009 0.80 35 2.5e-006 3.4e-002 1.8e-004 1.00e+000 1.145560241e+001 1.146227883e+001 1.7e-009 0.83 36 2.3e-006 3.1e-002 1.6e-004 1.00e+000 1.145611214e+001 1.146212103e+001 1.6e-009 0.89 37 2.1e-006 2.9e-002 1.4e-004 1.00e+000 1.145657073e+001 1.146197864e+001 1.4e-009 0.91 38 1.8e-006 2.7e-002 1.3e-004 9.99e-001 1.145698322e+001 1.146185062e+001 1.3e-009 0.92 39 1.7e-006 2.5e-002 1.2e-004 1.00e+000 1.145735454e+001 1.146173445e+001 1.1e-009 0.94 40 1.5e-006 2.3e-002 1.1e-004 1.00e+000 1.145768845e+001 1.146163050e+001 1.0e-009 0.95 41 1.3e-006 2.2e-002 9.5e-005 1.00e+000 1.145798896e+001 1.146153659e+001 9.2e-010 0.98 42 1.2e-006 2.0e-002 8.5e-005 1.00e+000 1.145825929e+001 1.146145221e+001 8.3e-010 1.00 43 1.1e-006 1.9e-002 7.7e-005 1.00e+000 1.145850256e+001 1.146137616e+001 7.4e-010 1.02 44 9.8e-007 1.8e-002 6.9e-005 9.99e-001 1.145872141e+001 1.146130788e+001 6.7e-010 1.03 45 8.8e-007 1.7e-002 6.2e-005 1.00e+000 1.145891843e+001 1.146124604e+001 6.0e-010 1.05 46 8.0e-007 1.6e-002 5.6e-005 9.98e-001 1.145909565e+001 1.146119070e+001 5.4e-010 1.06 47 7.2e-007 1.5e-002 5.0e-005 1.00e+000 1.145925517e+001 1.146114067e+001 4.9e-010 1.08 48 6.5e-007 1.4e-002 4.5e-005 9.93e-001 1.145939859e+001 1.146109612e+001 4.4e-010 1.13 49 5.8e-007 1.3e-002 4.1e-005 1.00e+000 1.145952777e+001 1.146105562e+001 4.0e-010 1.14 50 5.2e-007 1.3e-002 3.7e-005 1.00e+000 1.145964405e+001 1.146101907e+001 3.6e-010 1.16 51 4.7e-007 1.2e-002 3.3e-005 9.93e-001 1.145974858e+001 1.146098655e+001 3.2e-010 1.17 52 1.6e-007 4.2e-003 1.1e-005 9.98e-001 1.146036502e+001 1.146079279e+001 1.1e-010 1.19 53 1.5e-007 3.8e-003 1.0e-005 9.94e-001 1.146039778e+001 1.146078246e+001 1.0e-010 1.20 54 7.2e-008 1.4e-003 3.9e-006 1.09e+000 1.146057970e+001 1.146071647e+001 3.6e-011 1.24 55 6.4e-008 1.3e-003 3.5e-006 9.35e-001 1.146059065e+001 1.146071411e+001 3.3e-011 1.25 56 5.0e-008 2.4e-004 6.7e-007 9.72e-001 1.146067150e+001 1.146069550e+001 6.7e-012 1.27 57 4.3e-008 2.2e-004 6.0e-007 1.00e+000 1.146067336e+001 1.146069496e+001 6.0e-012 1.28 58 1.7e-008 1.3e-005 3.5e-008 9.53e-001 1.146068922e+001 1.146069051e+001 5.2e-013 1.30 Interior-point optimizer terminated. Time: 1.30. Optimizer terminated. Time: 1.33 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1460689222e+001 nrm: 1e+002 Viol. con: 5e-007 var: 0e+000 Dual. obj: 1.1460690508e+001 nrm: 8e+002 Viol. con: 0e+000 var: 9e-005 * End solution on dual form. * Transforming to primal solution. Solving took 1.37 seconds. result packing took 20% of solve time solution checking took 5.9% of solve time Using solver 'mosek' Solving for 1899 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6215) of matrix 'A'. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 487 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.03 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3607 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.05 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.53e+004 after factor : 1.76e+005 Factor - dense dim. : 0 flops : 3.97e+007 Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.232431026e+005 2.000000000e+000 1.0e+000 0.09 1 1.6e+003 2.1e+003 8.4e+004 -9.71e-001 -1.223419531e+005 2.778950136e+000 6.8e-001 0.13 2 7.2e+002 9.8e+002 3.9e+004 -9.56e-001 -1.191336129e+005 5.692850614e+000 3.2e-001 0.14 3 2.9e+002 3.9e+002 1.5e+004 -9.03e-001 -1.109286085e+005 2.474616581e+001 1.3e-001 0.17 4 2.9e+002 3.9e+002 1.5e+004 -7.66e-001 -1.085783492e+005 2.085489611e+003 1.3e-001 0.19 5 1.4e+002 1.9e+002 7.3e+003 -7.56e-001 -9.041732622e+004 6.351799209e+003 6.0e-002 0.20 6 4.2e+001 5.8e+001 2.3e+003 -4.99e-001 -4.826123235e+004 1.185406778e+004 1.9e-002 0.22 7 2.3e+001 3.2e+001 1.3e+003 2.08e-001 -3.105817588e+004 7.510012590e+003 1.0e-002 0.27 8 1.1e+001 1.5e+001 5.9e+002 5.41e-001 -1.585866515e+004 4.209590038e+003 4.8e-003 0.31 9 4.7e+000 6.5e+000 2.6e+002 8.02e-001 -6.975664285e+003 2.245625308e+003 2.1e-003 0.34 10 2.2e+000 3.0e+000 1.2e+002 9.33e-001 -3.084315196e+003 1.212783694e+003 9.7e-004 0.41 11 1.4e+000 2.0e+000 7.8e+001 9.84e-001 -2.022103155e+003 8.325182003e+002 6.4e-004 0.44 12 9.4e-001 1.3e+000 5.1e+001 9.86e-001 -1.320315765e+003 5.694009820e+002 4.2e-004 0.45 13 7.9e-001 1.2e+000 4.3e+001 9.64e-001 -1.125404795e+003 4.818052188e+002 3.6e-004 0.48 14 3.2e-001 5.0e-001 1.7e+001 9.90e-001 -4.404948808e+002 2.105525218e+002 1.4e-004 0.52 15 1.6e-001 2.6e-001 8.6e+000 1.00e+000 -2.130665440e+002 1.090956025e+002 7.2e-005 0.55 16 4.9e-002 1.5e-001 2.8e+000 1.00e+000 -6.344512603e+001 3.967169520e+001 2.3e-005 0.56 17 3.9e-002 1.3e-001 2.2e+000 1.00e+000 -4.946305378e+001 3.365014668e+001 1.9e-005 0.59 18 2.1e-002 9.0e-002 1.2e+000 1.00e+000 -2.266161789e+001 2.132969362e+001 1.0e-005 0.61 19 1.5e-002 6.9e-002 8.5e-001 1.02e+000 -1.286698302e+001 1.837467849e+001 7.2e-006 0.64 20 7.3e-003 4.9e-002 4.2e-001 1.03e+000 -1.033234457e-001 1.507023746e+001 3.6e-006 0.66 21 2.6e-003 6.9e-002 1.5e-001 1.02e+000 7.280752652e+000 1.268541519e+001 1.3e-006 0.69 22 1.4e-003 5.2e-002 8.4e-002 9.94e-001 9.002589472e+000 1.205333081e+001 7.4e-007 0.70 23 4.7e-004 7.3e-002 3.0e-002 9.80e-001 1.052993128e+001 1.161598245e+001 2.7e-007 0.72 24 1.8e-004 7.1e-002 1.2e-002 9.82e-001 1.101943461e+001 1.145844454e+001 1.1e-007 0.73 25 8.3e-005 6.7e-002 5.4e-003 9.93e-001 1.119955977e+001 1.140049957e+001 5.1e-008 0.77 26 3.9e-005 6.4e-002 2.6e-003 9.98e-001 1.128069463e+001 1.137551677e+001 2.4e-008 0.78 27 3.5e-005 5.9e-002 2.3e-003 9.99e-001 1.128995430e+001 1.137532058e+001 2.2e-008 0.81 28 3.1e-005 5.4e-002 2.1e-003 1.00e+000 1.129628352e+001 1.137311921e+001 1.9e-008 0.83 29 2.8e-005 4.9e-002 1.9e-003 1.00e+000 1.130207373e+001 1.137123387e+001 1.7e-008 0.86 30 2.5e-005 4.5e-002 1.7e-003 1.00e+000 1.130725615e+001 1.136950657e+001 1.6e-008 0.88 31 2.3e-005 4.1e-002 1.5e-003 1.00e+000 1.131190701e+001 1.136793763e+001 1.4e-008 0.89 32 2.1e-005 3.8e-002 1.4e-003 1.00e+000 1.131608086e+001 1.136651270e+001 1.3e-008 0.91 33 1.8e-005 3.5e-002 1.2e-003 1.00e+000 1.131982782e+001 1.136522014e+001 1.1e-008 0.92 34 1.7e-005 3.2e-002 1.1e-003 1.00e+000 1.132319219e+001 1.136404828e+001 1.0e-008 0.95 35 1.5e-005 3.0e-002 9.9e-004 1.00e+000 1.132621375e+001 1.136298677e+001 9.3e-009 0.97 36 1.3e-005 2.7e-002 8.9e-004 1.00e+000 1.132892792e+001 1.136202566e+001 8.4e-009 0.98 37 1.2e-005 2.5e-002 8.0e-004 1.00e+000 1.133136647e+001 1.136115605e+001 7.5e-009 1.00 38 1.1e-005 2.4e-002 7.2e-004 1.00e+000 1.133355774e+001 1.136036972e+001 6.8e-009 1.02 39 9.8e-006 2.2e-002 6.5e-004 1.00e+000 1.133552709e+001 1.135965905e+001 6.1e-009 1.03 40 8.8e-006 2.0e-002 5.9e-004 1.00e+000 1.133729721e+001 1.135901687e+001 5.5e-009 1.06 41 8.0e-006 1.9e-002 5.3e-004 1.00e+000 1.133888844e+001 1.135843703e+001 4.9e-009 1.08 42 7.2e-006 1.8e-002 4.7e-004 1.00e+000 1.134031899e+001 1.135791324e+001 4.4e-009 1.09 43 6.4e-006 1.7e-002 4.3e-004 1.00e+000 1.134160518e+001 1.135744060e+001 4.0e-009 1.11 44 5.8e-006 1.6e-002 3.8e-004 1.00e+000 1.134276160e+001 1.135701404e+001 3.6e-009 1.13 45 5.2e-006 1.5e-002 3.5e-004 1.00e+000 1.134380142e+001 1.135662905e+001 3.2e-009 1.16 46 4.7e-006 1.4e-002 3.1e-004 1.00e+000 1.134473646e+001 1.135628160e+001 2.9e-009 1.17 47 4.2e-006 1.4e-002 2.8e-004 1.00e+000 1.134557733e+001 1.135596813e+001 2.6e-009 1.19 48 3.8e-006 1.3e-002 2.5e-004 1.00e+000 1.134633355e+001 1.135568545e+001 2.4e-009 1.20 49 3.4e-006 1.2e-002 2.3e-004 1.00e+000 1.134701369e+001 1.135543061e+001 2.1e-009 1.22 50 3.1e-006 1.2e-002 2.0e-004 1.00e+000 1.134762549e+001 1.135520086e+001 1.9e-009 1.24 51 2.8e-006 1.1e-002 1.8e-004 1.00e+000 1.134817585e+001 1.135499385e+001 1.7e-009 1.27 52 2.5e-006 1.1e-002 1.7e-004 1.00e+000 1.134867098e+001 1.135480739e+001 1.6e-009 1.28 53 2.2e-006 1.1e-002 1.5e-004 1.00e+000 1.134911651e+001 1.135463932e+001 1.4e-009 1.30 54 2.0e-006 1.0e-002 1.3e-004 1.00e+000 1.134951737e+001 1.135448804e+001 1.3e-009 1.31 55 1.8e-006 1.0e-002 1.2e-004 1.00e+000 1.134987808e+001 1.135435186e+001 1.1e-009 1.33 56 1.6e-006 9.8e-003 1.1e-004 1.00e+000 1.135020271e+001 1.135422918e+001 1.0e-009 1.36 57 1.5e-006 9.5e-003 9.8e-005 1.00e+000 1.135049488e+001 1.135411866e+001 9.2e-010 1.38 58 1.3e-006 9.3e-003 8.8e-005 9.99e-001 1.135075776e+001 1.135401938e+001 8.2e-010 1.41 59 1.2e-006 9.1e-003 7.9e-005 1.00e+000 1.135099439e+001 1.135392990e+001 7.4e-010 1.44 60 1.1e-006 8.9e-003 7.1e-005 1.00e+000 1.135120735e+001 1.135384939e+001 6.7e-010 1.45 61 9.7e-007 8.8e-003 6.4e-005 9.99e-001 1.135139900e+001 1.135377703e+001 6.0e-010 1.47 62 8.7e-007 8.6e-003 5.8e-005 9.99e-001 1.135157151e+001 1.135371183e+001 5.4e-010 1.49 63 7.8e-007 8.5e-003 5.2e-005 1.00e+000 1.135172680e+001 1.135365307e+001 4.9e-010 1.50 64 7.0e-007 8.4e-003 4.7e-005 1.00e+000 1.135186657e+001 1.135360022e+001 4.4e-010 1.52 65 6.3e-007 8.3e-003 4.2e-005 9.99e-001 1.135199234e+001 1.135355271e+001 3.9e-010 1.58 66 5.7e-007 8.2e-003 3.8e-005 1.00e+000 1.135210556e+001 1.135350991e+001 3.6e-010 1.61 67 5.1e-007 8.1e-003 3.4e-005 1.00e+000 1.135220746e+001 1.135347141e+001 3.2e-010 1.64 68 4.6e-007 8.0e-003 3.1e-005 1.00e+000 1.135229919e+001 1.135343672e+001 2.9e-010 1.66 69 4.2e-007 7.9e-003 2.8e-005 9.99e-001 1.135238172e+001 1.135340555e+001 2.6e-010 1.70 70 3.7e-007 7.9e-003 2.5e-005 1.00e+000 1.135245604e+001 1.135337739e+001 2.3e-010 1.75 71 3.4e-007 7.8e-003 2.2e-005 1.00e+000 1.135252292e+001 1.135335209e+001 2.1e-010 1.77 72 3.0e-007 7.7e-003 2.0e-005 1.00e+000 1.135258310e+001 1.135332937e+001 1.9e-010 1.78 73 2.7e-007 7.7e-003 1.8e-005 9.99e-001 1.135263724e+001 1.135330896e+001 1.7e-010 1.80 74 2.5e-007 7.7e-003 1.6e-005 1.00e+000 1.135268604e+001 1.135329047e+001 1.5e-010 1.83 75 2.2e-007 7.6e-003 1.5e-005 9.99e-001 1.135272991e+001 1.135327391e+001 1.4e-010 1.84 76 2.0e-007 7.6e-003 1.3e-005 9.95e-001 1.135276936e+001 1.135325908e+001 1.2e-010 1.86 77 1.8e-007 7.5e-003 1.2e-005 9.95e-001 1.135280488e+001 1.135324572e+001 1.1e-010 1.89 78 1.6e-007 7.5e-003 1.1e-005 9.94e-001 1.135283683e+001 1.135323373e+001 1.0e-010 1.95 79 1.5e-007 7.5e-003 9.6e-006 9.93e-001 1.135286559e+001 1.135322292e+001 9.0e-011 2.00 80 1.3e-007 7.4e-003 8.7e-006 9.93e-001 1.135289146e+001 1.135321325e+001 8.1e-011 2.05 81 1.2e-007 7.4e-003 7.8e-006 9.94e-001 1.135291476e+001 1.135320449e+001 7.3e-011 2.11 82 1.1e-007 7.4e-003 7.0e-006 9.99e-001 1.135293575e+001 1.135319651e+001 6.6e-011 2.14 83 9.5e-008 6.6e-003 6.3e-006 1.01e+000 1.135295496e+001 1.135318916e+001 5.9e-011 2.19 84 8.6e-008 6.0e-003 5.7e-006 1.00e+000 1.135297200e+001 1.135318268e+001 5.3e-011 2.25 85 7.7e-008 5.4e-003 5.1e-006 9.86e-001 1.135298724e+001 1.135317699e+001 4.8e-011 2.30 86 6.9e-008 4.8e-003 4.6e-006 9.82e-001 1.135300095e+001 1.135317188e+001 4.3e-011 2.36 87 6.3e-008 4.3e-003 4.1e-006 1.00e+000 1.135301348e+001 1.135316706e+001 3.9e-011 2.42 88 5.6e-008 3.9e-003 3.7e-006 1.00e+000 1.135302471e+001 1.135316276e+001 3.5e-011 2.45 89 5.1e-008 3.5e-003 3.4e-006 1.02e+000 1.135303570e+001 1.135315846e+001 3.2e-011 2.50 90 4.6e-008 3.2e-003 3.0e-006 9.93e-001 1.135304459e+001 1.135315511e+001 2.9e-011 2.52 91 4.1e-008 2.9e-003 2.7e-006 9.75e-001 1.135305257e+001 1.135315216e+001 2.6e-011 2.53 92 3.7e-008 2.6e-003 2.4e-006 9.99e-001 1.135305977e+001 1.135314941e+001 2.3e-011 2.58 93 3.3e-008 2.3e-003 2.2e-006 9.52e-001 1.135306621e+001 1.135314710e+001 2.1e-011 2.59 94 3.0e-008 2.1e-003 2.0e-006 1.02e+000 1.135307243e+001 1.135314466e+001 1.9e-011 2.63 95 2.7e-008 1.9e-003 1.8e-006 1.02e+000 1.135307812e+001 1.135314229e+001 1.7e-011 2.64 96 2.4e-008 1.7e-003 1.6e-006 9.93e-001 1.135308276e+001 1.135314054e+001 1.6e-011 2.67 97 2.2e-008 1.5e-003 1.4e-006 9.53e-001 1.135308692e+001 1.135313905e+001 1.4e-011 2.69 98 2.0e-008 1.4e-003 1.3e-006 9.48e-001 1.135309066e+001 1.135313772e+001 1.3e-011 2.70 99 1.8e-008 1.2e-003 1.2e-006 1.04e+000 1.135309461e+001 1.135313613e+001 1.2e-011 2.77 100 1.6e-008 1.1e-003 1.1e-006 1.13e+000 1.135309936e+001 1.135313407e+001 1.1e-011 2.78 101 2.2e-008 8.0e-005 7.6e-008 8.72e-001 1.135312476e+001 1.135312762e+001 1.9e-012 2.81 102 2.2e-008 7.2e-005 6.9e-008 9.47e-001 1.135312402e+001 1.135312610e+001 1.5e-012 2.91 103 7.4e-009 4.3e-006 4.1e-009 1.00e+000 1.135312456e+001 1.135312468e+001 9.4e-014 2.94 Interior-point optimizer terminated. Time: 2.95. Optimizer terminated. Time: 2.97 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1353124559e+001 nrm: 4e+001 Viol. con: 7e-008 var: 0e+000 Dual. obj: 1.1353124683e+001 nrm: 8e+002 Viol. con: 0e+000 var: 3e-005 * End solution on dual form. * Transforming to primal solution. Solving took 3 seconds. result packing took 13% of solve time solution checking took 2.8% of solve time Using solver 'mosek' Solving for 1899 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 487 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.02 Lin. dep. - number : 0 Presolve terminated. Time: 0.05 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 929 Optimizer - Cones : 0 Optimizer - Scalar variables : 3608 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.05 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.53e+004 after factor : 1.76e+005 Factor - dense dim. : 0 flops : 3.97e+007 Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.230179556e+005 2.000000000e+000 1.0e+000 0.11 1 1.5e+003 2.1e+003 8.3e+004 -9.71e-001 -1.220991743e+005 2.793962899e+000 6.8e-001 0.14 2 6.9e+002 9.4e+002 3.7e+004 -9.56e-001 -1.186976852e+005 5.883138646e+000 3.0e-001 0.19 3 3.0e+002 4.1e+002 1.6e+004 -9.00e-001 -1.112572403e+005 2.390134570e+001 1.3e-001 0.22 4 2.8e+002 3.8e+002 1.5e+004 -7.78e-001 -1.081041296e+005 2.168457188e+003 1.2e-001 0.23 5 1.5e+002 2.0e+002 8.0e+003 -7.53e-001 -9.295145595e+004 5.769454091e+003 6.6e-002 0.27 6 4.2e+001 5.8e+001 2.3e+003 -5.39e-001 -4.795051819e+004 1.225786017e+004 1.9e-002 0.28 7 2.2e+001 2.9e+001 1.2e+003 2.09e-001 -2.863213812e+004 7.786858693e+003 9.5e-003 0.30 8 1.1e+001 1.4e+001 5.7e+002 5.82e-001 -1.523939674e+004 4.289996173e+003 4.7e-003 0.31 9 3.8e+000 5.2e+000 2.1e+002 8.14e-001 -5.622505805e+003 1.872958878e+003 1.7e-003 0.33 10 1.8e+000 2.6e+000 1.0e+002 9.53e-001 -2.530304055e+003 1.153325989e+003 8.3e-004 0.36 11 9.6e-001 1.3e+000 5.3e+001 9.87e-001 -1.337472284e+003 6.074705589e+002 4.4e-004 0.38 12 9.0e-001 1.3e+000 4.9e+001 9.69e-001 -1.273592954e+003 5.615267699e+002 4.1e-004 0.39 13 4.9e-001 7.0e-001 2.7e+001 9.82e-001 -6.887430815e+002 3.104832483e+002 2.2e-004 0.41 14 1.9e-001 4.4e-001 1.0e+001 9.97e-001 -2.668057530e+002 1.250516527e+002 8.8e-005 0.42 15 8.4e-002 2.2e-001 4.7e+000 1.01e+000 -1.118259481e+002 6.257865469e+001 3.9e-005 0.45 16 3.4e-002 1.2e-001 1.9e+000 1.01e+000 -4.180551488e+001 2.927422600e+001 1.6e-005 0.47 17 2.8e-002 1.0e-001 1.6e+000 9.96e-001 -3.248567431e+001 2.669190643e+001 1.4e-005 0.48 18 1.1e-002 9.4e-002 6.2e-001 1.01e+000 -6.973560407e+000 1.600448669e+001 5.3e-006 0.50 19 4.5e-003 8.6e-002 2.7e-001 1.04e+000 4.334500116e+000 1.391030045e+001 2.3e-006 0.52 20 1.9e-003 6.2e-002 1.1e-001 9.89e-001 8.149913380e+000 1.222230321e+001 9.8e-007 0.53 21 1.1e-003 4.8e-002 6.8e-002 9.57e-001 9.322384415e+000 1.184885231e+001 6.0e-007 0.56 22 3.4e-004 7.5e-002 2.2e-002 9.52e-001 1.068414954e+001 1.151808200e+001 2.0e-007 0.58 23 1.8e-004 5.8e-002 1.2e-002 9.66e-001 1.096353766e+001 1.142095314e+001 1.1e-007 0.59 24 1.6e-004 5.3e-002 1.1e-002 9.76e-001 1.100142609e+001 1.141320477e+001 1.0e-007 0.61 25 1.5e-004 4.8e-002 9.7e-003 9.76e-001 1.103388081e+001 1.140498098e+001 9.0e-008 0.64 26 1.3e-004 4.4e-002 8.7e-003 9.77e-001 1.106457734e+001 1.139903531e+001 8.1e-008 0.66 27 1.2e-004 4.0e-002 7.8e-003 9.79e-001 1.109220971e+001 1.139361614e+001 7.3e-008 0.67 28 1.1e-004 3.7e-002 7.1e-003 9.81e-001 1.111706209e+001 1.138865580e+001 6.5e-008 0.69 29 9.6e-005 3.4e-002 6.3e-003 9.83e-001 1.113938048e+001 1.138408606e+001 5.9e-008 0.70 30 8.7e-005 3.1e-002 5.7e-003 9.84e-001 1.115941801e+001 1.137987728e+001 5.3e-008 0.73 31 7.8e-005 2.9e-002 5.1e-003 9.86e-001 1.117740241e+001 1.137600091e+001 4.8e-008 0.78 32 7.0e-005 2.7e-002 4.6e-003 9.87e-001 1.119354069e+001 1.137243208e+001 4.3e-008 0.84 33 6.3e-005 2.5e-002 4.2e-003 9.88e-001 1.120802005e+001 1.136914808e+001 3.9e-008 0.92 34 5.7e-005 2.3e-002 3.8e-003 9.90e-001 1.122100983e+001 1.136612861e+001 3.5e-008 1.00 35 5.1e-005 2.1e-002 3.4e-003 9.91e-001 1.123266262e+001 1.136335471e+001 3.1e-008 1.02 36 4.6e-005 2.0e-002 3.0e-003 9.91e-001 1.124311575e+001 1.136080846e+001 2.8e-008 1.05 37 4.1e-005 1.9e-002 2.7e-003 9.92e-001 1.125249308e+001 1.135847392e+001 2.5e-008 1.06 38 3.7e-005 1.7e-002 2.5e-003 9.93e-001 1.126090514e+001 1.135633482e+001 2.3e-008 1.08 39 3.4e-005 1.6e-002 2.2e-003 9.94e-001 1.126845164e+001 1.135437671e+001 2.1e-008 1.09 40 3.0e-005 1.5e-002 2.0e-003 9.94e-001 1.127522197e+001 1.135258604e+001 1.9e-008 1.11 41 2.7e-005 1.5e-002 1.8e-003 9.95e-001 1.128129623e+001 1.135094964e+001 1.7e-008 1.13 42 2.4e-005 1.4e-002 1.6e-003 9.95e-001 1.128674678e+001 1.134945585e+001 1.5e-008 1.14 43 2.2e-005 1.3e-002 1.5e-003 9.96e-001 1.129163854e+001 1.134809389e+001 1.4e-008 1.16 44 2.0e-005 1.3e-002 1.3e-003 9.96e-001 1.129602959e+001 1.134685349e+001 1.2e-008 1.19 45 1.8e-005 1.2e-002 1.2e-003 9.97e-001 1.129997186e+001 1.134572481e+001 1.1e-008 1.20 46 1.6e-005 1.2e-002 1.1e-003 9.97e-001 1.130351185e+001 1.134469879e+001 9.9e-009 1.22 47 1.4e-005 1.1e-002 9.6e-004 9.97e-001 1.130669116e+001 1.134376704e+001 8.9e-009 1.24 48 1.3e-005 1.1e-002 8.6e-004 9.98e-001 1.130954692e+001 1.134292139e+001 8.0e-009 1.25 49 1.2e-005 1.0e-002 7.7e-004 9.98e-001 1.131211251e+001 1.134215458e+001 7.2e-009 1.27 50 1.1e-005 1.0e-002 7.0e-004 9.98e-001 1.131441771e+001 1.134145961e+001 6.5e-009 1.30 51 9.5e-006 9.8e-003 6.3e-004 9.98e-001 1.131648924e+001 1.134083025e+001 5.8e-009 1.31 52 8.5e-006 9.5e-003 5.6e-004 9.99e-001 1.131835098e+001 1.134026061e+001 5.2e-009 1.34 53 7.7e-006 9.3e-003 5.1e-004 9.99e-001 1.132002432e+001 1.133974522e+001 4.7e-009 1.38 54 6.9e-006 9.1e-003 4.6e-004 9.99e-001 1.132152846e+001 1.133927916e+001 4.3e-009 1.39 55 6.2e-006 8.9e-003 4.1e-004 9.99e-001 1.132288059e+001 1.133885765e+001 3.8e-009 1.41 56 5.6e-006 8.7e-003 3.7e-004 9.99e-001 1.132409615e+001 1.133847667e+001 3.4e-009 1.42 57 5.0e-006 8.5e-003 3.3e-004 9.99e-001 1.132518897e+001 1.133813239e+001 3.1e-009 1.44 58 4.5e-006 8.4e-003 3.0e-004 9.99e-001 1.132617146e+001 1.133782147e+001 2.8e-009 1.49 59 4.1e-006 8.3e-003 2.7e-004 9.99e-001 1.132705483e+001 1.133754050e+001 2.5e-009 1.55 60 3.7e-006 8.2e-003 2.4e-004 9.99e-001 1.132784913e+001 1.133728676e+001 2.3e-009 1.56 61 3.3e-006 8.1e-003 2.2e-004 1.00e+000 1.132856340e+001 1.133705768e+001 2.0e-009 1.59 62 3.0e-006 8.0e-003 2.0e-004 1.00e+000 1.132920578e+001 1.133685086e+001 1.8e-009 1.63 63 2.7e-006 7.9e-003 1.8e-004 1.00e+000 1.132978353e+001 1.133666440e+001 1.6e-009 1.64 64 2.4e-006 7.8e-003 1.6e-004 1.00e+000 1.133030324e+001 1.133649615e+001 1.5e-009 1.66 65 2.2e-006 7.7e-003 1.4e-004 1.00e+000 1.133077074e+001 1.133634453e+001 1.3e-009 1.67 66 2.0e-006 7.7e-003 1.3e-004 1.00e+000 1.133119133e+001 1.133620790e+001 1.2e-009 1.69 67 1.8e-006 7.6e-003 1.2e-004 1.00e+000 1.133156975e+001 1.133608474e+001 1.1e-009 1.70 68 1.6e-006 7.5e-003 1.0e-004 1.00e+000 1.133191024e+001 1.133597374e+001 9.7e-010 1.72 69 1.4e-006 7.5e-003 9.4e-005 1.00e+000 1.133221660e+001 1.133587384e+001 8.8e-010 1.75 70 1.3e-006 7.4e-003 8.5e-005 1.00e+000 1.133249226e+001 1.133578386e+001 7.9e-010 1.77 71 1.2e-006 7.4e-003 7.6e-005 1.00e+000 1.133274032e+001 1.133570281e+001 7.1e-010 1.78 72 1.0e-006 7.4e-003 6.9e-005 1.00e+000 1.133296355e+001 1.133562982e+001 6.4e-010 1.80 73 9.3e-007 7.3e-003 6.2e-005 1.00e+000 1.133316445e+001 1.133556403e+001 5.7e-010 1.81 74 8.4e-007 7.3e-003 5.6e-005 1.00e+000 1.133334521e+001 1.133550489e+001 5.2e-010 1.83 75 7.6e-007 7.3e-003 5.0e-005 1.00e+000 1.133350791e+001 1.133545154e+001 4.7e-010 1.84 76 6.8e-007 7.2e-003 4.5e-005 1.00e+000 1.133365430e+001 1.133540359e+001 4.2e-010 1.86 77 6.1e-007 7.2e-003 4.1e-005 9.99e-001 1.133378603e+001 1.133536049e+001 3.8e-010 1.88 78 5.5e-007 7.2e-003 3.6e-005 1.00e+000 1.133390460e+001 1.133532162e+001 3.4e-010 1.89 79 5.0e-007 7.2e-003 3.3e-005 1.00e+000 1.133401132e+001 1.133528655e+001 3.1e-010 1.91 80 4.5e-007 7.1e-003 3.0e-005 9.99e-001 1.133410733e+001 1.133525510e+001 2.7e-010 1.92 81 4.0e-007 7.1e-003 2.7e-005 1.00e+000 1.133419374e+001 1.133522676e+001 2.5e-010 1.94 82 3.6e-007 7.1e-003 2.4e-005 1.00e+000 1.133427150e+001 1.133520124e+001 2.2e-010 1.95 83 3.3e-007 7.1e-003 2.2e-005 1.00e+000 1.133434149e+001 1.133517825e+001 2.0e-010 1.99 84 2.9e-007 7.1e-003 1.9e-005 1.00e+000 1.133440448e+001 1.133515754e+001 1.8e-010 2.00 85 2.6e-007 7.1e-003 1.7e-005 1.00e+000 1.133446133e+001 1.133513883e+001 1.6e-010 2.02 86 2.4e-007 7.1e-003 1.6e-005 1.00e+000 1.133451232e+001 1.133512209e+001 1.5e-010 2.03 87 2.1e-007 7.0e-003 1.4e-005 9.97e-001 1.133455819e+001 1.133510708e+001 1.3e-010 2.05 88 1.9e-007 7.0e-003 1.3e-005 1.00e+000 1.133459949e+001 1.133509350e+001 1.2e-010 2.06 89 1.7e-007 7.0e-003 1.1e-005 9.98e-001 1.133463664e+001 1.133508132e+001 1.1e-010 2.08 90 1.6e-007 7.0e-003 1.0e-005 9.96e-001 1.133467007e+001 1.133507037e+001 9.6e-011 2.09 91 1.4e-007 7.0e-003 9.3e-006 1.00e+000 1.133470018e+001 1.133506044e+001 8.6e-011 2.11 92 1.3e-007 7.0e-003 8.3e-006 9.95e-001 1.133472725e+001 1.133505157e+001 7.8e-011 2.14 93 1.1e-007 7.0e-003 7.5e-006 9.98e-001 1.133475163e+001 1.133504354e+001 7.0e-011 2.16 94 1.0e-007 7.0e-003 6.8e-006 1.00e+000 1.133477358e+001 1.133503630e+001 6.3e-011 2.17 95 9.2e-008 6.9e-003 6.1e-006 9.95e-001 1.133479331e+001 1.133502982e+001 5.7e-011 2.22 96 8.3e-008 6.9e-003 5.5e-006 9.98e-001 1.133481108e+001 1.133502397e+001 5.1e-011 2.25 97 7.4e-008 6.9e-003 4.9e-006 1.00e+000 1.133482707e+001 1.133501868e+001 4.6e-011 2.27 98 6.7e-008 6.2e-003 4.4e-006 1.01e+000 1.133484182e+001 1.133501375e+001 4.1e-011 2.28 99 6.0e-008 5.6e-003 4.0e-006 1.01e+000 1.133485524e+001 1.133500925e+001 3.7e-011 2.30 100 5.4e-008 5.0e-003 3.6e-006 9.83e-001 1.133486679e+001 1.133500552e+001 3.4e-011 2.31 101 4.9e-008 4.5e-003 3.2e-006 1.00e+000 1.133487732e+001 1.133500201e+001 3.0e-011 2.34 102 4.4e-008 4.1e-003 2.9e-006 1.02e+000 1.133488732e+001 1.133499863e+001 2.8e-011 2.38 103 4.0e-008 3.7e-003 2.6e-006 1.01e+000 1.133489594e+001 1.133499576e+001 2.5e-011 2.39 104 3.6e-008 3.3e-003 2.4e-006 1.01e+000 1.133490359e+001 1.133499321e+001 2.2e-011 2.41 105 3.2e-008 3.0e-003 2.1e-006 1.00e+000 1.133491033e+001 1.133499099e+001 2.0e-011 2.42 106 2.9e-008 2.7e-003 1.9e-006 9.99e-001 1.133491639e+001 1.133498898e+001 1.8e-011 2.44 107 1.1e-007 2.5e-003 1.8e-006 1.01e+000 1.133492338e+001 1.133497895e+001 1.6e-011 2.47 108 2.0e-008 4.7e-004 3.4e-007 1.00e+000 1.133496179e+001 1.133497244e+001 3.0e-012 2.48 109 1.2e-009 2.6e-005 1.9e-008 9.90e-001 1.133497044e+001 1.133497104e+001 1.8e-013 2.50 Interior-point optimizer terminated. Time: 2.50. Optimizer terminated. Time: 2.52 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1334970439e+001 nrm: 5e+001 Viol. con: 1e-008 var: 0e+000 Dual. obj: 1.1334971037e+001 nrm: 8e+002 Viol. con: 0e+000 var: 2e-004 * End solution on dual form. * Transforming to primal solution. Solving took 2.56 seconds. result packing took 72% of solve time solution checking took 3.3% of solve time Solving took 6 GP solves and 45.8 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 2418945.24546 force_pound * meter but the right hand side evaluated to 2375463.46832 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 32774.4494772 force_pound but the right hand side evaluated to 32399.9999983 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 2.21510116801 meter but the right hand side evaluated to 2.08163799485 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 1243585.11889 joule / kilogram but the right hand side evaluated to 1.5612453679 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 664768.948101 joule / kilogram but the right hand side evaluated to 0.667348960596 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 18.3998846711 meter but the right hand side evaluated to 16.3228538601 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 10.903638454726586 but the right hand side evaluated to 4.7888567104431745 (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 10.019875156016207 but the right hand side evaluated to 4.788856703434532 (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 8.144905507897082 but the right hand side evaluated to 4.7888567121676475 (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 18.3622045037 meter but the right hand side evaluated to 18.1376992949 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 18.3622045037 meter but the right hand side evaluated to 18.2420306092 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 0.2960301088493189 but the right hand side evaluated to 0.18973756114239743 (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 0.23302056648262948 but the right hand side evaluated to 0.17434671984925168 (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 7.563261738189791 but the right hand side evaluated to 4.73063931874231 (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 7.58309922089107 but the right hand side evaluated to 4.757850808429351 (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 57.803s OK Generating XML reports... Cloning into 'solar'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-nfxzwn Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-bjfwuw\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-hfuzxm Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in c:\users\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 c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0) Building wheels for collected packages: gassolar Running setup.py bdist_wheel for gassolar: started Running setup.py bdist_wheel for gassolar: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-k9sfey\wheels\fe\11\0a\2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e Successfully built gassolar grin 1.2.1 requires argparse>=1.1, which is not installed. Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\solar Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1) Requirement already satisfied: gpkitmodels in c:\users\jenkins\workspace\gplibrary_pr_models\mosek (from solar==0.0.0.0) (0.0.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2017.3) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.11.0) Building wheels for collected packages: solar Running setup.py bdist_wheel for solar: started Running setup.py bdist_wheel for solar: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-8v8r2d\wheels\f4\d5\5c\e37fedf74a44fbd5641b13d5622b97d759218ff594b631174a 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 5.59 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 1388461.0993 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 1248774.5487 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 82150.9623 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 2.29645500327 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645193703 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 5.71 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 1388463.4586 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 1248776.6745 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 82150.9601 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 2.29645501839 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645195175 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 5.38 seconds. Allowing negative dual variable(s) as small as -8.19247542299993e-11. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2510 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 765970.6061 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 3.48 seconds. Allowing negative dual variable(s) as small as -7.834061262334159e-11. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1911 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 862671.9975 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 5.92 seconds. Allowing negative dual variable(s) as small as -2.918435053034562e-11. 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 987087.3059 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 1.8 seconds. Allowing negative dual variable(s) as small as -3.12870574518503e-11. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.0863 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 1058302.4851 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 3.68 seconds. Allowing negative dual variable(s) as small as -1.0471123535107248e-11. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2510 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 765970.5160 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 3.63 seconds. Allowing negative dual variable(s) as small as -8.117145612342004e-11. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1911 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 862671.9978 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 3.38 seconds. Allowing negative dual variable(s) as small as -6.930846963973269e-11. 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 987087.3138 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 1.75 seconds. Allowing negative dual variable(s) as small as -2.0105004462850625e-11. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.0863 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 1058302.4804 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 5.11 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 1388461.1258 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 1248774.5739 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 82150.9608 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 2.29645499448 meter ** 2 / second ** 2 but the right hand side evaluated to 2.2964519278 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 5.23 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 1388485.8708 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 1248796.8535 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 82150.9545 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 2.29645531221 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645224651 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 0.422 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 838075.6769 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 4.8 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 1017215.3805 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 78650.4125 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 2.62125882769 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124747684 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 1.95293542382 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215473 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 1.0427594177 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521865 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 0.46769813495 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697004612 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 0.139006791945 meter ** 2 / second ** 2 but the right hand side evaluated to 0.13900657379 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 0.43 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 6.01 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/Ai Running tests... ---------------------------------------------------------------------- ..C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun) ....EE ====================================================================== ERROR [37.575s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "solar.py", line 654, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 633, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 83, in __init__ CostedConstraintSet.__init__(self, cost, constraints, substitutions) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__ ConstraintSet.__init__(self, constraints, subs) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__ list.__setitem__(self, i, ConstraintSet(constraint)) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__ raise_elementhasnumpybools(constraint) File "c:\users\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 [11.053s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "solar.py", line 654, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 633, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkitrcraftDrag.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 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]' \gpkit\constraints\model.py", line 83, in __init__ CostedConstraintSet.__init__(self, cost, constraints, substitutions) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__ ConstraintSet.__init__(self, constraints, subs) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__ list.__setitem__(self, i, ConstraintSet(constraint)) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__ raise_elementhasnumpybools(constraint) File "c:\users\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 519.843s FAILED (errors=2) Generating XML reports... Cloning into 'gplibrary'... Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0) Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-cnr3wn Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-h4dhmq\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gplibrary Requirement already satisfied: numpy>=1.12 in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1) Building wheels for collected packages: gpkitmodels Running setup.py bdist_wheel for gpkitmodels: started Running setup.py bdist_wheel for gpkitmodels: finished with status 'done' Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-8bktga\wheels\a3\80\70\6d80d6b876aaa160fc8dda3c238a4f64c571e65f335a009034 Successfully built gpkitmodels grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Successfully installed gpkitmodels-0.0.0.0 adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py' adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py' adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py' adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py' adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py' Using solver 'mosek' Solving for 11 variables. Solving took 0.032 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.103 seconds. Using solver 'mosek' Solving for 9 variables. Solving took 0.023 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.025 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.027 seconds. Beginning signomial solve. Solving took 16 GP solves and 2.41 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 985.544375341 meter * revolutions_per_minute but the right hand side evaluated to 103.041410023 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 0.420585906135 meter ** 2 / second ** 2 but the right hand side evaluated to 0.42057312607 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 0.314645036828 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629898059 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 0.168936439983 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931605546 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 0.0639642366761 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631365881 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 0.0226356536661 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354007108 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%) Using solver 'mosek_cli' Solving for 9 variables. Solving took 0.13 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.134 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.134 seconds. Beginning signomial solve. Solving took 16 GP solves and 4.48 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 100.006572888 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 985.544273012 meter * revolutions_per_minute but the right hand side evaluated to 103.041409265 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 0.420585155677 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420572612637 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 0.314644832147 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629685653 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 0.168936363968 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 0.063964388845 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639632465767 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0018%) 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 0.0226356607395 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226353885393 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0012%) Using solver 'mosek' Solving for 13 variables. Solving took 0.029 seconds. Beginning signomial solve. Solving took 11 GP solves and 1.45 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 1619898.0082 but bound is 700000.0000 Using solver 'mosek_cli' Solving for 13 variables. Solving took 0.083 seconds. Beginning signomial solve. Solving took 11 GP solves and 2.77 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 1619891.9379 but bound is 700000.0000 Warning: Constraint [0.151*B_BladeElementProp/BladeElementPerf_(1,)**-2*F_BladeElementProp/BladeElementPerf_(1,)**2*R_Pro... >= 0.00633*B_BladeElementProp/BladeElementPerf_(1,)**2*G_BladeElementProp/BladeElementPerf_(1,)**2*r_Bl...] is not tight because the left hand side evaluated to 3.18328390896 meter ** 2 / second ** 2 but the right hand side evaluated to 3.18327922145 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00015%) Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3838 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9776 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3883 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9590 but bound is 1000000.0000 Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000 Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000 Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.6332 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.1579 but bound is 700000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000 Running tests... ---------------------------------------------------------------------- .......... ---------------------------------------------------------------------- Ran 10 tests in 18.561s OK Generating XML reports... Cloning into 'eVTOL'... adding test for 'aircraft_models.py' Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 2.552s OK Generating XML reports... USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'git+https://github.com/hoburg/turbofan.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) (venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>exit 0 Build step 'Console output (build log) parsing' changed build result to FAILURE [xUnit] [INFO] - Starting to record. [xUnit] [INFO] - Processing JUnit [xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek' for the testing framework 'JUnit'. [xUnit] [INFO] - Check 'Failed Tests' threshold. [xUnit] [INFO] - Check 'Skipped Tests' threshold. [xUnit] [INFO] - Setting the build status to FAILURE [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: FAILURE