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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 macys_VM in workspace /Users/jenkins/workspace/gplibrary_PR_Models/mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > git init /Users/jenkins/workspace/gplibrary_PR_Models/mosek # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git --version # timeout=10 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 > git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10 > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master Merging Revision c93bb9e622d1f8dbc3f0371ffe91258327ee398f (refs/remotes/origin/pr/169/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='default', fastForwardMode='--ff'} > git rev-parse origin/master^{commit} # timeout=10 > git config core.sparsecheckout # timeout=10 > git checkout -f origin/master # timeout=3 > git merge --ff c93bb9e622d1f8dbc3f0371ffe91258327ee398f # timeout=10 > git rev-parse HEAD^{commit} # timeout=10 Seen branch in repository origin/1682literate Seen branch in repository origin/1682master Seen branch in repository origin/Breakdown Seen branch in repository origin/SPaircraft Seen branch in repository origin/aerosurf Seen branch in repository origin/atmosphere Seen branch in repository origin/boundj Seen branch in repository origin/bounds5 Seen branch in repository origin/boxspar Seen branch in repository origin/breguet_range Seen branch in repository origin/breguetsetup Seen branch in repository origin/climb Seen branch in repository origin/commercial_sizing Seen branch in repository origin/d8 Seen branch in 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origin/prop_beta Seen branch in repository origin/qstr Seen branch in repository origin/quadrotor Seen branch in repository origin/revert-120-SPaircraft Seen branch in repository origin/rockets Seen branch in repository origin/sigeq_paper Seen branch in repository origin/simple_HT_sizing Seen branch in repository origin/simple_flight_profile Seen branch in repository origin/sparlS Seen branch in repository origin/standard_atmosphere Seen branch in repository origin/sutherland Seen branch in repository origin/troposphere Seen branch in repository origin/vectorizeplanform Seen branch in repository origin/wide_body Seen branch in repository origin/wvl Seen 207 remote branches > git show-ref --tags -d # timeout=10 Checking out Revision c93bb9e622d1f8dbc3f0371ffe91258327ee398f (origin/pr/169/merge, origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f c93bb9e622d1f8dbc3f0371ffe91258327ee398f # timeout=3 Commit message: "Merge d057fc54b0626b10dd6fdfee52a83746da2e48ee into f92158c8230dad6f2a09c90b265a9ce8ff32c7da" Using 'Changelog to branch' strategy. Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [description-setter] Description set: <a title="move outboard moment and shear equations to aircraft models" href="https://github.com/convexengineering/gplibrary/pull/169">PR 169</a>: move outboard moment and shear equations to aircraft models [Execution node] check if [macys_VM] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] enabling perform for step [Execute shell] [mosek] $ /bin/bash -xe /var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/jenkins2000589473154446076.sh + [[ macys_VM == *macys* ]] + export PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ + PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ + virtualenv /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit New python executable in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/python Installing setuptools, pip, wheel...done. + . /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/activate ++ deactivate nondestructive ++ unset -f pydoc ++ '[' -z '' ']' ++ '[' -z '' ']' ++ '[' -n /bin/bash ']' ++ hash -r ++ '[' -z '' ']' ++ unset VIRTUAL_ENV ++ '[' '!' nondestructive = nondestructive ']' ++ VIRTUAL_ENV=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit ++ export VIRTUAL_ENV ++ _OLD_VIRTUAL_PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export PATH ++ '[' -z '' ']' ++ '[' -z '' ']' ++ _OLD_VIRTUAL_PS1= ++ '[' x '!=' x ']' +++ basename /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit ++ PS1='(venv2_gpkit) ' ++ export PS1 ++ alias pydoc ++ '[' -n /bin/bash ']' ++ hash -r ++ which pip + export PIP=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip + PIP=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip + python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade pip Requirement already up-to-date: pip in ./venv2_gpkit/lib/python2.7/site-packages (10.0.1) + [[ macys_VM == *reynolds* ]] + [[ macys_VM == *macys* ]] + [[ mosek == mosek ]] + [[ macys_VM == macys ]] + export PATH=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin + PATH=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin + export DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin + DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin + python /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/setup.py install running install running build running build_py running install_lib creating /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib/mosek/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib/mosek/array.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek creating /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib/mosek/fusion/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib/mosek/fusion/SolverInfo.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib/mosek/fusion/Utils.py -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/__init__.py to __init__.pyc byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/array.py to array.pyc byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/__init__.py to __init__.pyc byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/SolverInfo.py to SolverInfo.pyc byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/Utils.py to Utils.pyc running install_data copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosek64.7.1.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosekglb64.7.1.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libiomp5.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosekxx7_1.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../../../../license.pdf -> /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek running install_egg_info Writing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/Mosek-7.1.28-py2.7.egg-info Please review the MOSEK license conditions in license.pdf + [[ mosek == mosek ]] + python -c '__import__("mosek").Env()' + msktestlic Computer Platform : MACOSX/64-X86 Cores : 4 Problem Name : Objective sense : min Type : LO (linear optimization problem) Constraints : 1 Cones : 0 Scalar variables : 5000 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator - tries : 0 time : 0.00 Eliminator - elim's : 0 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.01 ************************************ A license was checked out correctly. ************************************ + export 'GPKITSOLVERS=mosek, mosek_cli' + GPKITSOLVERS='mosek, mosek_cli' + [[ mosek == cvxopt ]] + python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade xmlrunner Collecting xmlrunner Installing collected packages: xmlrunner Successfully installed xmlrunner-1.7.7 + python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade pint Collecting pint Installing collected packages: pint Successfully installed pint-0.8.1 + python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade numpy Collecting numpy Using cached https://files.pythonhosted.org/packages/b8/97/ecff917542e3a8a33bc8e88c031ed50c90577fd205eab362b29f3e57c09e/numpy-1.14.3-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl Installing collected packages: numpy Successfully installed numpy-1.14.3 + python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade scipy Collecting scipy Using cached https://files.pythonhosted.org/packages/aa/48/517a82fbbe1746318c19ffb32bb0e9592a0e2fd26adcb1506b383999721f/scipy-1.0.1-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl Requirement not upgraded as not directly required: numpy>=1.8.2 in ./venv2_gpkit/lib/python2.7/site-packages (from scipy) (1.14.3) Installing collected packages: scipy Successfully installed scipy-1.0.1 + python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade ctypesgen Collecting ctypesgen Installing collected packages: ctypesgen Successfully installed ctypesgen-0.post125 + python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade pandas Collecting pandas Using cached https://files.pythonhosted.org/packages/82/62/e9058dc7f4d3be74d1111c14bc69a6edb8aeefbd4f6974f151d9d724fe04/pandas-0.22.0-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl Collecting pytz>=2011k (from pandas) Using cached https://files.pythonhosted.org/packages/dc/83/15f7833b70d3e067ca91467ca245bae0f6fe56ddc7451aa0dc5606b120f2/pytz-2018.4-py2.py3-none-any.whl Requirement not upgraded as not directly required: numpy>=1.9.0 in ./venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3) Collecting python-dateutil (from pandas) Using cached https://files.pythonhosted.org/packages/0c/57/19f3a65bcf6d5be570ee8c35a5398496e10a0ddcbc95393b2d17f86aaaf8/python_dateutil-2.7.2-py2.py3-none-any.whl Collecting six>=1.5 (from python-dateutil->pandas) Using cached https://files.pythonhosted.org/packages/67/4b/141a581104b1f6397bfa78ac9d43d8ad29a7ca43ea90a2d863fe3056e86a/six-1.11.0-py2.py3-none-any.whl Installing collected packages: pytz, six, python-dateutil, pandas Successfully installed pandas-0.22.0 python-dateutil-2.7.2 pytz-2018.4 six-1.11.0 + python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade matplotlib Collecting matplotlib Using cached https://files.pythonhosted.org/packages/61/38/d70e8bf77d5cb27d5f3595edd0b3978825063feadd023786d2591e393e6e/matplotlib-2.2.2-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl Collecting backports.functools-lru-cache (from matplotlib) Using cached https://files.pythonhosted.org/packages/03/8e/2424c0e65c4a066e28f539364deee49b6451f8fcd4f718fefa50cc3dcf48/backports.functools_lru_cache-1.5-py2.py3-none-any.whl Requirement not upgraded as not directly required: six>=1.10 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.11.0) Requirement not upgraded as not directly required: pytz in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2018.4) Collecting subprocess32 (from matplotlib) Collecting cycler>=0.10 (from matplotlib) Using cached https://files.pythonhosted.org/packages/f7/d2/e07d3ebb2bd7af696440ce7e754c59dd546ffe1bbe732c8ab68b9c834e61/cycler-0.10.0-py2.py3-none-any.whl Collecting kiwisolver>=1.0.1 (from matplotlib) Using cached https://files.pythonhosted.org/packages/79/d8/94633718f3f77dcb638687a77ba199325a1cb158d2d4b00c9dc17f2b5c72/kiwisolver-1.0.1-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl Requirement not upgraded as not directly required: python-dateutil>=2.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2.7.2) Collecting pyparsing!=2.0.4,!=2.1.2,!=2.1.6,>=2.0.1 (from matplotlib) Using cached https://files.pythonhosted.org/packages/6a/8a/718fd7d3458f9fab8e67186b00abdd345b639976bc7fb3ae722e1b026a50/pyparsing-2.2.0-py2.py3-none-any.whl Requirement not upgraded as not directly required: numpy>=1.7.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.14.3) Requirement not upgraded as not directly required: setuptools in ./venv2_gpkit/lib/python2.7/site-packages (from kiwisolver>=1.0.1->matplotlib) (39.1.0) Installing collected packages: backports.functools-lru-cache, subprocess32, cycler, kiwisolver, pyparsing, matplotlib Successfully installed backports.functools-lru-cache-1.5 cycler-0.10.0 kiwisolver-1.0.1 matplotlib-2.2.2 pyparsing-2.2.0 subprocess32-3.2.7 + export GPKITBUILD=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/build_gpkit + GPKITBUILD=/Users/jenkins/workspace/gplibrary_PR_Models/mosek/build_gpkit + python -c 'import scipy; print scipy.__version__' 1.0.1 + python -c 'import numpy; print numpy.__version__' 1.14.3 + python -c 'import pint; print pint.__version__' 0.8.1 + git clone --depth 1 https://github.com/convexengineering/gpkit.git Cloning into 'gpkit'... + python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit Requirement already satisfied: numpy>=1.12.1 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.7.0.0) (1.14.3) Requirement already satisfied: pint>=0.7 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.7.0.0) (0.8.1) Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.7.0.0) (1.0.1) Collecting ad (from gpkit==0.7.0.0) Downloading https://files.pythonhosted.org/packages/3b/f0/16776411190d53745d0d020a242e2890a59c0752b133a3476d35aa63e4a2/ad-1.3.2.zip Installing collected packages: ad, gpkit Running setup.py install for ad: started Running setup.py install for ad: finished with status 'done' Running setup.py develop for gpkit Successfully installed ad-1.3.2 gpkit + python /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_PR_Models/mosek Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/mosek Requirement already satisfied: numpy>=1.12 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.8.1) Installing collected packages: gpkitmodels Running setup.py develop for gpkitmodels Successfully installed gpkitmodels + cat /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/env/settings installed_solvers : mosek, mosek_cli mosek_bin_dir : /Users/jenkins/mosek/7/tools/platform/osx64x86/bin + ls /Users/jenkins/workspace/gplibrary_PR_Models/mosek/build_gpkit expopt.so + export MSK_IPAR_NUM_THREADS=2 + MSK_IPAR_NUM_THREADS=2 + export MKL_NUM_THREADS=2 + MKL_NUM_THREADS=2 + export NUMEXPR_NUM_THREADS=2 + NUMEXPR_NUM_THREADS=2 + export OPENBLAS_NUM_THREADS=2 + OPENBLAS_NUM_THREADS=2 + export OMP_NUM_THREADS=2 + OMP_NUM_THREADS=2 + python -c 'from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)' Obtaining file:///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'... Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 0.487s OK Generating XML reports... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.0134 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.0125 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.234 seconds. Cloning into 'gassolar'... Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3) Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-XldGtR Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-Y6Yb5L/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Installing collected packages: gpfit Successfully installed gpfit-0.1 Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gassolar Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2018.4) Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.7.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-0edaoA/wheels/62/18/d3/616f96cc7315a5d96e00418a41713828819a211a1260f4c2f6 Successfully built gassolar Installing collected packages: gassolar Successfully installed gassolar-0.0.0.0 Running tests... ---------------------------------------------------------------------- ../Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 4 tests in 26.116s OK Generating XML reports... 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 0.062 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 0.654 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 0.0542 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 0.625 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 0.409 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1496 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.1345 but bound is 150000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.14/GustL.14_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.13/GustL.13_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.19/GustL.19_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.20/GustL.20_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.16/GustL.16_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.15/GustL.15_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.12/GustL.12_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.17/GustL.17_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.18/GustL.18_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.11/GustL.11_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.21/GustL.21_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 4 GP solves and 1.8 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0581 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.9086 but bound is 150000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek_cli' Solving for 1250 variables. Solving took 0.282 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 3.55 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 Cloning into 'jho'... Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3) Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-eA2sZW Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-xtp5aS/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 38.633s OK Generating XML reports... adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -5.0964441000722616e-14. Allowing negative dual variable(s) as small as -7.307002225509507e-14. Allowing negative dual variable(s) as small as -1.4965372691078116e-13. Allowing negative dual variable(s) as small as -1.4989485347394194e-13. Solving took 4 GP solves and 1.71 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.0799208589635825e-14. Allowing negative dual variable(s) as small as -7.570203144902088e-14. Allowing negative dual variable(s) as small as -1.5119719712353152e-13. Allowing negative dual variable(s) as small as -1.4940999826240642e-13. Solving took 4 GP solves and 2.03 seconds. Allowing negative dual variable(s) as small as -5.164531996504351e-13. Allowing negative dual variable(s) as small as -1.4299689904406776e-12. Allowing negative dual variable(s) as small as -4.4561229706197025e-13. Allowing negative dual variable(s) as small as -4.429824562723894e-13. Allowing negative dual variable(s) as small as -1.2979032995921735e-12. Allowing negative dual variable(s) as small as -1.091828667407202e-12. Allowing negative dual variable(s) as small as -1.0908848694160533e-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 -3.8077180297690916e-16. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.490211082231377e-14. Allowing negative dual variable(s) as small as -5.695999135751002e-12. Allowing negative dual variable(s) as small as -2.087890496640573e-11. Allowing negative dual variable(s) as small as -2.0880792395707826e-11. Solving took 4 GP solves and 4.73 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.19 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.171679057225376e-13. Allowing negative dual variable(s) as small as -1.4311728885330055e-12. Allowing negative dual variable(s) as small as -4.4396777920674424e-13. Allowing negative dual variable(s) as small as -4.45555051187263e-13. Allowing negative dual variable(s) as small as -1.2969963644748894e-12. Allowing negative dual variable(s) as small as -1.0911537515548297e-12. Allowing negative dual variable(s) as small as -1.090691881429351e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.5357274140916234e-14. Allowing negative dual variable(s) as small as -5.6960093788145544e-12. Allowing negative dual variable(s) as small as -2.087895526793376e-11. Allowing negative dual variable(s) as small as -2.0880742739327736e-11. Solving took 4 GP solves and 2.15 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.9 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Cloning into 'turbofan'... Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/turbofan Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-BWMvc9/wheels/5a/d9/61/61e35684062bfcf52c1d9781b80aeffbe3c3604f4de326b4d2 Successfully built turbofan Installing collected packages: turbofan Successfully installed turbofan-0.0.0.0 Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 1.301s OK Generating XML reports... adding test for 'turbofan/engine_validation.py' Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528315 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%) Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485055 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Cloning into 'SPaircraft'... Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-QRQYds Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-zPTcxY/wheels/49/e6/3a/5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5 Successfully built turbofan Running tests... ---------------------------------------------------------------------- adding test for 'SP_aircraft.py' Beginning signomial solve. Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : MACOSX/64-X86 Cores : 4 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1015 Eliminator terminated. Eliminator started. Total number of eliminations : 1025 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1025 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.02 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 826 Optimizer - Cones : 0 Optimizer - Scalar variables : 3575 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.05 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 1.67e+04 after factor : 1.69e+05 Factor - dense dim. : 0 flops : 0.00e+00 Factor - GP saved nzs : 0 GP saved flops : 0.00e+00 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.290114216e+05 2.000000000e+00 1.0e+00 0.07 1 1.1e+03 1.4e+03 6.2e+04 -9.71e-01 -1.268480541e+05 3.677917588e+00 4.8e-01 0.53 2 3.8e+02 4.9e+02 2.1e+04 -9.36e-01 -1.195240616e+05 1.166054397e+01 1.7e-01 0.65 3 2.8e+02 3.7e+02 1.6e+04 -8.21e-01 -1.157847903e+05 9.419380750e+01 1.2e-01 0.84 4 2.8e+02 3.6e+02 1.6e+04 -7.55e-01 -1.126192885e+05 2.644815609e+03 1.2e-01 0.95 5 6.4e+01 8.3e+01 3.6e+03 -7.45e-01 -6.715490567e+04 1.234316434e+04 2.8e-02 1.29 6 2.9e+01 3.8e+01 1.7e+03 -8.76e-02 -3.900247076e+04 1.063813187e+04 1.3e-02 1.57 7 1.5e+01 1.9e+01 8.3e+02 4.08e-01 -2.201101408e+04 6.179481181e+03 6.5e-03 1.75 8 6.2e+00 8.1e+00 3.5e+02 7.01e-01 -9.556932382e+03 3.306290049e+03 2.8e-03 2.00 9 2.9e+00 3.7e+00 1.6e+02 9.00e-01 -4.198892234e+03 1.894112680e+03 1.3e-03 2.35 10 9.4e-01 1.2e+00 5.4e+01 9.67e-01 -1.111371535e+03 9.394246146e+02 4.3e-04 2.39 11 6.8e-01 9.5e-01 3.9e+01 9.87e-01 -6.962698209e+02 7.955224154e+02 3.1e-04 2.45 12 5.3e-01 7.4e-01 3.0e+01 9.84e-01 -4.682721695e+02 7.028962849e+02 2.4e-04 2.68 13 2.2e-01 3.3e-01 1.3e+01 9.84e-01 1.279679145e+01 5.050163626e+02 1.0e-04 2.96 14 9.3e-02 2.2e-01 5.5e+00 9.97e-01 2.102997069e+02 4.213184014e+02 4.4e-05 3.27 15 2.3e-02 1.4e-01 1.4e+00 9.94e-01 3.195642046e+02 3.727189962e+02 1.1e-05 3.43 16 5.9e-03 1.4e-01 3.7e-01 1.00e+00 3.472576359e+02 3.614178634e+02 3.1e-06 3.80 17 2.4e-03 1.2e-01 1.5e-01 1.00e+00 3.531037493e+02 3.589508980e+02 1.3e-06 4.10 18 3.9e-04 1.7e-01 2.5e-02 1.00e+00 3.566421741e+02 3.576042395e+02 2.1e-07 4.35 19 1.5e-04 1.1e-01 9.8e-03 9.89e-01 3.570738940e+02 3.574516584e+02 8.4e-08 4.63 20 4.1e-05 1.1e-01 2.7e-03 9.99e-01 3.572730425e+02 3.573766516e+02 2.3e-08 4.99 21 1.8e-05 9.0e-02 1.2e-03 9.93e-01 3.573159415e+02 3.573607606e+02 9.9e-09 5.30 22 6.2e-06 8.4e-02 4.1e-04 9.97e-01 3.573370870e+02 3.573529071e+02 3.5e-09 5.62 23 2.8e-06 7.1e-02 1.9e-04 1.00e+00 3.573433680e+02 3.573505739e+02 1.6e-09 5.83 24 2.5e-06 6.5e-02 1.7e-04 1.00e+00 3.573439017e+02 3.573503858e+02 1.4e-09 5.95 25 2.3e-06 5.9e-02 1.5e-04 1.00e+00 3.573443724e+02 3.573502079e+02 1.3e-09 6.08 26 2.1e-06 5.4e-02 1.4e-04 1.00e+00 3.573447969e+02 3.573500488e+02 1.2e-09 6.33 27 1.9e-06 4.9e-02 1.2e-04 1.00e+00 3.573451789e+02 3.573499056e+02 1.0e-09 6.71 28 1.7e-06 4.5e-02 1.1e-04 1.00e+00 3.573455227e+02 3.573497767e+02 9.4e-10 6.83 29 1.5e-06 4.1e-02 9.9e-05 1.00e+00 3.573458322e+02 3.573496606e+02 8.5e-10 6.86 30 1.4e-06 3.8e-02 8.9e-05 1.00e+00 3.573461106e+02 3.573495562e+02 7.6e-10 6.95 31 1.2e-06 3.5e-02 8.0e-05 1.00e+00 3.573463612e+02 3.573494622e+02 6.9e-10 7.38 32 1.1e-06 3.2e-02 7.2e-05 1.00e+00 3.573465867e+02 3.573493776e+02 6.2e-10 7.89 33 9.9e-07 2.9e-02 6.5e-05 1.00e+00 3.573467897e+02 3.573493015e+02 5.6e-10 8.41 34 8.9e-07 2.7e-02 5.9e-05 1.00e+00 3.573469723e+02 3.573492329e+02 5.0e-10 8.86 35 8.0e-07 2.5e-02 5.3e-05 1.00e+00 3.573471367e+02 3.573491712e+02 4.5e-10 9.03 36 7.2e-07 2.3e-02 4.7e-05 1.00e+00 3.573472846e+02 3.573491157e+02 4.0e-10 9.06 37 6.5e-07 2.2e-02 4.3e-05 1.00e+00 3.573474177e+02 3.573490657e+02 3.6e-10 9.26 38 5.8e-07 2.0e-02 3.8e-05 1.00e+00 3.573475375e+02 3.573490207e+02 3.3e-10 9.84 39 5.2e-07 1.9e-02 3.5e-05 1.00e+00 3.573476453e+02 3.573489802e+02 2.9e-10 10.38 40 4.7e-07 1.8e-02 3.1e-05 1.00e+00 3.573477423e+02 3.573489437e+02 2.7e-10 10.72 41 4.3e-07 1.7e-02 2.8e-05 1.00e+00 3.573478296e+02 3.573489109e+02 2.4e-10 11.09 42 3.8e-07 1.6e-02 2.5e-05 1.00e+00 3.573479082e+02 3.573488813e+02 2.2e-10 11.32 43 3.4e-07 1.5e-02 2.3e-05 1.00e+00 3.573479789e+02 3.573488547e+02 1.9e-10 11.86 44 3.1e-07 1.4e-02 2.0e-05 1.00e+00 3.573480425e+02 3.573488307e+02 1.7e-10 12.35 45 2.8e-07 1.3e-02 1.8e-05 1.00e+00 3.573480997e+02 3.573488091e+02 1.6e-10 12.85 46 2.5e-07 1.3e-02 1.7e-05 1.00e+00 3.573481512e+02 3.573487897e+02 1.4e-10 13.30 47 2.3e-07 1.2e-02 1.5e-05 1.00e+00 3.573481976e+02 3.573487722e+02 1.3e-10 13.53 48 2.0e-07 1.2e-02 1.3e-05 1.00e+00 3.573482393e+02 3.573487564e+02 1.1e-10 13.55 49 1.8e-07 1.1e-02 1.2e-05 1.00e+00 3.573482768e+02 3.573487422e+02 1.0e-10 13.58 50 1.6e-07 1.1e-02 1.1e-05 1.00e+00 3.573483106e+02 3.573487295e+02 9.3e-11 13.62 51 1.5e-07 1.0e-02 9.8e-06 9.99e-01 3.573483410e+02 3.573487180e+02 8.3e-11 13.67 52 1.3e-07 1.0e-02 8.8e-06 1.00e+00 3.573483683e+02 3.573487077e+02 7.5e-11 13.86 53 1.2e-07 9.8e-03 7.9e-06 9.99e-01 3.573483929e+02 3.573486983e+02 6.7e-11 13.98 54 1.1e-07 9.6e-03 7.1e-06 1.01e+00 3.573484156e+02 3.573486897e+02 6.1e-11 14.09 55 9.7e-08 9.4e-03 6.4e-06 1.00e+00 3.573484355e+02 3.573486822e+02 5.5e-11 14.24 56 8.8e-08 9.2e-03 5.8e-06 9.99e-01 3.573484534e+02 3.573486754e+02 4.9e-11 14.69 57 7.9e-08 8.9e-03 5.2e-06 9.97e-01 3.573484695e+02 3.573486693e+02 4.4e-11 15.24 58 7.1e-08 8.8e-03 4.7e-06 9.97e-01 3.573484840e+02 3.573486638e+02 4.0e-11 15.48 59 6.4e-08 8.6e-03 4.2e-06 9.99e-01 3.573484970e+02 3.573486589e+02 3.6e-11 15.80 60 5.7e-08 8.5e-03 3.8e-06 9.97e-01 3.573485088e+02 3.573486545e+02 3.2e-11 15.90 61 5.2e-08 8.3e-03 3.4e-06 1.00e+00 3.573485193e+02 3.573486505e+02 2.9e-11 16.10 62 4.7e-08 8.2e-03 3.1e-06 9.97e-01 3.573485288e+02 3.573486469e+02 2.6e-11 16.27 63 4.2e-08 8.1e-03 2.8e-06 9.99e-01 3.573485374e+02 3.573486436e+02 2.4e-11 16.33 64 3.8e-08 8.0e-03 2.5e-06 1.00e+00 3.573485451e+02 3.573486407e+02 2.1e-11 16.58 65 3.4e-08 8.0e-03 2.2e-06 1.01e+00 3.573485522e+02 3.573486380e+02 1.9e-11 17.09 66 3.1e-08 7.9e-03 2.0e-06 9.90e-01 3.573485584e+02 3.573486356e+02 1.7e-11 17.17 67 2.7e-08 7.9e-03 1.8e-06 1.01e+00 3.573485642e+02 3.573486334e+02 1.6e-11 17.19 68 2.5e-08 7.8e-03 1.6e-06 9.93e-01 3.573485692e+02 3.573486316e+02 1.4e-11 17.20 69 2.2e-08 7.0e-03 1.5e-06 1.01e+00 3.573485739e+02 3.573486297e+02 1.3e-11 17.23 70 2.0e-08 7.0e-03 1.3e-06 9.86e-01 3.573485780e+02 3.573486282e+02 1.1e-11 17.25 71 1.8e-08 7.0e-03 1.2e-06 9.83e-01 3.573485816e+02 3.573486269e+02 1.0e-11 17.26 72 1.6e-08 6.3e-03 1.1e-06 9.96e-01 3.573485849e+02 3.573486256e+02 9.3e-12 17.27 73 1.5e-08 5.6e-03 9.6e-07 9.89e-01 3.573485878e+02 3.573486245e+02 8.3e-12 17.28 74 1.3e-08 5.1e-03 8.7e-07 9.81e-01 3.573485905e+02 3.573486235e+02 7.5e-12 17.30 75 1.2e-08 4.6e-03 7.8e-07 9.68e-01 3.573485929e+02 3.573486226e+02 6.7e-12 17.31 76 1.1e-08 4.1e-03 7.0e-07 1.01e+00 3.573485951e+02 3.573486218e+02 6.1e-12 17.32 77 9.6e-09 3.7e-03 6.3e-07 9.85e-01 3.573485970e+02 3.573486211e+02 5.5e-12 17.34 78 8.6e-09 3.3e-03 5.7e-07 1.03e+00 3.573485990e+02 3.573486203e+02 5.0e-12 17.35 79 7.8e-09 3.0e-03 5.1e-07 9.79e-01 3.573486005e+02 3.573486197e+02 4.5e-12 17.36 80 7.0e-09 2.7e-03 4.6e-07 9.70e-01 3.573486019e+02 3.573486192e+02 4.1e-12 17.37 81 6.3e-09 2.4e-03 4.1e-07 1.02e+00 3.573486033e+02 3.573486187e+02 3.7e-12 17.39 82 5.7e-09 2.2e-03 3.7e-07 1.05e+00 3.573486046e+02 3.573486181e+02 3.4e-12 17.40 83 5.1e-09 2.0e-03 3.4e-07 1.02e+00 3.573486057e+02 3.573486177e+02 3.1e-12 17.41 84 4.6e-09 1.8e-03 3.0e-07 9.70e-01 3.573486065e+02 3.573486174e+02 2.8e-12 17.43 85 8.8e-10 3.4e-04 5.7e-08 9.98e-01 3.573486129e+02 3.573486150e+02 5.3e-13 17.45 Interior-point optimizer terminated. Time: 17.45. Optimizer terminated. Time: 17.46 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 3.5734861289e+02 Viol. con: 1e-08 var: 0e+00 Dual. obj: 3.5734861495e+02 Viol. con: 0e+00 var: 2e-03 * End solution on dual form. * Transforming to primal solution. Solving took 17.5 seconds. result packing took 1.5% of solve time solution checking took 0.3% of solve time Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : MACOSX/64-X86 Cores : 4 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1012 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 1.67e+04 after factor : 1.72e+05 Factor - dense dim. : 0 flops : 0.00e+00 Factor - GP saved nzs : 0 GP saved flops : 0.00e+00 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.289216043e+05 2.000000000e+00 1.0e+00 0.04 1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.267234623e+05 3.765824503e+00 4.8e-01 0.06 2 4.4e+02 5.7e+02 2.5e+04 -9.36e-01 -1.207891902e+05 1.079220691e+01 1.9e-01 0.07 3 2.9e+02 3.7e+02 1.6e+04 -8.43e-01 -1.159643308e+05 6.124840828e+01 1.3e-01 0.09 4 2.9e+02 3.7e+02 1.6e+04 -7.61e-01 -1.137878989e+05 1.933393792e+03 1.3e-01 0.10 5 8.6e+01 1.1e+02 4.9e+03 -7.56e-01 -7.882906409e+04 1.027174313e+04 3.8e-02 0.11 6 2.9e+01 3.7e+01 1.6e+03 -2.77e-01 -3.734750354e+04 1.217880930e+04 1.3e-02 0.12 7 1.4e+01 1.8e+01 7.6e+02 4.30e-01 -2.027313469e+04 6.145213791e+03 6.0e-03 0.14 8 7.6e+00 9.8e+00 4.3e+02 7.36e-01 -1.178613541e+04 3.700599158e+03 3.3e-03 0.15 9 2.9e+00 3.7e+00 1.6e+02 8.69e-01 -4.521200153e+03 1.607709349e+03 1.3e-03 0.16 10 1.4e+00 1.8e+00 7.8e+01 9.69e-01 -1.993005273e+03 9.612507840e+02 6.1e-04 0.17 11 9.6e-01 1.2e+00 5.4e+01 9.89e-01 -1.376515273e+03 6.927086538e+02 4.3e-04 0.19 12 8.3e-01 1.1e+00 4.7e+01 9.73e-01 -1.213273138e+03 6.063516568e+02 3.7e-04 0.20 13 3.4e-01 4.4e-01 2.0e+01 9.84e-01 -4.820538742e+02 2.711213101e+02 1.5e-04 0.22 14 1.8e-01 2.4e-01 1.0e+01 1.01e+00 -2.287524663e+02 1.619767187e+02 8.1e-05 0.24 15 6.3e-02 1.3e-01 3.7e+00 9.99e-01 -6.068927446e+01 8.123123925e+01 3.0e-05 0.25 16 2.7e-02 8.9e-02 1.6e+00 1.00e+00 -5.697627928e+00 5.547999163e+01 1.3e-05 0.26 17 1.4e-02 7.6e-02 8.5e-01 1.00e+00 1.353067984e+01 4.630833761e+01 6.9e-06 0.27 18 3.0e-03 1.3e-01 1.9e-01 1.00e+00 3.130591998e+01 3.844542071e+01 1.5e-06 0.28 19 1.8e-03 9.3e-02 1.1e-01 1.00e+00 3.336544937e+01 3.754073389e+01 9.0e-07 0.30 20 4.6e-04 1.1e-01 2.9e-02 1.00e+00 3.548910442e+01 3.658515813e+01 2.4e-07 0.31 21 2.3e-04 8.4e-02 1.5e-02 1.00e+00 3.585850844e+01 3.641775559e+01 1.2e-07 0.32 22 2.1e-04 7.6e-02 1.3e-02 1.00e+00 3.589840106e+01 3.640172481e+01 1.1e-07 0.34 23 1.3e-04 6.2e-02 7.8e-03 1.00e+00 3.603816411e+01 3.633745893e+01 6.5e-08 0.35 24 1.1e-04 5.6e-02 7.0e-03 1.00e+00 3.605907806e+01 3.632844021e+01 5.9e-08 0.36 25 1.0e-04 5.1e-02 6.3e-03 1.00e+00 3.607756211e+01 3.631997480e+01 5.3e-08 0.38 26 9.2e-05 4.7e-02 5.7e-03 1.00e+00 3.609418421e+01 3.631234574e+01 4.8e-08 0.39 27 8.2e-05 4.3e-02 5.1e-03 1.00e+00 3.610913213e+01 3.630546920e+01 4.3e-08 0.41 28 7.4e-05 3.9e-02 4.6e-03 1.00e+00 3.612257883e+01 3.629927542e+01 3.9e-08 0.42 29 6.7e-05 3.6e-02 4.2e-03 1.00e+00 3.613467576e+01 3.629369718e+01 3.5e-08 0.43 30 6.0e-05 3.3e-02 3.7e-03 1.00e+00 3.614555903e+01 3.628867381e+01 3.1e-08 0.45 31 5.4e-05 3.1e-02 3.4e-03 1.00e+00 3.615535074e+01 3.628415041e+01 2.8e-08 0.46 32 4.9e-05 2.8e-02 3.0e-03 1.00e+00 3.616416070e+01 3.628007743e+01 2.5e-08 0.47 33 4.4e-05 2.6e-02 2.7e-03 1.00e+00 3.617208756e+01 3.627641025e+01 2.3e-08 0.48 34 3.9e-05 2.4e-02 2.5e-03 1.00e+00 3.617922007e+01 3.627310857e+01 2.0e-08 0.50 35 3.5e-05 2.3e-02 2.2e-03 1.00e+00 3.618563797e+01 3.627013608e+01 1.8e-08 0.51 36 3.2e-05 2.1e-02 2.0e-03 1.00e+00 3.619141301e+01 3.626746008e+01 1.7e-08 0.52 37 2.9e-05 2.0e-02 1.8e-03 1.00e+00 3.619660968e+01 3.626505104e+01 1.5e-08 0.53 38 2.6e-05 1.8e-02 1.6e-03 1.00e+00 3.620128599e+01 3.626288242e+01 1.3e-08 0.54 39 2.3e-05 1.7e-02 1.4e-03 1.00e+00 3.620549411e+01 3.626093028e+01 1.2e-08 0.55 40 2.1e-05 1.6e-02 1.3e-03 1.00e+00 3.620928097e+01 3.625917304e+01 1.1e-08 0.56 41 1.9e-05 1.5e-02 1.2e-03 1.00e+00 3.621268878e+01 3.625759125e+01 9.8e-09 0.57 42 1.7e-05 1.5e-02 1.1e-03 1.00e+00 3.621575551e+01 3.625616742e+01 8.8e-09 0.58 43 1.5e-05 1.4e-02 9.5e-04 1.00e+00 3.621851532e+01 3.625488580e+01 7.9e-09 0.60 44 1.4e-05 1.3e-02 8.6e-04 1.00e+00 3.622099893e+01 3.625373218e+01 7.1e-09 0.61 45 1.2e-05 1.3e-02 7.7e-04 1.00e+00 3.622323400e+01 3.625269377e+01 6.4e-09 0.62 46 1.1e-05 1.2e-02 6.9e-04 1.00e+00 3.622524541e+01 3.625175909e+01 5.8e-09 0.64 47 1.0e-05 1.2e-02 6.2e-04 1.00e+00 3.622705552e+01 3.625091776e+01 5.2e-09 0.65 48 9.0e-06 1.1e-02 5.6e-04 1.00e+00 3.622868450e+01 3.625016046e+01 4.7e-09 0.66 49 8.1e-06 1.1e-02 5.1e-04 1.00e+00 3.623015046e+01 3.624947879e+01 4.2e-09 0.67 50 7.3e-06 1.0e-02 4.5e-04 1.00e+00 3.623146972e+01 3.624886518e+01 3.8e-09 0.69 51 6.6e-06 1.0e-02 4.1e-04 1.00e+00 3.623265696e+01 3.624831285e+01 3.4e-09 0.70 52 5.9e-06 9.8e-03 3.7e-04 1.00e+00 3.623372539e+01 3.624781568e+01 3.1e-09 0.72 53 5.3e-06 9.5e-03 3.3e-04 1.00e+00 3.623468689e+01 3.624736816e+01 2.8e-09 0.73 54 4.8e-06 9.3e-03 3.0e-04 1.00e+00 3.623555217e+01 3.624696530e+01 2.5e-09 0.74 55 4.3e-06 9.1e-03 2.7e-04 1.00e+00 3.623633086e+01 3.624660267e+01 2.2e-09 0.76 56 3.9e-06 8.9e-03 2.4e-04 1.00e+00 3.623703161e+01 3.624627625e+01 2.0e-09 0.77 57 3.5e-06 8.7e-03 2.2e-04 1.00e+00 3.623766224e+01 3.624598241e+01 1.8e-09 0.79 58 3.1e-06 8.6e-03 2.0e-04 1.00e+00 3.623822975e+01 3.624571793e+01 1.6e-09 0.80 59 2.8e-06 8.4e-03 1.8e-04 1.00e+00 3.623874047e+01 3.624547984e+01 1.5e-09 0.81 60 2.5e-06 8.3e-03 1.6e-04 1.00e+00 3.623920007e+01 3.624526552e+01 1.3e-09 0.82 61 2.3e-06 8.2e-03 1.4e-04 1.00e+00 3.623961368e+01 3.624507260e+01 1.2e-09 0.83 62 2.1e-06 8.1e-03 1.3e-04 1.00e+00 3.623998590e+01 3.624489893e+01 1.1e-09 0.85 63 1.9e-06 8.0e-03 1.2e-04 1.00e+00 3.624032087e+01 3.624474260e+01 9.7e-10 0.86 64 1.7e-06 7.9e-03 1.0e-04 1.00e+00 3.624062231e+01 3.624460188e+01 8.7e-10 0.87 65 1.5e-06 7.8e-03 9.4e-05 1.00e+00 3.624089359e+01 3.624447523e+01 7.8e-10 0.88 66 1.4e-06 7.8e-03 8.4e-05 1.00e+00 3.624113772e+01 3.624436121e+01 7.0e-10 0.90 67 1.2e-06 7.7e-03 7.6e-05 1.00e+00 3.624135742e+01 3.624425856e+01 6.3e-10 0.91 68 1.1e-06 7.6e-03 6.8e-05 1.00e+00 3.624155514e+01 3.624416616e+01 5.7e-10 0.92 69 9.9e-07 7.6e-03 6.1e-05 1.00e+00 3.624173307e+01 3.624408300e+01 5.1e-10 0.94 70 8.9e-07 7.5e-03 5.5e-05 1.00e+00 3.624189320e+01 3.624400813e+01 4.6e-10 0.95 71 8.0e-07 7.5e-03 5.0e-05 1.00e+00 3.624203730e+01 3.624394073e+01 4.2e-10 0.96 72 7.2e-07 7.5e-03 4.5e-05 1.00e+00 3.624216699e+01 3.624388007e+01 3.7e-10 0.97 73 6.5e-07 7.4e-03 4.0e-05 1.00e+00 3.624228370e+01 3.624382547e+01 3.4e-10 0.99 74 5.8e-07 7.4e-03 3.6e-05 1.00e+00 3.624238873e+01 3.624377633e+01 3.0e-10 1.00 75 5.2e-07 7.4e-03 3.3e-05 1.00e+00 3.624248325e+01 3.624373208e+01 2.7e-10 1.01 76 4.7e-07 7.3e-03 2.9e-05 1.00e+00 3.624256831e+01 3.624369227e+01 2.5e-10 1.02 77 4.2e-07 7.3e-03 2.6e-05 1.00e+00 3.624264486e+01 3.624365643e+01 2.2e-10 1.03 78 3.8e-07 7.3e-03 2.4e-05 1.00e+00 3.624271375e+01 3.624362416e+01 2.0e-10 1.05 79 3.4e-07 7.3e-03 2.1e-05 1.00e+00 3.624277575e+01 3.624359511e+01 1.8e-10 1.06 80 3.1e-07 7.2e-03 1.9e-05 1.00e+00 3.624283155e+01 3.624356897e+01 1.6e-10 1.07 81 2.8e-07 7.2e-03 1.7e-05 1.00e+00 3.624288176e+01 3.624354545e+01 1.4e-10 1.08 82 2.5e-07 7.2e-03 1.6e-05 1.00e+00 3.624292695e+01 3.624352427e+01 1.3e-10 1.09 83 2.3e-07 7.2e-03 1.4e-05 1.00e+00 3.624296762e+01 3.624350521e+01 1.2e-10 1.11 84 2.0e-07 7.2e-03 1.3e-05 1.00e+00 3.624300422e+01 3.624348806e+01 1.1e-10 1.12 85 1.8e-07 7.2e-03 1.1e-05 1.00e+00 3.624303715e+01 3.624347262e+01 9.5e-11 1.13 86 1.6e-07 7.1e-03 1.0e-05 1.00e+00 3.624306680e+01 3.624345872e+01 8.6e-11 1.15 87 1.5e-07 7.1e-03 9.2e-06 1.00e+00 3.624309348e+01 3.624344619e+01 7.7e-11 1.16 88 1.3e-07 7.1e-03 8.3e-06 1.00e+00 3.624311749e+01 3.624343492e+01 6.9e-11 1.17 89 1.2e-07 7.1e-03 7.5e-06 1.00e+00 3.624313910e+01 3.624342478e+01 6.2e-11 1.18 90 1.1e-07 7.1e-03 6.7e-06 1.00e+00 3.624315854e+01 3.624341565e+01 5.6e-11 1.19 91 9.7e-08 7.1e-03 6.0e-06 1.00e+00 3.624317605e+01 3.624340743e+01 5.1e-11 1.20 92 8.7e-08 7.1e-03 5.4e-06 1.00e+00 3.624319179e+01 3.624340004e+01 4.6e-11 1.22 93 7.9e-08 7.1e-03 4.9e-06 1.00e+00 3.624320597e+01 3.624339339e+01 4.1e-11 1.23 94 7.1e-08 7.1e-03 4.4e-06 1.00e+00 3.624321875e+01 3.624338738e+01 3.7e-11 1.24 95 6.4e-08 7.1e-03 4.0e-06 1.00e+00 3.624323025e+01 3.624338198e+01 3.3e-11 1.25 96 5.7e-08 7.1e-03 3.6e-06 9.99e-01 3.624324057e+01 3.624337713e+01 3.0e-11 1.27 97 5.2e-08 7.0e-03 3.2e-06 9.97e-01 3.624324986e+01 3.624337279e+01 2.7e-11 1.28 98 4.6e-08 7.0e-03 2.9e-06 1.00e+00 3.624325823e+01 3.624336886e+01 2.4e-11 1.29 99 4.2e-08 7.0e-03 2.6e-06 9.99e-01 3.624326575e+01 3.624336533e+01 2.2e-11 1.31 100 3.8e-08 6.3e-03 2.3e-06 1.00e+00 3.624327257e+01 3.624336212e+01 2.0e-11 1.32 101 3.4e-08 5.7e-03 2.1e-06 1.00e+00 3.624327869e+01 3.624335924e+01 1.8e-11 1.33 102 3.1e-08 5.1e-03 1.9e-06 9.97e-01 3.624328416e+01 3.624335667e+01 1.6e-11 1.35 103 2.7e-08 4.6e-03 1.7e-06 1.00e+00 3.624328911e+01 3.624335435e+01 1.4e-11 1.36 104 2.5e-08 4.1e-03 1.5e-06 9.99e-01 3.624329355e+01 3.624335226e+01 1.3e-11 1.37 105 2.2e-08 3.7e-03 1.4e-06 1.00e+00 3.624329760e+01 3.624335035e+01 1.2e-11 1.39 106 2.0e-08 3.4e-03 1.2e-06 9.92e-01 3.624330119e+01 3.624334868e+01 1.0e-11 1.40 107 1.8e-08 3.0e-03 1.1e-06 1.00e+00 3.624330446e+01 3.624334713e+01 9.4e-12 1.41 108 1.6e-08 2.7e-03 1.0e-06 1.00e+00 3.624330740e+01 3.624334575e+01 8.5e-12 1.43 109 1.5e-08 2.4e-03 9.1e-07 1.00e+00 3.624331001e+01 3.624334452e+01 7.6e-12 1.44 110 1.3e-08 2.2e-03 8.2e-07 9.97e-01 3.624331236e+01 3.624334342e+01 6.9e-12 1.45 111 1.2e-08 2.0e-03 7.4e-07 1.00e+00 3.624331447e+01 3.624334243e+01 6.2e-12 1.47 112 1.1e-08 1.8e-03 6.6e-07 1.00e+00 3.624331637e+01 3.624334153e+01 5.6e-12 1.48 113 9.6e-09 1.6e-03 6.0e-07 1.00e+00 3.624331808e+01 3.624334073e+01 5.0e-12 1.49 114 8.6e-09 1.4e-03 5.4e-07 1.00e+00 3.624331962e+01 3.624334000e+01 4.5e-12 1.51 115 7.8e-09 1.3e-03 4.8e-07 1.00e+00 3.624332101e+01 3.624333935e+01 4.1e-12 1.52 116 7.0e-09 1.2e-03 4.3e-07 1.00e+00 3.624332226e+01 3.624333877e+01 3.7e-12 1.53 117 6.3e-09 1.1e-03 3.9e-07 9.99e-01 3.624332338e+01 3.624333824e+01 3.3e-12 1.54 118 5.7e-09 9.5e-04 3.5e-07 1.00e+00 3.624332439e+01 3.624333776e+01 3.0e-12 1.55 119 5.1e-09 8.5e-04 3.2e-07 1.00e+00 3.624332530e+01 3.624333733e+01 2.7e-12 1.57 120 4.6e-09 7.7e-04 2.8e-07 1.00e+00 3.624332612e+01 3.624333695e+01 2.4e-12 1.58 121 4.1e-09 6.9e-04 2.6e-07 9.98e-01 3.624332686e+01 3.624333660e+01 2.2e-12 1.59 122 3.7e-09 6.2e-04 2.3e-07 1.00e+00 3.624332752e+01 3.624333629e+01 1.9e-12 1.60 123 3.3e-09 5.6e-04 2.1e-07 9.95e-01 3.624332812e+01 3.624333601e+01 1.7e-12 1.62 124 3.0e-09 5.0e-04 1.9e-07 1.00e+00 3.624332865e+01 3.624333576e+01 1.6e-12 1.63 125 2.7e-09 4.5e-04 1.7e-07 9.96e-01 3.624332914e+01 3.624333553e+01 1.4e-12 1.65 126 2.4e-09 4.1e-04 1.5e-07 9.96e-01 3.624332957e+01 3.624333533e+01 1.3e-12 1.66 127 2.2e-09 3.7e-04 1.4e-07 9.98e-01 3.624332996e+01 3.624333514e+01 1.1e-12 1.68 128 2.0e-09 3.3e-04 1.2e-07 9.95e-01 3.624333031e+01 3.624333498e+01 1.0e-12 1.69 129 1.8e-09 3.0e-04 1.1e-07 1.01e+00 3.624333064e+01 3.624333482e+01 9.3e-13 1.71 Interior-point optimizer terminated. Time: 1.71. Optimizer terminated. Time: 1.72 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 3.6243330643e+01 Viol. con: 3e-08 var: 0e+00 Dual. obj: 3.6243334822e+01 Viol. con: 0e+00 var: 2e-03 * End solution on dual form. * Transforming to primal solution. Solving took 1.73 seconds. result packing took 13% of solve time solution checking took 2.3% of solve time Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : MACOSX/64-X86 Cores : 4 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1012 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 1.67e+04 after factor : 1.72e+05 Factor - dense dim. : 0 flops : 0.00e+00 Factor - GP saved nzs : 0 GP saved flops : 0.00e+00 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.288863852e+05 2.000000000e+00 1.0e+00 0.04 1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.266799740e+05 3.737215724e+00 4.7e-01 0.12 2 4.2e+02 5.4e+02 2.4e+04 -9.36e-01 -1.204137685e+05 1.081474458e+01 1.8e-01 0.15 3 2.8e+02 3.7e+02 1.6e+04 -8.37e-01 -1.157988456e+05 6.704673556e+01 1.3e-01 0.16 4 2.8e+02 3.7e+02 1.6e+04 -7.58e-01 -1.132306394e+05 2.253045276e+03 1.3e-01 0.18 5 7.6e+01 9.8e+01 4.3e+03 -7.52e-01 -7.382394348e+04 1.111355904e+04 3.4e-02 0.19 6 3.1e+01 4.0e+01 1.8e+03 -1.94e-01 -4.049559709e+04 1.108917967e+04 1.4e-02 0.20 7 1.4e+01 1.8e+01 7.8e+02 3.80e-01 -2.080684221e+04 5.941320219e+03 6.1e-03 0.22 8 9.1e+00 1.2e+01 5.2e+02 7.28e-01 -1.424623613e+04 4.128716146e+03 4.1e-03 0.23 9 3.6e+00 4.7e+00 2.1e+02 8.32e-01 -5.839215063e+03 1.817801176e+03 1.6e-03 0.25 10 2.0e+00 2.6e+00 1.1e+02 9.53e-01 -2.953947261e+03 1.332822177e+03 9.0e-04 0.26 11 9.0e-01 1.2e+00 5.1e+01 9.84e-01 -1.322579450e+03 6.197743176e+02 4.1e-04 0.28 12 8.6e-01 1.2e+00 4.9e+01 9.64e-01 -1.285058493e+03 5.818497496e+02 3.9e-04 0.29 13 3.8e-01 5.3e-01 2.2e+01 9.81e-01 -5.636699146e+02 2.752505431e+02 1.7e-04 0.30 14 1.5e-01 2.3e-01 8.6e+00 1.00e+00 -2.175200599e+02 1.113181181e+02 6.9e-05 0.32 15 8.6e-02 1.5e-01 5.0e+00 1.00e+00 -1.179427063e+02 7.374921181e+01 4.0e-05 0.33 16 2.6e-02 1.2e-01 1.6e+00 1.00e+00 -2.814157347e+01 3.134816581e+01 1.3e-05 0.34 17 1.1e-02 9.3e-02 6.9e-01 1.00e+00 -5.280765552e+00 2.122383972e+01 5.7e-06 0.36 18 1.0e-02 8.5e-02 6.3e-01 1.01e+00 -3.406745398e+00 2.059327021e+01 5.2e-06 0.37 19 6.6e-03 6.5e-02 4.0e-01 1.01e+00 2.894576956e+00 1.822729806e+01 3.3e-06 0.39 20 4.5e-03 4.7e-02 2.8e-01 1.01e+00 6.717097158e+00 1.712679430e+01 2.3e-06 0.40 21 1.8e-03 5.9e-02 1.1e-01 1.01e+00 1.120114772e+01 1.544829274e+01 9.4e-07 0.41 22 1.0e-03 4.8e-02 6.2e-02 1.02e+00 1.265245550e+01 1.495250883e+01 5.1e-07 0.43 23 4.6e-04 5.4e-02 2.9e-02 1.02e+00 1.351747145e+01 1.458911796e+01 2.4e-07 0.44 24 2.6e-04 5.1e-02 1.6e-02 1.01e+00 1.386210015e+01 1.445405105e+01 1.3e-07 0.46 25 1.3e-04 5.2e-02 8.4e-03 1.01e+00 1.406311438e+01 1.437335788e+01 7.1e-08 0.47 26 8.9e-05 4.6e-02 5.6e-03 1.01e+00 1.413708318e+01 1.434303546e+01 4.7e-08 0.49 27 8.0e-05 4.2e-02 5.0e-03 1.00e+00 1.415521252e+01 1.434064262e+01 4.2e-08 0.50 28 7.2e-05 3.9e-02 4.5e-03 1.00e+00 1.416777945e+01 1.433463439e+01 3.8e-08 0.51 29 6.5e-05 3.6e-02 4.1e-03 1.00e+00 1.417931972e+01 1.432946942e+01 3.4e-08 0.52 30 5.8e-05 3.3e-02 3.7e-03 1.00e+00 1.418965248e+01 1.432477063e+01 3.1e-08 0.54 31 5.3e-05 3.0e-02 3.3e-03 1.00e+00 1.419893103e+01 1.432052404e+01 2.8e-08 0.56 32 4.7e-05 2.8e-02 3.0e-03 1.00e+00 1.420726064e+01 1.431668303e+01 2.5e-08 0.57 33 4.3e-05 2.6e-02 2.7e-03 1.00e+00 1.421473934e+01 1.431321087e+01 2.3e-08 0.59 34 3.8e-05 2.4e-02 2.4e-03 1.00e+00 1.422145490e+01 1.431007209e+01 2.0e-08 0.60 35 3.4e-05 2.2e-02 2.2e-03 1.00e+00 1.422748674e+01 1.430723620e+01 1.8e-08 0.62 36 3.1e-05 2.1e-02 2.0e-03 1.00e+00 1.423290581e+01 1.430467537e+01 1.6e-08 0.63 37 2.8e-05 2.0e-02 1.8e-03 1.00e+00 1.423777534e+01 1.430236429e+01 1.5e-08 0.64 38 2.5e-05 1.8e-02 1.6e-03 1.00e+00 1.424215176e+01 1.430027866e+01 1.3e-08 0.65 39 2.3e-05 1.7e-02 1.4e-03 1.00e+00 1.424608562e+01 1.429839752e+01 1.2e-08 0.67 40 2.0e-05 1.6e-02 1.3e-03 1.00e+00 1.424962203e+01 1.429670093e+01 1.1e-08 0.68 41 1.8e-05 1.6e-02 1.2e-03 1.00e+00 1.425280152e+01 1.429517100e+01 9.7e-09 0.70 42 1.6e-05 1.5e-02 1.0e-03 1.00e+00 1.425566037e+01 1.429379168e+01 8.7e-09 0.71 43 1.5e-05 1.4e-02 9.4e-04 1.00e+00 1.425823111e+01 1.429254809e+01 7.9e-09 0.72 44 1.3e-05 1.3e-02 8.4e-04 1.00e+00 1.426054286e+01 1.429142738e+01 7.1e-09 0.74 45 1.2e-05 1.3e-02 7.6e-04 1.00e+00 1.426262173e+01 1.429041719e+01 6.4e-09 0.75 46 1.1e-05 1.2e-02 6.8e-04 1.00e+00 1.426449120e+01 1.428950672e+01 5.7e-09 0.76 47 9.7e-06 1.2e-02 6.1e-04 1.00e+00 1.426617238e+01 1.428868558e+01 5.2e-09 0.77 48 8.8e-06 1.1e-02 5.5e-04 1.00e+00 1.426768414e+01 1.428794585e+01 4.6e-09 0.78 49 7.9e-06 1.1e-02 5.0e-04 1.00e+00 1.426904341e+01 1.428727910e+01 4.2e-09 0.80 50 7.1e-06 1.1e-02 4.5e-04 1.00e+00 1.427026569e+01 1.428667734e+01 3.8e-09 0.81 51 6.4e-06 1.0e-02 4.0e-04 1.00e+00 1.427136469e+01 1.428613499e+01 3.4e-09 0.82 52 5.8e-06 1.0e-02 3.6e-04 1.00e+00 1.427235289e+01 1.428564569e+01 3.0e-09 0.83 53 5.2e-06 9.8e-03 3.3e-04 1.00e+00 1.427324142e+01 1.428520502e+01 2.7e-09 0.85 54 4.7e-06 9.5e-03 2.9e-04 1.00e+00 1.427404046e+01 1.428480769e+01 2.5e-09 0.86 55 4.2e-06 9.3e-03 2.6e-04 1.00e+00 1.427475907e+01 1.428444986e+01 2.2e-09 0.87 56 3.8e-06 9.1e-03 2.4e-04 1.00e+00 1.427540546e+01 1.428412738e+01 2.0e-09 0.88 57 3.4e-06 9.0e-03 2.1e-04 1.00e+00 1.427598701e+01 1.428383663e+01 1.8e-09 0.89 58 3.1e-06 8.8e-03 1.9e-04 1.00e+00 1.427651020e+01 1.428357479e+01 1.6e-09 0.90 59 2.8e-06 8.7e-03 1.7e-04 1.00e+00 1.427698094e+01 1.428333888e+01 1.5e-09 0.92 60 2.5e-06 8.5e-03 1.6e-04 9.99e-01 1.427740441e+01 1.428312679e+01 1.3e-09 0.93 61 2.2e-06 8.4e-03 1.4e-04 1.00e+00 1.427778550e+01 1.428293546e+01 1.2e-09 0.94 62 2.0e-06 8.3e-03 1.3e-04 9.99e-01 1.427812834e+01 1.428276351e+01 1.1e-09 0.95 63 1.8e-06 8.2e-03 1.1e-04 9.99e-01 1.427843681e+01 1.428260873e+01 9.6e-10 0.96 64 1.6e-06 8.1e-03 1.0e-04 1.00e+00 1.427871445e+01 1.428246909e+01 8.6e-10 0.98 65 1.5e-06 8.1e-03 9.2e-05 1.00e+00 1.427896425e+01 1.428234351e+01 7.7e-10 0.99 66 1.3e-06 8.0e-03 8.3e-05 1.00e+00 1.427918910e+01 1.428223016e+01 7.0e-10 1.00 67 1.2e-06 7.9e-03 7.5e-05 9.99e-01 1.427939136e+01 1.428212845e+01 6.3e-10 1.01 68 1.1e-06 7.9e-03 6.7e-05 9.99e-01 1.427957334e+01 1.428203691e+01 5.6e-10 1.02 69 9.6e-07 7.8e-03 6.0e-05 9.99e-01 1.427973711e+01 1.428195449e+01 5.1e-10 1.04 70 8.6e-07 7.8e-03 5.4e-05 9.98e-01 1.427988447e+01 1.428188032e+01 4.6e-10 1.05 71 7.8e-07 7.7e-03 4.9e-05 1.00e+00 1.428001714e+01 1.428181331e+01 4.1e-10 1.06 72 7.0e-07 7.7e-03 4.4e-05 1.00e+00 1.428013773e+01 1.428175219e+01 3.7e-10 1.07 73 6.3e-07 7.7e-03 4.0e-05 1.00e+00 1.428024502e+01 1.428169806e+01 3.3e-10 1.08 74 5.7e-07 6.9e-03 3.6e-05 1.01e+00 1.428034406e+01 1.428164769e+01 3.0e-10 1.09 75 5.1e-07 6.2e-03 3.2e-05 9.98e-01 1.428043068e+01 1.428160408e+01 2.7e-10 1.10 76 4.6e-07 5.6e-03 2.9e-05 1.00e+00 1.428050884e+01 1.428156451e+01 2.4e-10 1.12 77 4.1e-07 5.0e-03 2.6e-05 1.00e+00 1.428057899e+01 1.428152910e+01 2.2e-10 1.13 78 3.7e-07 4.5e-03 2.3e-05 9.99e-01 1.428064210e+01 1.428149725e+01 2.0e-10 1.15 79 3.3e-07 4.1e-03 2.1e-05 9.92e-01 1.428069884e+01 1.428146877e+01 1.8e-10 1.16 80 3.0e-07 3.7e-03 1.9e-05 1.01e+00 1.428075076e+01 1.428144237e+01 1.6e-10 1.17 81 2.7e-07 3.3e-03 1.7e-05 1.01e+00 1.428079890e+01 1.428141775e+01 1.5e-10 1.19 82 2.4e-07 3.0e-03 1.5e-05 9.97e-01 1.428084000e+01 1.428139705e+01 1.3e-10 1.20 83 2.2e-07 2.7e-03 1.4e-05 1.01e+00 1.428087863e+01 1.428137730e+01 1.2e-10 1.21 84 2.0e-07 2.4e-03 1.2e-05 1.01e+00 1.428091352e+01 1.428135947e+01 1.1e-10 1.22 85 1.8e-07 2.2e-03 1.1e-05 9.94e-01 1.428094313e+01 1.428134461e+01 9.6e-11 1.23 86 1.6e-07 2.0e-03 1.0e-05 1.00e+00 1.428097010e+01 1.428133094e+01 8.7e-11 1.24 87 1.4e-07 1.8e-03 9.1e-06 9.95e-01 1.428099406e+01 1.428131889e+01 7.8e-11 1.25 88 1.3e-07 1.6e-03 8.2e-06 9.97e-01 1.428101563e+01 1.428130802e+01 7.0e-11 1.27 89 1.2e-07 1.4e-03 7.3e-06 1.04e+00 1.428103860e+01 1.428129597e+01 6.4e-11 1.28 90 1.1e-07 1.3e-03 6.6e-06 1.03e+00 1.428105801e+01 1.428128593e+01 5.9e-11 1.29 91 9.5e-08 1.2e-03 6.0e-06 9.56e-01 1.428107310e+01 1.428127868e+01 5.3e-11 1.31 92 8.5e-08 1.0e-03 5.4e-06 9.74e-01 1.428108671e+01 1.428127198e+01 4.8e-11 1.32 93 7.7e-08 9.3e-04 4.8e-06 1.02e+00 1.428109982e+01 1.428126526e+01 4.3e-11 1.33 94 6.9e-08 8.4e-04 4.3e-06 9.93e-01 1.428111080e+01 1.428125976e+01 3.9e-11 1.34 95 6.2e-08 7.6e-04 3.9e-06 9.97e-01 1.428112070e+01 1.428125477e+01 3.5e-11 1.36 96 5.6e-08 6.8e-04 3.5e-06 9.34e-01 1.428112952e+01 1.428125059e+01 3.1e-11 1.37 97 5.0e-08 6.1e-04 3.2e-06 1.01e+00 1.428113788e+01 1.428124628e+01 2.8e-11 1.39 98 4.5e-08 5.5e-04 2.8e-06 9.53e-01 1.428114502e+01 1.428124282e+01 2.6e-11 1.40 99 4.1e-08 5.0e-04 2.6e-06 9.30e-01 1.428115143e+01 1.428123975e+01 2.3e-11 1.41 100 3.7e-08 4.5e-04 2.3e-06 1.02e+00 1.428115779e+01 1.428123641e+01 2.1e-11 1.42 101 3.4e-08 4.0e-04 2.1e-06 9.48e-01 1.428116295e+01 1.428123389e+01 1.9e-11 1.43 102 3.0e-08 3.6e-04 1.9e-06 9.89e-01 1.428116762e+01 1.428123150e+01 1.7e-11 1.45 103 2.7e-08 3.3e-04 1.7e-06 1.02e+00 1.428117230e+01 1.428122903e+01 1.5e-11 1.46 104 2.5e-08 2.9e-04 1.5e-06 1.05e+00 1.428117681e+01 1.428122660e+01 1.4e-11 1.48 105 2.2e-08 2.6e-04 1.4e-06 1.00e+00 1.428118011e+01 1.428122492e+01 1.3e-11 1.49 106 2.0e-08 2.4e-04 1.2e-06 1.01e+00 1.428118321e+01 1.428122330e+01 1.2e-11 1.50 107 1.8e-08 2.1e-04 1.1e-06 1.01e+00 1.428118595e+01 1.428122188e+01 1.0e-11 1.51 108 1.6e-08 1.9e-04 9.9e-07 9.95e-01 1.428118833e+01 1.428122067e+01 9.4e-12 1.53 109 1.5e-08 1.7e-04 8.9e-07 1.02e+00 1.428119064e+01 1.428121946e+01 8.6e-12 1.54 110 1.3e-08 1.6e-04 8.0e-07 9.75e-01 1.428119255e+01 1.428121851e+01 7.7e-12 1.55 111 1.2e-08 1.4e-04 7.2e-07 9.75e-01 1.428119426e+01 1.428121766e+01 6.9e-12 1.56 112 1.1e-08 1.3e-04 6.5e-07 9.74e-01 1.428119580e+01 1.428121689e+01 6.2e-12 1.58 113 9.6e-09 1.1e-04 5.9e-07 1.01e+00 1.428119723e+01 1.428121614e+01 5.6e-12 1.59 114 8.6e-09 1.0e-04 5.3e-07 9.76e-01 1.428119848e+01 1.428121552e+01 5.1e-12 1.60 115 7.7e-09 9.2e-05 4.7e-07 1.01e+00 1.428119966e+01 1.428121490e+01 4.6e-12 1.62 116 6.9e-09 8.3e-05 4.3e-07 9.76e-01 1.428120066e+01 1.428121440e+01 4.1e-12 1.63 117 6.3e-09 7.4e-05 3.8e-07 9.52e-01 1.428120156e+01 1.428121395e+01 3.7e-12 1.65 118 5.6e-09 6.7e-05 3.5e-07 1.07e+00 1.428120263e+01 1.428121335e+01 3.5e-12 1.66 119 5.1e-09 6.0e-05 3.1e-07 1.01e+00 1.428120336e+01 1.428121297e+01 3.1e-12 1.68 120 4.6e-09 5.4e-05 2.8e-07 9.78e-01 1.428120400e+01 1.428121265e+01 2.8e-12 1.69 121 4.1e-09 4.9e-05 2.5e-07 9.49e-01 1.428120456e+01 1.428121238e+01 2.5e-12 1.70 122 3.8e-09 4.4e-05 2.3e-07 9.91e-01 1.428120508e+01 1.428121212e+01 2.3e-12 1.72 123 3.4e-09 4.0e-05 2.0e-07 9.73e-01 1.428120554e+01 1.428121188e+01 2.1e-12 1.73 124 3.0e-09 3.6e-05 1.8e-07 9.67e-01 1.428120596e+01 1.428121168e+01 1.9e-12 1.75 125 2.7e-09 3.2e-05 1.7e-07 9.67e-01 1.428120633e+01 1.428121149e+01 1.7e-12 1.76 126 2.4e-09 2.9e-05 1.5e-07 1.06e+00 1.428120675e+01 1.428121125e+01 1.5e-12 1.77 Interior-point optimizer terminated. Time: 1.77. Optimizer terminated. Time: 1.79 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.4281206753e+01 Viol. con: 3e-08 var: 0e+00 Dual. obj: 1.4281211253e+01 Viol. con: 0e+00 var: 2e-04 * End solution on dual form. * Transforming to primal solution. Solving took 1.82 seconds. result packing took 12% of solve time solution checking took 3.3% of solve time Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : MACOSX/64-X86 Cores : 4 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1012 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 1.67e+04 after factor : 1.72e+05 Factor - dense dim. : 0 flops : 0.00e+00 Factor - GP saved nzs : 0 GP saved flops : 0.00e+00 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.288406701e+05 2.000000000e+00 1.0e+00 0.04 1 1.1e+03 1.4e+03 6.0e+04 -9.71e-01 -1.265938175e+05 3.741347980e+00 4.7e-01 0.06 2 3.9e+02 5.1e+02 2.2e+04 -9.35e-01 -1.197051951e+05 1.137045121e+01 1.7e-01 0.07 3 2.8e+02 3.6e+02 1.6e+04 -8.27e-01 -1.156625895e+05 8.552142189e+01 1.2e-01 0.09 4 2.8e+02 3.6e+02 1.6e+04 -7.56e-01 -1.122976017e+05 2.872321472e+03 1.2e-01 0.10 5 6.3e+01 8.2e+01 3.5e+03 -7.46e-01 -6.619536732e+04 1.271038544e+04 2.8e-02 0.11 6 3.9e+01 5.1e+01 2.2e+03 -6.91e-02 -4.844537929e+04 1.115153891e+04 1.7e-02 0.13 7 2.8e+01 3.6e+01 1.6e+03 2.52e-01 -3.791431313e+04 8.619731531e+03 1.2e-02 0.14 8 1.5e+01 2.0e+01 8.6e+02 4.44e-01 -2.328435911e+04 5.313107855e+03 6.8e-03 0.15 9 6.0e+00 7.7e+00 3.3e+02 6.90e-01 -9.515409828e+03 2.662684666e+03 2.7e-03 0.17 10 3.3e+00 4.2e+00 1.8e+02 8.99e-01 -5.026896801e+03 1.803370375e+03 1.5e-03 0.18 11 1.1e+00 1.4e+00 6.3e+01 9.61e-01 -1.688868294e+03 6.957120438e+02 5.1e-04 0.19 12 9.2e-01 1.3e+00 5.2e+01 9.86e-01 -1.369158163e+03 5.981708123e+02 4.1e-04 0.21 13 7.0e-01 1.2e+00 4.0e+01 9.72e-01 -1.053992189e+03 4.589009827e+02 3.2e-04 0.22 14 3.7e-01 6.3e-01 2.1e+01 9.98e-01 -5.484823519e+02 2.641306531e+02 1.7e-04 0.23 15 1.2e-01 2.2e-01 6.7e+00 9.94e-01 -1.705883670e+02 8.558555560e+01 5.4e-05 0.25 16 8.2e-02 1.7e-01 4.8e+00 1.01e+00 -1.180796582e+02 6.428810300e+01 3.9e-05 0.26 17 3.3e-02 1.1e-01 1.9e+00 1.01e+00 -4.269690979e+01 3.062910524e+01 1.6e-05 0.28 18 1.8e-02 8.2e-02 1.1e+00 1.01e+00 -2.015630876e+01 2.028110290e+01 8.7e-06 0.29 19 1.7e-02 8.0e-02 1.0e+00 1.02e+00 -1.887696319e+01 2.020534080e+01 8.4e-06 0.31 20 1.0e-02 6.0e-02 6.2e-01 1.02e+00 -5.845028948e+00 1.715578959e+01 5.0e-06 0.32 21 4.3e-03 6.0e-02 2.6e-01 1.02e+00 4.114426981e+00 1.377847873e+01 2.1e-06 0.33 22 2.2e-03 5.7e-02 1.3e-01 1.01e+00 7.628991769e+00 1.261891761e+01 1.1e-06 0.34 23 6.0e-04 8.3e-02 3.9e-02 9.80e-01 1.031693955e+01 1.179907082e+01 3.4e-07 0.35 24 1.8e-04 8.8e-02 1.2e-02 9.64e-01 1.108838889e+01 1.156024526e+01 1.1e-07 0.36 25 5.7e-05 8.5e-02 4.2e-03 9.80e-01 1.132954698e+01 1.149081037e+01 3.9e-08 0.38 26 2.1e-05 8.3e-02 1.5e-03 9.93e-01 1.141259491e+01 1.147151384e+01 1.4e-08 0.39 27 7.6e-06 8.1e-02 5.7e-04 9.98e-01 1.144298894e+01 1.146498938e+01 5.4e-09 0.41 28 6.9e-06 7.3e-02 5.1e-04 1.00e+00 1.144491223e+01 1.146471444e+01 4.8e-09 0.42 29 6.2e-06 6.7e-02 4.6e-04 1.00e+00 1.144649823e+01 1.146432105e+01 4.4e-09 0.43 30 5.6e-06 6.1e-02 4.2e-04 1.00e+00 1.144792581e+01 1.146396703e+01 3.9e-09 0.45 31 5.0e-06 5.5e-02 3.7e-04 1.00e+00 1.144920803e+01 1.146364568e+01 3.5e-09 0.46 32 4.5e-06 5.1e-02 3.4e-04 1.00e+00 1.145036089e+01 1.146335519e+01 3.2e-09 0.48 33 4.0e-06 4.6e-02 3.0e-04 1.00e+00 1.145139734e+01 1.146309256e+01 2.9e-09 0.49 34 3.6e-06 4.2e-02 2.7e-04 1.00e+00 1.145232925e+01 1.146285521e+01 2.6e-09 0.51 35 3.3e-06 3.9e-02 2.5e-04 1.00e+00 1.145316725e+01 1.146264083e+01 2.3e-09 0.52 36 3.0e-06 3.6e-02 2.2e-04 1.00e+00 1.145392086e+01 1.146244726e+01 2.1e-09 0.53 37 2.7e-06 3.3e-02 2.0e-04 1.00e+00 1.145459865e+01 1.146227257e+01 1.9e-09 0.54 38 2.4e-06 3.0e-02 1.8e-04 1.00e+00 1.145520829e+01 1.146211496e+01 1.7e-09 0.55 39 2.2e-06 2.8e-02 1.6e-04 1.00e+00 1.145575669e+01 1.146197278e+01 1.5e-09 0.57 40 1.9e-06 2.6e-02 1.4e-04 1.00e+00 1.145625002e+01 1.146184459e+01 1.4e-09 0.58 41 1.7e-06 2.4e-02 1.3e-04 1.00e+00 1.145669386e+01 1.146172900e+01 1.2e-09 0.60 42 1.6e-06 2.2e-02 1.2e-04 1.00e+00 1.145709316e+01 1.146162484e+01 1.1e-09 0.62 43 1.4e-06 2.1e-02 1.1e-04 1.00e+00 1.145745243e+01 1.146153096e+01 1.0e-09 0.63 44 1.3e-06 1.9e-02 9.5e-05 1.00e+00 1.145777568e+01 1.146144640e+01 9.0e-10 0.65 45 1.1e-06 1.8e-02 8.5e-05 1.00e+00 1.145806653e+01 1.146137023e+01 8.1e-10 0.66 46 1.0e-06 1.7e-02 7.7e-05 1.00e+00 1.145832824e+01 1.146130161e+01 7.3e-10 0.68 47 9.3e-07 1.6e-02 6.9e-05 1.00e+00 1.145856373e+01 1.146123983e+01 6.5e-10 0.69 48 8.3e-07 1.5e-02 6.2e-05 1.00e+00 1.145877564e+01 1.146118421e+01 5.9e-10 0.71 49 7.5e-07 1.4e-02 5.6e-05 1.00e+00 1.145896637e+01 1.146113401e+01 5.3e-10 0.72 50 6.8e-07 1.3e-02 5.0e-05 1.00e+00 1.145913799e+01 1.146108884e+01 4.8e-10 0.73 51 6.1e-07 1.3e-02 4.5e-05 1.00e+00 1.145929243e+01 1.146104819e+01 4.3e-10 0.75 52 5.5e-07 1.2e-02 4.1e-05 1.00e+00 1.145943142e+01 1.146101155e+01 3.9e-10 0.76 53 4.9e-07 1.2e-02 3.7e-05 1.00e+00 1.145955650e+01 1.146097859e+01 3.5e-10 0.77 54 1.7e-07 4.0e-03 1.3e-05 1.00e+00 1.146029202e+01 1.146078436e+01 1.2e-10 0.79 55 1.5e-07 3.6e-03 1.1e-05 9.89e-01 1.146033118e+01 1.146077459e+01 1.1e-10 0.80 56 5.3e-08 1.2e-03 3.9e-06 1.00e+00 1.146056193e+01 1.146071327e+01 3.7e-11 0.82 57 4.7e-08 1.1e-03 3.5e-06 9.54e-01 1.146057387e+01 1.146071037e+01 3.3e-11 0.83 58 2.3e-08 2.1e-04 6.8e-07 9.51e-01 1.146066182e+01 1.146068884e+01 7.1e-12 0.85 59 4.2e-08 1.7e-05 5.4e-08 6.40e-01 1.146068285e+01 1.146068548e+01 1.5e-12 0.86 Interior-point optimizer terminated. Time: 0.86. Optimizer terminated. Time: 0.87 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1460682848e+01 Viol. con: 1e-06 var: 0e+00 Dual. obj: 1.1460685476e+01 Viol. con: 0e+00 var: 2e-04 * End solution on dual form. * Transforming to primal solution. Solving took 0.885 seconds. result packing took 18% of solve time solution checking took 5.2% of solve time Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : MACOSX/64-X86 Cores : 4 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1010 Eliminator terminated. Eliminator started. Total number of eliminations : 1022 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1022 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 831 Optimizer - Cones : 0 Optimizer - Scalar variables : 3581 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 1.67e+04 after factor : 1.72e+05 Factor - dense dim. : 0 flops : 0.00e+00 Factor - GP saved nzs : 0 GP saved flops : 0.00e+00 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.288998738e+05 2.000000000e+00 1.0e+00 0.04 1 1.1e+03 1.4e+03 6.0e+04 -9.71e-01 -1.266356782e+05 3.742466303e+00 4.7e-01 0.06 2 3.9e+02 5.0e+02 2.2e+04 -9.35e-01 -1.196284907e+05 1.157203858e+01 1.7e-01 0.07 3 2.8e+02 3.6e+02 1.6e+04 -8.26e-01 -1.157140989e+05 9.724057478e+01 1.2e-01 0.08 4 2.8e+02 3.6e+02 1.6e+04 -7.57e-01 -1.123511293e+05 2.829388016e+03 1.2e-01 0.10 5 7.6e+01 9.8e+01 4.2e+03 -7.46e-01 -7.380967141e+04 1.079459502e+04 3.4e-02 0.11 6 3.7e+01 4.8e+01 2.1e+03 -1.89e-01 -4.675722457e+04 1.109128351e+04 1.7e-02 0.12 7 2.2e+01 2.8e+01 1.2e+03 2.80e-01 -3.081541539e+04 7.269390122e+03 9.5e-03 0.13 8 9.8e+00 1.3e+01 5.5e+02 5.68e-01 -1.544098001e+04 3.913371832e+03 4.4e-03 0.15 9 4.3e+00 5.6e+00 2.4e+02 8.18e-01 -6.768112187e+03 2.130355833e+03 1.9e-03 0.16 10 2.0e+00 2.6e+00 1.1e+02 9.38e-01 -2.992698654e+03 1.174799003e+03 8.8e-04 0.17 11 1.4e+00 1.8e+00 8.0e+01 9.83e-01 -2.138707564e+03 8.478865648e+02 6.3e-04 0.19 12 9.0e-01 1.2e+00 5.1e+01 9.85e-01 -1.363634644e+03 5.635919871e+02 4.1e-04 0.20 13 7.5e-01 1.1e+00 4.3e+01 9.64e-01 -1.152075919e+03 4.738480141e+02 3.4e-04 0.22 14 2.9e-01 4.3e-01 1.6e+01 9.89e-01 -4.269921860e+02 1.973406903e+02 1.3e-04 0.23 15 1.5e-01 2.3e-01 8.6e+00 1.00e+00 -2.190991757e+02 1.087008569e+02 6.9e-05 0.24 16 4.4e-02 1.5e-01 2.6e+00 1.00e+00 -6.101628124e+01 3.727872936e+01 2.1e-05 0.25 17 3.6e-02 1.3e-01 2.1e+00 1.00e+00 -4.921130413e+01 3.255959002e+01 1.8e-05 0.26 18 2.0e-02 9.0e-02 1.2e+00 1.00e+00 -2.393026911e+01 2.130462308e+01 9.7e-06 0.28 19 1.5e-02 7.0e-02 8.7e-01 1.02e+00 -1.436289991e+01 1.845715779e+01 7.1e-06 0.29 20 8.1e-03 4.7e-02 4.8e-01 1.03e+00 -2.350889896e+00 1.563155325e+01 4.0e-06 0.30 21 2.3e-03 8.8e-02 1.4e-01 1.02e+00 7.461337378e+00 1.257956393e+01 1.2e-06 0.31 22 1.2e-03 5.9e-02 7.6e-02 9.89e-01 9.105578203e+00 1.193704105e+01 6.5e-07 0.33 23 4.1e-04 7.4e-02 2.7e-02 9.72e-01 1.056480326e+01 1.158093808e+01 2.4e-07 0.34 24 1.6e-04 6.8e-02 1.1e-02 9.77e-01 1.102200922e+01 1.144791876e+01 1.0e-07 0.35 25 7.0e-05 6.7e-02 4.8e-03 9.91e-01 1.120973433e+01 1.139320258e+01 4.3e-08 0.37 26 3.3e-05 6.3e-02 2.3e-03 9.96e-01 1.128506255e+01 1.137214654e+01 2.1e-08 0.38 27 1.5e-05 6.3e-02 1.1e-03 9.99e-01 1.132162374e+01 1.136210584e+01 9.6e-09 0.39 28 7.4e-06 6.0e-02 5.2e-04 1.00e+00 1.133790034e+01 1.135773455e+01 4.7e-09 0.40 29 6.7e-06 5.4e-02 4.7e-04 1.00e+00 1.133972590e+01 1.135757838e+01 4.3e-09 0.42 30 6.0e-06 5.0e-02 4.2e-04 1.00e+00 1.134106845e+01 1.135713603e+01 3.8e-09 0.43 31 5.4e-06 4.5e-02 3.8e-04 1.00e+00 1.134227911e+01 1.135674027e+01 3.4e-09 0.44 32 4.9e-06 4.2e-02 3.4e-04 1.00e+00 1.134336687e+01 1.135638219e+01 3.1e-09 0.46 33 4.4e-06 3.8e-02 3.1e-04 1.00e+00 1.134434516e+01 1.135605920e+01 2.8e-09 0.47 34 3.9e-06 3.5e-02 2.8e-04 1.00e+00 1.134522489e+01 1.135576775e+01 2.5e-09 0.48 35 3.5e-06 3.2e-02 2.5e-04 1.00e+00 1.134601608e+01 1.135550484e+01 2.3e-09 0.49 36 3.2e-06 3.0e-02 2.2e-04 1.00e+00 1.134672772e+01 1.135526774e+01 2.0e-09 0.51 37 2.9e-06 2.7e-02 2.0e-04 1.00e+00 1.134736784e+01 1.135505398e+01 1.8e-09 0.52 38 2.6e-06 2.5e-02 1.8e-04 1.00e+00 1.134794370e+01 1.135486132e+01 1.7e-09 0.53 39 2.3e-06 2.4e-02 1.6e-04 1.00e+00 1.134846179e+01 1.135468774e+01 1.5e-09 0.54 40 2.1e-06 2.2e-02 1.5e-04 1.00e+00 1.134892793e+01 1.135453138e+01 1.3e-09 0.56 41 1.9e-06 2.0e-02 1.3e-04 1.00e+00 1.134934738e+01 1.135439053e+01 1.2e-09 0.57 42 1.7e-06 1.9e-02 1.2e-04 1.00e+00 1.134972481e+01 1.135426374e+01 1.1e-09 0.58 43 1.5e-06 1.8e-02 1.1e-04 1.00e+00 1.135006448e+01 1.135414956e+01 9.7e-10 0.59 44 1.4e-06 1.7e-02 9.6e-05 1.00e+00 1.135037015e+01 1.135404677e+01 8.8e-10 0.60 45 1.2e-06 1.6e-02 8.7e-05 1.00e+00 1.135064524e+01 1.135395426e+01 7.9e-10 0.61 46 1.1e-06 1.5e-02 7.8e-05 1.00e+00 1.135089283e+01 1.135387099e+01 7.1e-10 0.63 47 1.0e-06 1.4e-02 7.0e-05 1.00e+00 1.135111566e+01 1.135379604e+01 6.4e-10 0.64 48 9.0e-07 1.3e-02 6.3e-05 1.00e+00 1.135131621e+01 1.135372858e+01 5.8e-10 0.65 49 8.1e-07 1.3e-02 5.7e-05 1.00e+00 1.135149672e+01 1.135366787e+01 5.2e-10 0.66 50 7.3e-07 1.2e-02 5.1e-05 1.00e+00 1.135165919e+01 1.135361323e+01 4.7e-10 0.67 51 6.6e-07 1.2e-02 4.6e-05 1.00e+00 1.135180541e+01 1.135356407e+01 4.2e-10 0.68 52 5.9e-07 1.1e-02 4.2e-05 1.00e+00 1.135193703e+01 1.135351981e+01 3.8e-10 0.70 53 5.3e-07 1.1e-02 3.7e-05 1.00e+00 1.135205547e+01 1.135348002e+01 3.4e-10 0.71 54 4.8e-07 1.0e-02 3.4e-05 1.00e+00 1.135216209e+01 1.135344418e+01 3.1e-10 0.72 55 4.3e-07 1.0e-02 3.0e-05 1.00e+00 1.135225804e+01 1.135341194e+01 2.8e-10 0.73 56 3.9e-07 9.8e-03 2.7e-05 1.00e+00 1.135234441e+01 1.135338291e+01 2.5e-10 0.75 57 3.5e-07 9.5e-03 2.5e-05 1.00e+00 1.135242214e+01 1.135335679e+01 2.2e-10 0.76 58 3.1e-07 9.3e-03 2.2e-05 1.00e+00 1.135249210e+01 1.135333328e+01 2.0e-10 0.78 59 2.8e-07 9.0e-03 2.0e-05 1.00e+00 1.135255506e+01 1.135331212e+01 1.8e-10 0.79 60 2.5e-07 8.8e-03 1.8e-05 1.00e+00 1.135261173e+01 1.135329308e+01 1.6e-10 0.81 61 2.3e-07 8.7e-03 1.6e-05 1.00e+00 1.135266272e+01 1.135327596e+01 1.5e-10 0.83 62 2.1e-07 8.5e-03 1.4e-05 1.00e+00 1.135270862e+01 1.135326054e+01 1.3e-10 0.84 63 1.9e-07 8.3e-03 1.3e-05 9.99e-01 1.135274992e+01 1.135324668e+01 1.2e-10 0.85 64 1.7e-07 8.2e-03 1.2e-05 9.99e-01 1.135278710e+01 1.135323420e+01 1.1e-10 0.86 65 1.5e-07 8.1e-03 1.1e-05 1.00e+00 1.135282055e+01 1.135322295e+01 9.6e-11 1.05 66 1.4e-07 8.0e-03 9.5e-06 1.00e+00 1.135285067e+01 1.135321281e+01 8.6e-11 1.29 67 1.2e-07 7.9e-03 8.6e-06 1.00e+00 1.135287777e+01 1.135320370e+01 7.8e-11 1.32 68 1.1e-07 7.8e-03 7.7e-06 9.98e-01 1.135290215e+01 1.135319552e+01 7.0e-11 1.37 69 9.8e-08 7.7e-03 6.9e-06 9.99e-01 1.135292410e+01 1.135318815e+01 6.3e-11 1.40 70 8.9e-08 7.6e-03 6.2e-06 9.99e-01 1.135294385e+01 1.135318151e+01 5.7e-11 1.54 71 8.0e-08 7.6e-03 5.6e-06 9.99e-01 1.135296163e+01 1.135317553e+01 5.1e-11 1.86 72 7.2e-08 7.5e-03 5.1e-06 1.00e+00 1.135297764e+01 1.135317012e+01 4.6e-11 1.98 73 6.5e-08 7.5e-03 4.5e-06 9.99e-01 1.135299203e+01 1.135316528e+01 4.1e-11 2.07 74 5.8e-08 7.4e-03 4.1e-06 1.00e+00 1.135300502e+01 1.135316090e+01 3.7e-11 2.14 75 5.2e-08 7.4e-03 3.7e-06 1.00e+00 1.135301671e+01 1.135315695e+01 3.3e-11 2.66 76 4.7e-08 7.3e-03 3.3e-06 9.99e-01 1.135302720e+01 1.135315342e+01 3.0e-11 2.95 77 4.2e-08 7.3e-03 3.0e-06 1.00e+00 1.135303677e+01 1.135315018e+01 2.7e-11 3.38 78 3.8e-08 7.3e-03 2.7e-06 1.00e+00 1.135304534e+01 1.135314728e+01 2.4e-11 4.01 79 3.4e-08 6.6e-03 2.4e-06 1.01e+00 1.135305312e+01 1.135314464e+01 2.2e-11 4.51 80 3.1e-08 5.9e-03 2.2e-06 1.01e+00 1.135306012e+01 1.135314227e+01 2.0e-11 5.00 81 2.8e-08 5.3e-03 2.0e-06 1.00e+00 1.135306628e+01 1.135314019e+01 1.8e-11 5.40 82 2.5e-08 4.8e-03 1.8e-06 1.00e+00 1.135307181e+01 1.135313833e+01 1.6e-11 6.05 83 2.3e-08 4.3e-03 1.6e-06 1.01e+00 1.135307693e+01 1.135313659e+01 1.5e-11 6.49 84 2.0e-08 3.9e-03 1.4e-06 1.01e+00 1.135308167e+01 1.135313497e+01 1.3e-11 6.93 85 1.8e-08 3.5e-03 1.3e-06 1.00e+00 1.135308566e+01 1.135313363e+01 1.2e-11 7.35 86 1.6e-08 3.2e-03 1.2e-06 1.02e+00 1.135308949e+01 1.135313231e+01 1.1e-11 7.61 87 1.5e-08 2.8e-03 1.0e-06 1.00e+00 1.135309272e+01 1.135313123e+01 9.7e-12 7.93 88 1.3e-08 2.6e-03 9.4e-07 1.00e+00 1.135309560e+01 1.135313027e+01 8.7e-12 7.94 89 1.2e-08 2.3e-03 8.4e-07 9.88e-01 1.135309820e+01 1.135312941e+01 7.9e-12 7.96 90 1.1e-08 2.1e-03 7.6e-07 9.98e-01 1.135310053e+01 1.135312863e+01 7.1e-12 7.97 91 1.4e-09 2.2e-04 8.0e-08 1.01e+00 1.135311931e+01 1.135312226e+01 7.3e-13 8.08 Interior-point optimizer terminated. Time: 8.08. Optimizer terminated. Time: 8.09 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1353119313e+01 Viol. con: 2e-08 var: 0e+00 Dual. obj: 1.1353122258e+01 Viol. con: 0e+00 var: 2e-03 * End solution on dual form. * Transforming to primal solution. Solving took 8.11 seconds. result packing took 4.1% of solve time solution checking took 0.83% of solve time Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : MACOSX/64-X86 Cores : 4 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1012 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 4 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.67e+04 after factor : 1.72e+05 Factor - dense dim. : 0 flops : 0.00e+00 Factor - GP saved nzs : 0 GP saved flops : 0.00e+00 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.288293938e+05 2.000000000e+00 1.0e+00 0.04 1 1.1e+03 1.4e+03 6.0e+04 -9.71e-01 -1.265602744e+05 3.737386399e+00 4.7e-01 0.26 2 3.8e+02 4.9e+02 2.1e+04 -9.35e-01 -1.193807305e+05 1.174272380e+01 1.7e-01 0.27 3 2.8e+02 3.6e+02 1.6e+04 -8.23e-01 -1.156142613e+05 1.083094934e+02 1.2e-01 0.28 4 2.8e+02 3.6e+02 1.5e+04 -7.56e-01 -1.122192171e+05 2.799904447e+03 1.2e-01 0.29 5 7.6e+01 9.8e+01 4.2e+03 -7.45e-01 -7.374220699e+04 1.082357382e+04 3.4e-02 0.31 6 3.6e+01 4.7e+01 2.0e+03 -1.89e-01 -4.564258809e+04 1.110470097e+04 1.6e-02 0.32 7 2.0e+01 2.6e+01 1.1e+03 2.99e-01 -2.889285897e+04 7.167284593e+03 8.9e-03 0.33 8 9.6e+00 1.2e+01 5.4e+02 6.01e-01 -1.507094688e+04 3.884653365e+03 4.3e-03 0.35 9 4.4e+00 5.6e+00 2.4e+02 8.25e-01 -6.840633585e+03 2.132789525e+03 1.9e-03 0.36 10 1.6e+00 2.1e+00 8.8e+01 9.39e-01 -2.330022415e+03 9.750273579e+02 7.0e-04 0.37 11 1.1e+00 1.5e+00 6.4e+01 9.89e-01 -1.687064702e+03 7.037796274e+02 5.1e-04 0.38 12 7.5e-01 9.9e-01 4.3e+01 9.84e-01 -1.140329077e+03 4.823243128e+02 3.4e-04 0.39 13 6.0e-01 7.8e-01 3.4e+01 9.85e-01 -8.873150164e+02 3.932700086e+02 2.7e-04 0.41 14 2.2e-01 2.9e-01 1.2e+01 9.88e-01 -3.281497701e+02 1.436253318e+02 1.0e-04 0.42 15 9.0e-02 1.4e-01 5.2e+00 1.01e+00 -1.298110274e+02 6.747969165e+01 4.2e-05 0.43 16 3.6e-02 9.9e-02 2.1e+00 1.00e+00 -4.860051361e+01 3.127930705e+01 1.7e-05 0.44 17 2.9e-02 8.4e-02 . ---------------------------------------------------------------------- Ran 1 test in 43.210s OK Generating XML reports... 1.7e+00 9.96e-01 -3.782951806e+01 2.775874789e+01 1.4e-05 0.45 18 1.8e-02 6.6e-02 1.1e+00 1.01e+00 -1.989103628e+01 2.054747499e+01 8.8e-06 0.47 19 1.6e-02 5.9e-02 9.4e-01 1.02e+00 -1.598897012e+01 1.956697830e+01 7.7e-06 0.48 20 5.8e-03 6.7e-02 3.4e-01 1.02e+00 1.489501410e+00 1.421978821e+01 2.8e-06 0.49 21 2.0e-03 7.7e-02 1.2e-01 1.02e+00 7.927354811e+00 1.240182595e+01 1.0e-06 0.50 22 1.4e-03 5.8e-02 8.7e-02 9.67e-01 8.833042722e+00 1.205662758e+01 7.5e-07 0.51 23 4.9e-04 6.7e-02 3.2e-02 9.59e-01 1.037967587e+01 1.160988415e+01 2.9e-07 0.53 24 2.0e-04 6.0e-02 1.3e-02 9.57e-01 1.091536080e+01 1.143360511e+01 1.2e-07 0.54 25 1.8e-04 5.5e-02 1.2e-02 9.75e-01 1.095407958e+01 1.142030179e+01 1.1e-07 0.56 26 1.6e-04 5.0e-02 1.1e-02 9.73e-01 1.098988415e+01 1.141004377e+01 9.8e-08 0.57 27 1.5e-04 4.6e-02 9.8e-03 9.75e-01 1.102488785e+01 1.140360520e+01 8.8e-08 0.58 28 1.3e-04 4.2e-02 8.8e-03 9.77e-01 1.105652841e+01 1.139786922e+01 7.9e-08 0.59 29 1.2e-04 3.8e-02 7.9e-03 9.79e-01 1.108501983e+01 1.139264096e+01 7.1e-08 0.61 30 1.1e-04 3.5e-02 7.2e-03 9.81e-01 1.111061417e+01 1.138781721e+01 6.4e-08 0.62 31 9.5e-05 3.2e-02 6.4e-03 9.82e-01 1.113359680e+01 1.138336467e+01 5.8e-08 0.63 32 8.6e-05 3.0e-02 5.8e-03 9.84e-01 1.115422748e+01 1.137925460e+01 5.2e-08 0.64 33 7.7e-05 2.7e-02 5.2e-03 9.85e-01 1.117274240e+01 1.137546192e+01 4.7e-08 0.66 34 6.9e-05 2.5e-02 4.7e-03 9.87e-01 1.118935547e+01 1.137196420e+01 4.2e-08 0.67 35 6.3e-05 2.4e-02 4.2e-03 9.88e-01 1.120425997e+01 1.136874073e+01 3.8e-08 0.68 36 5.6e-05 2.2e-02 3.8e-03 9.89e-01 1.121763068e+01 1.136577286e+01 3.4e-08 0.70 37 5.1e-05 2.0e-02 3.4e-03 9.90e-01 1.122962508e+01 1.136304321e+01 3.1e-08 0.71 38 4.6e-05 1.9e-02 3.1e-03 9.91e-01 1.124038484e+01 1.136053530e+01 2.8e-08 0.73 39 4.1e-05 1.8e-02 2.8e-03 9.92e-01 1.125003725e+01 1.135823351e+01 2.5e-08 0.74 40 3.7e-05 1.7e-02 2.5e-03 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1.00e+00 1.133346267e+01 1.133544767e+01 4.6e-10 1.24 78 6.7e-07 7.2e-03 4.6e-05 1.00e+00 1.133361348e+01 1.133540003e+01 4.1e-10 1.25 79 6.1e-07 7.2e-03 4.1e-05 1.00e+00 1.133374921e+01 1.133535712e+01 3.7e-10 1.27 80 5.5e-07 7.1e-03 3.7e-05 1.00e+00 1.133387136e+01 1.133531848e+01 3.3e-10 1.28 81 4.9e-07 7.1e-03 3.3e-05 1.00e+00 1.133398131e+01 1.133528364e+01 3.0e-10 1.29 82 4.4e-07 7.1e-03 3.0e-05 1.00e+00 1.133408023e+01 1.133525233e+01 2.7e-10 1.31 83 4.0e-07 7.1e-03 2.7e-05 1.00e+00 1.133416926e+01 1.133522413e+01 2.4e-10 1.32 84 3.6e-07 7.0e-03 2.4e-05 9.99e-01 1.133424936e+01 1.133519882e+01 2.2e-10 1.33 85 3.2e-07 7.0e-03 2.2e-05 9.99e-01 1.133432145e+01 1.133517601e+01 2.0e-10 1.34 86 2.9e-07 7.0e-03 2.0e-05 1.00e+00 1.133438634e+01 1.133515543e+01 1.8e-10 1.35 87 2.6e-07 7.0e-03 1.8e-05 1.00e+00 1.133444473e+01 1.133513691e+01 1.6e-10 1.37 88 2.3e-07 7.0e-03 1.6e-05 1.00e+00 1.133449729e+01 1.133512021e+01 1.4e-10 1.38 89 2.1e-07 7.0e-03 1.4e-05 1.00e+00 1.133454458e+01 1.133510522e+01 1.3e-10 1.39 90 1.9e-07 7.0e-03 1.3e-05 1.00e+00 1.133458722e+01 1.133509164e+01 1.2e-10 1.41 91 1.7e-07 7.0e-03 1.2e-05 9.97e-01 1.133462549e+01 1.133507955e+01 1.0e-10 1.42 92 1.5e-07 6.9e-03 1.0e-05 1.00e+00 1.133465996e+01 1.133506859e+01 9.4e-11 1.43 93 1.4e-07 6.9e-03 9.4e-06 9.99e-01 1.133469096e+01 1.133505875e+01 8.5e-11 1.44 94 1.2e-07 6.9e-03 8.5e-06 9.95e-01 1.133471886e+01 1.133504994e+01 7.6e-11 1.46 95 1.1e-07 6.9e-03 7.6e-06 1.00e+00 1.133474398e+01 1.133504193e+01 6.9e-11 1.47 96 1.0e-07 6.9e-03 6.9e-06 9.98e-01 1.133476658e+01 1.133503476e+01 6.2e-11 1.49 97 9.1e-08 6.9e-03 6.2e-06 9.98e-01 1.133478691e+01 1.133502830e+01 5.6e-11 1.50 98 8.2e-08 6.9e-03 5.6e-06 9.98e-01 1.133480521e+01 1.133502249e+01 5.0e-11 1.52 99 7.4e-08 6.9e-03 5.0e-06 9.89e-01 1.133482166e+01 1.133501732e+01 4.5e-11 1.53 100 6.6e-08 6.2e-03 4.5e-06 1.00e+00 1.133483649e+01 1.133501258e+01 4.1e-11 1.54 101 6.0e-08 5.6e-03 4.0e-06 9.98e-01 1.133484984e+01 1.133500832e+01 3.7e-11 1.55 102 5.4e-08 5.0e-03 3.6e-06 1.01e+00 1.133486214e+01 1.133500436e+01 3.3e-11 1.56 103 4.8e-08 4.5e-03 3.3e-06 1.01e+00 1.133487325e+01 1.133500077e+01 3.0e-11 1.58 104 4.4e-08 4.0e-03 3.0e-06 9.98e-01 1.133488292e+01 1.133499770e+01 2.7e-11 1.59 105 3.9e-08 3.6e-03 2.7e-06 9.96e-01 1.133489161e+01 1.133499493e+01 2.4e-11 1.61 106 3.5e-08 3.3e-03 2.4e-06 9.94e-01 1.133489943e+01 1.133499245e+01 2.2e-11 1.62 107 3.2e-08 3.0e-03 2.2e-06 1.01e+00 1.133490692e+01 1.133499001e+01 2.0e-11 1.64 108 2.9e-08 2.7e-03 1.9e-06 1.01e+00 1.133491341e+01 1.133498792e+01 1.8e-11 1.65 109 2.6e-08 2.4e-03 1.7e-06 1.01e+00 1.133491924e+01 1.133498604e+01 1.6e-11 1.66 110 2.3e-08 2.2e-03 1.6e-06 1.01e+00 1.133492449e+01 1.133498435e+01 1.4e-11 1.68 111 4.7e-09 4.1e-04 3.0e-07 9.91e-01 1.133496129e+01 1.133497275e+01 2.8e-12 1.69 112 3.3e-10 2.3e-05 1.7e-08 9.94e-01 1.133496941e+01 1.133497005e+01 1.6e-13 1.71 Interior-point optimizer terminated. Time: 1.71. Optimizer terminated. Time: 1.72 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1334969408e+01 Viol. con: 4e-09 var: 0e+00 Dual. obj: 1.1334970046e+01 Viol. con: 0e+00 var: 2e-04 * End solution on dual form. * Transforming to primal solution. Solving took 1.74 seconds. result packing took 13% of solve time solution checking took 3.3% of solve time Solving took 6 GP solves and 36.9 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 2418945.42998 force_pound * meter but the right hand side evaluated to 2375460.26652 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 32774.3840524 force_pound but the right hand side evaluated to 32399.9999979 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 2.21510116794 meter but the right hand side evaluated to 2.08158998623 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 1243577.59304 joule / kilogram but the right hand side evaluated to 1.56108620499 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 664758.081535 joule / kilogram but the right hand side evaluated to 0.667335981287 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 18.3998944307 meter but the right hand side evaluated to 16.3229091228 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 10.903622596120185 but the right hand side evaluated to 4.78885938102334 (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 10.019784964863485 but the right hand side evaluated to 4.788859371698595 (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 8.144914254479277 but the right hand side evaluated to 4.788859383282723 (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 18.3622490934 meter but the right hand side evaluated to 18.1377347716 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 18.3622490934 meter but the right hand side evaluated to 18.2420728675 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 0.2960360769645103 but the right hand side evaluated to 0.1897390319295513 (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 0.23302198447857414 but the right hand side evaluated to 0.17434702035108607 (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 7.563246028526445 but the right hand side evaluated to 4.730639540469531 (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 7.583088759828249 but the right hand side evaluated to 4.757852746971243 (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 Cloning into 'solar'... Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3) Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0) Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-YcTLDM Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-EPHIZZ/wheels/d5/94/ac/b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12 Successfully built gpfit Collecting git+https://github.com/convexengineering/gassolar.git Cloning https://github.com/convexengineering/gassolar.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-ffDvBR Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2018.4) Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.7.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-CT0MmW/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e Successfully built gassolar Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/solar Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from solar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.1) Requirement already satisfied: gpkitmodels in /Users/jenkins/workspace/gplibrary_PR_Models/mosek (from solar==0.0.0.0) (0.0.0.0) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.3.2) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2018.4) Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2.7.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-WgJmDJ/wheels/1f/1c/61/aec93436439dcd4a965e159a026d3a7ed265e591b64e6d6bfc Successfully built solar Installing collected packages: solar Successfully installed solar-0.0.0.0 Running tests... ---------------------------------------------------------------------- ../Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun) 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 3.08 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 1388463.0636 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 1248776.3259 but bound is 1000000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 82150.9611 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.29645501007 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194395 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 3.02 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 1388463.0578 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 1248776.3207 but bound is 1000000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 82150.9611 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.29645500997 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194385 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.22/GustL.22_(0,). (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) Using solver 'mosek' Solving for 12129 variables. Solving took 2.05 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2510 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 765970.5149 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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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 1.96 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1911 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 862671.9717 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 1.83 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1202 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 987087.2997 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 6269 variables. Solving took 0.824 seconds. Warning: .Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.0863 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1058302.4686 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,). (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) Using solver 'mosek' Solving for 12129 variables. Solving took 2.09 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2510 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 765970.5364 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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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/FlightS..egment.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 2 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1911 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 862671.9718 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 1.88 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1202 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 987087.2997 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 6269 variables. Solving took 0.792 seconds. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.0863 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1058302.4684 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 2.96 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 1388463.0669 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 1248776.3288 but bound is 1000000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 82150.9611 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.29645501012 meter ** 2 / second ** 2 but the right hand side evaluated to 2.296451944 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 2.89 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 1388463.0655 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 .EE ====================================================================== ERROR [9.406s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/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 "/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 "/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 "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 83, in __init__ CostedConstraintSet.__init__(self, cost, constraints, substitutions) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/costed.py", line 21, in __init__ ConstraintSet.__init__(self, constraints, subs) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 58, in __init__ list.__setitem__(self, i, ConstraintSet(constraint)) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 67, in __init__ raise_elementhasnumpybools(constraint) File "/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 [7.652s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/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 "/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 "/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 "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 83, in __init__ CostedConstraintSet.__init__(self, cost, constraints, substitutions) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/costed.py", line 21, in __init__ ConstraintSet.__init__(self, constraints, subs) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 58, in __init__ list.__setitem__(self, i, ConstraintSet(constraint)) File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 67, in __init__ raise_elementhasnumpybools(constraint) File "/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 230.022s FAILED (errors=2) Generating XML reports... bound. Solution is 1248776.3276 but bound is 1000000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 82150.9611 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.29645501007 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194396 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 0.12 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 838075.6768 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 2.32 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 1017215.9272 but bound is 600000.0000 Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,), could cause inaccurate result because it is below lower bound. Solution is 78650.4124 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 2.62125883012 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124747926 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 1.95293542205 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215295 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 1.04275941611 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521706 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 0.467698134217 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697003879 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 0.139006791928 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006573773 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 0.287 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 3.99 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.1418 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1017215.9574 but bound is 600000.0000 Warning: Constraint [dQ_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2,) [N... >= B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2,)*G_M...] is not tight because the left hand side evaluated to 0.546199983583 meter * newton but the right hand side evaluated to 0.54619937481 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,), could cause inaccurate result because it is below lower bound. Solution is 78650.5577 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 2.62125881924 meter ** 2 / second ** 2 but the right hand side evaluated to 2.6212478085 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00042%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(1... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.9529359766 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292347375 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00064%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.04275932764 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275522741 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00039%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(3... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.467698058867 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697044815 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00022%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(4... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.13900678254 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006562766 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%) Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible 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]' Cloning into 'gplibrary'... Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3) Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-k4fObY Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-V9jpZR/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gplibrary Requirement already satisfied: numpy>=1.12 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-2QlTQE/wheels/89/83/63/5c5e519ca7ad1fa93cf087f53642d88b5b0eb066ca83d4bb19 Successfully built gpkitmodels 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 Running tests... ---------------------------------------------------------------------- .......... ---------------------------------------------------------------------- Ran 10 tests in 17.112s OK Generating XML reports... 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 0.0141 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.244 seconds. Using solver 'mosek' Solving for 9 variables. Solving took 0.0156 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.0109 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.0137 seconds. Beginning signomial solve. Solving took 16 GP solves and 1.48 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 100.006556021 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 985.544371521 meter * revolutions_per_minute but the right hand side evaluated to 103.041409431 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 0.420585924963 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573144903 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 0.314645033959 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629895196 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 0.168936438406 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931603972 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 0.0639642380858 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631379982 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 0.0226356535429 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354005877 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%) Using solver 'mosek_cli' Solving for 9 variables. Solving took 0.226 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.27 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.237 seconds. Beginning signomial solve. Solving took 16 GP solves and 4.88 seconds. Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006568341 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%) Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544539109 meter * revolutions_per_minute but the right hand side evaluated to 103.041408191 meter / second (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [dQ_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [N*m]... >= B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement_...] is not tight because the left hand side evaluated to 74.5041627751 meter * newton but the right hand side evaluated to 74.5040725471 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%) Warning: Constraint [-B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement... >= dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [lbf]...] is not tight because the left hand side evaluated to 134.449579759 kilogram * meter / second ** 2 but the right hand side evaluated to 30.2255018449 force_pound (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585903433 meter ** 2 / second ** 2 but the right hand side evaluated to 0.42057303321 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0031%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.314644998908 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629685653 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0049%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.16893640237 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931506563 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.063964051843 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639630073546 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0016%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226356673111 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226353930664 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0012%) Using solver 'mosek' Solving for 13 variables. Solving took 0.0103 seconds. Beginning signomial solve. Solving took 11 GP solves and 1.06 seconds. Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742 Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619897.4168 but bound is 700000.0000 Using solver 'mosek_cli' Solving for 13 variables. Solving took 0.225 seconds. Beginning signomial solve. Solving took 11 GP solves and 3.34 seconds. Warning: Constraint [omega_BladeElementProp/BladeElementPerf_(0,)*r_BladeElementProp/BladeElementPerf_(0,) [m*rpm]... >= Wt_BladeElementProp/BladeElementPerf_(0,) + vt_BladeElementProp/BladeElementPerf_(0,) [m/s]...] is not tight because the left hand side evaluated to 147.268875342 meter * revolutions_per_minute but the right hand side evaluated to 15.4219435408 meter / second (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [dQ_BladeElementProp/BladeElementPerf_(3,) [N*m]... >= B_BladeElementProp/BladeElementPerf_(3,)*G_BladeElementProp/BladeElementPerf_(3,)*Wa_BladeElementPro...] is not tight because the left hand side evaluated to 42.7884411703 meter * newton but the right hand side evaluated to 42.7884887635 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742 Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000 Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3481 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9721 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3856 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9562 but bound is 1000000.0000 Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000 Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000 Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.2729 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.1579 but bound is 700000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000 Cloning into 'eVTOL'... Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 1.333s OK Generating XML reports... adding test for 'aircraft_models.py' USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/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 ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/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 ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/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 ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/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 ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/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 ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/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 ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) [Execution node] check if [macys_VM] is in [[windows10x64, windows7x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] 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 '/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