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Started by upstream project "gpkit_commons_PR_Models" build number 17 originally caused by: GitHub pull request #120 of commit 160a35033d3e8c86df93697211d390fb97088648, no merge conflicts. Building remotely on reynolds in workspace /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > git init /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/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 6d4ad2a7242f7a61f99f81a91f111d5ca42bddea (refs/remotes/origin/pr/120/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 6d4ad2a7242f7a61f99f81a91f111d5ca42bddea # 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/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 repository origin/d8fuselage Seen branch in 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origin/simple_flight_profile Seen branch in repository origin/standard_atmosphere Seen branch in repository origin/sutherland Seen branch in repository origin/tailfoam Seen branch in repository origin/troposphere Seen branch in repository origin/wide_body Seen 153 remote branches > git tag -l # timeout=10 > git rev-parse refs/tags/include^{commit} # timeout=10 > git rev-parse refs/tags/DF70^{commit} # timeout=10 > git rev-parse refs/tags/linking^{commit} # timeout=10 > git rev-parse refs/tags/csv^{commit} # timeout=10 > git rev-parse refs/tags/start^{commit} # timeout=10 > git rev-parse refs/tags/pay^{commit} # timeout=10 > git rev-parse refs/tags/sum^{commit} # timeout=10 > git rev-parse refs/tags/clean^{commit} # timeout=10 > git rev-parse refs/tags/sys^{commit} # timeout=10 > git rev-parse refs/tags/pshaft^{commit} # timeout=10 > git rev-parse refs/tags/solarmd^{commit} # timeout=10 > git rev-parse refs/tags/climb^{commit} # timeout=10 > git rev-parse refs/tags/fuse^{commit} # timeout=10 > git rev-parse refs/tags/mission^{commit} # timeout=10 > git rev-parse refs/tags/discret^{commit} # timeout=10 > git rev-parse refs/tags/plot^{commit} # timeout=10 > git rev-parse refs/tags/md^{commit} # timeout=10 > git rev-parse refs/tags/atm^{commit} # timeout=10 > git rev-parse refs/tags/make^{commit} # timeout=10 > git rev-parse refs/tags/eng^{commit} # timeout=10 Checking out Revision 6d4ad2a7242f7a61f99f81a91f111d5ca42bddea (origin/pr/120/merge, origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f 6d4ad2a7242f7a61f99f81a91f111d5ca42bddea # timeout=3 Commit message: "Merge 160a35033d3e8c86df93697211d390fb97088648 into 662ac9f55e6990e08a236d1fb87442c7d54c6596" Using 'Changelog to branch' strategy. Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [description-setter] Description set: <a title="Merging SimPleAC to master pt. 3 " href="https://github.com/convexengineering/gplibrary/pull/120">PR 120</a>: Merging SimPleAC to master pt. 3 [Execution node] check if [reynolds] is in [[macys, macys_Sierra, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] enabling perform for step [Execute shell] [mosek] $ /bin/bash -xe /tmp/jenkins1349417102935068292.sh + [[ reynolds == *macys* ]] + virtualenv --system-site-packages /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit New python executable in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/python2 Also creating executable in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/python Installing setuptools, pkg_resources, pip, wheel...done. Running virtualenv with interpreter /usr/bin/python2 + . /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/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=/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit ++ export VIRTUAL_ENV ++ _OLD_VIRTUAL_PATH=/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games ++ PATH=/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games ++ export PATH ++ '[' -z '' ']' ++ '[' -z '' ']' ++ _OLD_VIRTUAL_PS1= ++ '[' x '!=' x ']' +++ basename /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit ++ PS1='(venv2_gpkit) ' ++ export PS1 ++ alias pydoc ++ '[' -n /bin/bash ']' ++ hash -r ++ which pip + export PIP=/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip + PIP=/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip + python /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade pip Requirement already up-to-date: pip in ./venv2_gpkit/lib/python2.7/site-packages + [[ reynolds == *reynolds* ]] + export CVXOPT_SUITESPARSE_INC_DIR=/usr/include/suitesparse + CVXOPT_SUITESPARSE_INC_DIR=/usr/include/suitesparse + export PATH=/home/jenkins/.local/bin/:/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games + PATH=/home/jenkins/.local/bin/:/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games + [[ mosek == mosek ]] + [[ reynolds == reynolds-ubuntu16 ]] + export PATH=/home/jenkins/.local/bin/:/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/home/jenkins/mosek/7/tools/platform/linux64x86/bin + PATH=/home/jenkins/.local/bin/:/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/home/jenkins/mosek/7/tools/platform/linux64x86/bin + python /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/setup.py install running install running build running build_py running install_lib creating /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib.linux-x86_64-2.7/mosek/array.py -> /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek creating /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib.linux-x86_64-2.7/mosek/fusion/Utils.py -> /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib.linux-x86_64-2.7/mosek/fusion/__init__.py -> /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib.linux-x86_64-2.7/mosek/fusion/SolverInfo.py -> /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib.linux-x86_64-2.7/mosek/__init__.py -> /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek byte-compiling /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/array.py to array.pyc byte-compiling /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/Utils.py to Utils.pyc byte-compiling /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/__init__.py to __init__.pyc byte-compiling /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/SolverInfo.py to SolverInfo.pyc byte-compiling /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/__init__.py to __init__.pyc running install_data copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../bin/libmosek64.so.7.1 -> /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../bin/libiomp5.so -> /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../bin/libmosekxx7_1.so -> /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../bin/libmosekglb64.so.7.1 -> /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../../../../license.pdf -> /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek running install_egg_info Writing /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/Mosek-7.1.20-py2.7.egg-info Please review the MOSEK license conditions in license.pdf + [[ mosek == cvxopt ]] + [[ mosek == mosek ]] + python -c '__import__("mosek").Env()' + msktestlic Computer Platform : Linux/64-X86 Cores : 20 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: 0.03 ************************************ A license was checked out correctly. ************************************ + export 'GPKITSOLVERS=mosek, mosek_cli' + GPKITSOLVERS='mosek, mosek_cli' + [[ mosek == cvxopt ]] + python /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade xmlrunner Collecting xmlrunner Installing collected packages: xmlrunner Successfully installed xmlrunner-1.7.7 + python /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade pint Collecting pint Installing collected packages: pint Successfully installed pint-0.8.1 + python /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade numpy Collecting numpy Using cached numpy-1.13.3-cp27-cp27mu-manylinux1_x86_64.whl Installing collected packages: numpy Found existing installation: numpy 1.11.0 Not uninstalling numpy at /usr/lib/python2.7/dist-packages, outside environment /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit Successfully installed numpy-1.13.3 + python /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade scipy Collecting scipy Using cached scipy-0.19.1-cp27-cp27mu-manylinux1_x86_64.whl Requirement already up-to-date: numpy>=1.8.2 in ./venv2_gpkit/lib/python2.7/site-packages (from scipy) Installing collected packages: scipy Found existing installation: scipy 0.17.0 Not uninstalling scipy at /usr/lib/python2.7/dist-packages, outside environment /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit Successfully installed scipy-0.19.1 + python /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade ctypesgen Collecting ctypesgen Installing collected packages: ctypesgen Successfully installed ctypesgen-0.post125 + python /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade pandas Collecting pandas Using cached pandas-0.20.3-cp27-cp27mu-manylinux1_x86_64.whl Collecting pytz>=2011k (from pandas) Using cached pytz-2017.2-py2.py3-none-any.whl Collecting python-dateutil (from pandas) Using cached python_dateutil-2.6.1-py2.py3-none-any.whl Requirement already up-to-date: numpy>=1.7.0 in ./venv2_gpkit/lib/python2.7/site-packages (from pandas) Collecting six>=1.5 (from python-dateutil->pandas) Using cached six-1.11.0-py2.py3-none-any.whl Installing collected packages: pytz, six, python-dateutil, pandas Found existing installation: pytz 2014.10 Not uninstalling pytz at /usr/lib/python2.7/dist-packages, outside environment /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit Found existing installation: six 1.10.0 Not uninstalling six at /jenkins/.local/lib/python2.7/site-packages, outside environment /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit Found existing installation: python-dateutil 2.4.2 Not uninstalling python-dateutil at /usr/lib/python2.7/dist-packages, outside environment /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit Successfully installed pandas-0.20.3 python-dateutil-2.6.1 pytz-2017.2 six-1.11.0 + export GPKITBUILD=/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/build_gpkit + GPKITBUILD=/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/build_gpkit ++ which coverage + COVERAGE=/home/jenkins/.local/bin//coverage + python -c 'import scipy; print scipy.__version__' 0.19.1 + python -c 'import numpy; print numpy.__version__' 1.13.3 + python -c 'import pint; print pint.__version__' 0.8.1 + git clone --depth 1 https://github.com/convexengineering/gpkit.git Cloning into 'gpkit'... + python /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit Requirement already satisfied: numpy>=1.8.1 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.5.3.0) Requirement already satisfied: pint in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.5.3.0) Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.5.3.0) Installing collected packages: gpkit Running setup.py develop for gpkit Successfully installed gpkit + python /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek Requirement already satisfied: numpy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) Requirement already satisfied: pint in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) Installing collected packages: gpkitmodels Running setup.py develop for gpkitmodels Successfully installed gpkitmodels + cat /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/env/settings installed_solvers : mosek, mosek_cli mosek_bin_dir : /jenkins/mosek/7/tools/platform/linux64x86/bin + ls /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/build_gpkit expopt.so + python -c 'from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True)' Cloning into 'gpkit-models'... Cloning into 'shopping'... Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 0.597s OK Generating XML reports... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.105 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.0313 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.228 seconds. Cloning into 'jho'... From https://github.com/convexengineering/gpkit-models * branch master -> FETCH_HEAD Note: checking out 'FETCH_HEAD'. You are in 'detached HEAD' state. You can look around, make experimental changes and commit them, and you can discard any commits you make in this state without impacting any branches by performing another checkout. If you want to create a new branch to retain commits you create, you may do so (now or later) by using -b with the checkout command again. Example: git checkout -b <new-branch-name> HEAD is now at 662ac9f... add readme with build status Cannot uninstall requirement gpkit-models, not installed Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit-models Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Requirement already satisfied: pandas in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: python-dateutil in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: numpy>=1.7.0 in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /tmp/pip-Z65tbJ-build Requirement already satisfied: numpy in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: scipy in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit (from gpfit==0.1) Requirement already satisfied: pint in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) Installing collected packages: gpfit Running setup.py install for gpfit: started Running setup.py install for gpfit: finished with status 'done' Successfully installed gpfit-0.1 Running tests... ---------------------------------------------------------------------- ...adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -9.47111312988e-14. Allowing negative dual variable(s) as small as -1.21423314112e-12. Allowing negative dual variable(s) as small as -1.13634102128e-12. Allowing negative dual variable(s) as small as -1.15124880115e-12. Solving took 4 GP solves and 1.95 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -9.90466389461e-14. Allowing negative dual variable(s) as small as -1.18703658014e-12. Allowing negative dual variable(s) as small as -1.13059648449e-12. Allowing negative dual variable(s) as small as -1.15178569807e-12. Solving took 4 GP solves and 1.68 seconds. Allowing negative dual variable(s) as small as -1.56981979499e-12. Allowing negative dual variable(s) as small as -3.96074579384e-12. Allowing negative dual variable(s) as small as -1.78671053647e-12. Allowing negative dual variable(s) as small as -2.08185638867e-12. Allowing negative dual variable(s) as small as -2.08109744715e-12. Allowing negative dual variable(s) as small as -4.80314139156e-13. Allowing negative dual variable(s) as small as -8.94229677285e-13. Allowing negative dual variable(s) as small as -9.41481267946e-13. Allowing negative dual variable(s) as small as -9.43160155011e-13. MTOW [lbs] = 141.59 Zero fuel weight [lbs] = 53.63 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.38838462896e-13. Allowing negative dual variable(s) as small as -9.26242589572e-14. Allowing negative dual variable(s) as small as -1.20164186761e-13. Allowing negative dual variable(s) as small as -1.20525442925e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -9.61917441706e-13. Allowing negative dual variable(s) as small as -2.01716711077e-12. Allowing negative dual variable(s) as small as -1.27541982327e-14. Allowing negative dual variable(s) as small as -1.71969090698e-14. Solving took 4 GP solves and 2.46 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Solving took 4 GP solves and 1.91 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -1.56943815582e-12. Allowing negative dual variable(s) as small as -3.96109967743e-12. Allowing negative dual variable(s) as small as -1.78644338905e-12. Allowing negative dual variable(s) as small as -2.08268818858e-12. Allowing negative dual variable(s) as small as -2.08066897045e-12. Allowing negative dual variable(s) as small as -4.74114454294e-13. Allowing negative dual variable(s) as small as -8.93198167339e-13. Allowing negative dual variable(s) as small as -9.419073594e-13. Allowing negative dual variable(s) as small as -9.43064528379e-13. MTOW [lbs] = 141.59 Zero fuel weight [lbs] = 53.63 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.3170397892e-13. Allowing negative dual variable(s) as small as -9.2364158856e-14. Allowing negative du. ---------------------------------------------------------------------- Ran 4 tests in 58.760s OK Generating XML reports... al variable(s) as small as -1.19361226632e-13. Allowing negative dual variable(s) as small as -1.20466570747e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -9.61297649064e-13. Allowing negative dual variable(s) as small as -2.01675253237e-12. Allowing negative dual variable(s) as small as -1.27118212802e-14. Allowing negative dual variable(s) as small as -1.66097144376e-14. Solving took 4 GP solves and 2.38 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Solving took 4 GP solves and 1.68 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Cloning into 'turbofan'... Cannot uninstall requirement turbofan, not installed Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/turbofan Installing collected packages: turbofan Running setup.py develop for turbofan Successfully installed turbofan From https://github.com/convexengineering/gpkit-models * branch master -> FETCH_HEAD HEAD is now at 662ac9f... add readme with build status Cannot uninstall requirement gpkit-models, not installed Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit-models Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Running tests... ---------------------------------------------------------------------- adding test for 'turbofan/engine_validation.py' adding test for 'turbofan/engine_flight_profile_fleet.py' T_{t_{4.1_{max}}}_FleetMission/Aircraft/Engine has no upper bound Beginning signomial solve. Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Linux/64-X86 Cores : 20 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 987 Eliminator terminated. Eliminator started. Total number of eliminations : 990 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 990 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 : 20 Optimizer - solved problem : the primal Optimizer - Constraints : 329 Optimizer - Cones : 0 Optimizer - Scalar variables : 1038 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.04 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 6388 after factor : 1.11e+04 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 1.2e+03 1.8e+04 2.1e+04 0.00e+00 -2.068680080e+04 1.023181539e-12 1.0e+00 0.07 1 9.0e+02 1.3e+04 1.5e+04 -1.09e-01 -1.772330983e+04 2.816114920e+00 7.3e-01 0.07 2 3.6e+02 5.2e+03 6.0e+03 4.01e-02 -1.101717325e+04 1.002495905e+01 3.0e-01 0.08 3 1.9e+02 2.7e+03 3.1e+03 6.47e-01 -5.771839810e+03 1.375654854e+01 1.7e-01 0.08 4 5.8e+01 8.4e+02 9.8e+02 1.20e+00 -1.604918635e+03 1.625572655e+01 5.7e-02 0.09 5 3.1e+01 4.5e+02 5.2e+02 1.69e+00 -6.741478721e+02 1.621109159e+01 3.1e-02 0.09 6 1.0e+01 1.4e+02 1.7e+02 1.50e+00 -1.669863359e+02 1.570744588e+01 1.0e-02 0.09 7 4.4e+00 6.5e+01 7.4e+01 1.15e+00 -6.548739018e+01 1.497803151e+01 4.8e-03 0.10 8 2.1e+00 3.2e+01 3.6e+01 8.76e-01 -3.005256964e+01 1.440711237e+01 2.4e-03 0.10 9 9.8e-01 1.8e+01 1.7e+01 5.55e-01 -1.315134616e+01 1.384573179e+01 1.2e-03 0.11 10 3.3e-01 6.3e+00 5.6e+00 5.48e-01 1.831260374e+00 1.321132297e+01 4.6e-04 0.11 11 1.5e-01 3.2e+00 2.6e+00 6.35e-01 7.016966888e+00 1.295295961e+01 2.2e-04 0.11 12 9.8e-02 2.6e+00 1.7e+00 7.48e-01 8.807730406e+00 1.282129471e+01 1.5e-04 0.12 13 2.3e-02 1.5e+00 4.1e-01 8.18e-01 1.155765314e+01 1.259121309e+01 4.1e-05 0.12 14 7.4e-03 1.5e+00 1.3e-01 9.41e-01 1.219956454e+01 1.254374827e+01 1.5e-05 0.13 15 2.0e-03 1.5e+00 3.7e-02 9.82e-01 1.242496748e+01 1.252084270e+01 4.4e-06 0.13 16 5.9e-04 1.3e+00 1.1e-02 9.90e-01 1.248692459e+01 1.251548595e+01 1.3e-06 0.13 17 2.4e-04 1.0e+00 4.4e-03 9.79e-01 1.250285127e+01 1.251430574e+01 5.4e-07 0.14 18 2.1e-04 9.6e-01 4.0e-03 9.99e-01 1.250386922e+01 1.251422581e+01 4.8e-07 0.14 19 1.9e-04 8.7e-01 3.6e-03 9.59e-01 1.250480760e+01 1.251416253e+01 4.4e-07 0.15 20 1.7e-04 7.9e-01 3.2e-03 1.01e+00 1.250569062e+01 1.251409866e+01 3.9e-07 0.15 21 1.6e-04 7.2e-01 2.9e-03 9.43e-01 1.250644661e+01 1.251404521e+01 3.5e-07 0.16 22 1.4e-04 6.6e-01 2.6e-03 1.02e+00 1.250720208e+01 1.251399350e+01 3.2e-07 0.16 23 1.3e-04 6.0e-01 2.3e-03 9.12e-01 1.250781960e+01 1.251394778e+01 2.9e-07 0.16 24 1.1e-04 5.5e-01 2.1e-03 1.02e+00 1.250844454e+01 1.251390333e+01 2.6e-07 0.17 25 1.0e-04 5.1e-01 1.9e-03 9.88e-01 1.250895404e+01 1.251386570e+01 2.4e-07 0.17 26 9.2e-05 4.7e-01 1.7e-03 9.38e-01 1.250942558e+01 1.251382848e+01 2.1e-07 0.18 27 8.3e-05 4.3e-01 1.5e-03 9.77e-01 1.250982653e+01 1.251380285e+01 1.9e-07 0.18 28 7.4e-05 3.9e-01 1.4e-03 9.78e-01 1.251019482e+01 1.251377749e+01 1.7e-07 0.18 29 6.7e-05 3.8e-01 1.2e-03 1.10e+00 1.251067871e+01 1.251374447e+01 1.6e-07 0.19 30 6.0e-05 3.5e-01 1.1e-03 9.85e-01 1.251095400e+01 1.251372615e+01 1.5e-07 0.19 31 5.4e-05 3.2e-01 1.0e-03 9.95e-01 1.251120465e+01 1.251371011e+01 1.3e-07 0.19 32 4.9e-05 3.0e-01 9.0e-04 8.00e-01 1.251143277e+01 1.251369386e+01 1.2e-07 0.20 33 4.4e-05 2.8e-01 8.1e-04 8.78e-01 1.251164267e+01 1.251367967e+01 1.1e-07 0.20 34 4.0e-05 2.5e-01 7.3e-04 1.09e+00 1.251193226e+01 1.251365553e+01 1.0e-07 0.20 35 3.6e-05 2.4e-01 6.6e-04 1.25e+00 1.251210938e+01 1.251363964e+01 9.0e-08 0.21 36 3.2e-05 2.1e-01 5.9e-04 1.04e+00 1.251228697e+01 1.251362644e+01 8.3e-08 0.21 37 2.9e-05 1.9e-01 5.3e-04 1.07e+00 1.251246308e+01 1.251361332e+01 7.7e-08 0.22 38 2.6e-05 1.8e-01 4.8e-04 7.91e-01 1.251256472e+01 1.251360763e+01 6.9e-08 0.22 39 2.3e-05 1.6e-01 4.3e-04 2.17e+00 1.251270680e+01 1.251359108e+01 6.2e-08 0.23 40 2.1e-05 1.5e-01 3.9e-04 7.02e-01 1.251277708e+01 1.251358935e+01 5.6e-08 0.23 41 1.9e-05 1.4e-01 3.5e-04 1.33e+00 1.251284928e+01 1.251358633e+01 5.0e-08 0.24 42 1.7e-05 1.3e-01 3.2e-04 7.59e-01 1.251292716e+01 1.251358035e+01 4.5e-08 0.24 43 1.5e-05 1.2e-01 2.8e-04 1.52e+00 1.251300403e+01 1.251357385e+01 4.0e-08 0.24 44 1.4e-05 1.0e-01 2.6e-04 2.30e+00 1.251303501e+01 1.251357595e+01 3.6e-08 0.25 45 1.3e-05 9.3e-02 2.3e-04 1.17e+00 1.251313799e+01 1.251356766e+01 3.5e-08 0.25 46 1.1e-05 8.4e-02 2.1e-04 1.50e+00 1.251318400e+01 1.251356438e+01 3.2e-08 0.26 47 1.0e-05 7.6e-02 1.9e-04 6.97e-01 1.251323241e+01 1.251356001e+01 2.8e-08 0.26 48 9.2e-06 6.8e-02 1.7e-04 9.41e-01 1.251326231e+01 1.251355902e+01 2.6e-08 0.26 49 8.3e-06 6.1e-02 1.5e-04 2.99e+00 1.251329828e+01 1.251355638e+01 2.3e-08 0.27 50 7.5e-06 5.5e-02 1.4e-04 1.00e+00 1.251332369e+01 1.251355540e+01 2.1e-08 0.27 51 6.7e-06 5.0e-02 1.2e-04 1.67e+00 1.251334803e+01 1.251355416e+01 1.9e-08 0.27 52 6.3e-06 4.6e-02 1.1e-04 7.69e+00 1.251340135e+01 1.251354691e+01 1.5e-08 0.28 53 5.6e-06 4.2e-02 1.0e-04 -1.70e+00 1.251340417e+01 1.251354786e+01 1.4e-08 0.28 54 5.4e-06 3.9e-02 9.6e-05 3.91e+00 1.251344123e+01 1.251354517e+01 1.1e-08 0.29 55 4.9e-06 3.5e-02 8.6e-05 -9.23e-01 1.251344845e+01 1.251354547e+01 1.0e-08 0.29 56 4.4e-06 3.2e-02 7.7e-05 1.44e+00 1.251345863e+01 1.251354556e+01 9.2e-09 0.30 57 4.0e-06 2.8e-02 7.0e-05 -1.81e-01 1.251347055e+01 1.251354549e+01 8.2e-09 0.30 58 3.6e-06 2.6e-02 6.1e-05 1.00e+00 1.251347997e+01 1.251354562e+01 7.4e-09 0.30 59 3.2e-06 2.3e-02 5.5e-05 -7.79e-02 1.251348797e+01 1.251354564e+01 6.6e-09 0.31 60 2.9e-06 2.1e-02 5.0e-05 1.00e+00 1.251349367e+01 1.251354575e+01 5.9e-09 0.31 61 8.6e-07 5.1e-03 1.2e-05 6.67e-01 1.251352825e+01 1.251354750e+01 2.3e-09 0.31 62 1.5e-06 2.8e-04 1.6e-05 1.00e+00 1.251352159e+01 1.251354662e+01 1.3e-10 0.32 63 2.4e-06 1.7e-06 2.6e-05 1.00e+00 1.251350557e+01 1.251354657e+01 8.1e-13 0.32 64 2.2e-06 1.6e-06 2.4e-05 1.00e+00 1.251350972e+01 1.251354657e+01 7.2e-13 0.32 65 2.0e-06 1.4e-06 2.1e-05 -8.68e-01 1.251351069e+01 1.251354657e+01 6.5e-13 0.33 66 2.0e-06 2.1e-05 2.1e-05 2.15e-01 1.251351082e+01 1.251354657e+01 6.5e-13 0.33 67 1.8e-06 1.9e-05 2.0e-05 1.00e+00 1.251351240e+01 1.251354657e+01 5.8e-13 0.34 68 1.6e-06 1.7e-05 1.8e-05 4.05e+00 1.251352146e+01 1.251354657e+01 4.8e-13 0.34 69 1.5e-06 1.5e-05 1.7e-05 1.13e+00 1.251352409e+01 1.251354657e+01 4.6e-13 0.34 70 1.4e-06 1.4e-05 1.5e-05 1.61e-01 1.251352442e+01 1.251354657e+01 4.3e-13 0.35 71 1.2e-06 1.3e-05 1.4e-05 1.00e+00 1.251352654e+01 1.251354657e+01 3.9e-13 0.35 72 1.1e-06 1.1e-05 1.3e-05 1.00e+00 1.251352849e+01 1.251354657e+01 3.5e-13 0.35 73 1.0e-06 1.0e-05 1.1e-05 1.00e+00 1.251353011e+01 1.251354657e+01 3.1e-13 0.36 74 9.4e-07 9.7e-06 1.1e-05 -3.40e-01 1.251353036e+01 1.251354657e+01 2.9e-13 0.36 75 8.5e-07 8.7e-06 1.0e-05 1.00e+00 1.251353138e+01 1.251354657e+01 2.6e-13 0.36 76 8.5e-07 8.7e-06 1.0e-05 1.92e+00 1.251353138e+01 1.251354657e+01 2.6e-13 0.37 77 7.5e-07 7.9e-06 9.1e-06 7.68e+00 1.251353372e+01 1.251354657e+01 2.3e-13 0.37 Interior-point optimizer terminated. Time: 0.38. Optimizer terminated. Time: 0.40 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.2513533718e+01 Viol. con: 8e-07 var: 0e+00 Dual. obj: 1.2513546570e+01 Viol. con: 0e+00 var: 2e-06 * End solution on dual form. * Transforming to primal solution. Solving took 0.422 seconds. result packing took 34% of solve time solution checking took 14% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Linux/64-X86 Cores : 20 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1027 Eliminator terminated. Eliminator started. Total number of eliminations : 1039 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1039 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 : 20 Optimizer - solved problem : the primal Optimizer - Constraints : 284 Optimizer - Cones : 0 Optimizer - Scalar variables : 993 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 : 6448 after factor : 1.06e+04 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 2.5e+03 3.7e+03 5.3e+03 0.00e+00 -5.325756637e+03 1.023181539e-12 1.0e+00 0.05 1 8.2e+02 1.2e+03 1.8e+03 1.03e-01 -2.371266859e+03 9.792679717e+00 3.5e-01 0.05 2 3.0e+02 4.5e+02 6.6e+02 1.32e+00 -7.245360697e+02 1.367511733e+01 1.4e-01 0.06 3 1.7e+02 2.5e+02 3.6e+02 1.70e+00 -3.148516461e+02 1.384412666e+01 7.8e-02 0.07 4 3.7e+01 5.7e+01 8.2e+01 1.49e+00 -4.662899925e+01 1.313835852e+01 1.8e-02 0.07 5 1.1e+01 2.0e+01 2.5e+01 1.13e+00 -6.181686216e+00 1.155427500e+01 6.3e-03 0.08 6 2.4e+00 1.0e+01 5.5e+00 1.07e+00 6.968209948e+00 1.071631782e+01 1.6e-03 0.08 7 1.3e+00 9.8e+00 3.1e+00 8.91e-01 8.257360883e+00 1.060244355e+01 9.1e-04 0.09 8 1.1e+00 8.2e+00 2.6e+00 5.62e-01 8.392169379e+00 1.057186061e+01 7.7e-04 0.09 9 6.4e-01 4.8e+00 1.5e+00 5.02e-01 8.893774605e+00 1.047405825e+01 4.6e-04 0.09 10 3.1e-01 3.1e+00 7.3e-01 5.42e-01 9.448291780e+00 1.037319993e+01 2.4e-04 0.10 11 7.9e-02 2.9e+00 2.0e-01 6.37e-01 9.966691040e+00 1.026402209e+01 7.4e-05 0.10 12 2.9e-02 2.9e+00 7.5e-02 8.63e-01 1.011194519e+01 1.022857646e+01 2.9e-05 0.11 13 1.2e-02 2.4e+00 3.0e-02 9.43e-01 1.016567263e+01 1.021409927e+01 1.2e-05 0.11 14 1.1e-02 2.1e+00 2.7e-02 9.76e-01 1.017028039e+01 1.021399004e+01 1.1e-05 0.12 15 9.6e-03 1.9e+00 2.5e-02 9.76e-01 1.017356901e+01 1.021296809e+01 9.9e-06 0.12 16 8.6e-03 1.8e+00 2.2e-02 9.78e-01 1.017654793e+01 1.021205134e+01 8.9e-06 0.12 17 7.8e-03 1.6e+00 2.0e-02 9.80e-01 1.017923515e+01 1.021122353e+01 8.0e-06 0.13 18 7.0e-03 1.5e+00 1.8e-02 9.81e-01 1.018165760e+01 1.021047614e+01 7.2e-06 0.13 19 6.3e-03 1.3e+00 1.6e-02 9.83e-01 1.018384102e+01 1.020980151e+01 6.5e-06 0.14 20 5.7e-03 1.2e+00 1.5e-02 9.85e-01 1.018580877e+01 1.020919277e+01 5.8e-06 0.14 21 5.1e-03 1.1e+00 1.3e-02 9.86e-01 1.018758200e+01 1.020864364e+01 5.2e-06 0.14 22 4.6e-03 1.0e+00 1.2e-02 9.87e-01 1.018917978e+01 1.020814844e+01 4.7e-06 0.15 23 4.1e-03 9.4e-01 1.1e-02 9.88e-01 1.019061939e+01 1.020770199e+01 4.3e-06 0.15 24 3.7e-03 8.6e-01 9.5e-03 9.89e-01 1.019191640e+01 1.020729963e+01 3.8e-06 0.15 25 3.3e-03 8.0e-01 8.6e-03 9.90e-01 1.019308491e+01 1.020693711e+01 3.4e-06 0.16 26 3.0e-03 7.3e-01 7.7e-03 9.91e-01 1.019413761e+01 1.020661059e+01 3.1e-06 0.16 27 2.7e-03 6.8e-01 7.0e-03 9.92e-01 1.019508597e+01 1.020631660e+01 2.8e-06 0.16 28 2.4e-03 6.3e-01 6.3e-03 9.92e-01 1.019594035e+01 1.020605199e+01 2.5e-06 0.17 29 2.2e-03 5.8e-01 5.6e-03 9.93e-01 1.019671006e+01 1.020581390e+01 2.3e-06 0.17 30 2.0e-03 5.4e-01 5.1e-03 9.93e-01 1.019740353e+01 1.020559975e+01 2.0e-06 0.17 31 1.8e-03 5.1e-01 4.6e-03 9.94e-01 1.019802832e+01 1.020540721e+01 1.8e-06 0.18 32 1.6e-03 4.8e-01 4.1e-03 9.95e-01 1.019859126e+01 1.020523416e+01 1.6e-06 0.18 33 1.4e-03 4.5e-01 3.7e-03 9.95e-01 1.019909849e+01 1.020507866e+01 1.5e-06 0.18 34 1.3e-03 4.2e-01 3.3e-03 9.95e-01 1.019955553e+01 1.020493898e+01 1.3e-06 0.19 35 1.2e-03 4.0e-01 3.0e-03 9.96e-01 1.019996735e+01 1.020481353e+01 1.2e-06 0.19 36 1.0e-03 3.7e-01 2.7e-03 9.96e-01 1.020033843e+01 1.020470088e+01 1.1e-06 0.20 37 9.4e-04 3.5e-01 2.4e-03 9.96e-01 1.020067278e+01 1.020459972e+01 9.7e-07 0.20 38 3.0e-04 1.1e-01 7.8e-04 9.97e-01 1.020273089e+01 1.020398729e+01 3.1e-07 0.20 39 2.7e-04 1.0e-01 7.0e-04 9.99e-01 1.020282875e+01 1.020395953e+01 2.8e-07 0.21 40 1.0e-04 3.9e-02 2.7e-04 9.99e-01 1.020337064e+01 1.020380423e+01 1.1e-07 0.21 41 9.3e-05 3.5e-02 2.4e-04 1.00e+00 1.020340341e+01 1.020379364e+01 9.7e-08 0.21 42 8.4e-05 3.2e-02 2.2e-04 1.00e+00 1.020343379e+01 1.020378502e+01 8.7e-08 0.22 43 7.5e-05 2.8e-02 2.0e-04 1.00e+00 1.020346118e+01 1.020377728e+01 7.8e-08 0.22 44 6.8e-05 2.6e-02 1.8e-04 1.00e+00 1.020348584e+01 1.020377034e+01 7.1e-08 0.22 45 6.1e-05 2.3e-02 1.6e-04 1.00e+00 1.020350805e+01 1.020376411e+01 6.3e-08 0.23 46 5.5e-05 2.1e-02 1.4e-04 1.00e+00 1.020352805e+01 1.020375851e+01 5.7e-08 0.23 47 5.0e-05 1.9e-02 1.3e-04 1.00e+00 1.020354606e+01 1.020375347e+01 5.1e-08 0.23 48 4.5e-05 1.7e-02 1.2e-04 1.00e+00 1.020356228e+01 1.020374895e+01 4.6e-08 0.24 49 4.0e-05 1.5e-02 1.0e-04 1.00e+00 1.020357687e+01 1.020374488e+01 4.2e-08 0.24 50 3.6e-05 1.4e-02 9.3e-05 1.00e+00 1.020359002e+01 1.020374123e+01 3.7e-08 0.24 51 3.2e-05 1.2e-02 8.4e-05 1.00e+00 1.020360185e+01 1.020373794e+01 3.4e-08 0.25 52 2.9e-05 1.1e-02 7.6e-05 1.00e+00 1.020361251e+01 1.020373499e+01 3.0e-08 0.25 53 2.6e-05 9.9e-03 6.8e-05 1.00e+00 1.020362210e+01 1.020373233e+01 2.7e-08 0.25 54 2.4e-05 8.9e-03 6.1e-05 1.00e+00 1.020363073e+01 1.020372995e+01 2.5e-08 0.26 55 4.7e-06 1.8e-03 1.2e-05 1.00e+00 1.020369307e+01 1.020371286e+01 4.9e-09 0.26 56 2.6e-07 1.0e-04 6.9e-07 1.00e+00 1.020370771e+01 1.020370883e+01 2.8e-10 0.26 57 1.4e-09 5.1e-07 3.9e-09 9.97e-01 1.020370859e+01 1.020370859e+01 2.0e-12 0.27 Interior-point optimizer terminated. Time: 0.27. Optimizer terminated. Time: 0.30 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0203708586e+01 Viol. con: 2e-09 var: 0e+00 Dual. obj: 1.0203708592e+01 Viol. con: 0e+00 var: 2e-07 * End solution on dual form. * Transforming to primal solution. Solving took 0.322 seconds. result packing took 35% of solve time solution checking took 16% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Linux/64-X86 Cores : 20 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1026 Eliminator terminated. Eliminator started. Total number of eliminations : 1041 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1041 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 : 20 Optimizer - solved problem : the primal Optimizer - Constraints : 286 Optimizer - Cones : 0 Optimizer - Scalar variables : 995 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 6537 after factor : 1.08e+04 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 2.7e+03 3.8e+03 5.3e+03 0.00e+00 -5.251121697e+03 1.023181539e-12 1.0e+00 0.05 1 8.6e+02 1.2e+03 1.7e+03 6.91e-03 -2.364367375e+03 9.864623595e+00 3.4e-01 0.05 2 3.9e+02 5.3e+02 7.6e+02 1.39e+00 -8.727659085e+02 1.336999675e+01 1.6e-01 0.06 3 3.6e+02 4.9e+02 7.0e+02 1.66e+00 -7.530375575e+02 1.344253930e+01 1.5e-01 0.06 4 1.5e+02 2.1e+02 3.0e+02 1.62e+00 -2.485548346e+02 1.390020333e+01 6.8e-02 0.06 5 4.0e+01 5.6e+01 8.0e+01 1.47e+00 -4.351515881e+01 1.303626013e+01 1.9e-02 0.07 6 1.0e+01 1.9e+01 2.1e+01 1.13e+00 -2.510178360e+00 1.139217737e+01 5.4e-03 0.07 7 5.3e+00 9.9e+00 1.1e+01 9.94e-01 3.647741830e+00 1.098758593e+01 2.9e-03 0.07 8 2.1e+00 1.1e+01 4.4e+00 9.83e-01 7.610043907e+00 1.068230268e+01 1.3e-03 0.08 9 1.9e+00 9.7e+00 4.0e+00 6.80e-01 7.723905695e+00 1.066267061e+01 1.1e-03 0.08 10 1.8e+00 9.1e+00 3.7e+00 6.27e-01 7.519343571e+00 1.065797510e+01 1.1e-03 0.09 11 5.6e-01 7.7e+00 1.2e+00 6.30e-01 9.160191312e+00 1.044563849e+01 3.7e-04 0.09 12 4.2e-01 7.7e+00 9.0e-01 4.74e-01 9.324597354e+00 1.040415320e+01 2.9e-04 0.09 13 9.2e-02 3.4e+00 2.1e-01 5.40e-01 9.935489196e+00 1.025961707e+01 8.4e-05 0.10 14 2.6e-02 3.0e+00 6.2e-02 8.67e-01 1.011326068e+01 1.021253682e+01 2.7e-05 0.10 15 8.3e-03 2.9e+00 2.1e-02 9.67e-01 1.016493941e+01 1.019837810e+01 9.2e-06 0.10 16 3.0e-03 2.7e+00 7.6e-03 9.91e-01 1.018150150e+01 1.019383582e+01 3.4e-06 0.11 17 1.3e-03 2.2e+00 3.2e-03 9.97e-01 1.018701152e+01 1.019224213e+01 1.5e-06 0.11 18 5.9e-04 1.9e+00 1.5e-03 9.98e-01 1.018921478e+01 1.019161093e+01 6.7e-07 0.12 19 2.7e-04 1.8e+00 6.7e-04 9.98e-01 1.019023104e+01 1.019132474e+01 3.1e-07 0.12 20 1.2e-04 1.7e+00 3.0e-04 9.93e-01 1.019070398e+01 1.019119360e+01 1.4e-07 0.12 21 1.1e-04 1.6e+00 2.7e-04 8.69e-01 1.019071153e+01 1.019123118e+01 1.2e-07 0.13 22 1.0e-04 1.6e+00 2.6e-04 9.27e-01 1.019075254e+01 1.019120228e+01 1.2e-07 0.13 23 7.7e-05 1.2e+00 1.9e-04 7.62e-01 1.019083764e+01 1.019121642e+01 8.8e-08 0.13 24 3.8e-05 5.7e-01 9.5e-05 9.93e-01 1.019099571e+01 1.019118163e+01 4.3e-08 0.14 25 3.4e-05 5.5e-01 8.5e-05 9.94e-01 1.019100736e+01 1.019117478e+01 3.9e-08 0.14 26 3.0e-05 5.1e-01 7.7e-05 9.91e-01 1.019102156e+01 1.019117212e+01 3.5e-08 0.14 27 2.7e-05 4.7e-01 6.9e-05 9.89e-01 1.019103444e+01 1.019116994e+01 3.2e-08 0.14 28 2.5e-05 4.4e-01 6.2e-05 9.89e-01 1.019104609e+01 1.019116812e+01 2.8e-08 0.15 29 2.2e-05 4.1e-01 5.6e-05 9.91e-01 1.019105662e+01 1.019116653e+01 2.6e-08 0.15 30 2.0e-05 3.8e-01 5.0e-05 9.93e-01 1.019106611e+01 1.019116509e+01 2.3e-08 0.15 31 1.8e-05 3.5e-01 4.5e-05 9.95e-01 1.019107465e+01 1.019116378e+01 2.1e-08 0.16 32 1.6e-05 3.3e-01 4.1e-05 9.96e-01 1.019108234e+01 1.019116259e+01 1.9e-08 0.16 33 1.5e-05 3.1e-01 3.7e-05 9.97e-01 1.019108927e+01 1.019116150e+01 1.7e-08 0.16 34 1.3e-05 3.0e-01 3.3e-05 9.98e-01 1.019109550e+01 1.019116052e+01 1.5e-08 0.17 35 1.2e-05 2.8e-01 3.0e-05 9.98e-01 1.019110111e+01 1.019115963e+01 1.4e-08 0.17 36 1.1e-05 2.7e-01 2.7e-05 9.98e-01 1.019110616e+01 1.019115884e+01 1.2e-08 0.17 37 9.6e-06 2.5e-01 2.4e-05 9.99e-01 1.019111070e+01 1.019115812e+01 1.1e-08 0.18 38 8.6e-06 2.4e-01 2.2e-05 9.99e-01 1.019111480e+01 1.019115747e+01 9.9e-09 0.18 39 7.7e-06 2.3e-01 1.9e-05 9.99e-01 1.019111848e+01 1.019115689e+01 8.9e-09 0.18 40 7.0e-06 2.2e-01 1.8e-05 9.99e-01 1.019112180e+01 1.019115637e+01 8.0e-09 0.18 41 6.3e-06 2.2e-01 1.6e-05 1.00e+00 1.019112479e+01 1.019115591e+01 7.2e-09 0.19 42 5.6e-06 2.1e-01 1.4e-05 9.99e-01 1.019112748e+01 1.019115549e+01 6.5e-09 0.19 43 5.1e-06 2.0e-01 1.3e-05 1.00e+00 1.019112990e+01 1.019115511e+01 5.9e-09 0.19 44 4.6e-06 2.0e-01 1.2e-05 9.99e-01 1.019113208e+01 1.019115477e+01 5.3e-09 0.20 45 4.1e-06 1.9e-01 1.0e-05 1.00e+00 1.019113404e+01 1.019115446e+01 4.7e-09 0.20 46 3.7e-06 1.9e-01 9.3e-06 9.99e-01 1.019113581e+01 1.019115419e+01 4.3e-09 0.20 47 3.3e-06 1.8e-01 8.4e-06 1.00e+00 1.019113740e+01 1.019115394e+01 3.8e-09 0.20 48 3.0e-06 1.8e-01 7.6e-06 1.00e+00 1.019113883e+01 1.019115372e+01 3.5e-09 0.21 49 2.7e-06 1.7e-01 6.8e-06 1.00e+00 1.019114012e+01 1.019115352e+01 3.1e-09 0.21 50 2.4e-06 1.7e-01 6.1e-06 1.00e+00 1.019114128e+01 1.019115334e+01 2.8e-09 0.21 51 2.2e-06 1.7e-01 5.5e-06 1.00e+00 1.019114233e+01 1.019115318e+01 2.5e-09 0.22 52 2.0e-06 1.6e-01 5.0e-06 1.00e+00 1.019114327e+01 1.019115304e+01 2.3e-09 0.22 53 1.8e-06 1.6e-01 4.5e-06 1.00e+00 1.019114411e+01 1.019115291e+01 2.0e-09 0.22 54 1.6e-06 1.6e-01 4.0e-06 1.00e+00 1.019114488e+01 1.019115279e+01 1.8e-09 0.23 55 1.4e-06 1.6e-01 3.6e-06 1.00e+00 1.019114556e+01 1.019115268e+01 1.7e-09 0.23 56 1.3e-06 1.6e-01 3.3e-06 9.99e-01 1.019114618e+01 1.019115259e+01 1.5e-09 0.23 57 1.2e-06 1.6e-01 2.9e-06 9.99e-01 1.019114674e+01 1.019115250e+01 1.3e-09 0.23 58 1.0e-06 1.5e-01 2.6e-06 9.99e-01 1.019114724e+01 1.019115243e+01 1.2e-09 0.24 59 9.4e-07 1.5e-01 2.4e-06 9.99e-01 1.019114769e+01 1.019115236e+01 1.1e-09 0.24 60 8.5e-07 1.5e-01 2.1e-06 9.98e-01 1.019114809e+01 1.019115230e+01 9.8e-10 0.24 61 7.6e-07 1.5e-01 1.9e-06 1.00e+00 1.019114846e+01 1.019115224e+01 8.8e-10 0.25 62 6.9e-07 1.5e-01 1.7e-06 1.00e+00 1.019114878e+01 1.019115219e+01 7.9e-10 0.25 63 6.2e-07 1.5e-01 1.6e-06 9.97e-01 1.019114908e+01 1.019115215e+01 7.1e-10 0.25 64 5.6e-07 1.5e-01 1.4e-06 9.99e-01 1.019114935e+01 1.019115210e+01 6.4e-10 0.26 65 5.0e-07 1.5e-01 1.3e-06 1.00e+00 1.019114959e+01 1.019115207e+01 5.8e-10 0.26 66 4.5e-07 1.3e-01 1.1e-06 1.01e+00 1.019114981e+01 1.019115203e+01 5.2e-10 0.26 67 4.1e-07 1.2e-01 1.0e-06 9.94e-01 1.019115000e+01 1.019115201e+01 4.7e-10 0.26 68 3.6e-07 1.1e-01 9.2e-07 1.00e+00 1.019115017e+01 1.019115198e+01 4.2e-10 0.27 69 3.3e-07 9.7e-02 8.3e-07 1.01e+00 1.019115033e+01 1.019115195e+01 3.8e-10 0.27 70 3.0e-07 8.7e-02 7.4e-07 9.98e-01 1.019115047e+01 1.019115193e+01 3.4e-10 0.27 71 2.7e-07 7.8e-02 6.7e-07 9.92e-01 1.019115060e+01 1.019115191e+01 3.1e-10 0.28 72 2.4e-07 7.0e-02 6.0e-07 1.00e+00 1.019115071e+01 1.019115190e+01 2.8e-10 0.28 73 2.2e-07 6.3e-02 5.4e-07 9.96e-01 1.019115082e+01 1.019115188e+01 2.5e-10 0.28 74 1.9e-07 5.7e-02 4.9e-07 9.98e-01 1.019115091e+01 1.019115187e+01 2.2e-10 0.29 75 1.7e-07 5.1e-02 4.4e-07 9.84e-01 1.019115099e+01 1.019115185e+01 2.0e-10 0.29 76 1.6e-07 4.6e-02 4.0e-07 1.02e+00 1.019115107e+01 1.019115184e+01 1.8e-10 0.29 77 1.4e-07 4.2e-02 3.6e-07 1.01e+00 1.019115114e+01 1.019115183e+01 1.7e-10 0.29 78 1.3e-07 3.7e-02 3.2e-07 1.01e+00 1.019115120e+01 1.019115182e+01 1.5e-10 0.30 79 1.1e-07 3.4e-02 2.9e-07 9.90e-01 1.019115126e+01 1.019115181e+01 1.3e-10 0.30 80 1.0e-07 3.0e-02 2.6e-07 1.03e+00 1.019115131e+01 1.019115181e+01 1.2e-10 0.30 81 9.3e-08 2.7e-02 2.3e-07 9.70e-01 1.019115135e+01 1.019115180e+01 1.1e-10 0.31 82 5.4e-09 1.6e-03 1.4e-08 9.57e-01 1.019115172e+01 1.019115175e+01 8.4e-12 0.31 83 4.9e-09 1.4e-03 1.2e-08 1.00e+00 1.019115172e+01 1.019115175e+01 7.5e-12 0.31 84 4.8e-10 1.1e-04 9.4e-10 1.10e+00 1.019115174e+01 1.019115174e+01 4.5e-13 0.32 Interior-point optimizer terminated. Time: 0.32. Optimizer terminated. Time: 0.34 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0191151740e+01 Viol. con: 4e-10 var: 0e+00 Dual. obj: 1.0191151741e+01 Viol. con: 0e+00 var: 4e-05 * End solution on dual form. * Transforming to primal solution. Solving took 0.363 seconds. result packing took 42% of solve time solution checking took 23% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Linux/64-X86 Cores : 20 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1026 Eliminator terminated. Eliminator started. Total number of eliminations : 1043 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1043 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 : 20 Optimizer - solved problem : the primal Optimizer - Constraints : 286 Optimizer - Cones : 0 Optimizer - Scalar variables : 995 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 : 6557 after factor : 1.08e+04 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 2.5e+03 3.8e+03 7.7e+03 0.00e+00 -7.710634219e+03 1.023181539e-12 1.0e+00 0.06 1 7.9e+02 1.2e+03 2.4e+03 -1.02e-03 -3.455815973e+03 9.887470561e+00 3.4e-01 0.06 2 5.9e+02 8.8e+02 1.8e+03 1.40e+00 -2.233543660e+03 1.170313279e+01 2.5e-01 0.06 3 3.6e+02 5.3e+02 1.1e+03 1.45e+00 -1.157846755e+03 1.326815640e+01 1.6e-01 0.06 4 1.2e+02 1.8e+02 3.8e+02 1.58e+00 -2.954576803e+02 1.395262261e+01 5.6e-02 0.07 5 3.9e+01 6.0e+01 1.2e+02 1.45e+00 -7.301335947e+01 1.289186321e+01 1.9e-02 0.07 6 9.7e+00 2.0e+01 3.0e+01 1.14e+00 -8.861755138e+00 1.133463102e+01 5.4e-03 0.07 7 2.4e+00 1.5e+01 7.6e+00 1.01e+00 5.597942485e+00 1.067653219e+01 1.5e-03 0.08 8 2.2e+00 1.4e+01 7.0e+00 7.89e-01 5.808260413e+00 1.066015633e+01 1.4e-03 0.08 9 1.0e+00 9.8e+00 3.3e+00 7.43e-01 7.722057236e+00 1.051633303e+01 7.2e-04 0.08 10 8.0e-01 9.9e+00 2.6e+00 4.53e-01 8.056007060e+00 1.047012355e+01 5.6e-04 0.09 11 3.9e-01 6.6e+00 1.3e+00 4.91e-01 8.908552153e+00 1.036283697e+01 2.9e-04 0.09 12 2.8e-01 4.8e+00 9.2e-01 5.43e-01 9.174057863e+00 1.032567825e+01 2.1e-04 0.09 13 4.9e-02 4.0e+00 1.7e-01 6.16e-01 9.948200214e+00 1.021226767e+01 5.3e-05 0.09 14 1.5e-02 3.7e+00 5.3e-02 9.08e-01 1.010040316e+01 1.018375019e+01 1.7e-05 0.10 15 5.9e-03 3.4e+00 2.1e-02 9.80e-01 1.014208309e+01 1.017613382e+01 7.2e-06 0.10 16 1.4e-03 3.2e+00 5.0e-03 9.91e-01 1.016356048e+01 1.017158508e+01 1.7e-06 0.10 17 3.5e-04 3.2e+00 1.3e-03 9.97e-01 1.016855827e+01 1.017058435e+01 4.4e-07 0.10 18 8.7e-05 3.1e+00 3.2e-04 9.99e-01 1.016983601e+01 1.017034908e+01 1.1e-07 0.11 19 2.2e-05 2.9e+00 8.2e-05 9.99e-01 1.017015666e+01 1.017028719e+01 2.9e-08 0.11 20 2.0e-05 2.6e+00 7.4e-05 9.98e-01 1.017016683e+01 1.017028461e+01 2.6e-08 0.11 21 1.8e-05 2.4e+00 6.6e-05 9.98e-01 1.017017673e+01 1.017028276e+01 2.3e-08 0.12 22 1.6e-05 2.2e+00 6.0e-05 9.99e-01 1.017018567e+01 1.017028111e+01 2.1e-08 0.12 23 1.4e-05 2.0e+00 5.4e-05 9.99e-01 1.017019372e+01 1.017027963e+01 1.9e-08 0.12 24 1.3e-05 1.8e+00 4.8e-05 9.99e-01 1.017020097e+01 1.017027829e+01 1.7e-08 0.12 25 1.2e-05 1.6e+00 4.3e-05 1.00e+00 1.017020749e+01 1.017027708e+01 1.5e-08 0.13 26 1.1e-05 1.5e+00 3.9e-05 1.00e+00 1.017021337e+01 1.017027599e+01 1.4e-08 0.13 27 9.5e-06 1.4e+00 3.5e-05 1.00e+00 1.017021865e+01 1.017027502e+01 1.2e-08 0.13 28 8.5e-06 1.2e+00 3.2e-05 1.00e+00 1.017022341e+01 1.017027414e+01 1.1e-08 0.13 29 7.7e-06 1.1e+00 2.9e-05 1.00e+00 1.017022769e+01 1.017027335e+01 1.0e-08 0.14 30 6.9e-06 1.0e+00 2.6e-05 1.00e+00 1.017023154e+01 1.017027263e+01 9.1e-09 0.14 31 6.2e-06 9.5e-01 2.3e-05 1.00e+00 1.017023501e+01 1.017027199e+01 8.2e-09 0.14 32 5.6e-06 8.7e-01 2.1e-05 1.00e+00 1.017023813e+01 1.017027142e+01 7.4e-09 0.14 33 5.0e-06 8.0e-01 1.9e-05 1.00e+00 1.017024094e+01 1.017027090e+01 6.6e-09 0.15 34 4.5e-06 7.4e-01 1.7e-05 1.00e+00 1.017024347e+01 1.017027043e+01 6.0e-09 0.15 35 4.1e-06 6.8e-01 1.5e-05 1.00e+00 1.017024575e+01 1.017027001e+01 5.4e-09 0.15 36 3.7e-06 6.3e-01 1.4e-05 1.00e+00 1.017024779e+01 1.017026963e+01 4.8e-09 0.15 37 3.3e-06 5.9e-01 1.2e-05 9.99e-01 1.017024964e+01 1.017026929e+01 4.4e-09 0.16 38 3.0e-06 5.5e-01 1.1e-05 9.99e-01 1.017025130e+01 1.017026898e+01 3.9e-09 0.16 39 2.7e-06 5.1e-01 9.9e-06 1.00e+00 1.017025279e+01 1.017026871e+01 3.5e-09 0.16 40 2.4e-06 4.8e-01 8.9e-06 1.00e+00 1.017025413e+01 1.017026846e+01 3.2e-09 0.17 41 2.2e-06 4.5e-01 8.1e-06 9.99e-01 1.017025534e+01 1.017026824e+01 2.9e-09 0.17 42 2.0e-06 4.2e-01 7.2e-06 9.99e-01 1.017025643e+01 1.017026804e+01 2.6e-09 0.17 43 1.8e-06 4.0e-01 6.5e-06 1.00e+00 1.017025741e+01 1.017026785e+01 2.3e-09 0.17 44 1.6e-06 3.7e-01 5.9e-06 1.00e+00 1.017025829e+01 1.017026769e+01 2.1e-09 0.18 45 1.4e-06 3.5e-01 5.3e-06 9.99e-01 1.017025908e+01 1.017026754e+01 1.9e-09 0.18 46 1.3e-06 3.4e-01 4.8e-06 1.00e+00 1.017025980e+01 1.017026741e+01 1.7e-09 0.18 47 1.2e-06 3.2e-01 4.3e-06 1.00e+00 1.017026044e+01 1.017026729e+01 1.5e-09 0.18 48 1.0e-06 3.1e-01 3.9e-06 1.00e+00 1.017026102e+01 1.017026719e+01 1.4e-09 0.19 49 9.3e-07 2.9e-01 3.5e-06 1.00e+00 1.017026154e+01 1.017026709e+01 1.2e-09 0.19 50 8.4e-07 2.8e-01 3.1e-06 1.00e+00 1.017026201e+01 1.017026700e+01 1.1e-09 0.19 51 7.6e-07 2.7e-01 2.8e-06 1.00e+00 1.017026243e+01 1.017026692e+01 1.0e-09 0.19 52 6.8e-07 2.6e-01 2.5e-06 1.00e+00 1.017026281e+01 1.017026685e+01 9.0e-10 0.20 53 6.1e-07 2.5e-01 2.3e-06 9.99e-01 1.017026315e+01 1.017026679e+01 8.1e-10 0.20 54 5.5e-07 2.5e-01 2.0e-06 1.00e+00 1.017026346e+01 1.017026673e+01 7.3e-10 0.20 55 5.0e-07 2.4e-01 1.8e-06 1.00e+00 1.017026373e+01 1.017026668e+01 6.5e-10 0.20 56 4.5e-07 2.3e-01 1.7e-06 1.00e+00 1.017026398e+01 1.017026664e+01 5.9e-10 0.21 57 4.0e-07 2.3e-01 1.5e-06 1.00e+00 1.017026421e+01 1.017026659e+01 5.3e-10 0.21 58 3.6e-07 2.2e-01 1.3e-06 9.99e-01 1.017026441e+01 1.017026656e+01 4.8e-10 0.21 59 3.3e-07 2.2e-01 1.2e-06 9.95e-01 1.017026459e+01 1.017026652e+01 4.3e-10 0.21 60 2.9e-07 2.2e-01 1.1e-06 9.95e-01 1.017026475e+01 1.017026649e+01 3.9e-10 0.22 61 2.6e-07 2.1e-01 9.8e-07 1.00e+00 1.017026490e+01 1.017026647e+01 3.5e-10 0.22 62 2.4e-07 2.1e-01 8.8e-07 9.97e-01 1.017026503e+01 1.017026644e+01 3.1e-10 0.22 63 2.1e-07 2.1e-01 7.9e-07 1.00e+00 1.017026515e+01 1.017026642e+01 2.8e-10 0.22 64 1.9e-07 2.0e-01 7.1e-07 1.01e+00 1.017026526e+01 1.017026640e+01 2.5e-10 0.23 65 1.7e-07 2.0e-01 6.4e-07 9.96e-01 1.017026535e+01 1.017026638e+01 2.3e-10 0.23 66 3.4e-08 4.0e-02 1.3e-07 9.82e-01 1.017026605e+01 1.017026625e+01 4.7e-11 0.23 67 5.5e-09 5.9e-03 1.9e-08 1.10e+00 1.017026619e+01 1.017026622e+01 5.5e-12 0.23 68 3.8e-10 3.8e-04 1.2e-09 8.98e-01 1.017026622e+01 1.017026622e+01 4.2e-13 0.24 Interior-point optimizer terminated. Time: 0.24. Optimizer terminated. Time: 0.26 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0170266218e+01 Viol. con: 3e-10 var: 0e+00 Dual. obj: 1.0170266220e+01 Viol. con: 0e+00 var: 1e-04 * End solution on dual form. * Transforming to primal solution. Solving took 0.282 seconds. result packing took 37% of solve time solution checking took 17% of solve time Using solver 'mosek' Solving for 2480 variables. Warning: The variable with index '1860' has only negative coefficients akj. The problem is possibly ill-posed. Number of Hessian non-zeros: 1090 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Linux/64-X86 Cores : 20 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 2481 Cones : 0 Scalar variables : 5898 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1026 Eliminator terminated. Eliminator started. Total number of eliminations : 1041 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1041 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 : 20 Optimizer - solved problem : the primal Optimizer - Constraints : 286 Optimizer - Cones : 0 Optimizer - Scalar variables : 995 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 : 6557 after factor : 1.08e+04 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 2.6e+03 3.8e+03 7.7e+03 0.00e+00 -7.721659770e+03 1.023181539e-12 1.0e+00 0.05 1 7.9e+02 1.2e+03 2.4e+03 -2.26e-03 -3.459676542e+03 9.890412861e+00 3.4e-01 0.05 2 5.9e+02 8.8e+02 1.8e+03 1.40e+00 -2.229481992e+03 1.171399326e+01 2.5e-01 0.06 3 3.8e+02 5.6e+02 1.2e+03 1.45e+00 -1.236932528e+03 1.314735671e+01 1.6e-01 0.06 4 1.3e+02 2.0e+02 4.0e+02 1.56e+00 -3.250030035e+02 1.397273830e+01 6.0e-02 0.06 5 4.2e+01 6.3e+01 1.3e+02 1.47e+00 -7.775573201e+01 1.298048490e+01 2.0e-02 0.07 6 1.1e+01 2.0e+01 3.4e+01 1.15e+00 -1.121670886e+01 1.141514472e+01 6.0e-03 0.07 7 2.4e+00 1.5e+01 7.6e+00 1.02e+00 5.607836541e+00 1.067191889e+01 1.5e-03 0.07 8 2.2e+00 1.4e+01 7.1e+00 7.87e-01 5.805611268e+00 1.065685039e+01 1.4e-03 0.08 9 1.1e+00 9.6e+00 3.5e+00 7.42e-01 7.632566582e+00 1.052164444e+01 7.5e-04 0.08 10 1.0e+00 9.2e+00 3.3e+00 4.62e-01 7.565640878e+00 1.051356540e+01 7.2e-04 0.09 11 3.9e-01 6.8e+00 1.3e+00 5.15e-01 8.911366908e+00 1.036016093e+01 3.0e-04 0.09 12 2.8e-01 4.9e+00 9.1e-01 5.59e-01 9.186998351e+00 1.032243398e+01 2.2e-04 0.09 13 4.6e-02 4.2e+00 1.6e-01 6.42e-01 9.960818345e+00 1.020958597e+01 5.2e-05 0.10 14 1.4e-02 3.9e+00 5.2e-02 9.15e-01 1.010227262e+01 1.018331304e+01 1.8e-05 0.10 15 5.5e-03 3.6e+00 2.0e-02 9.80e-01 1.014379781e+01 1.017568096e+01 7.0e-06 0.10 16 1.2e-03 3.4e+00 4.4e-03 9.91e-01 1.016437022e+01 1.017127248e+01 1.6e-06 0.11 17 2.7e-04 3.4e+00 1.0e-03 9.97e-01 1.016879790e+01 1.017038000e+01 3.6e-07 0.11 18 6.2e-05 3.2e+00 2.3e-04 9.99e-01 1.016982386e+01 1.017018981e+01 8.5e-08 0.11 19 1.5e-05 3.0e+00 5.7e-05 9.99e-01 1.017005488e+01 1.017014539e+01 2.1e-08 0.12 20 1.4e-05 2.7e+00 5.2e-05 9.99e-01 1.017006190e+01 1.017014358e+01 1.9e-08 0.12 21 1.2e-05 2.5e+00 4.6e-05 9.99e-01 1.017006878e+01 1.017014231e+01 1.7e-08 0.12 22 1.1e-05 2.2e+00 4.2e-05 9.99e-01 1.017007497e+01 1.017014116e+01 1.5e-08 0.12 23 1.0e-05 2.0e+00 3.8e-05 1.00e+00 1.017008056e+01 1.017014012e+01 1.4e-08 0.13 24 9.0e-06 1.8e+00 3.4e-05 1.00e+00 1.017008558e+01 1.017013919e+01 1.3e-08 0.13 25 8.1e-06 1.7e+00 3.0e-05 1.00e+00 1.017009010e+01 1.017013835e+01 1.1e-08 0.13 26 7.3e-06 1.5e+00 2.7e-05 1.00e+00 1.017009417e+01 1.017013759e+01 1.0e-08 0.14 27 6.5e-06 1.4e+00 2.5e-05 1.00e+00 1.017009783e+01 1.017013691e+01 9.1e-09 0.14 28 5.9e-06 1.3e+00 2.2e-05 1.00e+00 1.017010113e+01 1.017013630e+01 8.2e-09 0.14 29 5.3e-06 1.2e+00 2.0e-05 1.00e+00 1.017010409e+01 1.017013575e+01 7.4e-09 0.14 30 4.8e-06 1.1e+00 1.8e-05 1.00e+00 1.017010676e+01 1.017013525e+01 6.6e-09 0.15 31 4.3e-06 9.7e-01 1.6e-05 1.00e+00 1.017010916e+01 1.017013481e+01 6.0e-09 0.15 32 3.9e-06 8.9e-01 1.5e-05 1.00e+00 1.017011133e+01 1.017013441e+01 5.4e-09 0.15 33 3.5e-06 8.2e-01 1.3e-05 1.00e+00 1.017011327e+01 1.017013404e+01 4.8e-09 0.16 34 3.1e-06 7.6e-01 1.2e-05 1.00e+00 1.017011503e+01 1.017013372e+01 4.4e-09 0.16 35 2.8e-06 7.0e-01 1.1e-05 1.00e+00 1.017011660e+01 1.017013343e+01 3.9e-09 0.16 36 2.5e-06 6.5e-01 9.5e-06 1.00e+00 1.017011802e+01 1.017013316e+01 3.5e-09 0.16 37 2.3e-06 6.0e-01 8.6e-06 1.00e+00 1.017011930e+01 1.017013293e+01 3.2e-09 0.17 38 2.1e-06 5.6e-01 7.7e-06 1.00e+00 1.017012045e+01 1.017013271e+01 2.9e-09 0.17 39 1.8e-06 5.2e-01 7.0e-06 9.99e-01 1.017012148e+01 1.017013252e+01 2.6e-09 0.17 40 1.7e-06 4.9e-01 6.3e-06 1.00e+00 1.017012241e+01 1.017013235e+01 2.3e-09 0.17 41 1.5e-06 4.6e-01 5.6e-06 9.99e-01 1.017012325e+01 1.017013219e+01 2.1e-09 0.18 42 1.3e-06 4.3e-01 5.1e-06 9.99e-01 1.017012400e+01 1.017013205e+01 1.9e-09 0.18 43 1.2e-06 4.0e-01 4.6e-06 1.00e+00 1.017012468e+01 1.017013192e+01 1.7e-09 0.18 44 1.1e-06 3.8e-01 4.1e-06 1.00e+00 1.017012529e+01 1.017013181e+01 1.5e-09 0.19 45 9.8e-07 3.6e-01 3.7e-06 1.00e+00 1.017012584e+01 1.017013171e+01 1.4e-09 0.19 46 8.8e-07 3.4e-01 3.3e-06 1.00e+00 1.017012633e+01 1.017013161e+01 1.2e-09 0.19 47 8.0e-07 3.3e-01 3.0e-06 1.00e+00 1.017012678e+01 1.017013153e+01 1.1e-09 0.19 48 7.2e-07 3.1e-01 2.7e-06 1.00e+00 1.017012718e+01 1.017013146e+01 1.0e-09 0.20 49 6.4e-07 3.0e-01 2.4e-06 1.00e+00 1.017012754e+01 1.017013139e+01 9.0e-10 0.20 50 5.8e-07 2.9e-01 2.2e-06 9.93e-01 1.017012786e+01 1.017013133e+01 8.1e-10 0.20 51 5.2e-07 2.8e-01 2.0e-06 9.97e-01 1.017012816e+01 1.017013127e+01 7.3e-10 0.20 52 4.7e-07 2.7e-01 1.8e-06 1.00e+00 1.017012842e+01 1.017013122e+01 6.6e-10 0.21 53 4.2e-07 2.6e-01 1.6e-06 9.98e-01 1.017012866e+01 1.017013118e+01 5.9e-10 0.21 54 3.8e-07 2.5e-01 1.4e-06 1.00e+00 1.017012887e+01 1.017013114e+01 5.3e-10 0.21 55 3.4e-07 2.4e-01 1.3e-06 9.97e-01 1.017012906e+01 1.017013111e+01 4.8e-10 0.21 56 3.1e-07 2.4e-01 1.2e-06 1.00e+00 1.017012923e+01 1.017013107e+01 4.3e-10 0.22 57 2.8e-07 2.3e-01 1.0e-06 1.01e+00 1.017012939e+01 1.017013104e+01 3.9e-10 0.22 58 2.5e-07 2.3e-01 9.4e-07 9.99e-01 1.017012953e+01 1.017013102e+01 3.5e-10 0.22 59 2.2e-07 2.2e-01 8.5e-07 9.96e-01 1.017012966e+01 1.017013099e+01 3.1e-10 0.22 60 2.0e-07 2.2e-01 7.6e-07 1.01e+00 1.017012978e+01 1.017013097e+01 2.8e-10 0.23 61 1.8e-07 2.2e-01 6.9e-07 1.00e+00 1.017012988e+01 1.017013095e+01 2.6e-10 0.23 62 1.6e-07 2.2e-01 6.2e-07 9.91e-01 1.017012997e+01 1.017013093e+01 2.3e-10 0.23 63 1.5e-07 2.1e-01 5.6e-07 1.00e+00 1.017013005e+01 1.017013092e+01 2.1e-10 0.23 64 1.3e-07 1.9e-01 5.0e-07 1.02e+00 1.017013013e+01 1.017013090e+01 1.9e-10 0.24 65 1.2e-07 1.9e-01 4.5e-07 9.94e-01 1.017013020e+01 1.017013089e+01 1.7e-10 0.24 66 1.1e-07 1.7e-01 4.0e-07 1.02e+00 1.017013026e+01 1.017013088e+01 1.5e-10 0.24 67 9.7e-08 1.5e-01 3.6e-07 1.03e+00 1.017013032e+01 1.017013087e+01 1.4e-10 0.24 68 8.7e-08 1.4e-01 3.3e-07 9.80e-01 1.017013037e+01 1.017013086e+01 1.3e-10 0.25 69 7.8e-08 1.2e-01 3.0e-07 9.73e-01 1.017013041e+01 1.017013085e+01 1.1e-10 0.25 70 7.1e-08 1.1e-01 2.7e-07 9.67e-01 1.017013044e+01 1.017013085e+01 1.0e-10 0.25 71 6.4e-08 1.0e-01 2.4e-07 9.74e-01 1.017013048e+01 1.017013084e+01 9.3e-11 0.25 72 5.7e-08 9.1e-02 2.2e-07 1.02e+00 1.017013051e+01 1.017013083e+01 8.4e-11 0.26 73 6.1e-09 9.3e-03 2.2e-08 9.75e-01 1.017013075e+01 1.017013079e+01 9.0e-12 0.26 74 2.7e-10 1.1e-04 2.7e-10 9.89e-01 1.017013078e+01 1.017013078e+01 4.7e-13 0.26 Interior-point optimizer terminated. Time: 0.26. Optimizer terminated. Time: 0.29 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.0170130782e+01 Viol. con: 3e-10 var: 0e+00 Dual. obj: 1.0170130783e+01 Viol. con: 0e+00 var: 3e-05 * End solution on dual form. * Transforming to primal solution. Solving took 0.307 seconds. result packing took 35% of solve time solution checking took 16% of solve time Solving took 5 GP solves and 4.14 seconds. Warning: Constraint [W_{total}_FleetMission_(0,) [N]... >= W_{dry}_FleetMission_(0,) + W_{f_{total}}_FleetMission_(0,) [N]...] is not tight because the left hand side evaluated to 366641.680195 newton but the right hand side evaluated to 366630.068414 newton (Allowable error: 0.0001%, Actual error: 0.0032%) Warning: Constraint [W_{total}_FleetMission_(1,) [N]... >= W_{dry}_FleetMission_(1,) + W_{f_{total}}_FleetMission_(1,) [N]...] is not tight because the left hand side evaluated to 377162.194209 newton but the right hand side evaluated to 377115.443502 newton (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [W_{total}_FleetMission_(2,) [N]... >= W_{dry}_FleetMission_(2,) + W_{f_{total}}_FleetMission_(2,) [N]...] is not tight because the left hand side evaluated to 388105.092605 newton but the right hand side evaluated to 387998.86218 newton (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [W_{total}_FleetMission_(3,) [N]... >= W_{dry}_FleetMission_(3,) + W_{f_{total}}_FleetMission_(3,) [N]...] is not tight because the left hand side evaluated to 399470.246705 newton but the right hand side evaluated to 399279.095417 newton (Allowable error: 0.0001%, Actual error: 0.048%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 361212.196395 newton but the right hand side evaluated to 361206.371769 newton (Allowable error: 0.0001%, Actual error: 0.0016%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 1) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 1) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 371522.143071 newton but the right hand side evaluated to 371498.546562 newton (Allowable error: 0.0001%, Actual error: 0.0064%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 2) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 2) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 382190.308663 newton but the right hand side evaluated to 382135.970301 newton (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 3) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 3) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 393255.645417 newton but the right hand side evaluated to 393156.480231 newton (Allowable error: 0.0001%, Actual error: 0.025%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 356181.888961 newton but the right hand side evaluated to 356176.101846 newton (Allowable error: 0.0001%, Actual error: 0.0016%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 1) [N]... >= W_{burn}_FleetMissi.on/CruiseSegment/CruiseP/AircraftP.1_(1, 1) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 361243.205961 newton but the right hand side evaluated to 361220.0518 newton (Allowable error: 0.0001%, Actual error: 0.0064%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 2) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 2) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 366354.227472 newton but the right hand side evaluated to 366302.335513 newton (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 3) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 3) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 371535.457326 newton but the right hand side evaluated to 371443.471321 newton (Allowable error: 0.0001%, Actual error: 0.025%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) [N]...] is not tight because the left hand side evaluated to 18366.9604209 newton but the right hand side evaluated to 18366.717608 newton (Allowable error: 0.0001%, Actual error: 0.0013%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 1) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 1) [N]...] is not tight because the left hand side evaluated to 18344.4542986 newton but the right hand side evaluated to 18344.2049569 newton (Allowable error: 0.0001%, Actual error: 0.0014%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 2) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 2) [N]...] is not tight because the left hand side evaluated to 18344.4542426 newton but the right hand side evaluated to 18344.2048708 newton (Allowable error: 0.0001%, Actual error: 0.0014%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 3) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 3) [N]...] is not tight because the left hand side evaluated to 18344.4542667 newton but the right hand side evaluated to 18344.2048935 newton (Allowable error: 0.0001%, Actual error: 0.0014%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) [N]...] is not tight because the left hand side evaluated to 18924.2853633 newton but the right hand side evaluated to 18924.2648757 newton (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 2) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 2) [N]...] is not tight because the left hand side evaluated to 8445.89963749 newton but the right hand side evaluated to 8445.84800367 newton (Allowable error: 0.0001%, Actual error: 0.00061%) Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 3) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 3) [N]...] is not tight because the left hand side evaluated to 8626.29336582 newton but the right hand side evaluated to 8626.24784647 newton (Allowable error: 0.0001%, Actual error: 0.00053%) Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528315 newton but the right hand side evaluated to 24184.16 newton. ---------------------------------------------------------------------- Ran 2 tests in 10.446s OK Generating XML reports... (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 'gassolar'... Cannot uninstall requirement gassolar, not installed Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gassolar Installing collected packages: gassolar Running setup.py develop for gassolar Successfully installed gassolar From https://github.com/convexengineering/gpkit-models * branch tailfoam -> FETCH_HEAD Previous HEAD position was 662ac9f... add readme with build status HEAD is now at 238e02f... explicitly add wing interior to v-h tails Cannot uninstall requirement gpkit-models, not installed Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit-models Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Requirement already satisfied: pandas in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: python-dateutil in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: numpy>=1.7.0 in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /tmp/pip-4Fc1Su-build Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: scipy in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit (from gpfit==0.1) Requirement already satisfied: pint in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) Running tests... ---------------------------------------------------------------------- ..../jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gassolar/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/gas/gas_simple/gassimple.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 564 variables. Solving took 0.276 seconds. Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 564 variables. Solving took 0.193 seconds. Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 564 variables. Solving took 0.198 seconds. Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek_cli' Solving for 564 variables. Solving took 0.265 seconds. Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 79 variables. Solving took 0.0489 seconds. Using solver 'mosek_cli' Solving for 79 variables. Solving took 0.231 seconds. Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(0,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(0,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.21497919994 but the right hand side evaluated to 0.214980884457 (Allowable error: 0.0001%, Actual error: 0.00078%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(1,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(1,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.20177138095 but the right hand side evaluated to 0.201784261577 (Allowable error: 0.0001%, Actual error: 0.0064%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(2,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(2,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.197670258036 but the right hand side evaluated to 0.197679911636 (Allowable error: 0.0001%, Actual error: 0.0049%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(3,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(3,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.20177138095 but the right hand side evaluated to 0.201764084159 (Allowable error: 0.0001%, Actual error: 0.0036%) Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(4,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(4,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.21497919994 but the right hand side evaluated to 0.214970135681 (Allowable error: 0.0001%, Actual error: 0.0042%) Using solver 'mosek' Solving for 1067 varia.. ---------------------------------------------------------------------- Ran 6 tests in 20.817s OK Generating XML reports... bles. Solving took 0.321 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 134065.0320 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.1/AircraftPerf.1/WingAero.1 could cause inaccurate result because it is below lower bound. Solution is 132709.8903 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 134071.9969 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 11 is a constraining latitude Beginning signomial solve. Solving took 4 GP solves and 1.98 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 136276.7307 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 136278.3666 but bound is 150000.0000 1 is a constraining latitude 11 is a constraining latitude Using solver 'mosek_cli' Solving for 1067 variables. Solving took 0.5 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 134064.9952 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.1/AircraftPerf.1/WingAero.1 could cause inaccurate result because it is below lower bound. Solution is 132709.7909 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 134071.6986 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 11 is a constraining latitude Beginning signomial solve. Solving took 4 GP solves and 2.79 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 136276.3380 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 136277.7007 but bound is 150000.0000 1 is a constraining latitude 11 is a constraining latitude Cloning into 'SPaircraft'... From https://github.com/convexengineering/gpkit-models * branch master -> FETCH_HEAD Warning: you are leaving 1 commit behind, not connected to any of your branches: 238e02f explicitly add wing interior to v-h tails If you want to keep it by creating a new branch, this may be a good time to do so with: git branch <new-branch-name> 238e02f HEAD is now at 662ac9f... add readme with build status Cannot uninstall requirement gpkit-models, not installed Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit-models Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to /tmp/pip-S5AzQA-build Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/turbofan Requirement already satisfied: numpy in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) Requirement already satisfied: scipy in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) Requirement already satisfied: pint in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) Running tests... ---------------------------------------------------------------------- adding test for 'SP_aircraft.py' Beginning signomial solve. Solving took 7 GP solves and 8.84 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 2427082.5723 force_pound * meter but the right hand side evaluated to 2397885.14052 force_pound * meter (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116759 meter but the right hand side evaluated to 1.96470867632 meter (Allowable error: 0.1%, Actual error: 11%) Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) [N]...] is not tight because the left hand side evaluated to 17472.5818091 newton but the right hand side evaluated to 17443.2490577 newton (Allowable error: 0.1%, Actual error: 0.17%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1242117.2725 joule / kilogram but the right hand side evaluated to 1.48135523531 megajoule / kilogram (Allowable error: 0.1%, Actual error: 9.5%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 642471.541334 joule / kilogram but the right hand side evaluated to 0.643956047306 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.1%) Warning: Constraint [W_{lg}_Mission/Aircraft/LandingGear*x_{CG_{lg}}_Mission/Aircraft/LandingGear [N*m]... >= W_{mg}_Mission/Aircraft/LandingGear*x_m_Mission/Aircraft/LandingGear + W_{ng}_Mission/Aircraft/Landi...] is not tight because the left hand side evaluated to 271789.717031 meter * newton but the right hand side evaluated to 263034.845086 meter * newton (Allowable error: 1.0%, Actual error: 3.3%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.575979985 meter but the right hand side evaluated to 16.612043215 meter (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.9551756346 but the right hand side evaluated to 4.85819314236 (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 10.006938764 but the right hand side evaluated to 4.85820336586 (Allowable error: 0.1%, Actual error: 51%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.21525013388 but the right hand side evaluated to 4.85820341322 (Allowable error: 0.1%, Actual error: 41%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/C.ruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.6219968125 meter but the right hand side evaluated to 18.3758628368 meter (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.6219968125 meter but the right hand side evaluated to 18.4513221959 meter (Allowable error: 0.1%, Actual error: 0.92%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.67771779164 but the right hand side evaluated to 4.79404645127 (Allowable error: 0.1%, Actual error: 2.4%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.7311423781 but the right hand side evaluated to 4.81373291041 (Allowable error: 0.1%, Actual error: 1.7%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.60828449078 but the right hand side evaluated to 4.79404645127 (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 7.57970897832 but the right hand side evaluated to 4.81373291041 (Allowable error: 0.1%, Actual error: 36%) Solves with these variables bounded: value near lower bound: [MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, CruiseAlt_Mission, ClimbDistance_Mission] value near upper bound: [TotalTime_Mission, A_{tri}_Mission/Aircraft/Wing/WingNoStruct] Checking for relaxed constants... WEIGHT DIFFERENCES Total Fuel Weight Percent Diff: [-6.97454608] Total Aircraft Weight Percent Diff: [-4.95043612] Engine Weight Percent Diff: -8.23499665259 Fuselage Weight Percent Diff: -10.9542147524 Payload Weight Percent Diff: [-0.04003559] VT Weight Percent Diff: -24.5190100377 HT Weight Percent Diff: -85.1525337465 Wing Weight Percent Diff: 0.426070945786 WING DIFFERENCES Wing Span Percent Diff: 0.921607293156 Wing Area Percent Diff: -6.86185072219 HORIZONTAL TAIL DIFFERENCES HT Area Percent Diff: -54.6185010751 VERTICAL TAIL DIFFERENCES VT Span Percent Diff: -16.3232130666 VT Area Percent Diff: -29.9970042226 CRUISE SEGMENT 1 DRAG DIFFERENCES Overall Cd Percent Diff: [-0.13083876] Nacelle Cd Percent Diff: [ 23.80939021] HT Cd Percent Diff: [-63.50967811] dimensionless Fuselage Cd Percent Diff: [ 45.32349081] VT Cd Percent Diff: [ 60.36861227] dimensionless Induced Drag Cd Percent Diff: [ 1.0638299] Wing Profile Cd Percent Diff: [-15.69392187] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [ 2.99108352] FUSELAGE DIFFERENCES Fan Propulsive Efficiency in Cruise Segment 1 --------------------- 0.790004744144 Beginning signomial solve. Solving took 7 GP solves and 10.3 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 2427083.77006 force_pound * meter but the right hand side evaluated to 2397878.31804 force_pound * meter (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.2151029155 meter but the right hand side evaluated to 1.96471264896 meter (Allowable error: 0.1%, Actual error: 11%) Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) [N]...] is not tight because the left hand side evaluated to 17472.4999511 newton but the right hand side evaluated to 17443.2145325 newton (Allowable error: 0.1%, Actual error: 0.17%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1242107.96665 joule / kilogram but the right hand side evaluated to 1.48150929195 megajoule / kilogram (Allowable error: 0.1%, Actual error: 9.5%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 642492.385771 joule / kilogram but the right hand side evaluated to 0.643976760313 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.1%) Warning: Constraint [W_{lg}_Mission/Aircraft/LandingGear*x_{CG_{lg}}_Mission/Aircraft/LandingGear [N*m]... >= W_{mg}_Mission/Aircraft/LandingGear*x_m_Mission/Aircraft/LandingGear + W_{ng}_Mission/Aircraft/Landi...] is not tight because the left hand side evaluated to 271790.00319 meter * newton but the right hand side evaluated to 263034.971207 meter * newton (Allowable error: 1.0%, Actual error: 3.3%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.575992106 meter but the right hand side evaluated to 16.6120444244 meter (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.9552310926 but the right hand side evaluated to 4.8581805724 (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 10.0071246035 but the right hand side evaluated to 4.85819028877 (Allowable error: 0.1%, Actual error: 51%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.21526190168 but the right hand side evaluated to 4.85819028877 (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 18.6220009448 meter but the right hand side evaluated to 18.3758811924 meter (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.. ---------------------------------------------------------------------- Ran 2 tests in 28.003s OK Generating XML reports... 1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.6220009448 meter but the right hand side evaluated to 18.4513216119 meter (Allowable error: 0.1%, Actual error: 0.92%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 4.67770643186 but the right hand side evaluated to 4.79403770011 (Allowable error: 0.1%, Actual error: 2.4%) Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 4.73112718468 but the right hand side evaluated to 4.81371916251 (Allowable error: 0.1%, Actual error: 1.7%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.60820068312 but the right hand side evaluated to 4.79403770011 (Allowable error: 0.1%, Actual error: 37%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.5796952927 but the right hand side evaluated to 4.81371916251 (Allowable error: 0.1%, Actual error: 36%) Solves with these variables bounded: value near lower bound: [MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, CruiseAlt_Mission, ClimbDistance_Mission] value near upper bound: [TotalTime_Mission, A_{tri}_Mission/Aircraft/Wing/WingNoStruct] Checking for relaxed constants... WEIGHT DIFFERENCES Total Fuel Weight Percent Diff: [-6.97422995] Total Aircraft Weight Percent Diff: [-4.95044675] Engine Weight Percent Diff: -8.23468392487 Fuselage Weight Percent Diff: -10.954618425 Payload Weight Percent Diff: [-0.04052335] VT Weight Percent Diff: -24.5186291271 HT Weight Percent Diff: -85.1525984735 Wing Weight Percent Diff: 0.425462741526 WING DIFFERENCES Wing Span Percent Diff: 0.921619801497 Wing Area Percent Diff: -6.86162729346 HORIZONTAL TAIL DIFFERENCES HT Area Percent Diff: -54.6182474474 VERTICAL TAIL DIFFERENCES VT Span Percent Diff: -16.3230602377 VT Area Percent Diff: -29.9967358734 CRUISE SEGMENT 1 DRAG DIFFERENCES Overall Cd Percent Diff: [-0.12878397] Nacelle Cd Percent Diff: [ 23.80939215] HT Cd Percent Diff: [-63.50956764] dimensionless Fuselage Cd Percent Diff: [ 45.32347143] VT Cd Percent Diff: [ 60.36836498] dimensionless Induced Drag Cd Percent Diff: [ 1.06883829] Wing Profile Cd Percent Diff: [-15.69240054] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [ 2.99029634] FUSELAGE DIFFERENCES Fan Propulsive Efficiency in Cruise Segment 1 --------------------- 0.790005398454 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gpkit-models.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'master'] attempt 1 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/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 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'turbofan'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'master'] attempt 1 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gassolar'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'tailfoam'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'tailfoam'] attempt 1 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/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/SPaircraft.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['git', 'fetch', '--depth', '1', 'origin', 'master'] attempt 1 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models'] attempt 1 calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git'] attempt 1 [Execution node] check if [reynolds] is in [[windows10x64, windows7x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] [xUnit] [INFO] - Starting to record. [xUnit] [INFO] - Processing JUnit [xUnit] [INFO] - [JUnit] - 5 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek' for the testing framework 'JUnit'. [xUnit] [INFO] - Check 'Failed Tests' threshold. [xUnit] [INFO] - Check 'Skipped Tests' threshold. [xUnit] [INFO] - Setting the build status to SUCCESS [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: SUCCESS