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Started by upstream project "gplibrary_PR_Models" build number 60 originally caused by: GitHub pull request #143 of commit 1eadb2b91c8354dd9493d46bb7d1a8f0475444a5, no merge conflicts. Building remotely on reynolds in workspace /jenkins/workspace/gplibrary_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/gplibrary_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 8b92f30b9df5332458a14a1e9ae689f398bdb1a3 (refs/remotes/origin/pr/143/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 8b92f30b9df5332458a14a1e9ae689f398bdb1a3 # 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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Seen branch in repository origin/troposphere Seen branch in repository origin/vectorizeplanform Seen branch in repository origin/wide_body Seen branch in repository origin/wvl Seen 173 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 8b92f30b9df5332458a14a1e9ae689f398bdb1a3 (origin/pr/143/merge, origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f 8b92f30b9df5332458a14a1e9ae689f398bdb1a3 # timeout=3 Commit message: "Merge 1eadb2b91c8354dd9493d46bb7d1a8f0475444a5 into 761babf99cf90418f3bf608eff9933bfffed0a68" 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="remove duplicate vertical tail constraints" href="https://github.com/convexengineering/gplibrary/pull/143">PR 143</a>: remove duplicate vertical tail constraints [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/jenkins1411118990074662416.sh + [[ reynolds == *macys* ]] + virtualenv --system-site-packages /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit New python executable in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/python2 Also creating executable in /jenkins/workspace/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip + PIP=/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip + python /jenkins/workspace/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib.linux-x86_64-2.7/mosek/__init__.py -> /jenkins/workspace/gplibrary_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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek creating /jenkins/workspace/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion byte-compiling /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/__init__.py to __init__.pyc byte-compiling /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/array.py to array.pyc byte-compiling /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/__init__.py to __init__.pyc byte-compiling /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/Utils.py to Utils.pyc byte-compiling /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/SolverInfo.py to SolverInfo.pyc running install_data copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../bin/libmosek64.so.7.1 -> /jenkins/workspace/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek running install_egg_info Writing /jenkins/workspace/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit Successfully installed numpy-1.13.3 + python /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade scipy Collecting scipy Using cached scipy-1.0.0-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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit Successfully installed scipy-1.0.0 + python /jenkins/workspace/gplibrary_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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade pandas Collecting pandas Using cached pandas-0.21.0-cp27-cp27mu-manylinux1_x86_64.whl Collecting pytz>=2011k (from pandas) Using cached pytz-2017.3-py2.py3-none-any.whl Requirement already up-to-date: numpy>=1.9.0 in ./venv2_gpkit/lib/python2.7/site-packages (from pandas) Collecting python-dateutil (from pandas) Using cached python_dateutil-2.6.1-py2.py3-none-any.whl 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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit Found existing installation: six 1.10.0 Not uninstalling six at /home/jenkins/.local/lib/python2.7/site-packages, outside environment /jenkins/workspace/gplibrary_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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit Successfully installed pandas-0.21.0 python-dateutil-2.6.1 pytz-2017.3 six-1.11.0 + export GPKITBUILD=/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/build_gpkit + GPKITBUILD=/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/build_gpkit ++ which coverage + COVERAGE=/home/jenkins/.local/bin//coverage + python -c 'import scipy; print scipy.__version__' 1.0.0 + 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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit Obtaining file:///jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit Requirement already satisfied: numpy>=1.12.1 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.6.0.0) Requirement already satisfied: pint>=0.7 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.6.0.0) Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.6.0.0) Installing collected packages: gpkit Running setup.py develop for gpkit Successfully installed gpkit + python /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek Obtaining file:///jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek Requirement already satisfied: numpy>=1.12 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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/env/settings installed_solvers : mosek, mosek_cli mosek_bin_dir : /home/jenkins/mosek/7/tools/platform/linux64x86/bin + ls /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/build_gpkit expopt.so + python -c 'from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)' Obtaining file:///jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Cloning into 'shopping'... Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 0.607s OK Generating XML reports... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.161 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.0232 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.238 seconds. Cloning into 'gassolar'... Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_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-sGjQz2-build Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_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 Processing /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gassolar Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit (from gassolar==0.0.0.0) Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpfit in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) Installing collected packages: gassolar Running setup.py install for gassolar: started Running setup.py install for gassolar: finished with status 'done' Successfully installed gassolar-0.0.0.0 Running tests... ---------------------------------------------------------------------- ../jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/local/lib/python2.7/site-packages/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/solar/solar.py' Using solver 'mosek' Solving for 574 variables. Solving took 0.237 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 0.2125 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 Beginning signomial solve. Solving took 4 GP solves and 1.17 seconds. Warning: Variable P_{ref}_Mission.1/Aircraft.1/Engine.1**-1*P_{sl-max}_Mission.1/Aircraft.1/Engine.1 could cause inaccurate result because it is below lower bound. Solution is 0.2140 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 574 variables. Solving took 0.221 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 0.2125 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 Beginning signomial solve. Solving took 4 GP solves and 1.15 seconds. Warning: Variable P_{ref}_Mission.1/Aircraft.1/Engine.1**-1*P_{sl-max}_Mission.1/Aircraft.1/Engine.1 could cause inaccurate result because it is below lower bound. Solution is 0.2140 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 1187 variables. Solving took 0.317 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 107909.6240 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 107910.9775 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 3 is a constraining latitude 4 is a constraining latitude 5 is a constraining latitude 6 is a constraining latitude 7 is a constraining latitude 8 is a constraining latitude 9 is a constraining latitude 10 is a constraining latitude 11 is a constraining latitude Beginning signomial solve. Solving took 4 GP solves and 2.33 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 109221.9349 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 109223.2155 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 3 is a constraining latitude 4 is a constraining latitude 5 is a constraining latitude 6 is a constraining latitude 7 is a constraining latitude 8 is a constraining latitude 9 is a constraining latitude 10 is a constraining latitude 11 is a constraining latitude Using solver 'mosek_cli' Solving for 1187 variables. Solving took 0.501 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 107909.6951 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 107910.7742 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 3 is a constraining la. ---------------------------------------------------------------------- Ran 4 tests in 22.278s OK Generating XML reports... titude 4 is a constraining latitude 5 is a constraining latitude 6 is a constraining latitude 7 is a constraining latitude 8 is a constraining latitude 9 is a constraining latitude 10 is a constraining latitude 11 is a constraining latitude Beginning signomial solve. Solving took 4 GP solves and 2.75 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 109222.2417 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 109223.3339 but bound is 150000.0000 1 is a constraining latitude 2 is a constraining latitude 3 is a constraining latitude 4 is a constraining latitude 5 is a constraining latitude 6 is a constraining latitude 7 is a constraining latitude 8 is a constraining latitude 9 is a constraining latitude 10 is a constraining latitude 11 is a constraining latitude Cloning into 'jho'... Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_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-P9wzRJ-build Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->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 -4.27261524771e-13. Allowing negative dual variable(s) as small as -1.01601257789e-12. Allowing negative dual variable(s) as small as -3.0217670163e-11. Allowing negative dual variable(s) as small as -2.87745838441e-11. Solving took 4 GP solves and 3.3 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -4.26466154058e-13. Allowing negative dual variable(s) as small as -1.01954143912e-12. Allowing negative dual variable(s) as small as -3.02160798552e-11. Allowing negative dual variable(s) as small as -2.8772405682e-11. Solving took 4 GP solves and 3.19 seconds. Allowing negative dual variable(s) as small as -6.96141169883e-13. Allowing negative dual variable(s) as small as -3.80193489538e-13. Allowing negative dual variable(s) as small as -2.8748379545e-14. Allowing negative dual variable(s) as small as -2.87141187563e-14. Allowing negative dual variable(s) as small as -1.16885559391e-13. Allowing negative dual variable(s) as small as -5.83278786978e-10. Allowing negative dual variable(s) as small as -2.86085445698e-14. Allowing negative dual variable(s) as small as -3.07499251756e-14. MTOW [lbs] = 132.53 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 = 20.352 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.301 Allowing negative dual variable(s) as small as -5.01274754209e-10. Allowing negative dual variable(s) as small as -4.84333201285e-10. Allowing negative dual variable(s) as small as -5.96148919888e-11. Allowing negative dual variable(s) as small as -5.95298931948e-11. optimum loiter speed for min power, start of loiter [m/s] = 23.618 optimum loiter speed for min power, end of loiter [m/s] = 16.685 optimum cruise speed, inbound [m/s] = 31.024 optimum cruise speed, outbound [m/s] = 23.411 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.44118429016e-12. Allowing negative dual variable(s) as small as -2.90973270186e-12. Allowing negative dual variable(s) as small as -3.02526682047e-12. Allowing negative dual variable(s) as small as -3.02603313808e-12. Solving took 4 GP solves and 2.71 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 1.97 seconds. Max payload weight [lbf] = 9.228 Max take off weight [lbf] = 140.364 Allowing negative dual variable(s) as small as -6.96241783844e-13. Allowing negative dual variable(s) as small as -3.80071625214e-13. Allowing negative dual variable(s) as small as -2.85304549083e-14. Allowing negative dual variable(s) as small as -2.86789906059e-14. Allowing negative dual variable(s) as small as -1.15304575783e-13. Allowing negative dual variable(s) as small as -5.83278931664e-10. Allowing negative dual variable(s) as small as -3.24327966827e-14. Allowing negative dual variable(s) as small as -2.85062500948e-14. MTOW [lbs] = 132.53 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 = 20.352 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.301 Allowing negative dual variable(s) as small as -5.01274953756e-10. Allowing negative dual variable(s) as small as -4.84333523266e-10. Allowing negative dual variable(s) as small as -5.96166518387e-11. Allowing negative dual variable(s) as small as -5.9529602466e-11. optimum loiter speed for min power, start of loiter [m/s] = 23.618 optimum loiter speed for min power, end of loiter [m/s] = 16.685 optimum cruise speed, inbound [m/s] = 31.024 optimum cruise speed, outbound [m/s] = 23.411 Beginning signomial solve. Allow. ---------------------------------------------------------------------- Ran 4 tests in 42.877s OK Generating XML reports... ing negative dual variable(s) as small as -5.44103969622e-12. Allowing negative dual variable(s) as small as -2.90983117429e-12. Allowing negative dual variable(s) as small as -3.02528192473e-12. Allowing negative dual variable(s) as small as -3.02597200955e-12. Solving took 4 GP solves and 2.47 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 1.7 seconds. Max payload weight [lbf] = 9.228 Max take off weight [lbf] = 140.364 Cloning into 'turbofan'... Processing /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/turbofan Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_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/gplibrary_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/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) Installing collected packages: turbofan Running setup.py install for turbofan: started Running setup.py install for turbofan: finished with status 'done' Successfully installed turbofan-0.0.0.0 Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 1.514s OK Generating XML reports... adding test for 'turbofan/engine_validation.py' Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528315 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%) Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485055 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Cloning into 'SPaircraft'... Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to /tmp/pip-RhY1eu-build Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_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/gplibrary_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/gplibrary_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' Solving over 9 passes. 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 2519607.63977 force_pound * meter but the right hand side evaluated to 2468463.68448 force_pound * meter (Allowable error: 0.1%, Actual error: 2.1%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4916466 force_pound but the right hand side evaluated to 32399.9999989 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116797 meter but the right hand side evaluated to 1.96396175659 meter (Allowable error: 0.1%, Actual error: 11%) Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) [N]...] is not tight because the left hand side evaluated to 48608.9374957 newton but the right hand side evaluated to 48529.7554989 newton (Allowable error: 0.1%, Actual error: 0.16%) Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) [N]...] is not tight because the left hand side evaluated to 49704.3712834 newton but the right hand side evaluated to 49411.0881074 newton (Allowable error: 0.1%, Actual error: 0.59%) 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 18949.0872962 newton but the right hand side evaluated to 18923.0889414 newton (Allowable error: 0.1%, Actual error: 0.14%) Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(4, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(4, 0) [N]...] is not tight because the left hand side evaluated to 16591.9858032 newton but the right hand side evaluated to 16565.785707 newton (Allowable error: 0.1%, Actual error: 0.16%) 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 1002807.29804 joule / kilogram but the right hand side evaluated to 1.15238853589 megajoule / kilogram (Allowable error: 0.1%, Actual error: 7.1%) 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 895037.2394 joule / kilogram but the right hand side evaluated to 0.897466394332 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.13%) 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 1072947.06521 joule / kilogram but the right hand side evaluated to 1.19569631361 megajoule / kilogram (Allowable error: 0.1%, Actual error: 5.6%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 596870.58287 joule / kilogram but the right hand side evaluated to 0.615557129968 megajoule / kilogram (Allowable error: 0.1%, Actual error: 1.3%) 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 786921.773123 joule / kilogram but the right hand side evaluated to 0.790360540084 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.22%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.3465533937 meter but the right hand side evaluated to 16.3967754922 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 11.085406527 but the right hand side evaluated to 4.68078583398 (Allowable error: 0.1%, Actual error: 58%) 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 9.79174342747 but the right hand side evaluated to 4.68078582974 (Allowable error: 0.1%, Actual error: 52%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.22912408471 but the right hand side evaluated to 4.68078583522 (Allowable error: 0.1%, Actual error: 43%) 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 18.4249253673 meter but the right hand side evaluated to 18.165984066 meter (Allowable error: 0.1%, Actual error: 1.4%) 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 18.4249253673 meter but the right hand side evaluated to 18.2854579385 meter (Allowable error: 0.1%, Actual error: 0.76%) 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 4.49878853415 but the right hand side evaluated to 4.61598272092 (Allowable error: 0.1%, Actual error: 2.5%) 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 4.58150053143 but the right hand side evaluated to 4.64634107249 (Allowable error: 0.1%, Actual error: 1.4%) 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 7.27503380385 but the right hand side evaluated to 4.61598272092 (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 7.45366719624 but the right hand side evaluated to 4.64634107249 (Allowable error: 0.1%, Actual error: 38%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission 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 2504977.33997 force_pound * meter but the right hand side evaluated to 2454470.99425 force_pound * meter (Allowable error: 0.1%, Actual error: 2.1%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4706114 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116793 meter but the right hand side evaluated to 1.96383017979 meter (Allowable error: 0.1%, Actual error: 11%) 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 982256.65429 joule / kilogram but the right hand side evaluated to 1.20547002733 megajoule / kilogram (Allowable error: 0.1%, Actual error: 10%) 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 1151137.27321 joule / kilogram but the right hand side evaluated to 1.88379362412 megajoule / kilogram (Allowable error: 0.1%, Actual error: 25%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4111624703 meter but the right hand side evaluated to 16.4524824083 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 11.0893102023 but the right hand side evaluated to 4.7313210685 (Allowable error: 0.1%, Actual error: 57%) 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 9.74913367839 but the right hand side evaluated to 4.73132106102 (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 8.19783398037 but the right hand side evaluated to 4.73132107116 (Allowable error: 0.1%, Actual error: 42%) 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 18.4749976337 meter but the right hand side evaluated to 18.2223430008 meter (Allowable error: 0.1%, Actual error: 1.4%) 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 18.4749976337 meter but the right hand side evaluated to 18.3384483908 meter (Allowable error: 0.1%, Actual error: 0.74%) 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 4.55043970698 but the right hand side evaluated to 4.66698073968 (Allowable error: 0.1%, Actual error: 2.5%) 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 4.63158705893 but the right hand side evaluated to 4.69671685094 (Allowable error: 0.1%, Actual error: 1.4%) 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 7.43022200257 but the right hand side evaluated to 4.66698073968 (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 7.49547617443 but the right hand side evaluated to 4.69671685094 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission 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 2481455.71328 force_pound * meter but the right hand side evaluated to 2426089.61543 force_pound * meter (Allowable error: 0.1%, Actual error: 2.3%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4884204 force_pound but the right hand side evaluated to 32399.9999991 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.215101168 meter but the right hand side evaluated to 1.83120103511 meter (Allowable error: 0.1%, Actual error: 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 1203383.93514 joule / kilogram but the right hand side evaluated to 1.66382890644 megajoule / kilogram (Allowable error: 0.1%, Actual error: 17%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4693762033 meter but the right hand side evaluated to 16.6432009244 meter (Allowable error: 0.1%, Actual error: 11%) 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 11.0473080642 but the right hand side evaluated to 4.80181031995 (Allowable error: 0.1%, Actual error: 57%) 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 9.67070769876 but the right hand side evaluated to 4.80181031543 (Allowable error: 0.1%, Actual error: 50%) 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 8.22137554703 but the right hand side evaluated to 4.80181032138 (Allowable error: 0.1%, Actual error: 42%) 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 18.6280048698 meter but the right hand side evaluated to 18.3449847685 meter (Allowable error: 0.1%, Actual error: 1.5%) 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 18.6280048698 meter but the right hand side evaluated to 18.4743839538 meter (Allowable error: 0.1%, Actual error: 0.82%) 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 4.59899293052 but the right hand side evaluated to 4.72922349911 (Allowable error: 0.1%, Actual error: 2.8%) 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 4.6892147279 but the right hand side evaluated to 4.76258180798 (Allowable error: 0.1%, Actual error: 1.5%) 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 7.45561879594 but the right hand side evaluated to 4.72922349911 (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 7.54886829354 but the right hand side evaluated to 4.76258180798 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission 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 2455568.07949 force_pound * meter but the right hand side evaluated to 2407712.16686 force_pound * meter (Allowable error: 0.1%, Actual error: 2%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4882046 force_pound but the right hand side evaluated to 32399.9999989 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116799 meter but the right hand side evaluated to 1.99552117087 meter (Allowable error: 0.1%, Actual error: 9.9%) 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 1227633.92696 joule / kilogram but the right hand side evaluated to 1.7235977089 megajoule / kilogram (Allowable error: 0.1%, Actual error: 18%) 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 677538.823531 joule / kilogram but the right hand side evaluated to 0.679181841305 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.11%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4156360641 meter but the right hand side evaluated to 16.4239734847 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 10.9749700318 but the right hand side evaluated to 4.76255478822 (Allowable error: 0.1%, Actual error: 57%) 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 9.75289660439 but the right hand side evaluated to 4.76255478121 (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 8.15871856506 but the right hand side evaluated to 4.76255479024 (Allowable error: 0.1%, Actual error: 42%) 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 18.4488732667 meter but the right hand side evaluated to 18.2046638098 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 18.4488732667 meter but the right hand side evaluated to 18.317619014 meter (Allowable error: 0.1%, Actual error: 0.71%) 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 4.58582625947 but the right hand side evaluated to 4.69978355945 (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 4.6655917748 but the right hand side evaluated to 4.72894449408 (Allowable error: 0.1%, Actual error: 1.3%) 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 7.50481924211 but the right hand side evaluated to 4.69978355945 (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 7.52765876444 but the right hand side evaluated to 4.72894449408 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission 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 2436785.51261 force_pound * meter but the right hand side evaluated to 2390898.41362 force_pound * meter (Allowable error: 0.1%, Actual error: 1.9%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4625387 force_pound but the right hand side evaluated to 32399.9999997 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116812 meter but the right hand side evaluated to 2.03201108866 meter (Allowable error: 0.1%, Actual error: 8.3%) 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 1233975.11259 joule / kilogram but the right hand side evaluated to 1.62325979319 megajoule / kilogram (Allowable error: 0.1%, Actual error: 15%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4095772583 meter but the right hand side evaluated to 16.3813510144 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 10.9310500325 but the right hand side evaluated to 4.78771844644 (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 9.87336390298 but the right hand side evaluated to 4.78771844267 (Allowable error: 0.1%, Actual error: 52%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.15464743328 but the right hand side evaluated to 4.78771844737 (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 18.4102710931 meter but the right hand side evaluated to 18.1746813249 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 18.4102710931 meter but the right hand side evaluated to 18.2839322313 meter (Allowable error: 0.1%, Actual error: 0.69%) 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 4.61574415085 but the right hand side evaluated to 4.726722532 (Allowable error: 0.1%, Actual error: 2.3%) 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 4.69362626306 but the right hand side evaluated to 4.75513561455 (Allowable error: 0.1%, Actual error: 1.3%) 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 7.5364849428 but the right hand side evaluated to 4.726722532 (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 7.55140036918 but the right hand side evaluated to 4.75513561455 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission 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 2418324.14825 force_pound * meter but the right hand side evaluated to 2374883.17837 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4708201 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116786 meter but the right hand side evaluated to 2.08236095998 meter (Allowable error: 0.1%, Actual error: 6%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1244507.79683 joule / kilogram but the right hand side evaluated to 1.55928593095 megajoule / kilogram (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 664751.337828 joule / kilogram but the right hand side evaluated to 0.667402933478 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.18%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4000459664 meter but the right hand side evaluated to 16.3223711737 meter (Allowable error: 0.1%, Actual error: 13%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.9040394017 but the right hand side evaluated to 4.78950192838 (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 10.0259853353 but the right hand side evaluated to 4.78950191778 (Allowable error: 0.1%, Actual error: 52%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.14555451912 but the right hand side evaluated to 4.78950193107 (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 18.3617936435 meter but the right hand side evaluated to 18.1374255554 meter (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3617936435 meter but the right hand side evaluated to 18.2416846273 meter (Allowable error: 0.1%, Actual error: 0.65%) 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 4.6250780058 but the right hand side evaluated to 4.73131691106 (Allowable error: 0.1%, Actual error: 2.2%) 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 4.69987263458 but the right hand side evaluated to 4.75851386404 (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.5653459624 but the right hand side evaluated to 4.73131691106 (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 7.58381895813 but the right hand side evaluated to 4.75851386404 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission 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 2405734.86608 force_pound * meter but the right hand side evaluated to 2358168.29482 force_pound * meter (Allowable error: 0.1%, Actual error: 2%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.432492 force_pound but the right hand side evaluated to 32399.9999993 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116811 meter but the right hand side evaluated to 1.97490993326 meter (Allowable error: 0.1%, Actual error: 11%) 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 1245747.37398 joule / kilogram but the right hand side evaluated to 1.35773076215 megajoule / kilogram (Allowable error: 0.1%, Actual error: 4.7%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4441337265 meter but the right hand side evaluated to 16.4749778314 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 10.9331078172 but the right hand side evaluated to 4.8317175463 (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 10.1921395411 but the right hand side evaluated to 4.83171753039 (Allowable error: 0.1%, Actual error: 53%) 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 8.19565637891 but the right hand side evaluated to 4.83171754949 (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 18.486130247 meter but the right hand side evaluated to 18.2368501005 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 18.486130247 meter but the right hand side evaluated to 18.3518655582 meter (Allowable error: 0.1%, Actual error: 0.73%) 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 4.64971755979 but the right hand side evaluated to 4.7669781447 (Allowable error: 0.1%, Actual error: 2.5%) 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 4.73177028506 but the right hand side evaluated to 4.79704233729 (Allowable error: 0.1%, Actual error: 1.4%) 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 7.54212856497 but the right hand side evaluated to 4.7669781447 (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 7.59702315964 but the right hand side evaluated to 4.79704233729 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission 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 2391779.32727 force_pound * meter but the right hand side evaluated to 2346059.34249 force_pound * meter (Allowable error: 0.1%, Actual error: 1.9%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4266881 force_pound but the right hand side evaluated to 32399.9999991 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116808 meter but the right hand side evaluated to 2.01208211291 meter (Allowable error: 0.1%, Actual error: 9.2%) 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 1263254.6252 joule / kilogram but the right hand side evaluated to 1.3293379349 megajoule / kilogram (Allowable error: 0.1%, Actual error: 2.8%) 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 643003.181314 joule / kilogram but the right hand side evaluated to 0.644587798212 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.11%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.439188522 meter but the right hand side evaluated to 16.4333015262 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 10.9270580046 but the right hand side evaluated to 4.82709677192 (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 10.3328493334 but the right hand side evaluated to 4.82709675381 (Allowable error: 0.1%, Actual error: 53%) 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 8.18819651703 but the right hand side evaluated to 4.82709677637 (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 18.4531697713 meter but the right hand side evaluated to 18.212378832 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 18.4531697713 meter but the right hand side evaluated to 18.3237329359 meter (Allowable error: 0.1%, Actual error: 0.7%) 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 4.65099003402 but the right hand side evaluated to 4.76456167997 (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 4.73069529675 but the right hand side evaluated to 4.79369315705 (Allowable error: 0.1%, Actual error: 1.3%) 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 7.55428836791 but the right hand side evaluated to 4.76456167997 (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 7.61783175909 but the right hand side evaluated to 4.79369315705 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission 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 2376282.77291 force_pound * meter but the right hand side evaluated to 2334600.02524 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.5314338 force_pound but the right hand side evaluated to 32399.9999968 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116778 meter but the right hand side evaluated to 2.09817282873 meter (Allowable error: 0.1%, Actual error: 5.3%) 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 1283641.55174 joule / kilogram but the right hand side evaluated to 1.28936253066 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.24%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4146021443 meter but the right hand side evaluated to 16.318341673 meter (Allowable error: 0.1%, Actual error: 13%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.9374634855 but the right hand side evaluated to 4.824379032 (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 10.5713441569 but the right hand side evaluated to 4.82437901227 (Allowable error: 0.1%, Actual error: 54%) 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 8.19385094701 but the right hand side evaluated to 4.82437903724 (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 18.3565590358 meter but the right hand side evaluated to 18.1377559036 meter (Allowable . ---------------------------------------------------------------------- Ran 1 test in 628.795s OK Generating XML reports... error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3565590358 meter but the right hand side evaluated to 18.2401773354 meter (Allowable error: 0.1%, Actual error: 0.63%) 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 4.6621579593 but the right hand side evaluated to 4.76702030175 (Allowable error: 0.1%, Actual error: 2.2%) 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 4.73627141541 but the right hand side evaluated to 4.7939390147 (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.62007212075 but the right hand side evaluated to 4.76702030175 (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 7.68939359018 but the right hand side evaluated to 4.7939390147 (Allowable error: 0.1%, Actual error: 38%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Sweeping took 626 seconds. Cloning into 'solar'... Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to /tmp/pip-A1JY2X-build Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) Collecting git+https://github.com/convexengineering/gassolar.git Cloning https://github.com/convexengineering/gassolar.git to /tmp/pip-AZJhkD-build Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit (from gassolar==0.0.0.0) Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpfit in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) Processing /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/solar Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit (from solar==0.0.0.0) Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) Requirement already satisfied: gpfit in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) Requirement already satisfied: gpkitmodels in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek (from solar==0.0.0.0) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->solar==0.0.0.0) Installing collected packages: solar Running setup.py install for solar: started Running setup.py install for solar: finished with status 'done' Successfully installed solar-0.0.0.0 Running tests... ---------------------------------------------------------------------- /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun) ...... ---------------------------------------------------------------------- Ran 6 tests in 129.184s OK Generating XML reports... adding test for 'solar/solar.py' adding test for 'solar/sens_chart.py' adding test for 'solar/season.py' Using solver 'mosek' Solving for 5643 variables. Solving took 6.08 seconds. Using solver 'mosek' Solving for 5643 variables. Solving took 1.53 seconds. Using solver 'mosek' Solving for 5643 variables. Solving took 1.38 seconds. Using solver 'mosek' Solving for 2883 variables. Solving took 0.503 seconds. Using solver 'mosek' Solving for 5643 variables. Solving took 1.31 seconds. Using solver 'mosek' Solving for 5643 variables. Solving took 1.28 seconds. Using solver 'mosek' Solving for 5643 variables. Solving took 1.13 seconds. Using solver 'mosek' Solving for 2883 variables. Solving took 0.458 seconds. Using solver 'mosek' Solving for 261 variables. Solving took 0.168 seconds. Using solver 'mosek' Solving for 261 variables. Solving took 0.175 seconds. Using solver 'mosek' Solving for 2883 variables. Solving took 0.502 seconds. Beginning signomial solve. Solving took 4 GP solves and 3.57 seconds. Using solver 'mosek_cli' Solving for 2883 variables. Solving took 0.715 seconds. Beginning signomial solve. Solving took 4 GP solves and 4.88 seconds. Cloning into 'gplibrary'... Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_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 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolCollecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /tmp/pip-Vp_NRu-build Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) Processing /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gplibrary Requirement already satisfied (use --upgrade to upgrade): gpkitmodels==0.0.0.0 from file:///jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gplibrary in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek Requirement already satisfied: numpy>=1.12 in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) Requirement already satisfied: pint in /jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 3.130s OK Generating XML reports... adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py' adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py' Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3642 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9486 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2272209.7006 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2195218.1937 but bound is 1000000.0000 Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2272202.0833 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2195213.7936 but bound is 1000000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 2147759.9054 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 2232694.7572 but bound is 700000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 2232695.1475 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 2232695.1475 but bound is 700000.0000 ds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.'] 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] - 7 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/jenkins/workspace/gplibrary_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