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Started by upstream project "gplibrary_PR_Models" build number 63 originally caused by: GitHub pull request #146 of commit 6a04d7a8531e7ba8ef06aa8f9881443b92d069c7, no merge conflicts. Building remotely on macys in workspace /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > git init /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 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origin/rockets Seen branch in repository origin/sigeq_paper Seen branch in repository origin/simple_HT_sizing Seen branch in repository origin/simple_flight_profile Seen branch in repository origin/standard_atmosphere Seen branch in repository origin/sutherland Seen branch in repository origin/troposphere Seen branch in repository origin/vectorizeplanform Seen branch in repository origin/wide_body Seen branch in repository origin/wvl Seen 179 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 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 (origin/pr/146/merge, origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f 2a7497c2e0e8ce8c85c047cea71ffd7cbee4e871 # timeout=3 Commit message: "Merge 6ef200c93b75c6359f18295b5a541fc98586263d into 62026ae2ee1965aa7005a73cc1f60d704fd1c8b0" 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="allow for different spar in tailboom bending and flex models" href="https://github.com/convexengineering/gplibrary/pull/146">PR 146</a>: allow for different spar in tailboom bending and flex models [Execution node] check if [macys] is in [[macys, macys_Sierra, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] enabling perform for step [Execute shell] [mosek] $ /bin/bash -xe /var/folders/wp/20zl4b2n0qxcrp90f31275f80000gp/T/jenkins4193281950707053258.sh + [[ macys == *macys* ]] + export PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ + PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ + virtualenv --system-site-packages /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit New python executable in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/python Installing setuptools, pip, wheel...done. + . /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit ++ export VIRTUAL_ENV ++ _OLD_VIRTUAL_PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export PATH ++ '[' -z '' ']' ++ '[' -z '' ']' ++ _OLD_VIRTUAL_PS1= ++ '[' x '!=' x ']' +++ basename /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit ++ PS1='(venv2_gpkit) ' ++ export PS1 ++ alias pydoc ++ '[' -n /bin/bash ']' ++ hash -r ++ which pip + export PIP=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip + PIP=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip + python /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade pip Requirement already up-to-date: pip in ./venv2_gpkit/lib/python2.7/site-packages + [[ macys == *reynolds* ]] + [[ macys == *macys* ]] + [[ mosek == mosek ]] + [[ macys == macys_Sierra ]] + export PATH=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin + PATH=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin + export DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin + DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin + python /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/setup.py install running install running build running build_py running install_lib creating /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib/mosek/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib/mosek/array.py -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek creating /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib/mosek/fusion/__init__.py -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib/mosek/fusion/SolverInfo.py -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib/mosek/fusion/Utils.py -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/__init__.py to __init__.pyc byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/array.py to array.pyc byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/__init__.py to __init__.pyc byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/SolverInfo.py to SolverInfo.pyc byte-compiling /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/Utils.py to Utils.pyc running install_data copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosek64.7.1.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosekglb64.7.1.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libiomp5.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosekxx7_1.dylib -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../../../../license.pdf -> /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek running install_egg_info Writing /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/Mosek-7.1.28-py2.7.egg-info Please review the MOSEK license conditions in license.pdf + [[ mosek == cvxopt ]] + [[ mosek == mosek ]] + python -c '__import__("mosek").Env()' + msktestlic Computer Platform : MACOSX/64-X86 Cores : 8 Problem Name : Objective sense : min Type : LO (linear optimization problem) Constraints : 1 Cones : 0 Scalar variables : 5000 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator - tries : 0 time : 0.00 Eliminator - elim's : 0 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.01 ************************************ A license was checked out correctly. ************************************ + export 'GPKITSOLVERS=mosek, mosek_cli' + GPKITSOLVERS='mosek, mosek_cli' + [[ mosek == cvxopt ]] + python /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade xmlrunner /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:318: SNIMissingWarning: An HTTPS request has been made, but the SNI (Subject Name Indication) extension to TLS is not available on this platform. This may cause the server to present an incorrect TLS certificate, which can cause validation failures. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#snimissingwarning. SNIMissingWarning /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:122: InsecurePlatformWarning: A true SSLContext object is not available. This prevents urllib3 from configuring SSL appropriately and may cause certain SSL connections to fail. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#insecureplatformwarning. InsecurePlatformWarning Requirement already up-to-date: xmlrunner in /Library/Python/2.7/site-packages + python /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade pint /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:318: SNIMissingWarning: An HTTPS request has been made, but the SNI (Subject Name Indication) extension to TLS is not available on this platform. This may cause the server to present an incorrect TLS certificate, which can cause validation failures. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#snimissingwarning. SNIMissingWarning /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:122: InsecurePlatformWarning: A true SSLContext object is not available. This prevents urllib3 from configuring SSL appropriately and may cause certain SSL connections to fail. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#insecureplatformwarning. InsecurePlatformWarning Collecting pint Installing collected packages: pint Found existing installation: Pint 0.7.2 Not uninstalling pint at /Library/Python/2.7/site-packages, outside environment /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit Successfully installed pint-0.8.1 + python /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade numpy /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:318: SNIMissingWarning: An HTTPS request has been made, but the SNI (Subject Name Indication) extension to TLS is not available on this platform. This may cause the server to present an incorrect TLS certificate, which can cause validation failures. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#snimissingwarning. SNIMissingWarning /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:122: InsecurePlatformWarning: A true SSLContext object is not available. This prevents urllib3 from configuring SSL appropriately and may cause certain SSL connections to fail. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#insecureplatformwarning. InsecurePlatformWarning Collecting numpy Using cached numpy-1.13.3-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl Installing collected packages: numpy Found existing installation: numpy 1.9.2 Not uninstalling numpy at /Library/Python/2.7/site-packages/numpy-1.9.2-py2.7-macosx-10.9-intel.egg, outside environment /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit Successfully installed numpy-1.13.3 + python /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade scipy /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:318: SNIMissingWarning: An HTTPS request has been made, but the SNI (Subject Name Indication) extension to TLS is not available on this platform. This may cause the server to present an incorrect TLS certificate, which can cause validation failures. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#snimissingwarning. SNIMissingWarning /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:122: InsecurePlatformWarning: A true SSLContext object is not available. This prevents urllib3 from configuring SSL appropriately and may cause certain SSL connections to fail. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#insecureplatformwarning. InsecurePlatformWarning Collecting scipy Using cached scipy-1.0.0-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl 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 0.11.0 Not uninstalling scipy at /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python, outside environment /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit Successfully installed scipy-1.0.0 + python /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade ctypesgen /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:318: SNIMissingWarning: An HTTPS request has been made, but the SNI (Subject Name Indication) extension to TLS is not available on this platform. This may cause the server to present an incorrect TLS certificate, which can cause validation failures. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#snimissingwarning. SNIMissingWarning /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:122: InsecurePlatformWarning: A true SSLContext object is not available. This prevents urllib3 from configuring SSL appropriately and may cause certain SSL connections to fail. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#insecureplatformwarning. InsecurePlatformWarning Requirement already up-to-date: ctypesgen in /Library/Python/2.7/site-packages + python /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade pandas Collecting pandas /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:318: SNIMissingWarning: An HTTPS request has been made, but the SNI (Subject Name Indication) extension to TLS is not available on this platform. This may cause the server to present an incorrect TLS certificate, which can cause validation failures. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#snimissingwarning. SNIMissingWarning /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pip/_vendor/requests/packages/urllib3/util/ssl_.py:122: InsecurePlatformWarning: A true SSLContext object is not available. This prevents urllib3 from configuring SSL appropriately and may cause certain SSL connections to fail. You can upgrade to a newer version of Python to solve this. For more information, see https://urllib3.readthedocs.io/en/latest/security.html#insecureplatformwarning. InsecurePlatformWarning Using cached pandas-0.21.1-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl Collecting python-dateutil (from pandas) Using cached python_dateutil-2.6.1-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 pytz>=2011k (from pandas) Using cached pytz-2017.3-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: six, python-dateutil, pytz, pandas Found existing installation: six 1.10.0 Not uninstalling six at /Library/Python/2.7/site-packages, outside environment /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit Found existing installation: python-dateutil 1.5 Not uninstalling python-dateutil at /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python, outside environment /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit Found existing installation: pytz 2012d Not uninstalling pytz at /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python, outside environment /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit Successfully installed pandas-0.21.1 python-dateutil-2.6.1 pytz-2017.3 six-1.11.0 + export GPKITBUILD=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/build_gpkit + GPKITBUILD=/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/build_gpkit ++ which coverage + COVERAGE=/usr/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 /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/env/settings installed_solvers : mosek, mosek_cli mosek_bin_dir : /Users/jenkins/mosek/7/tools/platform/osx64x86/bin + ls /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/build_gpkit expopt.so + python -c 'from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)' Obtaining file:///Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 0.673s OK Generating XML reports... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.0542 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.108 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.232 seconds. Cloning into 'gassolar'... Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 /private/var/folders/wp/20zl4b2n0qxcrp90f31275f80000gp/T/pip-P9DHZa-build Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gassolar Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit (from gassolar==0.0.0.0) Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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... ---------------------------------------------------------------------- EE/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) EE ====================================================================== ERROR [10.264s]: test_gassolar_gas_gas_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "gas.py", line 209, in test File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 166, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 51, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [5.181s]: test_gassolar_gas_gas_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "gas.py", line 209, in test File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 166, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "gas.py", line 51, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [4.026s]: test_gassolar_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "solar.py", line 359, in test File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 309, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 49, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [3.327s]: test_gassolar_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "solar.py", line 359, in test File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 309, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 49, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ---------------------------------------------------------------------- Ran 4 tests in 22.798s FAILED (errors=4) Generating XML reports... adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 593 variables. Solving took 7.16 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 0.2090 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 593 variables. Solving took 3.33 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 0.2090 but bound is 0.2955 Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 1206 variables. Solving took 0.29 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 97517.0234 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 97518.5695 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 1206 variables. Solving took 0.296 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 97516.8049 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 97518.7552 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 /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 /private/var/folders/wp/20zl4b2n0qxcrp90f31275f80000gp/T/pip-E0xenJ-build Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) Running tests... ---------------------------------------------------------------------- EEEE ====================================================================== ERROR [0.504s]: test_model_jho_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "jho.py", line 355, in test File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ====================================================================== ERROR [0.222s]: test_model_jho_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "jho.py", line 355, in test File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ====================================================================== ERROR [0.271s]: test_model_print_perf_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "print_perf.py", line 192, in test File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ====================================================================== ERROR [0.223s]: test_model_print_perf_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "print_perf.py", line 192, in test File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 322, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "jho.py", line 58, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/set.py", line 59, in __getitem__ return self._choosevar(key, self.variables_byname(key)) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/set.py", line 63, in _choosevar raise KeyError(key) KeyError: 'm_w' ---------------------------------------------------------------------- Ran 4 tests in 1.220s FAILED (errors=4) Generating XML reports... adding test for 'model/jho.py' adding test for 'model/print_perf.py' Cloning into 'turbofan'... Processing /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/turbofan Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 3.297s OK Generating XML reports... adding test for 'turbofan/engine_validation.py' Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528315 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%) Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485055 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Cloning into 'SPaircraft'... Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to /private/var/folders/wp/20zl4b2n0qxcrp90f31275f80000gp/T/pip-a4DjQ2-build Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 2519606.232 force_pound * meter but the right hand side evaluated to 2468463.64209 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 32774.4636554 force_pound but the right hand side evaluated to 32399.9999987 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 2.21510116791 meter but the right hand side evaluated to 1.9639617814 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 48608.9348923 newton but the right hand side evaluated to 48529.7540637 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 49704.3793689 newton but the right hand side evaluated to 49411.0984835 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 18949.086506 newton but the right hand side evaluated to 18923.0881244 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 16591.985431 newton but the right hand side evaluated to 16565.7851109 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 1002807.61359 joule / kilogram but the right hand side evaluated to 1.15239019444 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 895037.655187 joule / kilogram but the right hand side evaluated to 0.897466794343 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 1072947.09026 joule / kilogram but the right hand side evaluated to 1.19569695621 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 596870.637406 joule / kilogram but the right hand side evaluated to 0.615557181245 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 786921.823147 joule / kilogram but the right hand side evaluated to 0.790360597265 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 18.3465536705 meter but the right hand side evaluated to 16.396775738 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 11.0854063749 but the right hand side evaluated to 4.68078573795 (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 9.79174361036 but the right hand side evaluated to 4.68078573276 (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 8.22912409602 but the right hand side evaluated to 4.68078573945 (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 18.4249256546 meter but the right hand side evaluated to 18.1659848306 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 18.4249256546 meter but the right hand side evaluated to 18.2854616792 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 4.49878854459 but the right hand side evaluated to 4.61598275154 (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 4.58149985578 but the right hand side evaluated to 4.64634185828 (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 7.27503376999 but the right hand side evaluated to 4.61598275154 (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 7.45366472792 but the right hand side evaluated to 4.64634185828 (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 2504976.77617 force_pound * meter but the right hand side evaluated to 2454470.92966 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 32774.4874599 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 2.21510116794 meter but the right hand side evaluated to 1.96383106792 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 982256.835595 joule / kilogram but the right hand side evaluated to 1.20547042934 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 1151137.2905 joule / kilogram but the right hand side evaluated to 1.8837941351 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 18.4111620964 meter but the right hand side evaluated to 16.4524811464 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 11.0893101753 but the right hand side evaluated to 4.73132103007 (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 9.74913449744 but the right hand side evaluated to 4.73132102268 (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 8.19783406024 but the right hand side evaluated to 4.73132103257 (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 18.4749965574 meter but the right hand side evaluated to 18.2223419283 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 18.4749965574 meter but the right hand side evaluated to 18.3384467022 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 4.55043976265 but the right hand side evaluated to 4.66698069846 (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 4.63158648053 but the right hand side evaluated to 4.69671665344 (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 7.43022271769 but the right hand side evaluated to 4.66698069846 (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 7.49547541541 but the right hand side evaluated to 4.69671665344 (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 2481455.31991 force_pound * meter but the right hand side evaluated to 2426089.48355 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 32774.4892796 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 1.83120061022 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 1203383.57304 joule / kilogram but the right hand side evaluated to 1.66382510815 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 18.4693762575 meter but the right hand side evaluated to 16.6432014302 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 11.0473078647 but the right hand side evaluated to 4.80180930834 (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 9.67070683035 but the right hand side evaluated to 4.8018093038 (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 8.22137540879 but the right hand side evaluated to 4.80180930981 (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 18.6280054367 meter but the right hand side evaluated to 18.3449855638 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 18.6280054367 meter but the right hand side evaluated to 18.474385094 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 4.59899196072 but the right hand side evaluated to 4.72922256619 (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 4.68921354957 but the right hand side evaluated to 4.76258095594 (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 7.4556187839 but the right hand side evaluated to 4.72922256619 (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 7.54886690922 but the right hand side evaluated to 4.76258095594 (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 2455568.40292 force_pound * meter but the right hand side evaluated to 2407712.09244 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 32774.4625088 force_pound but the right hand side evaluated to 32399.9999996 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 1.99552114205 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 1227633.92312 joule / kilogram but the right hand side evaluated to 1.72359771207 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 677538.845314 joule / kilogram but the right hand side evaluated to 0.679181860451 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 18.4156356966 meter but the right hand side evaluated to 16.4239731381 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 10.9749701784 but the right hand side evaluated to 4.76255495056 (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 9.75289701434 but the right hand side evaluated to 4.76255494571 (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 8.15871867769 but the right hand side evaluated to 4.76255495183 (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 18.4488728606 meter but the right hand side evaluated to 18.2046632669 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 18.4488728606 meter but the right hand side evaluated to 18.317620254 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 4.58582637825 but the right hand side evaluated to 4.69978367526 (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 4.66559273562 but the right hand side evaluated to 4.72894507176 (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 7.50481931555 but the right hand side evaluated to 4.69978367526 (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 7.52765964565 but the right hand side evaluated to 4.72894507176 (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 2436785.6419 force_pound * meter but the right hand side evaluated to 2390898.59642 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 32774.4727321 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 2.21510116796 meter but the right hand side evaluated to 2.03201161999 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 1233975.4223 joule / kilogram but the right hand side evaluated to 1.62326325955 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 18.4095777457 meter but the right hand side evaluated to 16.3813510316 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 10.931050361 but the right hand side evaluated to 4.78771779572 (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 9.87336289689 but the right hand side evaluated to 4.78771778814 (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 8.1546470681 but the right hand side evaluated to 4.78771779786 (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 18.4102713696 meter but the right hand side evaluated to 18.1746820197 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 18.4102713696 meter but the right hand side evaluated to 18.2839317442 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 4.61574367336 but the right hand side evaluated to 4.72672201544 (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 4.69362541172 but the right hand side evaluated to 4.75513478642 (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 7.53648527184 but the right hand side evaluated to 4.72672201544 (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 7.55139991912 but the right hand side evaluated to 4.75513478642 (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 2418324.12859 force_pound * meter but the right hand side evaluated to 2374882.88584 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 32774.4714378 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 2.21510116783 meter but the right hand side evaluated to 2.082354618 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 1244506.50064 joule / kilogram but the right hand side evaluated to 1.55926550629 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 664750.101539 joule / kilogram but the right hand side evaluated to 0.6674014397 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 18.4000474441 meter but the right hand side evaluated to 16.3223787699 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 10.9040384725 but the right hand side evaluated to 4.78950263273 (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 10.0259776343 but the right hand side evaluated to 4.78950262135 (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 8.14555612113 but the right hand side evaluated to 4.78950263555 (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 18.3617997907 meter but the right hand side evaluated to 18.1374302661 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 18.3617997907 meter but the right hand side evaluated to 18.2416903719 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 4.62507773068 but the right hand side evaluated to 4.73131723723 (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 4.69987287439 but the right hand side evaluated to 4.75851445472 (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 7.56534517456 but the right hand side evaluated to 4.73131723723 (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 7.58381623912 but the right hand side evaluated to 4.75851445472 (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 2405735.03764 force_pound * meter but the right hand side evaluated to 2358168.23394 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 32774.4360263 force_pound but the right hand side evaluated to 32399.9999992 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 2.21510116809 meter but the right hand side evaluated to 1.97491259844 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 1245747.36532 joule / kilogram but the right hand side evaluated to 1.35773060236 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 18.4441328811 meter but the right hand side evaluated to 16.474974465 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 10.9331062433 but the right hand side evaluated to 4.83171722163 (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 10.1921384346 but the right hand side evaluated to 4.83171720413 (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 8.19565540562 but the right hand side evaluated to 4.83171722514 (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 18.4861274936 meter but the right hand side evaluated to 18.2368478917 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 18.4861274936 meter but the right hand side evaluated to 18.3518624415 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 4.64971762815 but the right hand side evaluated to 4.76697796961 (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 4.73177040003 but the right hand side evaluated to 4.7970419274 (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 7.54212869906 but the right hand side evaluated to 4.76697796961 (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 7.59702353757 but the right hand side evaluated to 4.7970419274 (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 2391778.66008 force_pound * meter but the right hand side evaluated to 2346059.34671 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 32774.4560168 force_pound but the right hand side evaluated to 32399.9999992 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 2.21510116809 meter but the right hand side evaluated to 2.01208208261 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 1263254.6012 joule / kilogram but the right hand side evaluated to 1.32933804471 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 643003.166308 joule / kilogram but the right hand side evaluated to 0.644587784359 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 18.43918851 meter but the right hand side evaluated to 16.4333015372 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 10.9270580924 but the right hand side evaluated to 4.82709676731 (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 10.3328494394 but the right hand side evaluated to 4.82709674915 (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 8.18819655124 but the right hand side evaluated to 4.82709677168 (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 18.4531697743 meter but the right hand side evaluated to 18.2123788076 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 18.4531697743 meter but the right hand side evaluated to 18.3237315509 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 4.65099002024 but the right hand side evaluated to 4.7645616667 (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 4.73069425364 but the right hand side evaluated to 4.7936927878 (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 7.55428851143 but the right hand sid. ---------------------------------------------------------------------- Ran 1 test in 1138.805s OK Generating XML reports... e evaluated to 4.7645616667 (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 7.61783041165 but the right hand side evaluated to 4.7936927878 (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 2376281.98754 force_pound * meter but the right hand side evaluated to 2334599.71572 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 32774.5069792 force_pound but the right hand side evaluated to 32399.9999986 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 2.21510116804 meter but the right hand side evaluated to 2.09817322809 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 1283640.81884 joule / kilogram but the right hand side evaluated to 1.28935980117 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 18.4146008244 meter but the right hand side evaluated to 16.3183399116 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 10.937463708 but the right hand side evaluated to 4.8243790453 (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 10.5713466579 but the right hand side evaluated to 4.82437903588 (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 8.19385115143 but the right hand side evaluated to 4.82437904778 (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 18.3565572611 meter but the right hand side evaluated to 18.137753638 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 18.3565572611 meter but the right hand side evaluated to 18.2401763169 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 4.66215786122 but the right hand side evaluated to 4.76702012677 (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 4.73627117897 but the right hand side evaluated to 4.79393916988 (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 7.62007115001 but the right hand side evaluated to 4.76702012677 (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 7.68939259324 but the right hand side evaluated to 4.79393916988 (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 1.13e+03 seconds. Cloning into 'solar'... Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 /private/var/folders/wp/20zl4b2n0qxcrp90f31275f80000gp/T/pip-s_srbS-build Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 /private/var/folders/wp/20zl4b2n0qxcrp90f31275f80000gp/T/pip-2coX2q-build Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit (from gassolar==0.0.0.0) Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) Processing /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/solar Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit (from solar==0.0.0.0) Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) Requirement already satisfied: gpkitmodels in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek (from solar==0.0.0.0) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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... ---------------------------------------------------------------------- /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun) ....EE ====================================================================== ERROR [10.259s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "solar.py", line 486, in test File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 467, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 85, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ====================================================================== ERROR [7.166s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "solar.py", line 486, in test File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 467, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 85, in setup File "/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member TypeError: setup() takes exactly 4 arguments (5 given) ---------------------------------------------------------------------- Ran 6 tests in 144.729s FAILED (errors=2) 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 5670 variables. Solving took 1.33 seconds. Warning: Variable Re_Mission/FlightSegment.38/AircraftPerf.38/WingAero.38 could cause inaccurate result because it is below lower bound. Solution is 120042.1846 but bound is 125000.0000 Warning: Variable Re_Mission/FlightSegment.39/AircraftPerf.39/WingAero.39 could cause inaccurate result because it is below lower bound. Solution is 121471.1982 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 1.42 seconds. Warning: Variable Re_Mission.1/FlightSegment.78/AircraftPerf.78/WingAero.78 could cause inaccurate result because it is below lower bound. Solution is 122823.1089 but bound is 125000.0000 Warning: Variable Re_Mission.1/FlightSegment.79/AircraftPerf.79/WingAero.79 could cause inaccurate result because it is below lower bound. Solution is 123244.6837 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 0.891 seconds. Using solver 'mosek' Solving for 2910 variables. Solving took 0.459 seconds. Using solver 'mosek' Solving for 5670 variables. Solving took 1.15 seconds. Warning: Variable Re_Mission/FlightSegment.38/AircraftPerf.38/WingAero.38 could cause inaccurate result because it is below lower bound. Solution is 120042.1845 but bound is 125000.0000 Warning: Variable Re_Mission/FlightSegment.39/AircraftPerf.39/WingAero.39 could cause inaccurate result because it is below lower bound. Solution is 121471.1971 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 1.24 seconds. Warning: Variable Re_Mission.1/FlightSegment.78/AircraftPerf.78/WingAero.78 could cause inaccurate result because it is below lower bound. Solution is 122823.1089 but bound is 125000.0000 Warning: Variable Re_Mission.1/FlightSegment.79/AircraftPerf.79/WingAero.79 could cause inaccurate result because it is below lower bound. Solution is 123244.6837 but bound is 125000.0000 Using solver 'mosek' Solving for 5670 variables. Solving took 0.859 seconds. Using solver 'mosek' Solving for 2910 variables. Solving took 0.59 seconds. Using solver 'mosek' Solving for 288 variables. Solving took 0.671 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 122179.8905 but bound is 125000.0000 Using solver 'mosek' Solving for 288 variables. Solving took 1.4 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 122179.8905 but bound is 125000.0000 Using solver 'mosek' Solving for 2910 variables. Solving took 0.516 seconds. Using solver 'mosek_cli' Solving for 2910 variables. Solving took 0.816 seconds. Cloning into 'gplibrary'... Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 /private/var/folders/wp/20zl4b2n0qxcrp90f31275f80000gp/T/pip-mYgS3w-build Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gpkit (from gpfit==0.1) Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) Processing /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gplibrary Requirement already satisfied (use --upgrade to upgrade): gpkitmodels==0.0.0.0 from file:///Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/gplibrary in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek Requirement already satisfied: numpy>=1.12 in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 5.964s 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 2262061.5401 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2262061.2755 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 2262068.0066 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2262068.0066 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 USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 [Execution node] check if [macys] is in [[windows10x64, windows7x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] Build step 'Console output (build log) parsing' changed build result to FAILURE [xUnit] [INFO] - Starting to record. [xUnit] [INFO] - Processing JUnit [xUnit] [INFO] - [JUnit] - 7 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/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 FAILURE [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: FAILURE