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Started by upstream project "gplibrary_Push_Models" build number 191 originally caused by: Started by GitHub push by bqpd Running as SYSTEM [EnvInject] - Loading node environment variables. Building remotely on macys in workspace /Users/jenkins/workspace/gplibrary_Push_Models/mosek No credentials specified Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > git init /Users/jenkins/workspace/gplibrary_Push_Models/mosek # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git --version # timeout=10 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* # timeout=10 > 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 # timeout=10 Checking out Revision 145ec7275df0fabdf50524f8ca1ac0334caf59a6 (origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f 145ec7275df0fabdf50524f8ca1ac0334caf59a6 # timeout=3 Commit message: "multiline setup for parse_variables" > git rev-list --no-walk 63ae1326e4eefeecd9a48333e95458ee330210b2 # timeout=10 Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [Execution node] check if [macys] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] enabling perform for step [Execute shell] [mosek] $ /bin/bash -xe /var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/jenkins6740194368252443792.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 /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit New python executable in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/python Installing setuptools, pip, wheel...done. + . /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/activate ++ deactivate nondestructive ++ unset -f pydoc ++ '[' -z '' ']' ++ '[' -z '' ']' ++ '[' -n /bin/bash ']' ++ hash -r ++ '[' -z '' ']' ++ unset VIRTUAL_ENV ++ '[' '!' nondestructive = nondestructive ']' ++ VIRTUAL_ENV=/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit ++ export VIRTUAL_ENV ++ _OLD_VIRTUAL_PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export PATH ++ '[' -z '' ']' ++ '[' -z '' ']' ++ _OLD_VIRTUAL_PS1= ++ '[' x '!=' x ']' +++ basename /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit ++ PS1='(venv2_gpkit) ' ++ export PS1 ++ alias pydoc ++ '[' -n /bin/bash ']' ++ hash -r ++ which pip + export PIP=/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip + PIP=/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip + pip_install pip + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade pip DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Requirement already up-to-date: pip in ./venv2_gpkit/lib/python2.7/site-packages (19.2.3) + [[ macys == *reynolds* ]] + [[ macys == *macys* ]] + [[ mosek == mosek ]] + [[ macys == macys ]] + export PATH=/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin + PATH=/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin + export DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin + DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin + python /Users/jenkins/mosek/8/tools/platform/osx64x86/python/2/setup.py install running install running build running build_py running build_ext copying mosek/_msk.so -> build/lib.macosx-10.13-intel-2.7/mosek copying mosek/fusion/impl/fragments.so -> build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl running install_lib creating /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib.macosx-10.13-intel-2.7/mosek/__init__.py -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib.macosx-10.13-intel-2.7/mosek/_msk.so -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek creating /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/__init__.py -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion creating /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl/__init__.py -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl/_implementation.py -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl/fragments.so -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/Utils.py -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion byte-compiling /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/__init__.py to __init__.pyc byte-compiling /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/__init__.py to __init__.pyc byte-compiling /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl/__init__.py to __init__.pyc byte-compiling /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl/_implementation.py to _implementation.pyc byte-compiling /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/Utils.py to Utils.pyc running install_egg_info Writing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/Mosek-8.1.41-py2.7.egg-info Fixing library paths copying /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/ copying /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libcilkrts.5.dylib -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/ + [[ mosek == mosek ]] + python -c '__import__("mosek").Env()' + msktestlic Mosek license manager: License path: /Users/jenkins/mosek/mosek.lic Mosek license manager: Checkout license feature 'PTS' from flexlm. Mosek license manager: Checkout time 0.01. r: 0 status: 0 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. Presolve started. Eliminator started. Freed constraints in eliminator : 0 Eliminator terminated. Eliminator - tries : 1 time : 0.00 Lin. dep. - tries : 0 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Optimizer terminated. Time: 0.00 ************************************ A license was checked out correctly. ************************************ + export 'GPKITSOLVERS=mosek, mosek_cli' + GPKITSOLVERS='mosek, mosek_cli' + [[ mosek == cvxopt ]] + pip_install xmlrunner + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade xmlrunner DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting xmlrunner Installing collected packages: xmlrunner Successfully installed xmlrunner-1.7.7 + pip_install pint + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade pint DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting pint Using cached https://files.pythonhosted.org/packages/15/9d/bf177ebbc57d25e9e296addc14a1303d1e34d7964af5df428a8332349c42/Pint-0.9-py2.py3-none-any.whl Collecting funcsigs; python_version == "2.7" (from pint) Using cached https://files.pythonhosted.org/packages/69/cb/f5be453359271714c01b9bd06126eaf2e368f1fddfff30818754b5ac2328/funcsigs-1.0.2-py2.py3-none-any.whl Installing collected packages: funcsigs, pint Successfully installed funcsigs-1.0.2 pint-0.9 + pip_install numpy + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade numpy DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting numpy Using cached https://files.pythonhosted.org/packages/51/67/8907005262f493e356195bcbd61b41988eecf63cb1d97ea2f6e55fe24205/numpy-1.16.5-cp27-cp27m-macosx_10_9_x86_64.whl Installing collected packages: numpy Successfully installed numpy-1.16.5 + pip_install scipy + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade scipy DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting scipy Using cached https://files.pythonhosted.org/packages/a3/cf/36b77de4ccb1b841acd4c3c03abe38843c63c3a657cedee9e8fb19a02dc8/scipy-1.2.2-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl Requirement already satisfied, skipping upgrade: numpy>=1.8.2 in ./venv2_gpkit/lib/python2.7/site-packages (from scipy) (1.16.5) Installing collected packages: scipy Successfully installed scipy-1.2.2 + pip_install ad + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade ad DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting ad Installing collected packages: ad Successfully installed ad-1.3.2 + pip_install ctypesgen + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade ctypesgen DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting ctypesgen Installing collected packages: ctypesgen Successfully installed ctypesgen-0.post125 + pip_install pandas + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade pandas DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting pandas Using cached https://files.pythonhosted.org/packages/52/ff/912fe03a623a70bcf297d466013a0b4f4c68c3b60f86bf226682d061fc09/pandas-0.24.2-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl Collecting python-dateutil>=2.5.0 (from pandas) Using cached https://files.pythonhosted.org/packages/41/17/c62faccbfbd163c7f57f3844689e3a78bae1f403648a6afb1d0866d87fbb/python_dateutil-2.8.0-py2.py3-none-any.whl Requirement already satisfied, skipping upgrade: numpy>=1.12.0 in ./venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5) Collecting pytz>=2011k (from pandas) Using cached https://files.pythonhosted.org/packages/87/76/46d697698a143e05f77bec5a526bf4e56a0be61d63425b68f4ba553b51f2/pytz-2019.2-py2.py3-none-any.whl Collecting six>=1.5 (from python-dateutil>=2.5.0->pandas) Using cached https://files.pythonhosted.org/packages/73/fb/00a976f728d0d1fecfe898238ce23f502a721c0ac0ecfedb80e0d88c64e9/six-1.12.0-py2.py3-none-any.whl Installing collected packages: six, python-dateutil, pytz, pandas Successfully installed pandas-0.24.2 python-dateutil-2.8.0 pytz-2019.2 six-1.12.0 + pip_install matplotlib + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade matplotlib DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting matplotlib Using cached https://files.pythonhosted.org/packages/3e/d6/4c949597c4186599cc8be08cd11b1e83fe7966676aeee3868bf3e581d852/matplotlib-2.2.4-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 kiwisolver>=1.0.1 (from matplotlib) Using cached https://files.pythonhosted.org/packages/0d/15/ec5f70ac79f378ed0ef5ed8b71e8a04e382115426b2cda9a3ab5ffcf467f/kiwisolver-1.1.0-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl Collecting cycler>=0.10 (from matplotlib) Using cached https://files.pythonhosted.org/packages/f7/d2/e07d3ebb2bd7af696440ce7e754c59dd546ffe1bbe732c8ab68b9c834e61/cycler-0.10.0-py2.py3-none-any.whl Collecting subprocess32 (from matplotlib) Using cached https://files.pythonhosted.org/packages/35/f3/7cdeeef9cb05c42fadcc8aa040dd3b80d94e0f6a8dedc4bacebf796c2385/subprocess32-3.5.4-cp27-cp27m-macosx_10_6_intel.whl Requirement already satisfied, skipping upgrade: pytz in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2019.2) Requirement already satisfied, skipping upgrade: six>=1.10 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.12.0) Collecting backports.functools-lru-cache (from matplotlib) Using cached https://files.pythonhosted.org/packages/03/8e/2424c0e65c4a066e28f539364deee49b6451f8fcd4f718fefa50cc3dcf48/backports.functools_lru_cache-1.5-py2.py3-none-any.whl Requirement already satisfied, skipping upgrade: numpy>=1.7.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.16.5) Collecting pyparsing!=2.0.4,!=2.1.2,!=2.1.6,>=2.0.1 (from matplotlib) Using cached https://files.pythonhosted.org/packages/11/fa/0160cd525c62d7abd076a070ff02b2b94de589f1a9789774f17d7c54058e/pyparsing-2.4.2-py2.py3-none-any.whl Requirement already satisfied, skipping upgrade: python-dateutil>=2.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2.8.0) Requirement already satisfied, skipping upgrade: setuptools in ./venv2_gpkit/lib/python2.7/site-packages (from kiwisolver>=1.0.1->matplotlib) (41.2.0) Installing collected packages: kiwisolver, cycler, subprocess32, backports.functools-lru-cache, pyparsing, matplotlib Successfully installed backports.functools-lru-cache-1.5 cycler-0.10.0 kiwisolver-1.1.0 matplotlib-2.2.4 pyparsing-2.4.2 subprocess32-3.5.4 + pip_install future + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade future DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting future Installing collected packages: future Successfully installed future-0.17.1 + export GPKITBUILD=/Users/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit + GPKITBUILD=/Users/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit + python -c 'import scipy; print scipy.__version__' 1.2.2 + python -c 'import numpy; print numpy.__version__' 1.16.5 + python -c 'import pint; print pint.__version__' 0.9 + git clone --depth 1 https://github.com/convexengineering/gpkit.git Cloning into 'gpkit'... + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Obtaining file:///Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit Requirement already satisfied: numpy>=1.13.3 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.9.1.0) (1.16.5) Requirement already satisfied: pint>=0.8.1 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.9.1.0) (0.9) Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.9.1.0) (1.2.2) Requirement already satisfied: ad in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.9.1.0) (1.3.2) Collecting cvxopt>=1.1.8 (from gpkit==0.9.1.0) Downloading https://files.pythonhosted.org/packages/69/4f/167a7f5b11274eb8722e93b26c687c71499ae563083104c5b25dd2252990/cvxopt-1.2.3-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 (5.7MB) Requirement already satisfied: six in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.9.1.0) (1.12.0) Requirement already satisfied: funcsigs; python_version == "2.7" in ./venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit==0.9.1.0) (1.0.2) Installing collected packages: cvxopt, gpkit Running setup.py develop for gpkit Successfully installed cvxopt-1.2.3 gpkit + python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_Push_Models/mosek DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Obtaining file:///Users/jenkins/workspace/gplibrary_Push_Models/mosek Requirement already satisfied: numpy>=1.12 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.16.5) Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.2.2) Requirement already satisfied: pint in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.9) Requirement already satisfied: funcsigs; python_version == "2.7" in ./venv2_gpkit/lib/python2.7/site-packages (from pint->gpkitmodels==0.0.0.0) (1.0.2) Installing collected packages: gpkitmodels Running setup.py develop for gpkitmodels Successfully installed gpkitmodels + export MSK_IPAR_NUM_THREADS=2 + MSK_IPAR_NUM_THREADS=2 + export MKL_NUM_THREADS=2 + MKL_NUM_THREADS=2 + export NUMEXPR_NUM_THREADS=2 + NUMEXPR_NUM_THREADS=2 + export OPENBLAS_NUM_THREADS=2 + OPENBLAS_NUM_THREADS=2 + export OMP_NUM_THREADS=2 + OMP_NUM_THREADS=2 + python -c 'from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True)' No filename given. Usage: mskexpopt FILENAME [-primal] [-dual] [-p parameterfile] Return code: 1052 Description: MSK_RES_ERR_FILE_OPEN [An error occurred while opening a file.] ................................................................................................................................................................................................................................................... ---------------------------------------------------------------------- Ran 243 tests in 17.684s OK Cloning into 'gplibrary'... DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Obtaining file:///Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary 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 'robust'... DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Processing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/robust Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from robust==0.0.0) (0.9.1.0) Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from robust==0.0.0) (1.16.5) Requirement already satisfied: matplotlib in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from robust==0.0.0) (2.2.4) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from robust==0.0.0) (1.2.2) Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->robust==0.0.0) (0.9) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->robust==0.0.0) (1.3.2) Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->robust==0.0.0) (1.2.3) Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->robust==0.0.0) (1.12.0) Requirement already satisfied: kiwisolver>=1.0.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (1.1.0) Requirement already satisfied: cycler>=0.10 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (0.10.0) Requirement already satisfied: subprocess32 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (3.5.4) Requirement already satisfied: pytz in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (2019.2) Requirement already satisfied: backports.functools-lru-cache in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (1.5) Requirement already satisfied: pyparsing!=2.0.4,!=2.1.2,!=2.1.6,>=2.0.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (2.4.2) Requirement already satisfied: python-dateutil>=2.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (2.8.0) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->robust==0.0.0) (1.0.2) Requirement already satisfied: setuptools in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from kiwisolver>=1.0.1->matplotlib->robust==0.0.0) (41.2.0) Building wheels for collected packages: robust Building wheel for robust (setup.py): started Building wheel for robust (setup.py): finished with status 'done' Created wheel for robust: filename=robust-0.0.0-cp27-none-any.whl size=217819 sha256=c7492f5384adb9a6f40a9f1e8035d8d252d448ef217295622e02cac3de536d54 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-l55Kw3/wheels/f5/9a/8f/c003ca5afde488728c792838e0c6645a1e18500b3cc3703684 Successfully built robust Installing collected packages: robust Successfully installed robust-0.0.0 Running tests... ---------------------------------------------------------------------- .......... ---------------------------------------------------------------------- Ran 10 tests in 18.220s OK Generating XML reports... adding test for 'robust/testing/t_linearization.py' adding test for 'robust/testing/t_equivalent_posynomials.py' adding test for 'robust/testing/t_two_term_approximation.py' adding test for 'robust/testing/t_robust_gp_tools.py' adding test for 'robust/testing/t_primitives.py' Cloning into 'shopping'... Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 0.141s OK Generating XML reports... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.0109 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.00978 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.0319 seconds. Cloning into 'gassolar'... DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2) Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.8.0) Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2019.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0) DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-Y2NC4G Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-Y2NC4G Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.5) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gpfit==0.1) (0.9.1.0) Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2) Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3) Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.12.0) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2) Building wheels for collected packages: gpfit Building wheel for gpfit (setup.py): started Building wheel for gpfit (setup.py): finished with status 'done' Created wheel for gpfit: filename=gpfit-0.1-cp27-none-any.whl size=25151 sha256=18390403adff307f322b79d99f105b5713d26f60696368b75a7f250f5702dee6 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-nUDLUy/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Installing collected packages: gpfit Successfully installed gpfit-0.1 DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Processing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gassolar Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.16.5) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.2.2) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.9.1.0) Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.24.2) Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.9) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.2.3) Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.12.0) Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.8.0) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2019.2) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gassolar==0.0.0.0) (1.0.2) Building wheels for collected packages: gassolar Building wheel for gassolar (setup.py): started Building wheel for gassolar (setup.py): finished with status 'done' Created wheel for gassolar: filename=gassolar-0.0.0.0-cp27-none-any.whl size=4876517 sha256=88196ad6d1ec2f32dc2d6be06a59eb84fe58d4d3a766be945ba467eb436f1b53 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-bDZ_sc/wheels/41/0a/8d/447392359ea0dc499510d6781d4893f34e301ac2b844c7bed4 Successfully built gassolar Installing collected packages: gassolar Successfully installed gassolar-0.0.0.0 Running tests... ---------------------------------------------------------------------- EEEE ====================================================================== ERROR [0.009s]: test_gassolar_gas_gas_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "gas.py", line 4, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.001s]: test_gassolar_gas_gas_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "gas.py", line 4, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.116s]: test_gassolar_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "solar.py", line 12, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.001s]: test_gassolar_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "solar.py", line 12, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ---------------------------------------------------------------------- Ran 4 tests in 0.127s FAILED (errors=4) Generating XML reports... adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Cloning into 'jho'... DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2) Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.8.0) Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2019.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0) DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-5ARfV7 Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-5ARfV7 Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.5) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gpfit==0.1) (0.9.1.0) Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2) Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3) Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.12.0) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2) Building wheels for collected packages: gpfit Building wheel for gpfit (setup.py): started Building wheel for gpfit (setup.py): finished with status 'done' Created wheel for gpfit: filename=gpfit-0.1-cp27-none-any.whl size=25151 sha256=d513f6c6e0c21c93db0ae14235c89efee96139075d385062eebddda7f4672783 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-aUvEJH/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Running tests... ---------------------------------------------------------------------- EEEE ====================================================================== ERROR [0.009s]: test_model_jho_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "jho.py", line 6, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/SP/aircraft/wing/wing.py", line 3, in <module> from gpkitmodels.GP.aircraft.wing.wing import Wing as WingGP File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.001s]: test_model_jho_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "jho.py", line 6, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/SP/aircraft/wing/wing.py", line 3, in <module> from gpkitmodels.GP.aircraft.wing.wing import Wing as WingGP File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.093s]: test_model_print_perf_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "print_perf.py", line 4, in <module> File "jho.py", line 6, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/SP/aircraft/wing/wing.py", line 3, in <module> from gpkitmodels.GP.aircraft.wing.wing import Wing as WingGP File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.002s]: test_model_print_perf_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "print_perf.py", line 4, in <module> File "jho.py", line 6, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/SP/aircraft/wing/wing.py", line 3, in <module> from gpkitmodels.GP.aircraft.wing.wing import Wing as WingGP File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ---------------------------------------------------------------------- Ran 4 tests in 0.105s FAILED (errors=4) Generating XML reports... adding test for 'model/jho.py' adding test for 'model/print_perf.py' Cloning into 'turbofan'... DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Processing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/turbofan Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.16.5) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.2.2) Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.9) Requirement already satisfied: future in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.17.1) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint->turbofan==0.0.0.0) (1.0.2) Building wheels for collected packages: turbofan Building wheel for turbofan (setup.py): started Building wheel for turbofan (setup.py): finished with status 'done' Created wheel for turbofan: filename=turbofan-0.0.0.0-cp27-none-any.whl size=45142 sha256=73e572546adfbf8ca7e0ccc8c5e9e40ea8136d33e9ddf1832254466ab07671d1 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-6tQxA_/wheels/b5/2f/48/b751d4bab5d719a7de0cd9181de34b2f4449cb2da5aec6f23d Successfully built turbofan Installing collected packages: turbofan Successfully installed turbofan-0.0.0.0 Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 0.899s OK Generating XML reports... adding test for 'turbofan/engine_test.py' Beginning signomial solve. Using solver 'mosek' Solving for 327 variables. Solving took 0.0277 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.0187 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.0333 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.0237 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.019 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.0317 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.0274 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.0192 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.0206 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.0258 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.0219 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.024 seconds. Using solver 'mosek' Solving for 327 variables. Solving took 0.0238 seconds. Solving took 13 GP solves and 0.631 seconds. Cloning into 'SPaircraft'... DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-aluYth Running command git clone -q https://github.com/hoburg/turbofan.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-aluYth 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_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.16.5) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.2.2) Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.9) Requirement already satisfied: future in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.17.1) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint->turbofan==0.0.0.0) (1.0.2) Building wheels for collected packages: turbofan Building wheel for turbofan (setup.py): started Building wheel for turbofan (setup.py): finished with status 'done' Created wheel for turbofan: filename=turbofan-0.0.0.0-cp27-none-any.whl size=45142 sha256=95d9781e4b9b7b7d0079d58a1245046fa8e12951cf3f0721fab44eb4a5b1abc5 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-hA06g0/wheels/49/e6/3a/5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5 Successfully built turbofan DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Processing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/SPaircraft Requirement already satisfied: turbofan in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from SPaircraft==0.0.0) (0.0.0.0) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from SPaircraft==0.0.0) (0.9.1.0) Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan->SPaircraft==0.0.0) (0.9) Requirement already satisfied: future in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan->SPaircraft==0.0.0) (0.17.1) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan->SPaircraft==0.0.0) (1.2.2) Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan->SPaircraft==0.0.0) (1.16.5) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->SPaircraft==0.0.0) (1.3.2) Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->SPaircraft==0.0.0) (1.2.3) Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->SPaircraft==0.0.0) (1.12.0) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint->turbofan->SPaircraft==0.0.0) (1.0.2) Building wheels for collected packages: SPaircraft Building wheel for SPaircraft (setup.py): started Building wheel for SPaircraft (setup.py): finished with status 'done' Created wheel for SPaircraft: filename=SPaircraft-0.0.0-cp27-none-any.whl size=1833 sha256=a97c306ab634197c1bb36c0349d33f373245c9c70971d6d5af532ef1a5d021da Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-vq9IwZ/wheels/71/26/9f/5657db356ce6e0d3f9591b290e0bbf5df5bca9ab5b75809f6a Successfully built SPaircraft Installing collected packages: SPaircraft Successfully installed SPaircraft-0.0.0 Running tests... ---------------------------------------------------------------------- adding test for 'SPaircraft.py' Mission ======= Cost ---- W_{f_{total}}[:].sum() Constraints ----------- W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin} PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:]) x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:]) x_{CG}[3] <= \Delta x_n + x_n \Delta x_m + x_{CG}[3] >= x_m \tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m C_{D_{fuse}}[:] = 0.018081 M_{fuseD} = 0.72 W_{start}[0] = W_{total}[:] W_{start}[:] >= W_{end}[:] + W_{burn}[:] W_{start}[1:] = W_{end}[:4] W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1] W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2] W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1] hft[2] >= CruiseAlt hft[1:5] = hft[:4] + dhft[1:5] hft[0] = dhft[0] dhft[1:3] = dhft[:2] RC[0] >= 2.5e+03 RC[:3] >= RC_{min}[:3] \theta[2] >= 0.015 hft[2] >= MinCruiseAlt n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:] R_{segment}[3:4] = R_{segment}[4:5] M[3:5] >= M_{min} 0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req} Fsafetyfac*F[0] = T_e W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:] V_2[:] = M_2[:]*a[:] \alpha_{max,w}[:3] = 0.18 \alpha_{max,w}[3:] = 0.1 0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime 0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime ClimbTime <= MaxClimbTime T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}} F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:] F_{fuel}[:] <= 1.0000001 F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:] F_{fuel}[:] <= 1.0000001 F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:] F_{fuel}[:] <= 1.0000001 F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:] F_{fuel}[:] <= 1.0000001 F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:] F_{fuel}[:] <= 1.0000001 OPR[:] <= OPR_{max} Aircraft Fuselage W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on} W_{pass}[:] >= n_{pass}[:]*W_{avg. pass} W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo} W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}} W_{payload}[:] <= W_{payload_{max}} n_{pass}[:] <= n_{seat} n_{rows} = n_{seat}/SPR l_{shell} = n_{rows}*p_s \theta_{db} = w_{db}/R_{fuse} R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db} A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db} (PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse} A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin} w_{floor} = w_{fuse} R_{fuse} + w_{db} >= w_{fuse} h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse} t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell} S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2 S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2 l_{fuse} = l_{nose} + l_{shell} + l_{cone} l_{cone} = R_{fuse}/\lambda_{cone} x_{shell1} = l_{nose} x_{shell2} >= l_{nose} + l_{shell} t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin} t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin} \sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell}) \sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin} l_{floor} >= l_{shell} + 2*R_{fuse} P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat}) A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor} V_{floor} = 2*w_{floor}*A_{floor} W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor} \tau_{cone} = \sigma_{skin} W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame}) x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone} -2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}} (PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}} x_{hbend_{Land}} >= x_{wing} x_{hbend_{Land}} <= l_{fuse} x_{hbend_{MLF}} >= x_{wing} x_{hbend_{MLF}} <= l_{fuse} A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}}) A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}}) A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h}) A_{2h_{MLF}} >= Mission.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h}) A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2) A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}} A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}} A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}} A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}} A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}} A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}} A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}} A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}} V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission.Aircraft.Fuselage.r_{w/c} V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission.Aircraft.Fuselage.r_{w/c} V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}} W_{hbend} >= g*\rho_{bend}*V_{hbend} x_{vbend} >= x_{wing} x_{vbend} <= l_{fuse} B_{0v} = B_{1v}*(x_{tail} - x_{vbend}) B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2) B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}} 0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}} V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission.Aircraft.Fuselage.r_{w/c} V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}} W_{vbend} >= \rho_{bend}*g*V_{vbend} x_f = x_{wing} + 0.5*c_0*Mission.Aircraft.Fuselage.r_{w/c} x_b = x_{wing} - 0.5*c_0*Mission.Aircraft.Fuselage.r_{w/c} \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h} \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v} V_{cyl} = A_{skin}*l_{shell} V_{nose} = S_{nose}*t_{skin} V_{bulk} = S_{bulk}*t_{skin} V_{db} = A_{db}*l_{shell} V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse}) W_{apu} = W_{payload_{max}}*f_{apu} W_{db} = \rho_{skin}*g*V_{db} W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk}) W_{window} >= W'_{window}*l_{shell} W_{padd} = W_{payload_{max}}*f_{padd} W_{seat} >= W'_{seat}*n_{seat} W_{seat} >= f_{seat}*W_{payload_{max}} W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk}) W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db} W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone}) Wing WingNoStruct A_{rect} = c_{tip}*b 0.5*(1 - \lambda)*c_{root}*b <= A_{tri} p >= 1 + 2*\lambda 2*q >= 1 + p y_{mac} = b/3*q/p mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q \lambda = c_{tip}/c_{root} S = b*(c_{root} + c_{tip})/2 0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w) e*(1 + f(\lambda_w)*AR) <= 1 \lambda >= 0.15 V_{fuel, max} <= 0.303*mac^2*b*\tau W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g b <= b_{max} WingBox AR = b^2/S 0.423*Mission.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap} \nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56 W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5) \tau <= \tau_{max_w} W_{struct} >= W_{web} + W_{cap} AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12 W_{cap} >= 8*\rho_{cap}*g*Mission.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5) Mission.Aircraft.Wing.WingBox.N_{lift} = 3 Mission.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8 \lambda = taper W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt}) 0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}} Engine Compressor (no constraints) Combustor (no constraints) Turbine (no constraints) Thrust (no constraints) FanMap (no constraints) LPCMap (no constraints) HPCMap (no constraints) Sizing A_{2} >= A_{5} + A_{7} FlightState V[:] = V[:] a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5 V[:] = M[:]*a[:] Altitude h[:] = hft[:] Atmosphere (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:] \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:]) T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:] \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72) EnginePerformance CompressorPerformance T_{t_0}[:] = T_{atm}[:]/c1[:]^-1 h_{t_0}[:] = C_{p_{air}*T_{t_0}[:] P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:] T_{t_{1.8}}[:] = T_{t_0}[:] h_{t_{1.8}}[:] = h_{t_0}[:] P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5 T_{T_{2}}[:] = T_{t_{1.8}}[:] h_{T_{2}}[:] = h_{t_{1.8}}[:] P_{T_{2}}[:] = P_{t_{1.8}}[:] P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:] T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016 h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:] P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:] T_{t_7}[:] = T_{t_{2.1}}[:] h_{t_7}[:] = h_{t_{2.1}}[:] P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:] T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152 h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1} P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:] T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491 h_{t_3}[:] = C_{p_{2}*T_{t_3}[:] CombustorPerformance h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:] h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:] fp1[:] = f[:] + 1 M_{4a}[:] = 0.1025 fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5 T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]] P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891 u_{4a}[:] = M_{4a}[:]*(1.31*Mission.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a} u_c[:] = r_{uc}*u_{4a}[:] P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891 TurbinePerformance h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:] P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:] \pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565 h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:] P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:] T_{t_5}[:] = T_{t_{4.9}}[:] h_{t_5}[:] = h_{t_{4.9}}[:] ThrustPerformance P_{8}[:] = P_{atm}[:] h_{8}[:] = C_{p_{fex}*T_{8}[:] u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:] (P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:] h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:] P_{6}[:] = P_{atm}[:] (P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:] u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:] h_6[:] = C_{p_{tex}*T_{6}[:] h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:] \alpha[:] = m_{fan}[:]/m_{core}[:] \alpha_{+1}[:] = \alpha[:] + 1 \alpha[:] <= \alpha_{max} F[:] <= F_{6}[:] + F_{8}[:] F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:]) TSFC[:] = 1/I_{sp}[:] F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:] FanMapPerformance m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}} LPCMapPerformance m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D} HPCMapPerformance m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D} SizingPerformance P_{7}[:] >= P_{atm}[:] M_7[:] <= 1 a_{7}[:] = (1.4*Mission.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5 a_{7}[:]*M_7[:] = u_{7}[:] \rho_7[:] = P_{7}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{7}[:]) P_{5}[:] >= P_{atm}[:] M_5[:] <= 1 a_{5}[:] = (1.39*Mission.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5 a_{5}[:]*M_5[:] = u_{5}[:] \rho_5[:] = P_{5}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{5}[:]) h_{2}[:] = C_{p_{1}*T_{2}[:] \rho_{2}[:] = P_{2}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{2}[:]) u_{2}[:] = M_2[:]*(C_{p_{1}*Mission.Aircraft.Engine.EngineConstants.R*T_{2}[:]/781)^0.5 h_{2.5}[:] = C_{p_{2}*T_{2.5}[:] \rho_{2.5}[:] = P_{2.5}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]) u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/781)^0.5 m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine} d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5 d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5 \eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]]) h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:] P_{t_4}[:] = \pi_{b}*P_{t_3}[:] M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]] M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]]) P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:] \pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013 \pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10 \pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10 \pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10 m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref}) \pi_{f}[:] >= 1 \pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10 \pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10 \pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10 \pi_{lc}[:] >= 1 m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref}) \pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10 \pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10 \pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10 m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref}) \pi_{hc}[:] >= 1 OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:] P_{t_8}[:] = P_{t_7}[:] T_{t_8}[:] = T_{t_7}[:] P_{t_6}[:] = P_{t_5}[:] T_{t_6}[:] = T_{t_5}[:] F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:] I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g) N_{f}[:]*G_{f} = N_{1}[:] N_{1}[:] <= 1.1 N_{2}[:] <= 1.1 fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD} fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD} P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5 (T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2 P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979 (T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2 M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:] m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:] m_{total}[:] = m_{fan}[:] + m_{core}[:] P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512 T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1 m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2} P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857 T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1 m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5} 1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD} 0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD} 1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD} 0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD} m_{lc_D} >= 0.7*m_{coreD}/0.649 m_{lc_D} <= 1.3*m_{coreD}/0.649 m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23 m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23 \bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405 \bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405 F[:] = F_{spec}[:] T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}} OPR[:] <= OPR_{max} VerticalTail VerticalTailNoStruct C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}} L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}} c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt})) A_{vt} = b_{vt}^2/S_{vt} b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt} p_{vt} >= 1 + 2*\lambda_{vt} 2*q_{vt} >= 1 + p_{vt} y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt} z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt} 0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt} \lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}} \Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}} \Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt} \lambda_{vt} >= 0.25 V_{vt} >= V_{vt_{min}} WingBox AR_{vt} = (2*b_{vt})^2/(2*S_{vt}) 0.423*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap} \nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56 W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5) \tau_{vt} <= 0.14 W_{struct} >= 0.5*(W_{web} + W_{cap}) Mission.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24 AR_{vt}*2*L_{vt_{max}}*Mission.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12 W_{cap} >= 8*\rho_{cap}*g*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5) Mission.Aircraft.VerticalTail.WingBox.N_{lift} = 1 Mission.Aircraft.VerticalTail.WingBox.N_{lift}*Mission.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8 \lambda_{vt} = taper W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT}) HorizontalTail HorizontalTailNoStruct \Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht} \Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}} p_{ht} >= 1 + 2*\lambda_{ht} 2*q_{ht} >= 1 + p_{ht} y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht} 0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht} \lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}} S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2 0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht}) e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1 AR_{ht} = b_{ht}^2/S_{ht} \lambda_{ht} >= 0.2 \lambda_{ht} <= 1 WingBox AR_{ht} = b_{ht}^2/S_{ht} 0.423*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap} \nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56 W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5) \tau_{ht} <= 0.14 W_{struct} >= W_{web} + W_{cap} L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2 L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht}) 2*AR_{ht}*L_{shear}*Mission.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12 W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5) Mission.Aircraft.HorizontalTail.WingBox.N_{lift} = 1 Mission.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8 L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht} L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}} W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht}) LandingGear l_n + z_{wing} + y_m*\tan(\gamma) >= l_m T = 2*y_m x_m >= x_n + B x_n >= 5 \tan(\phi) = \tan(\phi_{min}) (z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1 \tan(\psi) <= \tan(\psi_{max}) x_{up} - x_m <= l_m/\tan(\theta_{max}) y_m >= l_m S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG}) l_{oleo} = 2.5*S_{sa} d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5 l_m >= l_{oleo} + d_{t_m}/2 F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in]) W_{wa,m} = 1.2*F_{w_m}^0.609 F_{w_n} = L_{w_n}*d_{t_n}/1e+03 W_{wa,n} = 1.2*F_{w_n}^0.609 L_{w_m} = L_m/(n_{mg}*n_{wps}) L_{w_n} = L_n/n_{wps} d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315 w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48 d_{t_n} = 0.8*d_{t_m} w_{t_n} = 0.8*w_{t_m} W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m W_{mw} = n_{wps}*W_{wa,m} W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g \sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}}) W_{nw} >= n_{wps}*W_{wa,n} L_m <= 9.87*E*I_m/(K*l_m)^2 I_m = PI*r_m^3*t_m L_n <= 9.87*E*I_n/(K*l_n)^2 I_n = PI*r_n^3*t_n 2*r_m/t_m <= 40 2*r_m/t_n <= 40 h_{hold} >= 2*w_{t_m} + 2*r_m 0.8 >= 2*w_{t_n} + 2*r_n W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m})) W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n}) W_{lg} >= C_{lg}*(W_{mg} + W_{ng}) W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m x_m >= x_{CG_{lg}} c_{root} = c_0 Mission.Aircraft.Wing.WingBox.r_{w/c} = Mission.Aircraft.Fuselage.r_{w/c} x_w = x_{wing} Mission.Aircraft.Fuselage.N_{lift} = Mission.Aircraft.Wing.WingBox.N_{lift} f_{L_{total/wing}}*L_{max} >= Mission.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}} W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc} W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:] W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:] W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:] W_{total}[:] <= W_{total, max} f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}} W_{misc} >= W_{lg} + W_{hpesys} W_{hpesys} = f_{hpesys}*W_{total, max} x_n <= l_{nose} x_m >= x_{wing} \Delta x_{AC_{wing}} + x_{wing} >= x_m x_{hpesys} = 1.1*l_{nose} x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys} d_{nacelle} >= d_{f} + 2*t_{nacelle} E_{land} >= W_{total, max}/(2*g)*w_{ult}^2 x_{up} = x_{shell2} L_n = W_{total, max}*\Delta x_m/B L_m = W_{total, max}*\Delta x_n/B L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max} y_{eng} >= y_m 3*n_{vt}*Mission.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}} V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse} W_{tail} >= n_{vt}*W_{vt} + W_{ht} 2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db} B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v}) m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht} x_{CG_{ht}} <= l_{fuse} V_{ht} = S_{ht}*l_{ht}/(S*mac) L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}} L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}} x_{CG_{vt}} <= l_{fuse} V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b) n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max} n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng} D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}} I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:] I_{z}[:] <= I_{z, max} S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2 l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}} f_{S_{nacelle}} = S_{nacelle}*S^-1 A_{inlet} = 0.4*S_{nacelle} A_{fancowl} = 0.2*S_{nacelle} A_{exh} = 0.4*S_{nacelle} A_{corecowl} = 3PI*d_{LPC}^2 W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl}) W_{eadd} = f_{eadd}*W_{engine} W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon} W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine}) y_{eng} = 0.5*w_{fuse} (L_{max} - Mission.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission.Aircraft.Wing.WingBox.M_r*c_{root} A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend}) A_{1h_{MLF}} >= (Mission.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h}) I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16) I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81 I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81) x_{shell2} + l_{cone} >= x_{eng} x_{eng} >= x_{shell2} + 0.75*l_{cone} S_{floor} = 0.312*P_{floor} M_{floor} = 0.0352*P_{floor}*w_{floor} \Delta R_{fuse} = R_{fuse}*0.43/1.75 b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2 b_{ht_{out}} = 0.5*b_{ht} - w_{fuse} L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}} M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}} L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}} c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach} \pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht}) FlightSegment FlightState V[:] = V[:] a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5 V[:] = M[:]*a[:] Altitude h[:] = hft[:] Atmosphere (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:] \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:]) T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:] \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72) FlightP P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:] RC[:] = P_{excess}[:]/W_{avg}[:] \theta[:]*V[:] = RC[:] dhft[:] = tmin[:]*RC[:] R_{segment}[:] = thr[:]*V[:] WingPerformance 0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:] \Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:] \Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2 (AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2 C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:] \alpha_w[:] <= \alpha_{max,w}[:] D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:] C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:] C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR) Re_w[:] = \rho[:]*V[:]*mac/\mu[:] C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114 FuselagePerformance (no constraints) VerticalTailPerformance D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:] Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:] C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577 HorizontalTailPerformance L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:] C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:] \alpha_{ht}[:] <= \alpha_{ht,max} C_{L_{\alpha,ht_0}}[:] = 6.28 D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:] C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht}) Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:] C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852 W_{burn}[:] = W_{burn}[:] F_{fuel}[:] = F_{fuel}[:] \rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:]) P_{cabin}[:] = 7.5e+04 T_{cabin}[:] = 297 V[:] >= V_{stall}[:] W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:] tmin[:] = thr[:] L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:] L_{total}[:] = f_{L_{total/wing}}*L_w[:] L_{total}[:] >= W_{avg}[:] + L_{ht}[:] D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2 D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:]) C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S) L/D[:] = W_{avg}[:]/D[:] W_{Load}[:] <= W_{Load_{max}}[:] W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S p_{o}[:] >= L_w[:]*c_{root}/S \eta_{o}[:] = w_{fuse}/(b/2) x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:] c_{m_{w}}[:] = 1.9 x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2) x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse} x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}} x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}} C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht} AR_{ht} >= 4 C_{L_{ht}}[:] >= 0.01 SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac SM[:] >= SM_{min} SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}} x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:] R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:] C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2 V_{nacelle}[:] = r_{v_{nacelle}}*V[:] V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]] r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0) C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0 D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S \Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}} M_2[:3] = M[:3] M_{2.5}[:3] = 0.6 hold_{2}[:3] = 1.07164 hold_{2.5}[:3] = 1.06372 P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:] c1[:] = 1 + 0.201*M[:]^2.0 M_2[3:] = M[3:] M_{2.5}[3:] = 0.6 hold_{2}[3:] = 1.07164 hold_{2.5}[3:] = 1.06372 Beginning signomial solve. Using solver 'mosek' Solving for 1748 variables. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 472 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 867 Optimizer - Cones : 0 Optimizer - Scalar variables : 3449 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05 Factor - dense dim. : 0 flops : 2.91e+07 Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.240554640e+05 2.000000000e+00 1.0e+00 0.03 1 1.6e+03 2.5e+03 8.6e+04 -9.71e-01 -1.231748620e+05 2.768564203e+00 6.9e-01 0.04 2 8.3e+02 1.3e+03 4.5e+04 -9.57e-01 -1.207102576e+05 5.074539575e+00 3.6e-01 0.05 3 2.9e+02 4.6e+02 1.6e+04 -9.16e-01 -1.119695293e+05 2.152151786e+01 1.3e-01 0.06 4 2.9e+02 4.6e+02 1.6e+04 -7.71e-01 -1.100217009e+05 1.714527825e+03 1.3e-01 0.06 5 1.1e+02 1.8e+02 6.1e+03 -7.62e-01 -8.610790684e+04 6.695162483e+03 4.9e-02 0.07 6 3.8e+01 6.0e+01 2.0e+03 -4.15e-01 -4.645329796e+04 1.061030954e+04 1.7e-02 0.08 7 2.0e+01 3.2e+01 1.1e+03 2.49e-01 -2.881094530e+04 6.918992390e+03 8.9e-03 0.08 8 9.3e+00 1.5e+01 5.1e+02 5.72e-01 -1.414104026e+04 4.203941881e+03 4.1e-03 0.09 9 4.7e+00 7.4e+00 2.6e+02 8.28e-01 -7.062773964e+03 2.484854671e+03 2.1e-03 0.10 10 1.4e+00 2.2e+00 7.8e+01 9.34e-01 -2.018136909e+03 9.357817475e+02 6.3e-04 0.10 11 6.4e-01 1.0e+00 3.5e+01 9.94e-01 -6.982656505e+02 6.561046293e+02 2.9e-04 0.11 12 4.8e-01 7.6e-01 2.7e+01 9.96e-01 -4.637672981e+02 5.552260964e+02 2.2e-04 0.12 13 3.5e-01 7.8e-01 1.9e+01 9.80e-01 -2.759129050e+02 4.726371230e+02 1.6e-04 0.12 14 1.7e-01 3.9e-01 9.5e+00 9.96e-01 -5.042629419e+00 3.635650326e+02 7.9e-05 0.13 15 5.6e-02 1.6e-01 3.2e+00 9.94e-01 1.664733408e+02 2.896174723e+02 2.7e-05 0.14 16 3.2e-02 1.3e-01 1.9e+00 1.00e+00 2.020980643e+02 2.743670523e+02 1.6e-05 0.14 17 5.2e-03 1.8e-01 3.2e-01 1.00e+00 2.448158456e+02 2.572499035e+02 2.8e-06 0.15 18 1.5e-03 1.3e-01 9.5e-02 1.00e+00 2.510419816e+02 2.546930667e+02 8.5e-07 0.16 19 4.9e-04 1.1e-01 3.1e-02 1.00e+00 2.528147431e+02 2.540233778e+02 2.8e-07 0.16 20 2.1e-04 8.7e-02 1.4e-02 1.00e+00 2.533049609e+02 2.538348974e+02 1.2e-07 0.17 21 1.9e-04 7.9e-02 1.2e-02 1.00e+00 2.533443648e+02 2.538213184e+02 1.1e-07 0.18 22 1.7e-04 7.2e-02 1.1e-02 1.00e+00 2.533787262e+02 2.538079586e+02 1.0e-07 0.18 23 1.6e-04 6.6e-02 1.0e-02 1.00e+00 2.534096894e+02 2.537959814e+02 9.1e-08 0.19 24 1.4e-04 6.0e-02 9.1e-03 1.00e+00 2.534375306e+02 2.537851789e+02 8.2e-08 0.20 25 1.3e-04 5.4e-02 8.2e-03 1.00e+00 2.534625698e+02 2.537754412e+02 7.4e-08 0.20 26 1.1e-04 5.0e-02 7.3e-03 1.00e+00 2.534850882e+02 2.537666624e+02 6.6e-08 0.21 27 1.0e-04 4.6e-02 6.6e-03 1.00e+00 2.535053418e+02 2.537587504e+02 6.0e-08 0.22 28 9.2e-05 4.2e-02 5.9e-03 1.00e+00 2.535235593e+02 2.537516203e+02 5.4e-08 0.22 29 8.3e-05 3.8e-02 5.4e-03 1.00e+00 2.535399463e+02 2.537451957e+02 4.8e-08 0.23 30 7.4e-05 3.5e-02 4.8e-03 1.00e+00 2.535546874e+02 2.537394073e+02 4.4e-08 0.24 31 6.7e-05 3.2e-02 4.3e-03 1.00e+00 2.535679483e+02 2.537341927e+02 3.9e-08 0.24 32 6.0e-05 3.0e-02 3.9e-03 1.00e+00 2.535798780e+02 2.537294951e+02 3.5e-08 0.25 33 5.4e-05 2.8e-02 3.5e-03 1.00e+00 2.535906105e+02 2.537252636e+02 3.2e-08 0.26 34 4.9e-05 2.6e-02 3.2e-03 1.00e+00 2.536002661e+02 2.537214521e+02 2.9e-08 0.26 35 4.4e-05 2.4e-02 2.8e-03 1.00e+00 2.536089531e+02 2.537180190e+02 2.6e-08 0.27 36 4.0e-05 2.2e-02 2.6e-03 1.00e+00 2.536167687e+02 2.537149269e+02 2.3e-08 0.28 37 3.6e-05 2.1e-02 2.3e-03 1.00e+00 2.536238006e+02 2.537121421e+02 2.1e-08 0.29 38 3.2e-05 1.9e-02 2.1e-03 1.00e+00 2.536301274e+02 2.537096341e+02 1.9e-08 0.29 39 2.9e-05 1.8e-02 1.9e-03 1.00e+00 2.536358199e+02 2.537073754e+02 1.7e-08 0.30 40 2.6e-05 1.7e-02 1.7e-03 1.00e+00 2.536409418e+02 2.537053414e+02 1.5e-08 0.31 41 2.3e-05 1.6e-02 1.5e-03 1.00e+00 2.536455504e+02 2.537035098e+02 1.4e-08 0.31 42 2.1e-05 1.5e-02 1.4e-03 1.00e+00 2.536496972e+02 2.537018604e+02 1.2e-08 0.32 43 1.9e-05 1.5e-02 1.2e-03 1.00e+00 2.536534285e+02 2.537003753e+02 1.1e-08 0.33 44 1.7e-05 1.4e-02 1.1e-03 1.00e+00 2.536567861e+02 2.536990381e+02 1.0e-08 0.33 45 1.5e-05 1.3e-02 9.9e-04 1.00e+00 2.536598074e+02 2.536978341e+02 9.0e-09 0.34 46 1.4e-05 1.3e-02 8.9e-04 1.00e+00 2.536625261e+02 2.536967502e+02 8.1e-09 0.35 47 1.2e-05 1.2e-02 8.0e-04 1.00e+00 2.536649726e+02 2.536957743e+02 7.3e-09 0.35 48 1.1e-05 1.2e-02 7.2e-04 1.00e+00 2.536671742e+02 2.536948957e+02 6.5e-09 0.36 49 1.0e-05 1.1e-02 6.5e-04 1.00e+00 2.536691554e+02 2.536941047e+02 5.9e-09 0.37 50 9.0e-06 1.1e-02 5.9e-04 1.00e+00 2.536709383e+02 2.536933927e+02 5.3e-09 0.38 51 8.1e-06 1.1e-02 5.3e-04 1.00e+00 2.536725427e+02 2.536927517e+02 4.8e-09 0.38 52 7.3e-06 1.0e-02 4.7e-04 1.00e+00 2.536739866e+02 2.536921747e+02 4.3e-09 0.39 53 6.6e-06 1.0e-02 4.3e-04 1.00e+00 2.536752860e+02 2.536916553e+02 3.9e-09 0.40 54 5.9e-06 9.8e-03 3.8e-04 1.00e+00 2.536764553e+02 2.536911878e+02 3.5e-09 0.40 55 5.3e-06 9.6e-03 3.5e-04 1.00e+00 2.536775077e+02 2.536907669e+02 3.1e-09 0.41 56 4.8e-06 9.4e-03 3.1e-04 1.00e+00 2.536784547e+02 2.536903881e+02 2.8e-09 0.42 57 4.3e-06 9.2e-03 2.8e-04 1.00e+00 2.536793070e+02 2.536900470e+02 2.5e-09 0.42 58 3.9e-06 9.0e-03 2.5e-04 1.00e+00 2.536800740e+02 2.536897401e+02 2.3e-09 0.43 59 3.5e-06 8.9e-03 2.3e-04 1.00e+00 2.536807643e+02 2.536894637e+02 2.1e-09 0.44 60 3.2e-06 8.7e-03 2.0e-04 1.00e+00 2.536813855e+02 2.536892150e+02 1.8e-09 0.44 61 1.2e-06 3.4e-03 7.9e-05 1.00e+00 2.536848025e+02 2.536878456e+02 7.2e-10 0.45 62 1.1e-06 3.0e-03 7.1e-05 1.00e+00 2.536850202e+02 2.536877590e+02 6.5e-10 0.46 63 3.9e-07 1.1e-03 2.6e-05 1.00e+00 2.536862733e+02 2.536872564e+02 2.3e-10 0.47 64 3.6e-07 9.8e-04 2.3e-05 1.00e+00 2.536863436e+02 2.536872284e+02 2.1e-10 0.47 65 3.2e-07 8.9e-04 2.1e-05 1.00e+00 2.536864067e+02 2.536872030e+02 1.9e-10 0.48 66 2.9e-07 8.0e-04 1.9e-05 1.00e+00 2.536864635e+02 2.536871802e+02 1.7e-10 0.49 67 2.6e-07 7.2e-04 1.7e-05 1.00e+00 2.536865146e+02 2.536871596e+02 1.5e-10 0.49 68 2.3e-07 6.5e-04 1.5e-05 1.00e+00 2.536865606e+02 2.536871412e+02 1.4e-10 0.50 69 2.1e-07 5.8e-04 1.4e-05 1.00e+00 2.536866020e+02 2.536871245e+02 1.2e-10 0.51 70 1.9e-07 5.2e-04 1.2e-05 1.00e+00 2.536866393e+02 2.536871096e+02 1.1e-10 0.51 71 1.7e-07 4.7e-04 1.1e-05 1.00e+00 2.536866729e+02 2.536870961e+02 1.0e-10 0.52 72 1.5e-07 4.2e-04 9.9e-06 1.00e+00 2.536867031e+02 2.536870839e+02 9.0e-11 0.53 73 1.4e-07 3.8e-04 8.9e-06 1.00e+00 2.536867302e+02 2.536870730e+02 8.1e-11 0.53 74 1.2e-07 3.4e-04 8.1e-06 1.00e+00 2.536867547e+02 2.536870632e+02 7.3e-11 0.54 75 1.1e-07 3.1e-04 7.2e-06 1.00e+00 2.536867767e+02 2.536870544e+02 6.6e-11 0.55 76 1.0e-07 2.8e-04 6.5e-06 1.00e+00 2.536867965e+02 2.536870464e+02 5.9e-11 0.55 77 9.0e-08 2.5e-04 5.9e-06 1.00e+00 2.536868143e+02 2.536870392e+02 5.3e-11 0.56 78 8.1e-08 2.3e-04 5.3e-06 1.00e+00 2.536868303e+02 2.536870328e+02 4.8e-11 0.57 79 7.3e-08 2.0e-04 4.8e-06 1.00e+00 2.536868448e+02 2.536870270e+02 4.3e-11 0.57 80 6.6e-08 1.8e-04 4.3e-06 1.00e+00 2.536868578e+02 2.536870217e+02 3.9e-11 0.58 81 5.9e-08 1.6e-04 3.9e-06 1.00e+00 2.536868695e+02 2.536870170e+02 3.5e-11 0.59 82 5.3e-08 1.5e-04 3.5e-06 1.00e+00 2.536868800e+02 2.536870128e+02 3.1e-11 0.59 83 4.8e-08 1.3e-04 3.1e-06 1.00e+00 2.536868894e+02 2.536870090e+02 2.8e-11 0.60 84 4.3e-08 1.2e-04 2.8e-06 1.00e+00 2.536868980e+02 2.536870056e+02 2.5e-11 0.61 85 3.9e-08 1.1e-04 2.5e-06 1.00e+00 2.536869056e+02 2.536870025e+02 2.3e-11 0.61 86 3.5e-08 9.7e-05 2.3e-06 1.00e+00 2.536869125e+02 2.536869997e+02 2.1e-11 0.62 87 3.1e-08 8.7e-05 2.0e-06 1.00e+00 2.536869188e+02 2.536869972e+02 1.9e-11 0.63 88 2.8e-08 7.8e-05 1.8e-06 1.00e+00 2.536869243e+02 2.536869949e+02 1.7e-11 0.63 89 2.6e-08 7.1e-05 1.7e-06 1.00e+00 2.536869294e+02 2.536869929e+02 1.5e-11 0.64 90 2.3e-08 6.4e-05 1.5e-06 1.00e+00 2.536869339e+02 2.536869911e+02 1.3e-11 0.65 91 2.1e-08 5.7e-05 1.3e-06 1.00e+00 2.536869380e+02 2.536869894e+02 1.2e-11 0.65 92 1.9e-08 5.1e-05 1.2e-06 9.99e-01 2.536869416e+02 2.536869880e+02 1.1e-11 0.66 93 1.7e-08 4.6e-05 1.1e-06 1.00e+00 2.536869449e+02 2.536869866e+02 9.8e-12 0.67 94 1.5e-08 4.2e-05 9.8e-07 1.00e+00 2.536869479e+02 2.536869854e+02 8.9e-12 0.67 95 1.4e-08 3.8e-05 8.8e-07 1.00e+00 2.536869506e+02 2.536869843e+02 8.0e-12 0.68 96 1.2e-08 3.4e-05 7.9e-07 1.00e+00 2.536869530e+02 2.536869834e+02 7.2e-12 0.69 Optimizer terminated. Time: 0.69 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 2.5368695299e+02 nrm: 4e+01 Viol. con: 2e-07 var: 0e+00 Dual. obj: 2.5368698338e+02 nrm: 8e+02 Viol. con: 0e+00 var: 2e-04 * End solution on dual form. * Transforming to primal solution. Solving took 0.712 seconds. Using solver 'mosek' Solving for 1748 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 472 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 868 Optimizer - Cones : 0 Optimizer - Scalar variables : 3451 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05 Factor - dense dim. : 0 flops : 2.93e+07 Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237120597e+05 2.000000000e+00 1.0e+00 0.03 1 1.6e+03 2.5e+03 8.6e+04 -9.71e-01 -1.228589965e+05 2.751831010e+00 7.0e-01 0.04 2 7.9e+02 1.2e+03 4.3e+04 -9.57e-01 -1.201055617e+05 5.326974937e+00 3.5e-01 0.04 3 3.0e+02 4.7e+02 1.6e+04 -9.12e-01 -1.116972905e+05 2.210725287e+01 1.3e-01 0.05 4 2.9e+02 4.7e+02 1.6e+04 -7.71e-01 -1.098007288e+05 1.669805666e+03 1.3e-01 0.06 5 1.2e+02 2.0e+02 6.8e+03 -7.63e-01 -8.914530211e+04 6.028487627e+03 5.5e-02 0.06 6 3.9e+01 6.2e+01 2.1e+03 -4.65e-01 -4.731075280e+04 1.101859429e+04 1.7e-02 0.07 7 2.3e+01 3.6e+01 1.2e+03 2.31e-01 -3.188986622e+04 7.305151537e+03 1.0e-02 0.08 8 9.1e+00 1.4e+01 4.9e+02 5.19e-01 -1.390726678e+04 3.970193410e+03 4.0e-03 0.08 9 6.1e+00 9.6e+00 3.3e+02 8.31e-01 -9.268556419e+03 2.859448056e+03 2.7e-03 0.09 10 2.1e+00 3.3e+00 1.2e+02 9.02e-01 -3.163867678e+03 1.208066659e+03 9.4e-04 0.10 11 1.5e+00 2.4e+00 8.2e+01 9.76e-01 -2.158354396e+03 9.713866924e+02 6.7e-04 0.10 12 8.2e-01 1.4e+00 4.5e+01 9.80e-01 -1.092111068e+03 6.286525202e+02 3.7e-04 0.11 13 4.2e-01 8.1e-01 2.3e+01 9.88e-01 -4.661197429e+02 4.147126547e+02 1.9e-04 0.12 14 2.0e-01 3.9e-01 1.1e+01 1.00e+00 -1.249220987e+02 2.924420143e+02 9.0e-05 0.12 15 7.1e-02 1.6e-01 4.0e+00 1.00e+00 6.301524973e+01 2.167838530e+02 3.4e-05 0.13 16 2.8e-02 1.2e-01 1.6e+00 1.01e+00 1.288290682e+02 1.894676038e+02 1.3e-05 0.14 17 9.0e-03 1.1e-01 5.3e-01 1.01e+00 1.578773200e+02 1.781360078e+02 4.6e-06 0.14 18 3.5e-03 9.5e-02 2.1e-01 1.00e+00 1.667254586e+02 1.745981914e+02 1.8e-06 0.15 19 8.9e-04 1.2e-01 5.5e-02 9.96e-01 1.708742732e+02 1.729794156e+02 4.9e-07 0.16 20 3.2e-04 9.8e-02 2.0e-02 9.84e-01 1.718440948e+02 1.726232491e+02 1.8e-07 0.16 21 1.3e-04 9.3e-02 8.1e-03 9.96e-01 1.721840324e+02 1.724937389e+02 7.2e-08 0.17 22 4.6e-05 9.0e-02 3.0e-03 9.80e-01 1.723224558e+02 1.724367754e+02 2.7e-08 0.18 23 4.2e-05 8.8e-02 2.7e-03 9.92e-01 1.723310420e+02 1.724347821e+02 2.4e-08 0.18 24 4.1e-05 8.5e-02 2.6e-03 9.83e-01 1.723333827e+02 1.724335011e+02 2.3e-08 0.19 25 3.0e-05 8.4e-02 2.0e-03 9.27e-01 1.723515646e+02 1.724203243e+02 1.7e-08 0.20 26 1.2e-05 6.4e-02 8.3e-04 5.08e-01 1.723804253e+02 1.724123065e+02 7.6e-09 0.20 27 1.1e-05 5.8e-02 7.7e-04 8.67e-01 1.723842833e+02 1.724130215e+02 7.0e-09 0.21 28 1.0e-05 5.5e-02 7.0e-04 1.00e+00 1.723862088e+02 1.724122141e+02 6.4e-09 0.22 29 9.1e-06 5.0e-02 6.3e-04 1.00e+00 1.723880259e+02 1.724114281e+02 5.7e-09 0.22 30 8.2e-06 4.6e-02 5.7e-04 1.00e+00 1.723896607e+02 1.724107219e+02 5.2e-09 0.23 31 7.4e-06 4.2e-02 5.1e-04 1.00e+00 1.723911307e+02 1.724100853e+02 4.7e-09 0.24 32 6.7e-06 3.9e-02 4.6e-04 1.00e+00 1.723924532e+02 1.724095118e+02 4.2e-09 0.24 33 6.0e-06 3.5e-02 4.1e-04 1.00e+00 1.723936429e+02 1.724089953e+02 3.8e-09 0.25 34 5.4e-06 3.3e-02 3.7e-04 1.00e+00 1.723947132e+02 1.724085300e+02 3.4e-09 0.26 35 4.9e-06 3.0e-02 3.4e-04 1.00e+00 1.723956761e+02 1.724081109e+02 3.1e-09 0.26 36 4.4e-06 2.8e-02 3.0e-04 1.00e+00 1.723965424e+02 1.724077335e+02 2.7e-09 0.27 37 3.9e-06 2.6e-02 2.7e-04 1.00e+00 1.723973218e+02 1.724073936e+02 2.5e-09 0.28 38 3.5e-06 2.4e-02 2.4e-04 1.00e+00 1.723980230e+02 1.724070875e+02 2.2e-09 0.28 39 3.2e-06 2.2e-02 2.2e-04 1.00e+00 1.723986539e+02 1.724068118e+02 2.0e-09 0.29 40 2.9e-06 2.1e-02 2.0e-04 1.00e+00 1.723992216e+02 1.724065636e+02 1.8e-09 0.30 41 2.6e-06 2.0e-02 1.8e-04 1.00e+00 1.723997324e+02 1.724063401e+02 1.6e-09 0.30 42 2.3e-06 1.8e-02 1.6e-04 1.00e+00 1.724001920e+02 1.724061388e+02 1.5e-09 0.31 43 2.1e-06 1.7e-02 1.4e-04 1.00e+00 1.724006056e+02 1.724059576e+02 1.3e-09 0.32 44 1.9e-06 1.6e-02 1.3e-04 1.00e+00 1.724009777e+02 1.724057945e+02 1.2e-09 0.32 45 1.7e-06 1.6e-02 1.2e-04 1.00e+00 1.724013125e+02 1.724056476e+02 1.1e-09 0.33 46 1.5e-06 1.5e-02 1.1e-04 1.00e+00 1.724016138e+02 1.724055153e+02 9.6e-10 0.34 47 1.4e-06 1.4e-02 9.5e-05 1.00e+00 1.724018849e+02 1.724053962e+02 8.6e-10 0.34 48 1.2e-06 1.3e-02 8.5e-05 1.00e+00 1.724021289e+02 1.724052890e+02 7.8e-10 0.35 49 1.1e-06 1.3e-02 7.7e-05 1.00e+00 1.724023484e+02 1.724051925e+02 7.0e-10 0.36 50 1.0e-06 1.2e-02 6.9e-05 1.00e+00 1.724025459e+02 1.724051056e+02 6.3e-10 0.36 51 9.0e-07 1.2e-02 6.2e-05 1.00e+00 1.724027237e+02 1.724050274e+02 5.7e-10 0.37 52 8.1e-07 1.1e-02 5.6e-05 1.00e+00 1.724028836e+02 1.724049570e+02 5.1e-10 0.38 53 7.3e-07 1.1e-02 5.0e-05 1.00e+00 1.724030276e+02 1.724048936e+02 4.6e-10 0.38 54 6.6e-07 1.1e-02 4.5e-05 1.00e+00 1.724031571e+02 1.724048365e+02 4.1e-10 0.39 55 5.9e-07 1.0e-02 4.1e-05 1.00e+00 1.724032737e+02 1.724047851e+02 3.7e-10 0.40 56 5.3e-07 1.0e-02 3.7e-05 1.00e+00 1.724033785e+02 1.724047388e+02 3.3e-10 0.40 57 4.8e-07 9.9e-03 3.3e-05 1.00e+00 1.724034729e+02 1.724046972e+02 3.0e-10 0.41 58 4.3e-07 9.7e-03 3.0e-05 1.00e+00 1.724035579e+02 1.724046597e+02 2.7e-10 0.42 59 3.9e-07 9.5e-03 2.7e-05 1.00e+00 1.724036343e+02 1.724046259e+02 2.4e-10 0.42 60 3.5e-07 9.3e-03 2.4e-05 1.00e+00 1.724037031e+02 1.724045956e+02 2.2e-10 0.43 61 3.1e-07 9.2e-03 2.2e-05 1.00e+00 1.724037650e+02 1.724045682e+02 2.0e-10 0.44 62 2.8e-07 9.0e-03 1.9e-05 1.00e+00 1.724038206e+02 1.724045436e+02 1.8e-10 0.44 63 2.5e-07 8.9e-03 1.8e-05 1.00e+00 1.724038708e+02 1.724045214e+02 1.6e-10 0.45 64 2.3e-07 8.7e-03 1.6e-05 1.00e+00 1.724039159e+02 1.724045014e+02 1.4e-10 0.46 65 2.1e-07 8.6e-03 1.4e-05 9.99e-01 1.724039565e+02 1.724044834e+02 1.3e-10 0.46 66 1.9e-07 8.5e-03 1.3e-05 1.00e+00 1.724039930e+02 1.724044673e+02 1.2e-10 0.47 67 1.7e-07 8.4e-03 1.2e-05 1.00e+00 1.724040259e+02 1.724044527e+02 1.0e-10 0.48 68 1.5e-07 8.4e-03 1.0e-05 9.97e-01 1.724040554e+02 1.724044396e+02 9.4e-11 0.48 69 1.4e-07 8.3e-03 9.3e-06 1.00e+00 1.724040820e+02 1.724044278e+02 8.5e-11 0.49 70 1.2e-07 8.2e-03 8.4e-06 9.99e-01 1.724041060e+02 1.724044171e+02 7.7e-11 0.50 71 1.1e-07 8.1e-03 7.6e-06 9.98e-01 1.724041276e+02 1.724044076e+02 6.9e-11 0.50 72 9.9e-08 8.1e-03 6.8e-06 1.00e+00 1.724041470e+02 1.724043989e+02 6.2e-11 0.51 73 8.9e-08 8.0e-03 6.1e-06 9.99e-01 1.724041644e+02 1.724043912e+02 5.6e-11 0.52 74 8.0e-08 7.2e-03 5.5e-06 1.01e+00 1.724041806e+02 1.724043840e+02 5.0e-11 0.52 75 7.2e-08 6.5e-03 5.0e-06 1.00e+00 1.724041947e+02 1.724043777e+02 4.5e-11 0.53 76 6.5e-08 5.9e-03 4.5e-06 9.99e-01 1.724042074e+02 1.724043721e+02 4.1e-11 0.54 77 5.8e-08 5.3e-03 4.0e-06 9.93e-01 1.724042188e+02 1.724043672e+02 3.7e-11 0.54 78 5.3e-08 4.8e-03 3.6e-06 1.00e+00 1.724042291e+02 1.724043626e+02 3.3e-11 0.55 79 4.8e-08 4.3e-03 3.3e-06 9.90e-01 1.724042383e+02 1.724043586e+02 3.0e-11 0.56 80 4.3e-08 3.8e-03 2.9e-06 1.03e+00 1.724042478e+02 1.724043542e+02 2.7e-11 0.57 81 3.8e-08 3.5e-03 2.6e-06 9.79e-01 1.724042552e+02 1.724043509e+02 2.4e-11 0.57 82 3.4e-08 3.1e-03 2.4e-06 1.02e+00 1.724042624e+02 1.724043476e+02 2.2e-11 0.58 83 3.1e-08 2.8e-03 2.1e-06 1.03e+00 1.724042690e+02 1.724043446e+02 2.0e-11 0.59 84 2.8e-08 2.5e-03 1.9e-06 9.12e-01 1.724042743e+02 1.724043422e+02 1.8e-11 0.59 85 4.5e-08 2.3e-03 1.7e-06 1.19e+00 1.724042829e+02 1.724043382e+02 1.8e-11 0.60 86 3.7e-08 2.0e-03 1.6e-06 1.04e+00 1.724042873e+02 1.724043365e+02 1.7e-11 0.61 87 2.2e-08 4.8e-04 3.7e-07 1.05e+00 1.724043138e+02 1.724043253e+02 4.2e-12 0.62 88 4.1e-08 2.2e-04 1.6e-07 2.36e-01 1.724043176e+02 1.724043220e+02 1.3e-12 0.63 89 2.9e-08 1.9e-04 1.5e-07 1.99e+00 1.724043178e+02 1.724043221e+02 1.2e-12 0.64 90 2.8e-08 1.7e-04 1.3e-07 8.57e-01 1.724043184e+02 1.724043219e+02 1.0e-12 0.65 91 3.0e-08 1.5e-04 1.1e-07 1.29e+00 1.724043178e+02 1.724043232e+02 8.8e-13 0.66 Optimizer terminated. Time: 0.66 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.7240431778e+02 nrm: 4e+01 Viol. con: 9e-07 var: 0e+00 Dual. obj: 1.7240432322e+02 nrm: 8e+02 Viol. con: 0e+00 var: 1e-03 * End solution on dual form. * Transforming to primal solution. Solving took 0.687 seconds. Using solver 'mosek' Solving for 1748 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 472 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 868 Optimizer - Cones : 0 Optimizer - Scalar variables : 3451 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05 Factor - dense dim. : 0 flops : 2.93e+07 Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.238236350e+05 2.000000000e+00 1.0e+00 0.03 1 1.6e+03 2.6e+03 8.9e+04 -9.71e-01 -1.230656737e+05 2.647019465e+00 7.2e-01 0.04 2 8.5e+02 1.3e+03 4.6e+04 -9.59e-01 -1.206096807e+05 4.826231613e+00 3.7e-01 0.05 3 2.9e+02 4.6e+02 1.6e+04 -9.19e-01 -1.118497077e+05 2.029621091e+01 1.3e-01 0.06 4 2.9e+02 4.6e+02 1.6e+04 -7.73e-01 -1.097490525e+05 1.850586108e+03 1.3e-01 0.07 5 1.2e+02 2.0e+02 6.7e+03 -7.63e-01 -8.916030429e+04 6.085082524e+03 5.5e-02 0.08 6 4.4e+01 6.9e+01 2.4e+03 -4.64e-01 -5.177804334e+04 1.031145337e+04 1.9e-02 0.08 7 2.6e+01 4.1e+01 1.4e+03 1.59e-01 -3.543323189e+04 7.187062739e+03 1.1e-02 0.09 8 1.3e+01 2.0e+01 6.9e+02 4.65e-01 -1.929026185e+04 4.600188328e+03 5.6e-03 0.10 9 4.5e+00 7.1e+00 2.4e+02 7.44e-01 -6.918526178e+03 2.202933527e+03 2.0e-03 0.10 10 3.2e+00 5.1e+00 1.8e+02 9.39e-01 -4.934163409e+03 1.735951750e+03 1.5e-03 0.11 11 1.1e+00 1.7e+00 6.0e+01 9.62e-01 -1.562948083e+03 7.020582355e+02 4.9e-04 0.12 12 8.7e-01 1.4e+00 4.8e+01 9.87e-01 -1.217636151e+03 6.233488377e+02 3.9e-04 0.12 13 7.0e-01 1.2e+00 3.9e+01 9.68e-01 -9.661564015e+02 5.337666482e+02 3.2e-04 0.13 14 3.7e-01 6.1e-01 2.0e+01 9.89e-01 -3.985115606e+02 3.850483742e+02 1.7e-04 0.14 15 1.9e-01 3.2e-01 1.1e+01 9.96e-01 -1.412662595e+02 2.691767565e+02 8.8e-05 0.14 16 8.6e-02 1.7e-01 4.8e+00 1.00e+00 1.778207455e+01 2.044312768e+02 4.0e-05 0.15 17 7.8e-02 1.6e-01 4.4e+00 1.01e+00 3.927330071e+01 2.075518436e+02 3.6e-05 0.16 18 3.1e-02 9.1e-02 1.7e+00 1.01e+00 1.160421338e+02 1.824337014e+02 1.4e-05 0.16 19 1.4e-02 1.2e-01 7.7e-01 1.02e+00 1.451390072e+02 1.745459003e+02 6.4e-06 0.17 20 6.5e-03 4.2e-01 3.7e-01 1.01e+00 1.561700198e+02 1.702886893e+02 3.1e-06 0.18 21 2.1e-03 1.6e-01 1.3e-01 1.01e+00 1.635809429e+02 1.683332990e+02 1.1e-06 0.19 22 1.7e-03 1.3e-01 9.8e-02 1.01e+00 1.644225804e+02 1.681013974e+02 8.2e-07 0.19 23 6.6e-04 9.4e-02 4.0e-02 1.01e+00 1.660456798e+02 1.675261264e+02 3.4e-07 0.20 24 4.1e-04 7.6e-02 2.4e-02 1.01e+00 1.664525288e+02 1.673655646e+02 2.1e-07 0.21 25 3.7e-04 7.0e-02 2.2e-02 1.01e+00 1.665206591e+02 1.673421416e+02 1.9e-07 0.21 26 3.3e-04 6.3e-02 2.0e-02 1.01e+00 1.665794090e+02 1.673184976e+02 1.7e-07 0.22 27 3.0e-04 5.8e-02 1.8e-02 1.01e+00 1.666325754e+02 1.672975734e+02 1.5e-07 0.23 28 2.7e-04 5.3e-02 1.6e-02 1.01e+00 1.666802184e+02 1.672785665e+02 1.4e-07 0.23 29 2.4e-04 4.8e-02 1.4e-02 1.01e+00 1.667229548e+02 1.672613467e+02 1.2e-07 0.24 30 2.2e-04 4.4e-02 1.3e-02 1.01e+00 1.667612707e+02 1.672457248e+02 1.1e-07 0.25 31 1.9e-04 4.1e-02 1.2e-02 1.01e+00 1.667956243e+02 1.672315526e+02 1.0e-07 0.25 32 1.8e-04 3.7e-02 1.1e-02 1.01e+00 1.668264232e+02 1.672186933e+02 9.0e-08 0.26 33 1.6e-04 3.4e-02 9.5e-03 1.01e+00 1.668540348e+02 1.672070251e+02 8.1e-08 0.27 34 1.4e-04 3.2e-02 8.5e-03 1.00e+00 1.668787897e+02 1.671964382e+02 7.3e-08 0.28 35 1.3e-04 2.9e-02 7.7e-03 1.00e+00 1.669009849e+02 1.671868358e+02 6.6e-08 0.28 36 1.2e-04 2.7e-02 6.9e-03 1.00e+00 1.669208870e+02 1.671781271e+02 5.9e-08 0.29 37 1.0e-04 2.5e-02 6.2e-03 1.00e+00 1.669387360e+02 1.671702309e+02 5.3e-08 0.30 38 9.3e-05 2.3e-02 5.6e-03 1.00e+00 1.669547475e+02 1.671630747e+02 4.8e-08 0.30 39 8.4e-05 2.2e-02 5.0e-03 1.00e+00 1.669691132e+02 1.671565940e+02 4.3e-08 0.31 40 7.5e-05 2.0e-02 4.5e-03 1.00e+00 1.669820037e+02 1.671507256e+02 3.9e-08 0.32 41 6.8e-05 1.9e-02 4.1e-03 1.00e+00 1.669935725e+02 1.671454125e+02 3.5e-08 0.33 42 6.1e-05 1.8e-02 3.7e-03 1.00e+00 1.670039573e+02 1.671406082e+02 3.1e-08 0.34 43 5.5e-05 1.7e-02 3.3e-03 1.00e+00 1.670132789e+02 1.671362608e+02 2.8e-08 0.34 44 5.0e-05 1.6e-02 3.0e-03 1.00e+00 1.670216485e+02 1.671323292e+02 2.5e-08 0.35 45 4.5e-05 1.5e-02 2.7e-03 1.00e+00 1.670291639e+02 1.671287745e+02 2.3e-08 0.36 46 4.0e-05 1.5e-02 2.4e-03 1.00e+00 1.670359132e+02 1.671255600e+02 2.1e-08 0.36 47 3.6e-05 1.4e-02 2.2e-03 1.00e+00 1.670419753e+02 1.671226558e+02 1.9e-08 0.37 48 3.2e-05 1.3e-02 2.0e-03 1.00e+00 1.670474206e+02 1.671200297e+02 1.7e-08 0.38 49 2.9e-05 1.3e-02 1.8e-03 1.00e+00 1.670523127e+02 1.671176570e+02 1.5e-08 0.38 50 2.6e-05 1.2e-02 1.6e-03 1.00e+00 1.670567081e+02 1.671155162e+02 1.4e-08 0.39 51 2.4e-05 1.2e-02 1.4e-03 1.00e+00 1.670606568e+02 1.671135837e+02 1.2e-08 0.40 52 2.1e-05 1.2e-02 1.3e-03 1.00e+00 1.670642048e+02 1.671118395e+02 1.1e-08 0.40 53 1.9e-05 1.1e-02 1.2e-03 1.00e+00 1.670673932e+02 1.671102652e+02 9.9e-09 0.41 54 1.7e-05 1.1e-02 1.0e-03 1.00e+00 1.670702588e+02 1.671088431e+02 8.9e-09 0.42 55 1.6e-05 1.1e-02 9.4e-04 1.00e+00 1.670728345e+02 1.671075617e+02 8.0e-09 0.42 56 1.4e-05 1.1e-02 8.4e-04 1.00e+00 1.670751497e+02 1.671064039e+02 7.2e-09 0.43 57 1.3e-05 1.0e-02 7.6e-04 1.00e+00 1.670772310e+02 1.671053606e+02 6.5e-09 0.44 58 1.1e-05 1.0e-02 6.8e-04 1.00e+00 1.670791022e+02 1.671044185e+02 5.8e-09 0.44 59 1.0e-05 1.0e-02 6.1e-04 1.00e+00 1.670807846e+02 1.671035703e+02 5.2e-09 0.45 60 9.2e-06 9.8e-03 5.5e-04 1.00e+00 1.670822972e+02 1.671028046e+02 4.7e-09 0.46 61 8.3e-06 9.6e-03 5.0e-04 1.00e+00 1.670836577e+02 1.671021134e+02 4.3e-09 0.46 62 7.4e-06 9.5e-03 4.5e-04 1.00e+00 1.670848812e+02 1.671014903e+02 3.8e-09 0.47 63 6.7e-06 9.4e-03 4.0e-04 1.00e+00 1.670859815e+02 1.671009293e+02 3.4e-09 0.48 64 6.0e-06 9.3e-03 3.6e-04 1.00e+00 1.670869709e+02 1.671004242e+02 3.1e-09 0.49 65 5.4e-06 9.2e-03 3.3e-04 9.99e-01 1.670878607e+02 1.670999696e+02 2.8e-09 0.49 66 2.1e-06 3.5e-03 1.3e-04 1.00e+00 1.670927599e+02 1.670974336e+02 1.1e-09 0.50 67 8.4e-07 1.4e-03 5.1e-05 1.00e+00 1.670945910e+02 1.670964807e+02 4.3e-10 0.51 68 7.6e-07 1.3e-03 4.6e-05 9.76e-01 1.670947193e+02 1.670964216e+02 3.9e-10 0.51 69 6.8e-07 1.2e-03 4.1e-05 9.78e-01 1.670948304e+02 1.670963642e+02 3.5e-10 0.52 70 6.1e-07 1.0e-03 3.7e-05 1.01e+00 1.670949327e+02 1.670963100e+02 3.2e-10 0.53 71 5.5e-07 9.3e-04 3.3e-05 1.01e+00 1.670950269e+02 1.670962602e+02 2.9e-10 0.53 72 5.0e-07 8.4e-04 3.0e-05 9.98e-01 1.670951078e+02 1.670962181e+02 2.6e-10 0.54 73 4.5e-07 7.6e-04 2.7e-05 1.00e+00 1.670951806e+02 1.670961797e+02 2.3e-10 0.55 74 4.0e-07 6.8e-04 2.4e-05 9.62e-01 1.670952457e+02 1.670961466e+02 2.1e-10 0.55 75 3.6e-07 6.1e-04 2.2e-05 1.00e+00 1.670953048e+02 1.670961152e+02 1.9e-10 0.56 76 3.3e-07 5.5e-04 2.0e-05 9.47e-01 1.670953574e+02 1.670960887e+02 1.7e-10 0.57 77 2.9e-07 5.0e-04 1.8e-05 9.83e-01 1.670954049e+02 1.670960640e+02 1.5e-10 0.57 78 2.6e-07 4.5e-04 1.6e-05 9.72e-01 1.670954477e+02 1.670960418e+02 1.4e-10 0.58 79 2.4e-07 4.0e-04 1.4e-05 9.74e-01 1.670954862e+02 1.670960216e+02 1.2e-10 0.59 80 2.1e-07 3.6e-04 1.3e-05 1.11e+00 1.670955379e+02 1.670959913e+02 1.2e-10 0.59 81 1.9e-07 3.3e-04 1.2e-05 1.05e+00 1.670955741e+02 1.670959712e+02 1.1e-10 0.60 82 1.7e-07 2.9e-04 1.1e-05 9.00e-01 1.670955997e+02 1.670959587e+02 9.7e-11 0.61 83 1.6e-07 2.6e-04 9.5e-06 9.56e-01 1.670956230e+02 1.670959468e+02 8.8e-11 0.61 84 1.4e-07 2.4e-04 8.5e-06 1.26e+00 1.670956449e+02 1.670959326e+02 7.9e-11 0.62 85 1.3e-07 2.1e-04 7.7e-06 1.02e+00 1.670956658e+02 1.670959215e+02 7.2e-11 0.63 86 1.1e-07 1.9e-04 6.9e-06 9.32e-01 1.670956824e+02 1.670959135e+02 6.5e-11 0.63 87 1.0e-07 1.7e-04 6.2e-06 9.84e-01 1.670956975e+02 1.670959055e+02 5.8e-11 0.64 88 9.2e-08 1.6e-04 5.6e-06 8.13e-01 1.670957107e+02 1.670958999e+02 5.2e-11 0.65 89 8.3e-08 1.4e-04 5.0e-06 8.80e-01 1.670957228e+02 1.670958941e+02 4.7e-11 0.65 90 7.6e-08 1.3e-04 4.5e-06 7.53e-01 1.670957335e+02 1.670958896e+02 4.2e-11 0.66 91 6.9e-08 1.1e-04 4.1e-06 7.15e-01 1.670957432e+02 1.670958858e+02 3.8e-11 0.67 92 6.1e-08 1.0e-04 3.7e-06 1.47e+00 1.670957529e+02 1.670958781e+02 3.4e-11 0.67 93 5.5e-08 9.2e-05 3.3e-06 8.63e-01 1.670957608e+02 1.670958741e+02 3.1e-11 0.68 94 4.9e-08 8.3e-05 3.0e-06 1.22e+00 1.670957685e+02 1.670958690e+02 2.8e-11 0.69 95 4.4e-08 7.5e-05 2.7e-06 1.18e+00 1.670957803e+02 1.670958618e+02 2.7e-11 0.70 96 4.3e-08 6.7e-05 2.4e-06 1.10e+00 1.670957883e+02 1.670958574e+02 2.6e-11 0.70 97 1.3e-07 6.5e-05 2.3e-06 2.34e+01 1.670957954e+02 1.670958412e+02 1.9e-11 0.71 98 1.2e-07 5.8e-05 2.1e-06 2.38e+00 1.670958013e+02 1.670958392e+02 1.7e-11 0.72 99 1.1e-07 5.3e-05 1.9e-06 9.21e-01 1.670958045e+02 1.670958387e+02 1.5e-11 0.72 100 1.0e-07 4.7e-05 1.7e-06 1.01e+00 1.670958077e+02 1.670958382e+02 1.4e-11 0.73 101 9.1e-08 4.3e-05 1.5e-06 9.95e-01 1.670958104e+02 1.670958377e+02 1.2e-11 0.74 102 8.1e-08 3.8e-05 1.4e-06 1.62e+00 1.670958132e+02 1.670958371e+02 1.1e-11 0.75 103 7.4e-08 3.5e-05 1.2e-06 1.22e+00 1.670958154e+02 1.670958367e+02 1.0e-11 0.75 Optimizer terminated. Time: 0.75 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6709581541e+02 nrm: 2e+01 Viol. con: 1e-06 var: 0e+00 Dual. obj: 1.6709583675e+02 nrm: 9e+02 Viol. con: 0e+00 var: 1e-04 * End solution on dual form. * Transforming to primal solution. Solving took 0.779 seconds. Using solver 'mosek' Solving for 1748 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 472 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 868 Optimizer - Cones : 0 Optimizer - Scalar variables : 3451 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05 Factor - dense dim. : 0 flops : 2.93e+07 Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237491052e+05 2.000000000e+00 1.0e+00 0.03 1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230051622e+05 2.628714936e+00 7.2e-01 0.04 2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.206769287e+05 4.656932367e+00 3.8e-01 0.04 3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.117660642e+05 2.006454280e+01 1.3e-01 0.05 4 2.9e+02 4.6e+02 1.6e+04 -7.73e-01 -1.095928583e+05 1.917273339e+03 1.3e-01 0.06 5 1.2e+02 1.9e+02 6.5e+03 -7.63e-01 -8.815406305e+04 6.301964476e+03 5.3e-02 0.07 6 4.0e+01 6.3e+01 2.2e+03 -4.50e-01 -4.810694490e+04 1.098450134e+04 1.8e-02 0.07 7 2.5e+01 3.9e+01 1.3e+03 2.23e-01 -3.417995100e+04 7.471100510e+03 1.1e-02 0.08 8 1.2e+01 1.9e+01 6.5e+02 4.89e-01 -1.841437506e+04 4.250327359e+03 5.3e-03 0.09 9 3.9e+00 6.2e+00 2.1e+02 7.62e-01 -6.079617169e+03 2.004072841e+03 1.8e-03 0.09 10 2.3e+00 3.6e+00 1.2e+02 9.51e-01 -3.348709564e+03 1.369385886e+03 1.0e-03 0.10 11 9.6e-01 1.5e+00 5.3e+01 9.83e-01 -1.341473639e+03 6.716781476e+02 4.4e-04 0.11 12 7.9e-01 1.3e+00 4.4e+01 9.79e-01 -1.108501626e+03 5.799282710e+02 3.6e-04 0.11 13 7.5e-01 1.2e+00 4.1e+01 9.86e-01 -1.026923381e+03 5.623532525e+02 3.4e-04 0.12 14 2.6e-01 4.5e-01 1.5e+01 9.85e-01 -2.677966215e+02 2.992138734e+02 1.2e-04 0.13 15 1.2e-01 3.5e-01 6.6e+00 1.01e+00 -3.926603929e+01 2.146631657e+02 5.5e-05 0.13 16 1.1e-01 3.3e-01 6.0e+00 1.01e+00 -1.198752865e+01 2.196214563e+02 5.0e-05 0.14 17 8.7e-02 4.3e-01 4.9e+00 1.01e+00 1.945767868e+01 2.094440827e+02 4.2e-05 0.15 18 3.7e-02 1.9e-01 2.1e+00 1.01e+00 1.045391567e+02 1.838693347e+02 1.7e-05 0.15 19 9.9e-03 1.9e-01 5.7e-01 1.02e+00 1.505055784e+02 1.721489517e+02 4.8e-06 0.16 20 3.9e-03 1.6e-01 2.3e-01 1.01e+00 1.603048687e+02 1.688286538e+02 1.9e-06 0.17 21 1.8e-03 9.1e-02 1.1e-01 1.01e+00 1.636747889e+02 1.677018607e+02 9.1e-07 0.17 22 6.6e-04 9.6e-02 4.0e-02 1.01e+00 1.655620826e+02 1.670587271e+02 3.4e-07 0.18 23 2.5e-04 9.7e-02 1.5e-02 1.01e+00 1.662322259e+02 1.668083553e+02 1.3e-07 0.19 24 2.3e-04 8.9e-02 1.4e-02 1.01e+00 1.662772825e+02 1.667957045e+02 1.2e-07 0.20 25 2.0e-04 8.1e-02 1.3e-02 1.01e+00 1.663139499e+02 1.667803791e+02 1.1e-07 0.20 26 1.8e-04 7.4e-02 1.1e-02 1.01e+00 1.663470167e+02 1.667666725e+02 9.7e-08 0.21 27 1.7e-04 6.7e-02 1.0e-02 1.01e+00 1.663766562e+02 1.667542395e+02 8.7e-08 0.22 28 1.5e-04 6.1e-02 9.1e-03 1.01e+00 1.664032653e+02 1.667430022e+02 7.9e-08 0.22 29 1.3e-04 5.6e-02 8.2e-03 1.01e+00 1.664271496e+02 1.667328408e+02 7.1e-08 0.23 30 1.2e-04 5.1e-02 7.4e-03 1.01e+00 1.664485904e+02 1.667236538e+02 6.4e-08 0.24 31 1.1e-04 4.7e-02 6.7e-03 1.01e+00 1.664678389e+02 1.667153482e+02 5.7e-08 0.24 32 9.8e-05 4.3e-02 6.0e-03 1.01e+00 1.664851201e+02 1.667078397e+02 5.2e-08 0.25 33 8.8e-05 3.9e-02 5.4e-03 1.00e+00 1.665006361e+02 1.667010524e+02 4.7e-08 0.26 34 7.9e-05 3.6e-02 4.9e-03 1.00e+00 1.665145680e+02 1.666949173e+02 4.2e-08 0.26 35 7.1e-05 3.3e-02 4.4e-03 1.00e+00 1.665270781e+02 1.666893721e+02 3.8e-08 0.27 36 6.4e-05 3.1e-02 3.9e-03 1.00e+00 1.665383122e+02 1.666843604e+02 3.4e-08 0.28 37 5.8e-05 2.9e-02 3.5e-03 1.00e+00 1.665484010e+02 1.666798312e+02 3.1e-08 0.29 38 5.2e-05 2.6e-02 3.2e-03 1.00e+00 1.665574617e+02 1.666757384e+02 2.7e-08 0.29 39 4.7e-05 2.5e-02 2.9e-03 1.00e+00 1.665655996e+02 1.666720402e+02 2.5e-08 0.30 40 4.2e-05 2.3e-02 2.6e-03 1.00e+00 1.665729091e+02 1.666686989e+02 2.2e-08 0.31 41 3.8e-05 2.1e-02 2.3e-03 1.00e+00 1.665794749e+02 1.666656804e+02 2.0e-08 0.31 42 3.4e-05 2.0e-02 2.1e-03 1.00e+00 1.665853730e+02 1.666629538e+02 1.8e-08 0.32 43 3.1e-05 1.9e-02 1.9e-03 1.00e+00 1.665906717e+02 1.666604911e+02 1.6e-08 0.33 44 2.8e-05 1.8e-02 1.7e-03 1.00e+00 1.665954321e+02 1.666582670e+02 1.5e-08 0.33 45 2.5e-05 1.7e-02 1.5e-03 1.00e+00 1.665997093e+02 1.666562586e+02 1.3e-08 0.34 46 2.2e-05 1.6e-02 1.4e-03 1.00e+00 1.666035525e+02 1.666544453e+02 1.2e-08 0.35 47 2.0e-05 1.5e-02 1.2e-03 1.00e+00 1.666070060e+02 1.666528083e+02 1.1e-08 0.35 48 1.8e-05 1.4e-02 1.1e-03 1.00e+00 1.666101095e+02 1.666513306e+02 9.6e-09 0.36 49 1.6e-05 1.4e-02 1.0e-03 1.00e+00 1.666128986e+02 1.666499970e+02 8.6e-09 0.37 50 1.5e-05 1.3e-02 9.0e-04 1.00e+00 1.666154055e+02 1.666487934e+02 7.8e-09 0.37 51 1.3e-05 1.3e-02 8.1e-04 1.00e+00 1.666176587e+02 1.666477075e+02 7.0e-09 0.38 52 1.2e-05 1.2e-02 7.3e-04 1.00e+00 1.666196841e+02 1.666467277e+02 6.3e-09 0.39 53 1.1e-05 1.2e-02 6.6e-04 1.00e+00 1.666215048e+02 1.666458439e+02 5.7e-09 0.39 54 9.6e-06 1.2e-02 5.9e-04 1.00e+00 1.666231416e+02 1.666450466e+02 5.1e-09 0.40 55 8.7e-06 1.1e-02 5.3e-04 1.00e+00 1.666246131e+02 1.666443276e+02 4.6e-09 0.41 56 7.8e-06 1.1e-02 4.8e-04 1.00e+00 1.666259362e+02 1.666436791e+02 4.1e-09 0.41 57 7.0e-06 1.1e-02 4.3e-04 1.00e+00 1.666271257e+02 1.666430944e+02 3.7e-09 0.42 58 6.3e-06 1.0e-02 3.9e-04 1.00e+00 1.666281953e+02 1.666425671e+02 3.3e-09 0.43 59 5.7e-06 1.0e-02 3.5e-04 1.00e+00 1.666291571e+02 1.666420917e+02 3.0e-09 0.43 60 5.1e-06 1.0e-02 3.1e-04 1.00e+00 1.666300219e+02 1.666416631e+02 2.7e-09 0.44 61 4.6e-06 9.8e-03 2.8e-04 1.00e+00 1.666307995e+02 1.666412766e+02 2.4e-09 0.45 62 4.2e-06 9.7e-03 2.5e-04 1.00e+00 1.666314988e+02 1.666409282e+02 2.2e-09 0.45 63 3.7e-06 9.5e-03 2.3e-04 1.00e+00 1.666321275e+02 1.666406140e+02 2.0e-09 0.46 64 3.4e-06 9.4e-03 2.1e-04 1.00e+00 1.666326929e+02 1.666403308e+02 1.8e-09 0.47 65 3.0e-06 9.3e-03 1.9e-04 1.00e+00 1.666332012e+02 1.666400754e+02 1.6e-09 0.47 66 2.7e-06 9.2e-03 1.7e-04 1.00e+00 1.666336584e+02 1.666398451e+02 1.4e-09 0.48 67 2.5e-06 9.1e-03 1.5e-04 1.00e+00 1.666340695e+02 1.666396376e+02 1.3e-09 0.49 68 2.2e-06 9.0e-03 1.4e-04 1.00e+00 1.666344393e+02 1.666394506e+02 1.2e-09 0.49 69 2.0e-06 8.9e-03 1.2e-04 1.00e+00 1.666347718e+02 1.666392821e+02 1.1e-09 0.50 70 1.8e-06 8.9e-03 1.1e-04 1.00e+00 1.666350710e+02 1.666391302e+02 9.5e-10 0.51 71 1.6e-06 8.8e-03 9.9e-05 1.00e+00 1.666353400e+02 1.666389933e+02 8.5e-10 0.51 72 1.4e-06 8.7e-03 8.9e-05 1.00e+00 1.666355820e+02 1.666388700e+02 7.7e-10 0.52 73 1.3e-06 8.7e-03 8.0e-05 1.00e+00 1.666357997e+02 1.666387589e+02 6.9e-10 0.53 74 1.2e-06 8.6e-03 7.2e-05 1.00e+00 1.666359954e+02 1.666386588e+02 6.2e-10 0.53 75 1.1e-06 8.6e-03 6.5e-05 1.00e+00 1.666361715e+02 1.666385685e+02 5.6e-10 0.54 76 9.5e-07 8.5e-03 5.8e-05 1.00e+00 1.666363299e+02 1.666384872e+02 5.0e-10 0.55 77 8.5e-07 8.5e-03 5.2e-05 1.00e+00 1.666364723e+02 1.666384139e+02 4.5e-10 0.55 78 7.7e-07 8.4e-03 4.7e-05 1.00e+00 1.666366004e+02 1.666383478e+02 4.1e-10 0.56 79 6.9e-07 8.4e-03 4.3e-05 1.00e+00 1.666367156e+02 1.666382883e+02 3.7e-10 0.57 80 6.2e-07 8.4e-03 3.8e-05 1.00e+00 1.666368191e+02 1.666382346e+02 3.3e-10 0.57 81 5.6e-07 8.3e-03 3.4e-05 1.00e+00 1.666369123e+02 1.666381862e+02 3.0e-10 0.58 82 5.0e-07 8.3e-03 3.1e-05 1.00e+00 1.666369960e+02 1.666381425e+02 2.7e-10 0.59 83 4.5e-07 8.3e-03 2.8e-05 1.00e+00 1.666370713e+02 1.666381032e+02 2.4e-10 0.59 84 4.1e-07 8.2e-03 2.5e-05 1.00e+00 1.666371390e+02 1.666380677e+02 2.2e-10 0.60 85 3.7e-07 8.2e-03 2.3e-05 1.00e+00 1.666371999e+02 1.666380357e+02 1.9e-10 0.61 86 3.3e-07 8.2e-03 2.0e-05 1.00e+00 1.666372547e+02 1.666380069e+02 1.8e-10 0.62 87 3.0e-07 8.2e-03 1.8e-05 1.00e+00 1.666373039e+02 1.666379810e+02 1.6e-10 0.62 88 2.7e-07 8.1e-03 1.6e-05 1.00e+00 1.666373482e+02 1.666379576e+02 1.4e-10 0.63 89 2.4e-07 8.1e-03 1.5e-05 1.00e+00 1.666373881e+02 1.666379365e+02 1.3e-10 0.64 90 2.2e-07 8.1e-03 1.3e-05 1.00e+00 1.666374239e+02 1.666379175e+02 1.2e-10 0.64 91 2.0e-07 8.1e-03 1.2e-05 1.00e+00 1.666374562e+02 1.666379004e+02 1.0e-10 0.65 92 1.8e-07 8.0e-03 1.1e-05 9.99e-01 1.666374852e+02 1.666378850e+02 9.3e-11 0.66 93 1.6e-07 8.0e-03 9.7e-06 1.00e+00 1.666375113e+02 1.666378711e+02 8.4e-11 0.66 94 1.4e-07 8.0e-03 8.8e-06 1.00e+00 1.666375348e+02 1.666378586e+02 7.6e-11 0.67 95 1.3e-07 8.0e-03 7.9e-06 1.00e+00 1.666375559e+02 1.666378474e+02 6.8e-11 0.68 96 1.2e-07 8.0e-03 7.1e-06 1.00e+00 1.666375750e+02 1.666378372e+02 6.1e-11 0.68 97 1.0e-07 8.0e-03 6.4e-06 1.00e+00 1.666375921e+02 1.666378281e+02 5.5e-11 0.69 98 9.4e-08 7.9e-03 5.7e-06 1.00e+00 1.666376075e+02 1.666378199e+02 5.0e-11 0.70 99 8.4e-08 7.9e-03 5.2e-06 1.00e+00 1.666376213e+02 1.666378126e+02 4.5e-11 0.70 100 7.6e-08 7.9e-03 4.7e-06 1.00e+00 1.666376338e+02 1.666378059e+02 4.0e-11 0.71 101 6.8e-08 7.9e-03 4.2e-06 1.00e+00 1.666376450e+02 1.666377999e+02 3.6e-11 0.72 102 6.1e-08 7.9e-03 3.8e-06 9.99e-01 1.666376551e+02 1.666377945e+02 3.3e-11 0.72 103 5.5e-08 7.8e-03 3.4e-06 1.00e+00 1.666376642e+02 1.666377897e+02 2.9e-11 0.73 104 5.0e-08 7.8e-03 3.1e-06 9.99e-01 1.666376724e+02 1.666377853e+02 2.6e-11 0.74 105 4.5e-08 7.8e-03 2.7e-06 9.99e-01 1.666376798e+02 1.666377814e+02 2.4e-11 0.74 106 4.0e-08 7.8e-03 2.5e-06 1.00e+00 1.666376864e+02 1.666377779e+02 2.1e-11 0.75 107 3.6e-08 7.0e-03 2.2e-06 1.00e+00 1.666376924e+02 1.666377747e+02 1.9e-11 0.76 108 3.3e-08 6.3e-03 2.0e-06 1.00e+00 1.666376978e+02 1.666377718e+02 1.7e-11 0.76 109 2.9e-08 5.7e-03 1.8e-06 1.00e+00 1.666377026e+02 1.666377692e+02 1.6e-11 0.77 110 2.6e-08 5.1e-03 1.6e-06 1.00e+00 1.666377069e+02 1.666377669e+02 1.4e-11 0.78 111 2.4e-08 4.6e-03 1.5e-06 1.00e+00 1.666377109e+02 1.666377648e+02 1.3e-11 0.78 112 2.1e-08 4.1e-03 1.3e-06 9.97e-01 1.666377144e+02 1.666377629e+02 1.1e-11 0.79 113 1.9e-08 3.7e-03 1.2e-06 9.99e-01 1.666377176e+02 1.666377612e+02 1.0e-11 0.80 114 1.7e-08 3.4e-03 1.1e-06 9.99e-01 1.666377204e+02 1.666377597e+02 9.2e-12 0.80 115 1.6e-08 3.0e-03 9.6e-07 9.99e-01 1.666377230e+02 1.666377583e+02 8.3e-12 0.81 116 1.4e-08 2.7e-03 8.6e-07 1.00e+00 1.666377253e+02 1.666377571e+02 7.5e-12 0.82 117 1.3e-08 2.4e-03 7.8e-07 9.90e-01 1.666377273e+02 1.666377561e+02 6.7e-12 0.82 118 1.1e-08 2.2e-03 7.0e-07 1.00e+00 1.666377292e+02 1.666377551e+02 6.0e-12 0.83 119 1.0e-08 2.0e-03 6.3e-07 9.96e-01 1.666377309e+02 1.666377542e+02 5.4e-12 0.84 120 9.3e-09 1.8e-03 5.7e-07 1.00e+00 1.666377324e+02 1.666377534e+02 4.9e-12 0.84 121 8.3e-09 1.6e-03 5.1e-07 1.00e+00 1.666377338e+02 1.666377526e+02 4.4e-12 0.85 122 7.5e-09 1.4e-03 4.6e-07 1.01e+00 1.666377350e+02 1.666377519e+02 4.0e-12 0.86 123 6.8e-09 1.3e-03 4.1e-07 1.01e+00 1.666377362e+02 1.666377513e+02 3.6e-12 0.87 124 6.1e-09 1.2e-03 3.7e-07 1.01e+00 1.666377372e+02 1.666377507e+02 3.3e-12 0.87 125 5.5e-09 1.1e-03 3.3e-07 9.99e-01 1.666377381e+02 1.666377503e+02 2.9e-12 0.88 126 5.0e-09 9.5e-04 3.0e-07 1.01e+00 1.666377389e+02 1.666377498e+02 2.7e-12 0.89 127 4.5e-09 8.5e-04 2.7e-07 1.02e+00 1.666377397e+02 1.666377494e+02 2.4e-12 0.89 128 5.6e-08 1.1e-05 3.5e-09 7.43e-01 1.666377472e+02 1.666377474e+02 4.8e-13 0.90 Optimizer terminated. Time: 0.90 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6663774725e+02 nrm: 2e+01 Viol. con: 2e-06 var: 0e+00 Dual. obj: 1.6663774741e+02 nrm: 9e+02 Viol. con: 0e+00 var: 1e-04 * End solution on dual form. * Transforming to primal solution. Solving took 0.924 seconds. Using solver 'mosek' Solving for 1748 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 472 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 868 Optimizer - Cones : 0 Optimizer - Scalar variables : 3451 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05 Factor - dense dim. : 0 flops : 2.93e+07 Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237753739e+05 2.000000000e+00 1.0e+00 0.03 1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230370335e+05 2.621294786e+00 7.3e-01 0.04 2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.207091912e+05 4.644578295e+00 3.8e-01 0.04 3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.117445296e+05 2.001309028e+01 1.3e-01 0.05 4 2.9e+02 4.6e+02 1.6e+04 -7.72e-01 -1.095031374e+05 1.974666468e+03 1.3e-01 0.06 5 1.2e+02 1.9e+02 6.4e+03 -7.62e-01 -8.799037449e+04 6.314305350e+03 5.3e-02 0.06 6 4.2e+01 6.6e+01 2.3e+03 -4.47e-01 -4.984556168e+04 1.081696070e+04 1.8e-02 0.07 7 2.5e+01 4.0e+01 1.4e+03 1.91e-01 -3.456473041e+04 7.453847367e+03 1.1e-02 0.08 8 1.3e+01 2.0e+01 7.0e+02 4.82e-01 -1.966103600e+04 4.634640429e+03 5.7e-03 0.08 9 4.9e+00 7.7e+00 2.7e+02 7.41e-01 -7.622087862e+03 2.281743691e+03 2.2e-03 0.09 10 2.3e+00 3.7e+00 1.3e+02 9.30e-01 -3.406598713e+03 1.397641560e+03 1.0e-03 0.10 11 1.5e+00 2.3e+00 8.1e+01 9.81e-01 -2.141147845e+03 9.482776310e+02 6.7e-04 0.11 12 8.6e-01 1.4e+00 4.7e+01 9.88e-01 -1.174998359e+03 6.210539829e+02 3.9e-04 0.11 13 7.5e-01 1.2e+00 4.1e+01 9.55e-01 -1.042162751e+03 5.605880191e+02 3.4e-04 0.12 14 3.8e-01 6.2e-01 2.1e+01 9.87e-01 -4.228247028e+02 3.771747290e+02 1.7e-04 0.13 15 1.8e-01 3.1e-01 1.0e+01 9.99e-01 -1.361354275e+02 2.593484518e+02 8.5e-05 0.13 16 9.2e-02 1.8e-01 5.2e+00 1.01e+00 7.062921614e+00 2.057327727e+02 4.3e-05 0.14 17 8.9e-02 1.7e-01 5.0e+00 1.01e+00 1.638500422e+01 2.077013944e+02 4.1e-05 0.15 18 6.2e-02 1.2e-01 3.5e+00 1.01e+00 6.254439192e+01 1.952098048e+02 2.9e-05 0.15 19 3.0e-02 7.9e-02 1.7e+00 1.01e+00 1.175697610e+02 1.808611984e+02 1.4e-05 0.16 20 8.5e-03 1.8e-01 4.9e-01 1.01e+00 1.531753702e+02 1.715704380e+02 4.0e-06 0.17 21 2.5e-03 1.9e-01 1.5e-01 1.00e+00 1.623486761e+02 1.679511923e+02 1.2e-06 0.17 22 1.5e-03 1.2e-01 8.6e-02 1.00e+00 1.641427991e+02 1.674087189e+02 7.3e-07 0.18 23 5.2e-04 1.0e-01 3.1e-02 1.01e+00 1.656943758e+02 1.668625159e+02 2.6e-07 0.19 24 1.9e-04 1.0e-01 1.2e-02 1.01e+00 1.662226038e+02 1.666602047e+02 1.0e-07 0.19 25 1.7e-04 9.1e-02 1.1e-02 1.01e+00 1.662565312e+02 1.666502281e+02 9.1e-08 0.20 26 1.5e-04 8.3e-02 9.5e-03 1.01e+00 1.662843877e+02 1.666385768e+02 8.2e-08 0.21 27 1.4e-04 7.5e-02 8.5e-03 1.01e+00 1.663096002e+02 1.666282610e+02 7.3e-08 0.21 28 1.2e-04 6.8e-02 7.7e-03 1.01e+00 1.663321764e+02 1.666188810e+02 6.6e-08 0.22 29 1.1e-04 6.2e-02 6.9e-03 1.01e+00 1.663524351e+02 1.666103947e+02 5.9e-08 0.23 30 1.0e-04 5.7e-02 6.2e-03 1.01e+00 1.663706092e+02 1.666027116e+02 5.4e-08 0.23 31 9.1e-05 5.2e-02 5.6e-03 1.01e+00 1.663869151e+02 1.665957570e+02 4.8e-08 0.24 32 8.2e-05 4.8e-02 5.0e-03 1.01e+00 1.664015458e+02 1.665894624e+02 4.3e-08 0.25 33 7.4e-05 4.4e-02 4.5e-03 1.01e+00 1.664146744e+02 1.665837659e+02 3.9e-08 0.25 34 6.6e-05 4.0e-02 4.1e-03 1.01e+00 1.664264566e+02 1.665786118e+02 3.5e-08 0.26 35 6.0e-05 3.7e-02 3.7e-03 1.01e+00 1.664370315e+02 1.665739492e+02 3.2e-08 0.27 36 5.4e-05 3.4e-02 3.3e-03 1.00e+00 1.664465241e+02 1.665697322e+02 2.8e-08 0.27 37 4.8e-05 3.1e-02 3.0e-03 1.00e+00 1.664550460e+02 1.665659190e+02 2.6e-08 0.28 38 4.4e-05 2.9e-02 2.7e-03 1.00e+00 1.664626974e+02 1.665624716e+02 2.3e-08 0.29 39 3.9e-05 2.7e-02 2.4e-03 1.00e+00 1.664695680e+02 1.665593556e+02 2.1e-08 0.29 40 3.5e-05 2.5e-02 2.2e-03 1.00e+00 1.664757382e+02 1.665565397e+02 1.9e-08 0.30 41 3.2e-05 2.3e-02 1.9e-03 1.00e+00 1.664812799e+02 1.665539954e+02 1.7e-08 0.31 42 2.9e-05 2.2e-02 1.8e-03 1.00e+00 1.664862576e+02 1.665516970e+02 1.5e-08 0.31 43 2.6e-05 2.0e-02 1.6e-03 1.00e+00 1.664907293e+02 1.665496211e+02 1.4e-08 0.32 44 2.3e-05 1.9e-02 1.4e-03 1.00e+00 1.664947468e+02 1.665477465e+02 1.2e-08 0.33 45 2.1e-05 1.8e-02 1.3e-03 1.00e+00 1.664983566e+02 1.665460541e+02 1.1e-08 0.33 46 1.9e-05 1.7e-02 1.2e-03 1.00e+00 1.665016004e+02 1.665445264e+02 9.9e-09 0.34 47 1.7e-05 1.6e-02 1.0e-03 1.00e+00 1.665045157e+02 1.665431477e+02 9.0e-09 0.35 48 1.5e-05 1.5e-02 9.3e-04 1.00e+00 1.665071361e+02 1.665419038e+02 8.1e-09 0.35 49 1.4e-05 1.5e-02 8.4e-04 1.00e+00 1.665094915e+02 1.665407817e+02 7.3e-09 0.36 50 1.2e-05 1.4e-02 7.6e-04 1.00e+00 1.665116092e+02 1.665397698e+02 6.5e-09 0.37 51 1.1e-05 1.3e-02 6.8e-04 1.00e+00 1.665135132e+02 1.665388573e+02 5.9e-09 0.37 52 1.0e-05 1.3e-02 6.1e-04 1.00e+00 1.665152253e+02 1.665380346e+02 5.3e-09 0.38 53 9.0e-06 1.2e-02 5.5e-04 1.00e+00 1.665167650e+02 1.665372932e+02 4.8e-09 0.39 54 8.1e-06 1.2e-02 5.0e-04 1.00e+00 1.665181497e+02 1.665366249e+02 4.3e-09 0.39 55 7.3e-06 1.1e-02 4.5e-04 1.00e+00 1.665193951e+02 1.665360228e+02 3.9e-09 0.40 56 6.5e-06 1.1e-02 4.0e-04 1.00e+00 1.665205154e+02 1.665354802e+02 3.5e-09 0.41 57 5.9e-06 1.1e-02 3.6e-04 1.00e+00 1.665215231e+02 1.665349914e+02 3.1e-09 0.41 58 5.3e-06 1.1e-02 3.3e-04 1.00e+00 1.665224295e+02 1.665345509e+02 2.8e-09 0.42 59 4.8e-06 1.0e-02 2.9e-04 1.00e+00 1.665232448e+02 1.665341542e+02 2.5e-09 0.43 60 4.3e-06 1.0e-02 2.6e-04 1.00e+00 1.665239782e+02 1.665337967e+02 2.3e-09 0.43 61 3.9e-06 9.9e-03 2.4e-04 1.00e+00 1.665246379e+02 1.665334746e+02 2.0e-09 0.44 62 3.5e-06 9.7e-03 2.1e-04 1.00e+00 1.665252313e+02 1.665331843e+02 1.8e-09 0.45 63 3.1e-06 9.6e-03 1.9e-04 1.00e+00 1.665257650e+02 1.665329227e+02 1.7e-09 0.46 64 2.8e-06 9.4e-03 1.7e-04 1.00e+00 1.665262450e+02 1.665326870e+02 1.5e-09 0.46 65 2.5e-06 9.3e-03 1.6e-04 1.00e+00 1.665266767e+02 1.665324746e+02 1.3e-09 0.47 66 2.3e-06 9.2e-03 1.4e-04 1.00e+00 1.665270651e+02 1.665322832e+02 1.2e-09 0.48 67 2.1e-06 9.1e-03 1.3e-04 1.00e+00 1.665274145e+02 1.665321108e+02 1.1e-09 0.48 68 1.8e-06 9.0e-03 1.1e-04 1.00e+00 1.665277288e+02 1.665319555e+02 9.8e-10 0.49 69 1.7e-06 8.9e-03 1.0e-04 1.00e+00 1.665280116e+02 1.665318156e+02 8.8e-10 0.50 70 1.5e-06 8.8e-03 9.2e-05 1.00e+00 1.665282659e+02 1.665316896e+02 7.9e-10 0.50 71 1.3e-06 8.7e-03 8.3e-05 1.00e+00 1.665284948e+02 1.665315761e+02 7.2e-10 0.51 72 1.2e-06 8.7e-03 7.4e-05 1.00e+00 1.665287006e+02 1.665314738e+02 6.4e-10 0.52 73 1.1e-06 8.6e-03 6.7e-05 1.00e+00 1.665288858e+02 1.665313817e+02 5.8e-10 0.52 74 9.8e-07 8.6e-03 6.0e-05 1.00e+00 1.665290524e+02 1.665312987e+02 5.2e-10 0.53 75 8.8e-07 8.5e-03 5.4e-05 1.00e+00 1.665292022e+02 1.665312239e+02 4.7e-10 0.54 76 7.9e-07 8.5e-03 4.9e-05 1.00e+00 1.665293369e+02 1.665311565e+02 4.2e-10 0.55 77 7.2e-07 8.4e-03 4.4e-05 1.00e+00 1.665294581e+02 1.665310958e+02 3.8e-10 0.55 78 6.4e-07 8.4e-03 4.0e-05 1.00e+00 1.665295672e+02 1.665310410e+02 3.4e-10 0.56 79 5.8e-07 8.3e-03 3.6e-05 1.00e+00 1.665296652e+02 1.665309917e+02 3.1e-10 0.57 80 5.2e-07 8.3e-03 3.2e-05 1.00e+00 1.665297533e+02 1.665309472e+02 2.8e-10 0.57 81 4.7e-07 8.3e-03 2.9e-05 1.00e+00 1.665298326e+02 1.665309071e+02 2.5e-10 0.58 82 4.2e-07 8.2e-03 2.6e-05 1.00e+00 1.665299039e+02 1.665308709e+02 2.2e-10 0.59 83 3.8e-07 8.2e-03 2.3e-05 1.00e+00 1.665299680e+02 1.665308384e+02 2.0e-10 0.59 84 3.4e-07 8.2e-03 2.1e-05 1.00e+00 1.665300257e+02 1.665308090e+02 1.8e-10 0.60 85 3.1e-07 8.2e-03 1.9e-05 1.00e+00 1.665300775e+02 1.665307825e+02 1.6e-10 0.61 86 2.8e-07 8.1e-03 1.7e-05 1.00e+00 1.665301241e+02 1.665307586e+02 1.5e-10 0.61 87 2.5e-07 8.1e-03 1.5e-05 1.00e+00 1.665301661e+02 1.665307371e+02 1.3e-10 0.62 88 2.2e-07 8.1e-03 1.4e-05 1.00e+00 1.665302038e+02 1.665307178e+02 1.2e-10 0.63 89 2.0e-07 8.1e-03 1.2e-05 1.00e+00 1.665302377e+02 1.665307003e+02 1.1e-10 0.63 90 1.8e-07 8.1e-03 1.1e-05 1.00e+00 1.665302683e+02 1.665306845e+02 9.7e-11 0.64 91 1.6e-07 8.0e-03 1.0e-05 1.00e+00 1.665302958e+02 1.665306704e+02 8.7e-11 0.65 92 1.5e-07 8.0e-03 9.1e-06 1.00e+00 1.665303205e+02 1.665306576e+02 7.8e-11 0.65 93 1.3e-07 8.0e-03 8.1e-06 1.00e+00 1.665303427e+02 1.665306462e+02 7.0e-11 0.66 94 1.2e-07 8.0e-03 7.3e-06 1.00e+00 1.665303627e+02 1.665306358e+02 6.3e-11 0.67 95 1.1e-07 7.9e-03 6.6e-06 1.00e+00 1.665303807e+02 1.665306265e+02 5.7e-11 0.67 96 9.7e-08 7.9e-03 5.9e-06 1.00e+00 1.665303969e+02 1.665306182e+02 5.1e-11 0.68 97 8.7e-08 7.9e-03 5.3e-06 1.00e+00 1.665304115e+02 1.665306106e+02 4.6e-11 0.69 98 7.8e-08 7.9e-03 4.8e-06 1.00e+00 1.665304246e+02 1.665306038e+02 4.2e-11 0.69 99 7.0e-08 7.9e-03 4.3e-06 1.00e+00 1.665304364e+02 1.665305977e+02 3.7e-11 0.70 100 6.3e-08 7.9e-03 3.9e-06 1.00e+00 1.665304471e+02 1.665305922e+02 3.4e-11 0.71 101 5.7e-08 7.8e-03 3.5e-06 9.99e-01 1.665304566e+02 1.665305873e+02 3.0e-11 0.71 102 5.1e-08 7.8e-03 3.2e-06 9.99e-01 1.665304652e+02 1.665305828e+02 2.7e-11 0.72 103 1.3e-07 7.6e-03 3.1e-06 9.90e-01 1.665304639e+02 1.665305917e+02 2.6e-11 0.73 104 1.3e-07 7.3e-03 2.8e-06 1.00e+00 1.665304717e+02 1.665305876e+02 2.4e-11 0.73 105 1.2e-07 7.3e-03 2.5e-06 9.99e-01 1.665304788e+02 1.665305831e+02 2.1e-11 0.74 106 1.1e-07 7.3e-03 2.2e-06 9.97e-01 1.665304851e+02 1.665305790e+02 1.9e-11 0.75 107 9.5e-08 7.2e-03 2.0e-06 1.00e+00 1.665304909e+02 1.665305754e+02 1.7e-11 0.75 108 8.5e-08 7.2e-03 1.8e-06 1.00e+00 1.665304961e+02 1.665305721e+02 1.6e-11 0.76 109 7.7e-08 7.1e-03 1.6e-06 9.97e-01 1.665305008e+02 1.665305691e+02 1.4e-11 0.77 110 6.9e-08 7.1e-03 1.5e-06 1.00e+00 1.665305050e+02 1.665305665e+02 1.3e-11 0.78 111 6.2e-08 7.1e-03 1.3e-06 9.99e-01 1.665305087e+02 1.665305641e+02 1.1e-11 0.78 112 5.6e-08 6.4e-03 1.2e-06 1.01e+00 1.665305122e+02 1.665305619e+02 1.0e-11 0.79 113 5.0e-08 5.7e-03 1.1e-06 1.00e+00 1.665305152e+02 1.665305600e+02 9.2e-12 0.80 114 4.6e-08 5.2e-03 9.7e-07 9.95e-01 1.665305180e+02 1.665305583e+02 8.3e-12 0.80 115 4.1e-08 4.6e-03 8.7e-07 1.00e+00 1.665305204e+02 1.665305567e+02 7.5e-12 0.81 116 3.7e-08 4.2e-03 7.8e-07 9.93e-01 1.665305227e+02 1.665305553e+02 6.7e-12 0.82 117 3.3e-08 3.8e-03 7.0e-07 1.00e+00 1.665305247e+02 1.665305540e+02 6.1e-12 0.82 118 8.3e-08 3.4e-03 6.3e-07 9.34e-01 1.665305257e+02 1.665305588e+02 5.3e-12 0.83 119 4.3e-08 3.0e-03 5.7e-07 1.01e+00 1.665305272e+02 1.665305547e+02 4.7e-12 0.84 120 4.3e-08 2.7e-03 5.1e-07 9.21e-01 1.665305288e+02 1.665305507e+02 4.1e-12 0.84 121 2.7e-08 2.5e-03 4.6e-07 9.95e-01 1.665305300e+02 1.665305510e+02 3.7e-12 0.85 122 2.5e-08 2.3e-03 4.2e-07 1.01e+00 1.665305312e+02 1.665305502e+02 3.4e-12 0.86 123 2.4e-08 2.0e-03 3.7e-07 9.96e-01 1.665305324e+02 1.665305495e+02 3.0e-12 0.86 124 2.2e-08 1.8e-03 3.4e-07 9.97e-01 1.665305334e+02 1.665305488e+02 2.7e-12 0.87 125 2.0e-08 1.6e-03 3.0e-07 1.00e+00 1.665305343e+02 1.665305482e+02 2.4e-12 0.88 126 1.8e-08 1.5e-03 2.7e-07 1.00e+00 1.665305352e+02 1.665305476e+02 2.2e-12 0.88 127 2.6e-08 1.3e-03 2.4e-07 1.00e+00 1.665305363e+02 1.665305471e+02 2.0e-12 0.89 128 5.3e-08 1.2e-03 2.2e-07 9.12e-01 1.665305367e+02 1.665305467e+02 1.9e-12 0.90 129 4.1e-08 1.1e-03 2.0e-07 1.01e+00 1.665305373e+02 1.665305462e+02 1.7e-12 0.91 130 3.7e-08 1.0e-03 1.8e-07 1.00e+00 1.665305380e+02 1.665305459e+02 1.5e-12 0.91 131 3.3e-08 9.1e-04 1.6e-07 1.00e+00 1.665305385e+02 1.665305455e+02 1.4e-12 0.92 132 3.0e-08 8.2e-04 1.4e-07 9.95e-01 1.665305389e+02 1.665305453e+02 1.2e-12 0.93 133 2.7e-08 7.4e-04 1.3e-07 1.00e+00 1.665305393e+02 1.665305450e+02 1.1e-12 0.93 134 2.5e-08 6.6e-04 1.2e-07 1.00e+00 1.665305396e+02 1.665305448e+02 9.9e-13 0.94 Optimizer terminated. Time: 0.94 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6653053960e+02 nrm: 2e+01 Viol. con: 7e-07 var: 0e+00 Dual. obj: 1.6653054477e+02 nrm: 1e+03 Viol. con: 0e+00 var: 6e-03 * End solution on dual form. * Transforming to primal solution. Solving took 0.963 seconds. Using solver 'mosek' Solving for 1748 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (312) of matrix 'A'. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 472 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 868 Optimizer - Cones : 0 Optimizer - Scalar variables : 3451 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05 Factor - dense dim. : 0 flops : 2.93e+07 Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237723965e+05 2.000000000e+00 1.0e+00 0.03 1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230338911e+05 2.619367871e+00 7.3e-01 0.04 2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.207104755e+05 4.635090693e+00 3.8e-01 0.05 3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.116924132e+05 2.006515812e+01 1.3e-01 0.05 4 2.9e+02 4.6e+02 1.6e+04 -7.72e-01 -1.094707951e+05 1.962598695e+03 1.3e-01 0.06 5 1.2e+02 1.9e+02 6.4e+03 -7.62e-01 -8.788226104e+04 6.303856314e+03 5.2e-02 0.07 6 3.3e+01 5.2e+01 1.8e+03 -4.45e-01 -4.126301059e+04 1.179599132e+04 1.5e-02 0.08 7 2.0e+01 3.2e+01 1.1e+03 3.46e-01 -2.865074013e+04 7.420402322e+03 9.0e-03 0.08 8 1.0e+01 1.6e+01 5.5e+02 5.88e-01 -1.559269793e+04 4.104339917e+03 4.5e-03 0.09 9 3.8e+00 6.0e+00 2.1e+02 8.10e-01 -5.894597930e+03 1.898576709e+03 1.7e-03 0.10 10 2.1e+00 3.3e+00 1.1e+02 9.51e-01 -3.065562116e+03 1.212591869e+03 9.2e-04 0.10 11 8.8e-01 1.4e+00 4.8e+01 9.86e-01 -1.199429749e+03 6.419680197e+02 4.0e-04 0.11 12 8.4e-01 1.3e+00 4.6e+01 9.64e-01 -1.163808416e+03 6.115786890e+02 3.8e-04 0.12 13 5.3e-01 8.3e-01 2.9e+01 9.74e-01 -6.960284870e+02 4.363811472e+02 2.4e-04 0.13 14 3.5e-01 5.5e-01 1.9e+01 1.00e+00 -3.813368667e+02 3.597045054e+02 1.6e-04 0.14 15 1.4e-01 2.3e-01 7.7e+00 9.97e-01 -6.719842854e+01 2.314917281e+02 6.5e-05 0.15 16 8.5e-02 1.5e-01 4.7e+00 1.01e+00 2.005116100e+01 2.025960004e+02 4.0e-05 0.16 17 8.2e-02 1.4e-01 4.6e+00 1.02e+00 2.553737299e+01 2.015018767e+02 3.8e-05 0.17 18 5.7e-02 1.0e-01 3.2e+00 1.02e+00 7.030708921e+01 1.929667335e+02 2.7e-05 0.18 19 1.8e-02 8.3e-02 1.0e+00 1.02e+00 1.375642693e+02 1.754927782e+02 8.4e-06 0.19 20 5.4e-03 1.9e-01 3.1e-01 1.01e+00 1.579583233e+02 1.696376159e+02 2.6e-06 0.20 21 3.0e-03 2.2e-01 1.8e-01 1.01e+00 1.615621834e+02 1.681592421e+02 1.5e-06 0.21 22 1.1e-03 1.2e-01 6.4e-02 1.01e+00 1.647466837e+02 1.671515795e+02 5.4e-07 0.22 23 3.3e-04 1.2e-01 2.0e-02 1.01e+00 1.659527749e+02 1.666952723e+02 1.7e-07 0.23 24 1.5e-04 9.6e-02 9.0e-03 1.01e+00 1.662411411e+02 1.665782592e+02 7.8e-08 0.24 25 1.3e-04 8.8e-02 8.1e-03 1.01e+00 1.662670615e+02 1.665704340e+02 7.0e-08 0.25 26 1.2e-04 8.0e-02 7.3e-03 1.01e+00 1.662882724e+02 1.665611881e+02 6.3e-08 0.26 27 1.1e-04 7.2e-02 6.6e-03 1.01e+00 1.663074622e+02 1.665530014e+02 5.7e-08 0.27 28 9.6e-05 6.6e-02 5.9e-03 1.01e+00 1.663246400e+02 1.665455534e+02 5.1e-08 0.28 29 8.7e-05 6.0e-02 5.3e-03 1.01e+00 1.663400561e+02 1.665388193e+02 4.6e-08 0.29 30 7.8e-05 5.5e-02 4.8e-03 1.01e+00 1.663538858e+02 1.665327239e+02 4.2e-08 0.29 31 7.0e-05 5.0e-02 4.3e-03 1.01e+00 1.663662942e+02 1.665272085e+02 3.7e-08 0.30 32 6.3e-05 4.6e-02 3.9e-03 1.01e+00 1.663774282e+02 1.665222182e+02 3.4e-08 0.31 33 5.7e-05 4.2e-02 3.5e-03 1.01e+00 1.663874199e+02 1.665177040e+02 3.0e-08 0.32 34 5.1e-05 3.9e-02 3.2e-03 1.01e+00 1.663963874e+02 1.665136211e+02 2.7e-08 0.32 35 4.6e-05 3.6e-02 2.8e-03 1.01e+00 1.664044369e+02 1.665099292e+02 2.5e-08 0.33 36 4.1e-05 3.3e-02 2.6e-03 1.00e+00 1.664116630e+02 1.665065915e+02 2.2e-08 0.34 37 3.7e-05 3.0e-02 2.3e-03 1.00e+00 1.664181509e+02 1.665035746e+02 2.0e-08 0.35 38 3.4e-05 2.8e-02 2.1e-03 1.00e+00 1.664239766e+02 1.665008483e+02 1.8e-08 0.35 39 3.0e-05 2.6e-02 1.9e-03 1.00e+00 1.664292085e+02 1.664983851e+02 1.6e-08 0.36 40 2.7e-05 2.4e-02 1.7e-03 1.00e+00 1.664339074e+02 1.664961602e+02 1.5e-08 0.37 41 2.4e-05 2.3e-02 1.5e-03 1.00e+00 1.664381284e+02 1.664941507e+02 1.3e-08 0.38 42 2.2e-05 2.1e-02 1.4e-03 1.00e+00 1.664419202e+02 1.664923363e+02 1.2e-08 0.38 43 2.0e-05 2.0e-02 1.2e-03 1.00e+00 1.664453271e+02 1.664906982e+02 1.1e-08 0.39 44 1.8e-05 1.9e-02 1.1e-03 1.00e+00 1.664483883e+02 1.664892197e+02 9.5e-09 0.40 45 1.6e-05 1.8e-02 9.9e-04 1.00e+00 1.664511392e+02 1.664878854e+02 8.6e-09 0.41 46 1.4e-05 1.7e-02 8.9e-04 1.00e+00 1.664536115e+02 1.664866815e+02 7.7e-09 0.41 47 1.3e-05 1.6e-02 8.0e-04 1.00e+00 1.664558338e+02 1.664855955e+02 7.0e-09 0.42 48 1.2e-05 1.5e-02 7.2e-04 1.00e+00 1.664578313e+02 1.664846159e+02 6.3e-09 0.43 49 1.1e-05 1.4e-02 6.5e-04 1.00e+00 1.664596272e+02 1.664837325e+02 5.6e-09 0.44 50 9.5e-06 1.4e-02 5.9e-04 1.00e+00 1.664612418e+02 1.664829359e+02 5.1e-09 0.45 51 8.5e-06 1.3e-02 5.3e-04 1.00e+00 1.664626936e+02 1.664822179e+02 4.6e-09 0.46 52 7.7e-06 1.3e-02 4.7e-04 1.00e+00 1.664639992e+02 1.664815706e+02 4.1e-09 0.47 53 6.9e-06 1.2e-02 4.3e-04 1.00e+00 1.664651733e+02 1.664809873e+02 3.7e-09 0.47 54 6.2e-06 1.2e-02 3.8e-04 1.00e+00 1.664662292e+02 1.664804617e+02 3.3e-09 0.48 55 5.6e-06 1.1e-02 3.5e-04 1.00e+00 1.664671790e+02 1.664799881e+02 3.0e-09 0.49 56 5.0e-06 1.1e-02 3.1e-04 1.00e+00 1.664680333e+02 1.664795614e+02 2.7e-09 0.50 57 4.5e-06 1.1e-02 2.8e-04 1.00e+00 1.664688018e+02 1.664791770e+02 2.4e-09 0.51 58 4.1e-06 1.0e-02 2.5e-04 1.00e+00 1.664694931e+02 1.664788307e+02 2.2e-09 0.52 59 3.7e-06 1.0e-02 2.3e-04 1.00e+00 1.664701149e+02 1.664785187e+02 2.0e-09 0.52 60 3.3e-06 9.9e-03 2.0e-04 1.00e+00 1.664706742e+02 1.664782377e+02 1.8e-09 0.53 61 3.0e-06 9.7e-03 1.8e-04 1.00e+00 1.664711774e+02 1.664779845e+02 1.6e-09 0.54 62 2.7e-06 9.5e-03 1.7e-04 1.00e+00 1.664716301e+02 1.664777565e+02 1.4e-09 0.55 63 2.4e-06 9.4e-03 1.5e-04 1.00e+00 1.664720374e+02 1.664775512e+02 1.3e-09 0.56 64 2.2e-06 9.2e-03 1.3e-04 1.00e+00 1.664724039e+02 1.664773663e+02 1.2e-09 0.57 65 2.0e-06 9.1e-03 1.2e-04 1.00e+00 1.664727338e+02 1.664771999e+02 1.0e-09 0.58 66 1.8e-06 9.0e-03 1.1e-04 1.00e+00 1.664730306e+02 1.664770501e+02 9.4e-10 0.58 67 1.6e-06 8.9e-03 9.8e-05 1.00e+00 1.664732977e+02 1.664769153e+02 8.5e-10 0.59 68 1.4e-06 8.8e-03 8.8e-05 1.00e+00 1.664735380e+02 1.664767939e+02 7.6e-10 0.60 69 1.3e-06 8.7e-03 7.9e-05 1.00e+00 1.664737543e+02 1.664766846e+02 6.9e-10 0.61 70 1.2e-06 8.6e-03 7.1e-05 1.00e+00 1.664739490e+02 1.664765862e+02 6.2e-10 0.62 71 1.0e-06 8.5e-03 6.4e-05 1.00e+00 1.664741241e+02 1.664764977e+02 5.6e-10 0.62 72 9.3e-07 8.4e-03 5.8e-05 1.00e+00 1.664742818e+02 1.664764180e+02 5.0e-10 0.64 73 8.4e-07 8.4e-03 5.2e-05 1.00e+00 1.664744236e+02 1.664763462e+02 4.5e-10 0.65 74 7.6e-07 8.3e-03 4.7e-05 1.00e+00 1.664745512e+02 1.664762816e+02 4.0e-10 0.65 75 6.8e-07 8.3e-03 4.2e-05 1.00e+00 1.664746661e+02 1.664762234e+02 3.6e-10 0.66 76 6.1e-07 8.2e-03 3.8e-05 1.00e+00 1.664747694e+02 1.664761710e+02 3.3e-10 0.67 77 5.5e-07 8.2e-03 3.4e-05 1.00e+00 1.664748623e+02 1.664761238e+02 3.0e-10 0.68 78 5.0e-07 8.1e-03 3.1e-05 1.00e+00 1.664749459e+02 1.664760812e+02 2.7e-10 0.68 79 4.5e-07 8.1e-03 2.8e-05 1.00e+00 1.664750211e+02 1.664760429e+02 2.4e-10 0.69 80 4.0e-07 8.0e-03 2.5e-05 1.00e+00 1.664750888e+02 1.664760084e+02 2.2e-10 0.70 81 3.6e-07 8.0e-03 2.2e-05 1.00e+00 1.664751496e+02 1.664759773e+02 1.9e-10 0.71 82 3.3e-07 8.0e-03 2.0e-05 1.00e+00 1.664752044e+02 1.664759493e+02 1.7e-10 0.72 83 2.9e-07 8.0e-03 1.8e-05 1.00e+00 1.664752536e+02 1.664759240e+02 1.6e-10 0.73 84 2.6e-07 7.9e-03 1.6e-05 1.00e+00 1.664752979e+02 1.664759013e+02 1.4e-10 0.74 85 2.4e-07 7.9e-03 1.5e-05 1.00e+00 1.664753378e+02 1.664758808e+02 1.3e-10 0.75 86 2.1e-07 7.9e-03 1.3e-05 1.00e+00 1.664753737e+02 1.664758624e+02 1.1e-10 0.76 87 1.9e-07 7.9e-03 1.2e-05 1.00e+00 1.664754059e+02 1.664758458e+02 1.0e-10 0.76 88 1.7e-07 7.8e-03 1.1e-05 1.00e+00 1.664754350e+02 1.664758309e+02 9.3e-11 0.77 89 1.6e-07 7.8e-03 9.6e-06 1.00e+00 1.664754611e+02 1.664758175e+02 8.3e-11 0.78 90 1.4e-07 7.8e-03 8.7e-06 1.00e+00 1.664754846e+02 1.664758053e+02 7.5e-11 0.79 91 1.3e-07 7.0e-03 7.8e-06 1.00e+00 1.664755058e+02 1.664757942e+02 6.8e-11 0.80 92 1.1e-07 6.3e-03 7.0e-06 1.00e+00 1.664755248e+02 1.664757844e+02 6.1e-11 0.81 93 1.0e-07 5.7e-03 6.3e-06 1.00e+00 1.664755420e+02 1.664757756e+02 5.5e-11 0.82 94 9.2e-08 5.1e-03 5.7e-06 1.00e+00 1.664755574e+02 1.664757676e+02 4.9e-11 0.82 95 8.3e-08 4.6e-03 5.1e-06 9.99e-01 1.664755713e+02 1.664757605e+02 4.4e-11 0.83 96 7.4e-08 4.1e-03 4.6e-06 1.00e+00 1.664755837e+02 1.664757541e+02 4.0e-11 0.84 97 6.7e-08 3.7e-03 4.1e-06 1.00e+00 1.664755950e+02 1.664757483e+02 3.6e-11 0.85 98 6.0e-08 3.4e-03 3.7e-06 1.00e+00 1.664756051e+02 1.664757431e+02 3.2e-11 0.86 99 5.4e-08 3.0e-03 3.4e-06 9.99e-01 1.664756142e+02 1.664757384e+02 2.9e-11 0.86 100 4.9e-08 2.7e-03 3.0e-06 1.00e+00 1.664756224e+02 1.664757342e+02 2.6e-11 0.87 101 4.4e-08 2.4e-03 2.7e-06 1.00e+00 1.664756297e+02 1.664757304e+02 2.4e-11 0.88 102 4.0e-08 2.2e-03 2.4e-06 1.00e+00 1.664756364e+02 1.664757269e+02 2.1e-11 0.89 103 3.6e-08 2.0e-03 2.2e-06 1.00e+00 1.664756424e+02 1.664757238e+02 1.9e-11 0.89 104 3.2e-08 1.8e-03 2.0e-06 1.00e+00 1.664756477e+02 1.664757210e+02 1.7e-11 0.90 105 2.9e-08 1.6e-03 1.8e-06 1.00e+00 1.664756526e+02 1.664757185e+02 1.5e-11 0.91 106 2.6e-08 1.4e-03 1.6e-06 9.97e-01 1.664756569e+02 1.664757163e+02 1.4e-11 0.92 107 2.3e-08 1.3e-03 1.4e-06 9.98e-01 1.664756608e+02 1.664757143e+02 1.3e-11 0.93 108 2.1e-08 1.2e-03 1.3e-06 9.99e-01 1.664756644e+02 1.664757125e+02 1.1e-11 0.93 109 1.9e-08 1.1e-03 1.2e-06 1.00e+00 1.664756675e+02 1.664757108e+02 1.0e-11 0.94 110 1.7e-08 9.5e-04 1.1e-06 1.00e+00 1.664756704e+02 1.664757093e+02 9.1e-12 0.95 111 1.5e-08 8.5e-04 9.5e-07 1.00e+00 1.664756730e+02 1.664757080e+02 8.2e-12 0.96 112 1.4e-08 7.7e-04 8.5e-07 9.96e-01 1.664756753e+02 1.664757068e+02 7.4e-12 0.96 113 1.2e-08 6.9e-04 7.7e-07 1.01e+00 1.664756774e+02 1.664757057e+02 6.7e-12 0.97 114 1.1e-08 6.2e-04 6.9e-07 9.97e-01 1.664756793e+02 1.664757048e+02 6.0e-12 0.98 115 1.0e-08 5.6e-04 6.2e-07 1.01e+00 1.664756810e+02 1.664757039e+02 5.4e-12 0.99 116 9.1e-09 5.0e-04 5.6e-07 1.00e+00 1.664756825e+02 1.664757031e+02 4.9e-12 0.99 117 3.7e-09 5.2e-05 5.8e-08 1.00e+00 1.664756946e+02 1.664756968e+02 5.0e-13 1.00 Optimizer terminated. Time: 1.00 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6647569465e+02 nrm: 2e+01 Viol. con: 1e-07 var: 0e+00 Dual. obj: 1.6647569678e+02 nrm: 1e+03 Viol. con: 0e+00 var: 4e-04 * End solution on dual form. * Transforming to primal solution. Solving took 1.04 seconds. Using solver 'mosek' Solving for 1748 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (312) of matrix 'A'. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 472 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 868 Optimizer - Cones : 0 Optimizer - Scalar variables : 3451 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05 Factor - dense dim. : 0 flops : 2.93e+07 Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237711052e+05 2.000000000e+00 1.0e+00 0.03 1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230327955e+05 2.618555380e+00 7.3e-01 0.04 2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.207105230e+05 4.631548915e+00 3.8e-01 0.04 3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.116593625e+05 2.009145839e+01 1.3e-01 0.05 4 2.9e+02 4.6e+02 1.6e+04 -7.71e-01 -1.094464055e+05 1.958106253e+03 1.3e-01 0.06 5 1.2e+02 1.9e+02 6.4e+03 -7.62e-01 -8.784887085e+04 6.286653597e+03 5.2e-02 0.06 6 2.8e+01 4.4e+01 1.5e+03 -4.45e-01 -3.521466166e+04 1.246995668e+04 1.2e-02 0.07 7 1.8e+01 2.8e+01 9.7e+02 4.59e-01 -2.555040771e+04 7.282601029e+03 8.0e-03 0.08 8 1.0e+01 1.6e+01 5.5e+02 6.44e-01 -1.530962368e+04 4.310256051e+03 4.5e-03 0.09 9 4.0e+00 6.3e+00 2.2e+02 8.15e-01 -6.206808585e+03 1.970157915e+03 1.8e-03 0.09 10 2.1e+00 3.3e+00 1.1e+02 9.47e-01 -3.076258621e+03 1.206432808e+03 9.2e-04 0.10 11 8.6e-01 1.4e+00 4.7e+01 9.86e-01 -1.172512749e+03 6.452584713e+02 3.9e-04 0.11 12 8.3e-01 1.3e+00 4.6e+01 9.58e-01 -1.152704090e+03 6.177874298e+02 3.8e-04 0.11 13 5.3e-01 8.4e-01 2.9e+01 9.71e-01 -6.979547615e+02 4.416984539e+02 2.4e-04 0.12 14 3.5e-01 5.6e-01 1.9e+01 1.00e+00 -3.846816526e+02 3.613124056e+02 1.6e-04 0.12 15 1.1e-01 2.1e-01 6.5e+00 9.97e-01 -3.287554343e+01 2.179223059e+02 5.4e-05 0.13 16 8.4e-02 1.5e-01 4.7e+00 1.02e+00 2.205475750e+01 2.043964349e+02 4.0e-05 0.14 17 5.0e-02 9.3e-02 2.8e+00 1.02e+00 8.341064309e+01 1.909653399e+02 2.4e-05 0.14 18 1.3e-02 1.6e-01 7.4e-01 1.02e+00 1.456020178e+02 1.736314114e+02 6.2e-06 0.15 19 4.1e-03 2.0e-01 2.4e-01 1.01e+00 1.597194211e+02 1.687954823e+02 2.0e-06 0.16 20 2.1e-03 2.3e-01 1.2e-01 1.01e+00 1.630439252e+02 1.676586776e+02 1.0e-06 0.16 21 6.3e-04 1.5e-01 3.8e-02 1.01e+00 1.654295900e+02 1.668596314e+02 3.2e-07 0.17 22 4.2e-04 1.1e-01 2.6e-02 9.98e-01 1.657668009e+02 1.667213273e+02 2.2e-07 0.18 23 2.5e-04 8.1e-02 1.5e-02 9.86e-01 1.660455576e+02 1.666106550e+02 1.3e-07 0.18 24 2.0e-04 6.9e-02 1.2e-02 9.99e-01 1.661253082e+02 1.665840040e+02 1.1e-07 0.19 25 1.8e-04 6.4e-02 1.1e-02 1.01e+00 1.661579659e+02 1.665705552e+02 9.5e-08 0.20 26 1.6e-04 5.8e-02 9.9e-03 1.01e+00 1.661869284e+02 1.665581251e+02 8.5e-08 0.21 27 1.5e-04 5.3e-02 8.9e-03 1.00e+00 1.662130795e+02 1.665471131e+02 7.7e-08 0.21 28 1.3e-04 4.8e-02 8.1e-03 1.00e+00 1.662365215e+02 1.665371132e+02 6.9e-08 0.22 29 1.2e-04 4.4e-02 7.2e-03 1.00e+00 1.662575651e+02 1.665280693e+02 6.2e-08 0.23 30 1.1e-04 4.0e-02 6.5e-03 1.00e+00 1.662764527e+02 1.665198850e+02 5.6e-08 0.23 31 9.5e-05 3.7e-02 5.9e-03 1.00e+00 1.662934068e+02 1.665124797e+02 5.0e-08 0.24 32 8.6e-05 3.4e-02 5.3e-03 1.00e+00 1.663086255e+02 1.665057792e+02 4.5e-08 0.25 33 7.7e-05 3.1e-02 4.8e-03 1.00e+00 1.663222870e+02 1.664997165e+02 4.1e-08 0.25 34 6.9e-05 2.9e-02 4.3e-03 1.00e+00 1.663345508e+02 1.664942311e+02 3.7e-08 0.26 35 6.2e-05 2.7e-02 3.9e-03 1.00e+00 1.663455607e+02 1.664892683e+02 3.3e-08 0.27 36 5.6e-05 2.5e-02 3.5e-03 1.00e+00 1.663554455e+02 1.664847790e+02 3.0e-08 0.27 37 5.1e-05 2.3e-02 3.1e-03 1.00e+00 1.663643208e+02 1.664807187e+02 2.7e-08 0.28 38 4.6e-05 2.2e-02 2.8e-03 1.00e+00 1.663722906e+02 1.664770470e+02 2.4e-08 0.29 39 4.1e-05 2.0e-02 2.5e-03 1.00e+00 1.663794477e+02 1.664737273e+02 2.2e-08 0.29 40 3.7e-05 1.9e-02 2.3e-03 1.00e+00 1.663858757e+02 1.664707266e+02 2.0e-08 0.30 41 3.3e-05 1.8e-02 2.0e-03 1.00e+00 1.663916493e+02 1.664680146e+02 1.8e-08 0.31 42 3.0e-05 1.7e-02 1.8e-03 1.00e+00 1.663968354e+02 1.664655639e+02 1.6e-08 0.31 43 2.7e-05 1.6e-02 1.7e-03 1.00e+00 1.664014943e+02 1.664633498e+02 1.4e-08 0.32 44 2.4e-05 1.5e-02 1.5e-03 1.00e+00 1.664056797e+02 1.664613496e+02 1.3e-08 0.33 45 2.2e-05 1.4e-02 1.3e-03 1.00e+00 1.664094400e+02 1.664595429e+02 1.2e-08 0.33 46 2.0e-05 1.4e-02 1.2e-03 1.00e+00 1.664128185e+02 1.664579112e+02 1.0e-08 0.34 47 1.8e-05 1.3e-02 1.1e-03 1.00e+00 1.664158542e+02 1.664564378e+02 9.4e-09 0.35 48 1.6e-05 1.3e-02 9.8e-04 1.00e+00 1.664185821e+02 1.664551074e+02 8.4e-09 0.35 49 1.4e-05 1.2e-02 8.8e-04 1.00e+00 1.664210334e+02 1.664539063e+02 7.6e-09 0.36 50 1.3e-05 1.2e-02 7.9e-04 1.00e+00 1.664232364e+02 1.664528222e+02 6.8e-09 0.37 51 1.2e-05 1.1e-02 7.2e-04 1.00e+00 1.664252163e+02 1.664518437e+02 6.1e-09 0.38 52 1.0e-05 1.1e-02 6.4e-04 1.00e+00 1.664269959e+02 1.664509607e+02 5.5e-09 0.39 53 9.4e-06 1.1e-02 5.8e-04 1.00e+00 1.664285955e+02 1.664501639e+02 5.0e-09 0.39 54 8.4e-06 1.0e-02 5.2e-04 1.00e+00 1.664300333e+02 1.664494451e+02 4.5e-09 0.40 55 7.6e-06 1.0e-02 4.7e-04 1.00e+00 1.664313259e+02 1.664487966e+02 4.0e-09 0.41 56 6.8e-06 9.9e-03 4.2e-04 1.00e+00 1.664324880e+02 1.664482118e+02 3.6e-09 0.41 57 6.2e-06 9.7e-03 3.8e-04 1.00e+00 1.664335328e+02 1.664476843e+02 3.3e-09 0.42 58 5.5e-06 9.6e-03 3.4e-04 1.00e+00 1.664344722e+02 1.664472086e+02 2.9e-09 0.43 59 5.0e-06 9.4e-03 3.1e-04 1.00e+00 1.664353168e+02 1.664467797e+02 2.6e-09 0.43 60 4.5e-06 9.3e-03 2.8e-04 1.00e+00 1.664360762e+02 1.664463929e+02 2.4e-09 0.44 61 4.0e-06 9.1e-03 2.5e-04 1.00e+00 1.664367591e+02 1.664460442e+02 2.1e-09 0.45 62 3.6e-06 9.0e-03 2.2e-04 1.00e+00 1.664373731e+02 1.664457298e+02 1.9e-09 0.45 63 3.3e-06 8.9e-03 2.0e-04 1.00e+00 1.664379253e+02 1.664454463e+02 1.7e-09 0.46 64 2.9e-06 8.8e-03 1.8e-04 1.00e+00 1.664384218e+02 1.664451908e+02 1.6e-09 0.47 65 2.6e-06 8.7e-03 1.6e-04 1.00e+00 1.664388683e+02 1.664449605e+02 1.4e-09 0.47 66 2.4e-06 8.7e-03 1.5e-04 1.00e+00 1.664392699e+02 1.664447529e+02 1.3e-09 0.48 67 2.1e-06 8.6e-03 1.3e-04 1.00e+00 1.664396311e+02 1.664445659e+02 1.1e-09 0.49 68 1.9e-06 8.5e-03 1.2e-04 1.00e+00 1.664399561e+02 1.664443974e+02 1.0e-09 0.49 69 1.7e-06 8.4e-03 1.1e-04 1.00e+00 1.664402485e+02 1.664442457e+02 9.2e-10 0.50 70 1.6e-06 8.4e-03 9.7e-05 1.00e+00 1.664405115e+02 1.664441090e+02 8.3e-10 0.51 71 1.4e-06 8.3e-03 8.7e-05 1.00e+00 1.664407481e+02 1.664439859e+02 7.5e-10 0.51 72 1.3e-06 8.3e-03 7.8e-05 1.00e+00 1.664409609e+02 1.664438750e+02 6.7e-10 0.52 73 1.1e-06 8.2e-03 7.0e-05 1.00e+00 1.664411524e+02 1.664437751e+02 6.1e-10 0.53 74 1.0e-06 8.2e-03 6.3e-05 1.00e+00 1.664413247e+02 1.664436851e+02 5.5e-10 0.54 75 9.2e-07 8.1e-03 5.7e-05 1.00e+00 1.664414797e+02 1.664436041e+02 4.9e-10 0.54 76 8.3e-07 8.1e-03 5.1e-05 1.00e+00 1.664416192e+02 1.664435311e+02 4.4e-10 0.55 77 7.5e-07 8.1e-03 4.6e-05 1.00e+00 1.664417446e+02 1.664434654e+02 4.0e-10 0.56 78 6.7e-07 8.0e-03 4.2e-05 1.00e+00 1.664418575e+02 1.664434062e+02 3.6e-10 0.56 79 6.1e-07 8.0e-03 3.7e-05 1.00e+00 1.664419590e+02 1.664433528e+02 3.2e-10 0.57 80 5.5e-07 8.0e-03 3.4e-05 1.00e+00 1.664420503e+02 1.664433048e+02 2.9e-10 0.58 81 4.9e-07 7.9e-03 3.0e-05 1.00e+00 1.664421325e+02 1.664432615e+02 2.6e-10 0.58 82 4.4e-07 7.9e-03 2.7e-05 1.00e+00 1.664422064e+02 1.664432225e+02 2.3e-10 0.59 83 4.0e-07 7.9e-03 2.5e-05 1.00e+00 1.664422728e+02 1.664431874e+02 2.1e-10 0.60 84 3.6e-07 7.9e-03 2.2e-05 1.00e+00 1.664423326e+02 1.664431558e+02 1.9e-10 0.60 85 3.2e-07 7.8e-03 2.0e-05 1.00e+00 1.664423865e+02 1.664431273e+02 1.7e-10 0.61 86 2.9e-07 7.8e-03 1.8e-05 1.00e+00 1.664424349e+02 1.664431016e+02 1.5e-10 0.62 87 2.6e-07 7.8e-03 1.6e-05 1.00e+00 1.664424785e+02 1.664430785e+02 1.4e-10 0.62 88 2.3e-07 7.8e-03 1.5e-05 1.00e+00 1.664425177e+02 1.664430577e+02 1.2e-10 0.63 89 2.1e-07 7.8e-03 1.3e-05 1.00e+00 1.664425530e+02 1.664430390e+02 1.1e-10 0.64 90 1.9e-07 7.7e-03 1.2e-05 1.00e+00 1.664425847e+02 1.664430222e+02 1.0e-10 0.64 91 1.7e-07 7.7e-03 1.1e-05 1.00e+00 1.664426133e+02 1.664430070e+02 9.1e-11 0.65 92 1.5e-07 7.7e-03 9.5e-06 1.00e+00 1.664426390e+02 1.664429934e+02 8.2e-11 0.66 93 1.4e-07 7.7e-03 8.6e-06 1.00e+00 1.664426622e+02 1.664429811e+02 7.4e-11 0.66 94 1.2e-07 7.7e-03 7.7e-06 1.00e+00 1.664426830e+02 1.664429701e+02 6.6e-11 0.67 95 1.1e-07 7.7e-03 6.9e-06 1.00e+00 1.664427018e+02 1.664429601e+02 6.0e-11 0.68 96 1.0e-07 7.7e-03 6.2e-06 1.00e+00 1.664427187e+02 1.664429512e+02 5.4e-11 0.68 97 9.1e-08 7.6e-03 5.6e-06 1.00e+00 1.664427339e+02 1.664429431e+02 4.8e-11 0.69 98 8.2e-08 7.6e-03 5.1e-06 1.00e+00 1.664427476e+02 1.664429359e+02 4.4e-11 0.70 99 7.4e-08 7.6e-03 4.6e-06 1.00e+00 1.664427599e+02 1.664429294e+02 3.9e-11 0.70 100 6.6e-08 6.9e-03 4.1e-06 1.00e+00 1.664427710e+02 1.664429234e+02 3.5e-11 0.71 101 6.0e-08 6.2e-03 3.7e-06 1.00e+00 1.664427809e+02 1.664429182e+02 3.2e-11 0.72 102 5.4e-08 5.6e-03 3.3e-06 1.00e+00 1.664427899e+02 1.664429134e+02 2.9e-11 0.72 103 4.8e-08 5.0e-03 3.0e-06 9.99e-01 1.664427980e+02 1.664429092e+02 2.6e-11 0.73 104 4.3e-08 4.5e-03 2.7e-06 1.00e+00 1.664428052e+02 1.664429053e+02 2.3e-11 0.74 105 3.9e-08 4.1e-03 2.4e-06 9.98e-01 1.664428118e+02 1.664429019e+02 2.1e-11 0.74 106 3.5e-08 3.6e-03 2.2e-06 1.00e+00 1.664428177e+02 1.664428987e+02 1.9e-11 0.75 107 3.2e-08 3.3e-03 2.0e-06 1.00e+00 1.664428230e+02 1.664428959e+02 1.7e-11 0.76 108 2.9e-08 3.0e-03 1.8e-06 1.00e+00 1.664428277e+02 1.664428934e+02 1.5e-11 0.76 109 2.6e-08 2.7e-03 1.6e-06 1.00e+00 1.664428320e+02 1.664428911e+02 1.4e-11 0.77 110 2.3e-08 2.4e-03 1.4e-06 9.97e-01 1.664428359e+02 1.664428891e+02 1.2e-11 0.78 111 2.1e-08 2.2e-03 1.3e-06 1.00e+00 1.664428394e+02 1.664428873e+02 1.1e-11 0.78 112 1.9e-08 1.9e-03 1.2e-06 9.98e-01 1.664428425e+02 1.664428857e+02 1.0e-11 0.79 113 1.7e-08 1.7e-03 1.0e-06 1.00e+00 1.664428453e+02 1.664428842e+02 9.0e-12 0.80 114 1.6e-08 1.6e-03 9.4e-07 9.77e-01 1.664428478e+02 1.664428830e+02 8.1e-12 0.80 115 1.4e-08 1.4e-03 8.4e-07 1.00e+00 1.664428501e+02 1.664428817e+02 7.3e-12 0.81 116 1.3e-08 1.3e-03 7.6e-07 9.88e-01 1.664428521e+02 1.664428807e+02 6.5e-12 0.82 117 1.2e-08 1.1e-03 6.8e-07 1.01e+00 1.664428541e+02 1.664428796e+02 5.9e-12 0.82 118 1.1e-08 1.0e-03 6.2e-07 1.00e+00 1.664428557e+02 1.664428787e+02 5.3e-12 0.83 119 9.6e-09 9.3e-04 5.5e-07 9.88e-01 1.664428572e+02 1.664428779e+02 4.8e-12 0.84 120 8.7e-09 8.3e-04 5.0e-07 9.93e-01 1.664428586e+02 1.664428772e+02 4.3e-12 0.85 121 1.9e-08 7.5e-04 4.5e-07 1.01e+00 1.664428598e+02 1.664428765e+02 3.9e-12 0.85 122 2.1e-08 6.8e-04 4.0e-07 1.01e+00 1.664428610e+02 1.664428759e+02 3.5e-12 0.86 123 1.9e-08 6.1e-04 3.6e-07 1.02e+00 1.664428620e+02 1.664428753e+02 3.2e-12 0.87 124 1.7e-08 5.5e-04 3.3e-07 1.00e+00 1.664428629e+02 1.664428748e+02 2.9e-12 0.87 125 1.5e-08 4.9e-04 2.9e-07 9.79e-01 1.664428637e+02 1.664428744e+02 2.6e-12 0.88 126 1.4e-08 4.4e-04 2.6e-07 1.02e+00 1.664428644e+02 1.664428740e+02 2.4e-12 0.89 127 1.3e-08 4.0e-04 2.4e-07 1.00e+00 1.664428650e+02 1.664428737e+02 2.1e-12 0.89 128 1.1e-08 3.6e-04 2.1e-07 1.02e+00 1.664428657e+02 1.664428734e+02 1.9e-12 0.90 129 1.1e-08 3.2e-04 1.9e-07 9.81e-01 1.664428662e+02 1.664428731e+02 1.7e-12 0.91 130 9.6e-09 2.9e-04 1.7e-07 9.92e-01 1.664428666e+02 1.664428729e+02 1.6e-12 0.91 131 8.7e-09 2.6e-04 1.6e-07 1.03e+00 1.664428671e+02 1.664428726e+02 1.4e-12 0.92 132 7.8e-09 2.4e-04 1.4e-07 9.97e-01 1.664428674e+02 1.664428724e+02 1.3e-12 0.93 133 6.9e-09 2.1e-04 1.3e-07 9.85e-01 1.664428677e+02 1.664428723e+02 1.2e-12 0.93 134 6.2e-09 1.9e-04 1.1e-07 9.94e-01 1.664428680e+02 1.664428721e+02 1.0e-12 0.94 135 5.6e-09 1.7e-04 1.0e-07 9.91e-01 1.664428683e+02 1.664428720e+02 9.3e-13 0.95 Optimizer terminated. Time: 0.95 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6644286830e+02 nrm: 2e+01 Viol. con: 2e-07 var: 0e+00 Dual. obj: 1.6644287195e+02 nrm: 1e+03 Viol. con: 0e+00 var: 1e-03 * End solution on dual form. * Transforming to primal solution. Solving took 0.972 seconds. Using solver 'mosek' Solving for 1748 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 472 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 868 Optimizer - Cones : 0 Optimizer - Scalar variables : 3451 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05 Factor - dense dim. : 0 flops : 2.93e+07 Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237706206e+05 2.000000000e+00 1.0e+00 0.03 1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230321596e+05 2.618476980e+00 7.3e-01 0.04 2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.207092172e+05 4.631299788e+00 3.8e-01 0.04 3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.116388875e+05 2.010679045e+01 1.3e-01 0.05 4 2.9e+02 4.5e+02 1.6e+04 -7.71e-01 -1.094230997e+05 1.962291865e+03 1.3e-01 0.06 5 1.2e+02 1.9e+02 6.4e+03 -7.61e-01 -8.785793218e+04 6.263182648e+03 5.2e-02 0.06 6 2.6e+01 4.1e+01 1.4e+03 -4.45e-01 -3.316835220e+04 1.269767615e+04 1.2e-02 0.07 7 1.7e+01 2.7e+01 9.2e+02 4.98e-01 -2.422632748e+04 7.083733147e+03 7.5e-03 0.08 8 1.0e+01 1.6e+01 5.4e+02 6.67e-01 -1.518713164e+04 4.349438842e+03 4.4e-03 0.08 9 4.0e+00 6.3e+00 2.2e+02 8.16e-01 -6.253806240e+03 1.985800338e+03 1.8e-03 0.09 10 2.1e+00 3.3e+00 1.1e+02 9.46e-01 -3.093879792e+03 1.203594049e+03 9.3e-04 0.10 11 8.4e-01 1.3e+00 4.6e+01 9.86e-01 -1.145500547e+03 6.338782408e+02 3.8e-04 0.10 12 8.2e-01 1.3e+00 4.5e+01 9.50e-01 -1.137960646e+03 6.093711314e+02 3.7e-04 0.11 13 5.2e-01 8.3e-01 2.9e+01 9.70e-01 -6.844600457e+02 4.368156380e+02 2.4e-04 0.12 14 3.3e-01 5.4e-01 1.9e+01 1.00e+00 -3.665602888e+02 3.537892051e+02 1.5e-04 0.12 15 1.1e-01 2.0e-01 6.3e+00 9.97e-01 -2.732814371e+01 2.163541368e+02 5.3e-05 0.13 16 8.4e-02 1.5e-01 4.7e+00 1.02e+00 2.245602987e+01 2.054082491e+02 4.0e-05 0.14 17 4.4e-02 9.1e-02 2.5e+00 1.02e+00 9.404505834e+01 1.878214886e+02 2.1e-05 0.14 18 1.5e-02 8.6e-02 8.4e-01 1.02e+00 1.425020548e+02 1.744453424e+02 7.1e-06 0.15 19 6.8e-03 7.5e-02 3.9e-01 1.01e+00 1.551720364e+02 1.698416553e+02 3.3e-06 0.16 20 1.6e-03 1.6e-01 9.8e-02 1.01e+00 1.637887523e+02 1.674579832e+02 8.2e-07 0.16 21 9.3e-04 1.1e-01 5.6e-02 9.78e-01 1.649100104e+02 1.670143929e+02 4.7e-07 0.17 22 2.9e-04 1.1e-01 1.8e-02 9.88e-01 1.659434069e+02 1.666331473e+02 1.6e-07 0.18 23 1.3e-04 9.3e-02 8.0e-03 1.01e+00 1.662132718e+02 1.665137253e+02 6.9e-08 0.18 24 1.1e-04 8.6e-02 7.2e-03 1.01e+00 1.662362811e+02 1.665066924e+02 6.2e-08 0.19 25 1.0e-04 7.8e-02 6.5e-03 1.01e+00 1.662550118e+02 1.664982554e+02 5.6e-08 0.20 26 9.1e-05 7.1e-02 5.9e-03 1.01e+00 1.662720854e+02 1.664909344e+02 5.1e-08 0.21 27 8.2e-05 6.4e-02 5.3e-03 1.01e+00 1.662873803e+02 1.664842821e+02 4.6e-08 0.21 28 7.4e-05 5.9e-02 4.7e-03 1.01e+00 1.663011123e+02 1.664782724e+02 4.1e-08 0.22 29 6.6e-05 5.3e-02 4.3e-03 1.01e+00 1.663134330e+02 1.664728330e+02 3.7e-08 0.23 30 6.0e-05 4.9e-02 3.8e-03 1.01e+00 1.663244890e+02 1.664679121e+02 3.3e-08 0.23 31 5.4e-05 4.5e-02 3.5e-03 1.01e+00 1.663344111e+02 1.664634611e+02 3.0e-08 0.24 32 4.8e-05 4.1e-02 3.1e-03 1.01e+00 1.663433169e+02 1.664594363e+02 2.7e-08 0.25 33 4.4e-05 3.8e-02 2.8e-03 1.01e+00 1.663513115e+02 1.664557980e+02 2.4e-08 0.26 34 3.9e-05 3.5e-02 2.5e-03 1.01e+00 1.663584889e+02 1.664525096e+02 2.2e-08 0.26 35 3.5e-05 3.2e-02 2.3e-03 1.01e+00 1.663649336e+02 1.664495382e+02 2.0e-08 0.27 36 3.2e-05 3.0e-02 2.0e-03 1.00e+00 1.663707209e+02 1.664468536e+02 1.8e-08 0.28 37 2.9e-05 2.7e-02 1.8e-03 1.00e+00 1.663759184e+02 1.664444285e+02 1.6e-08 0.28 38 2.6e-05 2.5e-02 1.7e-03 1.00e+00 1.663805867e+02 1.664422382e+02 1.4e-08 0.29 39 2.3e-05 2.4e-02 1.5e-03 1.00e+00 1.663847800e+02 1.664402602e+02 1.3e-08 0.30 40 2.1e-05 2.2e-02 1.3e-03 1.00e+00 1.663885470e+02 1.664384742e+02 1.2e-08 0.30 41 1.9e-05 2.1e-02 1.2e-03 1.00e+00 1.663919312e+02 1.664368618e+02 1.0e-08 0.31 42 1.7e-05 1.9e-02 1.1e-03 1.00e+00 1.663949719e+02 1.664354061e+02 9.4e-09 0.32 43 1.5e-05 1.8e-02 9.8e-04 1.00e+00 1.663977039e+02 1.664340922e+02 8.5e-09 0.32 44 1.4e-05 1.7e-02 8.8e-04 1.00e+00 1.664001590e+02 1.664329064e+02 7.6e-09 0.33 45 1.2e-05 1.6e-02 7.9e-04 1.00e+00 1.664023653e+02 1.664318363e+02 6.9e-09 0.34 46 1.1e-05 1.6e-02 7.1e-04 1.00e+00 1.664043481e+02 1.664308707e+02 6.2e-09 0.34 47 1.0e-05 1.5e-02 6.4e-04 1.00e+00 1.664061303e+02 1.664299996e+02 5.6e-09 0.35 48 9.0e-06 1.4e-02 5.8e-04 1.00e+00 1.664077322e+02 1.664292138e+02 5.0e-09 0.36 49 8.1e-06 1.4e-02 5.2e-04 1.00e+00 1.664091722e+02 1.664285050e+02 4.5e-09 0.36 50 7.3e-06 1.3e-02 4.7e-04 1.00e+00 1.664104668e+02 1.664278658e+02 4.1e-09 0.37 51 6.5e-06 1.2e-02 4.2e-04 1.00e+00 1.664116306e+02 1.664272894e+02 3.6e-09 0.38 52 5.9e-06 1.2e-02 3.8e-04 1.00e+00 1.664126770e+02 1.664267697e+02 3.3e-09 0.38 53 5.3e-06 1.2e-02 3.4e-04 1.00e+00 1.664136179e+02 1.664263011e+02 3.0e-09 0.39 54 4.8e-06 1.1e-02 3.1e-04 1.00e+00 1.664144640e+02 1.664258787e+02 2.7e-09 0.40 55 4.3e-06 1.1e-02 2.8e-04 1.00e+00 1.664152247e+02 1.664254979e+02 2.4e-09 0.40 56 3.9e-06 1.1e-02 2.5e-04 1.00e+00 1.664159088e+02 1.664251546e+02 2.2e-09 0.41 57 3.5e-06 1.0e-02 2.2e-04 1.00e+00 1.664165240e+02 1.664248452e+02 1.9e-09 0.42 58 3.1e-06 1.0e-02 2.0e-04 1.00e+00 1.664170772e+02 1.664245662e+02 1.7e-09 0.42 59 2.8e-06 1.0e-02 1.8e-04 1.00e+00 1.664175747e+02 1.664243148e+02 1.6e-09 0.43 60 2.5e-06 9.8e-03 1.6e-04 1.00e+00 1.664180222e+02 1.664240883e+02 1.4e-09 0.44 61 2.3e-06 9.7e-03 1.5e-04 1.00e+00 1.664184247e+02 1.664238842e+02 1.3e-09 0.44 62 2.1e-06 9.5e-03 1.3e-04 1.00e+00 1.664187868e+02 1.664237003e+02 1.1e-09 0.45 63 1.8e-06 9.4e-03 1.2e-04 1.00e+00 1.664191125e+02 1.664235347e+02 1.0e-09 0.46 64 1.7e-06 9.2e-03 1.1e-04 1.00e+00 1.664194056e+02 1.664233856e+02 9.3e-10 0.46 65 1.5e-06 9.1e-03 9.6e-05 1.00e+00 1.664196692e+02 1.664232513e+02 8.3e-10 0.47 66 1.3e-06 9.0e-03 8.7e-05 1.00e+00 1.664199064e+02 1.664231303e+02 7.5e-10 0.48 67 1.2e-06 8.9e-03 7.8e-05 1.00e+00 1.664201198e+02 1.664230213e+02 6.8e-10 0.48 68 1.1e-06 8.8e-03 7.0e-05 1.00e+00 1.664203118e+02 1.664229232e+02 6.1e-10 0.49 69 9.8e-07 8.7e-03 6.3e-05 1.00e+00 1.664204846e+02 1.664228348e+02 5.5e-10 0.50 70 8.8e-07 8.6e-03 5.7e-05 1.00e+00 1.664206400e+02 1.664227552e+02 4.9e-10 0.50 71 8.0e-07 8.6e-03 5.1e-05 1.00e+00 1.664207798e+02 1.664226835e+02 4.4e-10 0.51 72 7.2e-07 8.5e-03 4.6e-05 1.00e+00 1.664209056e+02 1.664226189e+02 4.0e-10 0.52 73 6.4e-07 8.4e-03 4.2e-05 1.00e+00 1.664210187e+02 1.664225608e+02 3.6e-10 0.52 74 5.8e-07 8.4e-03 3.7e-05 1.00e+00 1.664211205e+02 1.664225084e+02 3.2e-10 0.53 75 5.2e-07 8.3e-03 3.4e-05 1.00e+00 1.664212121e+02 1.664224611e+02 2.9e-10 0.54 76 4.7e-07 8.3e-03 3.0e-05 1.00e+00 1.664212945e+02 1.664224186e+02 2.6e-10 0.54 77 4.2e-07 8.2e-03 2.7e-05 1.00e+00 1.664213686e+02 1.664223803e+02 2.4e-10 0.55 78 3.8e-07 8.2e-03 2.5e-05 1.00e+00 1.664214352e+02 1.664223458e+02 2.1e-10 0.56 79 3.4e-07 8.1e-03 2.2e-05 1.00e+00 1.664214952e+02 1.664223147e+02 1.9e-10 0.56 80 3.1e-07 8.1e-03 2.0e-05 1.00e+00 1.664215491e+02 1.664222867e+02 1.7e-10 0.57 81 2.8e-07 8.1e-03 1.8e-05 1.00e+00 1.664215977e+02 1.664222615e+02 1.5e-10 0.58 82 2.5e-07 8.0e-03 1.6e-05 1.00e+00 1.664216413e+02 1.664222387e+02 1.4e-10 0.58 83 2.2e-07 8.0e-03 1.4e-05 1.00e+00 1.664216806e+02 1.664222183e+02 1.3e-10 0.59 84 2.0e-07 8.0e-03 1.3e-05 1.00e+00 1.664217160e+02 1.664221999e+02 1.1e-10 0.60 85 1.8e-07 7.9e-03 1.2e-05 1.00e+00 1.664217478e+02 1.664221833e+02 1.0e-10 0.60 86 1.6e-07 7.9e-03 1.1e-05 1.00e+00 1.664217764e+02 1.664221684e+02 9.1e-11 0.61 87 1.5e-07 7.9e-03 9.5e-06 1.00e+00 1.664218022e+02 1.664221550e+02 8.2e-11 0.62 88 1.3e-07 7.9e-03 8.6e-06 1.00e+00 1.664218254e+02 1.664221429e+02 7.4e-11 0.62 89 1.2e-07 7.8e-03 7.7e-06 1.00e+00 1.664218463e+02 1.664221320e+02 6.7e-11 0.63 90 1.1e-07 7.8e-03 6.9e-06 1.00e+00 1.664218650e+02 1.664221222e+02 6.0e-11 0.64 91 9.7e-08 7.8e-03 6.2e-06 1.00e+00 1.664218819e+02 1.664221134e+02 5.4e-11 0.64 92 8.7e-08 7.8e-03 5.6e-06 1.00e+00 1.664218971e+02 1.664221055e+02 4.9e-11 0.65 93 7.8e-08 7.8e-03 5.1e-06 1.00e+00 1.664219108e+02 1.664220983e+02 4.4e-11 0.66 94 7.1e-08 7.8e-03 4.5e-06 1.00e+00 1.664219231e+02 1.664220919e+02 3.9e-11 0.66 95 6.4e-08 7.7e-03 4.1e-06 1.00e+00 1.664219342e+02 1.664220861e+02 3.5e-11 0.67 96 5.7e-08 7.0e-03 3.7e-06 1.00e+00 1.664219443e+02 1.664220807e+02 3.2e-11 0.68 97 5.1e-08 6.3e-03 3.3e-06 1.00e+00 1.664219532e+02 1.664220760e+02 2.9e-11 0.68 98 4.6e-08 5.6e-03 3.0e-06 1.00e+00 1.664219613e+02 1.664220718e+02 2.6e-11 0.69 99 4.2e-08 5.1e-03 2.7e-06 9.99e-01 1.664219686e+02 1.664220680e+02 2.3e-11 0.70 100 3.8e-08 4.6e-03 2.4e-06 1.00e+00 1.664219751e+02 1.664220646e+02 2.1e-11 0.71 101 3.4e-08 4.1e-03 2.2e-06 9.99e-01 1.664219810e+02 1.664220616e+02 1.9e-11 0.71 102 3.0e-08 3.7e-03 2.0e-06 1.00e+00 1.664219863e+02 1.664220588e+02 1.7e-11 0.72 103 2.7e-08 3.3e-03 1.8e-06 9.97e-01 1.664219910e+02 1.664220564e+02 1.5e-11 0.73 104 2.5e-08 3.0e-03 1.6e-06 1.00e+00 1.664219953e+02 1.664220542e+02 1.4e-11 0.73 105 2.2e-08 2.7e-03 1.4e-06 9.98e-01 1.664219992e+02 1.664220521e+02 1.2e-11 0.74 106 2.0e-08 2.4e-03 1.3e-06 1.00e+00 1.664220027e+02 1.664220503e+02 1.1e-11 0.75 107 1.8e-08 2.2e-03 1.2e-06 1.00e+00 1.664220058e+02 1.664220487e+02 1.0e-11 0.75 108 1.6e-08 2.0e-03 1.0e-06 1.00e+00 1.664220086e+02 1.664220472e+02 9.0e-12 0.76 109 1.5e-08 1.8e-03 9.4e-07 9.97e-01 1.664220112e+02 1.664220459e+02 8.1e-12 0.77 110 1.3e-08 1.6e-03 8.4e-07 1.00e+00 1.664220134e+02 1.664220447e+02 7.3e-12 0.77 111 1.2e-08 1.4e-03 7.6e-07 9.96e-01 1.664220155e+02 1.664220437e+02 6.6e-12 0.78 112 1.1e-08 1.3e-03 6.8e-07 9.99e-01 1.664220173e+02 1.664220427e+02 5.9e-12 0.79 113 9.6e-09 1.2e-03 6.1e-07 9.97e-01 1.664220190e+02 1.664220418e+02 5.3e-12 0.79 114 8.6e-09 1.0e-03 5.5e-07 9.91e-01 1.664220205e+02 1.664220410e+02 4.8e-12 0.80 115 7.8e-09 9.4e-04 5.0e-07 1.01e+00 1.664220219e+02 1.664220403e+02 4.3e-12 0.81 116 7.0e-09 8.5e-04 4.5e-07 9.92e-01 1.664220231e+02 1.664220397e+02 3.9e-12 0.81 117 1.4e-08 7.6e-04 4.0e-07 1.02e+00 1.664220242e+02 1.664220394e+02 3.5e-12 0.82 118 2.0e-08 6.9e-04 3.6e-07 9.99e-01 1.664220252e+02 1.664220387e+02 3.2e-12 0.83 119 1.8e-08 6.2e-04 3.3e-07 1.01e+00 1.664220261e+02 1.664220382e+02 2.9e-12 0.83 120 3.3e-08 5.6e-04 2.9e-07 9.98e-01 1.664220268e+02 1.664220382e+02 2.6e-12 0.84 121 2.2e-08 5.0e-04 2.6e-07 9.99e-01 1.664220276e+02 1.664220373e+02 2.3e-12 0.85 122 2.0e-08 4.5e-04 2.4e-07 1.01e+00 1.664220282e+02 1.664220370e+02 2.1e-12 0.85 123 1.8e-08 4.1e-04 2.1e-07 1.00e+00 1.664220288e+02 1.664220367e+02 1.9e-12 0.86 124 1.7e-08 3.7e-04 1.9e-07 1.02e+00 1.664220294e+02 1.664220364e+02 1.7e-12 0.87 125 1.5e-08 3.3e-04 1.7e-07 1.01e+00 1.664220298e+02 1.664220361e+02 1.5e-12 0.87 126 1.3e-08 3.0e-04 1.6e-07 1.00e+00 1.664220303e+02 1.664220359e+02 1.4e-12 0.88 127 1.2e-08 2.7e-04 1.4e-07 9.96e-01 1.664220306e+02 1.664220357e+02 1.2e-12 0.89 128 1.1e-08 2.4e-04 1.3e-07 1.01e+00 1.664220310e+02 1.664220355e+02 1.1e-12 0.89 129 9.9e-09 2.2e-04 1.1e-07 1.00e+00 1.664220313e+02 1.664220354e+02 1.0e-12 0.90 130 1.0e-09 2.2e-05 1.2e-08 1.00e+00 1.664220337e+02 1.664220341e+02 1.0e-13 0.91 Optimizer terminated. Time: 0.91 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6642203368e+02 nrm: 2e+01 Viol. con: 2e-08 var: 0e+00 Dual. obj: 1.6642203410e+02 nrm: 1e+03 Viol. con: 0e+00 var: 2e-04 * End solution on dual form. * Transforming to primal solution. Solving took 0.932 seconds. Using solver 'mosek' Solving for 1748 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (312) of matrix 'A'. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 472 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 868 Optimizer - Cones : 0 Optimizer - Scalar variables : 3451 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05 Factor - dense dim. : 0 flops : 2.93e+07 Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237697757e+05 2.000000000e+00 1.0e+00 0.03 1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230310708e+05 2.618658392e+00 7.3e-01 0.04 2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.207072283e+05 4.631967602e+00 3.8e-01 0.04 3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.116239239e+05 2.011668198e+01 1.3e-01 0.05 4 2.9e+02 4.5e+02 1.6e+04 -7.71e-01 -1.094044853e+05 1.966473714e+03 1.3e-01 0.06 5 1.2e+02 1.9e+02 6.4e+03 -7.61e-01 -8.784053867e+04 6.251650733e+03 5.2e-02 0.06 6 2.6e+01 4.1e+01 1.4e+03 -4.45e-01 -3.306603809e+04 1.270142506e+04 1.2e-02 0.07 7 1.7e+01 2.7e+01 9.1e+02 4.99e-01 -2.410345416e+04 7.059532995e+03 7.5e-03 0.08 8 9.9e+00 1.6e+01 5.4e+02 6.69e-01 -1.509576583e+04 4.325329085e+03 4.4e-03 0.08 9 3.9e+00 6.2e+00 2.1e+02 8.17e-01 -6.165428475e+03 1.962599328e+03 1.8e-03 0.09 10 2.0e+00 3.2e+00 1.1e+02 9.46e-01 -3.034895445e+03 1.193153232e+03 9.1e-04 0.10 11 8.5e-01 1.3e+00 4.7e+01 9.86e-01 -1.168555856e+03 6.294711099e+02 3.9e-04 0.10 12 8.2e-01 1.3e+00 4.5e+01 9.51e-01 -1.158089507e+03 6.045830226e+02 3.8e-04 0.11 13 5.2e-01 8.3e-01 2.9e+01 9.70e-01 -6.910803073e+02 4.348560115e+02 2.4e-04 0.12 14 3.3e-01 5.3e-01 1.8e+01 1.00e+00 -3.582552166e+02 3.500458516e+02 1.5e-04 0.12 15 1.1e-01 2.0e-01 6.2e+00 9.97e-01 -2.527655392e+01 2.158431403e+02 5.2e-05 0.13 16 8.3e-02 1.5e-01 4.7e+00 1.02e+00 2.363102125e+01 2.049700552e+02 3.9e-05 0.14 17 4.1e-02 8.8e-02 2.3e+00 1.02e+00 9.799313343e+01 1.868005351e+02 1.9e-05 0.14 18 1.1e-02 1.7e-01 6.3e-01 1.02e+00 1.487956591e+02 1.727754642e+02 5.3e-06 0.15 19 3.5e-03 2.0e-01 2.1e-01 1.01e+00 1.605532700e+02 1.683301713e+02 1.7e-06 0.16 20 1.3e-03 1.4e-01 8.0e-02 1.01e+00 1.642277735e+02 1.672301862e+02 6.8e-07 0.16 21 8.8e-04 1.0e-01 5.3e-02 9.84e-01 1.649840636e+02 1.669558345e+02 4.5e-07 0.17 22 2.6e-04 1.1e-01 1.7e-02 9.86e-01 1.659721215e+02 1.665916548e+02 1.4e-07 0.18 23 9.3e-05 1.1e-01 6.0e-03 1.01e+00 1.662531933e+02 1.664754263e+02 5.2e-08 0.18 24 3.5e-05 1.0e-01 2.3e-03 1.01e+00 1.663489963e+02 1.664340420e+02 2.0e-08 0.19 25 1.6e-05 8.4e-02 1.1e-03 1.00e+00 1.663808103e+02 1.664201668e+02 9.4e-09 0.20 26 1.5e-05 7.7e-02 9.6e-04 1.00e+00 1.663840618e+02 1.664194962e+02 8.4e-09 0.20 27 1.3e-05 7.0e-02 8.6e-04 1.01e+00 1.663864463e+02 1.664183305e+02 7.6e-09 0.21 28 1.2e-05 6.3e-02 7.7e-04 1.00e+00 1.663886321e+02 1.664173227e+02 6.8e-09 0.22 29 1.1e-05 5.8e-02 7.0e-04 1.00e+00 1.663905903e+02 1.664164076e+02 6.2e-09 0.22 30 9.6e-06 5.3e-02 6.3e-04 1.00e+00 1.663923512e+02 1.664155833e+02 5.5e-09 0.23 31 8.7e-06 4.8e-02 5.6e-04 1.00e+00 1.663939340e+02 1.664148400e+02 5.0e-09 0.24 32 7.8e-06 4.4e-02 5.1e-04 1.00e+00 1.663953569e+02 1.664141700e+02 4.5e-09 0.25 33 7.0e-06 4.1e-02 4.6e-04 1.00e+00 1.663966362e+02 1.664135660e+02 4.0e-09 0.25 34 6.3e-06 3.7e-02 4.1e-04 1.00e+00 1.663977864e+02 1.664130217e+02 3.6e-09 0.26 35 5.7e-06 3.5e-02 3.7e-04 1.00e+00 1.663988207e+02 1.664125312e+02 3.3e-09 0.27 36 5.1e-06 3.2e-02 3.3e-04 1.00e+00 1.663997507e+02 1.664120891e+02 2.9e-09 0.27 37 4.6e-06 2.9e-02 3.0e-04 1.00e+00 1.664005870e+02 1.664116908e+02 2.6e-09 0.28 38 4.1e-06 2.7e-02 2.7e-04 1.00e+00 1.664013391e+02 1.664113318e+02 2.4e-09 0.29 39 3.7e-06 2.5e-02 2.4e-04 1.00e+00 1.664020155e+02 1.664110084e+02 2.1e-09 0.29 40 3.4e-06 2.4e-02 2.2e-04 1.00e+00 1.664026238e+02 1.664107169e+02 1.9e-09 0.30 41 3.0e-06 2.2e-02 2.0e-04 1.00e+00 1.664031708e+02 1.664104542e+02 1.7e-09 0.31 42 2.7e-06 2.1e-02 1.8e-04 1.00e+00 1.664036628e+02 1.664102176e+02 1.6e-09 0.31 43 2.4e-06 1.9e-02 1.6e-04 1.00e+00 1.664041053e+02 1.664100044e+02 1.4e-09 0.32 44 2.2e-06 1.8e-02 1.4e-04 1.00e+00 1.664045034e+02 1.664098124e+02 1.3e-09 0.33 45 2.0e-06 1.7e-02 1.3e-04 1.00e+00 1.664048615e+02 1.664096395e+02 1.1e-09 0.33 46 1.8e-06 1.6e-02 1.2e-04 1.00e+00 1.664051837e+02 1.664094838e+02 1.0e-09 0.34 47 1.6e-06 1.5e-02 1.0e-04 1.00e+00 1.664054736e+02 1.664093436e+02 9.2e-10 0.35 48 1.4e-06 1.5e-02 9.4e-05 1.00e+00 1.664057344e+02 1.664092173e+02 8.3e-10 0.36 49 1.3e-06 1.4e-02 8.5e-05 1.00e+00 1.664059691e+02 1.664091036e+02 7.5e-10 0.36 50 1.2e-06 1.3e-02 7.6e-05 1.00e+00 1.664061802e+02 1.664090012e+02 6.7e-10 0.37 51 1.1e-06 1.3e-02 6.9e-05 1.00e+00 1.664063701e+02 1.664089090e+02 6.1e-10 0.38 52 9.5e-07 1.2e-02 6.2e-05 1.00e+00 1.664065410e+02 1.664088260e+02 5.5e-10 0.38 53 8.5e-07 1.2e-02 5.6e-05 1.00e+00 1.664066948e+02 1.664087512e+02 4.9e-10 0.39 54 7.7e-07 1.1e-02 5.0e-05 1.00e+00 1.664068331e+02 1.664086839e+02 4.4e-10 0.39 55 6.9e-07 1.1e-02 4.5e-05 1.00e+00 1.664069575e+02 1.664086232e+02 4.0e-10 0.40 56 6.2e-07 1.1e-02 4.1e-05 1.00e+00 1.664070695e+02 1.664085686e+02 3.6e-10 0.41 57 5.6e-07 1.0e-02 3.7e-05 1.00e+00 1.664071702e+02 1.664085194e+02 3.2e-10 0.42 58 5.0e-07 1.0e-02 3.3e-05 1.00e+00 1.664072608e+02 1.664084750e+02 2.9e-10 0.42 59 4.5e-07 9.9e-03 3.0e-05 1.00e+00 1.664073423e+02 1.664084351e+02 2.6e-10 0.43 60 4.1e-07 9.7e-03 2.7e-05 1.00e+00 1.664074156e+02 1.664083991e+02 2.4e-10 0.44 61 3.7e-07 9.5e-03 2.4e-05 1.00e+00 1.664074815e+02 1.664083667e+02 2.1e-10 0.44 62 3.3e-07 9.3e-03 2.2e-05 1.00e+00 1.664075408e+02 1.664083374e+02 1.9e-10 0.45 63 3.0e-07 9.2e-03 1.9e-05 1.00e+00 1.664075942e+02 1.664083111e+02 1.7e-10 0.46 64 2.7e-07 9.0e-03 1.7e-05 1.00e+00 1.664076422e+02 1.664082874e+02 1.5e-10 0.46 65 2.4e-07 8.9e-03 1.6e-05 1.00e+00 1.664076853e+02 1.664082661e+02 1.4e-10 0.47 66 2.2e-07 8.8e-03 1.4e-05 1.00e+00 1.664077242e+02 1.664082469e+02 1.2e-10 0.48 67 2.0e-07 8.7e-03 1.3e-05 1.00e+00 1.664077592e+02 1.664082296e+02 1.1e-10 0.48 68 1.8e-07 8.6e-03 1.1e-05 1.00e+00 1.664077906e+02 1.664082140e+02 1.0e-10 0.49 69 1.6e-07 8.5e-03 1.0e-05 1.00e+00 1.664078190e+02 1.664082000e+02 9.1e-11 0.50 70 1.4e-07 8.4e-03 9.3e-06 1.00e+00 1.664078444e+02 1.664081874e+02 8.2e-11 0.50 71 1.3e-07 8.3e-03 8.4e-06 1.00e+00 1.664078674e+02 1.664081760e+02 7.4e-11 0.51 72 1.2e-07 8.2e-03 7.5e-06 1.00e+00 1.664078880e+02 1.664081658e+02 6.6e-11 0.52 73 1.0e-07 8.2e-03 6.8e-06 1.00e+00 1.664079065e+02 1.664081567e+02 6.0e-11 0.52 74 9.3e-08 8.1e-03 6.1e-06 1.00e+00 1.664079232e+02 1.664081484e+02 5.4e-11 0.53 75 8.4e-08 8.1e-03 5.5e-06 1.00e+00 1.664079383e+02 1.664081409e+02 4.8e-11 0.54 76 7.6e-08 8.0e-03 4.9e-06 1.00e+00 1.664079518e+02 1.664081342e+02 4.4e-11 0.54 77 6.8e-08 8.0e-03 4.4e-06 1.00e+00 1.664079640e+02 1.664081281e+02 3.9e-11 0.55 78 6.1e-08 7.9e-03 4.0e-06 1.00e+00 1.664079750e+02 1.664081227e+02 3.5e-11 0.56 79 5.5e-08 7.9e-03 3.6e-06 1.00e+00 1.664079848e+02 1.664081178e+02 3.2e-11 0.56 80 5.0e-08 7.9e-03 3.2e-06 1.00e+00 1.664079937e+02 1.664081134e+02 2.9e-11 0.57 81 4.5e-08 7.9e-03 2.9e-06 1.00e+00 1.664080017e+02 1.664081094e+02 2.6e-11 0.58 82 4.0e-08 7.8e-03 2.6e-06 1.00e+00 1.664080089e+02 1.664081058e+02 2.3e-11 0.58 83 3.6e-08 7.8e-03 2.4e-06 1.00e+00 1.664080153e+02 1.664081026e+02 2.1e-11 0.59 84 3.3e-08 7.8e-03 2.1e-06 1.00e+00 1.664080212e+02 1.664080997e+02 1.9e-11 0.60 85 2.9e-08 7.8e-03 1.9e-06 1.00e+00 1.664080264e+02 1.664080970e+02 1.7e-11 0.60 86 2.6e-08 7.7e-03 1.7e-06 1.00e+00 1.664080311e+02 1.664080947e+02 1.5e-11 0.61 87 2.4e-08 7.7e-03 1.5e-06 9.99e-01 1.664080354e+02 1.664080926e+02 1.4e-11 0.62 88 2.1e-08 7.7e-03 1.4e-06 1.00e+00 1.664080392e+02 1.664080907e+02 1.2e-11 0.62 89 1.9e-08 7.7e-03 1.3e-06 1.00e+00 1.664080426e+02 1.664080890e+02 1.1e-11 0.63 90 1.7e-08 7.6e-03 1.1e-06 9.93e-01 1.664080457e+02 1.664080875e+02 1.0e-11 0.64 91 1.6e-08 7.6e-03 1.0e-06 9.96e-01 1.664080485e+02 1.664080861e+02 9.0e-12 0.64 92 1.4e-08 7.6e-03 9.1e-07 1.00e+00 1.664080510e+02 1.664080848e+02 8.1e-12 0.65 93 1.3e-08 6.8e-03 8.2e-07 1.01e+00 1.664080533e+02 1.664080837e+02 7.3e-12 0.66 94 1.2e-08 6.2e-03 7.4e-07 9.98e-01 1.664080553e+02 1.664080827e+02 6.6e-12 0.66 95 1.0e-08 5.5e-03 6.7e-07 9.97e-01 1.664080571e+02 1.664080818e+02 5.9e-12 0.67 96 9.4e-09 5.0e-03 6.0e-07 9.95e-01 1.664080588e+02 1.664080810e+02 5.3e-12 0.68 97 8.4e-09 4.5e-03 5.4e-07 1.00e+00 1.664080603e+02 1.664080802e+02 4.8e-12 0.68 98 7.5e-09 4.0e-03 4.9e-07 9.83e-01 1.664080616e+02 1.664080795e+02 4.3e-12 0.69 99 6.8e-09 3.6e-03 4.4e-07 9.99e-01 1.664080628e+02 1.664080789e+02 3.9e-12 0.70 100 6.1e-09 3.3e-03 3.9e-07 1.02e+00 1.664080639e+02 1.664080784e+02 3.5e-12 0.70 101 5.5e-09 2.9e-03 3.5e-07 1.01e+00 1.664080649e+02 1.664080779e+02 3.2e-12 0.71 102 4.9e-09 2.6e-03 3.2e-07 1.02e+00 1.664080658e+02 1.664080774e+02 2.9e-12 0.72 103 4.4e-09 2.4e-03 2.9e-07 1.01e+00 1.664080666e+02 1.664080770e+02 2.6e-12 0.73 104 4.0e-09 2.1e-03 2.6e-07 1.04e+00 1.664080674e+02 1.664080765e+02 2.4e-12 0.73 105 3.7e-09 1.9e-03 2.3e-07 1.00e+00 1.664080680e+02 1.664080763e+02 2.1e-12 0.74 106 3.3e-09 1.7e-03 2.1e-07 1.04e+00 1.664080687e+02 1.664080759e+02 2.0e-12 0.75 107 2.9e-09 1.6e-03 1.9e-07 9.99e-01 1.664080692e+02 1.664080757e+02 1.8e-12 0.75 108 2.6e-09 1.4e-03 1.7e-07 9.99e-01 1.664080696e+02 1.664080755e+02 1.6e-12 0.76 109 2.4e-09 1.3e-03 1.5e-07 1.00e+00 1.664080700e+02 1.664080753e+02 1.4e-12 0.76 110 2.2e-09 1.1e-03 1.4e-07 1.00e+00 1.664080704e+02 1.664080751e+02 1.3e-12 0.77 111 1.9e-09 1.0e-03 1.2e-07 1.01e+00 1.664080707e+02 1.664080749e+02 1.2e-12 0.78 112 1.7e-09 9.2e-04 1.1e-07 9.94e-01 1.664080710e+02 1.664080748e+02 1.0e-12 0.78 113 1.6e-09 8.3e-04 1.0e-07 1.00e+00 1.664080712e+02 1.664080747e+02 9.5e-13 0.79 Optimizer terminated. Time: 0.79 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6640807123e+02 nrm: 2e+01 Viol. con: 2e-08 var: 0e+00 Dual. obj: 1.6640807466e+02 nrm: 1e+03 Viol. con: 0e+00 var: 5e-03 * End solution on dual form. * Transforming to primal solution. Solving took 0.816 seconds. Solving took 9 GP solves and 14.6 seconds. Solves with these variables bounded: value near lower bound: Mission.CruiseAlt value near upper bound: Mission.Aircraft.HorizontalTail.WingBox.M_{r_{out}}, Mission.Aircraft.Engine.Thrust.\alpha_{max}, Mission.Aircraft.Wing.WingNoStruct.A_{tri}, Mission.TotalTime, Mission.Aircraft.LandingGear.d_{nacelle}, Mission.T_{t_{4.1_{max-Cruise}}} Checking for relaxed constants... Solution check warning: Primal solution computed cost did not match solver-returned cost: 1.495742457694431e+110 vs 1.4956976656e+110 GP iteration 0 has relaxed constants Cost ---- 1.496e+110 Free Variables -------------- | Mission.Aircraft.Engine.Turbine.Relax C_{p_{t2}} : 2.251 Cp Value for Combustion Products in LP Turbine | Mission.Aircraft.Fuselage.Relax l_{nose} : 1.042 Nose length n_{pass} : [ 2.86 ] Number of passengers | Mission.Aircraft.Relax f_{L_{total/wing}} : 1.656 Total lift as a percentage of wing lift | Mission.Aircraft.Wing.WingNoStruct.Relax \tan(\Lambda) : 1.133 Tangent of quarter-chord sweep angle | Mission.FlightState.Atmosphere.Relax L_{atm} : [ 1.77 1 1 1 1 ] Temperature lapse rate T_{sl} : [ 1 1 1.25 1 1 ] Temperature at sea level | Mission.Relax R_{req} : 2.362 Required Cruise Range GP iteration 1 has relaxed constants Cost ---- 7.486e+74 Free Variables -------------- | Mission.Aircraft.Engine.Combustor.Relax hold_{4a} : 1.093 1+(gamma-1)/2 * M_4a**2 | Mission.Aircraft.Fuselage.Relax n_{pass} : [ 1.03 ] Number of passengers | Mission.Aircraft.LandingGear.Relax h_{hold} : 1.006 Hold height Solution check warning: Primal solution computed cost did not match solver-returned cost: 3.7050980759335926e+72 vs 3.70502020539e+72 WEIGHT DIFFERENCES Total Fuel Weight Percent Diff: [-92.94682113] Total Aircraft Weight Percent Diff: [-21.48054877] Engine Weight Percent Diff: -56.278166751133654 Fuselage Weight Percent Diff: -0.8697062242189039 Payload Weight Percent Diff: [-0.04003553] VT Weight Percent Diff: -8.607369318686331 HT Weight Percent Diff: -93.23322032086058 Wing Weight Percent Diff: 8.26743549310153 WING DIFFERENCES Wing Span Percent Diff: -0.029997996845333903 Wing Area Percent Diff: 32.90022842687177 HORIZONTAL TAIL DIFFERENCES HT Area Percent Diff: 40.489576650137494 VERTICAL TAIL DIFFERENCES VT Span Percent Diff: -11.022306825728005 VT Area Percent Diff: -60.38680571118094 CRUISE SEGMENT 1 DRAG DIFFERENCES Overall Cd Percent Diff: [-18.54737792] L/D Percent Diff: [24.01020217] Nacelle Cd Percent Diff: [-94.27640436] HT Cd Percent Diff: [-80.76934841] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-58.00304986] dimensionless Wing Cd percent Diff: [-14.22936117] Induced Drag Cd Percent Diff: [1.21931584] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-90.57035921] FUSELAGE DIFFERENCES Weight of HB material: -38.35923841364424 Weight of VB material: 87.8307550215667 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.71260527] Mission1 ======== Cost ---- W_{f_{total}}[:].sum() Constraints ----------- W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin} PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:]) x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:]) x_{CG}[3] <= \Delta x_n + x_n \Delta x_m + x_{CG}[3] >= x_m \tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m C_{D_{fuse}}[:] = 0.018081 M_{fuseD} = 0.72 W_{start}[0] = W_{total}[:] W_{start}[:] >= W_{end}[:] + W_{burn}[:] W_{start}[1:] = W_{end}[:4] W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1] W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2] W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1] hft[2] >= CruiseAlt hft[1:5] = hft[:4] + dhft[1:5] hft[0] = dhft[0] dhft[1:3] = dhft[:2] RC[0] >= 2.5e+03 RC[:3] >= RC_{min}[:3] \theta[2] >= 0.015 hft[2] >= MinCruiseAlt n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:] R_{segment}[3:4] = R_{segment}[4:5] M[3:5] >= M_{min} 0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req} Fsafetyfac*F[0] = T_e W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:] V_2[:] = M_2[:]*a[:] \alpha_{max,w}[:3] = 0.18 \alpha_{max,w}[3:] = 0.1 0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime 0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime ClimbTime <= MaxClimbTime T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}} F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:] F_{fuel}[:] <= 1.0000001 F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:] F_{fuel}[:] <= 1.0000001 F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:] F_{fuel}[:] <= 1.0000001 F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:] F_{fuel}[:] <= 1.0000001 F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:] F_{fuel}[:] <= 1.0000001 OPR[:] <= OPR_{max} Aircraft Fuselage W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on} W_{pass}[:] >= n_{pass}[:]*W_{avg. pass} W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo} W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}} W_{payload}[:] <= W_{payload_{max}} n_{pass}[:] <= n_{seat} n_{rows} = n_{seat}/SPR l_{shell} = n_{rows}*p_s \theta_{db} = w_{db}/R_{fuse} R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db} A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db} (PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse} A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin} w_{floor} = w_{fuse} R_{fuse} + w_{db} >= w_{fuse} h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse} t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell} S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2 S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2 l_{fuse} = l_{nose} + l_{shell} + l_{cone} l_{cone} = R_{fuse}/\lambda_{cone} x_{shell1} = l_{nose} x_{shell2} >= l_{nose} + l_{shell} t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin} t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin} \sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell}) \sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin} l_{floor} >= l_{shell} + 2*R_{fuse} P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat}) A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor} V_{floor} = 2*w_{floor}*A_{floor} W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor} \tau_{cone} = \sigma_{skin} W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame}) x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone} -2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}} (PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}} x_{hbend_{Land}} >= x_{wing} x_{hbend_{Land}} <= l_{fuse} x_{hbend_{MLF}} >= x_{wing} x_{hbend_{MLF}} <= l_{fuse} A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}}) A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}}) A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h}) A_{2h_{MLF}} >= Mission1.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h}) A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2) A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}} A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}} A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}} A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}} A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}} A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}} A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}} A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}} V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c} V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c} V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}} W_{hbend} >= g*\rho_{bend}*V_{hbend} x_{vbend} >= x_{wing} x_{vbend} <= l_{fuse} B_{0v} = B_{1v}*(x_{tail} - x_{vbend}) B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2) B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}} 0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}} V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission1.Aircraft.Fuselage.r_{w/c} V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}} W_{vbend} >= \rho_{bend}*g*V_{vbend} x_f = x_{wing} + 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c} x_b = x_{wing} - 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c} \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h} \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v} V_{cyl} = A_{skin}*l_{shell} V_{nose} = S_{nose}*t_{skin} V_{bulk} = S_{bulk}*t_{skin} V_{db} = A_{db}*l_{shell} V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse}) W_{apu} = W_{payload_{max}}*f_{apu} W_{db} = \rho_{skin}*g*V_{db} W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk}) W_{window} >= W'_{window}*l_{shell} W_{padd} = W_{payload_{max}}*f_{padd} W_{seat} >= W'_{seat}*n_{seat} W_{seat} >= f_{seat}*W_{payload_{max}} W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk}) W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db} W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone}) Wing WingNoStruct A_{rect} = c_{tip}*b 0.5*(1 - \lambda)*c_{root}*b <= A_{tri} p >= 1 + 2*\lambda 2*q >= 1 + p y_{mac} = b/3*q/p mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q \lambda = c_{tip}/c_{root} S = b*(c_{root} + c_{tip})/2 0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w) e*(1 + f(\lambda_w)*AR) <= 1 \lambda >= 0.15 V_{fuel, max} <= 0.303*mac^2*b*\tau W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g b <= b_{max} WingBox AR = b^2/S 0.423*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap} \nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56 W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5) \tau <= \tau_{max_w} W_{struct} >= W_{web} + W_{cap} AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12 W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5) Mission1.Aircraft.Wing.WingBox.N_{lift} = 3 Mission1.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8 \lambda = taper W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt}) 0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}} Engine Compressor (no constraints) Combustor (no constraints) Turbine (no constraints) Thrust (no constraints) FanMap (no constraints) LPCMap (no constraints) HPCMap (no constraints) Sizing A_{2} >= A_{5} + A_{7} FlightState V[:] = V[:] a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5 V[:] = M[:]*a[:] Altitude h[:] = hft[:] Atmosphere (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:] \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:]) T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:] \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72) EnginePerformance CompressorPerformance T_{t_0}[:] = T_{atm}[:]/c1[:]^-1 h_{t_0}[:] = C_{p_{air}*T_{t_0}[:] P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:] T_{t_{1.8}}[:] = T_{t_0}[:] h_{t_{1.8}}[:] = h_{t_0}[:] P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5 T_{T_{2}}[:] = T_{t_{1.8}}[:] h_{T_{2}}[:] = h_{t_{1.8}}[:] P_{T_{2}}[:] = P_{t_{1.8}}[:] P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:] T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016 h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:] P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:] T_{t_7}[:] = T_{t_{2.1}}[:] h_{t_7}[:] = h_{t_{2.1}}[:] P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:] T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152 h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1} P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:] T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491 h_{t_3}[:] = C_{p_{2}*T_{t_3}[:] CombustorPerformance h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:] h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:] fp1[:] = f[:] + 1 M_{4a}[:] = 0.1025 fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5 T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]] P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891 u_{4a}[:] = M_{4a}[:]*(1.31*Mission1.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a} u_c[:] = r_{uc}*u_{4a}[:] P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891 TurbinePerformance h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:] P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:] \pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565 h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:] P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:] T_{t_5}[:] = T_{t_{4.9}}[:] h_{t_5}[:] = h_{t_{4.9}}[:] ThrustPerformance P_{8}[:] = P_{atm}[:] h_{8}[:] = C_{p_{fex}*T_{8}[:] u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:] (P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:] h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:] P_{6}[:] = P_{atm}[:] (P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:] u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:] h_6[:] = C_{p_{tex}*T_{6}[:] h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:] \alpha[:] = m_{fan}[:]/m_{core}[:] \alpha_{+1}[:] = \alpha[:] + 1 \alpha[:] <= \alpha_{max} F[:] <= F_{6}[:] + F_{8}[:] F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:]) TSFC[:] = 1/I_{sp}[:] F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:] FanMapPerformance m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}} LPCMapPerformance m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D} HPCMapPerformance m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D} SizingPerformance P_{7}[:] >= P_{atm}[:] M_7[:] <= 1 a_{7}[:] = (1.4*Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5 a_{7}[:]*M_7[:] = u_{7}[:] \rho_7[:] = P_{7}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:]) P_{5}[:] >= P_{atm}[:] M_5[:] <= 1 a_{5}[:] = (1.39*Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5 a_{5}[:]*M_5[:] = u_{5}[:] \rho_5[:] = P_{5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:]) h_{2}[:] = C_{p_{1}*T_{2}[:] \rho_{2}[:] = P_{2}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:]) u_{2}[:] = M_2[:]*(C_{p_{1}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:]/781)^0.5 h_{2.5}[:] = C_{p_{2}*T_{2.5}[:] \rho_{2.5}[:] = P_{2.5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]) u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/781)^0.5 m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine} d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5 d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5 \eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]]) h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:] P_{t_4}[:] = \pi_{b}*P_{t_3}[:] M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]] M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]]) P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:] \pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013 \pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10 \pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10 \pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10 m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref}) \pi_{f}[:] >= 1 \pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10 \pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10 \pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10 \pi_{lc}[:] >= 1 m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref}) \pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10 \pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10 \pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10 m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref}) \pi_{hc}[:] >= 1 OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:] P_{t_8}[:] = P_{t_7}[:] T_{t_8}[:] = T_{t_7}[:] P_{t_6}[:] = P_{t_5}[:] T_{t_6}[:] = T_{t_5}[:] F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:] I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g) N_{f}[:]*G_{f} = N_{1}[:] N_{1}[:] <= 1.1 N_{2}[:] <= 1.1 fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD} fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD} P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5 (T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2 P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979 (T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2 M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:] m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:] m_{total}[:] = m_{fan}[:] + m_{core}[:] P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512 T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1 m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2} P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857 T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1 m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5} 1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD} 0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD} 1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD} 0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD} m_{lc_D} >= 0.7*m_{coreD}/0.649 m_{lc_D} <= 1.3*m_{coreD}/0.649 m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23 m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23 \bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405 \bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405 F[:] = F_{spec}[:] T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}} OPR[:] <= OPR_{max} VerticalTail VerticalTailNoStruct C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}} L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}} c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt})) A_{vt} = b_{vt}^2/S_{vt} b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt} p_{vt} >= 1 + 2*\lambda_{vt} 2*q_{vt} >= 1 + p_{vt} y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt} z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt} 0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt} \lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}} \Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}} \Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt} \lambda_{vt} >= 0.25 V_{vt} >= V_{vt_{min}} WingBox AR_{vt} = (2*b_{vt})^2/(2*S_{vt}) 0.423*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap} \nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56 W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5) \tau_{vt} <= 0.14 W_{struct} >= 0.5*(W_{web} + W_{cap}) Mission1.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24 AR_{vt}*2*L_{vt_{max}}*Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12 W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5) Mission1.Aircraft.VerticalTail.WingBox.N_{lift} = 1 Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*Mission1.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8 \lambda_{vt} = taper W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT}) HorizontalTail HorizontalTailNoStruct \Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht} \Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}} p_{ht} >= 1 + 2*\lambda_{ht} 2*q_{ht} >= 1 + p_{ht} y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht} 0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht} \lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}} S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2 0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht}) e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1 AR_{ht} = b_{ht}^2/S_{ht} \lambda_{ht} >= 0.2 \lambda_{ht} <= 1 WingBox AR_{ht} = b_{ht}^2/S_{ht} 0.423*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap} \nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56 W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5) \tau_{ht} <= 0.14 W_{struct} >= W_{web} + W_{cap} L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2 L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht}) 2*AR_{ht}*L_{shear}*Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12 W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5) Mission1.Aircraft.HorizontalTail.WingBox.N_{lift} = 1 Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission1.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8 L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht} L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}} W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht}) LandingGear l_n + z_{wing} + y_m*\tan(\gamma) >= l_m T = 2*y_m x_m >= x_n + B x_n >= 5 \tan(\phi) = \tan(\phi_{min}) (z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1 \tan(\psi) <= \tan(\psi_{max}) x_{up} - x_m <= l_m/\tan(\theta_{max}) y_m >= l_m S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG}) l_{oleo} = 2.5*S_{sa} d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5 l_m >= l_{oleo} + d_{t_m}/2 F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in]) W_{wa,m} = 1.2*F_{w_m}^0.609 F_{w_n} = L_{w_n}*d_{t_n}/1e+03 W_{wa,n} = 1.2*F_{w_n}^0.609 L_{w_m} = L_m/(n_{mg}*n_{wps}) L_{w_n} = L_n/n_{wps} d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315 w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48 d_{t_n} = 0.8*d_{t_m} w_{t_n} = 0.8*w_{t_m} W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m W_{mw} = n_{wps}*W_{wa,m} W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g \sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}}) W_{nw} >= n_{wps}*W_{wa,n} L_m <= 9.87*E*I_m/(K*l_m)^2 I_m = PI*r_m^3*t_m L_n <= 9.87*E*I_n/(K*l_n)^2 I_n = PI*r_n^3*t_n 2*r_m/t_m <= 40 2*r_m/t_n <= 40 h_{hold} >= 2*w_{t_m} + 2*r_m 0.8 >= 2*w_{t_n} + 2*r_n W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m})) W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n}) W_{lg} >= C_{lg}*(W_{mg} + W_{ng}) W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m x_m >= x_{CG_{lg}} c_{root} = c_0 Mission1.Aircraft.Wing.WingBox.r_{w/c} = Mission1.Aircraft.Fuselage.r_{w/c} x_w = x_{wing} Mission1.Aircraft.Fuselage.N_{lift} = Mission1.Aircraft.Wing.WingBox.N_{lift} f_{L_{total/wing}}*L_{max} >= Mission1.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}} W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc} W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:] W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:] W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:] W_{total}[:] <= W_{total, max} f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}} W_{misc} >= W_{lg} + W_{hpesys} W_{hpesys} = f_{hpesys}*W_{total, max} x_n <= l_{nose} x_m >= x_{wing} \Delta x_{AC_{wing}} + x_{wing} >= x_m x_{hpesys} = 1.1*l_{nose} x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys} d_{nacelle} >= d_{f} + 2*t_{nacelle} E_{land} >= W_{total, max}/(2*g)*w_{ult}^2 x_{up} = x_{shell2} L_n = W_{total, max}*\Delta x_m/B L_m = W_{total, max}*\Delta x_n/B L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max} y_{eng} >= y_m 3*n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}} V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse} W_{tail} >= n_{vt}*W_{vt} + W_{ht} 2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db} B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v}) m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht} x_{CG_{ht}} <= l_{fuse} V_{ht} = S_{ht}*l_{ht}/(S*mac) L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}} L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}} x_{CG_{vt}} <= l_{fuse} V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b) n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max} n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng} D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}} I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:] I_{z}[:] <= I_{z, max} S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2 l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}} f_{S_{nacelle}} = S_{nacelle}*S^-1 A_{inlet} = 0.4*S_{nacelle} A_{fancowl} = 0.2*S_{nacelle} A_{exh} = 0.4*S_{nacelle} A_{corecowl} = 3PI*d_{LPC}^2 W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl}) W_{eadd} = f_{eadd}*W_{engine} W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon} W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine}) y_{eng} = 0.5*w_{fuse} (L_{max} - Mission1.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission1.Aircraft.Wing.WingBox.M_r*c_{root} A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend}) A_{1h_{MLF}} >= (Mission1.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h}) I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16) I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81 I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81) x_{shell2} + l_{cone} >= x_{eng} x_{eng} >= x_{shell2} + 0.75*l_{cone} S_{floor} = 0.312*P_{floor} M_{floor} = 0.0352*P_{floor}*w_{floor} \Delta R_{fuse} = R_{fuse}*0.43/1.75 b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2 b_{ht_{out}} = 0.5*b_{ht} - w_{fuse} L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}} M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}} L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}} c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach} \pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht}) FlightSegment FlightState V[:] = V[:] a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5 V[:] = M[:]*a[:] Altitude h[:] = hft[:] Atmosphere (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:] \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:]) T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:] \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72) FlightP P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:] RC[:] = P_{excess}[:]/W_{avg}[:] \theta[:]*V[:] = RC[:] dhft[:] = tmin[:]*RC[:] R_{segment}[:] = thr[:]*V[:] WingPerformance 0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:] \Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:] \Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2 (AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2 C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:] \alpha_w[:] <= \alpha_{max,w}[:] D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:] C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:] C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR) Re_w[:] = \rho[:]*V[:]*mac/\mu[:] C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114 FuselagePerformance (no constraints) VerticalTailPerformance D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:] Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:] C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577 HorizontalTailPerformance L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:] C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:] \alpha_{ht}[:] <= \alpha_{ht,max} C_{L_{\alpha,ht_0}}[:] = 6.28 D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:] C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht}) Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:] C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852 W_{burn}[:] = W_{burn}[:] F_{fuel}[:] = F_{fuel}[:] \rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:]) P_{cabin}[:] = 7.5e+04 T_{cabin}[:] = 297 V[:] >= V_{stall}[:] W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:] tmin[:] = thr[:] L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:] L_{total}[:] = f_{L_{total/wing}}*L_w[:] L_{total}[:] >= W_{avg}[:] + L_{ht}[:] D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2 D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:]) C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S) L/D[:] = W_{avg}[:]/D[:] W_{Load}[:] <= W_{Load_{max}}[:] W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S p_{o}[:] >= L_w[:]*c_{root}/S \eta_{o}[:] = w_{fuse}/(b/2) x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:] c_{m_{w}}[:] = 1.9 x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2) x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse} x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}} x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}} C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht} AR_{ht} >= 4 C_{L_{ht}}[:] >= 0.01 SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac SM[:] >= SM_{min} SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}} x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:] R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:] C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2 V_{nacelle}[:] = r_{v_{nacelle}}*V[:] V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]] r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0) C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0 D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S \Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}} M_2[:3] = M[:3] M_{2.5}[:3] = 0.6 hold_{2}[:3] = 1.07164 hold_{2.5}[:3] = 1.06372 P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:] c1[:] = 1 + 0.201*M[:]^2.0 M_2[3:] = M[3:] M_{2.5}[3:] = 0.6 hold_{2}[3:] = 1.07164 hold_{2.5}[3:] = 1.06372 Beginning signomial solve. Using solver 'mosek' Solving for 1748 variables. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 471 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 869 Optimizer - Cones : 0 Optimizer - Scalar variables : 3451 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.02 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 1.48e+04 after factor : 1.46e+05 Factor - dense dim. : 0 flops : 2.87e+07 Factor - GP saved nzs : 3.32e+04 GP saved flops : 9.06e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.1e+03 1.2e+05 0.00e+00 -1.225677090e+05 2.000000000e+00 1.0e+00 0.03 1 1.6e+03 2.1e+03 8.4e+04 -9.71e-01 -1.216848616e+05 2.766603376e+00 6.9e-01 0.04 2 8.2e+02 1.1e+03 4.4e+04 -9.57e-01 -1.192284454e+05 5.074629256e+00 3.6e-01 0.05 3 2.9e+02 3.9e+02 1.6e+04 -9.16e-01 -1.104950334e+05 2.156321042e+01 1.3e-01 0.06 4 2.9e+02 3.9e+02 1.6e+04 -7.68e-01 -1.085357608e+05 1.724066982e+03 1.3e-01 0.06 5 1.1e+02 1.5e+02 6.0e+03 -7.59e-01 -8.496747542e+04 6.645584441e+03 4.9e-02 0.07 6 3.8e+01 5.0e+01 2.0e+03 -4.14e-01 -4.573108853e+04 1.064008602e+04 1.7e-02 0.08 7 2.0e+01 2.7e+01 1.1e+03 2.50e-01 -2.853524473e+04 6.956951010e+03 9.0e-03 0.08 8 9.4e+00 1.3e+01 5.1e+02 5.70e-01 -1.401680654e+04 4.219068590e+03 4.2e-03 0.09 9 4.7e+00 6.4e+00 2.6e+02 8.27e-01 -7.046366663e+03 2.497942694e+03 2.1e-03 0.10 10 1.4e+00 1.9e+00 7.8e+01 9.33e-01 -2.013352976e+03 9.403827672e+02 6.4e-04 0.10 11 6.4e-01 8.6e-01 3.5e+01 9.93e-01 -6.804485566e+02 6.596896968e+02 2.9e-04 0.11 12 4.8e-01 6.5e-01 2.6e+01 9.96e-01 -4.518204661e+02 5.573058292e+02 2.2e-04 0.12 13 3.5e-01 7.3e-01 1.9e+01 9.80e-01 -2.686036694e+02 4.735665754e+02 1.6e-04 0.13 14 1.7e-01 3.6e-01 9.5e+00 9.96e-01 -1.706351213e+00 3.632401846e+02 7.9e-05 0.13 15 5.7e-02 1.5e-01 3.2e+00 9.94e-01 1.663588588e+02 2.900324402e+02 2.7e-05 0.14 16 3.3e-02 1.3e-01 1.9e+00 1.00e+00 2.025528074e+02 2.744117059e+02 1.6e-05 0.15 17 5.1e-03 1.9e-01 3.2e-01 1.00e+00 2.450077405e+02 2.572047198e+02 2.8e-06 0.15 18 1.5e-03 1.3e-01 9.4e-02 1.00e+00 2.510860215e+02 2.546831567e+02 8.5e-07 0.16 19 4.8e-04 1.1e-01 3.1e-02 1.00e+00 2.528335324e+02 2.540184841e+02 2.8e-07 0.17 20 2.1e-04 8.8e-02 1.3e-02 1.00e+00 2.533175848e+02 2.538309261e+02 1.2e-07 0.17 21 1.9e-04 8.0e-02 1.2e-02 1.00e+00 2.533556918e+02 2.538177109e+02 1.1e-07 0.18 22 1.7e-04 7.3e-02 1.1e-02 1.00e+00 2.533889178e+02 2.538047106e+02 9.9e-08 0.19 23 1.5e-04 6.6e-02 9.8e-03 1.00e+00 2.534188561e+02 2.537930533e+02 9.0e-08 0.19 24 1.4e-04 6.0e-02 8.8e-03 1.00e+00 2.534457755e+02 2.537825390e+02 8.1e-08 0.20 25 1.2e-04 5.5e-02 7.9e-03 1.00e+00 2.534699859e+02 2.537730615e+02 7.3e-08 0.21 26 1.1e-04 5.0e-02 7.1e-03 1.00e+00 2.534917592e+02 2.537645177e+02 6.5e-08 0.21 27 1.0e-04 4.6e-02 6.4e-03 1.00e+00 2.535113429e+02 2.537568176e+02 5.9e-08 0.22 28 9.0e-05 4.2e-02 5.8e-03 1.00e+00 2.535289580e+02 2.537498787e+02 5.3e-08 0.23 29 8.1e-05 3.9e-02 5.2e-03 1.00e+00 2.535448032e+02 2.537436266e+02 4.8e-08 0.24 30 7.3e-05 3.6e-02 4.7e-03 1.00e+00 2.535590570e+02 2.537379938e+02 4.3e-08 0.24 31 6.6e-05 3.3e-02 4.2e-03 1.00e+00 2.535718796e+02 2.537329193e+02 3.9e-08 0.25 32 5.9e-05 3.0e-02 3.8e-03 1.00e+00 2.535834151e+02 2.537283480e+02 3.5e-08 0.26 33 5.3e-05 2.8e-02 3.4e-03 1.00e+00 2.535937929e+02 2.537242304e+02 3.1e-08 0.26 34 4.8e-05 2.6e-02 3.1e-03 1.00e+00 2.536031295e+02 2.537205215e+02 2.8e-08 0.27 35 4.3e-05 2.4e-02 2.8e-03 1.00e+00 2.536115294e+02 2.537171809e+02 2.5e-08 0.28 36 3.9e-05 2.2e-02 2.5e-03 1.00e+00 2.536190868e+02 2.537141721e+02 2.3e-08 0.28 37 3.5e-05 2.1e-02 2.2e-03 1.00e+00 2.536258864e+02 2.537114623e+02 2.0e-08 0.29 38 3.1e-05 2.0e-02 2.0e-03 1.00e+00 2.536320042e+02 2.537090219e+02 1.8e-08 0.30 39 2.8e-05 1.8e-02 1.8e-03 1.00e+00 2.536375087e+02 2.537068241e+02 1.7e-08 0.30 40 2.5e-05 1.7e-02 1.6e-03 1.00e+00 2.536424614e+02 2.537048450e+02 1.5e-08 0.31 41 2.3e-05 1.6e-02 1.5e-03 1.00e+00 2.536469178e+02 2.537030627e+02 1.3e-08 0.32 42 2.1e-05 1.6e-02 1.3e-03 1.00e+00 2.536509277e+02 2.537014579e+02 1.2e-08 0.32 43 1.9e-05 1.5e-02 1.2e-03 1.00e+00 2.536545358e+02 2.537000129e+02 1.1e-08 0.33 44 1.7e-05 1.4e-02 1.1e-03 1.00e+00 2.536577825e+02 2.536987118e+02 9.8e-09 0.34 45 1.5e-05 1.3e-02 9.6e-04 1.00e+00 2.536607040e+02 2.536975404e+02 8.8e-09 0.34 46 1.3e-05 1.3e-02 8.7e-04 1.00e+00 2.536633330e+02 2.536964857e+02 7.9e-09 0.35 47 1.2e-05 1.2e-02 7.8e-04 1.00e+00 2.536656987e+02 2.536955361e+02 7.1e-09 0.36 48 1.1e-05 1.2e-02 7.0e-04 1.00e+00 2.536678276e+02 2.536946813e+02 6.4e-09 0.37 49 9.8e-06 1.1e-02 6.3e-04 1.00e+00 2.536697434e+02 2.536939118e+02 5.8e-09 0.37 50 8.9e-06 1.1e-02 5.7e-04 1.00e+00 2.536714675e+02 2.536932190e+02 5.2e-09 0.38 51 8.0e-06 1.1e-02 5.1e-04 1.00e+00 2.536730190e+02 2.536925954e+02 4.7e-09 0.39 52 7.2e-06 1.0e-02 4.6e-04 1.00e+00 2.536744152e+02 2.536920340e+02 4.2e-09 0.39 53 6.5e-06 1.0e-02 4.1e-04 1.00e+00 2.536756717e+02 2.536915286e+02 3.8e-09 0.40 54 5.8e-06 9.8e-03 3.7e-04 1.00e+00 2.536768025e+02 2.536910737e+02 3.4e-09 0.41 55 5.2e-06 9.6e-03 3.4e-04 1.00e+00 2.536778201e+02 2.536906643e+02 3.1e-09 0.41 56 4.7e-06 9.4e-03 3.0e-04 1.00e+00 2.536787359e+02 2.536902957e+02 2.8e-09 0.42 57 4.2e-06 9.2e-03 2.7e-04 1.00e+00 2.536795600e+02 2.536899639e+02 2.5e-09 0.43 58 3.8e-06 9.0e-03 2.5e-04 1.00e+00 2.536803017e+02 2.536896652e+02 2.2e-09 0.43 59 3.4e-06 8.9e-03 2.2e-04 1.00e+00 2.536809692e+02 2.536893963e+02 2.0e-09 0.44 60 3.1e-06 8.8e-03 2.0e-04 1.00e+00 2.536815699e+02 2.536891543e+02 1.8e-09 0.45 61 1.2e-06 3.4e-03 7.7e-05 1.00e+00 2.536848849e+02 2.536878177e+02 7.0e-10 0.45 62 1.1e-06 3.0e-03 6.9e-05 1.00e+00 2.536850944e+02 2.536877339e+02 6.3e-10 0.46 63 3.8e-07 1.1e-03 2.5e-05 1.00e+00 2.536863010e+02 2.536872470e+02 2.3e-10 0.47 64 3.5e-07 9.8e-04 2.2e-05 1.00e+00 2.536863685e+02 2.536872198e+02 2.0e-10 0.47 65 3.1e-07 8.8e-04 2.0e-05 1.00e+00 2.536864291e+02 2.536871953e+02 1.8e-10 0.48 66 2.8e-07 7.9e-04 1.8e-05 1.00e+00 2.536864836e+02 2.536871733e+02 1.7e-10 0.49 67 2.5e-07 7.1e-04 1.6e-05 1.00e+00 2.536865328e+02 2.536871534e+02 1.5e-10 0.49 68 2.3e-07 6.4e-04 1.5e-05 1.00e+00 2.536865770e+02 2.536871356e+02 1.3e-10 0.50 69 2.0e-07 5.8e-04 1.3e-05 1.00e+00 2.536866167e+02 2.536871195e+02 1.2e-10 0.51 70 1.8e-07 5.2e-04 1.2e-05 1.00e+00 2.536866525e+02 2.536871050e+02 1.1e-10 0.51 71 1.7e-07 4.7e-04 1.1e-05 1.00e+00 2.536866848e+02 2.536870920e+02 9.8e-11 0.52 72 1.5e-07 4.2e-04 9.6e-06 1.00e+00 2.536867138e+02 2.536870803e+02 8.8e-11 0.53 73 1.3e-07 3.8e-04 8.6e-06 1.00e+00 2.536867399e+02 2.536870697e+02 7.9e-11 0.53 74 1.2e-07 3.4e-04 7.8e-06 1.00e+00 2.536867634e+02 2.536870602e+02 7.1e-11 0.54 75 1.1e-07 3.1e-04 7.0e-06 1.00e+00 2.536867845e+02 2.536870517e+02 6.4e-11 0.55 76 9.8e-08 2.8e-04 6.3e-06 1.00e+00 2.536868035e+02 2.536870440e+02 5.8e-11 0.55 77 8.8e-08 2.5e-04 5.7e-06 1.00e+00 2.536868206e+02 2.536870371e+02 5.2e-11 0.56 78 7.9e-08 2.2e-04 5.1e-06 1.00e+00 2.536868360e+02 2.536870308e+02 4.7e-11 0.57 79 7.1e-08 2.0e-04 4.6e-06 1.00e+00 2.536868499e+02 2.536870252e+02 4.2e-11 0.57 80 6.4e-08 1.8e-04 4.1e-06 1.00e+00 2.536868624e+02 2.536870202e+02 3.8e-11 0.58 81 5.8e-08 1.6e-04 3.7e-06 1.00e+00 2.536868736e+02 2.536870156e+02 3.4e-11 0.59 82 5.2e-08 1.5e-04 3.3e-06 1.00e+00 2.536868837e+02 2.536870115e+02 3.1e-11 0.60 83 4.7e-08 1.3e-04 3.0e-06 1.00e+00 2.536868928e+02 2.536870078e+02 2.8e-11 0.60 84 4.2e-08 1.2e-04 2.7e-06 1.00e+00 2.536869010e+02 2.536870045e+02 2.5e-11 0.61 85 3.8e-08 1.1e-04 2.4e-06 1.00e+00 2.536869084e+02 2.536870015e+02 2.2e-11 0.62 86 3.4e-08 9.7e-05 2.2e-06 1.00e+00 2.536869150e+02 2.536869988e+02 2.0e-11 0.62 87 3.1e-08 8.7e-05 2.0e-06 1.00e+00 2.536869210e+02 2.536869964e+02 1.8e-11 0.63 88 2.8e-08 7.8e-05 1.8e-06 9.99e-01 2.536869263e+02 2.536869943e+02 1.6e-11 0.64 89 2.5e-08 7.0e-05 1.6e-06 1.00e+00 2.536869312e+02 2.536869923e+02 1.5e-11 0.65 90 2.2e-08 6.3e-05 1.4e-06 1.00e+00 2.536869355e+02 2.536869905e+02 1.3e-11 0.65 91 2.0e-08 5.7e-05 1.3e-06 1.00e+00 2.536869394e+02 2.536869889e+02 1.2e-11 0.66 92 1.8e-08 5.1e-05 1.2e-06 9.99e-01 2.536869429e+02 2.536869875e+02 1.1e-11 0.67 93 1.6e-08 4.6e-05 1.0e-06 1.00e+00 2.536869461e+02 2.536869862e+02 9.6e-12 0.67 94 1.5e-08 4.2e-05 9.4e-07 1.00e+00 2.536869490e+02 2.536869851e+02 8.6e-12 0.68 95 1.3e-08 3.7e-05 8.5e-07 9.99e-01 2.536869515e+02 2.536869840e+02 7.8e-12 0.69 96 1.2e-08 3.4e-05 7.7e-07 9.98e-01 2.536869538e+02 2.536869831e+02 7.0e-12 0.69 97 1.1e-08 3.0e-05 6.9e-07 9.99e-01 2.536869559e+02 2.536869822e+02 6.3e-12 0.70 Optimizer terminated. Time: 0.70 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 2.5368695593e+02 nrm: 4e+01 Viol. con: 2e-07 var: 0e+00 Dual. obj: 2.5368698225e+02 nrm: 8e+02 Viol. con: 0e+00 var: 2e-04 * End solution on dual form. * Transforming to primal solution. Solving took 0.725 seconds. Using solver 'mosek' Solving for 1748 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'. Number of Hessian non-zeros: 2054 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 471 Eliminator terminated. Eliminator started. Freed constraints in eliminator : 6 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1749 Cones : 0 Scalar variables : 6101 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 870 Optimizer - Cones : 0 Optimizer - Scalar variables : 3453 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.02 Factor - nonzeros before factor : 1.48e+04 after factor : 1.47e+05 Factor - dense dim. : 0 flops : 2.89e+07 Factor - GP saved nzs : 3.32e+04 GP saved flops : 9.06e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.1e+03 1.2e+05 0.00e+00 -1.222298263e+05 2.000000000e+00 1.0e+00 0.04 1 1.6e+03 2.1e+03 8.5e+04 -9.71e-01 -1.213710455e+05 2.752982256e+00 6.9e-01 0.05 2 7.8e+02 1.0e+03 4.2e+04 -9.57e-01 -1.186217467e+05 5.334792787e+00 3.4e-01 0.06 3 2.9e+02 3.9e+02 1.6e+04 -9.11e-01 -1.102259194e+05 2.219994521e+01 1.3e-01 0.06 4 2.9e+02 3.9e+02 1.6e+04 -7.68e-01 -1.083267789e+05 1.672821615e+03 1.3e-01 0.07 5 1.2e+02 1.6e+02 6.6e+03 -7.60e-01 -8.749626988e+04 6.083313951e+03 5.4e-02 0.08 6 3.9e+01 5.3e+01 2.1e+03 -4.56e-01 -4.677954462e+04 1.085256007e+04 1.7e-02 0.08 7 2.3e+01 3.0e+01 1.2e+03 2.29e-01 -3.113771930e+04 7.216008013e+03 1.0e-02 0.09 8 9.3e+00 1.2e+01 5.0e+02 5.24e-01 -1.393505869e+04 3.980814731e+03 4.1e-03 0.10 9 6.0e+00 8.0e+00 3.2e+02 8.27e-01 -9.009823590e+03 2.812604557e+03 2.7e-03 0.11 10 2.1e+00 2.8e+00 1.1e+02 9.04e-01 -3.057301137e+03 1.183564269e+03 9.3e-04 0.12 11 1.4e+00 1.9e+00 7.7e+01 9.76e-01 -1.997372761e+03 9.332543213e+02 6.4e-04 0.12 12 7.4e-01 1.0e+00 4.0e+01 9.81e-01 -9.699632101e+02 5.758019022e+02 3.3e-04 0.13 13 4.2e-01 7.2e-01 2.3e+01 9.89e-01 -4.606257868e+02 4.178451514e+02 1.9e-04 0.14 14 1.6e-01 2.8e-01 8.7e+00 9.97e-01 -6.512326323e+01 2.680538298e+02 7.3e-05 0.15 15 8.8e-02 1.6e-01 4.9e+00 1.00e+00 3.921207159e+01 2.264578862e+02 4.1e-05 0.16 16 3.1e-02 1.2e-01 1.7e+00 1.00e+00 1.252317814e+02 1.912713104e+02 1.5e-05 0.17 17 1.1e-02 9.8e-02 6.5e-01 1.01e+00 1.548024777e+02 1.794850661e+02 5.6e-06 0.18 18 6.0e-03 7.7e-02 3.5e-01 1.01e+00 1.628860752e+02 1.761840348e+02 3.0e-06 0.18 19 1.1e-03 1.5e-01 6.8e-02 1.01e+00 1.705511844e+02 1.731209203e+02 6.1e-07 0.19 20 4.2e-04 1.1e-01 2.6e-02 1.01e+00 1.716970465e+02 1.726831638e+02 2.4e-07 0.20 21 1.8e-04 9.1e-02 1.1e-02 1.00e+00 1.721010799e+02 1.725269096e+02 1.0e-07 0.21 22 1.0e-04 7.2e-02 6.3e-03 1.00e+00 1.722342738e+02 1.724717849e+02 5.7e-08 0.22 23 9.0e-05 6.5e-02 5.6e-03 1.00e+00 1.722520170e+02 1.724658133e+02 5.1e-08 0.22 24 8.1e-05 6.0e-02 5.1e-03 1.00e+00 1.722673117e+02 1.724597216e+02 4.6e-08 0.23 25 7.3e-05 5.5e-02 4.6e-03 1.00e+00 1.722811705e+02 1.724543346e+02 4.2e-08 0.24 26 6.6e-05 5.0e-02 4.1e-03 1.00e+00 1.722936134e+02 1.724494569e+02 3.7e-08 0.25 27 5.9e-05 4.6e-02 3.7e-03 1.00e+00 1.723047998e+02 1.724450554e+02 3.4e-08 0.26 28 5.3e-05 4.2e-02 3.3e-03 1.00e+00 1.723148518e+02 1.724410789e+02 3.0e-08 0.26 29 4.8e-05 3.9e-02 3.0e-03 1.00e+00 1.723238843e+02 1.724374861e+02 2.7e-08 0.27 30 4.3e-05 3.6e-02 2.7e-03 1.00e+00 1.723320001e+02 1.724342397e+02 2.5e-08 0.28 31 3.9e-05 3.3e-02 2.4e-03 1.00e+00 1.723392924e+02 1.724313064e+02 2.2e-08 0.29 32 3.5e-05 3.0e-02 2.2e-03 1.00e+00 1.723458452e+02 1.724286563e+02 2.0e-08 0.30 33 3.1e-05 2.8e-02 2.0e-03 1.00e+00 1.723517339e+02 1.724262629e+02 1.8e-08 0.31 34 2.8e-05 2.6e-02 1.8e-03 1.00e+00 1.723570267e+02 1.724241018e+02 1.6e-08 0.32 35 2.5e-05 2.4e-02 1.6e-03 1.00e+00 1.723617843e+02 1.724221513e+02 1.5e-08 0.33 36 2.3e-05 2.3e-02 1.4e-03 1.00e+00 1.723660614e+02 1.724203911e+02 1.3e-08 0.34 37 2.1e-05 2.1e-02 1.3e-03 1.00e+00 1.723699069e+02 1.724188032e+02 1.2e-08 0.34 38 1.9e-05 2.0e-02 1.2e-03 1.00e+00 1.723733647e+02 1.724173710e+02 1.1e-08 0.35 39 1.7e-05 1.9e-02 1.0e-03 1.00e+00 1.723764740e+02 1.724160795e+02 9.5e-09 0.36 40 1.5e-05 1.8e-02 9.4e-04 1.00e+00 1.723792702e+02 1.724149150e+02 8.6e-09 0.37 41 1.4e-05 1.7e-02 8.5e-04 1.00e+00 1.723817850e+02 1.724138651e+02 7.7e-09 0.37 42 1.2e-05 1.6e-02 7.6e-04 1.00e+00 1.723840467e+02 1.724129188e+02 6.9e-09 0.38 43 1.1e-05 1.5e-02 6.9e-04 1.00e+00 1.723860810e+02 1.724120658e+02 6.2e-09 0.39 44 9.9e-06 1.4e-02 6.2e-04 1.00e+00 1.723879108e+02 1.724112971e+02 5.6e-09 0.40 45 8.9e-06 1.4e-02 5.6e-04 1.00e+00 1.723895567e+02 1.724106044e+02 5.1e-09 0.40 46 8.0e-06 1.3e-02 5.0e-04 1.00e+00 1.723910373e+02 1.724099802e+02 4.6e-09 0.41 47 7.2e-06 1.3e-02 4.5e-04 1.00e+00 1.723923692e+02 1.724094178e+02 4.1e-09 0.42 48 6.5e-06 1.2e-02 4.1e-04 1.00e+00 1.723935674e+02 1.724089112e+02 3.7e-09 0.43 49 5.8e-06 1.2e-02 3.6e-04 1.00e+00 1.723946453e+02 1.724084548e+02 3.3e-09 0.44 50 5.2e-06 1.1e-02 3.3e-04 1.00e+00 1.723956151e+02 1.724080436e+02 3.0e-09 0.45 51 4.7e-06 1.1e-02 3.0e-04 1.00e+00 1.723964875e+02 1.724076733e+02 2.7e-09 0.45 52 4.2e-06 1.1e-02 2.7e-04 1.00e+00 1.723972725e+02 1.724073397e+02 2.4e-09 0.46 53 3.8e-06 1.0e-02 2.4e-04 1.00e+00 1.723979788e+02 1.724070393e+02 2.2e-09 0.47 54 3.4e-06 1.0e-02 2.2e-04 1.00e+00 1.723986142e+02 1.724067687e+02 2.0e-09 0.48 55 3.1e-06 9.9e-03 1.9e-04 1.00e+00 1.723991860e+02 1.724065251e+02 1.8e-09 0.48 56 2.8e-06 9.7e-03 1.7e-04 1.00e+00 1.723997005e+02 1.724063056e+02 1.6e-09 0.49 57 2.5e-06 9.5e-03 1.6e-04 1.00e+00 1.724001634e+02 1.724061080e+02 1.4e-09 0.50 58 2.3e-06 9.3e-03 1.4e-04 1.00e+00 1.724005799e+02 1.724059301e+02 1.3e-09 0.51 59 2.0e-06 9.2e-03 1.3e-04 1.00e+00 1.724009547e+02 1.724057699e+02 1.2e-09 0.51 60 1.8e-06 9.0e-03 1.1e-04 1.00e+00 1.724012919e+02 1.724056257e+02 1.0e-09 0.52 61 1.6e-06 8.9e-03 1.0e-04 1.00e+00 1.724015954e+02 1.724054958e+02 9.4e-10 0.53 62 1.5e-06 8.8e-03 9.3e-05 1.00e+00 1.724018684e+02 1.724053788e+02 8.4e-10 0.54 63 1.3e-06 8.7e-03 8.4e-05 1.00e+00 1.724021142e+02 1.724052735e+02 7.6e-10 0.55 64 1.2e-06 8.6e-03 7.5e-05 1.00e+00 1.724023353e+02 1.724051787e+02 6.8e-10 0.55 65 1.1e-06 8.5e-03 6.8e-05 1.00e+00 1.724025342e+02 1.724050933e+02 6.2e-10 0.56 66 9.7e-07 8.4e-03 6.1e-05 1.00e+00 1.724027133e+02 1.724050165e+02 5.5e-10 0.57 67 8.7e-07 8.3e-03 5.5e-05 1.00e+00 1.724028744e+02 1.724049473e+02 5.0e-10 0.58 68 7.9e-07 8.3e-03 4.9e-05 1.00e+00 1.724030194e+02 1.724048850e+02 4.5e-10 0.59 69 7.1e-07 8.2e-03 4.4e-05 1.00e+00 1.724031498e+02 1.724048289e+02 4.0e-10 0.59 70 6.4e-07 8.1e-03 4.0e-05 1.00e+00 1.724032672e+02 1.724047784e+02 3.6e-10 0.60 71 5.7e-07 8.1e-03 3.6e-05 1.00e+00 1.724033729e+02 1.724047329e+02 3.3e-10 0.61 72 5.2e-07 8.0e-03 3.2e-05 1.00e+00 1.724034679e+02 1.724046920e+02 2.9e-10 0.62 73 4.6e-07 8.0e-03 2.9e-05 1.00e+00 1.724035535e+02 1.724046551e+02 2.7e-10 0.63 74 4.2e-07 7.9e-03 2.6e-05 1.00e+00 1.724036305e+02 1.724046220e+02 2.4e-10 0.64 75 3.8e-07 7.9e-03 2.4e-05 1.00e+00 1.724036997e+02 1.724045921e+02 2.1e-10 0.64 76 3.4e-07 7.9e-03 2.1e-05 1.00e+00 1.724037621e+02 1.724045652e+02 1.9e-10 0.65 77 3.1e-07 7.8e-03 1.9e-05 1.00e+00 1.724038182e+02 1.724045410e+02 1.7e-10 0.66 78 2.7e-07 7.8e-03 1.7e-05 1.00e+00 1.724038687e+02 1.724045192e+02 1.6e-10 0.67 79 2.5e-07 7.8e-03 1.5e-05 1.00e+00 1.724039141e+02 1.724044996e+02 1.4e-10 0.68 80 2.2e-07 7.7e-03 1.4e-05 1.00e+00 1.724039550e+02 1.724044819e+02 1.3e-10 0.69 81 2.0e-07 7.7e-03 1.3e-05 1.00e+00 1.724039918e+02 1.724044660e+02 1.1e-10 0.70 82 1.8e-07 7.7e-03 1.1e-05 1.00e+00 1.72E ====================================================================== ERROR [24.768s]: test_SPaircraft_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 40, in test_fn mod.test() File "SPaircraft.py", line 87, in test sol = optimize_aircraft(m, substitutions, fixedBPR, pRatOpt, mutategparg) File "SPaircraft.py", line 62, in optimize_aircraft sol = m_relax.localsolve(verbosity=4, iteration_limit=200, reltol=0.01, mutategp=mutategparg, x0 = x0) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/constraints/prog_factories.py", line 124, in solvefn result = progsolve(solver, verbosity, **kwargs) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/constraints/sgp.py", line 149, in localsolve feas_constrs, None) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/constraints/gp.py", line 112, in __init__ + boundstrs) ValueError: Geometric Program is not fully bounded: Mission1.Aircraft.Engine.EngineConstants.Relax1.R has no lower bound Mission1.Aircraft.Engine.EngineConstants.Relax1.g has no lower bound ---------------------------------------------------------------------- Ran 1 test in 24.768s FAILED (errors=1) Generating XML reports... 4040249e+02 1.724044517e+02 1.0e-10 0.71 83 1.6e-07 7.7e-03 1.0e-05 1.00e+00 1.724040546e+02 1.724044388e+02 9.2e-11 0.72 84 1.5e-07 7.7e-03 9.1e-06 1.00e+00 1.724040815e+02 1.724044272e+02 8.3e-11 0.73 85 1.3e-07 7.6e-03 8.2e-06 1.00e+00 1.724041056e+02 1.724044167e+02 7.5e-11 0.74 86 1.2e-07 7.6e-03 7.4e-06 1.00e+00 1.724041273e+02 1.724044073e+02 6.7e-11 0.75 87 1.1e-07 7.6e-03 6.7e-06 1.00e+00 1.724041470e+02 1.724043988e+02 6.1e-11 0.75 88 9.6e-08 7.6e-03 6.0e-06 1.00e+00 1.724041646e+02 1.724043912e+02 5.5e-11 0.76 89 8.6e-08 7.6e-03 5.4e-06 1.00e+00 1.724041804e+02 1.724043843e+02 4.9e-11 0.77 90 7.8e-08 7.6e-03 4.9e-06 9.97e-01 1.724041946e+02 1.724043781e+02 4.4e-11 0.78 91 7.0e-08 7.5e-03 4.4e-06 1.00e+00 1.724042074e+02 1.724043726e+02 4.0e-11 0.79 92 6.3e-08 7.5e-03 3.9e-06 9.99e-01 1.724042189e+02 1.724043676e+02 3.6e-11 0.80 93 5.7e-08 6.8e-03 3.5e-06 1.02e+00 1.724042300e+02 1.724043628e+02 3.3e-11 0.81 94 5.1e-08 6.1e-03 3.2e-06 1.01e+00 1.724042398e+02 1.724043585e+02 2.9e-11 0.82 95 4.6e-08 5.5e-03 2.9e-06 1.01e+00 1.724042484e+02 1.724043549e+02 2.7e-11 0.83 96 4.2e-08 4.9e-03 2.6e-06 1.02e+00 1.724042564e+02 1.724043515e+02 2.4e-11 0.84 97 3.8e-08 4.4e-03 2.3e-06 9.97e-01 1.724042630e+02 1.724043486e+02 2.2e-11 0.85 98 3.4e-08 4.0e-03 2.1e-06 9.95e-01 1.724042689e+02 1.724043460e+02 2.0e-11 0.86 99 3.1e-08 3.6e-03 1.9e-06 9.91e-01 1.724042743e+02 1.724043436e+02 1.8e-11 0.86 100 2.8e-08 3.2e-03 1.7e-06 9.09e-01 1.724042791e+02 1.724043415e+02 1.6e-11 0.87 101 3.9e-08 7.7e-04 4.0e-07 1.00e+00 1.724043125e+02 1.724043276e+02 4.0e-12 0.88 102 1.1e-07 6.9e-04 3.6e-07 -7.72e-01 1.724043128e+02 1.724043312e+02 3.4e-12 0.89 103 1.1e-07 6.9e-04 3.6e-07 -3.73e+00 1.724043128e+02 1.724043312e+02 3.4e-12 0.90 Optimizer terminated. Time: 0.91 solsta = 7, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : NEAR_OPTIMAL Primal. obj: 1.7240431284e+02 nrm: 4e+01 Viol. con: 3e-06 var: 0e+00 Dual. obj: 1.7240433117e+02 nrm: 8e+02 Viol. con: 0e+00 var: 7e-03 * End solution on dual form. * Transforming to primal solution. Solving took 0.931 seconds. Cloning into 'solar'... DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2) Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.8.0) Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2019.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0) DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-LDdnh5 Running command git clone -q https://github.com/convexengineering/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-LDdnh5 Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.5) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gpfit==0.1) (0.9.1.0) Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2) Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3) Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.12.0) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2) Building wheels for collected packages: gpfit Building wheel for gpfit (setup.py): started Building wheel for gpfit (setup.py): finished with status 'done' Created wheel for gpfit: filename=gpfit-0.1-cp27-none-any.whl size=25151 sha256=a56cf1dee449751dc1cf78981e9adeca39c41072f0b972327237ab3afc150ddb Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-MH9fC2/wheels/d5/94/ac/b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12 Successfully built gpfit DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting git+https://github.com/convexengineering/gassolar.git Cloning https://github.com/convexengineering/gassolar.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-uhJojs Running command git clone -q https://github.com/convexengineering/gassolar.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-uhJojs 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_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.16.5) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.2.2) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.9.1.0) Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.24.2) Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.9) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.2.3) Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.12.0) Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.8.0) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2019.2) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gassolar==0.0.0.0) (1.0.2) Building wheels for collected packages: gassolar Building wheel for gassolar (setup.py): started Building wheel for gassolar (setup.py): finished with status 'done' Created wheel for gassolar: filename=gassolar-0.0.0.0-cp27-none-any.whl size=4876517 sha256=580fc020ea74a5316a6bb39163d7a63f29ffc6100341291de3a48245825c2d98 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-xXmbGU/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e Successfully built gassolar DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Processing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/solar Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.16.5) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.2.2) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from solar==0.0.0.0) (0.9.1.0) Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.24.2) Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.1) Requirement already satisfied: gpkitmodels in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary (from solar==0.0.0.0) (0.0.0.0) Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (0.9) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.3.2) Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.2.3) Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.12.0) Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2.8.0) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2019.2) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->solar==0.0.0.0) (1.0.2) Building wheels for collected packages: solar Building wheel for solar (setup.py): started Building wheel for solar (setup.py): finished with status 'done' Created wheel for solar: filename=solar-0.0.0.0-cp27-none-any.whl size=14811 sha256=e3ba3974d2eda5459901970fd9ae442a03afb896b958ed85e5c747c3194be67d Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-Jcrvjv/wheels/55/91/84/60653f7cb392791f8ec648fb5ef240c78233b7566d69a6c92c Successfully built solar Installing collected packages: solar Successfully installed solar-0.0.0.0 Running tests... ---------------------------------------------------------------------- EEEEEE ====================================================================== ERROR [0.120s]: test_solar_npod_trade_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 40, in test_fn mod.test() File "npod_trade.py", line 91, in test File "npod_trade.py", line 16, in pods File "solar.py", line 14, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.002s]: test_solar_npod_trade_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 40, in test_fn mod.test() File "npod_trade.py", line 91, in test File "npod_trade.py", line 16, in pods File "solar.py", line 14, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.003s]: test_solar_season_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "season.py", line 6, in <module> File "solar.py", line 14, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.002s]: test_solar_season_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "season.py", line 6, in <module> File "solar.py", line 14, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.004s]: test_solar_sens_chart_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "sens_chart.py", line 7, in <module> File "solar.py", line 14, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.002s]: test_solar_sens_chart_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "sens_chart.py", line 7, in <module> File "solar.py", line 14, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ---------------------------------------------------------------------- Ran 6 tests in 0.133s FAILED (errors=6) Generating XML reports... adding test for 'solar/sens_chart.py' adding test for 'solar/season.py' adding test for 'solar/npod_trade.py' N=1 N=1 fatal: destination path 'gplibrary' already exists and is not an empty directory. fatal: destination path 'gplibrary' already exists and is not an empty directory. fatal: destination path 'gplibrary' already exists and is not an empty directory. fatal: destination path 'gplibrary' already exists and is not an empty directory. fatal: destination path 'gplibrary' already exists and is not an empty directory. DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2) Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.8.0) Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5) Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2019.2) Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0) DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-mc3J0t Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-mc3J0t Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.5) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2) Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gpfit==0.1) (0.9.1.0) Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9) Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2) Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3) Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.12.0) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2) Building wheels for collected packages: gpfit Building wheel for gpfit (setup.py): started Building wheel for gpfit (setup.py): finished with status 'done' Created wheel for gpfit: filename=gpfit-0.1-cp27-none-any.whl size=25151 sha256=f4f02f77304ff108cb6381aacb906242d31320fda52faad49cdc713c769e9cf0 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-eVoPEH/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support Processing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary Requirement already satisfied: numpy>=1.12 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.16.5) Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.2.2) Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.9) Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint->gpkitmodels==0.0.0.0) (1.0.2) Building wheels for collected packages: gpkitmodels Building wheel for gpkitmodels (setup.py): started Building wheel for gpkitmodels (setup.py): finished with status 'done' Created wheel for gpkitmodels: filename=gpkitmodels-0.0.0.0-cp27-none-any.whl size=65697 sha256=ae86bca306de8e7ef6015a28fd030d3b27e1724266158d193872fba358a6c515 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-fSgLb5/wheels/ab/79/3c/c09e2173989dc969f23a5e4c34887060b900152ee1d8be6e1c Successfully built gpkitmodels Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Successfully installed gpkitmodels-0.0.0.0 Running tests... ---------------------------------------------------------------------- EEEEEEEEEE...... ====================================================================== ERROR [0.003s]: test_gpkitmodels_GP_aircraft_fuselage_test_fuselage_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "test_fuselage.py", line 2, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/fuselage/elliptical_fuselage.py", line 4, in <module> from gpkitmodels.GP.materials import cfrpfabric File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.002s]: test_gpkitmodels_GP_aircraft_fuselage_test_fuselage_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "test_fuselage.py", line 2, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/fuselage/elliptical_fuselage.py", line 4, in <module> from gpkitmodels.GP.materials import cfrpfabric File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.004s]: test_gpkitmodels_GP_aircraft_motor_motor_test_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "motor_test.py", line 2, in <module> File "motor.py", line 4, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/prop/propeller.py", line 9, in <module> class ActuatorProp(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/prop/propeller.py", line 36, in ActuatorProp @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.001s]: test_gpkitmodels_GP_aircraft_motor_motor_test_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "motor_test.py", line 2, in <module> File "motor.py", line 4, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/prop/propeller.py", line 9, in <module> class ActuatorProp(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/prop/propeller.py", line 36, in ActuatorProp @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.001s]: test_gpkitmodels_GP_aircraft_prop_prop_test_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "prop_test.py", line 2, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/prop/propeller.py", line 9, in <module> class ActuatorProp(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/prop/propeller.py", line 36, in ActuatorProp @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.001s]: test_gpkitmodels_GP_aircraft_prop_prop_test_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "prop_test.py", line 2, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/prop/propeller.py", line 9, in <module> class ActuatorProp(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/prop/propeller.py", line 36, in ActuatorProp @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.002s]: test_gpkitmodels_GP_aircraft_tail_tail_tests_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "tail_tests.py", line 2, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/tail/horizontal_tail.py", line 4, in <module> from .tail_aero import TailAero File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/tail/tail_aero.py", line 10, in <module> class TailAero(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/tail/tail_aero.py", line 31, in TailAero @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.001s]: test_gpkitmodels_GP_aircraft_tail_tail_tests_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "tail_tests.py", line 2, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/tail/horizontal_tail.py", line 4, in <module> from .tail_aero import TailAero File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/tail/tail_aero.py", line 10, in <module> class TailAero(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/tail/tail_aero.py", line 31, in TailAero @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.002s]: test_gpkitmodels_GP_aircraft_wing_wing_test_py_mosek (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "wing_test.py", line 2, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ====================================================================== ERROR [0.001s]: test_gpkitmodels_GP_aircraft_wing_wing_test_py_mosek_cli (gpkit.tests.from_paths.TestFiles) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn mod = __import__(os.path.basename(path)[:-3]) File "wing_test.py", line 2, in <module> File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/wing/wing.py", line 7, in <module> from .wing_core import WingCore File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/aircraft/wing/wing_core.py", line 3, in <module> from gpkitmodels.GP.materials import foamhd File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/__init__.py", line 1, in <module> from composite import CFRPFabric, CFRPUD, Kevlar File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/composite.py", line 3, in <module> class CFRPFabric(Model): File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gpkitmodels/GP/materials/composite.py", line 22, in CFRPFabric @parse_variables(__doc__, globals()) TypeError: 'str' object is not callable ---------------------------------------------------------------------- Ran 16 tests in 2.759s FAILED (errors=10) Generating XML reports... adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py' adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py' adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py' adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py' adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py' adding test for 'gpkitmodels/SP/SimPleAC/SimPleAC.py' adding test for 'gpkitmodels/SP/SimPleAC/SimPleAC_mission.py' adding test for 'gpkitmodels/SP/SimPleAC/SimPleAC_multimission.py' SP is not converging! Last GP iteration had a higher cost (3e+03) than the previous one (2.7e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again. SP is not converging! Last GP iteration had a higher cost (3e+03) than the previous one (2.7e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again. SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (3.4e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again. SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again. SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again. SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (3.4e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again. SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again. SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again. Beginning signomial solve. Using solver 'mosek' Solving for 20 variables. Solving took 0.0105 seconds. Using solver 'mosek' Solving for 20 variables. Solving took 0.0126 seconds. Using solver 'mosek' Solving for 20 variables. Solving took 0.0124 seconds. Using solver 'mosek' Solving for 20 variables. Solving took 0.0122 seconds. Solving took 4 GP solves and 0.0534 seconds. Beginning signomial solve. Using solver 'mosek_cli' Solving for 20 variables. Solving took 0.0412 seconds. Using solver 'mosek_cli' Solving for 20 variables. Solving took 0.0411 seconds. Using solver 'mosek_cli' Solving for 20 variables. Solving took 0.038 seconds. Using solver 'mosek_cli' Solving for 20 variables. Solving took 0.038 seconds. Solving took 4 GP solves and 0.18 seconds. Cloning into 'eVTOL'... Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 3.774s OK Generating XML reports... adding test for 'models/model_tests.py' Found no installed solvers, beginning a build. # Moving to the directory from which GPkit was imported. Started building gpkit... Attempting to find and build solvers: # Looking for mosek # Found /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h # Found /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib # Found /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.c # Found /Users/jenkins/mosek/8/tools/examples/c/expopt.c # Found /Users/jenkins/mosek/8/tools/examples/c/dgopt.c # Found /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.h # Found /Users/jenkins/mosek/8/tools/examples/c/expopt.h # Found /Users/jenkins/mosek/8/tools/examples/c/dgopt.h # Found /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h # Found mosek version 8, installed to /Users/jenkins/mosek # # Building mosek... # Replacing directory _mosek/lib # Replacing directory _mosek/build # Replacing directory /Users/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit # # Copying expopt library files to _mosek/build # Copying /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.c # Copying /Users/jenkins/mosek/8/tools/examples/c/expopt.c # Copying /Users/jenkins/mosek/8/tools/examples/c/dgopt.c # Copying /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.h # Copying /Users/jenkins/mosek/8/tools/examples/c/expopt.h # Copying /Users/jenkins/mosek/8/tools/examples/c/dgopt.h # Copying /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h # # Applying expopt patches... # # Change in _mosek/build/dgopt.con line 651 # -- printf("Number of Hessian non-zeros: %d\n",nlh[0]->numhesnz); # ++ MSK_echotask(task,MSK_STREAM_MSG,"Number of Hessian non-zeros: %d\n",n # # Change in _mosek/build/expopt.con line 566 # -- printf("Warning: The variable with index '%d' has only positiv # ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in # # Change in _mosek/build/expopt.con line 579 # -- printf("Warning: The variable with index '%d' has only negativ # ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in # # Change in _mosek/build/expopt.con line 1115 # -- printf ("solsta = %d, prosta = %d\n", (int)*solsta,(int)*prosta); # ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "solsta = %d, prosta = %d\n", # # Building expopt library... # Calling 'gcc -fpic -shared -Wl,-rpath "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin" _mosek/build/scopt-ext.c _mosek/build/expopt.c _mosek/build/dgopt.c "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib" -o /Users/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit/expopt.so' ## ### CALL BEGINS ### CALL ENDS ## # Calling 'install_name_tool -change libmosek64.8.1.dylib /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib /Users/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit/expopt.so' ## ### CALL BEGINS ### CALL ENDS ## # Calling 'install_name_tool -change libmosek64.8.1.dylib @executable_path/libmosek64.8.1.dylib /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/mskexpopt' ## ### CALL BEGINS ### CALL ENDS ## # # Building Python bindings for expopt and Mosek... # (if this fails on Windows, verify the mingw version) # Calling 'python modified_ctypesgen.py -a -l /Users/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit/expopt.so -l "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib" -o _mosek/lib/expopt_h.py _mosek/build/expopt.h' ## ### CALL BEGINS ### CALL ENDS ## # Done building mosek # Looking for mosek_cli # Trying to run mskexpopt... # Calling 'mskexpopt' ## ### CALL BEGINS ### CALL ENDS ## # Found mosek_cli in system path # Looking for cvxopt # Trying to import cvxopt... # Found cvxopt in Python path ...finished building gpkit. Replaced found solvers ([u'mosek', u'mosek_cli', u'cvxopt']) with environment var GPKITSOLVERS (mosek, mosek_cli) Found the following solvers: mosek, mosek_cli # Replacing directory env x[:] <= w GPkit is now installed with solver(s) [u'mosek', u'mosek_cli'] To incorporate new solvers at a later date, run `gpkit.build()`. If any tests didn't pass, please post the output above (starting from "Found no installed solvers, beginning a build.") to gpkit@mit.edu or https://github.com/convexengineering/gpkit/issues/new so we can prevent others from having these errors. The same goes for any other bugs you encounter with GPkit: send 'em our way, along with any interesting models, speculative features, comments, discussions, or clarifications you feel like sharing. Finally, we hope you find our documentation (https://gpkit.readthedocs.io/) and engineering-design models (https://github.com/convexengineering/gplibrary/) to be useful resources for your own applications. Enjoy! calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gplibrary'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/robust.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] 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_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] 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_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git'] attempt 1 attempt 2 attempt 3 attempt 4 attempt 5 SETTINGS defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'}) calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) [Execution node] check if [macys] 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 INFO: Starting to record. INFO: Processing JUnit INFO: [JUnit] - 9 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/Users/jenkins/workspace/gplibrary_Push_Models/mosek' for the testing framework 'JUnit'. INFO: Check 'Failed Tests' threshold. INFO: Check 'Skipped Tests' threshold. INFO: Setting the build status to FAILURE INFO: Stopping recording. [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... [WS-CLEANUP] done Finished: FAILURE