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Started by upstream project "gplibrary_Push_Models" build number 186 originally caused by: Started by upstream project "gpkit_Push" build number 653 originally caused by: Started by GitHub push by bqpd 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 62fd801e15375d0c0a052852b3f9d7633674eda8 (origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f 62fd801e15375d0c0a052852b3f9d7633674eda8 # timeout=3 Commit message: "SimPleAC update (new model that doesn't solve on cvxopt) (#175)" > git rev-list --no-walk 62fd801e15375d0c0a052852b3f9d7633674eda8 # 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/jenkins10827125528791095570.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/8f/0b/1a2c21bb69138337dc079841aa4a45e5b2fc7a4260c0907f5254fb08f02e/numpy-1.16.4-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 Installing collected packages: numpy Successfully installed numpy-1.16.4 + 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) (1.16.4) 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) (1.16.4) 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) (1.16.4) 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 + 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__' 1.16.4 + 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) (1.16.4) 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) (1.16.4) 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 18.381s 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 'shopping'... Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 0.226s OK Generating XML reports... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.0171 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.0155 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.0434 seconds. Cloning into 'gassolar'... 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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) (1.16.4) 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-iBRcqX Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-iBRcqX Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.4) 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=1910e58018c0ef0db1a6dd3bfc00b05888ac37f0c2bc037ee6fc6c9ebec62c8e Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-H7FXOO/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) (1.16.4) 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=c4c6bb230be4ff50fbcb0b533c1b44a020430618377365eda8a495abaaf2a1a5 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-ndPYX6/wheels/41/0a/8d/447392359ea0dc499510d6781d4893f34e301ac2b844c7bed4 Successfully built gassolar Installing collected packages: gassolar Successfully installed gassolar-0.0.0.0 Running tests... ---------------------------------------------------------------------- /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped. warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning) ../Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 4 tests in 22.426s OK Generating XML reports... adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 592 variables. Solving took 0.0786 seconds. Warning: Variable Mission.Climb.FlightSegment.AircraftPerf.EnginePerf.P_{total}[:]/Mission.Climb.FlightSegment.Aircraf could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Beginning signomial solve. Solving took 4 GP solves and 0.473 seconds. Warning: Variable Mission1.Climb.FlightSegment.AircraftPerf.EnginePerf.P_{total}[:]/Mission1.Climb.FlightSegment.Aircr could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 592 variables. Solving took 0.0821 seconds. Warning: Variable Mission.Climb.FlightSegment.AircraftPerf.EnginePerf.P_{total}[:]/Mission.Climb.FlightSegment.Aircraf could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Beginning signomial solve. Solving took 4 GP solves and 0.55 seconds. Warning: Variable Mission1.Climb.FlightSegment.AircraftPerf.EnginePerf.P_{total}[:]/Mission1.Climb.FlightSegment.Aircr could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 1250 variables. Solving took 0.333 seconds. Warning: Variable Mission.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.3538 but bound is 150000.0000 Warning: Variable Mission.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.3827 but bound is 150000.0000 Beginning signomial solve. Solving took 4 GP solves and 1.68 seconds. Warning: Variable Mission1.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103379.4301 but bound is 150000.0000 Warning: Variable Mission1.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103406.0835 but bound is 150000.0000 Using solver 'mosek_cli' Solving for 1250 variables. Solving took 0.432 seconds. Warning: Variable Mission.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.6388 but bound is 150000.0000 Warning: Variable Mission.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.6388 but bound is 150000.0000 Beginning signomial solve. Solving took 4 GP solves and 2.13 seconds. Warning: Variable Mission1.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103379.2971 but bound is 150000.0000 Warning: Variable Mission1.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103406.1793 but bound is 150000.0000 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) (1.16.4) 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-yTEAuj Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-yTEAuj 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) (1.16.4) 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=3fc019ccd58c6bad98cf87bb3c0b3170e02a9b90de93c4048249eb9eb6af6bcf Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-ufPnMe/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Running tests... ---------------------------------------------------------------------- /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped. warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning) .... ---------------------------------------------------------------------- Ran 4 tests in 24.940s OK Generating XML reports... adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -1.2566195913693567e-13. Solving took 4 GP solves and 1.11 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.269612e-13. Solving took 4 GP solves and 1.93 seconds. Allowing negative dual variable(s) as small as -6.193960275235888e-13. Allowing negative dual variable(s) as small as -1.3846424549469882e-13. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.829 speed at top of climb [m/s] = 26.626 design loiter speed [m/s] = 25.071 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -1.3846424549469882e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.356 optimum loiter speed for min power, end of loiter [m/s] = 25.000 optimum cruise speed, inbound [m/s] = 25.637 optimum cruise speed, outbound [m/s] = 36.421 Beginning signomial solve. Allowing negative dual variable(s) as small as -7.171202259721421e-12. Solving took 4 GP solves and 1.24 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 0.758 seconds. Max payload weight [lbf] = 28.242 Max take off weight [lbf] = 166.638 Allowing negative dual variable(s) as small as -6.188938e-13. Allowing negative dual variable(s) as small as -1.385335e-13. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.829 speed at top of climb [m/s] = 26.626 design loiter speed [m/s] = 25.071 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -1.385335e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.356 optimum loiter speed for min power, end of loiter [m/s] = 25.000 optimum cruise speed, inbound [m/s] = 25.637 optimum cruise speed, outbound [m/s] = 36.421 Beginning signomial solve. Allowing negative dual variable(s) as small as -7.171066e-12. Solving took 4 GP solves and 1.77 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.48 seconds. Max payload weight [lbf] = 28.242 Max take off weight [lbf] = 166.638 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) (1.16.4) 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) Collecting future (from turbofan==0.0.0.0) 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==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=45067 sha256=84e69b4a6cfa40760c44d218737c1fd820308bf4e860237e09d54f4526f4df4a Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-udFt4v/wheels/b5/2f/48/b751d4bab5d719a7de0cd9181de34b2f4449cb2da5aec6f23d Successfully built turbofan Installing collected packages: future, turbofan Successfully installed future-0.17.1 turbofan-0.0.0.0 Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 1.290s OK Generating XML reports... adding test for 'turbofan/engine_test.py' Beginning signomial solve. Using solver 'mosek' Solving for 335 variables. Solving took 0.0441 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.0337 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.0375 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.0354 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.0291 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.0307 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.0399 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.0341 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.0321 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.029 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.032 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.0317 seconds. Using solver 'mosek' Solving for 335 variables. Solving took 0.0313 seconds. Solving took 13 GP solves and 0.886 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-cNA2Ki Running command git clone -q https://github.com/hoburg/turbofan.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-cNA2Ki 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) (1.16.4) 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=45067 sha256=d94b738b0217cafe62d8adc566d82d2e4e521a09251987339d38a430d85f8fc2 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-BuiPG0/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) (1.16.4) 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=951bf091f43ff9639074a405af20779b7951ee0d4b835ccf71aca5cb637a5f31 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-qrnFhN/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}[:]/dum[:])^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}[:]/dum[:])^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 1768 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 482 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: 0.02 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 872 Optimizer - Cones : 0 Optimizer - Scalar variables : 3460 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 : 1.49e+04 after factor : 1.57e+05 Factor - dense dim. : 0 flops : 3.24e+07 Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.226649102e+05 2.000000000e+00 1.0e+00 0.05 1 1.6e+03 2.1e+03 8.5e+04 -9.71e-01 -1.217931396e+05 2.767433271e+00 6.9e-01 0.06 2 8.3e+02 1.1e+03 4.5e+04 -9.57e-01 -1.193765364e+05 5.044398797e+00 3.7e-01 0.08 3 2.9e+02 3.8e+02 1.6e+04 -9.17e-01 -1.106126807e+05 2.145823832e+01 1.3e-01 0.09 4 2.9e+02 3.8e+02 1.6e+04 -7.69e-01 -1.086003128e+05 1.772606687e+03 1.3e-01 0.10 5 1.1e+02 1.5e+02 6.0e+03 -7.60e-01 -8.493681606e+04 6.771650949e+03 4.9e-02 0.11 6 3.8e+01 5.0e+01 2.0e+03 -4.14e-01 -4.581119560e+04 1.071049050e+04 1.7e-02 0.12 7 2.0e+01 2.7e+01 1.1e+03 2.49e-01 -2.861440868e+04 7.031559683e+03 9.0e-03 0.13 8 9.3e+00 1.2e+01 5.0e+02 5.69e-01 -1.393983792e+04 4.245067693e+03 4.1e-03 0.14 9 4.7e+00 6.2e+00 2.6e+02 8.28e-01 -7.029110973e+03 2.527640603e+03 2.1e-03 0.15 10 1.4e+00 1.9e+00 7.7e+01 9.33e-01 -1.989522428e+03 9.440658307e+02 6.4e-04 0.16 11 6.4e-01 8.4e-01 3.5e+01 9.94e-01 -6.816062939e+02 6.602366188e+02 2.9e-04 0.18 12 4.8e-01 6.4e-01 2.6e+01 9.96e-01 -4.529918475e+02 5.592351333e+02 2.2e-04 0.19 13 3.5e-01 7.7e-01 1.9e+01 9.80e-01 -2.692234810e+02 4.765662154e+02 1.6e-04 0.20 14 1.7e-01 3.9e-01 9.5e+00 9.97e-01 -1.714746558e+00 3.652438284e+02 8.0e-05 0.21 15 5.6e-02 1.6e-01 3.2e+00 9.94e-01 1.676373028e+02 2.901745152e+02 2.7e-05 0.23 16 3.3e-02 1.4e-01 1.9e+00 1.00e+00 2.029391613e+02 2.746337593e+02 1.6e-05 0.24 17 5.1e-03 1.9e-01 3.2e-01 1.00e+00 2.450791195e+02 2.572416758e+02 2.8e-06 0.25 18 1.5e-03 1.3e-01 9.3e-02 1.00e+00 2.511104204e+02 2.546939126e+02 8.5e-07 0.26 19 4.9e-04 1.1e-01 3.1e-02 1.00e+00 2.528349632e+02 2.540244727e+02 2.8e-07 0.27 20 2.1e-04 8.8e-02 1.3e-02 1.00e+00 2.533186201e+02 2.538333673e+02 1.2e-07 0.29 21 1.9e-04 8.0e-02 1.2e-02 1.00e+00 2.533566246e+02 2.538199075e+02 1.1e-07 0.30 22 1.7e-04 7.3e-02 1.1e-02 1.00e+00 2.533897565e+02 2.538066870e+02 1.0e-07 0.31 23 1.5e-04 6.6e-02 9.8e-03 1.00e+00 2.534196107e+02 2.537948321e+02 9.0e-08 0.33 24 1.4e-04 6.0e-02 8.8e-03 1.00e+00 2.534464545e+02 2.537841402e+02 8.1e-08 0.34 25 1.2e-04 5.5e-02 8.0e-03 1.00e+00 2.534705969e+02 2.537745027e+02 7.3e-08 0.35 26 1.1e-04 5.0e-02 7.2e-03 1.00e+00 2.534923089e+02 2.537658147e+02 6.5e-08 0.36 27 1.0e-04 4.6e-02 6.4e-03 1.00e+00 2.535118375e+02 2.537579848e+02 5.9e-08 0.37 28 9.0e-05 4.2e-02 5.8e-03 1.00e+00 2.535294030e+02 2.537509292e+02 5.3e-08 0.38 29 8.1e-05 3.9e-02 5.2e-03 1.00e+00 2.535452035e+02 2.537445719e+02 4.8e-08 0.39 30 7.3e-05 3.6e-02 4.7e-03 1.00e+00 2.535594172e+02 2.537388444e+02 4.3e-08 0.41 31 6.6e-05 3.3e-02 4.2e-03 1.00e+00 2.535722036e+02 2.537336848e+02 3.9e-08 0.42 32 5.9e-05 3.0e-02 3.8e-03 1.00e+00 2.535837066e+02 2.537290369e+02 3.5e-08 0.43 33 5.3e-05 2.8e-02 3.4e-03 1.00e+00 2.535940552e+02 2.537248503e+02 3.1e-08 0.44 34 4.8e-05 2.6e-02 3.1e-03 1.00e+00 2.536033655e+02 2.537210794e+02 2.8e-08 0.45 35 4.3e-05 2.4e-02 2.8e-03 1.00e+00 2.536117418e+02 2.537176829e+02 2.5e-08 0.46 36 3.9e-05 2.2e-02 2.5e-03 1.00e+00 2.536192779e+02 2.537146239e+02 2.3e-08 0.47 37 3.5e-05 2.1e-02 2.2e-03 1.00e+00 2.536260583e+02 2.537118689e+02 2.1e-08 0.48 38 3.1e-05 2.0e-02 2.0e-03 1.00e+00 2.536321588e+02 2.537093877e+02 1.8e-08 0.49 39 2.8e-05 1.8e-02 1.8e-03 1.00e+00 2.536376478e+02 2.537071534e+02 1.7e-08 0.50 40 2.5e-05 1.7e-02 1.6e-03 1.00e+00 2.536425866e+02 2.537051412e+02 1.5e-08 0.52 41 2.3e-05 1.6e-02 1.5e-03 1.00e+00 2.536470305e+02 2.537033294e+02 1.3e-08 0.53 42 2.1e-05 1.6e-02 1.3e-03 1.00e+00 2.536510290e+02 2.537016979e+02 1.2e-08 0.54 43 1.9e-05 1.5e-02 1.2e-03 1.00e+00 2.536546270e+02 2.537002288e+02 1.1e-08 0.55 44 1.7e-05 1.4e-02 1.1e-03 1.00e+00 2.536578646e+02 2.536989061e+02 9.8e-09 0.56 45 1.5e-05 1.3e-02 9.7e-04 1.00e+00 2.536607779e+02 2.536977152e+02 8.8e-09 0.57 46 1.4e-05 1.3e-02 8.7e-04 1.00e+00 2.536633994e+02 2.536966430e+02 8.0e-09 0.58 47 1.2e-05 1.2e-02 7.8e-04 1.00e+00 2.536657585e+02 2.536956778e+02 7.2e-09 0.59 48 1.1e-05 1.2e-02 7.1e-04 1.00e+00 2.536678814e+02 2.536948088e+02 6.4e-09 0.60 49 9.9e-06 1.1e-02 6.3e-04 1.00e+00 2.536697919e+02 2.536940265e+02 5.8e-09 0.62 50 8.9e-06 1.1e-02 5.7e-04 1.00e+00 2.536715110e+02 2.536933222e+02 5.2e-09 0.63 51 8.0e-06 1.1e-02 5.1e-04 1.00e+00 2.536730582e+02 2.536926883e+02 4.7e-09 0.64 52 7.2e-06 1.0e-02 4.6e-04 1.00e+00 2.536744505e+02 2.536921176e+02 4.2e-09 0.64 53 6.5e-06 1.0e-02 4.2e-04 1.00e+00 2.536757035e+02 2.536916039e+02 3.8e-09 0.65 54 5.8e-06 9.8e-03 3.7e-04 1.00e+00 2.536768310e+02 2.536911414e+02 3.4e-09 0.66 55 5.2e-06 9.6e-03 3.4e-04 1.00e+00 2.536778458e+02 2.536907252e+02 3.1e-09 0.68 56 4.7e-06 9.4e-03 3.0e-04 1.00e+00 2.536787590e+02 2.536903505e+02 2.8e-09 0.69 57 4.2e-06 9.2e-03 2.7e-04 1.00e+00 2.536795809e+02 2.536900132e+02 2.5e-09 0.69 58 3.8e-06 9.0e-03 2.5e-04 1.00e+00 2.536803205e+02 2.536897096e+02 2.2e-09 0.70 59 3.4e-06 8.9e-03 2.2e-04 1.00e+00 2.536809861e+02 2.536894363e+02 2.0e-09 0.71 60 3.1e-06 8.8e-03 2.0e-04 1.00e+00 2.536815851e+02 2.536891903e+02 1.8e-09 0.73 61 1.2e-06 3.4e-03 7.7e-05 1.00e+00 2.536848908e+02 2.536878316e+02 7.0e-10 0.73 62 1.1e-06 3.0e-03 6.9e-05 1.00e+00 2.536850996e+02 2.536877464e+02 6.3e-10 0.74 63 3.9e-07 1.1e-03 2.5e-05 1.00e+00 2.536863029e+02 2.536872515e+02 2.3e-10 0.75 64 3.5e-07 9.8e-04 2.2e-05 1.00e+00 2.536863701e+02 2.536872239e+02 2.0e-10 0.76 65 3.1e-07 8.8e-04 2.0e-05 1.00e+00 2.536864306e+02 2.536871990e+02 1.8e-10 0.77 66 2.8e-07 7.9e-04 1.8e-05 1.00e+00 2.536864850e+02 2.536871766e+02 1.7e-10 0.79 67 2.5e-07 7.2e-04 1.6e-05 1.00e+00 2.536865340e+02 2.536871564e+02 1.5e-10 0.79 68 2.3e-07 6.4e-04 1.5e-05 1.00e+00 2.536865781e+02 2.536871382e+02 1.3e-10 0.80 69 2.0e-07 5.8e-04 1.3e-05 1.00e+00 2.536866177e+02 2.536871219e+02 1.2e-10 0.82 70 1.8e-07 5.2e-04 1.2e-05 1.00e+00 2.536866534e+02 2.536871072e+02 1.1e-10 0.83 71 1.7e-07 4.7e-04 1.1e-05 1.00e+00 2.536866856e+02 2.536870939e+02 9.8e-11 0.84 72 1.5e-07 4.2e-04 9.6e-06 1.00e+00 2.536867145e+02 2.536870820e+02 8.8e-11 0.85 73 1.3e-07 3.8e-04 8.7e-06 1.00e+00 2.536867405e+02 2.536870713e+02 7.9e-11 0.86 74 1.2e-07 3.4e-04 7.8e-06 1.00e+00 2.536867639e+02 2.536870616e+02 7.1e-11 0.88 75 1.1e-07 3.1e-04 7.0e-06 1.00e+00 2.536867850e+02 2.536870529e+02 6.4e-11 0.89 76 9.8e-08 2.8e-04 6.3e-06 1.00e+00 2.536868040e+02 2.536870451e+02 5.8e-11 0.89 77 8.8e-08 2.5e-04 5.7e-06 1.00e+00 2.536868211e+02 2.536870381e+02 5.2e-11 0.90 78 7.9e-08 2.2e-04 5.1e-06 1.00e+00 2.536868364e+02 2.536870317e+02 4.7e-11 0.91 79 7.1e-08 2.0e-04 4.6e-06 1.00e+00 2.536868502e+02 2.536870260e+02 4.2e-11 0.93 80 6.4e-08 1.8e-04 4.1e-06 1.00e+00 2.536868627e+02 2.536870209e+02 3.8e-11 0.94 81 5.8e-08 1.6e-04 3.7e-06 1.00e+00 2.536868739e+02 2.536870163e+02 3.4e-11 0.95 82 5.2e-08 1.5e-04 3.4e-06 1.00e+00 2.536868840e+02 2.536870121e+02 3.1e-11 0.96 83 4.7e-08 1.3e-04 3.0e-06 1.00e+00 2.536868930e+02 2.536870084e+02 2.8e-11 0.98 84 4.2e-08 1.2e-04 2.7e-06 1.00e+00 2.536869012e+02 2.536870050e+02 2.5e-11 0.99 85 3.8e-08 1.1e-04 2.4e-06 1.00e+00 2.536869085e+02 2.536870020e+02 2.2e-11 1.00 86 3.4e-08 9.7e-05 2.2e-06 1.00e+00 2.536869152e+02 2.536869992e+02 2.0e-11 1.01 87 3.1e-08 8.7e-05 2.0e-06 1.00e+00 2.536869211e+02 2.536869968e+02 1.8e-11 1.03 88 2.8e-08 7.8e-05 1.8e-06 1.00e+00 2.536869265e+02 2.536869946e+02 1.6e-11 1.04 89 2.5e-08 7.0e-05 1.6e-06 1.00e+00 2.536869313e+02 2.536869926e+02 1.5e-11 1.05 90 2.2e-08 6.3e-05 1.4e-06 1.00e+00 2.536869356e+02 2.536869908e+02 1.3e-11 1.05 91 2.0e-08 5.7e-05 1.3e-06 1.00e+00 2.536869395e+02 2.536869892e+02 1.2e-11 1.07 92 1.8e-08 5.1e-05 1.2e-06 1.00e+00 2.536869430e+02 2.536869877e+02 1.1e-11 1.08 93 1.6e-08 4.6e-05 1.1e-06 1.00e+00 2.536869462e+02 2.536869864e+02 9.6e-12 1.09 94 1.5e-08 4.2e-05 9.5e-07 1.00e+00 2.536869490e+02 2.536869852e+02 8.7e-12 1.10 95 1.3e-08 3.7e-05 8.5e-07 1.00e+00 2.536869516e+02 2.536869842e+02 7.8e-12 1.11 96 1.2e-08 3.4e-05 7.7e-07 9.99e-01 2.536869539e+02 2.536869832e+02 7.0e-12 1.12 97 1.1e-08 3.0e-05 6.9e-07 1.00e+00 2.536869560e+02 2.536869824e+02 6.3e-12 1.13 98 9.7e-09 2.7e-05 6.2e-07 1.00e+00 2.536869579e+02 2.536869816e+02 5.7e-12 1.14 Optimizer terminated. Time: 1.14 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 2.5368695785e+02 nrm: 4e+01 Viol. con: 2e-07 var: 0e+00 Dual. obj: 2.5368698159e+02 nrm: 8e+02 Viol. con: 0e+00 var: 2e-04 * End solution on dual form. * Transforming to primal solution. Solving took 1.18 seconds. Using solver 'mosek' Solving for 1768 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 482 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: 0.02 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 873 Optimizer - Cones : 0 Optimizer - Scalar variables : 3462 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 : 1.49e+04 after factor : 1.57e+05 Factor - dense dim. : 0 flops : 3.26e+07 Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223212570e+05 2.000000000e+00 1.0e+00 0.05 1 1.6e+03 2.1e+03 8.5e+04 -9.71e-01 -1.214747743e+05 2.752575575e+00 7.0e-01 0.06 2 7.9e+02 1.0e+03 4.2e+04 -9.57e-01 -1.187755977e+05 5.296041762e+00 3.5e-01 0.08 3 2.9e+02 3.8e+02 1.6e+04 -9.12e-01 -1.103368431e+05 2.203264810e+01 1.3e-01 0.09 4 2.9e+02 3.8e+02 1.6e+04 -7.69e-01 -1.083761453e+05 1.727258626e+03 1.3e-01 0.10 5 1.2e+02 1.6e+02 6.7e+03 -7.60e-01 -8.800457329e+04 6.084555600e+03 5.5e-02 0.12 6 4.0e+01 5.2e+01 2.1e+03 -4.64e-01 -4.680506254e+04 1.110444952e+04 1.7e-02 0.13 7 2.3e+01 3.0e+01 1.2e+03 2.28e-01 -3.156323145e+04 7.378658951e+03 1.0e-02 0.14 8 9.2e+00 1.2e+01 4.9e+02 5.17e-01 -1.374584088e+04 4.010207729e+03 4.1e-03 0.15 9 6.1e+00 8.0e+00 3.3e+02 8.30e-01 -9.165852854e+03 2.896344754e+03 2.7e-03 0.17 10 2.1e+00 2.8e+00 1.1e+02 9.01e-01 -3.097789795e+03 1.214838717e+03 9.5e-04 0.18 11 1.4e+00 1.8e+00 7.7e+01 9.77e-01 -1.975637992e+03 9.495166554e+02 6.4e-04 0.19 12 8.0e-01 1.1e+00 4.3e+01 9.78e-01 -1.031715276e+03 6.325091514e+02 3.6e-04 0.21 13 3.6e-01 5.1e-01 2.0e+01 9.87e-01 -3.672371328e+02 3.875420486e+02 1.6e-04 0.22 14 1.7e-01 2.7e-01 9.4e+00 1.00e+00 -8.076234759e+01 2.797885158e+02 7.9e-05 0.23 15 9.4e-02 3.7e-01 5.2e+00 1.00e+00 3.210635850e+01 2.313101926e+02 4.4e-05 0.25 16 3.2e-02 1.6e-01 1.8e+00 1.00e+00 1.233683660e+02 1.926862977e+02 1.5e-05 0.26 17 1.1e-02 1.1e-01 6.1e-01 1.01e+00 1.558649259e+02 1.792079582e+02 5.3e-06 0.27 18 5.9e-03 8.4e-02 3.4e-01 1.01e+00 1.631309139e+02 1.761451470e+02 3.0e-06 0.28 19 9.7e-04 1.7e-01 6.0e-02 1.01e+00 1.707545135e+02 1.730452352e+02 5.4e-07 0.29 20 4.4e-04 1.1e-01 2.7e-02 1.01e+00 1.716591469e+02 1.726961714e+02 2.5e-07 0.30 21 1.8e-04 9.2e-02 1.2e-02 1.00e+00 1.720916066e+02 1.725300157e+02 1.1e-07 0.32 22 1.0e-04 7.2e-02 6.5e-03 1.00e+00 1.722276530e+02 1.724746476e+02 5.9e-08 0.33 23 9.3e-05 6.6e-02 5.9e-03 1.00e+00 1.722460856e+02 1.724684160e+02 5.3e-08 0.34 24 8.4e-05 6.0e-02 5.3e-03 1.00e+00 1.722619800e+02 1.724620702e+02 4.8e-08 0.35 25 7.5e-05 5.5e-02 4.8e-03 1.00e+00 1.722763775e+02 1.724564538e+02 4.3e-08 0.37 26 6.8e-05 5.0e-02 4.3e-03 1.00e+00 1.722893049e+02 1.724513693e+02 3.9e-08 0.38 27 6.1e-05 4.6e-02 3.9e-03 1.00e+00 1.723009275e+02 1.724467820e+02 3.5e-08 0.39 28 5.5e-05 4.2e-02 3.5e-03 1.00e+00 1.723113721e+02 1.724426382e+02 3.2e-08 0.40 29 4.9e-05 3.9e-02 3.1e-03 1.00e+00 1.723207578e+02 1.724388948e+02 2.8e-08 0.41 30 4.5e-05 3.6e-02 2.8e-03 1.00e+00 1.723291911e+02 1.724355123e+02 2.6e-08 0.42 31 4.0e-05 3.3e-02 2.5e-03 1.00e+00 1.723367686e+02 1.724324560e+02 2.3e-08 0.43 32 3.6e-05 3.1e-02 2.3e-03 1.00e+00 1.723435774e+02 1.724296946e+02 2.1e-08 0.44 33 3.2e-05 2.8e-02 2.0e-03 1.00e+00 1.723496961e+02 1.724272004e+02 1.9e-08 0.45 34 2.9e-05 2.6e-02 1.8e-03 1.00e+00 1.723551951e+02 1.724249481e+02 1.7e-08 0.47 35 2.6e-05 2.5e-02 1.7e-03 1.00e+00 1.723601380e+02 1.724229149e+02 1.5e-08 0.48 36 2.4e-05 2.3e-02 1.5e-03 1.00e+00 1.723645814e+02 1.724210801e+02 1.4e-08 0.48 37 2.1e-05 2.2e-02 1.3e-03 1.00e+00 1.723685763e+02 1.724194246e+02 1.2e-08 0.50 38 1.9e-05 2.0e-02 1.2e-03 1.00e+00 1.723721683e+02 1.724179314e+02 1.1e-08 0.51 39 1.7e-05 1.9e-02 1.1e-03 1.00e+00 1.723753982e+02 1.724165848e+02 9.9e-09 0.52 40 1.6e-05 1.8e-02 9.8e-04 1.00e+00 1.723783028e+02 1.724153706e+02 8.9e-09 0.53 41 1.4e-05 1.7e-02 8.8e-04 1.00e+00 1.723809150e+02 1.724142759e+02 8.0e-09 0.54 42 1.3e-05 1.6e-02 7.9e-04 1.00e+00 1.723832643e+02 1.724132890e+02 7.2e-09 0.55 43 1.1e-05 1.5e-02 7.1e-04 1.00e+00 1.723853774e+02 1.724123996e+02 6.5e-09 0.57 44 1.0e-05 1.5e-02 6.4e-04 1.00e+00 1.723872780e+02 1.724115979e+02 5.9e-09 0.58 45 9.2e-06 1.4e-02 5.8e-04 1.00e+00 1.723889875e+02 1.724108755e+02 5.3e-09 0.59 46 8.2e-06 1.3e-02 5.2e-04 1.00e+00 1.723905254e+02 1.724102245e+02 4.7e-09 0.60 47 7.4e-06 1.3e-02 4.7e-04 1.00e+00 1.723919087e+02 1.724096380e+02 4.3e-09 0.61 48 6.7e-06 1.2e-02 4.2e-04 1.00e+00 1.723931532e+02 1.724091096e+02 3.8e-09 0.62 49 6.0e-06 1.2e-02 3.8e-04 1.00e+00 1.723942728e+02 1.724086335e+02 3.5e-09 0.64 50 5.4e-06 1.1e-02 3.4e-04 1.00e+00 1.723952800e+02 1.724082047e+02 3.1e-09 0.65 51 4.9e-06 1.1e-02 3.1e-04 1.00e+00 1.723961862e+02 1.724078185e+02 2.8e-09 0.66 52 4.4e-06 1.1e-02 2.8e-04 1.00e+00 1.723970014e+02 1.724074705e+02 2.5e-09 0.67 53 3.9e-06 1.0e-02 2.5e-04 1.00e+00 1.723977350e+02 1.724071572e+02 2.3e-09 0.68 54 3.6e-06 1.0e-02 2.2e-04 1.00e+00 1.723983950e+02 1.724068750e+02 2.0e-09 0.69 55 3.2e-06 9.9e-03 2.0e-04 1.00e+00 1.723989888e+02 1.724066208e+02 1.8e-09 0.70 56 2.9e-06 9.7e-03 1.8e-04 1.00e+00 1.723995231e+02 1.724063920e+02 1.7e-09 0.71 57 2.6e-06 9.5e-03 1.6e-04 1.00e+00 1.724000038e+02 1.724061859e+02 1.5e-09 0.72 58 2.3e-06 9.3e-03 1.5e-04 1.00e+00 1.724004364e+02 1.724060003e+02 1.3e-09 0.73 59 2.1e-06 9.2e-03 1.3e-04 1.00e+00 1.724008257e+02 1.724058332e+02 1.2e-09 0.75 60 1.9e-06 9.0e-03 1.2e-04 1.00e+00 1.724011759e+02 1.724056827e+02 1.1e-09 0.76 61 1.7e-06 8.9e-03 1.1e-04 1.00e+00 1.724014911e+02 1.724055472e+02 9.8e-10 0.77 62 1.5e-06 8.8e-03 9.6e-05 1.00e+00 1.724017747e+02 1.724054252e+02 8.8e-10 0.78 63 1.4e-06 8.7e-03 8.7e-05 1.00e+00 1.724020299e+02 1.724053153e+02 7.9e-10 0.79 64 1.2e-06 8.6e-03 7.8e-05 1.00e+00 1.724022595e+02 1.724052164e+02 7.1e-10 0.81 65 1.1e-06 8.5e-03 7.0e-05 1.00e+00 1.724024661e+02 1.724051274e+02 6.4e-10 0.82 66 1.0e-06 8.4e-03 6.3e-05 1.00e+00 1.724026521e+02 1.724050472e+02 5.8e-10 0.83 67 9.0e-07 8.3e-03 5.7e-05 1.00e+00 1.724028194e+02 1.724049750e+02 5.2e-10 0.84 68 8.1e-07 8.3e-03 5.1e-05 1.00e+00 1.724029700e+02 1.724049101e+02 4.7e-10 0.85 69 7.3e-07 8.2e-03 4.6e-05 1.00e+00 1.724031055e+02 1.724048516e+02 4.2e-10 0.87 70 6.6e-07 8.1e-03 4.2e-05 1.00e+00 1.724032274e+02 1.724047989e+02 3.8e-10 0.88 71 5.9e-07 8.1e-03 3.7e-05 1.00e+00 1.724033371e+02 1.724047515e+02 3.4e-10 0.89 72 5.3e-07 8.0e-03 3.4e-05 1.00e+00 1.724034358e+02 1.724047088e+02 3.1e-10 0.90 73 4.8e-07 8.0e-03 3.0e-05 1.00e+00 1.724035247e+02 1.724046703e+02 2.8e-10 0.91 74 4.3e-07 7.9e-03 2.7e-05 1.00e+00 1.724036046e+02 1.724046357e+02 2.5e-10 0.92 75 3.9e-07 7.9e-03 2.5e-05 1.00e+00 1.724036766e+02 1.724046046e+02 2.2e-10 0.94 76 3.5e-07 7.9e-03 2.2e-05 1.00e+00 1.724037413e+02 1.724045765e+02 2.0e-10 0.95 77 3.1e-07 7.8e-03 2.0e-05 1.00e+00 1.724037996e+02 1.724045512e+02 1.8e-10 0.96 78 2.8e-07 7.8e-03 1.8e-05 1.00e+00 1.724038520e+02 1.724045285e+02 1.6e-10 0.97 79 2.5e-07 7.8e-03 1.6e-05 1.00e+00 1.724038992e+02 1.724045081e+02 1.5e-10 0.98 80 2.3e-07 7.7e-03 1.4e-05 1.00e+00 1.724039416e+02 1.724044896e+02 1.3e-10 0.99 81 2.1e-07 7.7e-03 1.3e-05 1.00e+00 1.724039798e+02 1.724044730e+02 1.2e-10 1.01 82 1.9e-07 7.7e-03 1.2e-05 1.00e+00 1.724040142e+02 1.724044581e+02 1.1e-10 1.02 83 1.7e-07 7.7e-03 1.1e-05 9.98e-01 1.724040451e+02 1.724044447e+02 9.6e-11 1.03 84 1.5e-07 7.6e-03 9.5e-06 9.99e-01 1.724040730e+02 1.724044325e+02 8.7e-11 1.05 85 1.4e-07 7.6e-03 8.6e-06 1.00e+00 1.724040981e+02 1.724044216e+02 7.8e-11 1.06 86 1.2e-07 7.6e-03 7.7e-06 1.00e+00 1.724041206e+02 1.724044117e+02 7.0e-11 1.07 87 1.1e-07 7.6e-03 6.9e-06 9.96e-01 1.724041409e+02 1.724044029e+02 6.3e-11 1.08 88 9.9e-08 7.6e-03 6.2e-06 9.90e-01 1.724041592e+02 1.724043950e+02 5.7e-11 1.09 89 8.9e-08 7.6e-03 5.6e-06 9.97e-01 1.724041756e+02 1.724043878e+02 5.1e-11 1.10 90 8.0e-08 7.5e-03 5.0e-06 9.96e-01 1.724041904e+02 1.724043814e+02 4.6e-11 1.11 91 7.2e-08 6.8e-03 4.5e-06 1.00e+00 1.724042037e+02 1.724043755e+02 4.1e-11 1.12 92 6.5e-08 6.1e-03 4.1e-06 9.90e-01 1.724042157e+02 1.724043704e+02 3.7e-11 1.13 93 5.8e-08 5.5e-03 3.7e-06 9.89e-01 1.724042264e+02 1.724043657e+02 3.4e-11 1.14 94 5.3e-08 4.9e-03 3.3e-06 1.01e+00 1.724042366e+02 1.724043614e+02 3.0e-11 1.15 95 4.8e-08 4.5e-03 3.0e-06 9.85e-01 1.724042453e+02 1.724043576e+02 2.7e-11 1.16 96 4.3e-08 4.0e-03 2.7e-06 1.02e+00 1.724042539e+02 1.724043535e+02 2.5e-11 1.17 97 3.9e-08 3.6e-03 2.4e-06 9.62e-01 1.724042609e+02 1.724043505e+02 2.2e-11 1.18 98 3.5e-08 3.2e-03 2.2e-06 1.04e+00 1.724042682e+02 1.724043473e+02 2.1e-11 1.19 99 3.1e-08 2.9e-03 2.0e-06 9.48e-01 1.724042737e+02 1.724043449e+02 1.8e-11 1.20 100 3.3e-08 2.6e-03 1.8e-06 9.93e-01 1.724042787e+02 1.724043424e+02 1.7e-11 1.21 101 2.7e-08 6.0e-04 4.0e-07 1.07e+00 1.724043138e+02 1.724043283e+02 4.2e-12 1.22 102 1.9e-08 5.4e-04 3.6e-07 1.71e+00 1.724043148e+02 1.724043272e+02 3.8e-12 1.23 103 1.1e-08 4.9e-04 3.3e-07 6.62e+00 1.724043156e+02 1.724043269e+02 3.4e-12 1.25 104 3.8e-07 7.6e-05 6.8e-07 1.00e+00 1.724043006e+02 1.724043239e+02 5.3e-13 1.26 Optimizer terminated. Time: 1.26 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.7240430055e+02 nrm: 4e+01 Viol. con: 8e-06 var: 0e+00 Dual. obj: 1.7240432386e+02 nrm: 8e+02 Viol. con: 0e+00 var: 5e-04 * End solution on dual form. * Transforming to primal solution. Solving took 1.3 seconds. Using solver 'mosek' Solving for 1768 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 482 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: 0.02 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 873 Optimizer - Cones : 0 Optimizer - Scalar variables : 3462 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 : 1.49e+04 after factor : 1.57e+05 Factor - dense dim. : 0 flops : 3.26e+07 Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.224327551e+05 2.000000000e+00 1.0e+00 0.05 1 1.6e+03 2.2e+03 8.8e+04 -9.71e-01 -1.216813483e+05 2.647106674e+00 7.2e-01 0.06 2 8.5e+02 1.1e+03 4.6e+04 -9.59e-01 -1.192698611e+05 4.803201327e+00 3.7e-01 0.07 3 2.9e+02 3.8e+02 1.6e+04 -9.19e-01 -1.104970572e+05 2.024725330e+01 1.3e-01 0.08 4 2.9e+02 3.8e+02 1.6e+04 -7.71e-01 -1.083239769e+05 1.915508401e+03 1.3e-01 0.10 5 1.2e+02 1.6e+02 6.6e+03 -7.61e-01 -8.791520474e+04 6.170113737e+03 5.5e-02 0.11 6 4.4e+01 5.8e+01 2.4e+03 -4.62e-01 -5.104551639e+04 1.044227472e+04 1.9e-02 0.12 7 2.6e+01 3.4e+01 1.4e+03 1.59e-01 -3.546492403e+04 7.351516040e+03 1.2e-02 0.13 8 1.3e+01 1.7e+01 6.9e+02 4.56e-01 -1.916966663e+04 4.670190638e+03 5.7e-03 0.14 9 4.5e+00 5.9e+00 2.4e+02 7.41e-01 -6.827042953e+03 2.226858378e+03 2.0e-03 0.15 10 3.4e+00 4.4e+00 1.8e+02 9.39e-01 -5.017275706e+03 1.793655671e+03 1.5e-03 0.16 11 1.1e+00 1.5e+00 6.1e+01 9.61e-01 -1.587697556e+03 7.238657166e+02 5.1e-04 0.17 12 9.0e-01 1.2e+00 4.9e+01 9.87e-01 -1.219371388e+03 6.449524040e+02 4.1e-04 0.18 13 7.3e-01 1.1e+00 4.0e+01 9.68e-01 -9.758699756e+02 5.568100605e+02 3.3e-04 0.19 14 3.7e-01 5.4e-01 2.0e+01 9.89e-01 -3.947836917e+02 3.889130817e+02 1.7e-04 0.20 15 1.9e-01 2.9e-01 1.0e+01 9.96e-01 -1.338511558e+02 2.689192391e+02 8.8e-05 0.21 16 8.8e-02 1.7e-01 4.9e+00 1.00e+00 1.847645464e+01 2.059038853e+02 4.1e-05 0.22 17 7.9e-02 1.5e-01 4.4e+00 1.01e+00 4.014646721e+01 2.086163615e+02 3.7e-05 0.24 18 2.9e-02 9.0e-02 1.7e+00 1.01e+00 1.188557664e+02 1.819900126e+02 1.4e-05 0.25 19 1.2e-02 1.2e-01 6.8e-01 1.02e+00 1.480655786e+02 1.739328234e+02 5.8e-06 0.26 20 5.5e-03 3.7e-01 3.1e-01 1.01e+00 1.580265231e+02 1.698825938e+02 2.7e-06 0.27 21 2.1e-03 1.6e-01 1.2e-01 1.01e+00 1.637303347e+02 1.682841321e+02 1.0e-06 0.29 22 1.4e-03 1.2e-01 8.2e-02 1.01e+00 1.648886250e+02 1.679675561e+02 7.0e-07 0.30 23 5.7e-04 8.8e-02 3.4e-02 1.01e+00 1.662118945e+02 1.674692652e+02 2.9e-07 0.31 24 2.9e-04 7.7e-02 1.7e-02 1.01e+00 1.666551422e+02 1.672890941e+02 1.5e-07 0.32 25 2.6e-04 7.0e-02 1.5e-02 1.01e+00 1.667024392e+02 1.672728727e+02 1.3e-07 0.33 26 2.3e-04 6.4e-02 1.4e-02 1.01e+00 1.667425270e+02 1.672557272e+02 1.2e-07 0.34 27 2.1e-04 5.8e-02 1.2e-02 1.01e+00 1.667789192e+02 1.672406641e+02 1.1e-07 0.35 28 1.9e-04 5.3e-02 1.1e-02 1.01e+00 1.668114775e+02 1.672269336e+02 9.7e-08 0.36 29 1.7e-04 4.9e-02 1.0e-02 1.01e+00 1.668406754e+02 1.672144938e+02 8.7e-08 0.38 30 1.5e-04 4.5e-02 9.1e-03 1.01e+00 1.668668443e+02 1.672032053e+02 7.8e-08 0.39 31 1.4e-04 4.1e-02 8.2e-03 1.01e+00 1.668903032e+02 1.671929661e+02 7.1e-08 0.40 32 1.2e-04 3.8e-02 7.3e-03 1.01e+00 1.669113344e+02 1.671836806e+02 6.4e-08 0.42 33 1.1e-04 3.5e-02 6.6e-03 1.01e+00 1.669301919e+02 1.671752626e+02 5.7e-08 0.43 34 9.9e-05 3.2e-02 6.0e-03 1.00e+00 1.669471035e+02 1.671676342e+02 5.1e-08 0.44 35 9.0e-05 3.0e-02 5.4e-03 1.00e+00 1.669622729e+02 1.671607240e+02 4.6e-08 0.46 36 8.1e-05 2.8e-02 4.8e-03 1.00e+00 1.669758820e+02 1.671544676e+02 4.2e-08 0.48 37 7.3e-05 2.6e-02 4.3e-03 1.00e+00 1.669880933e+02 1.671488038e+02 3.8e-08 0.49 38 6.5e-05 2.4e-02 3.9e-03 1.00e+00 1.669990522e+02 1.671436782e+02 3.4e-08 0.51 39 5.9e-05 2.2e-02 3.5e-03 1.00e+00 1.670088888e+02 1.671390405e+02 3.0e-08 0.52 40 5.3e-05 2.1e-02 3.2e-03 1.00e+00 1.670177195e+02 1.671348474e+02 2.7e-08 0.53 41 4.8e-05 2.0e-02 2.8e-03 1.00e+00 1.670256477e+02 1.671310567e+02 2.5e-08 0.55 42 4.3e-05 1.8e-02 2.6e-03 1.00e+00 1.670327665e+02 1.671276302e+02 2.2e-08 0.56 43 3.9e-05 1.7e-02 2.3e-03 1.00e+00 1.670391594e+02 1.671245321e+02 2.0e-08 0.57 44 3.5e-05 1.7e-02 2.1e-03 1.00e+00 1.670449016e+02 1.671217321e+02 1.8e-08 0.59 45 3.1e-05 1.6e-02 1.9e-03 1.00e+00 1.670500597e+02 1.671192049e+02 1.6e-08 0.60 46 2.8e-05 1.5e-02 1.7e-03 1.00e+00 1.670546929e+02 1.671169216e+02 1.5e-08 0.61 47 2.5e-05 1.4e-02 1.5e-03 1.00e+00 1.670588557e+02 1.671148599e+02 1.3e-08 0.63 48 2.3e-05 1.4e-02 1.4e-03 1.00e+00 1.670625960e+02 1.671129976e+02 1.2e-08 0.64 49 2.0e-05 1.3e-02 1.2e-03 1.00e+00 1.670659573e+02 1.671113174e+02 1.1e-08 0.65 50 1.8e-05 1.3e-02 1.1e-03 1.00e+00 1.670689777e+02 1.671098016e+02 9.6e-09 0.67 51 1.7e-05 1.2e-02 9.9e-04 1.00e+00 1.670716922e+02 1.671084342e+02 8.6e-09 0.68 52 1.5e-05 1.2e-02 8.9e-04 1.00e+00 1.670741319e+02 1.671072001e+02 7.7e-09 0.69 53 1.3e-05 1.1e-02 8.0e-04 1.00e+00 1.670763250e+02 1.671060869e+02 7.0e-09 0.70 54 1.2e-05 1.1e-02 7.2e-04 1.00e+00 1.670782965e+02 1.671050829e+02 6.3e-09 0.72 55 1.1e-05 1.1e-02 6.5e-04 1.00e+00 1.670800691e+02 1.671041767e+02 5.6e-09 0.73 56 9.8e-06 1.1e-02 5.9e-04 1.00e+00 1.670816629e+02 1.671033600e+02 5.1e-09 0.74 57 8.8e-06 1.0e-02 5.3e-04 1.00e+00 1.670830960e+02 1.671026232e+02 4.6e-09 0.76 58 7.9e-06 1.0e-02 4.8e-04 1.00e+00 1.670843850e+02 1.671019578e+02 4.1e-09 0.77 59 7.1e-06 1.0e-02 4.3e-04 1.00e+00 1.670855442e+02 1.671013584e+02 3.7e-09 0.78 60 6.4e-06 9.8e-03 3.9e-04 1.00e+00 1.670865865e+02 1.671008191e+02 3.3e-09 0.80 61 5.8e-06 9.7e-03 3.5e-04 9.99e-01 1.670875237e+02 1.671003340e+02 3.0e-09 0.81 62 2.2e-06 3.6e-03 1.3e-04 1.00e+00 1.670927405e+02 1.670975940e+02 1.1e-09 0.82 63 8.8e-07 1.5e-03 5.3e-05 9.98e-01 1.670946467e+02 1.670965975e+02 4.6e-10 0.83 64 7.9e-07 1.3e-03 4.8e-05 9.88e-01 1.670947778e+02 1.670965343e+02 4.1e-10 0.85 65 4.8e-07 8.0e-04 2.9e-05 1.01e+00 1.670952311e+02 1.670962876e+02 2.5e-10 0.86 66 4.3e-07 7.2e-04 2.6e-05 9.82e-01 1.670953009e+02 1.670962527e+02 2.2e-10 0.87 67 3.9e-07 6.4e-04 2.3e-05 1.01e+00 1.670953651e+02 1.670962182e+02 2.0e-10 0.88 68 3.5e-07 5.8e-04 2.1e-05 9.96e-01 1.670954207e+02 1.670961888e+02 1.8e-10 0.90 69 3.1e-07 5.2e-04 1.9e-05 9.51e-01 1.670954705e+02 1.670961633e+02 1.6e-10 0.91 70 2.8e-07 4.7e-04 1.7e-05 1.04e+00 1.670955223e+02 1.670961346e+02 1.5e-10 0.92 71 2.5e-07 4.2e-04 1.5e-05 1.00e+00 1.670955621e+02 1.670961134e+02 1.3e-10 0.93 72 2.3e-07 3.8e-04 1.4e-05 1.09e+00 1.670956120e+02 1.670960845e+02 1.3e-10 0.95 73 2.1e-07 3.4e-04 1.2e-05 1.07e+00 1.670956528e+02 1.670960614e+02 1.2e-10 0.96 74 1.9e-07 3.1e-04 1.1e-05 1.02e+00 1.670956818e+02 1.670960459e+02 1.1e-10 0.97 75 1.7e-07 2.8e-04 1.0e-05 1.02e+00 1.670957070e+02 1.670960326e+02 9.7e-11 0.98 76 1.5e-07 2.5e-04 9.0e-06 9.55e-01 1.670957282e+02 1.670960220e+02 8.7e-11 1.00 77 1.4e-07 2.2e-04 8.1e-06 1.07e+00 1.670957537e+02 1.670960077e+02 8.1e-11 1.00 78 1.2e-07 2.0e-04 7.3e-06 1.07e+00 1.670957761e+02 1.670959950e+02 7.6e-11 1.02 79 1.1e-07 1.8e-04 6.6e-06 1.04e+00 1.670957934e+02 1.670959856e+02 7.0e-11 1.03 80 9.9e-08 1.6e-04 5.9e-06 9.23e-01 1.670958060e+02 1.670959795e+02 6.3e-11 1.04 81 9.0e-08 1.5e-04 5.3e-06 1.24e+00 1.670958180e+02 1.670959719e+02 5.6e-11 1.06 82 8.1e-08 1.3e-04 4.8e-06 8.86e-01 1.670958281e+02 1.670959671e+02 5.1e-11 1.07 83 7.2e-08 1.2e-04 4.3e-06 8.05e-01 1.670958370e+02 1.670959635e+02 4.6e-11 1.08 84 6.5e-08 1.1e-04 3.9e-06 8.67e-01 1.670958452e+02 1.670959597e+02 4.1e-11 1.09 85 5.9e-08 9.7e-05 3.5e-06 6.94e-01 1.670958524e+02 1.670959572e+02 3.7e-11 1.10 86 5.5e-08 8.7e-05 3.1e-06 2.15e+00 1.670958604e+02 1.670959489e+02 3.3e-11 1.12 87 5.0e-08 7.8e-05 2.8e-06 9.73e-01 1.670958664e+02 1.670959461e+02 3.0e-11 1.13 88 4.6e-08 7.0e-05 2.5e-06 1.10e+00 1.670958743e+02 1.670959420e+02 2.8e-11 1.14 89 6.9e-08 6.3e-05 2.3e-06 3.61e+00 1.670958814e+02 1.670959335e+02 2.4e-11 1.15 90 6.2e-08 5.7e-05 2.1e-06 1.04e+00 1.670958860e+02 1.670959319e+02 2.2e-11 1.16 91 5.8e-08 5.1e-05 1.9e-06 8.51e-01 1.670958893e+02 1.670959310e+02 2.0e-11 1.18 92 5.9e-08 4.6e-05 1.7e-06 3.05e+00 1.670958941e+02 1.670959277e+02 1.7e-11 1.19 93 5.4e-08 4.2e-05 1.5e-06 9.23e-01 1.670958966e+02 1.670959271e+02 1.6e-11 1.20 94 4.7e-08 3.7e-05 1.4e-06 8.68e-01 1.670958989e+02 1.670959265e+02 1.4e-11 1.21 95 4.4e-08 3.4e-05 1.2e-06 1.30e+00 1.670959011e+02 1.670959258e+02 1.3e-11 1.23 96 4.4e-08 3.0e-05 1.1e-06 2.49e+00 1.670959039e+02 1.670959244e+02 1.1e-11 1.24 97 4.8e-09 3.2e-06 1.1e-07 8.44e-01 1.670959190e+02 1.670959213e+02 1.7e-12 1.25 Optimizer terminated. Time: 1.26 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6709591897e+02 nrm: 2e+01 Viol. con: 6e-08 var: 0e+00 Dual. obj: 1.6709592125e+02 nrm: 9e+02 Viol. con: 0e+00 var: 1e-05 * End solution on dual form. * Transforming to primal solution. Solving took 1.3 seconds. Using solver 'mosek' Solving for 1768 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (313) 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 482 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: 0.02 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 873 Optimizer - Cones : 0 Optimizer - Scalar variables : 3462 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 : 1.49e+04 after factor : 1.57e+05 Factor - dense dim. : 0 flops : 3.26e+07 Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223581880e+05 2.000000000e+00 1.0e+00 0.05 1 1.7e+03 2.2e+03 8.9e+04 -9.71e-01 -1.216207073e+05 2.628833702e+00 7.2e-01 0.06 2 8.7e+02 1.1e+03 4.7e+04 -9.59e-01 -1.193316428e+05 4.638356624e+00 3.8e-01 0.08 3 2.9e+02 3.8e+02 1.6e+04 -9.21e-01 -1.104197427e+05 2.002454832e+01 1.3e-01 0.09 4 2.9e+02 3.8e+02 1.5e+04 -7.71e-01 -1.081724339e+05 1.983699491e+03 1.3e-01 0.10 5 1.2e+02 1.6e+02 6.4e+03 -7.61e-01 -8.690115711e+04 6.396992344e+03 5.3e-02 0.11 6 4.0e+01 5.3e+01 2.2e+03 -4.47e-01 -4.771003122e+04 1.103855097e+04 1.8e-02 0.13 7 2.5e+01 3.3e+01 1.3e+03 2.18e-01 -3.389201759e+04 7.549061717e+03 1.1e-02 0.14 8 1.1e+01 1.4e+01 5.8e+02 4.86e-01 -1.644444395e+04 4.097473790e+03 4.8e-03 0.15 9 4.2e+00 5.5e+00 2.3e+02 7.91e-01 -6.302686153e+03 2.124014637e+03 1.9e-03 0.17 10 2.4e+00 3.1e+00 1.3e+02 9.45e-01 -3.466909138e+03 1.414407312e+03 1.1e-03 0.18 11 1.1e+00 1.4e+00 5.9e+01 9.81e-01 -1.503911244e+03 7.432839272e+02 4.9e-04 0.19 12 8.3e-01 1.1e+00 4.5e+01 9.85e-01 -1.109403840e+03 6.058101723e+02 3.7e-04 0.20 13 5.8e-01 7.9e-01 3.2e+01 9.66e-01 -7.539123756e+02 4.697730967e+02 2.6e-04 0.21 14 3.3e-01 4.5e-01 1.8e+01 9.98e-01 -3.315180349e+02 3.561202862e+02 1.5e-04 0.23 15 9.9e-02 1.8e-01 5.6e+00 9.93e-01 -5.626632191e+00 2.082400810e+02 4.7e-05 0.24 16 9.0e-02 1.6e-01 5.1e+00 1.02e+00 1.966600076e+01 2.126774959e+02 4.3e-05 0.25 17 3.9e-02 1.0e-01 2.2e+00 1.02e+00 1.013712646e+02 1.848718234e+02 1.9e-05 0.26 18 1.1e-02 1.7e-01 6.1e-01 1.02e+00 1.498828807e+02 1.727908070e+02 5.1e-06 0.27 19 3.5e-03 1.9e-01 2.1e-01 1.01e+00 1.608923238e+02 1.685837962e+02 1.7e-06 0.29 20 1.4e-03 1.2e-01 8.1e-02 1.01e+00 1.644522069e+02 1.674814873e+02 6.9e-07 0.30 21 6.7e-04 8.4e-02 4.0e-02 9.99e-01 1.655690948e+02 1.670700255e+02 3.5e-07 0.31 22 2.9e-04 8.2e-02 1.7e-02 1.01e+00 1.661833190e+02 1.668310671e+02 1.5e-07 0.33 23 2.6e-04 7.6e-02 1.6e-02 1.01e+00 1.662352729e+02 1.668181495e+02 1.4e-07 0.34 24 2.3e-04 6.9e-02 1.4e-02 1.01e+00 1.662761249e+02 1.668005727e+02 1.2e-07 0.35 25 2.1e-04 6.3e-02 1.3e-02 1.01e+00 1.663130886e+02 1.667849709e+02 1.1e-07 0.36 26 1.9e-04 5.7e-02 1.1e-02 1.01e+00 1.663461849e+02 1.667707813e+02 9.9e-08 0.38 27 1.7e-04 5.2e-02 1.0e-02 1.01e+00 1.663758974e+02 1.667579550e+02 8.9e-08 0.39 28 1.5e-04 4.8e-02 9.3e-03 1.01e+00 1.664025669e+02 1.667463549e+02 8.0e-08 0.40 29 1.4e-04 4.4e-02 8.3e-03 1.01e+00 1.664265094e+02 1.667358675e+02 7.2e-08 0.42 30 1.2e-04 4.0e-02 7.5e-03 1.00e+00 1.664480051e+02 1.667263866e+02 6.5e-08 0.43 31 1.1e-04 3.7e-02 6.8e-03 1.00e+00 1.664673054e+02 1.667178163e+02 5.9e-08 0.44 32 1.0e-04 3.4e-02 6.1e-03 1.00e+00 1.664846353e+02 1.667100695e+02 5.3e-08 0.45 33 9.0e-05 3.2e-02 5.5e-03 1.00e+00 1.665001968e+02 1.667030675e+02 4.7e-08 0.46 34 8.1e-05 2.9e-02 4.9e-03 1.00e+00 1.665141711e+02 1.666967387e+02 4.3e-08 0.48 35 7.3e-05 2.7e-02 4.4e-03 1.00e+00 1.665267204e+02 1.666910189e+02 3.8e-08 0.49 36 6.5e-05 2.5e-02 4.0e-03 1.00e+00 1.665379905e+02 1.666858495e+02 3.5e-08 0.50 37 5.9e-05 2.4e-02 3.6e-03 1.00e+00 1.665481123e+02 1.666811779e+02 3.1e-08 0.51 38 5.3e-05 2.2e-02 3.2e-03 1.00e+00 1.665572032e+02 1.666769563e+02 2.8e-08 0.53 39 4.8e-05 2.1e-02 2.9e-03 1.00e+00 1.665653684e+02 1.666731419e+02 2.5e-08 0.54 40 4.3e-05 1.9e-02 2.6e-03 1.00e+00 1.665727028e+02 1.666696955e+02 2.3e-08 0.55 41 3.9e-05 1.8e-02 2.4e-03 1.00e+00 1.665792910e+02 1.666665819e+02 2.0e-08 0.57 42 3.5e-05 1.7e-02 2.1e-03 1.00e+00 1.665852094e+02 1.666637694e+02 1.8e-08 0.58 43 3.1e-05 1.6e-02 1.9e-03 1.00e+00 1.665905264e+02 1.666612290e+02 1.7e-08 0.59 44 2.8e-05 1.6e-02 1.7e-03 1.00e+00 1.665953034e+02 1.666589347e+02 1.5e-08 0.61 45 2.5e-05 1.5e-02 1.5e-03 1.00e+00 1.665995954e+02 1.666568629e+02 1.3e-08 0.62 46 2.3e-05 1.4e-02 1.4e-03 1.00e+00 1.666034519e+02 1.666549922e+02 1.2e-08 0.63 47 2.1e-05 1.4e-02 1.3e-03 1.00e+00 1.666069174e+02 1.666533033e+02 1.1e-08 0.65 48 1.8e-05 1.3e-02 1.1e-03 1.00e+00 1.666100317e+02 1.666517788e+02 9.8e-09 0.66 49 1.7e-05 1.3e-02 1.0e-03 1.00e+00 1.666128305e+02 1.666504028e+02 8.8e-09 0.68 50 1.5e-05 1.2e-02 9.1e-04 1.00e+00 1.666153460e+02 1.666491611e+02 7.9e-09 0.69 51 1.3e-05 1.2e-02 8.2e-04 1.00e+00 1.666176070e+02 1.666480406e+02 7.1e-09 0.70 52 1.2e-05 1.1e-02 7.4e-04 1.00e+00 1.666196393e+02 1.666470297e+02 6.4e-09 0.72 53 1.1e-05 1.1e-02 6.7e-04 1.00e+00 1.666214662e+02 1.666461177e+02 5.8e-09 0.73 54 9.8e-06 1.1e-02 6.0e-04 1.00e+00 1.666231086e+02 1.666452950e+02 5.2e-09 0.74 55 8.8e-06 1.1e-02 5.4e-04 1.00e+00 1.666245852e+02 1.666445530e+02 4.7e-09 0.76 56 8.0e-06 1.0e-02 4.9e-04 1.00e+00 1.666259127e+02 1.666438839e+02 4.2e-09 0.77 57 7.2e-06 1.0e-02 4.4e-04 1.00e+00 1.666271063e+02 1.666432805e+02 3.8e-09 0.78 58 6.4e-06 1.0e-02 3.9e-04 1.00e+00 1.666281795e+02 1.666427364e+02 3.4e-09 0.79 59 5.8e-06 9.8e-03 3.5e-04 1.00e+00 1.666291444e+02 1.666422458e+02 3.1e-09 0.81 60 5.2e-06 9.7e-03 3.2e-04 1.00e+00 1.666300122e+02 1.666418035e+02 2.8e-09 0.82 61 4.7e-06 9.5e-03 2.9e-04 1.00e+00 1.666307924e+02 1.666414047e+02 2.5e-09 0.83 62 4.2e-06 9.4e-03 2.6e-04 1.00e+00 1.666314940e+02 1.666410451e+02 2.2e-09 0.84 63 3.8e-06 9.3e-03 2.3e-04 1.00e+00 1.666321249e+02 1.666407210e+02 2.0e-09 0.85 64 3.4e-06 9.2e-03 2.1e-04 1.00e+00 1.666326921e+02 1.666404287e+02 1.8e-09 0.87 65 3.1e-06 9.1e-03 1.9e-04 1.00e+00 1.666332022e+02 1.666401652e+02 1.6e-09 0.88 66 2.8e-06 9.0e-03 1.7e-04 1.00e+00 1.666336608e+02 1.666399276e+02 1.5e-09 0.89 67 2.5e-06 8.9e-03 1.5e-04 1.00e+00 1.666340733e+02 1.666397134e+02 1.3e-09 0.91 68 2.2e-06 8.9e-03 1.4e-04 1.00e+00 1.666344443e+02 1.666395204e+02 1.2e-09 0.92 69 2.0e-06 8.8e-03 1.2e-04 1.00e+00 1.666347779e+02 1.666393465e+02 1.1e-09 0.93 70 1.8e-06 8.7e-03 1.1e-04 1.00e+00 1.666350780e+02 1.666391898e+02 9.7e-10 0.94 71 1.6e-06 8.7e-03 1.0e-04 1.00e+00 1.666353480e+02 1.666390486e+02 8.7e-10 0.95 72 1.5e-06 8.6e-03 9.0e-05 1.00e+00 1.666355907e+02 1.666389213e+02 7.8e-10 0.97 73 1.3e-06 8.6e-03 8.1e-05 1.00e+00 1.666358091e+02 1.666388067e+02 7.0e-10 0.98 74 1.2e-06 8.5e-03 7.3e-05 1.00e+00 1.666360055e+02 1.666387033e+02 6.3e-10 0.99 75 1.1e-06 8.5e-03 6.6e-05 1.00e+00 1.666361822e+02 1.666386102e+02 5.7e-10 1.00 76 9.7e-07 8.5e-03 5.9e-05 1.00e+00 1.666363410e+02 1.666385263e+02 5.1e-10 1.01 77 8.7e-07 8.4e-03 5.3e-05 1.00e+00 1.666364839e+02 1.666384506e+02 4.6e-10 1.03 78 7.8e-07 8.4e-03 4.8e-05 1.00e+00 1.666366124e+02 1.666383825e+02 4.2e-10 1.04 79 7.0e-07 8.4e-03 4.3e-05 1.00e+00 1.666367279e+02 1.666383210e+02 3.7e-10 1.05 80 6.3e-07 8.3e-03 3.9e-05 1.00e+00 1.666368319e+02 1.666382656e+02 3.4e-10 1.07 81 5.7e-07 8.3e-03 3.5e-05 1.00e+00 1.666369253e+02 1.666382157e+02 3.0e-10 1.08 82 5.1e-07 8.3e-03 3.1e-05 1.00e+00 1.666370093e+02 1.666381706e+02 2.7e-10 1.09 83 4.6e-07 8.3e-03 2.8e-05 1.00e+00 1.666370849e+02 1.666381300e+02 2.5e-10 1.10 84 4.2e-07 8.2e-03 2.5e-05 1.00e+00 1.666371528e+02 1.666380935e+02 2.2e-10 1.11 85 3.7e-07 8.2e-03 2.3e-05 1.00e+00 1.666372139e+02 1.666380605e+02 2.0e-10 1.13 86 3.4e-07 8.2e-03 2.1e-05 1.00e+00 1.666372688e+02 1.666380307e+02 1.8e-10 1.14 87 3.0e-07 8.2e-03 1.9e-05 1.00e+00 1.666373182e+02 1.666380040e+02 1.6e-10 1.15 88 2.7e-07 8.1e-03 1.7e-05 1.00e+00 1.666373626e+02 1.666379798e+02 1.5e-10 1.16 89 2.5e-07 8.1e-03 1.5e-05 1.00e+00 1.666374026e+02 1.666379581e+02 1.3e-10 1.17 90 2.2e-07 8.1e-03 1.4e-05 1.00e+00 1.666374385e+02 1.666379385e+02 1.2e-10 1.19 91 2.0e-07 8.1e-03 1.2e-05 1.00e+00 1.666374709e+02 1.666379208e+02 1.1e-10 1.20 92 1.8e-07 8.0e-03 1.1e-05 9.99e-01 1.666375000e+02 1.666379050e+02 9.5e-11 1.21 93 1.6e-07 8.0e-03 9.9e-06 9.99e-01 1.666375262e+02 1.666378908e+02 8.6e-11 1.23 94 1.5e-07 8.0e-03 8.9e-06 1.00e+00 1.666375497e+02 1.666378779e+02 7.7e-11 1.24 95 1.3e-07 8.0e-03 8.0e-06 1.00e+00 1.666375709e+02 1.666378663e+02 6.9e-11 1.25 96 1.2e-07 8.0e-03 7.2e-06 1.00e+00 1.666375900e+02 1.666378558e+02 6.2e-11 1.27 97 1.1e-07 7.9e-03 6.5e-06 1.00e+00 1.666376072e+02 1.666378464e+02 5.6e-11 1.28 98 9.5e-08 7.9e-03 5.8e-06 9.99e-01 1.666376226e+02 1.666378379e+02 5.1e-11 1.29 99 8.6e-08 7.9e-03 5.2e-06 1.00e+00 1.666376365e+02 1.666378303e+02 4.6e-11 1.30 100 7.7e-08 7.9e-03 4.7e-06 1.00e+00 1.666376490e+02 1.666378234e+02 4.1e-11 1.31 101 6.9e-08 7.9e-03 4.2e-06 1.00e+00 1.666376603e+02 1.666378172e+02 3.7e-11 1.33 102 6.2e-08 7.9e-03 3.8e-06 9.98e-01 1.666376704e+02 1.666378117e+02 3.3e-11 1.34 103 5.6e-08 7.8e-03 3.4e-06 1.00e+00 1.666376796e+02 1.666378067e+02 3.0e-11 1.35 104 5.1e-08 7.8e-03 3.1e-06 9.99e-01 1.666376878e+02 1.666378022e+02 2.7e-11 1.36 105 4.6e-08 7.8e-03 2.8e-06 1.00e+00 1.666376951e+02 1.666377981e+02 2.4e-11 1.38 106 4.1e-08 7.8e-03 2.5e-06 9.96e-01 1.666377018e+02 1.666377945e+02 2.2e-11 1.39 107 3.7e-08 7.8e-03 2.3e-06 9.98e-01 1.666377078e+02 1.666377912e+02 2.0e-11 1.40 108 3.3e-08 7.8e-03 2.0e-06 1.00e+00 1.666377132e+02 1.666377883e+02 1.8e-11 1.41 109 3.0e-08 7.0e-03 1.8e-06 1.01e+00 1.666377181e+02 1.666377855e+02 1.6e-11 1.42 110 2.7e-08 6.3e-03 1.6e-06 1.00e+00 1.666377224e+02 1.666377831e+02 1.4e-11 1.43 111 2.4e-08 5.7e-03 1.5e-06 1.00e+00 1.666377264e+02 1.666377810e+02 1.3e-11 1.45 112 2.2e-08 5.1e-03 1.3e-06 1.01e+00 1.666377300e+02 1.666377790e+02 1.2e-11 1.46 113 2.0e-08 4.6e-03 1.2e-06 1.00e+00 1.666377332e+02 1.666377772e+02 1.0e-11 1.47 114 2.0e-08 4.6e-03 1.2e-06 9.95e-01 1.666377333e+02 1.666377773e+02 1.0e-11 1.48 115 1.8e-08 4.1e-03 1.1e-06 9.97e-01 1.666377361e+02 1.666377757e+02 9.4e-12 1.49 116 1.6e-08 3.7e-03 9.7e-07 1.01e+00 1.666377387e+02 1.666377743e+02 8.5e-12 1.51 117 1.5e-08 3.3e-03 8.7e-07 1.01e+00 1.666377410e+02 1.666377730e+02 7.6e-12 1.52 118 1.3e-08 3.0e-03 7.8e-07 1.00e+00 1.666377431e+02 1.666377718e+02 6.9e-12 1.53 119 1.2e-08 2.7e-03 7.0e-07 9.99e-01 1.666377450e+02 1.666377708e+02 6.2e-12 1.54 120 1.1e-08 2.4e-03 6.3e-07 9.94e-01 1.666377466e+02 1.666377699e+02 5.6e-12 1.55 121 9.7e-09 2.2e-03 5.7e-07 9.92e-01 1.666377481e+02 1.666377690e+02 5.0e-12 1.56 122 9.0e-09 2.0e-03 5.1e-07 1.01e+00 1.666377495e+02 1.666377683e+02 4.5e-12 1.57 123 8.2e-09 1.8e-03 4.6e-07 9.94e-01 1.666377507e+02 1.666377676e+02 4.1e-12 1.59 124 7.3e-09 1.6e-03 4.2e-07 1.01e+00 1.666377519e+02 1.666377670e+02 3.7e-12 1.59 125 6.6e-09 1.4e-03 3.7e-07 1.00e+00 1.666377528e+02 1.666377664e+02 3.3e-12 1.61 126 5.9e-09 1.3e-03 3.4e-07 9.98e-01 1.666377537e+02 1.666377659e+02 3.0e-12 1.62 127 7.8e-09 1.2e-03 3.0e-07 9.92e-01 1.666377545e+02 1.666377655e+02 2.7e-12 1.63 128 7.0e-09 1.0e-03 2.7e-07 1.01e+00 1.666377552e+02 1.666377651e+02 2.4e-12 1.64 129 6.3e-09 9.4e-04 2.5e-07 1.04e+00 1.666377560e+02 1.666377647e+02 2.2e-12 1.65 130 4.4e-09 8.5e-04 2.2e-07 9.87e-01 1.666377566e+02 1.666377644e+02 2.0e-12 1.67 131 2.2e-08 2.4e-04 4.3e-09 7.60e-01 1.666377647e+02 1.666377650e+02 5.2e-13 1.68 Optimizer terminated. Time: 1.68 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6663776471e+02 nrm: 2e+01 Viol. con: 8e-07 var: 0e+00 Dual. obj: 1.6663776503e+02 nrm: 9e+02 Viol. con: 0e+00 var: 4e-03 * End solution on dual form. * Transforming to primal solution. Solving took 1.72 seconds. Using solver 'mosek' Solving for 1768 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 482 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: 0.02 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 873 Optimizer - Cones : 0 Optimizer - Scalar variables : 3462 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 : 1.49e+04 after factor : 1.57e+05 Factor - dense dim. : 0 flops : 3.26e+07 Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223844447e+05 2.000000000e+00 1.0e+00 0.05 1 1.7e+03 2.2e+03 8.9e+04 -9.71e-01 -1.216526186e+05 2.621307516e+00 7.3e-01 0.05 2 8.7e+02 1.1e+03 4.7e+04 -9.59e-01 -1.193637044e+05 4.626148661e+00 3.8e-01 0.06 3 2.9e+02 3.8e+02 1.5e+04 -9.21e-01 -1.103995372e+05 1.997391954e+01 1.3e-01 0.08 4 2.9e+02 3.8e+02 1.5e+04 -7.71e-01 -1.080822190e+05 2.042697686e+03 1.3e-01 0.09 5 1.2e+02 1.6e+02 6.4e+03 -7.60e-01 -8.699173306e+04 6.321800779e+03 5.3e-02 0.10 6 4.1e+01 5.4e+01 2.2e+03 -4.49e-01 -4.865820875e+04 1.101126990e+04 1.8e-02 0.11 7 2.4e+01 3.2e+01 1.3e+03 1.99e-01 -3.315603760e+04 7.461031895e+03 1.1e-02 0.12 8 1.2e+01 1.6e+01 6.5e+02 4.98e-01 -1.808984783e+04 4.488227388e+03 5.3e-03 0.14 9 4.6e+00 6.0e+00 2.5e+02 7.63e-01 -7.017022285e+03 2.200334188e+03 2.0e-03 0.15 10 2.1e+00 2.8e+00 1.1e+02 9.36e-01 -3.013574993e+03 1.298063265e+03 9.5e-04 0.16 11 1.3e+00 1.6e+00 6.8e+01 9.86e-01 -1.733134262e+03 8.404669180e+02 5.6e-04 0.17 12 8.1e-01 1.1e+00 4.4e+01 9.87e-01 -1.079217140e+03 6.046322849e+02 3.7e-04 0.19 13 6.1e-01 8.2e-01 3.3e+01 9.60e-01 -7.896096919e+02 4.869528628e+02 2.8e-04 0.20 14 3.6e-01 4.9e-01 1.9e+01 9.97e-01 -3.718428962e+02 3.755278439e+02 1.6e-04 0.21 15 1.8e-01 2.6e-01 1.0e+01 9.91e-01 -1.239916996e+02 2.622463982e+02 8.4e-05 0.23 16 8.5e-02 1.4e-01 4.7e+00 1.00e+00 2.254305964e+01 2.029655165e+02 4.0e-05 0.24 17 7.2e-02 1.1e-01 4.0e+00 1.02e+00 4.882140998e+01 2.008632442e+02 3.4e-05 0.25 18 2.2e-02 8.7e-02 1.3e+00 1.02e+00 1.302065439e+02 1.776815265e+02 1.1e-05 0.25 19 7.3e-03 1.8e-01 4.1e-01 1.01e+00 1.552256873e+02 1.707986362e+02 3.5e-06 0.27 20 2.9e-03 1.6e-01 1.7e-01 1.01e+00 1.619245831e+02 1.681612439e+02 1.4e-06 0.28 21 1.5e-03 1.0e-01 8.9e-02 1.00e+00 1.640996354e+02 1.674649706e+02 7.6e-07 0.29 22 5.3e-04 1.0e-01 3.1e-02 1.01e+00 1.656947408e+02 1.668767093e+02 2.7e-07 0.30 23 1.9e-04 1.0e-01 1.1e-02 1.01e+00 1.662324741e+02 1.666610701e+02 1.0e-07 0.31 24 1.7e-04 9.3e-02 1.0e-02 1.01e+00 1.662653398e+02 1.666509812e+02 9.0e-08 0.32 25 1.5e-04 8.5e-02 9.3e-03 1.01e+00 1.662923135e+02 1.666392585e+02 8.1e-08 0.33 26 1.4e-04 7.7e-02 8.4e-03 1.01e+00 1.663167164e+02 1.666288558e+02 7.3e-08 0.34 27 1.2e-04 7.0e-02 7.5e-03 1.01e+00 1.663385691e+02 1.666194032e+02 6.5e-08 0.35 28 1.1e-04 6.4e-02 6.8e-03 1.01e+00 1.663581774e+02 1.666108524e+02 5.9e-08 0.36 29 1.0e-04 5.8e-02 6.1e-03 1.01e+00 1.663757676e+02 1.666031129e+02 5.3e-08 0.37 30 9.1e-05 5.3e-02 5.5e-03 1.01e+00 1.663915491e+02 1.665961089e+02 4.8e-08 0.39 31 8.2e-05 4.9e-02 4.9e-03 1.01e+00 1.664057090e+02 1.665897710e+02 4.3e-08 0.40 32 7.4e-05 4.5e-02 4.4e-03 1.01e+00 1.664184151e+02 1.665840367e+02 3.9e-08 0.41 33 6.6e-05 4.1e-02 4.0e-03 1.01e+00 1.664298179e+02 1.665788495e+02 3.5e-08 0.42 34 6.0e-05 3.8e-02 3.6e-03 1.01e+00 1.664400524e+02 1.665741581e+02 3.1e-08 0.44 35 5.4e-05 3.5e-02 3.2e-03 1.00e+00 1.664492392e+02 1.665699159e+02 2.8e-08 0.45 36 4.8e-05 3.2e-02 2.9e-03 1.00e+00 1.664574865e+02 1.665660807e+02 2.5e-08 0.46 37 4.3e-05 3.0e-02 2.6e-03 1.00e+00 1.664648914e+02 1.665626140e+02 2.3e-08 0.48 38 3.9e-05 2.7e-02 2.4e-03 1.00e+00 1.664715405e+02 1.665594811e+02 2.1e-08 0.49 39 3.5e-05 2.5e-02 2.1e-03 1.00e+00 1.664775117e+02 1.665566504e+02 1.9e-08 0.50 40 3.2e-05 2.4e-02 1.9e-03 1.00e+00 1.664828746e+02 1.665540932e+02 1.7e-08 0.51 41 2.8e-05 2.2e-02 1.7e-03 1.00e+00 1.664876918e+02 1.665517834e+02 1.5e-08 0.53 42 2.6e-05 2.1e-02 1.6e-03 1.00e+00 1.664920191e+02 1.665496975e+02 1.3e-08 0.54 43 2.3e-05 1.9e-02 1.4e-03 1.00e+00 1.664959069e+02 1.665478142e+02 1.2e-08 0.55 44 2.1e-05 1.8e-02 1.3e-03 1.00e+00 1.664994001e+02 1.665461142e+02 1.1e-08 0.56 45 1.9e-05 1.7e-02 1.1e-03 1.00e+00 1.665025391e+02 1.665445798e+02 9.8e-09 0.57 46 1.7e-05 1.6e-02 1.0e-03 1.00e+00 1.665053603e+02 1.665431953e+02 8.9e-09 0.58 47 1.5e-05 1.5e-02 9.2e-04 1.00e+00 1.665078959e+02 1.665419462e+02 8.0e-09 0.59 48 1.4e-05 1.5e-02 8.2e-04 1.00e+00 1.665101753e+02 1.665408196e+02 7.2e-09 0.61 49 1.2e-05 1.4e-02 7.4e-04 1.00e+00 1.665122245e+02 1.665398036e+02 6.5e-09 0.62 50 1.1e-05 1.3e-02 6.7e-04 1.00e+00 1.665140670e+02 1.665388876e+02 5.8e-09 0.64 51 9.9e-06 1.3e-02 6.0e-04 1.00e+00 1.665157237e+02 1.665380619e+02 5.2e-09 0.65 52 8.9e-06 1.2e-02 5.4e-04 1.00e+00 1.665172136e+02 1.665373176e+02 4.7e-09 0.66 53 8.0e-06 1.2e-02 4.9e-04 1.00e+00 1.665185536e+02 1.665366470e+02 4.2e-09 0.67 54 7.2e-06 1.2e-02 4.4e-04 1.00e+00 1.665197588e+02 1.665360426e+02 3.8e-09 0.69 55 6.5e-06 1.1e-02 3.9e-04 1.00e+00 1.665208428e+02 1.665354981e+02 3.4e-09 0.70 56 5.9e-06 1.1e-02 3.6e-04 1.00e+00 1.665218178e+02 1.665350076e+02 3.1e-09 0.71 57 5.3e-06 1.1e-02 3.2e-04 1.00e+00 1.665226949e+02 1.665345656e+02 2.8e-09 0.73 58 4.8e-06 1.0e-02 2.9e-04 1.00e+00 1.665234838e+02 1.665341674e+02 2.5e-09 0.74 59 4.3e-06 1.0e-02 2.6e-04 1.00e+00 1.665241934e+02 1.665338087e+02 2.3e-09 0.75 60 3.8e-06 1.0e-02 2.3e-04 1.00e+00 1.665248317e+02 1.665334854e+02 2.0e-09 0.76 61 3.5e-06 9.8e-03 2.1e-04 1.00e+00 1.665254057e+02 1.665331941e+02 1.8e-09 0.78 62 3.1e-06 9.7e-03 1.9e-04 1.00e+00 1.665259221e+02 1.665329316e+02 1.6e-09 0.79 63 2.8e-06 9.5e-03 1.7e-04 1.00e+00 1.665263864e+02 1.665326951e+02 1.5e-09 0.80 64 2.5e-06 9.4e-03 1.5e-04 1.00e+00 1.665268042e+02 1.665324819e+02 1.3e-09 0.81 65 2.3e-06 9.2e-03 1.4e-04 1.00e+00 1.665271799e+02 1.665322899e+02 1.2e-09 0.83 66 2.0e-06 9.1e-03 1.2e-04 1.00e+00 1.665275179e+02 1.665321169e+02 1.1e-09 0.84 67 1.8e-06 9.0e-03 1.1e-04 1.00e+00 1.665278220e+02 1.665319611e+02 9.7e-10 0.85 68 1.7e-06 8.9e-03 1.0e-04 1.00e+00 1.665280955e+02 1.665318208e+02 8.7e-10 0.86 69 1.5e-06 8.9e-03 9.0e-05 1.00e+00 1.665283416e+02 1.665316944e+02 7.9e-10 0.88 70 1.3e-06 8.8e-03 8.1e-05 1.00e+00 1.665285630e+02 1.665315805e+02 7.1e-10 0.89 71 1.2e-06 8.7e-03 7.3e-05 1.00e+00 1.665287621e+02 1.665314779e+02 6.4e-10 0.90 72 1.1e-06 8.7e-03 6.6e-05 1.00e+00 1.665289413e+02 1.665313854e+02 5.7e-10 0.91 73 9.8e-07 8.6e-03 5.9e-05 1.00e+00 1.665291024e+02 1.665313022e+02 5.2e-10 0.92 74 8.8e-07 8.6e-03 5.3e-05 1.00e+00 1.665292473e+02 1.665312271e+02 4.6e-10 0.94 75 7.9e-07 8.5e-03 4.8e-05 1.00e+00 1.665293777e+02 1.665311595e+02 4.2e-10 0.95 76 7.1e-07 8.5e-03 4.3e-05 1.00e+00 1.665294950e+02 1.665310986e+02 3.8e-10 0.96 77 6.4e-07 8.4e-03 3.9e-05 1.00e+00 1.665296004e+02 1.665310437e+02 3.4e-10 0.97 78 5.8e-07 8.4e-03 3.5e-05 1.00e+00 1.665296952e+02 1.665309942e+02 3.0e-10 0.99 79 5.2e-07 8.3e-03 3.2e-05 1.00e+00 1.665297805e+02 1.665309496e+02 2.7e-10 1.00 80 4.7e-07 8.3e-03 2.8e-05 1.00e+00 1.665298572e+02 1.665309093e+02 2.5e-10 1.01 81 4.2e-07 8.3e-03 2.6e-05 1.00e+00 1.665299261e+02 1.665308731e+02 2.2e-10 1.02 82 3.8e-07 8.2e-03 2.3e-05 1.00e+00 1.665299881e+02 1.665308404e+02 2.0e-10 1.03 83 3.4e-07 8.2e-03 2.1e-05 1.00e+00 1.665300439e+02 1.665308109e+02 1.8e-10 1.04 84 3.1e-07 8.2e-03 1.9e-05 1.00e+00 1.665300941e+02 1.665307844e+02 1.6e-10 1.05 85 2.8e-07 8.2e-03 1.7e-05 1.00e+00 1.665301392e+02 1.665307605e+02 1.5e-10 1.06 86 2.5e-07 8.1e-03 1.5e-05 1.00e+00 1.665301797e+02 1.665307389e+02 1.3e-10 1.07 87 2.2e-07 8.1e-03 1.4e-05 1.00e+00 1.665302162e+02 1.665307195e+02 1.2e-10 1.08 88 2.0e-07 8.1e-03 1.2e-05 1.00e+00 1.665302490e+02 1.665307020e+02 1.1e-10 1.10 89 1.8e-07 8.1e-03 1.1e-05 1.00e+00 1.665302786e+02 1.665306863e+02 9.6e-11 1.11 90 1.6e-07 8.1e-03 9.9e-06 1.00e+00 1.665303052e+02 1.665306721e+02 8.6e-11 1.12 91 1.5e-07 8.0e-03 8.9e-06 1.00e+00 1.665303291e+02 1.665306593e+02 7.7e-11 1.13 92 1.3e-07 8.0e-03 8.0e-06 1.00e+00 1.665303506e+02 1.665306478e+02 7.0e-11 1.14 93 1.2e-07 8.0e-03 7.2e-06 1.00e+00 1.665303699e+02 1.665306374e+02 6.3e-11 1.15 94 1.1e-07 8.0e-03 6.5e-06 1.00e+00 1.665303873e+02 1.665306281e+02 5.6e-11 1.17 95 9.6e-08 8.0e-03 5.8e-06 1.00e+00 1.665304030e+02 1.665306197e+02 5.1e-11 1.18 96 8.7e-08 7.9e-03 5.3e-06 1.00e+00 1.665304171e+02 1.665306121e+02 4.6e-11 1.19 97 7.8e-08 7.9e-03 4.7e-06 1.00e+00 1.665304298e+02 1.665306053e+02 4.1e-11 1.20 98 7.0e-08 7.9e-03 4.3e-06 1.00e+00 1.665304412e+02 1.665305991e+02 3.7e-11 1.22 99 6.3e-08 7.9e-03 3.8e-06 9.99e-01 1.665304515e+02 1.665305936e+02 3.3e-11 1.23 100 5.7e-08 7.9e-03 3.4e-06 1.00e+00 1.665304607e+02 1.665305887e+02 3.0e-11 1.23 101 5.1e-08 7.8e-03 3.1e-06 1.00e+00 1.665304691e+02 1.665305842e+02 2.7e-11 1.24 102 4.6e-08 7.8e-03 2.8e-06 1.00e+00 1.665304766e+02 1.665305802e+02 2.4e-11 1.25 103 4.1e-08 7.8e-03 2.5e-06 9.99e-01 1.665304833e+02 1.665305766e+02 2.2e-11 1.26 104 3.7e-08 7.8e-03 2.3e-06 9.99e-01 1.665304894e+02 1.665305733e+02 2.0e-11 1.27 105 3.4e-08 7.8e-03 2.0e-06 9.99e-01 1.665304948e+02 1.665305704e+02 1.8e-11 1.28 106 3.0e-08 7.7e-03 1.8e-06 1.00e+00 1.665304997e+02 1.665305678e+02 1.6e-11 1.29 107 2.7e-08 7.7e-03 1.6e-06 1.00e+00 1.665305041e+02 1.665305655e+02 1.4e-11 1.30 108 2.4e-08 7.7e-03 1.5e-06 9.97e-01 1.665305081e+02 1.665305633e+02 1.3e-11 1.31 109 2.2e-08 6.9e-03 1.3e-06 1.00e+00 1.665305117e+02 1.665305614e+02 1.2e-11 1.33 110 2.0e-08 6.2e-03 1.2e-06 9.97e-01 1.665305149e+02 1.665305596e+02 1.0e-11 1.34 111 1.8e-08 5.6e-03 1.1e-06 9.97e-01 1.665305178e+02 1.665305581e+02 9.4e-12 1.35 112 1.6e-08 5.0e-03 9.7e-07 1.00e+00 1.665305205e+02 1.665305567e+02 8.5e-12 1.35 113 1.5e-08 4.5e-03 8.8e-07 9.96e-01 1.665305228e+02 1.665305554e+02 7.6e-12 1.37 114 1.3e-08 4.1e-03 7.9e-07 9.88e-01 1.665305249e+02 1.665305545e+02 6.9e-12 1.38 115 1.2e-08 3.7e-03 7.1e-07 9.88e-01 1.665305268e+02 1.665305535e+02 6.2e-12 1.39 116 1.1e-08 3.3e-03 6.4e-07 9.98e-01 1.665305285e+02 1.665305524e+02 5.6e-12 1.41 117 9.9e-09 3.0e-03 5.8e-07 9.78e-01 1.665305300e+02 1.665305517e+02 5.0e-12 1.42 118 8.9e-09 2.7e-03 5.2e-07 9.91e-01 1.665305314e+02 1.665305510e+02 4.5e-12 1.43 119 8.0e-09 2.4e-03 4.7e-07 9.99e-01 1.665305327e+02 1.665305503e+02 4.1e-12 1.44 120 7.2e-09 2.2e-03 4.2e-07 1.01e+00 1.665305338e+02 1.665305496e+02 3.7e-12 1.45 121 6.5e-09 2.0e-03 3.8e-07 9.92e-01 1.665305348e+02 1.665305491e+02 3.3e-12 1.46 122 5.9e-09 1.8e-03 3.4e-07 9.85e-01 1.665305358e+02 1.665305486e+02 3.0e-12 1.47 123 5.3e-09 1.6e-03 3.1e-07 9.93e-01 1.665305366e+02 1.665305481e+02 2.7e-12 1.48 124 4.8e-09 1.4e-03 2.8e-07 9.93e-01 1.665305373e+02 1.665305477e+02 2.4e-12 1.49 125 4.4e-09 1.3e-03 2.5e-07 9.82e-01 1.665305380e+02 1.665305473e+02 2.2e-12 1.50 126 3.9e-09 1.2e-03 2.2e-07 9.90e-01 1.665305386e+02 1.665305470e+02 2.0e-12 1.51 127 3.6e-09 1.0e-03 2.0e-07 1.00e+00 1.665305391e+02 1.665305467e+02 1.8e-12 1.52 128 3.4e-09 9.3e-04 1.8e-07 9.96e-01 1.665305396e+02 1.665305464e+02 1.6e-12 1.53 129 3.1e-09 8.4e-04 1.6e-07 1.01e+00 1.665305400e+02 1.665305462e+02 1.4e-12 1.54 130 3.3e-10 8.8e-05 1.7e-08 1.00e+00 1.665305435e+02 1.665305442e+02 1.5e-13 1.56 Optimizer terminated. Time: 1.56 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6653054354e+02 nrm: 2e+01 Viol. con: 5e-09 var: 0e+00 Dual. obj: 1.6653054419e+02 nrm: 1e+03 Viol. con: 0e+00 var: 6e-04 * End solution on dual form. * Transforming to primal solution. Solving took 1.59 seconds. Using solver 'mosek' Solving for 1768 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 482 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 873 Optimizer - Cones : 0 Optimizer - Scalar variables : 3462 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 : 1.49e+04 after factor : 1.57e+05 Factor - dense dim. : 0 flops : 3.26e+07 Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223814476e+05 2.000000000e+00 1.0e+00 0.04 1 1.7e+03 2.2e+03 8.9e+04 -9.71e-01 -1.216494472e+05 2.619367401e+00 7.3e-01 0.05 2 8.8e+02 1.1e+03 4.7e+04 -9.59e-01 -1.193668588e+05 4.615079961e+00 3.8e-01 0.06 3 2.9e+02 3.8e+02 1.5e+04 -9.22e-01 -1.103488376e+05 2.001954112e+01 1.3e-01 0.07 4 2.9e+02 3.7e+02 1.5e+04 -7.70e-01 -1.080517227e+05 2.030288678e+03 1.3e-01 0.08 5 1.2e+02 1.6e+02 6.4e+03 -7.60e-01 -8.691249091e+04 6.300042381e+03 5.3e-02 0.09 6 3.3e+01 4.4e+01 1.8e+03 -4.48e-01 -4.076173705e+04 1.195352215e+04 1.5e-02 0.10 7 2.0e+01 2.6e+01 1.1e+03 3.43e-01 -2.786822718e+04 7.429401555e+03 8.9e-03 0.11 8 1.0e+01 1.3e+01 5.5e+02 5.95e-01 -1.543124716e+04 4.210800516e+03 4.6e-03 0.13 9 3.8e+00 5.0e+00 2.0e+02 8.09e-01 -5.794203935e+03 1.901433143e+03 1.7e-03 0.14 10 2.0e+00 2.7e+00 1.1e+02 9.51e-01 -2.950006101e+03 1.198522177e+03 9.1e-04 0.15 11 8.4e-01 1.1e+00 4.6e+01 9.87e-01 -1.120062289e+03 6.297849203e+02 3.8e-04 0.16 12 8.2e-01 1.1e+00 4.4e+01 9.56e-01 -1.104063312e+03 6.055348872e+02 3.7e-04 0.17 13 5.2e-01 6.8e-01 2.8e+01 9.72e-01 -6.586925530e+02 4.339055833e+02 2.4e-04 0.18 14 3.3e-01 4.4e-01 1.8e+01 1.00e+00 -3.420367133e+02 3.489387007e+02 1.5e-04 0.20 15 1.1e-01 1.8e-01 6.4e+00 9.98e-01 -2.743178241e+01 2.173562659e+02 5.4e-05 0.21 16 8.4e-02 1.3e-01 4.7e+00 1.02e+00 2.608518550e+01 2.049294771e+02 4.0e-05 0.22 17 6.2e-02 9.8e-02 3.5e+00 1.02e+00 6.444236661e+01 1.967541398e+02 2.9e-05 0.23 18 2.0e-02 8.0e-02 1.1e+00 1.02e+00 1.340709579e+02 1.769759093e+02 9.6e-06 0.25 19 6.6e-03 1.7e-01 3.8e-01 1.01e+00 1.562513680e+02 1.703536155e+02 3.2e-06 0.26 20 2.7e-03 2.1e-01 1.6e-01 1.01e+00 1.620619472e+02 1.679613977e+02 1.3e-06 0.27 21 1.2e-03 1.2e-01 7.1e-02 1.01e+00 1.645571871e+02 1.672153103e+02 6.1e-07 0.28 22 3.4e-04 1.2e-01 2.1e-02 1.01e+00 1.659288219e+02 1.667080189e+02 1.8e-07 0.30 23 1.5e-04 1.0e-01 9.4e-03 1.01e+00 1.662327709e+02 1.665829207e+02 8.3e-08 0.31 24 7.1e-05 8.5e-02 4.4e-03 1.01e+00 1.663630105e+02 1.665261053e+02 3.9e-08 0.32 25 6.4e-05 7.7e-02 4.0e-03 1.01e+00 1.663764090e+02 1.665232521e+02 3.5e-08 0.34 26 5.8e-05 7.0e-02 3.6e-03 1.01e+00 1.663863543e+02 1.665184592e+02 3.1e-08 0.35 27 5.2e-05 6.4e-02 3.2e-03 1.01e+00 1.663954693e+02 1.665143316e+02 2.8e-08 0.36 28 4.7e-05 5.8e-02 2.9e-03 1.01e+00 1.664036141e+02 1.665105620e+02 2.6e-08 0.37 29 4.2e-05 5.3e-02 2.6e-03 1.01e+00 1.664109292e+02 1.665071595e+02 2.3e-08 0.38 30 3.8e-05 4.9e-02 2.3e-03 1.01e+00 1.664174953e+02 1.665040837e+02 2.1e-08 0.40 31 3.4e-05 4.5e-02 2.1e-03 1.01e+00 1.664233907e+02 1.665013049e+02 1.9e-08 0.41 32 3.1e-05 4.1e-02 1.9e-03 1.01e+00 1.664286846e+02 1.664987947e+02 1.7e-08 0.42 33 2.8e-05 3.8e-02 1.7e-03 1.00e+00 1.664334388e+02 1.664965276e+02 1.5e-08 0.44 34 2.5e-05 3.5e-02 1.5e-03 1.00e+00 1.664377089e+02 1.664944805e+02 1.4e-08 0.45 35 2.2e-05 3.2e-02 1.4e-03 1.00e+00 1.664415447e+02 1.664926323e+02 1.2e-08 0.46 36 2.0e-05 3.0e-02 1.2e-03 1.00e+00 1.664449907e+02 1.664909640e+02 1.1e-08 0.48 37 1.8e-05 2.8e-02 1.1e-03 1.00e+00 1.664480869e+02 1.664894583e+02 9.9e-09 0.49 38 1.6e-05 2.6e-02 1.0e-03 1.00e+00 1.664508690e+02 1.664880997e+02 8.9e-09 0.50 39 1.5e-05 2.4e-02 9.1e-04 1.00e+00 1.664533693e+02 1.664868740e+02 8.0e-09 0.51 40 1.3e-05 2.2e-02 8.2e-04 1.00e+00 1.664556164e+02 1.664857684e+02 7.2e-09 0.53 41 1.2e-05 2.1e-02 7.4e-04 1.00e+00 1.664576363e+02 1.664847712e+02 6.5e-09 0.54 42 1.1e-05 2.0e-02 6.6e-04 1.00e+00 1.664594521e+02 1.664838720e+02 5.8e-09 0.55 43 9.6e-06 1.8e-02 6.0e-04 1.00e+00 1.664610846e+02 1.664830613e+02 5.3e-09 0.57 44 8.7e-06 1.7e-02 5.4e-04 1.00e+00 1.664625525e+02 1.664823305e+02 4.7e-09 0.58 45 7.8e-06 1.6e-02 4.8e-04 1.00e+00 1.664638724e+02 1.664816719e+02 4.3e-09 0.59 46 7.0e-06 1.6e-02 4.3e-04 1.00e+00 1.664650594e+02 1.664810783e+02 3.8e-09 0.61 47 6.3e-06 1.5e-02 3.9e-04 1.00e+00 1.664661269e+02 1.664805435e+02 3.5e-09 0.62 48 5.7e-06 1.4e-02 3.5e-04 1.00e+00 1.664670870e+02 1.664800616e+02 3.1e-09 0.63 49 5.1e-06 1.3e-02 3.2e-04 1.00e+00 1.664679506e+02 1.664796275e+02 2.8e-09 0.64 50 4.6e-06 1.3e-02 2.9e-04 1.00e+00 1.664687275e+02 1.664792364e+02 2.5e-09 0.65 51 4.1e-06 1.2e-02 2.6e-04 1.00e+00 1.664694263e+02 1.664788842e+02 2.3e-09 0.67 52 3.7e-06 1.2e-02 2.3e-04 1.00e+00 1.664700549e+02 1.664785668e+02 2.0e-09 0.68 53 3.4e-06 1.2e-02 2.1e-04 1.00e+00 1.664706203e+02 1.664782810e+02 1.8e-09 0.69 54 3.0e-06 1.1e-02 1.9e-04 1.00e+00 1.664711290e+02 1.664780235e+02 1.7e-09 0.71 55 2.7e-06 1.1e-02 1.7e-04 1.00e+00 1.664715866e+02 1.664777916e+02 1.5e-09 0.72 56 2.4e-06 1.1e-02 1.5e-04 1.00e+00 1.664719983e+02 1.664775828e+02 1.3e-09 0.73 57 2.2e-06 1.0e-02 1.4e-04 1.00e+00 1.664723688e+02 1.664773948e+02 1.2e-09 0.74 58 2.0e-06 1.0e-02 1.2e-04 1.00e+00 1.664727021e+02 1.664772255e+02 1.1e-09 0.75 59 1.8e-06 9.8e-03 1.1e-04 1.00e+00 1.664730022e+02 1.664770732e+02 9.8e-10 0.77 60 1.6e-06 9.6e-03 9.9e-05 1.00e+00 1.664732721e+02 1.664769360e+02 8.8e-10 0.77 61 1.4e-06 9.4e-03 9.0e-05 1.00e+00 1.664735151e+02 1.664768126e+02 7.9e-10 0.78 62 1.3e-06 9.3e-03 8.1e-05 1.00e+00 1.664737337e+02 1.664767015e+02 7.1e-10 0.80 63 1.2e-06 9.1e-03 7.3e-05 1.00e+00 1.664739305e+02 1.664766015e+02 6.4e-10 0.81 64 1.1e-06 9.0e-03 6.5e-05 1.00e+00 1.664741076e+02 1.664765115e+02 5.8e-10 0.82 65 9.5e-07 8.9e-03 5.9e-05 1.00e+00 1.664742669e+02 1.664764304e+02 5.2e-10 0.82 66 8.5e-07 8.8e-03 5.3e-05 1.00e+00 1.664744103e+02 1.664763575e+02 4.7e-10 0.84 67 7.7e-07 8.7e-03 4.8e-05 1.00e+00 1.664745393e+02 1.664762918e+02 4.2e-10 0.85 68 6.9e-07 8.6e-03 4.3e-05 1.00e+00 1.664746554e+02 1.664762326e+02 3.8e-10 0.86 69 6.2e-07 8.5e-03 3.9e-05 1.00e+00 1.664747598e+02 1.664761793e+02 3.4e-10 0.88 70 5.6e-07 8.4e-03 3.5e-05 1.00e+00 1.664748538e+02 1.664761313e+02 3.1e-10 0.89 71 5.0e-07 8.4e-03 3.1e-05 1.00e+00 1.664749383e+02 1.664760881e+02 2.8e-10 0.90 72 4.5e-07 8.3e-03 2.8e-05 1.00e+00 1.664750143e+02 1.664760492e+02 2.5e-10 0.92 73 4.1e-07 8.3e-03 2.5e-05 1.00e+00 1.664750827e+02 1.664760141e+02 2.2e-10 0.93 74 3.7e-07 8.2e-03 2.3e-05 1.00e+00 1.664751442e+02 1.664759824e+02 2.0e-10 0.94 75 3.3e-07 8.2e-03 2.0e-05 1.00e+00 1.664751995e+02 1.664759540e+02 1.8e-10 0.96 76 3.0e-07 8.1e-03 1.8e-05 1.00e+00 1.664752493e+02 1.664759283e+02 1.6e-10 0.97 77 2.7e-07 8.1e-03 1.7e-05 1.00e+00 1.664752941e+02 1.664759052e+02 1.5e-10 0.98 78 2.4e-07 8.1e-03 1.5e-05 1.00e+00 1.664753344e+02 1.664758844e+02 1.3e-10 0.99 79 2.2e-07 8.0e-03 1.3e-05 1.00e+00 1.664753707e+02 1.664758656e+02 1.2e-10 1.01 80 2.0e-07 8.0e-03 1.2e-05 1.00e+00 1.664754033e+02 1.664758488e+02 1.1e-10 1.02 81 1.8e-07 8.0e-03 1.1e-05 1.00e+00 1.664754326e+02 1.664758336e+02 9.6e-11 1.03 82 1.6e-07 7.9e-03 9.8e-06 1.00e+00 1.664754590e+02 1.664758199e+02 8.7e-11 1.04 83 1.4e-07 7.9e-03 8.8e-06 1.00e+00 1.664754828e+02 1.664758076e+02 7.8e-11 1.05 84 1.3e-07 7.9e-03 7.9e-06 1.00e+00 1.664755042e+02 1.664757965e+02 7.0e-11 1.07 85 1.2e-07 7.9e-03 7.1e-06 1.00e+00 1.664755234e+02 1.664757865e+02 6.3e-11 1.08 86 1.0e-07 7.8e-03 6.4e-06 1.00e+00 1.664755408e+02 1.664757775e+02 5.7e-11 1.09 87 9.3e-08 7.8e-03 5.8e-06 1.00e+00 1.664755563e+02 1.664757694e+02 5.1e-11 1.10 88 8.4e-08 7.8e-03 5.2e-06 9.99e-01 1.664755704e+02 1.664757622e+02 4.6e-11 1.12 89 7.6e-08 7.8e-03 4.7e-06 1.00e+00 1.664755830e+02 1.664757556e+02 4.1e-11 1.13 90 6.8e-08 7.8e-03 4.2e-06 9.97e-01 1.664755943e+02 1.664757497e+02 3.7e-11 1.14 91 6.1e-08 7.8e-03 3.8e-06 1.00e+00 1.664756046e+02 1.664757444e+02 3.4e-11 1.15 92 5.5e-08 7.7e-03 3.4e-06 9.99e-01 1.664756138e+02 1.664757396e+02 3.0e-11 1.16 93 5.0e-08 7.7e-03 3.1e-06 1.00e+00 1.664756220e+02 1.664757353e+02 2.7e-11 1.18 94 4.5e-08 7.7e-03 2.8e-06 1.00e+00 1.664756295e+02 1.664757314e+02 2.4e-11 1.19 95 4.0e-08 7.7e-03 2.5e-06 1.00e+00 1.664756362e+02 1.664757279e+02 2.2e-11 1.20 96 3.6e-08 7.7e-03 2.2e-06 1.00e+00 1.664756422e+02 1.664757248e+02 2.0e-11 1.22 97 3.3e-08 7.7e-03 2.0e-06 1.00e+00 1.664756477e+02 1.664757220e+02 1.8e-11 1.23 98 2.9e-08 7.7e-03 1.8e-06 1.00e+00 1.664756526e+02 1.664757194e+02 1.6e-11 1.24 99 2.6e-08 7.7e-03 1.6e-06 1.00e+00 1.664756570e+02 1.664757171e+02 1.4e-11 1.26 100 2.4e-08 7.6e-03 1.5e-06 1.00e+00 1.664756609e+02 1.664757151e+02 1.3e-11 1.26 101 2.1e-08 7.6e-03 1.3e-06 1.00e+00 1.664756645e+02 1.664757132e+02 1.2e-11 1.27 102 1.9e-08 7.6e-03 1.2e-06 1.00e+00 1.664756677e+02 1.664757116e+02 1.1e-11 1.28 103 1.7e-08 7.6e-03 1.1e-06 9.94e-01 1.664756706e+02 1.664757101e+02 9.5e-12 1.29 104 1.6e-08 6.8e-03 9.7e-07 1.00e+00 1.664756732e+02 1.664757087e+02 8.5e-12 1.31 105 1.4e-08 6.2e-03 8.7e-07 1.01e+00 1.664756756e+02 1.664757075e+02 7.7e-12 1.32 106 1.3e-08 5.5e-03 7.8e-07 1.00e+00 1.664756777e+02 1.664757064e+02 6.9e-12 1.33 107 1.1e-08 5.0e-03 7.0e-07 1.00e+00 1.664756795e+02 1.664757054e+02 6.2e-12 1.35 108 1.0e-08 4.5e-03 6.3e-07 9.95e-01 1.664756812e+02 1.664757045e+02 5.6e-12 1.36 109 9.2e-09 4.0e-03 5.7e-07 1.01e+00 1.664756828e+02 1.664757037e+02 5.1e-12 1.37 110 3.5e-09 4.1e-04 5.8e-08 9.98e-01 1.664756951e+02 1.664756973e+02 5.3e-13 1.38 Optimizer terminated. Time: 1.39 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6647569515e+02 nrm: 2e+01 Viol. con: 1e-07 var: 0e+00 Dual. obj: 1.6647569729e+02 nrm: 1e+03 Viol. con: 0e+00 var: 3e-03 * End solution on dual form. * Transforming to primal solution. Solving took 1.42 seconds. Using solver 'mosek' Solving for 1768 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (313) 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 482 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 873 Optimizer - Cones : 0 Optimizer - Scalar variables : 3462 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 : 1.49e+04 after factor : 1.57e+05 Factor - dense dim. : 0 flops : 3.26e+07 Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223801642e+05 2.000000000e+00 1.0e+00 0.04 1 1.7e+03 2.2e+03 8.9e+04 -9.71e-01 -1.216483304e+05 2.618565322e+00 7.3e-01 0.05 2 8.8e+02 1.1e+03 4.7e+04 -9.59e-01 -1.193676752e+05 4.610922688e+00 3.8e-01 0.06 3 2.9e+02 3.8e+02 1.5e+04 -9.22e-01 -1.103165945e+05 2.004323456e+01 1.3e-01 0.07 4 2.9e+02 3.7e+02 1.5e+04 -7.70e-01 -1.080284782e+05 2.025515228e+03 1.3e-01 0.08 5 1.2e+02 1.5e+02 6.3e+03 -7.60e-01 -8.689193228e+04 6.277145300e+03 5.2e-02 0.10 6 2.9e+01 3.7e+01 1.5e+03 -4.47e-01 -3.555978381e+04 1.254685311e+04 1.3e-02 0.11 7 1.8e+01 2.4e+01 9.7e+02 4.41e-01 -2.517278879e+04 7.242664304e+03 8.0e-03 0.12 8 1.0e+01 1.3e+01 5.5e+02 6.44e-01 -1.529020587e+04 4.344385208e+03 4.5e-03 0.13 9 3.9e+00 5.1e+00 2.1e+02 8.11e-01 -6.021009645e+03 1.946579789e+03 1.8e-03 0.14 10 2.0e+00 2.6e+00 1.1e+02 9.48e-01 -2.964906920e+03 1.186949867e+03 9.1e-04 0.16 11 8.4e-01 1.1e+00 4.6e+01 9.87e-01 -1.106052242e+03 6.319965104e+02 3.8e-04 0.17 12 8.1e-01 1.1e+00 4.4e+01 9.51e-01 -1.097849102e+03 6.089590342e+02 3.7e-04 0.18 13 5.2e-01 6.8e-01 2.8e+01 9.70e-01 -6.574957640e+02 4.370627639e+02 2.4e-04 0.20 14 3.2e-01 4.3e-01 1.8e+01 1.00e+00 -3.348534794e+02 3.460902080e+02 1.5e-04 0.21 15 1.1e-01 1.7e-01 6.2e+00 9.99e-01 -2.180331029e+01 2.157527514e+02 5.2e-05 0.22 16 8.5e-02 1.3e-01 4.7e+00 1.02e+00 2.564071194e+01 2.060915714e+02 4.0e-05 0.23 17 4.8e-02 9.3e-02 2.7e+00 1.02e+00 8.830023858e+01 1.901940651e+02 2.3e-05 0.25 18 1.2e-02 1.7e-01 7.0e-01 1.02e+00 1.470192463e+02 1.734322407e+02 5.9e-06 0.25 19 3.5e-03 2.1e-01 2.1e-01 1.01e+00 1.607382761e+02 1.684750030e+02 1.7e-06 0.27 20 2.1e-03 2.2e-01 1.2e-01 1.00e+00 1.630800225e+02 1.676831725e+02 1.0e-06 0.28 21 6.2e-04 1.5e-01 3.7e-02 1.01e+00 1.654579564e+02 1.668570066e+02 3.2e-07 0.29 22 4.6e-04 1.2e-01 2.8e-02 9.95e-01 1.657162583e+02 1.667485014e+02 2.4e-07 0.31 23 2.4e-04 8.3e-02 1.5e-02 9.83e-01 1.660592328e+02 1.666093529e+02 1.3e-07 0.32 24 2.0e-04 7.0e-02 1.2e-02 1.00e+00 1.661253009e+02 1.665865316e+02 1.1e-07 0.33 25 1.8e-04 6.4e-02 1.1e-02 1.01e+00 1.661586806e+02 1.665735495e+02 9.6e-08 0.34 26 1.6e-04 5.9e-02 1.0e-02 1.01e+00 1.661875497e+02 1.665608333e+02 8.7e-08 0.35 27 1.5e-04 5.3e-02 9.0e-03 1.01e+00 1.662136630e+02 1.665495611e+02 7.8e-08 0.36 28 1.3e-04 4.9e-02 8.1e-03 1.00e+00 1.662370559e+02 1.665393192e+02 7.0e-08 0.37 29 1.2e-04 4.5e-02 7.3e-03 1.00e+00 1.662580556e+02 1.665300572e+02 6.3e-08 0.38 30 1.1e-04 4.1e-02 6.6e-03 1.00e+00 1.662769026e+02 1.665216766e+02 5.7e-08 0.39 31 9.6e-05 3.8e-02 5.9e-03 1.00e+00 1.662938192e+02 1.665140945e+02 5.1e-08 0.40 32 8.7e-05 3.5e-02 5.3e-03 1.00e+00 1.663090035e+02 1.665072347e+02 4.6e-08 0.41 33 7.8e-05 3.2e-02 4.8e-03 1.00e+00 1.663226331e+02 1.665010285e+02 4.2e-08 0.43 34 7.0e-05 3.0e-02 4.3e-03 1.00e+00 1.663348676e+02 1.664954137e+02 3.7e-08 0.44 35 6.3e-05 2.7e-02 3.9e-03 1.00e+00 1.663458504e+02 1.664903343e+02 3.4e-08 0.45 36 5.7e-05 2.5e-02 3.5e-03 1.00e+00 1.663557101e+02 1.664857397e+02 3.0e-08 0.46 37 5.1e-05 2.4e-02 3.1e-03 1.00e+00 1.663645623e+02 1.664815845e+02 2.7e-08 0.47 38 4.6e-05 2.2e-02 2.8e-03 1.00e+00 1.663725107e+02 1.664778272e+02 2.5e-08 0.48 39 4.1e-05 2.1e-02 2.6e-03 1.00e+00 1.663796481e+02 1.664744304e+02 2.2e-08 0.49 40 3.7e-05 1.9e-02 2.3e-03 1.00e+00 1.663860580e+02 1.664713600e+02 2.0e-08 0.51 41 3.4e-05 1.8e-02 2.1e-03 1.00e+00 1.663918150e+02 1.664685853e+02 1.8e-08 0.52 42 3.0e-05 1.7e-02 1.9e-03 1.00e+00 1.663969860e+02 1.664660781e+02 1.6e-08 0.53 43 2.7e-05 1.6e-02 1.7e-03 1.00e+00 1.664016309e+02 1.664638129e+02 1.5e-08 0.54 44 2.5e-05 1.5e-02 1.5e-03 1.00e+00 1.664058036e+02 1.664617668e+02 1.3e-08 0.56 45 2.2e-05 1.5e-02 1.4e-03 1.00e+00 1.664095523e+02 1.664599187e+02 1.2e-08 0.57 46 2.0e-05 1.4e-02 1.2e-03 1.00e+00 1.664129203e+02 1.664582497e+02 1.1e-08 0.58 47 1.8e-05 1.3e-02 1.1e-03 1.00e+00 1.664159464e+02 1.664567427e+02 9.5e-09 0.60 48 1.6e-05 1.3e-02 9.9e-04 1.00e+00 1.664186655e+02 1.664553820e+02 8.6e-09 0.60 49 1.4e-05 1.2e-02 8.9e-04 1.00e+00 1.664211089e+02 1.664541537e+02 7.7e-09 0.61 50 1.3e-05 1.2e-02 8.0e-04 1.00e+00 1.664233046e+02 1.664530450e+02 6.9e-09 0.62 51 1.2e-05 1.1e-02 7.2e-04 1.00e+00 1.664252780e+02 1.664520443e+02 6.3e-09 0.64 52 1.1e-05 1.1e-02 6.5e-04 1.00e+00 1.664270516e+02 1.664511413e+02 5.6e-09 0.64 53 9.5e-06 1.1e-02 5.8e-04 1.00e+00 1.664286458e+02 1.664503266e+02 5.1e-09 0.65 54 8.5e-06 1.1e-02 5.3e-04 1.00e+00 1.664300788e+02 1.664495916e+02 4.6e-09 0.66 55 7.7e-06 1.0e-02 4.7e-04 1.00e+00 1.664313669e+02 1.664489285e+02 4.1e-09 0.67 56 6.9e-06 1.0e-02 4.3e-04 1.00e+00 1.664325250e+02 1.664483305e+02 3.7e-09 0.69 57 6.2e-06 9.9e-03 3.8e-04 1.00e+00 1.664335662e+02 1.664477912e+02 3.3e-09 0.70 58 5.6e-06 9.7e-03 3.4e-04 1.00e+00 1.664345023e+02 1.664473049e+02 3.0e-09 0.71 59 5.0e-06 9.5e-03 3.1e-04 1.00e+00 1.664353439e+02 1.664468664e+02 2.7e-09 0.72 60 4.5e-06 9.4e-03 2.8e-04 1.00e+00 1.664361007e+02 1.664464710e+02 2.4e-09 0.73 61 4.1e-06 9.2e-03 2.5e-04 1.00e+00 1.664367812e+02 1.664461145e+02 2.2e-09 0.74 62 3.7e-06 9.1e-03 2.3e-04 1.00e+00 1.664373931e+02 1.664457931e+02 2.0e-09 0.76 63 3.3e-06 9.0e-03 2.0e-04 1.00e+00 1.664379433e+02 1.664455033e+02 1.8e-09 0.77 64 3.0e-06 8.9e-03 1.8e-04 1.00e+00 1.664384380e+02 1.664452421e+02 1.6e-09 0.78 65 2.7e-06 8.8e-03 1.7e-04 1.00e+00 1.664388829e+02 1.664450067e+02 1.4e-09 0.79 66 2.4e-06 8.7e-03 1.5e-04 1.00e+00 1.664392831e+02 1.664447945e+02 1.3e-09 0.80 67 2.2e-06 8.6e-03 1.3e-04 1.00e+00 1.664396430e+02 1.664446034e+02 1.2e-09 0.80 68 2.0e-06 8.6e-03 1.2e-04 1.00e+00 1.664399668e+02 1.664444312e+02 1.0e-09 0.81 69 1.8e-06 8.5e-03 1.1e-04 1.00e+00 1.664402581e+02 1.664442761e+02 9.4e-10 0.83 70 1.6e-06 8.4e-03 9.7e-05 1.00e+00 1.664405202e+02 1.664441363e+02 8.5e-10 0.84 71 1.4e-06 8.4e-03 8.8e-05 1.00e+00 1.664407559e+02 1.664440105e+02 7.6e-10 0.85 72 1.3e-06 8.3e-03 7.9e-05 1.00e+00 1.664409680e+02 1.664438972e+02 6.9e-10 0.86 73 1.2e-06 8.3e-03 7.1e-05 1.00e+00 1.664411588e+02 1.664437951e+02 6.2e-10 0.87 74 1.0e-06 8.2e-03 6.4e-05 1.00e+00 1.664413305e+02 1.664437031e+02 5.6e-10 0.88 75 9.3e-07 8.2e-03 5.8e-05 1.00e+00 1.664414849e+02 1.664436203e+02 5.0e-10 0.89 76 8.4e-07 8.1e-03 5.2e-05 1.00e+00 1.664416238e+02 1.664435457e+02 4.5e-10 0.90 77 7.6e-07 8.1e-03 4.7e-05 1.00e+00 1.664417488e+02 1.664434785e+02 4.0e-10 0.90 78 6.8e-07 8.1e-03 4.2e-05 1.00e+00 1.664418612e+02 1.664434180e+02 3.6e-10 0.91 79 6.1e-07 8.0e-03 3.8e-05 1.00e+00 1.664419624e+02 1.664433635e+02 3.3e-10 0.93 80 5.5e-07 8.0e-03 3.4e-05 1.00e+00 1.664420534e+02 1.664433144e+02 3.0e-10 0.94 81 5.0e-07 8.0e-03 3.1e-05 1.00e+00 1.664421352e+02 1.664432702e+02 2.7e-10 0.95 82 4.5e-07 7.9e-03 2.8e-05 1.00e+00 1.664422089e+02 1.664432303e+02 2.4e-10 0.96 83 4.0e-07 7.9e-03 2.5e-05 1.00e+00 1.664422751e+02 1.664431944e+02 2.2e-10 0.97 84 3.6e-07 7.9e-03 2.2e-05 1.00e+00 1.664423347e+02 1.664431621e+02 1.9e-10 0.98 85 3.3e-07 7.9e-03 2.0e-05 1.00e+00 1.664423883e+02 1.664431330e+02 1.7e-10 0.99 86 2.9e-07 7.8e-03 1.8e-05 1.00e+00 1.664424366e+02 1.664431067e+02 1.6e-10 1.00 87 2.6e-07 7.8e-03 1.6e-05 1.00e+00 1.664424800e+02 1.664430831e+02 1.4e-10 1.01 88 2.4e-07 7.8e-03 1.5e-05 1.00e+00 1.664425190e+02 1.664430619e+02 1.3e-10 1.02 89 2.1e-07 7.8e-03 1.3e-05 1.00e+00 1.664425542e+02 1.664430428e+02 1.1e-10 1.03 90 1.9e-07 7.8e-03 1.2e-05 1.00e+00 1.664425858e+02 1.664430256e+02 1.0e-10 1.04 91 1.7e-07 7.8e-03 1.1e-05 1.00e+00 1.664426143e+02 1.664430101e+02 9.3e-11 1.05 92 1.6e-07 7.7e-03 9.6e-06 1.00e+00 1.664426399e+02 1.664429961e+02 8.3e-11 1.06 93 1.4e-07 7.7e-03 8.6e-06 1.00e+00 1.664426630e+02 1.664429836e+02 7.5e-11 1.07 94 1.3e-07 7.7e-03 7.8e-06 1.00e+00 1.664426838e+02 1.664429723e+02 6.8e-11 1.08 95 1.1e-07 7.7e-03 7.0e-06 1.00e+00 1.664427025e+02 1.664429622e+02 6.1e-11 1.09 96 1.0e-07 7.7e-03 6.3e-06 1.00e+00 1.664427193e+02 1.664429530e+02 5.5e-11 1.10 97 9.2e-08 7.7e-03 5.7e-06 1.00e+00 1.664427344e+02 1.664429448e+02 4.9e-11 1.11 98 8.3e-08 7.7e-03 5.1e-06 9.99e-01 1.664427480e+02 1.664429374e+02 4.4e-11 1.12 99 7.5e-08 7.6e-03 4.6e-06 1.00e+00 1.664427603e+02 1.664429307e+02 4.0e-11 1.13 100 6.7e-08 7.6e-03 4.1e-06 1.00e+00 1.664427713e+02 1.664429247e+02 3.6e-11 1.14 101 6.0e-08 7.6e-03 3.7e-06 1.00e+00 1.664427813e+02 1.664429193e+02 3.2e-11 1.15 102 5.4e-08 7.6e-03 3.3e-06 9.98e-01 1.664427902e+02 1.664429145e+02 2.9e-11 1.16 103 4.9e-08 7.6e-03 3.0e-06 1.00e+00 1.664427983e+02 1.664429101e+02 2.6e-11 1.17 104 4.4e-08 7.6e-03 2.7e-06 1.00e+00 1.664428055e+02 1.664429062e+02 2.4e-11 1.18 105 4.0e-08 7.6e-03 2.4e-06 1.00e+00 1.664428120e+02 1.664429026e+02 2.1e-11 1.19 106 3.6e-08 7.6e-03 2.2e-06 1.00e+00 1.664428179e+02 1.664428994e+02 1.9e-11 1.20 107 3.2e-08 7.6e-03 2.0e-06 9.97e-01 1.664428232e+02 1.664428966e+02 1.7e-11 1.21 108 2.9e-08 7.6e-03 1.8e-06 9.99e-01 1.664428279e+02 1.664428940e+02 1.5e-11 1.22 109 2.6e-08 7.5e-03 1.6e-06 9.96e-01 1.664428322e+02 1.664428917e+02 1.4e-11 1.23 110 2.3e-08 7.5e-03 1.4e-06 9.98e-01 1.664428360e+02 1.664428896e+02 1.3e-11 1.24 111 2.1e-08 6.8e-03 1.3e-06 1.00e+00 1.664428395e+02 1.664428877e+02 1.1e-11 1.24 112 1.9e-08 6.1e-03 1.2e-06 9.97e-01 1.664428426e+02 1.664428860e+02 1.0e-11 1.26 113 1.7e-08 5.5e-03 1.1e-06 1.00e+00 1.664428454e+02 1.664428845e+02 9.1e-12 1.27 114 1.6e-08 4.9e-03 9.5e-07 1.00e+00 1.664428480e+02 1.664428831e+02 8.2e-12 1.28 115 1.4e-08 4.4e-03 8.5e-07 1.01e+00 1.664428503e+02 1.664428818e+02 7.4e-12 1.29 116 1.3e-08 4.0e-03 7.7e-07 1.00e+00 1.664428524e+02 1.664428807e+02 6.7e-12 1.30 117 1.2e-08 4.0e-03 6.9e-07 9.96e-01 1.664428541e+02 1.664428800e+02 6.0e-12 1.31 118 1.0e-08 3.6e-03 6.2e-07 9.92e-01 1.664428558e+02 1.664428791e+02 5.4e-12 1.32 119 9.2e-09 3.2e-03 5.6e-07 1.02e+00 1.664428574e+02 1.664428781e+02 4.9e-12 1.33 120 8.3e-09 2.9e-03 5.0e-07 9.88e-01 1.664428587e+02 1.664428774e+02 4.4e-12 1.34 121 7.5e-09 2.6e-03 4.5e-07 1.02e+00 1.664428601e+02 1.664428766e+02 4.0e-12 1.35 122 6.8e-09 2.3e-03 4.1e-07 9.75e-01 1.664428611e+02 1.664428760e+02 3.6e-12 1.36 123 6.1e-09 2.1e-03 3.7e-07 1.02e+00 1.664428621e+02 1.664428755e+02 3.3e-12 1.37 124 5.5e-09 1.9e-03 3.3e-07 9.96e-01 1.664428630e+02 1.664428750e+02 3.0e-12 1.39 125 5.0e-09 1.7e-03 3.0e-07 1.00e+00 1.664428638e+02 1.664428746e+02 2.7e-12 1.40 126 4.5e-09 1.5e-03 2.7e-07 9.84e-01 1.664428645e+02 1.664428742e+02 2.4e-12 1.41 127 4.6e-08 1.5e-03 2.6e-07 9.86e-01 1.664428643e+02 1.664428750e+02 2.3e-12 1.43 128 3.6e-08 1.4e-03 2.4e-07 1.06e+00 1.664428651e+02 1.664428743e+02 2.1e-12 1.44 129 3.2e-08 1.2e-03 2.1e-07 9.94e-01 1.664428657e+02 1.664428740e+02 1.9e-12 1.45 130 2.9e-08 1.1e-03 1.9e-07 1.03e+00 1.664428663e+02 1.664428736e+02 1.8e-12 1.45 131 2.6e-08 9.9e-04 1.7e-07 9.43e-01 1.664428667e+02 1.664428733e+02 1.6e-12 1.47 132 2.3e-08 8.9e-04 1.5e-07 1.01e+00 1.664428671e+02 1.664428731e+02 1.4e-12 1.48 133 2.1e-08 8.0e-04 1.4e-07 1.02e+00 1.664428675e+02 1.664428728e+02 1.3e-12 1.49 134 1.9e-08 7.2e-04 1.3e-07 1.01e+00 1.664428678e+02 1.664428726e+02 1.2e-12 1.50 135 1.7e-08 6.5e-04 1.1e-07 9.86e-01 1.664428681e+02 1.664428724e+02 1.1e-12 1.52 136 1.5e-08 5.8e-04 1.0e-07 9.94e-01 1.664428684e+02 1.664428722e+02 9.6e-13 1.53 Optimizer terminated. Time: 1.53 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6644286838e+02 nrm: 2e+01 Viol. con: 4e-07 var: 0e+00 Dual. obj: 1.6644287224e+02 nrm: 1e+03 Viol. con: 0e+00 var: 4e-03 * End solution on dual form. * Transforming to primal solution. Solving took 1.56 seconds. Using solver 'mosek' Solving for 1768 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 482 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: 0.02 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 873 Optimizer - Cones : 0 Optimizer - Scalar variables : 3462 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 : 1.49e+04 after factor : 1.57e+05 Factor - dense dim. : 0 flops : 3.26e+07 Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223796803e+05 2.000000000e+00 1.0e+00 0.05 1 1.7e+03 2.2e+03 8.9e+04 -9.71e-01 -1.216476084e+05 2.618554922e+00 7.3e-01 0.06 2 8.8e+02 1.1e+03 4.7e+04 -9.59e-01 -1.193666125e+05 4.610537506e+00 3.8e-01 0.08 3 2.9e+02 3.7e+02 1.5e+04 -9.22e-01 -1.102966097e+05 2.005786766e+01 1.3e-01 0.09 4 2.9e+02 3.7e+02 1.5e+04 -7.69e-01 -1.080118792e+05 2.024242288e+03 1.3e-01 0.10 5 1.2e+02 1.5e+02 6.3e+03 -7.60e-01 -8.686643901e+04 6.264842071e+03 5.2e-02 0.11 6 2.7e+01 3.5e+01 1.5e+03 -4.47e-01 -3.361423875e+04 1.275613178e+04 1.2e-02 0.13 7 1.7e+01 2.2e+01 9.2e+02 4.78e-01 -2.409624449e+04 7.121560004e+03 7.6e-03 0.14 8 1.0e+01 1.3e+01 5.3e+02 6.63e-01 -1.491091001e+04 4.313499207e+03 4.4e-03 0.15 9 3.8e+00 5.0e+00 2.1e+02 8.17e-01 -5.882084267e+03 1.917880415e+03 1.7e-03 0.16 10 2.0e+00 2.6e+00 1.1e+02 9.49e-01 -2.856912142e+03 1.168394898e+03 8.8e-04 0.17 11 8.4e-01 1.1e+00 4.6e+01 9.87e-01 -1.134284740e+03 6.217436659e+02 3.8e-04 0.18 12 8.2e-01 1.1e+00 4.5e+01 9.52e-01 -1.122688405e+03 5.985078074e+02 3.7e-04 0.19 13 5.2e-01 6.8e-01 2.8e+01 9.70e-01 -6.636991795e+02 4.331771302e+02 2.4e-04 0.20 14 3.0e-01 4.1e-01 1.7e+01 1.00e+00 -3.097111699e+02 3.352546183e+02 1.4e-04 0.22 15 1.1e-01 1.7e-01 5.9e+00 1.00e+00 -1.482958391e+01 2.136502396e+02 5.0e-05 0.23 16 8.4e-02 1.3e-01 4.7e+00 1.02e+00 2.760730165e+01 2.071351104e+02 4.0e-05 0.24 17 4.8e-02 9.4e-02 2.7e+00 1.02e+00 8.723176146e+01 1.898083063e+02 2.3e-05 0.26 18 1.6e-02 9.0e-02 8.7e-01 1.02e+00 1.418963690e+02 1.747571509e+02 7.4e-06 0.27 19 7.2e-03 7.0e-02 4.1e-01 1.01e+00 1.546961115e+02 1.700499165e+02 3.5e-06 0.28 20 1.7e-03 1.6e-01 1.0e-01 1.01e+00 1.636916571e+02 1.675254609e+02 8.6e-07 0.29 21 1.0e-03 1.1e-01 6.3e-02 9.76e-01 1.647504813e+02 1.670947428e+02 5.3e-07 0.30 22 3.5e-04 1.2e-01 2.2e-02 9.86e-01 1.658617377e+02 1.666773466e+02 1.9e-07 0.32 23 1.6e-04 9.6e-02 1.0e-02 1.00e+00 1.661549018e+02 1.665439119e+02 9.0e-08 0.33 24 6.2e-05 9.2e-02 4.0e-03 1.01e+00 1.663208740e+02 1.664687668e+02 3.5e-08 0.34 25 3.0e-05 7.9e-02 1.9e-03 1.01e+00 1.663730748e+02 1.664449304e+02 1.7e-08 0.35 26 2.7e-05 7.3e-02 1.7e-03 1.01e+00 1.663788267e+02 1.664435430e+02 1.5e-08 0.37 27 2.4e-05 6.6e-02 1.6e-03 1.01e+00 1.663831112e+02 1.664413337e+02 1.4e-08 0.38 28 2.2e-05 6.0e-02 1.4e-03 1.01e+00 1.663870609e+02 1.664394512e+02 1.2e-08 0.39 29 2.0e-05 5.5e-02 1.3e-03 1.01e+00 1.663905952e+02 1.664377370e+02 1.1e-08 0.40 30 1.8e-05 5.0e-02 1.1e-03 1.00e+00 1.663937727e+02 1.664361929e+02 1.0e-08 0.41 31 1.6e-05 4.6e-02 1.0e-03 1.00e+00 1.663966270e+02 1.664347990e+02 9.0e-09 0.42 32 1.4e-05 4.2e-02 9.2e-04 1.00e+00 1.663991915e+02 1.664335414e+02 8.1e-09 0.44 33 1.3e-05 3.9e-02 8.3e-04 1.00e+00 1.664014960e+02 1.664324068e+02 7.3e-09 0.45 34 1.2e-05 3.6e-02 7.5e-04 1.00e+00 1.664035668e+02 1.664313834e+02 6.6e-09 0.46 35 1.0e-05 3.3e-02 6.7e-04 1.00e+00 1.664054279e+02 1.664304602e+02 5.9e-09 0.47 36 9.4e-06 3.1e-02 6.1e-04 1.00e+00 1.664071006e+02 1.664296277e+02 5.3e-09 0.48 37 8.5e-06 2.8e-02 5.5e-04 1.00e+00 1.664086041e+02 1.664288769e+02 4.8e-09 0.49 38 7.6e-06 2.6e-02 4.9e-04 1.00e+00 1.664099557e+02 1.664281999e+02 4.3e-09 0.51 39 6.9e-06 2.4e-02 4.4e-04 1.00e+00 1.664111708e+02 1.664275896e+02 3.9e-09 0.52 40 6.2e-06 2.3e-02 4.0e-04 1.00e+00 1.664122633e+02 1.664270395e+02 3.5e-09 0.53 41 5.6e-06 2.1e-02 3.6e-04 1.00e+00 1.664132456e+02 1.664265435e+02 3.1e-09 0.54 42 5.0e-06 2.0e-02 3.2e-04 1.00e+00 1.664141289e+02 1.664260966e+02 2.8e-09 0.56 43 4.5e-06 1.9e-02 2.9e-04 1.00e+00 1.664149231e+02 1.664256937e+02 2.5e-09 0.57 44 4.1e-06 1.8e-02 2.6e-04 1.00e+00 1.664156374e+02 1.664253307e+02 2.3e-09 0.58 45 3.7e-06 1.7e-02 2.4e-04 1.00e+00 1.664162797e+02 1.664250035e+02 2.1e-09 0.59 46 3.3e-06 1.6e-02 2.1e-04 1.00e+00 1.664168573e+02 1.664247086e+02 1.9e-09 0.60 47 3.0e-06 1.5e-02 1.9e-04 1.00e+00 1.664173768e+02 1.664244429e+02 1.7e-09 0.61 48 2.7e-06 1.4e-02 1.7e-04 1.00e+00 1.664178440e+02 1.664242034e+02 1.5e-09 0.63 49 2.4e-06 1.4e-02 1.5e-04 1.00e+00 1.664182643e+02 1.664239877e+02 1.4e-09 0.64 50 2.2e-06 1.3e-02 1.4e-04 1.00e+00 1.664186423e+02 1.664237934e+02 1.2e-09 0.65 51 1.9e-06 1.3e-02 1.2e-04 1.00e+00 1.664189825e+02 1.664236185e+02 1.1e-09 0.67 52 1.7e-06 1.2e-02 1.1e-04 1.00e+00 1.664192885e+02 1.664234609e+02 9.8e-10 0.68 53 1.6e-06 1.2e-02 1.0e-04 1.00e+00 1.664195638e+02 1.664233190e+02 8.9e-10 0.69 54 1.4e-06 1.1e-02 9.1e-05 1.00e+00 1.664198115e+02 1.664231912e+02 8.0e-10 0.70 55 1.3e-06 1.1e-02 8.2e-05 1.00e+00 1.664200344e+02 1.664230761e+02 7.2e-10 0.71 56 1.1e-06 1.1e-02 7.4e-05 1.00e+00 1.664202349e+02 1.664229724e+02 6.5e-10 0.73 57 1.0e-06 1.0e-02 6.6e-05 1.00e+00 1.664204153e+02 1.664228791e+02 5.8e-10 0.74 58 9.3e-07 1.0e-02 6.0e-05 1.00e+00 1.664205776e+02 1.664227951e+02 5.2e-10 0.75 59 8.4e-07 9.9e-03 5.4e-05 1.00e+00 1.664207236e+02 1.664227194e+02 4.7e-10 0.77 60 7.5e-07 9.7e-03 4.8e-05 1.00e+00 1.664208550e+02 1.664226512e+02 4.2e-10 0.78 61 6.8e-07 9.5e-03 4.4e-05 1.00e+00 1.664209732e+02 1.664225898e+02 3.8e-10 0.79 62 6.1e-07 9.3e-03 3.9e-05 1.00e+00 1.664210796e+02 1.664225345e+02 3.4e-10 0.80 63 5.5e-07 9.2e-03 3.5e-05 1.00e+00 1.664211752e+02 1.664224847e+02 3.1e-10 0.82 64 4.9e-07 9.0e-03 3.2e-05 1.00e+00 1.664212613e+02 1.664224398e+02 2.8e-10 0.83 65 4.4e-07 8.9e-03 2.9e-05 1.00e+00 1.664213387e+02 1.664223994e+02 2.5e-10 0.83 66 4.0e-07 8.8e-03 2.6e-05 1.00e+00 1.664214083e+02 1.664223629e+02 2.3e-10 0.85 67 3.6e-07 8.7e-03 2.3e-05 1.00e+00 1.664214710e+02 1.664223301e+02 2.0e-10 0.86 68 3.2e-07 8.6e-03 2.1e-05 1.00e+00 1.664215273e+02 1.664223006e+02 1.8e-10 0.87 69 2.9e-07 8.5e-03 1.9e-05 1.00e+00 1.664215780e+02 1.664222740e+02 1.6e-10 0.88 70 2.6e-07 8.4e-03 1.7e-05 1.00e+00 1.664216237e+02 1.664222500e+02 1.5e-10 0.90 71 2.4e-07 8.4e-03 1.5e-05 1.00e+00 1.664216647e+02 1.664222284e+02 1.3e-10 0.91 72 2.1e-07 8.3e-03 1.4e-05 1.00e+00 1.664217017e+02 1.664222090e+02 1.2e-10 0.92 73 1.9e-07 8.2e-03 1.2e-05 1.00e+00 1.664217349e+02 1.664221915e+02 1.1e-10 0.94 74 1.7e-07 8.2e-03 1.1e-05 1.00e+00 1.664217648e+02 1.664221758e+02 9.7e-11 0.95 75 1.5e-07 8.1e-03 1.0e-05 1.00e+00 1.664217917e+02 1.664221616e+02 8.7e-11 0.97 76 1.4e-07 8.1e-03 9.0e-06 9.99e-01 1.664218160e+02 1.664221488e+02 7.9e-11 0.98 77 1.3e-07 8.0e-03 8.1e-06 1.00e+00 1.664218378e+02 1.664221373e+02 7.1e-11 0.99 78 1.1e-07 8.0e-03 7.3e-06 1.00e+00 1.664218574e+02 1.664221270e+02 6.4e-11 1.01 79 1.0e-07 8.0e-03 6.5e-06 1.00e+00 1.664218750e+02 1.664221177e+02 5.7e-11 1.02 80 9.1e-08 7.9e-03 5.9e-06 1.00e+00 1.664218909e+02 1.664221093e+02 5.2e-11 1.03 81 8.2e-08 7.9e-03 5.3e-06 1.00e+00 1.664219052e+02 1.664221018e+02 4.6e-11 1.04 82 7.4e-08 7.9e-03 4.8e-06 9.99e-01 1.664219181e+02 1.664220950e+02 4.2e-11 1.05 83 6.7e-08 7.9e-03 4.3e-06 1.00e+00 1.664219297e+02 1.664220889e+02 3.8e-11 1.06 84 6.0e-08 7.8e-03 3.9e-06 9.99e-01 1.664219401e+02 1.664220834e+02 3.4e-11 1.07 85 5.4e-08 7.8e-03 3.5e-06 1.00e+00 1.664219495e+02 1.664220784e+02 3.0e-11 1.09 86 4.9e-08 7.8e-03 3.1e-06 9.99e-01 1.664219579e+02 1.664220740e+02 2.7e-11 1.10 87 4.4e-08 7.8e-03 2.8e-06 9.99e-01 1.664219655e+02 1.664220700e+02 2.5e-11 1.11 88 3.9e-08 7.7e-03 2.5e-06 1.00e+00 1.664219723e+02 1.664220664e+02 2.2e-11 1.12 89 3.5e-08 7.7e-03 2.3e-06 1.00e+00 1.664219785e+02 1.664220631e+02 2.0e-11 1.13 90 3.2e-08 7.7e-03 2.1e-06 1.00e+00 1.664219840e+02 1.664220602e+02 1.8e-11 1.14 91 2.9e-08 7.7e-03 1.8e-06 1.00e+00 1.664219890e+02 1.664220576e+02 1.6e-11 1.15 92 2.6e-08 7.7e-03 1.7e-06 1.00e+00 1.664219935e+02 1.664220552e+02 1.5e-11 1.17 93 2.3e-08 7.7e-03 1.5e-06 9.99e-01 1.664219975e+02 1.664220531e+02 1.3e-11 1.17 94 2.1e-08 7.6e-03 1.3e-06 9.98e-01 1.664220012e+02 1.664220511e+02 1.2e-11 1.18 95 1.9e-08 7.6e-03 1.2e-06 1.00e+00 1.664220044e+02 1.664220494e+02 1.1e-11 1.19 96 1.7e-08 7.6e-03 1.1e-06 1.00e+00 1.664220074e+02 1.664220479e+02 9.6e-12 1.21 97 1.5e-08 7.6e-03 9.8e-07 1.00e+00 1.664220100e+02 1.664220465e+02 8.6e-12 1.22 98 1.4e-08 7.6e-03 8.8e-07 1.00e+00 1.664220124e+02 1.664220452e+02 7.8e-12 1.23 99 1.3e-08 6.8e-03 8.0e-07 1.01e+00 1.664220146e+02 1.664220441e+02 7.0e-12 1.24 100 1.1e-08 6.1e-03 7.2e-07 1.00e+00 1.664220165e+02 1.664220430e+02 6.3e-12 1.26 101 1.0e-08 5.5e-03 6.4e-07 9.99e-01 1.664220183e+02 1.664220421e+02 5.7e-12 1.27 102 9.1e-09 5.0e-03 5.8e-07 9.95e-01 1.664220198e+02 1.664220413e+02 5.1e-12 1.28 103 8.2e-09 4.5e-03 5.2e-07 1.00e+00 1.664220212e+02 1.664220406e+02 4.6e-12 1.29 104 7.4e-09 4.0e-03 4.7e-07 1.00e+00 1.664220225e+02 1.664220399e+02 4.1e-12 1.30 105 1.5e-08 3.7e-03 4.2e-07 9.00e-01 1.664220234e+02 1.664220402e+02 3.7e-12 1.31 106 1.7e-08 3.4e-03 3.8e-07 9.02e-01 1.664220242e+02 1.664220413e+02 3.3e-12 1.33 107 1.3e-08 3.0e-03 3.4e-07 1.00e+00 1.664220252e+02 1.664220407e+02 3.0e-12 1.34 108 1.2e-08 2.7e-03 3.1e-07 1.02e+00 1.664220261e+02 1.664220399e+02 2.7e-12 1.35 109 1.1e-08 2.5e-03 2.8e-07 1.00e+00 1.664220269e+02 1.664220393e+02 2.5e-12 1.37 110 1.0e-08 2.2e-03 2.5e-07 1.01e+00 1.664220276e+02 1.664220388e+02 2.2e-12 1.38 111 1.1e-08 2.0e-03 2.2e-07 8.59e-01 1.664220282e+02 1.664220388e+02 2.0e-12 1.39 112 9.5e-09 1.8e-03 2.0e-07 1.00e+00 1.664220288e+02 1.664220383e+02 1.8e-12 1.41 113 8.6e-09 1.6e-03 1.8e-07 1.00e+00 1.664220293e+02 1.664220379e+02 1.6e-12 1.42 114 7.8e-09 1.5e-03 1.6e-07 1.00e+00 1.664220298e+02 1.664220375e+02 1.5e-12 1.43 115 7.0e-09 1.3e-03 1.5e-07 9.96e-01 1.664220302e+02 1.664220371e+02 1.3e-12 1.45 116 6.3e-09 1.2e-03 1.3e-07 1.00e+00 1.664220305e+02 1.664220368e+02 1.2e-12 1.46 117 5.7e-09 1.1e-03 1.2e-07 9.97e-01 1.664220309e+02 1.664220365e+02 1.1e-12 1.47 118 5.2e-09 9.7e-04 1.1e-07 1.00e+00 1.664220312e+02 1.664220363e+02 9.7e-13 1.48 Optimizer terminated. Time: 1.49 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6642203117e+02 nrm: 2e+01 Viol. con: 1e-07 var: 0e+00 Dual. obj: 1.6642203625e+02 nrm: 1e+03 Viol. con: 0e+00 var: 9e-03 * End solution on dual form. * Transforming to primal solution. Solving took 1.53 seconds. Using solver 'mosek' Solving for 1768 variables. MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (313) 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 482 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: 0.02 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 873 Optimizer - Cones : 0 Optimizer - Scalar variables : 3462 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 : 1.49e+04 after factor : 1.57e+05 Factor - dense dim. : 0 flops : 3.26e+07 Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223788450e+05 2.000000000e+00 1.0e+00 0.05 1 1.7e+03 2.2e+03 8.9e+04 -9.71e-01 -1.216464201e+05 2.618823612e+00 7.3e-01 0.06 2 8.8e+02 1.1e+03 4.7e+04 -9.59e-01 -1.193651315e+05 4.610867248e+00 3.8e-01 0.08 3 2.9e+02 3.7e+02 1.5e+04 -9.22e-01 -1.102819975e+05 2.006632579e+01 1.3e-01 0.09 4 2.9e+02 3.7e+02 1.5e+04 -7.69e-01 -1.080008064e+05 2.022086612e+03 1.3e-01 0.10 5 1.2e+02 1.5e+02 6.3e+03 -7.59e-01 -8.679764001e+04 6.271578903e+03 5.2e-02 0.12 6 2.7e+01 3.5e+01 1.4e+03 -4.46e-01 -3.331156973e+04 1.276898522e+04 1.2e-02 0.13 7 1.7e+01 2.2e+01 9.1e+02 4.84e-01 -2.390955460e+04 7.088701501e+03 7.6e-03 0.14 8 9.9e+00 1.3e+01 5.3e+02 6.66e-01 -1.478698502e+04 4.288484843e+03 4.4e-03 0.16 9 3.8e+00 4.9e+00 2.0e+02 8.19e-01 -5.783602810e+03 1.894120710e+03 1.7e-03 0.17 10 1.9e+00 2.5e+00 1.0e+02 9.50e-01 -2.752723046e+03 1.147878748e+03 8.5e-04 0.18 11 8.6e-01 1.1e+00 4.7e+01 9.88e-01 -1.163553864e+03 6.311053338e+02 3.9e-04 0.20 12 8.3e-01 1.1e+00 4.5e+01 9.53e-01 -1.146181136e+03 6.056748478e+02 3.8e-04 0.21 13 5.2e-01 6.8e-01 2.8e+01 9.71e-01 -6.643878606e+02 4.338683157e+02 2.4e-04 0.22 14 3.0e-01 4.0e-01 1.6e+01 1.00e+00 -3.001695787e+02 3.312568167e+02 1.4e-04 0.24 15 1.0e-01 1.6e-01 5.8e+00 1.00e+00 -1.111857075e+01 2.124409044e+02 4.9e-05 0.25 16 8.3e-02 1.3e-01 4.6e+00 1.02e+00 2.954416115e+01 2.070652180e+02 3.9e-05 0.26 17 4.6e-02 9.2e-02 2.6e+00 1.02e+00 9.054315273e+01 1.887141196e+02 2.2e-05 0.28 18 1.2e-02 1.7e-01 6.8e-01 1.02e+00 1.474804520e+02 1.732840791e+02 5.8e-06 0.29 19 4.0e-03 1.9e-01 2.3e-01 1.01e+00 1.599979590e+02 1.685737685e+02 1.9e-06 0.30 20 1.6e-03 1.1e-01 9.4e-02 1.01e+00 1.638684180e+02 1.673751081e+02 8.0e-07 0.32 21 6.4e-04 9.4e-02 3.8e-02 1.01e+00 1.653872518e+02 1.668180858e+02 3.3e-07 0.33 22 2.4e-04 9.6e-02 1.4e-02 1.01e+00 1.660337135e+02 1.665706256e+02 1.3e-07 0.34 23 9.1e-05 9.3e-02 5.6e-03 1.01e+00 1.662643767e+02 1.664734884e+02 5.0e-08 0.36 24 8.2e-05 8.5e-02 5.1e-03 1.01e+00 1.662801856e+02 1.664683641e+02 4.5e-08 0.37 25 7.4e-05 7.7e-02 4.6e-03 1.01e+00 1.662931282e+02 1.664624192e+02 4.0e-08 0.38 26 6.7e-05 7.0e-02 4.1e-03 1.01e+00 1.663048697e+02 1.664571799e+02 3.6e-08 0.39 27 6.0e-05 6.4e-02 3.7e-03 1.01e+00 1.663153795e+02 1.664524151e+02 3.3e-08 0.41 28 5.4e-05 5.8e-02 3.3e-03 1.01e+00 1.663248144e+02 1.664481107e+02 2.9e-08 0.42 29 4.8e-05 5.3e-02 3.0e-03 1.01e+00 1.663332809e+02 1.664442181e+02 2.6e-08 0.43 30 4.4e-05 4.9e-02 2.7e-03 1.01e+00 1.663408801e+02 1.664406994e+02 2.4e-08 0.45 31 3.9e-05 4.5e-02 2.4e-03 1.01e+00 1.663477017e+02 1.664375192e+02 2.1e-08 0.46 32 3.5e-05 4.1e-02 2.2e-03 1.01e+00 1.663538259e+02 1.664346455e+02 1.9e-08 0.47 33 3.2e-05 3.8e-02 2.0e-03 1.01e+00 1.663593248e+02 1.664320492e+02 1.7e-08 0.49 34 2.9e-05 3.5e-02 1.8e-03 1.00e+00 1.663642629e+02 1.664297041e+02 1.6e-08 0.50 35 2.6e-05 3.2e-02 1.6e-03 1.00e+00 1.663686978e+02 1.664275861e+02 1.4e-08 0.51 36 2.3e-05 3.0e-02 1.4e-03 1.00e+00 1.663726813e+02 1.664256736e+02 1.3e-08 0.53 37 2.1e-05 2.8e-02 1.3e-03 1.00e+00 1.663762595e+02 1.664239469e+02 1.1e-08 0.54 38 1.9e-05 2.6e-02 1.2e-03 1.00e+00 1.663794741e+02 1.664223881e+02 1.0e-08 0.55 39 1.7e-05 2.4e-02 1.0e-03 1.00e+00 1.663823623e+02 1.664209811e+02 9.2e-09 0.56 40 1.5e-05 2.2e-02 9.4e-04 1.00e+00 1.663849573e+02 1.664197112e+02 8.3e-09 0.58 41 1.4e-05 2.1e-02 8.5e-04 1.00e+00 1.663872893e+02 1.664185653e+02 7.5e-09 0.59 42 1.2e-05 2.0e-02 7.6e-04 1.00e+00 1.663893850e+02 1.664175315e+02 6.7e-09 0.60 43 1.1e-05 1.8e-02 6.9e-04 1.00e+00 1.663912685e+02 1.664165987e+02 6.0e-09 0.62 44 1.0e-05 1.7e-02 6.2e-04 1.00e+00 1.663929614e+02 1.664157574e+02 5.4e-09 0.63 45 9.0e-06 1.7e-02 5.6e-04 1.00e+00 1.663944832e+02 1.664149986e+02 4.9e-09 0.64 46 8.1e-06 1.6e-02 5.0e-04 1.00e+00 1.663958513e+02 1.664143143e+02 4.4e-09 0.66 47 7.3e-06 1.5e-02 4.5e-04 1.00e+00 1.663970812e+02 1.664136972e+02 4.0e-09 0.67 48 6.5e-06 1.4e-02 4.1e-04 1.00e+00 1.663981870e+02 1.664131409e+02 3.6e-09 0.68 49 5.9e-06 1.4e-02 3.7e-04 1.00e+00 1.663991812e+02 1.664126394e+02 3.2e-09 0.69 50 5.3e-06 1.3e-02 3.3e-04 1.00e+00 1.664000753e+02 1.664121873e+02 2.9e-09 0.71 51 4.8e-06 1.3e-02 3.0e-04 1.00e+00 1.664008792e+02 1.664117798e+02 2.6e-09 0.72 52 4.3e-06 1.2e-02 2.7e-04 1.00e+00 1.664016021e+02 1.664114125e+02 2.3e-09 0.73 53 3.9e-06 1.2e-02 2.4e-04 1.00e+00 1.664022522e+02 1.664110814e+02 2.1e-09 0.74 54 3.5e-06 1.1e-02 2.2e-04 1.00e+00 1.664028368e+02 1.664107829e+02 1.9e-09 0.75 55 3.1e-06 1.1e-02 1.9e-04 1.00e+00 1.664033625e+02 1.664105139e+02 1.7e-09 0.77 56 2.8e-06 1.1e-02 1.7e-04 1.00e+00 1.664038353e+02 1.664102715e+02 1.5e-09 0.78 57 2.5e-06 1.1e-02 1.6e-04 1.00e+00 1.664042606e+02 1.664100531e+02 1.4e-09 0.79 58 2.3e-06 1.0e-02 1.4e-04 1.00e+00 1.664046431e+02 1.664098564e+02 1.2e-09 0.80 59 2.1e-06 1.0e-02 1.3e-04 1.00e+00 1.664049873e+02 1.664096792e+02 1.1e-09 0.82 60 1.8e-06 9.8e-03 1.1e-04 1.00e+00 1.664052969e+02 1.664095196e+02 1.0e-09 0.83 61 1.7e-06 9.7e-03 1.0e-04 1.00e+00 1.664055754e+02 1.664093758e+02 9.1e-10 0.84 62 1.5e-06 9.5e-03 9.3e-05 1.00e+00 1.664058260e+02 1.664092464e+02 8.2e-10 0.85 63 1.3e-06 9.3e-03 8.4e-05 1.00e+00 1.664060515e+02 1.664091298e+02 7.4e-10 0.86 64 1.2e-06 9.2e-03 7.5e-05 1.00e+00 1.664062543e+02 1.664090248e+02 6.6e-10 0.88 65 1.1e-06 9.1e-03 6.8e-05 1.00e+00 1.664064368e+02 1.664089302e+02 6.0e-10 0.89 66 9.8e-07 9.0e-03 6.1e-05 1.00e+00 1.664066010e+02 1.664088451e+02 5.4e-10 0.90 67 8.8e-07 8.9e-03 5.5e-05 1.00e+00 1.664067487e+02 1.664087684e+02 4.8e-10 0.91 68 8.0e-07 8.8e-03 4.9e-05 1.00e+00 1.664068816e+02 1.664086993e+02 4.3e-10 0.93 69 7.2e-07 8.7e-03 4.4e-05 1.00e+00 1.664070012e+02 1.664086371e+02 3.9e-10 0.94 70 6.4e-07 8.6e-03 4.0e-05 1.00e+00 1.664071087e+02 1.664085811e+02 3.5e-10 0.95 71 5.8e-07 8.5e-03 3.6e-05 1.00e+00 1.664072054e+02 1.664085306e+02 3.2e-10 0.96 72 5.2e-07 8.5e-03 3.2e-05 1.00e+00 1.664072925e+02 1.664084851e+02 2.9e-10 0.97 73 4.7e-07 8.4e-03 2.9e-05 1.00e+00 1.664073707e+02 1.664084441e+02 2.6e-10 0.99 74 4.2e-07 8.3e-03 2.6e-05 1.00e+00 1.664074411e+02 1.664084072e+02 2.3e-10 1.00 75 3.8e-07 8.3e-03 2.4e-05 1.00e+00 1.664075045e+02 1.664083739e+02 2.1e-10 1.01 76 3.4e-07 8.2e-03 2.1e-05 1.00e+00 1.664075614e+02 1.664083439e+02 1.9e-10 1.02 77 3.1e-07 8.2e-03 1.9e-05 1.00e+00 1.664076127e+02 1.664083169e+02 1.7e-10 1.03 78 2.8e-07 8.1e-03 1.7e-05 1.00e+00 1.664076588e+02 1.664082926e+02 1.5e-10 1.04 79 2.5e-07 8.1e-03 1.5e-05 1.00e+00 1.664077003e+02 1.664082707e+02 1.4e-10 1.06 80 2.2e-07 8.1e-03 1.4e-05 1.00e+00 1.664077376e+02 1.664082510e+02 1.2e-10 1.07 81 2.0e-07 8.0e-03 1.3e-05 1.00e+00 1.664077712e+02 1.664082333e+02 1.1e-10 1.08 82 1.8e-07 8.0e-03 1.1e-05 1.00e+00 1.664078015e+02 1.664082173e+02 9.9e-11 1.09 83 1.6e-07 8.0e-03 1.0e-05 1.00e+00 1.664078287e+02 1.664082029e+02 9.0e-11 1.11 84 1.5e-07 8.0e-03 9.2e-06 1.00e+00 1.664078531e+02 1.664081899e+02 8.1e-11 1.12 85 1.3e-07 7.9e-03 8.2e-06 1.00e+00 1.664078752e+02 1.664081783e+02 7.3e-11 1.13 86 1.2e-07 7.9e-03 7.4e-06 1.00e+00 1.664078950e+02 1.664081678e+02 6.5e-11 1.14 87 1.1e-07 7.9e-03 6.7e-06 1.00e+00 1.664079128e+02 1.664081583e+02 5.9e-11 1.16 88 9.7e-08 7.9e-03 6.0e-06 1.00e+00 1.664079289e+02 1.664081498e+02 5.3e-11 1.17 89 8.7e-08 7.8e-03 5.4e-06 1.00e+00 1.664079433e+02 1.664081422e+02 4.8e-11 1.18 90 7.8e-08 7.8e-03 4.9e-06 1.00e+00 1.664079563e+02 1.664081353e+02 4.3e-11 1.19 91 7.1e-08 7.8e-03 4.4e-06 1.00e+00 1.664079680e+02 1.664081291e+02 3.9e-11 1.20 92 6.4e-08 7.8e-03 3.9e-06 1.00e+00 1.664079785e+02 1.664081235e+02 3.5e-11 1.21 93 5.7e-08 7.8e-03 3.5e-06 1.00e+00 1.664079880e+02 1.664081185e+02 3.1e-11 1.22 94 5.1e-08 7.8e-03 3.2e-06 1.00e+00 1.664079965e+02 1.664081140e+02 2.8e-11 1.24 95 4.6e-08 7.8e-03 2.9e-06 1.00e+00 1.664080042e+02 1.664081099e+02 2.5e-11 1.25 96 4.2e-08 7.7e-03 2.6e-06 1.00e+00 1.664080111e+02 1.664081062e+02 2.3e-11 1.26 97 3.7e-08 7.7e-03 2.3e-06 1.00e+00 1.664080173e+02 1.664081029e+02 2.0e-11 1.27 98 3.4e-08 7.7e-03 2.1e-06 9.99e-01 1.664080229e+02 1.664080999e+02 1.8e-11 1.28 99 3.0e-08 7.7e-03 1.9e-06 1.00e+00 1.664080279e+02 1.664080973e+02 1.7e-11 1.29 100 2.7e-08 7.7e-03 1.7e-06 9.99e-01 1.664080325e+02 1.664080949e+02 1.5e-11 1.31 101 2.5e-08 7.7e-03 1.5e-06 9.99e-01 1.664080365e+02 1.664080927e+02 1.3e-11 1.32 102 2.2e-08 7.6e-03 1.4e-06 9.98e-01 1.664080402e+02 1.664080908e+02 1.2e-11 1.34 103 2.0e-08 7.6e-03 1.2e-06 1.00e+00 1.664080435e+02 1.664080891e+02 1.1e-11 1.35 104 1.8e-08 7.6e-03 1.1e-06 9.98e-01 1.664080465e+02 1.664080875e+02 9.8e-12 1.36 105 1.6e-08 7.6e-03 1.0e-06 9.98e-01 1.664080491e+02 1.664080861e+02 8.8e-12 1.37 106 1.5e-08 6.8e-03 9.0e-07 1.00e+00 1.664080515e+02 1.664080848e+02 7.9e-12 1.39 107 1.3e-08 6.2e-03 8.1e-07 9.99e-01 1.664080537e+02 1.664080836e+02 7.1e-12 1.40 108 1.2e-08 5.5e-03 7.3e-07 9.97e-01 1.664080557e+02 1.664080826e+02 6.4e-12 1.41 109 1.1e-08 5.0e-03 6.6e-07 9.97e-01 1.664080574e+02 1.664080816e+02 5.8e-12 1.42 110 9.6e-09 4.5e-03 5.9e-07 1.00e+00 1.664080590e+02 1.664080808e+02 5.2e-12 1.44 111 8.6e-09 4.0e-03 5.3e-07 1.01e+00 1.664080605e+02 1.664080800e+02 4.7e-12 1.46 112 7.7e-09 3.6e-03 4.8e-07 1.01e+00 1.664080618e+02 1.664080793e+02 4.3e-12 1.47 113 7.0e-09 3.3e-03 4.3e-07 1.00e+00 1.664080629e+02 1.664080787e+02 3.8e-12 1.48 114 6.3e-09 2.9e-03 3.9e-07 1.01e+00 1.664080640e+02 1.664080781e+02 3.5e-12 1.49 115 5.7e-09 2.6e-03 3.5e-07 9.94e-01 1.664080649e+02 1.664080776e+02 3.1e-12 1.50 116 5.1e-09 2.4e-03 3.1e-07 9.84e-01 1.664080657e+02 1.664080772e+02 2.8e-12 1.52 117 2.1e-08 2.4e-03 3.1e-07 -3.26e-01 1.664080664e+02 1.664080752e+02 2.6e-12 1.53 118 2.1e-08 2.1e-03 2.8e-07 1.02e+00 1.664080676e+02 1.664080744e+02 2.2e-12 1.54 119 1.8e-08 2.0e-03 2.5e-07 9.97e-01 1.664080680e+02 1.664080743e+02 2.0e-12 1.58 120 1.7e-08 1.8e-03 2.3e-07 9.92e-01 1.664080686e+02 1.664080742e+02 1.8e-12 1.59 121 1.5e-08 1.7e-03 2.1e-07 1.03e+00 1.664080691e+02 1.664080741e+02 1.6e-12 1.60 122 1.3e-08 1.5e-03 1.9e-07 1.02e+00 1.664080696e+02 1.664080740e+02 1.5e-12 1.62 123 1.2e-08 1.3e-03 1.7e-07 1.04e+00 1.664080700e+02 1.664080739e+02 1.3e-12 1.63 124 1.1e-08 1.2e-03 1.5e-07 1.01e+00 1.664080703e+02 1.664080738e+02 1.2e-12 1.64 125 9.8e-09 1.1e-03 1.4e-07 9.98e-01 1.664080706e+02 1.664080737e+02 1.1e-12 1.65 126 8.9e-09 9.8e-04 1.2e-07 9.96e-01 1.664080709e+02 1.664080737e+02 9.8e-13 1.67 Optimizer terminated. Time: 1.67 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.6640807086e+02 nrm: 2e+01 Viol. con: 1e-07 var: 0e+00 Dual. obj: 1.6640807369e+02 nrm: 1e+03 Viol. con: 0e+00 var: 4e-03 * End solution on dual form. * Transforming to primal solution. Solving took 1.71 seconds. Solving took 9 GP solves and 24.4 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: 1.4957403142127757e+110 vs 1.49570493199e+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 Solution check warning: Primal solution computed cost did not match solver-returned cost: 7.485942833952247e+74 vs 7.48576841516e+74 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 WEIGHT DIFFERENCES Total Fuel Weight Percent Diff: [-92.94682601] Total Aircraft Weight Percent Diff: [-21.48053826] Engine Weight Percent Diff: -56.27816263501683 Fuselage Weight Percent Diff: -0.8697283781658797 Payload Weight Percent Diff: [-0.0400356] VT Weight Percent Diff: -8.607712900393501 HT Weight Percent Diff: -93.23330431885311 Wing Weight Percent Diff: 8.267573259901017 WING DIFFERENCES Wing Span Percent Diff: -0.029994358510184876 Wing Area Percent Diff: 32.89970105408197 HORIZONTAL TAIL DIFFERENCES HT Area Percent Diff: 40.48862631668246 VERTICAL TAIL DIFFERENCES VT Span Percent Diff: -11.02232031308826 VT Area Percent Diff: -60.38681772051953 CRUISE SEGMENT 1 DRAG DIFFERENCES Overall Cd Percent Diff: [-18.54721004] L/D Percent Diff: [24.01023756] Nacelle Cd Percent Diff: [-94.27640786] HT Cd Percent Diff: [-80.7694112] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-58.00288783] dimensionless Wing Cd percent Diff: [-14.229156] Induced Drag Cd Percent Diff: [1.21939606] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-90.57036149] FUSELAGE DIFFERENCES Weight of HB material: -38.360425524416385 Weight of VB material: 87.8200230270085 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.71260522] 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}[:]/dum[:])^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}[:]/dum[:])^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 1768 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 476 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: 0.03 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 878 Optimizer - Cones : 0 Optimizer - Scalar variables : 3466 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.04 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.04 Factor - nonzeros before factor : 1.49e+04 after factor : 1.55e+05 Factor - dense dim. : 0 flops : 3.17e+07 Factor - GP saved nzs : 3.36e+04 GP saved flops : 9.32e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223083000e+05 2.000000000e+00 1.0e+00 0.07 1 1.6e+03 2.0e+03 8.4e+04 -9.71e-01 -1.214169755e+05 2.778937242e+00 6.8e-01 0.09 2 8.2e+02 1.1e+03 4.4e+04 -9.56e-01 -1.189685922e+05 5.116623673e+00 3.6e-01 0.10 3 2.9e+02 3.8e+02 1.6e+04 -9.15e-01 -1.102962345e+05 2.170095046e+01 1.3e-01 0.11 4 2.9e+02 3.8e+02 1.6e+04 -7.69e-01 -1.083159562e+05 1.743975991e+03 1.3e-01 0.13 5 1.1e+02 1.5e+02 6.0e+03 -7.60e-01 -8.473424866e+04 6.747984694e+03 5.0e-02 0.14 6 3.8e+01 4.9e+01 2.0e+03 -4.14e-01 -4.537005734e+04 1.080379792e+04 1.7e-02 0.15 7 2.0e+01 2.7e+01 1.1e+03 2.54e-01 -2.836625497e+04 7.045474557e+03 9.0e-03 0.18 8 9.4e+00 1.2e+01 5.0e+02 5.72e-01 -1.387003547e+04 4.245870985e+03 4.2e-03 0.19 9 4.7e+00 6.2e+00 2.6e+02 8.29e-01 -6.980052804e+03 2.517162242e+03 2.1e-03 0.21 10 1.4e+00 1.9e+00 7.8e+01 9.33e-01 -2.014621384e+03 9.508454525e+02 6.5e-04 0.22 11 6.4e-01 8.4e-01 3.5e+01 9.93e-01 -6.678945647e+02 6.594956157e+02 2.9e-04 0.24 12 4.8e-01 6.4e-01 2.7e+01 9.96e-01 -4.499444859e+02 5.609447906e+02 2.2e-04 0.25 13 3.5e-01 7.8e-01 1.9e+01 9.80e-01 -2.667764900e+02 4.766170471e+02 1.6e-04 0.27 14 1.7e-01 3.9e-01 9.5e+00 9.96e-01 3.398903189e-01 3.641145682e+02 8.0e-05 0.29 15 5.8e-02 1.6e-01 3.3e+00 9.94e-01 1.652792674e+02 2.911850936e+02 2.8e-05 0.30 16 3.3e-02 1.4e-01 1.9e+00 1.00e+00 2.032349806e+02 2.745517815e+02 1.6e-05 0.32 17 4.6e-03 2.1e-01 2.9e-01 1.00e+00 2.458601979e+02 2.569052088e+02 2.6e-06 0.33 18 1.3e-03 1.4e-01 8.6e-02 1.00e+00 2.513276389e+02 2.546006416e+02 7.8e-07 0.35 19 4.6e-04 1.1e-01 3.0e-02 1.00e+00 2.528755707e+02 2.540040947e+02 2.7e-07 0.36 20 1.8e-04 9.1e-02 1.2e-02 1.00e+00 2.533597014e+02 2.538150010e+02 1.1e-07 0.37 21 1.7e-04 8.2e-02 1.1e-02 1.00e+00 2.533933866e+02 2.538031620e+02 9.9e-08 0.39 22 1.5e-04 7.5e-02 9.7e-03 1.00e+00 2.534228246e+02 2.537915997e+02 8.9e-08 0.40 23 1.3e-04 6.8e-02 8.7e-03 1.00e+00 2.534493464e+02 2.537812275e+02 8.0e-08 0.44 24 1.2e-04 6.2e-02 7.8e-03 1.00e+00 2.534731930e+02 2.537718722e+02 7.2e-08 0.45 25 1.1e-04 5.6e-02 7.1e-03 1.00e+00 2.534946426e+02 2.537634424e+02 6.5e-08 0.46 26 9.8e-05 5.2e-02 6.4e-03 1.00e+00 2.535139347e+02 2.537558453e+02 5.8e-08 0.47 27 8.8e-05 4.7e-02 5.7e-03 1.00e+00 2.535312881e+02 2.537490000e+02 5.3e-08 0.49 28 7.9e-05 4.3e-02 5.1e-03 1.00e+00 2.535468982e+02 2.537428327e+02 4.7e-08 0.50 29 7.1e-05 4.0e-02 4.6e-03 1.00e+00 2.535609408e+02 2.537372768e+02 4.3e-08 0.52 30 6.4e-05 3.6e-02 4.2e-03 1.00e+00 2.535735736e+02 2.537322719e+02 3.8e-08 0.53 31 5.8e-05 3.4e-02 3.8e-03 1.00e+00 2.535849385e+02 2.537277637e+02 3.5e-08 0.54 32 5.2e-05 3.1e-02 3.4e-03 1.00e+00 2.535951630e+02 2.537237031e+02 3.1e-08 0.57 33 4.7e-05 2.9e-02 3.0e-03 1.00e+00 2.536043618e+02 2.537200458e+02 2.8e-08 0.58 34 4.2e-05 2.7e-02 2.7e-03 1.00e+00 2.536126378e+02 2.537167517e+02 2.5e-08 0.59 35 3.8e-05 2.5e-02 2.5e-03 1.00e+00 2.536200838e+02 2.537137851e+02 2.3e-08 0.60 36 3.4e-05 2.3e-02 2.2e-03 1.00e+00 2.536267832e+02 2.537111133e+02 2.0e-08 0.62 37 3.1e-05 2.1e-02 2.0e-03 1.00e+00 2.536328109e+02 2.537087072e+02 1.8e-08 0.63 38 2.8e-05 2.0e-02 1.8e-03 1.00e+00 2.536382344e+02 2.537065405e+02 1.7e-08 0.64 39 2.5e-05 1.9e-02 1.6e-03 1.00e+00 2.536431143e+02 2.537045893e+02 1.5e-08 0.66 40 2.2e-05 1.8e-02 1.5e-03 1.00e+00 2.536475051e+02 2.537028323e+02 1.3e-08 0.68 41 2.0e-05 1.7e-02 1.3e-03 1.00e+00 2.536514561e+02 2.537012503e+02 1.2e-08 0.69 42 1.8e-05 1.6e-02 1.2e-03 1.00e+00 2.536550112e+02 2.536998258e+02 1.1e-08 0.71 43 1.6e-05 1.5e-02 1.1e-03 1.00e+00 2.536582102e+02 2.536985432e+02 9.8e-09 0.72 44 1.5e-05 1.4e-02 9.5e-04 1.00e+00 2.536610889e+02 2.536973885e+02 8.8e-09 0.74 45 1.3e-05 1.4e-02 8.6e-04 1.00e+00 2.536636793e+02 2.536963489e+02 7.9e-09 0.75 46 1.2e-05 1.3e-02 7.7e-04 1.00e+00 2.536660103e+02 2.536954129e+02 7.1e-09 0.76 47 1.1e-05 1.2e-02 7.0e-04 1.00e+00 2.536681080e+02 2.536945703e+02 6.4e-09 0.78 48 9.6e-06 1.2e-02 6.3e-04 1.00e+00 2.536699957e+02 2.536938118e+02 5.8e-09 0.79 49 8.7e-06 1.2e-02 5.6e-04 1.00e+00 2.536716945e+02 2.536931290e+02 5.2e-09 0.80 50 7.8e-06 1.1e-02 5.1e-04 1.00e+00 2.536732232e+02 2.536925143e+02 4.7e-09 0.82 51 7.0e-06 1.1e-02 4.6e-04 1.00e+00 2.536745990e+02 2.536919610e+02 4.2e-09 0.83 52 6.3e-06 1.0e-02 4.1e-04 1.00e+00 2.536758371e+02 2.536914629e+02 3.8e-09 0.84 53 5.7e-06 1.0e-02 3.7e-04 1.00e+00 2.536769513e+02 2.536910146e+02 3.4e-09 0.85 54 5.1e-06 9.9e-03 3.3e-04 1.00e+00 2.536779540e+02 2.536906110e+02 3.1e-09 0.87 55 4.6e-06 9.7e-03 3.0e-04 1.00e+00 2.536788564e+02 2.536902477e+02 2.8e-09 0.88 56 4.1e-06 9.5e-03 2.7e-04 1.00e+00 2.536796685e+02 2.536899207e+02 2.5e-09 0.89 57 3.7e-06 9.3e-03 2.4e-04 1.00e+00 2.536803993e+02 2.536896263e+02 2.2e-09 0.91 58 3.4e-06 9.1e-03 2.2e-04 1.00e+00 2.536810570e+02 2.536893613e+02 2.0e-09 0.93 59 3.0e-06 8.9e-03 2.0e-04 1.00e+00 2.536816489e+02 2.536891228e+02 1.8e-09 0.94 60 1.2e-06 3.4e-03 7.6e-05 1.00e+00 2.536849211e+02 2.536878032e+02 7.0e-10 0.96 61 1.0e-06 3.1e-03 6.8e-05 1.00e+00 2.536851269e+02 2.536877209e+02 6.3e-10 0.97 62 3.7e-07 1.1e-03 2.4e-05 1.00e+00 2.536863131e+02 2.536872421e+02 2.2e-10 0.99 63 3.4e-07 1.0e-03 2.2e-05 1.00e+00 2.536863794e+02 2.536872155e+02 2.0e-10 1.01 64 3.0e-07 9.0e-04 2.0e-05 1.00e+00 2.536864389e+02 2.536871914e+02 1.8e-10 1.02 65 2.7e-07 8.1e-04 1.8e-05 1.00e+00 2.536864925e+02 2.536871697e+02 1.6e-10 1.04 66 2.5e-07 7.3e-04 1.6e-05 1.00e+00 2.536865407e+02 2.536871503e+02 1.5e-10 1.05 67 2.2e-07 6.6e-04 1.4e-05 1.00e+00 2.536865841e+02 2.536871327e+02 1.3e-10 1.07 68 2.0e-07 5.9e-04 1.3e-05 1.00e+00 2.536866232e+02 2.536871169e+02 1.2e-10 1.09 69 1.8e-07 5.3e-04 1.2e-05 1.00e+00 2.536866583e+02 2.536871027e+02 1.1e-10 1.10 70 1.6e-07 4.8e-04 1.1e-05 1.00e+00 2.536866900e+02 2.536870899e+02 9.7e-11 1.11 71 1.5e-07 4.3e-04 9.5e-06 1.00e+00 2.536867185e+02 2.536870784e+02 8.7e-11 1.13 72 1.3e-07 3.9e-04 8.5e-06 1.00e+00 2.536867441e+02 2.536870680e+02 7.8e-11 1.14 73 1.2e-07 3.5e-04 7.7e-06 1.00e+00 2.536867672e+02 2.536870587e+02 7.1e-11 1.15 74 1.1e-07 3.1e-04 6.9e-06 1.00e+00 2.536867879e+02 2.536870503e+02 6.3e-11 1.18 75 9.5e-08 2.8e-04 6.2e-06 1.00e+00 2.536868066e+02 2.536870427e+02 5.7e-11 1.19 76 8.6e-08 2.5e-04 5.6e-06 1.00e+00 2.536868234e+02 2.536870359e+02 5.1e-11 1.20 77 7.7e-08 2.3e-04 5.0e-06 1.00e+00 2.536868385e+02 2.536870298e+02 4.6e-11 1.22 78 6.9e-08 2.1e-04 4.5e-06 1.00e+00 2.536868521e+02 2.536870243e+02 4.2e-11 1.23 79 6.3e-08 1.9e-04 4.1e-06 1.00e+00 2.536868644e+02 2.536870193e+02 3.7e-11 1.24 80 5.6e-08 1.7e-04 3.7e-06 1.00e+00 2.536868754e+02 2.536870149e+02 3.4e-11 1.26 81 5.1e-08 1.5e-04 3.3e-06 1.00e+00 2.536868854e+02 2.536870109e+02 3.0e-11 1.28 82 4.6e-08 1.3e-04 3.0e-06 1.00e+00 2.536868943e+02 2.536870072e+02 2.7e-11 1.30 83 4.1e-08 1.2e-04 2.7e-06 1.00e+00 2.536869023e+02 2.536870040e+02 2.5e-11 1.31 84 3.7e-08 1.1e-04 2.4e-06 1.00e+00 2.536869096e+02 2.536870010e+02 2.2e-11 1.33 85 3.3e-08 9.8e-05 2.2e-06 1.00e+00 2.536869161e+02 2.536869984e+02 2.0e-11 1.34 86 3.0e-08 8.8e-05 1.9e-06 1.00e+00 2.536869219e+02 2.536869960e+02 1.8e-11 1.35 87 2.7e-08 8.0e-05 1.8e-06 1.00e+00 2.536869272e+02 2.536869939e+02 1.6e-11 1.37 88 2.4e-08 7.2e-05 1.6e-06 1.00e+00 2.536869319e+02 2.536869920e+02 1.5e-11 1.39 89 2.2e-08 6.5e-05 1.4e-06 1.00e+00 2.536869362e+02 2.536869902e+02 1.3e-11 1.40 90 2.0e-08 5.8e-05 1.3e-06 1.00e+00 2.536869401e+02 2.536869887e+02 1.2e-11 1.42 91 1.8e-08 5.2e-05 1.1e-06 1.00e+00 2.536869435e+02 2.536869873e+02 1.1e-11 1.44 92 1.6e-08 4.7e-05 1.0e-06 1.00e+00 2.536869466e+02 2.536869860e+02 9.5e-12 1.45 93 1.4e-08 4.2e-05 9.3e-07 1.00e+00 2.536869494e+02 2.536869849e+02 8.6e-12 1.47 94 1.3e-08 3.8e-05 8.4e-07 1.00e+00 2.536869520e+02 2.536869839e+02 7.7e-12 1.48 95 1.2e-08 3.4e-05 7.5e-07 1.00e+00 2.536869542e+02 2.536869829e+02 6.9e-12 1.50 96 1.0e-08 3.1e-05 6.8e-07 1.00e+00 2.536869563e+02 2.536869821e+02 6.2e-12 1.52 97 9.4e-09 2.8e-05 6.1e-07 1.00e+00 2.536869581e+02 2.536869814e+02 5.6e-12 1.53 Optimizer terminated. Time: 1.54 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 2.5368695810e+02 nrm: 4e+01 Viol. con: 2e-07 var: 0e+00 Dual. obj: 2.5368698136e+02 nrm: 8e+02 Viol. con: 0e+00 var: 2e-04 * End solution on dual form. * Transforming to primal solution. Solving took 1.58 seconds. Using solver 'mosek' Solving for 1768 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Freed constraints in eliminator : 476 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: 0.02 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 : 1769 Cones : 0 Scalar variables : 6131 Matrix variables : 0 Integer variables : 0 Optimizer - threads : 8 Optimizer - solved problem : the primal Optimizer - Constraints : 879 Optimizer - Cones : 0 Optimizer - Scalar variables : 3468 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 : 1.49e+04 after factor : 1.56e+05 Factor - dense dim. : 0 flops : 3.19e+07 Factor - GP saved nzs : 3.36e+04 GP saved flops : 9.32e+05 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.219705586e+05 2.000000000e+00 1.0e+00 0.05 1 1.6e+03 2.1e+03 8.4e+04 -9.71e-01 -1.211031020e+05 2.765533663e+00 6.9e-01 0.07 2 7.8e+02 1.0e+03 4.2e+04 -9.57e-01 -1.183621946e+05 5.379607955e+00 3.4e-01 0.08 3 2.9e+02 3.8e+02 1.6e+04 -9.11e-01 -1.100271642e+05 2.234927157e+01 1.3e-01 0.10 4 2.9e+02 3.8e+02 1.6e+04 -7.69e-01 -1.081090538e+05 1.691198782e+03 1.3e-01 0.13 5 1.2e+02 1.6e+02 6.6e+03 -7.61e-01 -8.730500726e+04 6.170178286e+03 5.4e-02 0.14 6 3.9e+01 5.1e+01 2.1e+03 -4.57e-01 -4.641557494e+04 1.102767695e+04 1.7e-02 0.15 7 2.3e+01 3.0e+01 1.2e+03 2.33e-01 -3.095362448e+04 7.311515434e+03 1.0e-02 0.17 8 9.3e+00 1.2e+01 5.0e+02 5.26e-01 -1.383958025e+04 4.015287293e+03 4.1e-03 0.18 9 6.1e+00 7.9e+00 3.2e+02 8.28e-01 -9.007628044e+03 2.852555853e+03 2.7e-03 0.19 10 2.1e+00 2.7e+00 1.1e+02 9.03e-01 -3.047258165e+03 1.195224977e+03 9.4e-04 0.21 11 1.6e+00 2.0e+00 8.5e+01 9.77e-01 -2.209373100e+03 9.993568394e+02 7.0e-04 0.22 12 1.0e+00 1.4e+00 5.6e+01 9.78e-01 -1.412745572e+03 7.362078430e+02 4.7e-04 0.24 13 4.1e-01 7.0e-01 2.2e+01 9.86e-01 -4.532334049e+02 3.966890953e+02 1.9e-04 0.27 14 2.4e-01 4.3e-01 1.3e+01 1.00e+00 -1.803313668e+02 3.208030866e+02 1.1e-04 0.28 15 7.5e-02 4.3e-01 4.2e+00 1.00e+00 5.907667930e+01 2.194258788e+02 3.6e-05 0.29 16 2.7e-02 1.8e-01 1.5e+00 1.01e+00 1.312032677e+02 1.889662771e+02 1.3e-05 0.31 17 8.9e-03 1.1e-01 5.2e-01 1.01e+00 1.583140177e+02 1.780792062e+02 4.6e-06 0.32 18 3.5e-03 9.8e-02 2.1e-01 1.01e+00 1.668085083e+02 1.746024948e+02 1.8e-06 0.34 19 9.2e-04 1.2e-01 5.6e-02 1.01e+00 1.708677782e+02 1.729897946e+02 5.1e-07 0.36 20 3.1e-04 1.0e-01 1.9e-02 1.00e+00 1.718819279e+02 1.726108386e+02 1.8e-07 0.37 21 1.1e-04 1.0e-01 7.1e-03 9.98e-01 1.722145287e+02 1.724820216e+02 6.5e-08 0.40 22 3.7e-05 1.0e-01 2.4e-03 9.99e-01 1.723408997e+02 1.724300134e+02 2.2e-08 0.41 23 3.4e-05 9.2e-02 2.1e-03 1.00e+00 1.723477057e+02 1.724279165e+02 1.9e-08 0.42 24 3.0e-05 8.4e-02 1.9e-03 1.00e+00 1.723534337e+02 1.724256231e+02 1.8e-08 0.44 25 2.7e-05 7.6e-02 1.7e-03 1.00e+00 1.723585613e+02 1.724235306e+02 1.6e-08 0.45 26 2.5e-05 7.0e-02 1.6e-03 1.00e+00 1.723631653e+02 1.724216358e+02 1.4e-08 0.47 27 2.2e-05 6.3e-02 1.4e-03 1.00e+00 1.723673034e+02 1.724199249e+02 1.3e-08 0.49 28 2.0e-05 5.8e-02 1.3e-03 1.00e+00 1.723710236e+02 1.724183812e+02 1.2e-08 0.51 29 1.8e-05 5.3e-02 1.1e-03 1.00e+00 1.723743688e+02 1.724169890e+02 1.0e-08 0.53 30 1.6e-05 4.8e-02 1.0e-03 1.00e+00 1.723773770e+02 1.724157339e+02 9.3e-09 0.55 31 1.5e-05 4.4e-02 9.2e-04 1.00e+00 1.723800823e+02 1.724146024e+02 8.4e-09 0.56 32 1.3e-05 4.1e-02 8.2e-04 1.00e+00 1.723825154e+02 1.724135826e+02 7.6e-09 0.58 33 1.2e-05 3.7e-02 7.4e-04 1.00e+00 1.723847038e+02 1.724126634e+02 6.8e-09 0.59 34 1.1e-05 3.4e-02 6.7e-04 1.00e+00 1.723866721e+02 1.724118351e+02 6.1e-09 0.61 35 9.5e-06 3.2e-02 6.0e-04 1.00e+00 1.723884426e+02 1.724110887e+02 5.5e-09 0.62 36 8.6e-06 2.9e-02 5.4e-04 1.00e+00 1.723900351e+02 1.724104163e+02 5.0e-09 0.64 37 7.7e-06 2.7e-02 4.9e-04 1.00e+00 1.723914678e+02 1.724098104e+02 4.5e-09 0.65 38 6.9e-06 2.5e-02 4.4e-04 1.00e+00 1.723927565e+02 1.724092646e+02 4.0e-09 0.66 39 6.3e-06 2.4e-02 3.9e-04 1.00e+00 1.723939159e+02 1.724087729e+02 3.6e-09 0.68 40 5.6e-06 2.2e-02 3.5e-04 1.00e+00 1.723949589e+02 1.724083301e+02 3.3e-09 0.69 41 5.1e-06 2.1e-02 3.2e-04 1.00e+00 1.723958973e+02 1.724079312e+02 2.9e-09 0.70 42 4.6e-06 1.9e-02 2.9e-04 1.00e+00 1.723967416e+02 1.724075719e+02 2.6e-09 0.72 43 4.1e-06 1.8e-02 2.6e-04 1.00e+00 1.723975012e+02 1.724072484e+02 2.4e-09 0.73 44 3.7e-06 1.7e-02 2.3e-04 1.00e+00 1.723981846e+02 1.724069570e+02 2.1e-09 0.74 45 3.3e-06 1.6e-02 2.1e-04 1.00e+00 1.723987995e+02 1.724066946e+02 1.9e-09 0.76 46 3.0e-06 1.5e-02 1.9e-04 1.00e+00 1.723993528e+02 1.724064584e+02 1.7e-09 0.77 47 2.7e-06 1.5e-02 1.7e-04 1.00e+00 1.723998506e+02 1.724062456e+02 1.6e-09 0.78 48 2.4e-06 1.4e-02 1.5e-04 1.00e+00 1.724002985e+02 1.724060540e+02 1.4e-09 0.79 49 2.2e-06 1.3e-02 1.4e-04 1.00e+00 1.724007016e+02 1.724058815e+02 1.3e-09 0.80 50 2.0e-06 1.3e-02 1.2e-04 1.00e+00 1.724010643e+02 1.724057262e+02 1.1e-09 0.82 51 1.8e-06 1.2e-02 1.1e-04 1.00e+00 1.724013906e+02 1.724055863e+02 1.0e-09 0.83 52 1.6e-06 1.2e-02 1.0e-04 1.00e+00 1.724016843e+02 1.724054604e+02 9.2e-10 0.84 53 1.4e-06 1.1e-02 9.0e-05 1.00e+00 1.724019485e+02 1.724053470e+02 8.3e-10 0.86 54 1.3e-06 1.1e-02 8.1e-05 1.00e+00 1.724021863e+02 1.724052450e+02 7.4e-10 0.87 55 1.2e-06 1.1e-02 7.3e-05 1.00e+00 1.724024003e+02 1.724051531e+02 6.7e-10 0.88 56 1.0e-06 1.0e-02 6.6e-05 1.00e+00 1.724025928e+02 1.724050703e+02 6.0e-10 0.90 57 9.4e-07 1.0e-02 5.9e-05 1.00e+00 1.724027661e+02 1.724049959e+02 5.4e-10 0.91 58 8.4e-07 9.8e-03 5.3e-05 1.00e+00 1.724029220e+02 1.724049288e+02 4.9e-10 0.93 59 7.6e-07 9.6e-03 4.8e-05 1.00e+00 1.724030623e+02 1.724048684e+02 4.4e-10 0.94 60 6.8e-07 9.4e-03 4.3e-05 1.00e+00 1.724031886e+02 1.724048141e+02 4.0e-10 0.96 61 6.2e-07 9.2e-03 3.9e-05 1.00e+00 1.724033022e+02 1.724047651e+02 3.6e-10 0.98 62 5.5e-07 9.1e-03 3.5e-05 1.00e+00 1.724034044e+02 1.724047211e+02 3.2e-10 0.99 63 5.0e-07 8.9e-03 3.1e-05 1.00e+00 1.724034964e+02 1.724046814e+02 2.9e-10 1.01 64 4.5e-07 8.8e-03 2.8e-05 1.00e+00 1.724035792e+02 1.724046457e+02 2.6e-10 1.02 65 4.0e-07 8.7e-03 2.5e-05 1.00e+00 1.724036537e+02 1.724046135e+02 2.3e-10 1.04 66 3.6e-07 8.6e-03 2.3e-05 1.00e+00 1.724037207e+02 1.724045846e+02 2.1e-10 1.06 67 3.3e-07 8.5e-03 2.1e-05 1.00e+00 1.724037810e+02 1.724045585e+02 1.9e-10 1.07 68 2.9e-07 8.4e-03 1.9e-05 1.00e+00 1.724038353e+02 1.724045351e+02 1.7e-10 1.09 69 2.7e-07 8.3e-03 1.7e-05 1.00e+00 1.724038842e+02 1.724045140e+02 1.5e-10 1.10 70 2.4e-07 8.2e-03 1.5e-05 1.00e+00 1.724039281e+02 1.724044949e+02 1.4e-10 1.11 71 2.1e-07 8.1e-03 1.4e-05 1.00e+00 1.724039677e+02 1.724044778e+02 1.2e-10 1.13 72 1.9e-07 8.1e-03 1.2e-05 1.00e+00 1.724040033e+02 1.724044624e+02 1.1e-10 1.15 73 1.7e-07 8.0e-03 1.1e-05 1.00e+00 1.724040353e+02 1.724044485e+02 1.0e-10 1.16 74 1.6e-07 8.0e-03 9.9e-06 9.99e-01 1.724040642e+02 1.724044360e+02 9.0e-11 1.17 75 1.4e-07 7.9e-03 8.9e-06 1.00e+00 1.724040901e+02 1.724044248e+02 8.1e-11 1.19 76 1.3e-07 7.9e-03 8.0e-06 1.00e+00 1.724041135e+02 1.724044147e+02 7.3e-11 1.20 77 1.1e-07 7.8e-03 7.2e-06 1.00e+00 1E ====================================================================== ERROR [43.093s]: 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 43.093s FAILED (errors=1) Generating XML reports... .724041344e+02 1.724044056e+02 6.6e-11 1.22 78 1.0e-07 7.8e-03 6.5e-06 1.00e+00 1.724041534e+02 1.724043974e+02 5.9e-11 1.23 79 9.2e-08 7.0e-03 5.8e-06 1.01e+00 1.724041707e+02 1.724043898e+02 5.4e-11 1.24 80 8.3e-08 6.3e-03 5.2e-06 9.98e-01 1.724041860e+02 1.724043831e+02 4.8e-11 1.26 81 7.5e-08 5.7e-03 4.7e-06 9.95e-01 1.724041998e+02 1.724043771e+02 4.3e-11 1.27 82 6.8e-08 5.1e-03 4.3e-06 9.94e-01 1.724042122e+02 1.724043717e+02 3.9e-11 1.29 83 6.1e-08 4.6e-03 3.8e-06 9.99e-01 1.724042233e+02 1.724043669e+02 3.5e-11 1.30 84 5.5e-08 4.1e-03 3.4e-06 9.99e-01 1.724042333e+02 1.724043626e+02 3.2e-11 1.31 85 4.9e-08 3.7e-03 3.1e-06 9.94e-01 1.724042423e+02 1.724043586e+02 2.8e-11 1.33 86 4.5e-08 3.4e-03 2.8e-06 9.91e-01 1.724042504e+02 1.724043551e+02 2.6e-11 1.34 87 4.0e-08 3.0e-03 2.5e-06 9.74e-01 1.724042578e+02 1.724043519e+02 2.3e-11 1.35 88 3.7e-08 2.7e-03 2.3e-06 9.78e-01 1.724042644e+02 1.724043489e+02 2.1e-11 1.37 89 3.2e-08 2.4e-03 2.0e-06 1.01e+00 1.724042705e+02 1.724043464e+02 1.9e-11 1.39 90 3.0e-08 2.2e-03 1.8e-06 1.05e+00 1.724042770e+02 1.724043434e+02 1.7e-11 1.40 91 2.7e-08 2.0e-03 1.6e-06 9.74e-01 1.724042816e+02 1.724043414e+02 1.6e-11 1.42 92 2.6e-08 1.8e-03 1.5e-06 1.01e+00 1.724042860e+02 1.724043393e+02 1.4e-11 1.43 93 2.5e-08 1.6e-03 1.3e-06 9.93e-01 1.724042898e+02 1.724043376e+02 1.3e-11 1.45 94 5.6e-08 2.3e-04 1.9e-07 7.69e-01 1.724043192e+02 1.724043264e+02 2.2e-12 1.46 95 2.7e-08 2.3e-04 1.9e-07 -1.73e+00 1.724043193e+02 1.724043245e+02 2.0e-12 1.47 96 4.0e-08 2.3e-04 2.1e-07 1.00e+00 1.724043188e+02 1.724043245e+02 2.0e-12 1.49 97 4.0e-08 2.3e-04 2.1e-07 1.03e+01 1.724043188e+02 1.724043245e+02 2.0e-12 1.51 Optimizer terminated. Time: 1.51 solsta = 7, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : NEAR_OPTIMAL Primal. obj: 1.7240431885e+02 nrm: 4e+01 Viol. con: 8e-07 var: 0e+00 Dual. obj: 1.7240432452e+02 nrm: 8e+02 Viol. con: 0e+00 var: 1e-03 * End solution on dual form. * Transforming to primal solution. Solving took 1.56 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) (1.16.4) 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-M0Tc57 Running command git clone -q https://github.com/convexengineering/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-M0Tc57 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) (1.16.4) 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=ad75d603de4abae019ace731f56b2fb8fe6b35514b5df11977aba8c7607d3bb9 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-zC46h1/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-hHHtSU Running command git clone -q https://github.com/convexengineering/gassolar.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-hHHtSU 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) (1.16.4) 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=6dc626e38153a614e36838aa02f45f17386df2a25f91d3a35ad715a3721f15e6 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-ZZYvIM/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) (1.16.4) 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=14822 sha256=35b91e5ba31474633f50cf341628d46879ce3f57aa3fb07679a9840e3bd22c46 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-f3HMQD/wheels/55/91/84/60653f7cb392791f8ec648fb5ef240c78233b7566d69a6c92c Successfully built solar Installing collected packages: solar Successfully installed solar-0.0.0.0 Running tests... ---------------------------------------------------------------------- /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped. warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning) ../Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun) .... ---------------------------------------------------------------------- Ran 6 tests in 258.344s OK 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 Beginning signomial solve. Solving took 5 GP solves and 1.11 seconds. Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 0.8904 but bound is 0.9465 Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1632916.9435 but bound is 600000.0000 Warning: Variable Mission.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1259333.2960 but bound is 1000000.0000 N=3 Beginning signomial solve. Solving took 5 GP solves and 1.18 seconds. Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1135 but bound is 0.9465 Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1036204.4449 but bound is 600000.0000 Warning: Variable Mission1.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1006645.3573 but bound is 1000000.0000 N=5 Beginning signomial solve. Solving took 5 GP solves and 1.26 seconds. Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1487 but bound is 0.9465 Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 989673.4666 but bound is 600000.0000 Warning: Variable Mission2.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1019678.5408 but bound is 1000000.0000 N=7 Beginning signomial solve. Solving took 5 GP solves and 1.23 seconds. Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465 Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 976142.1475 but bound is 600000.0000 Warning: Variable Mission3.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1042059.4123 but bound is 1000000.0000 N=9 Beginning signomial solve. Solving took 5 GP solves and 1.65 seconds. Warning: Variable Mission4.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1567 but bound is 0.9465 Warning: Variable Mission4.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1007400.4785 but bound is 600000.0000 Warning: Variable Mission4.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1092545.5150 but bound is 1000000.0000 N=0 Beginning signomial solve. Solving took 4 GP solves and 0.832 seconds. Warning: Variable Mission5.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465 Warning: Variable Mission5.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2078 but bound is 600000.0000 N=1 Beginning signomial solve. Solving took 5 GP solves and 2.16 seconds. Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 0.8904 but bound is 0.9465 Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1632919.3776 but bound is 600000.0000 Warning: Variable Mission.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1259329.5070 but bound is 1000000.0000 N=3 Beginning signomial solve. Solving took 5 GP solves and 2.28 seconds. Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1135 but bound is 0.9465 Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1036209.6021 but bound is 600000.0000 Warning: Variable Mission1.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1006641.3990 but bound is 1000000.0000 N=5 Beginning signomial solve. Solving took 5 GP solves and 1.59 seconds. Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1487 but bound is 0.9465 Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 989673.1341 but bound is 600000.0000 Warning: Variable Mission2.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1019680.6011 but bound is 1000000.0000 N=7 Beginning signomial solve. Solving took 5 GP solves and 1.79 seconds. Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465 Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 976138.7332 but bound is 600000.0000 Warning: Variable Mission3.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1042059.9154 but bound is 1000000.0000 N=9 Beginning signomial solve. Solving took 5 GP solves and 1.95 seconds. Warning: Variable Mission4.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1567 but bound is 0.9465 Warning: Variable Mission4.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1007396.6632 but bound is 600000.0000 Warning: Variable Mission4.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1092544.5684 but bound is 1000000.0000 N=0 Beginning signomial solve. Solving took 4 GP solves and 1.14 seconds. Warning: Variable Mission5.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465 Warning: Variable Mission5.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119116.3963 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.9 seconds. Allowing negative dual variable(s) as small as -3.6246815899639153e-11. Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.3227 but bound is 0.9465 Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 671709.7480 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.17 seconds. Allowing negative dual variable(s) as small as -5.780984487322902e-10. Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2812 but bound is 0.9465 Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 729183.6293 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.46 seconds. Allowing negative dual variable(s) as small as -7.486587934225628e-12. Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2258 but bound is 0.9465 Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 802959.5997 but bound is 600000.0000 Using solver 'mosek' Solving for 7672 variables. Solving took 2.69 seconds. Allowing negative dual variable(s) as small as -1.2634497534364602e-11. Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2008 but bound is 0.9465 Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 839122.5079 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.92 seconds. Allowing negative dual variable(s) as small as -3.6246815899639153e-11. Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.3227 but bound is 0.9465 Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 671709.7480 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.29 seconds. Allowing negative dual variable(s) as small as -5.780984487322902e-10. Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2812 but bound is 0.9465 Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 729183.6293 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.28 seconds. Allowing negative dual variable(s) as small as -7.486587934225628e-12. Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2258 but bound is 0.9465 Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 802959.5997 but bound is 600000.0000 Using solver 'mosek' Solving for 7672 variables. Solving took 2.6 seconds. Allowing negative dual variable(s) as small as -1.2634497534364602e-11. Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2008 but bound is 0.9465 Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 839122.5079 but bound is 600000.0000 Beginning signomial solve. Solving took 4 GP solves and 0.727 seconds. Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465 Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2076 but bound is 600000.0000 Beginning signomial solve. Solving took 4 GP solves and 0.762 seconds. Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465 Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2076 but bound is 600000.0000 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) (1.16.4) 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-Av9cBK Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-Av9cBK 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) (1.16.4) 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=8fc6d865a8673589e45cc35ff5f70a1044385cce807f4c7c2392591e4c765914 Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-aMOljk/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) (1.16.4) 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=65670 sha256=71ca66e701b63b5b0ce24b94a49004e84e3ff18cdf910641d666cb8bd230053d Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-tQuo6s/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... ---------------------------------------------------------------------- ../Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped. warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning) .............. ---------------------------------------------------------------------- Ran 16 tests in 11.227s OK Generating XML reports... adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py' adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py' adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py' adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py' adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py' 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' Using solver 'mosek' Solving for 11 variables. Solving took 0.0109 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.0474 seconds. Using solver 'mosek' Solving for 9 variables. Solving took 0.0148 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.00984 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.0139 seconds. Beginning signomial solve. Solving took 16 GP solves and 0.605 seconds. Using solver 'mosek_cli' Solving for 9 variables. Solving took 0.0394 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.0342 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.0353 seconds. Beginning signomial solve. Solving took 16 GP solves and 1.23 seconds. Using solver 'mosek' Solving for 13 variables. Solving took 0.0146 seconds. Beginning signomial solve. Solving took 11 GP solves and 0.459 seconds. Warning: Variable BladeElementProp.BladeElementPerf.cl[:] could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742 Warning: Variable BladeElementProp.BladeElementPerf.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1619898.0180 but bound is 700000.0000 Using solver 'mosek_cli' Solving for 13 variables. Solving took 0.0381 seconds. Beginning signomial solve. Solving took 11 GP solves and 0.872 seconds. Warning: Variable BladeElementProp.BladeElementPerf.cl[:] could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742 Warning: Variable BladeElementProp.BladeElementPerf.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000 Warning: Variable TailAero.Re could cause inaccurate result because it is above upper bound. Solution is 2220953.3838 but bound is 1000000.0000 Warning: Variable TailAero1.Re could cause inaccurate result because it is above upper bound. Solution is 2499787.9776 but bound is 1000000.0000 Warning: Variable TailAero2.Re could cause inaccurate result because it is above upper bound. Solution is 2223878.3883 but bound is 1000000.0000 Warning: Variable TailAero3.Re could cause inaccurate result because it is above upper bound. Solution is 2223877.9590 but bound is 1000000.0000 Warning: Variable TailAero4.Re could cause inaccurate result because it is above upper bound. Solution is 1853897.1004 but bound is 1000000.0000 Warning: Variable TailAero5.Re could cause inaccurate result because it is above upper bound. Solution is 1853897.1004 but bound is 1000000.0000 Warning: Variable TailAero.Re could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000 Warning: Variable TailAero1.Re could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000 Warning: Variable TailAero2.Re could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable TailAero3.Re could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable TailAero4.Re could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable TailAero5.Re could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable WingAero.Re could cause inaccurate result because it is above upper bound. Solution is 1884891.6332 but bound is 700000.0000 Warning: Variable WingAero1.Re could cause inaccurate result because it is above upper bound. Solution is 1910419.6195 but bound is 700000.0000 Warning: Variable WingAero.Re could cause inaccurate result because it is above upper bound. Solution is 1910412.9866 but bound is 700000.0000 Warning: Variable WingAero1.Re could cause inaccurate result because it is above upper bound. Solution is 1910412.9866 but bound is 700000.0000 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 0.0157 seconds. Using solver 'mosek' Solving for 20 variables. Solving took 0.0138 seconds. Using solver 'mosek' Solving for 20 variables. Solving took 0.0104 seconds. Using solver 'mosek' Solving for 20 variables. Solving took 0.00932 seconds. Solving took 4 GP solves and 0.0542 seconds. Beginning signomial solve. Using solver 'mosek_cli' Solving for 20 variables. Solving took 0.057 seconds. Using solver 'mosek_cli' Solving for 20 variables. Solving took 0.0445 seconds. Using solver 'mosek_cli' Solving for 20 variables. Solving took 0.047 seconds. Using solver 'mosek_cli' Solving for 20 variables. Solving took 0.0437 seconds. Solving took 4 GP solves and 0.206 seconds. Cloning into 'eVTOL'... Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 5.737s 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/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] - 8 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