Started by upstream project "gplibrary_Push_Models" build number 188
originally caused by:
Started by GitHub push by bqpd
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on macys_VM 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 4e2bfe5f549cc5e92fd1613513f6de169e4e5eca (origin/master)
> git config core.sparsecheckout # timeout=10
> git checkout -f 4e2bfe5f549cc5e92fd1613513f6de169e4e5eca # timeout=3
Commit message: "add robust to EXTERNALTESTS"
> 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_VM] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[mosek] $ /bin/bash -xe /var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/jenkins3442355128258613857.sh
+ [[ macys_VM == *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_VM == *reynolds* ]]
+ [[ macys_VM == *macys* ]]
+ [[ mosek == mosek ]]
+ [[ macys_VM == 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/7/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/7/tools/platform/osx64x86/bin
+ export DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin
+ DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/7/tools/platform/osx64x86/bin
+ python /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/setup.py install
running install
running build
running build_py
running install_lib
creating /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying build/lib/mosek/__init__.py -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying build/lib/mosek/array.py -> /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/mosek/fusion/__init__.py -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
copying build/lib/mosek/fusion/SolverInfo.py -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
copying build/lib/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/array.py to array.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/SolverInfo.py to SolverInfo.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_data
copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosek64.7.1.dylib -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosekglb64.7.1.dylib -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libiomp5.dylib -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../bin/libmosekxx7_1.dylib -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying /Users/jenkins/mosek/7/tools/platform/osx64x86/python/2/../../../../../license.pdf -> /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
running install_egg_info
Writing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/Mosek-7.1.28-py2.7.egg-info
Please review the MOSEK license conditions in license.pdf
+ [[ mosek == mosek ]]
+ python -c '__import__("mosek").Env()'
+ msktestlic
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : min
Type : LO (linear optimization problem)
Constraints : 1
Cones : 0
Scalar variables : 5000
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator - tries : 0 time : 0.00
Eliminator - elim's : 0
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.00
Interior-point optimizer terminated. Time: 0.00.
Optimizer terminated. Time: 0.01
************************************
A license was checked out correctly.
************************************
+ export 'GPKITSOLVERS=mosek, mosek_cli'
+ GPKITSOLVERS='mosek, mosek_cli'
+ [[ mosek == cvxopt ]]
+ pip_install xmlrunner
+ python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade xmlrunner
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting xmlrunner
Installing collected packages: xmlrunner
Successfully installed xmlrunner-1.7.7
+ pip_install pint
+ python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade pint
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting pint
Using cached https://files.pythonhosted.org/packages/15/9d/bf177ebbc57d25e9e296addc14a1303d1e34d7964af5df428a8332349c42/Pint-0.9-py2.py3-none-any.whl
Collecting funcsigs; python_version == "2.7" (from pint)
Using cached https://files.pythonhosted.org/packages/69/cb/f5be453359271714c01b9bd06126eaf2e368f1fddfff30818754b5ac2328/funcsigs-1.0.2-py2.py3-none-any.whl
Installing collected packages: funcsigs, pint
Successfully installed funcsigs-1.0.2 pint-0.9
+ pip_install numpy
+ python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade numpy
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting numpy
Using cached https://files.pythonhosted.org/packages/51/67/8907005262f493e356195bcbd61b41988eecf63cb1d97ea2f6e55fe24205/numpy-1.16.5-cp27-cp27m-macosx_10_9_x86_64.whl
Installing collected packages: numpy
Successfully installed numpy-1.16.5
+ pip_install scipy
+ python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade scipy
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting scipy
Using cached https://files.pythonhosted.org/packages/a3/cf/36b77de4ccb1b841acd4c3c03abe38843c63c3a657cedee9e8fb19a02dc8/scipy-1.2.2-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl
Requirement already satisfied, skipping upgrade: numpy>=1.8.2 in ./venv2_gpkit/lib/python2.7/site-packages (from scipy) (1.16.5)
Installing collected packages: scipy
Successfully installed scipy-1.2.2
+ pip_install ad
+ python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade ad
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting ad
Installing collected packages: ad
Successfully installed ad-1.3.2
+ pip_install ctypesgen
+ python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade ctypesgen
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting ctypesgen
Installing collected packages: ctypesgen
Successfully installed ctypesgen-0.post125
+ pip_install pandas
+ python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --upgrade pandas
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting pandas
Using cached https://files.pythonhosted.org/packages/52/ff/912fe03a623a70bcf297d466013a0b4f4c68c3b60f86bf226682d061fc09/pandas-0.24.2-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl
Collecting pytz>=2011k (from pandas)
Using cached https://files.pythonhosted.org/packages/87/76/46d697698a143e05f77bec5a526bf4e56a0be61d63425b68f4ba553b51f2/pytz-2019.2-py2.py3-none-any.whl
Requirement already satisfied, skipping upgrade: numpy>=1.12.0 in ./venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5)
Collecting 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
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: pytz, six, python-dateutil, 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 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: six>=1.10 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.12.0)
Requirement already satisfied, skipping upgrade: pytz in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2019.2)
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
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 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
Requirement already satisfied, skipping upgrade: python-dateutil>=2.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2.8.0)
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: numpy>=1.7.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.16.5)
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: backports.functools-lru-cache, subprocess32, cycler, kiwisolver, 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__'
1.16.5
+ python -c 'import pint; print pint.__version__'
0.9
+ git clone --depth 1 https://github.com/convexengineering/gpkit.git
Cloning into 'gpkit'...
+ python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Obtaining file:///Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit
Requirement already satisfied: numpy>=1.13.3 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.9.1.0) (1.16.5)
Requirement already satisfied: pint>=0.8.1 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.9.1.0) (0.9)
Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.9.1.0) (1.2.2)
Requirement already satisfied: ad in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.9.1.0) (1.3.2)
Collecting cvxopt>=1.1.8 (from gpkit==0.9.1.0)
Downloading https://files.pythonhosted.org/packages/69/4f/167a7f5b11274eb8722e93b26c687c71499ae563083104c5b25dd2252990/cvxopt-1.2.3-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl (5.7MB)
Requirement already satisfied: six in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.9.1.0) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in ./venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit==0.9.1.0) (1.0.2)
Installing collected packages: cvxopt, gpkit
Running setup.py develop for gpkit
Successfully installed cvxopt-1.2.3 gpkit
+ python /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gplibrary_Push_Models/mosek
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Obtaining file:///Users/jenkins/workspace/gplibrary_Push_Models/mosek
Requirement already satisfied: numpy>=1.12 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.16.5)
Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.9)
Requirement already satisfied: funcsigs; python_version == "2.7" in ./venv2_gpkit/lib/python2.7/site-packages (from pint->gpkitmodels==0.0.0.0) (1.0.2)
Installing collected packages: gpkitmodels
Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels
+ export MSK_IPAR_NUM_THREADS=2
+ MSK_IPAR_NUM_THREADS=2
+ export MKL_NUM_THREADS=2
+ MKL_NUM_THREADS=2
+ export NUMEXPR_NUM_THREADS=2
+ NUMEXPR_NUM_THREADS=2
+ export OPENBLAS_NUM_THREADS=2
+ OPENBLAS_NUM_THREADS=2
+ export OMP_NUM_THREADS=2
+ OMP_NUM_THREADS=2
+ python -c 'from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True)'
No filename given.
Usage:
mskexpopt FILENAME [-primal] [-dual] [-p parameterfile]
Return code: 1052
Description: MSK_RES_ERR_FILE_OPEN [An error occurred while opening a file.]
...................................................................................................................................................................................................................................................
----------------------------------------------------------------------
Ran 243 tests in 22.205s
OK
Cloning into 'gplibrary'...
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Obtaining file:///Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary
Installing collected packages: gpkitmodels
Found existing installation: gpkitmodels 0.0.0.0
Uninstalling gpkitmodels-0.0.0.0:
Successfully uninstalled gpkitmodels-0.0.0.0
Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels
Cloning into 'robust'...
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Processing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/robust
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from robust==0.0.0) (0.9.1.0)
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from robust==0.0.0) (1.16.5)
Requirement already satisfied: matplotlib in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from robust==0.0.0) (2.2.4)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from robust==0.0.0) (1.2.2)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->robust==0.0.0) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->robust==0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->robust==0.0.0) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->robust==0.0.0) (1.12.0)
Requirement already satisfied: backports.functools-lru-cache in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (1.5)
Requirement already satisfied: pytz in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (2019.2)
Requirement already satisfied: subprocess32 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (3.5.4)
Requirement already satisfied: cycler>=0.10 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (0.10.0)
Requirement already satisfied: kiwisolver>=1.0.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (1.1.0)
Requirement already satisfied: python-dateutil>=2.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (2.8.0)
Requirement already satisfied: pyparsing!=2.0.4,!=2.1.2,!=2.1.6,>=2.0.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (2.4.2)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->robust==0.0.0) (1.0.2)
Requirement already satisfied: setuptools in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from kiwisolver>=1.0.1->matplotlib->robust==0.0.0) (41.2.0)
Building wheels for collected packages: robust
Building wheel for robust (setup.py): started
Building wheel for robust (setup.py): finished with status 'done'
Created wheel for robust: filename=robust-0.0.0-cp27-none-any.whl size=216974 sha256=2e135b1859a70e776f2c0ab26069af4bf6ce8f9b94bafda1792a69b283ffc516
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-i72Nnt/wheels/f5/9a/8f/c003ca5afde488728c792838e0c6645a1e18500b3cc3703684
Successfully built robust
Installing collected packages: robust
Successfully installed robust-0.0.0
Running tests...
----------------------------------------------------------------------
EEEEEEEEEE
======================================================================
ERROR [0.003s]: test_robust_testing_t_equivalent_posynomials_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn
mod = __import__(os.path.basename(path)[:-3])
File "t_equivalent_posynomials.py", line 1, in <module>
ImportError: No module named builtins
======================================================================
ERROR [0.001s]: test_robust_testing_t_equivalent_posynomials_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn
mod = __import__(os.path.basename(path)[:-3])
File "t_equivalent_posynomials.py", line 1, in <module>
ImportError: No module named builtins
======================================================================
ERROR [0.003s]: test_robust_testing_t_linearization_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn
mod = __import__(os.path.basename(path)[:-3])
File "t_linearization.py", line 2, in <module>
ImportError: No module named builtins
======================================================================
ERROR [0.001s]: test_robust_testing_t_linearization_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn
mod = __import__(os.path.basename(path)[:-3])
File "t_linearization.py", line 2, in <module>
ImportError: No module named builtins
======================================================================
ERROR [0.002s]: test_robust_testing_t_primitives_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn
mod = __import__(os.path.basename(path)[:-3])
File "t_primitives.py", line 1, in <module>
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/robust/robust_gp_tools.py", line 3, in <module>
from builtins import range
ImportError: No module named builtins
======================================================================
ERROR [0.001s]: test_robust_testing_t_primitives_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn
mod = __import__(os.path.basename(path)[:-3])
File "t_primitives.py", line 1, in <module>
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/robust/robust_gp_tools.py", line 3, in <module>
from builtins import range
ImportError: No module named builtins
======================================================================
ERROR [0.002s]: test_robust_testing_t_robust_gp_tools_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn
mod = __import__(os.path.basename(path)[:-3])
File "t_robust_gp_tools.py", line 1, in <module>
ImportError: No module named builtins
======================================================================
ERROR [0.001s]: test_robust_testing_t_robust_gp_tools_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn
mod = __import__(os.path.basename(path)[:-3])
File "t_robust_gp_tools.py", line 1, in <module>
ImportError: No module named builtins
======================================================================
ERROR [0.002s]: test_robust_testing_t_two_term_approximation_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn
mod = __import__(os.path.basename(path)[:-3])
File "t_two_term_approximation.py", line 2, in <module>
ImportError: No module named builtins
======================================================================
ERROR [0.001s]: test_robust_testing_t_two_term_approximation_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 37, in test_fn
mod = __import__(os.path.basename(path)[:-3])
File "t_two_term_approximation.py", line 2, in <module>
ImportError: No module named builtins
----------------------------------------------------------------------
Ran 10 tests in 0.017s
FAILED (errors=10)
Generating XML reports...
adding test for 'robust/testing/t_linearization.py'
adding test for 'robust/testing/t_equivalent_posynomials.py'
adding test for 'robust/testing/t_two_term_approximation.py'
adding test for 'robust/testing/t_robust_gp_tools.py'
adding test for 'robust/testing/t_primitives.py'
Cloning into 'shopping'...
Running tests...
----------------------------------------------------------------------
...
----------------------------------------------------------------------
Ran 3 tests in 0.434s
OK
Generating XML reports...
adding test for 'test.py'
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0279 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0213 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.243 seconds.
Cloning into 'gassolar'...
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2019.2)
Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5)
Requirement already satisfied: 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: 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-Q2_JY6
Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-Q2_JY6
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Building wheels for collected packages: gpfit
Building wheel for gpfit (setup.py): started
Building wheel for gpfit (setup.py): finished with status 'done'
Created wheel for gpfit: filename=gpfit-0.1-cp27-none-any.whl size=25151 sha256=9301f21217fd43c3b5eb595119249ba79ca49ae59389f1a2f3de14095887a49e
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-mhJ3ce/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
Installing collected packages: gpfit
Successfully installed gpfit-0.1
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Processing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gassolar
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.24.2)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.12.0)
Requirement already satisfied: 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: 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: 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=589f60be42922ce3f9c316a522e723223d225b0b54b24f4a0fdd2e7dec2bf6d1
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-dvCld8/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 17.332s
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 0.0605 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 0.32 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 0.0566 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 0.467 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 0.181 seconds.
Warning: Variable Mission.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.3537 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 1.13 seconds.
Warning: Variable Mission1.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103406.0510 but bound is 150000.0000
Using solver 'mosek_cli'
Solving for 1250 variables.
Solving took 0.531 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 1.51 seconds.
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: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2019.2)
Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5)
Requirement already satisfied: 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: 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-DcqA1H
Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-DcqA1H
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Building wheels for collected packages: gpfit
Building wheel for gpfit (setup.py): started
Building wheel for gpfit (setup.py): finished with status 'done'
Created wheel for gpfit: filename=gpfit-0.1-cp27-none-any.whl size=25151 sha256=2d33ea29f58787a10717b86158930aff8069207052372b1772dd09988a25775c
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-l4PSt6/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 30.890s
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 -1.8072305804639477e-13.
Solving took 4 GP solves and 1.23 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.815904e-13.
Solving took 4 GP solves and 2.53 seconds.
Allowing negative dual variable(s) as small as -8.33996760540856e-12.
Allowing negative dual variable(s) as small as -1.2583666747500999e-12.
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 -1.2590451684696413e-12.
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 -2.2597651381591366e-11.
Solving took 4 GP solves and 1.35 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 0.698 seconds.
Max payload weight [lbf] = 28.242
Max take off weight [lbf] = 166.638
Allowing negative dual variable(s) as small as -8.341243e-12.
Allowing negative dual variable(s) as small as -1.258645e-12.
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 -1.259536e-12.
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 -2.25977e-11.
Solving took 4 GP solves and 3.44 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.67 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) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.9)
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=45142 sha256=81876179fa75369c9ab853a8b1e51efd05d894c8d1ffddbe66b73a8cebca0178
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-YeaDtt/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 1.823s
OK
Generating XML reports...
adding test for 'turbofan/engine_test.py'
Beginning signomial solve.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.129 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0374 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0343 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0847 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.109 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0603 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0641 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0323 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0284 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.197 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.029 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.15 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0321 seconds.
Solving took 13 GP solves and 1.43 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/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-khdyxA
Running command git clone -q https://github.com/hoburg/turbofan.git /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-khdyxA
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.9)
Requirement already satisfied: future in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.17.1)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint->turbofan==0.0.0.0) (1.0.2)
Building wheels for collected packages: turbofan
Building wheel for turbofan (setup.py): started
Building wheel for turbofan (setup.py): finished with status 'done'
Created wheel for turbofan: filename=turbofan-0.0.0.0-cp27-none-any.whl size=45142 sha256=ea080b4157e4826c5724be637d111984b2fb0b3be894de09b358b059b597b2c5
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-pNcn1g/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: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan->SPaircraft==0.0.0) (1.16.5)
Requirement already satisfied: 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: 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: 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: 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=a06aa53408cc747f7814bcc51eac59d7ff0decb8205627dc41d205ed2b014e4e
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-YmM9XM/wheels/71/26/9f/5657db356ce6e0d3f9591b290e0bbf5df5bca9ab5b75809f6a
Successfully built SPaircraft
Installing collected packages: SPaircraft
Successfully installed SPaircraft-0.0.0
Running tests...
----------------------------------------------------------------------
adding test for 'SPaircraft.py'
Mission
=======
Cost
----
W_{f_{total}}[:].sum()
Constraints
-----------
W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin}
PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:])
x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:])
x_{CG}[3] <= \Delta x_n + x_n
\Delta x_m + x_{CG}[3] >= x_m
\tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m
C_{D_{fuse}}[:] = 0.018081
M_{fuseD} = 0.72
W_{start}[0] = W_{total}[:]
W_{start}[:] >= W_{end}[:] + W_{burn}[:]
W_{start}[1:] = W_{end}[:4]
W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1]
W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2]
W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1]
hft[2] >= CruiseAlt
hft[1:5] = hft[:4] + dhft[1:5]
hft[0] = dhft[0]
dhft[1:3] = dhft[:2]
RC[0] >= 2.5e+03
RC[:3] >= RC_{min}[:3]
\theta[2] >= 0.015
hft[2] >= MinCruiseAlt
n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:]
R_{segment}[3:4] = R_{segment}[4:5]
M[3:5] >= M_{min}
0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req}
Fsafetyfac*F[0] = T_e
W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:]
V_2[:] = M_2[:]*a[:]
\alpha_{max,w}[:3] = 0.18
\alpha_{max,w}[3:] = 0.1
0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime
0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime
ClimbTime <= MaxClimbTime
T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}}
F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
OPR[:] <= OPR_{max}
Aircraft
Fuselage
W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on}
W_{pass}[:] >= n_{pass}[:]*W_{avg. pass}
W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo}
W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}}
W_{payload}[:] <= W_{payload_{max}}
n_{pass}[:] <= n_{seat}
n_{rows} = n_{seat}/SPR
l_{shell} = n_{rows}*p_s
\theta_{db} = w_{db}/R_{fuse}
R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db}
A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db}
(PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse}
A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin}
w_{floor} = w_{fuse}
R_{fuse} + w_{db} >= w_{fuse}
h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse}
t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell}
S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2
S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2
l_{fuse} = l_{nose} + l_{shell} + l_{cone}
l_{cone} = R_{fuse}/\lambda_{cone}
x_{shell1} = l_{nose}
x_{shell2} >= l_{nose} + l_{shell}
t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin}
t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin}
\sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell})
\sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin}
l_{floor} >= l_{shell} + 2*R_{fuse}
P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat})
A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor}
V_{floor} = 2*w_{floor}*A_{floor}
W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor}
\tau_{cone} = \sigma_{skin}
W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame})
x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone}
-2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}}
(PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}}
x_{hbend_{Land}} >= x_{wing}
x_{hbend_{Land}} <= l_{fuse}
x_{hbend_{MLF}} >= x_{wing}
x_{hbend_{MLF}} <= l_{fuse}
A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}})
A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}})
A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
A_{2h_{MLF}} >= Mission.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2)
A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}}
A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}}
A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}}
A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}}
A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}}
A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}}
A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}}
A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}}
V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission.Aircraft.Fuselage.r_{w/c}
V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission.Aircraft.Fuselage.r_{w/c}
V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}}
W_{hbend} >= g*\rho_{bend}*V_{hbend}
x_{vbend} >= x_{wing}
x_{vbend} <= l_{fuse}
B_{0v} = B_{1v}*(x_{tail} - x_{vbend})
B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2)
B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}}
0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}}
V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission.Aircraft.Fuselage.r_{w/c}
V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}}
W_{vbend} >= \rho_{bend}*g*V_{vbend}
x_f = x_{wing} + 0.5*c_0*Mission.Aircraft.Fuselage.r_{w/c}
x_b = x_{wing} - 0.5*c_0*Mission.Aircraft.Fuselage.r_{w/c}
\sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h}
\sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v}
V_{cyl} = A_{skin}*l_{shell}
V_{nose} = S_{nose}*t_{skin}
V_{bulk} = S_{bulk}*t_{skin}
V_{db} = A_{db}*l_{shell}
V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse})
W_{apu} = W_{payload_{max}}*f_{apu}
W_{db} = \rho_{skin}*g*V_{db}
W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk})
W_{window} >= W'_{window}*l_{shell}
W_{padd} = W_{payload_{max}}*f_{padd}
W_{seat} >= W'_{seat}*n_{seat}
W_{seat} >= f_{seat}*W_{payload_{max}}
W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk})
W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db}
W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone})
Wing
WingNoStruct
A_{rect} = c_{tip}*b
0.5*(1 - \lambda)*c_{root}*b <= A_{tri}
p >= 1 + 2*\lambda
2*q >= 1 + p
y_{mac} = b/3*q/p
mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q
\lambda = c_{tip}/c_{root}
S = b*(c_{root} + c_{tip})/2
0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w)
e*(1 + f(\lambda_w)*AR) <= 1
\lambda >= 0.15
V_{fuel, max} <= 0.303*mac^2*b*\tau
W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g
b <= b_{max}
WingBox
AR = b^2/S
0.423*Mission.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5)
\tau <= \tau_{max_w}
W_{struct} >= W_{web} + W_{cap}
AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= 8*\rho_{cap}*g*Mission.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5)
Mission.Aircraft.Wing.WingBox.N_{lift} = 3
Mission.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8
\lambda = taper
W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt})
0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}}
Engine
Compressor
(no constraints)
Combustor
(no constraints)
Turbine
(no constraints)
Thrust
(no constraints)
FanMap
(no constraints)
LPCMap
(no constraints)
HPCMap
(no constraints)
Sizing
A_{2} >= A_{5} + A_{7}
FlightState
V[:] = V[:]
a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
V[:] = M[:]*a[:]
Altitude
h[:] = hft[:]
Atmosphere
(P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
\rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
\mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
EnginePerformance
CompressorPerformance
T_{t_0}[:] = T_{atm}[:]/c1[:]^-1
h_{t_0}[:] = C_{p_{air}*T_{t_0}[:]
P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:]
T_{t_{1.8}}[:] = T_{t_0}[:]
h_{t_{1.8}}[:] = h_{t_0}[:]
P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5
T_{T_{2}}[:] = T_{t_{1.8}}[:]
h_{T_{2}}[:] = h_{t_{1.8}}[:]
P_{T_{2}}[:] = P_{t_{1.8}}[:]
P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:]
T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016
h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:]
P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:]
T_{t_7}[:] = T_{t_{2.1}}[:]
h_{t_7}[:] = h_{t_{2.1}}[:]
P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:]
T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152
h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1}
P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:]
T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491
h_{t_3}[:] = C_{p_{2}*T_{t_3}[:]
CombustorPerformance
h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:]
h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:]
fp1[:] = f[:] + 1
M_{4a}[:] = 0.1025
fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5
T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]]
P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891
u_{4a}[:] = M_{4a}[:]*(1.31*Mission.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a}
u_c[:] = r_{uc}*u_{4a}[:]
P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891
TurbinePerformance
h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:]
P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:]
\pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565
h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:]
P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:]
T_{t_5}[:] = T_{t_{4.9}}[:]
h_{t_5}[:] = h_{t_{4.9}}[:]
ThrustPerformance
P_{8}[:] = P_{atm}[:]
h_{8}[:] = C_{p_{fex}*T_{8}[:]
u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:]
(P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:]
h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:]
P_{6}[:] = P_{atm}[:]
(P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:]
u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:]
h_6[:] = C_{p_{tex}*T_{6}[:]
h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:]
\alpha[:] = m_{fan}[:]/m_{core}[:]
\alpha_{+1}[:] = \alpha[:] + 1
\alpha[:] <= \alpha_{max}
F[:] <= F_{6}[:] + F_{8}[:]
F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:])
TSFC[:] = 1/I_{sp}[:]
F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:]
FanMapPerformance
m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}}
LPCMapPerformance
m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D}
HPCMapPerformance
m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D}
SizingPerformance
P_{7}[:] >= P_{atm}[:]
M_7[:] <= 1
a_{7}[:] = (1.4*Mission.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5
a_{7}[:]*M_7[:] = u_{7}[:]
\rho_7[:] = P_{7}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{7}[:])
P_{5}[:] >= P_{atm}[:]
M_5[:] <= 1
a_{5}[:] = (1.39*Mission.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5
a_{5}[:]*M_5[:] = u_{5}[:]
\rho_5[:] = P_{5}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{5}[:])
h_{2}[:] = C_{p_{1}*T_{2}[:]
\rho_{2}[:] = P_{2}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{2}[:])
u_{2}[:] = M_2[:]*(C_{p_{1}*Mission.Aircraft.Engine.EngineConstants.R*T_{2}[:]/781)^0.5
h_{2.5}[:] = C_{p_{2}*T_{2.5}[:]
\rho_{2.5}[:] = P_{2.5}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{2.5}[:])
u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/781)^0.5
m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine}
d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5
d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5
\eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]])
h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:]
P_{t_4}[:] = \pi_{b}*P_{t_3}[:]
M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]]
M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]])
P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:]
\pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013
\pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10
\pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10
\pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10
m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
\pi_{f}[:] >= 1
\pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10
\pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10
\pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10
\pi_{lc}[:] >= 1
m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
\pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10
\pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10
\pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10
m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref})
\pi_{hc}[:] >= 1
OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:]
P_{t_8}[:] = P_{t_7}[:]
T_{t_8}[:] = T_{t_7}[:]
P_{t_6}[:] = P_{t_5}[:]
T_{t_6}[:] = T_{t_5}[:]
F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:]
I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g)
N_{f}[:]*G_{f} = N_{1}[:]
N_{1}[:] <= 1.1
N_{2}[:] <= 1.1
fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD}
fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD}
P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5
(T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2
P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979
(T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2
M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:]
m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:]
m_{total}[:] = m_{fan}[:] + m_{core}[:]
P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512
T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1
m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2}
P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857
T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1
m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5}
1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD}
0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD}
1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD}
0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD}
m_{lc_D} >= 0.7*m_{coreD}/0.649
m_{lc_D} <= 1.3*m_{coreD}/0.649
m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23
m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23
\bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405
\bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405
F[:] = F_{spec}[:]
T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}}
OPR[:] <= OPR_{max}
VerticalTail
VerticalTailNoStruct
C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}}
L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}}
c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt}))
A_{vt} = b_{vt}^2/S_{vt}
b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt}
p_{vt} >= 1 + 2*\lambda_{vt}
2*q_{vt} >= 1 + p_{vt}
y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt}
\lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}}
\Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}}
\Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt}
\lambda_{vt} >= 0.25
V_{vt} >= V_{vt_{min}}
WingBox
AR_{vt} = (2*b_{vt})^2/(2*S_{vt})
0.423*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
\tau_{vt} <= 0.14
W_{struct} >= 0.5*(W_{web} + W_{cap})
Mission.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24
AR_{vt}*2*L_{vt_{max}}*Mission.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= 8*\rho_{cap}*g*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
Mission.Aircraft.VerticalTail.WingBox.N_{lift} = 1
Mission.Aircraft.VerticalTail.WingBox.N_{lift}*Mission.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8
\lambda_{vt} = taper
W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT})
HorizontalTail
HorizontalTailNoStruct
\Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht}
\Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}}
p_{ht} >= 1 + 2*\lambda_{ht}
2*q_{ht} >= 1 + p_{ht}
y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht}
0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht}
\lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}}
S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2
0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht})
e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1
AR_{ht} = b_{ht}^2/S_{ht}
\lambda_{ht} >= 0.2
\lambda_{ht} <= 1
WingBox
AR_{ht} = b_{ht}^2/S_{ht}
0.423*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
\tau_{ht} <= 0.14
W_{struct} >= W_{web} + W_{cap}
L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2
L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht})
2*AR_{ht}*L_{shear}*Mission.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
Mission.Aircraft.HorizontalTail.WingBox.N_{lift} = 1
Mission.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8
L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht}
L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}}
W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht})
LandingGear
l_n + z_{wing} + y_m*\tan(\gamma) >= l_m
T = 2*y_m
x_m >= x_n + B
x_n >= 5
\tan(\phi) = \tan(\phi_{min})
(z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1
\tan(\psi) <= \tan(\psi_{max})
x_{up} - x_m <= l_m/\tan(\theta_{max})
y_m >= l_m
S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG})
l_{oleo} = 2.5*S_{sa}
d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5
l_m >= l_{oleo} + d_{t_m}/2
F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in])
W_{wa,m} = 1.2*F_{w_m}^0.609
F_{w_n} = L_{w_n}*d_{t_n}/1e+03
W_{wa,n} = 1.2*F_{w_n}^0.609
L_{w_m} = L_m/(n_{mg}*n_{wps})
L_{w_n} = L_n/n_{wps}
d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315
w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48
d_{t_n} = 0.8*d_{t_m}
w_{t_n} = 0.8*w_{t_m}
W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g
N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m
W_{mw} = n_{wps}*W_{wa,m}
W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g
\sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}})
W_{nw} >= n_{wps}*W_{wa,n}
L_m <= 9.87*E*I_m/(K*l_m)^2
I_m = PI*r_m^3*t_m
L_n <= 9.87*E*I_n/(K*l_n)^2
I_n = PI*r_n^3*t_n
2*r_m/t_m <= 40
2*r_m/t_n <= 40
h_{hold} >= 2*w_{t_m} + 2*r_m
0.8 >= 2*w_{t_n} + 2*r_n
W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m}))
W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n})
W_{lg} >= C_{lg}*(W_{mg} + W_{ng})
W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m
x_m >= x_{CG_{lg}}
c_{root} = c_0
Mission.Aircraft.Wing.WingBox.r_{w/c} = Mission.Aircraft.Fuselage.r_{w/c}
x_w = x_{wing}
Mission.Aircraft.Fuselage.N_{lift} = Mission.Aircraft.Wing.WingBox.N_{lift}
f_{L_{total/wing}}*L_{max} >= Mission.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}}
W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc}
W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:]
W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:]
W_{total}[:] <= W_{total, max}
f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}}
W_{misc} >= W_{lg} + W_{hpesys}
W_{hpesys} = f_{hpesys}*W_{total, max}
x_n <= l_{nose}
x_m >= x_{wing}
\Delta x_{AC_{wing}} + x_{wing} >= x_m
x_{hpesys} = 1.1*l_{nose}
x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys}
d_{nacelle} >= d_{f} + 2*t_{nacelle}
E_{land} >= W_{total, max}/(2*g)*w_{ult}^2
x_{up} = x_{shell2}
L_n = W_{total, max}*\Delta x_m/B
L_m = W_{total, max}*\Delta x_n/B
L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max}
y_{eng} >= y_m
3*n_{vt}*Mission.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}}
V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse}
W_{tail} >= n_{vt}*W_{vt} + W_{ht}
2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db}
B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v})
m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht}
x_{CG_{ht}} <= l_{fuse}
V_{ht} = S_{ht}*l_{ht}/(S*mac)
L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}}
L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}}
x_{CG_{vt}} <= l_{fuse}
V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b)
n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max}
n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng}
D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}}
I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:]
I_{z}[:] <= I_{z, max}
S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2
l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}}
f_{S_{nacelle}} = S_{nacelle}*S^-1
A_{inlet} = 0.4*S_{nacelle}
A_{fancowl} = 0.2*S_{nacelle}
A_{exh} = 0.4*S_{nacelle}
A_{corecowl} = 3PI*d_{LPC}^2
W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl})
W_{eadd} = f_{eadd}*W_{engine}
W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon}
W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine})
y_{eng} = 0.5*w_{fuse}
(L_{max} - Mission.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission.Aircraft.Wing.WingBox.M_r*c_{root}
A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend})
A_{1h_{MLF}} >= (Mission.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h})
I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16)
I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81
I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81)
x_{shell2} + l_{cone} >= x_{eng}
x_{eng} >= x_{shell2} + 0.75*l_{cone}
S_{floor} = 0.312*P_{floor}
M_{floor} = 0.0352*P_{floor}*w_{floor}
\Delta R_{fuse} = R_{fuse}*0.43/1.75
b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2
b_{ht_{out}} = 0.5*b_{ht} - w_{fuse}
L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}}
M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}}
L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}}
c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach}
\pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht})
FlightSegment
FlightState
V[:] = V[:]
a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
V[:] = M[:]*a[:]
Altitude
h[:] = hft[:]
Atmosphere
(P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
\rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
\mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
FlightP
P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:]
RC[:] = P_{excess}[:]/W_{avg}[:]
\theta[:]*V[:] = RC[:]
dhft[:] = tmin[:]*RC[:]
R_{segment}[:] = thr[:]*V[:]
WingPerformance
0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:]
\Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:]
\Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2
(AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2
C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:]
\alpha_w[:] <= \alpha_{max,w}[:]
D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:]
C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:]
C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR)
Re_w[:] = \rho[:]*V[:]*mac/\mu[:]
C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114
FuselagePerformance
(no constraints)
VerticalTailPerformance
D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:]
Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:]
C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577
HorizontalTailPerformance
L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:]
C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:]
\alpha_{ht}[:] <= \alpha_{ht,max}
C_{L_{\alpha,ht_0}}[:] = 6.28
D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:]
C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht})
Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:]
C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852
W_{burn}[:] = W_{burn}[:]
F_{fuel}[:] = F_{fuel}[:]
\rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:])
P_{cabin}[:] = 7.5e+04
T_{cabin}[:] = 297
V[:] >= V_{stall}[:]
W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:]
tmin[:] = thr[:]
L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:]
L_{total}[:] = f_{L_{total/wing}}*L_w[:]
L_{total}[:] >= W_{avg}[:] + L_{ht}[:]
D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2
D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:])
C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S)
L/D[:] = W_{avg}[:]/D[:]
W_{Load}[:] <= W_{Load_{max}}[:]
W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S
p_{o}[:] >= L_w[:]*c_{root}/S
\eta_{o}[:] = w_{fuse}/(b/2)
x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:]
c_{m_{w}}[:] = 1.9
x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2)
x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse}
x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}}
x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}}
C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht}
AR_{ht} >= 4
C_{L_{ht}}[:] >= 0.01
SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac
SM[:] >= SM_{min}
SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}}
x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:]
R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:]
C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2
V_{nacelle}[:] = r_{v_{nacelle}}*V[:]
V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]]
r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0)
C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0
D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S
\Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}}
M_2[:3] = M[:3]
M_{2.5}[:3] = 0.6
hold_{2}[:3] = 1.07164
hold_{2.5}[:3] = 1.06372
P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:]
c1[:] = 1 + 0.201*M[:]^2.0
M_2[3:] = M[3:]
M_{2.5}[3:] = 0.6
hold_{2}[3:] = 1.07164
hold_{2.5}[3:] = 1.06372
Beginning signomial solve.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 937
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 937
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.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 768
Optimizer - Cones : 0
Optimizer - Scalar variables : 3438 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.285824792e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.5e+03 6.3e+04 -9.71e-01 -1.265132514e+05 3.611589420e+00 4.9e-01 0.05
2 4.1e+02 5.4e+02 2.3e+04 -9.38e-01 -1.199666169e+05 1.064041138e+01 1.8e-01 0.06
3 2.9e+02 3.7e+02 1.6e+04 -8.34e-01 -1.156309126e+05 6.812702963e+01 1.3e-01 0.07
4 2.8e+02 3.7e+02 1.6e+04 -7.60e-01 -1.131522901e+05 2.113211995e+03 1.3e-01 0.08
5 8.8e+01 1.2e+02 5.0e+03 -7.53e-01 -8.096538237e+04 8.430204037e+03 3.9e-02 0.09
6 3.7e+01 4.8e+01 2.1e+03 -2.92e-01 -4.806295568e+04 1.015705753e+04 1.6e-02 0.12
7 2.1e+01 2.8e+01 1.2e+03 2.53e-01 -3.183959973e+04 7.147574260e+03 9.5e-03 0.16
8 9.4e+00 1.2e+01 5.3e+02 5.37e-01 -1.516213576e+04 4.167067597e+03 4.2e-03 0.25
9 5.5e+00 7.2e+00 3.1e+02 8.14e-01 -8.873654488e+03 2.833843752e+03 2.5e-03 0.28
10 1.3e+00 1.8e+00 7.7e+01 9.07e-01 -2.032976954e+03 9.282385087e+02 6.1e-04 0.34
11 7.0e-01 9.2e-01 4.0e+01 9.94e-01 -8.350002142e+02 7.206024908e+02 3.2e-04 0.36
12 4.7e-01 6.2e-01 2.7e+01 9.97e-01 -4.846306076e+02 5.632460213e+02 2.1e-04 0.41
13 3.5e-01 7.3e-01 2.0e+01 9.79e-01 -3.148957258e+02 4.857769751e+02 1.6e-04 0.45
14 1.7e-01 3.5e-01 9.8e+00 9.96e-01 -1.857417116e+01 3.656902710e+02 7.9e-05 0.47
15 5.5e-02 1.5e-01 3.3e+00 9.94e-01 1.620485362e+02 2.901550655e+02 2.6e-05 0.48
16 3.2e-02 1.3e-01 1.9e+00 1.00e+00 1.996394651e+02 2.746181590e+02 1.6e-05 0.49
17 5.1e-03 1.8e-01 3.3e-01 1.00e+00 2.444824012e+02 2.572405213e+02 2.8e-06 0.51
18 1.5e-03 1.3e-01 9.6e-02 1.00e+00 2.509288752e+02 2.546905409e+02 8.3e-07 0.52
19 4.8e-04 1.1e-01 3.2e-02 1.00e+00 2.527800443e+02 2.540213968e+02 2.8e-07 0.53
20 2.1e-04 8.6e-02 1.4e-02 1.00e+00 2.532857302e+02 2.538354980e+02 1.2e-07 0.54
21 1.9e-04 7.8e-02 1.3e-02 1.00e+00 2.533271035e+02 2.538219096e+02 1.1e-07 0.56
22 1.7e-04 7.1e-02 1.1e-02 1.00e+00 2.533631909e+02 2.538084914e+02 1.0e-07 0.57
23 1.5e-04 6.4e-02 1.0e-02 1.00e+00 2.533957124e+02 2.537964664e+02 9.0e-08 0.58
24 1.4e-04 5.9e-02 9.3e-03 1.00e+00 2.534249555e+02 2.537856200e+02 8.1e-08 0.60
25 1.2e-04 5.4e-02 8.3e-03 1.00e+00 2.534512557e+02 2.537758421e+02 7.3e-08 0.61
26 1.1e-04 4.9e-02 7.5e-03 1.00e+00 2.534749084e+02 2.537670264e+02 6.6e-08 0.62
27 1.0e-04 4.5e-02 6.8e-03 1.00e+00 2.534961824e+02 2.537590805e+02 5.9e-08 0.67
28 9.1e-05 4.1e-02 6.1e-03 1.00e+00 2.535153179e+02 2.537519196e+02 5.3e-08 0.75
29 8.2e-05 3.8e-02 5.5e-03 1.00e+00 2.535325308e+02 2.537454669e+02 4.8e-08 0.82
30 7.3e-05 3.5e-02 4.9e-03 1.00e+00 2.535480148e+02 2.537396530e+02 4.3e-08 0.86
31 6.6e-05 3.2e-02 4.4e-03 1.00e+00 2.535619442e+02 2.537344150e+02 3.9e-08 0.90
32 5.9e-05 2.9e-02 4.0e-03 1.00e+00 2.535744754e+02 2.537296963e+02 3.5e-08 0.95
33 5.3e-05 2.7e-02 3.6e-03 1.00e+00 2.535857490e+02 2.537254456e+02 3.1e-08 0.97
34 4.8e-05 2.5e-02 3.2e-03 1.00e+00 2.535958915e+02 2.537216167e+02 2.8e-08 1.00
35 4.3e-05 2.4e-02 2.9e-03 1.00e+00 2.536050166e+02 2.537181679e+02 2.5e-08 1.04
36 3.9e-05 2.2e-02 2.6e-03 1.00e+00 2.536132264e+02 2.537150615e+02 2.3e-08 1.09
37 3.5e-05 2.0e-02 2.4e-03 1.00e+00 2.536206130e+02 2.537122637e+02 2.1e-08 1.14
38 3.2e-05 1.9e-02 2.1e-03 1.00e+00 2.536272589e+02 2.537097440e+02 1.9e-08 1.15
39 2.8e-05 1.8e-02 1.9e-03 1.00e+00 2.536332386e+02 2.537074747e+02 1.7e-08 1.19
40 2.6e-05 1.7e-02 1.7e-03 1.00e+00 2.536386189e+02 2.537054310e+02 1.5e-08 1.20
41 2.3e-05 1.6e-02 1.5e-03 1.00e+00 2.536434601e+02 2.537035907e+02 1.4e-08 1.21
42 2.1e-05 1.5e-02 1.4e-03 1.00e+00 2.536478161e+02 2.537019335e+02 1.2e-08 1.22
43 1.9e-05 1.4e-02 1.3e-03 1.00e+00 2.536517357e+02 2.537004413e+02 1.1e-08 1.24
44 1.7e-05 1.4e-02 1.1e-03 1.00e+00 2.536552627e+02 2.536990976e+02 9.8e-09 1.24
45 1.5e-05 1.3e-02 1.0e-03 1.00e+00 2.536584365e+02 2.536978878e+02 8.9e-09 1.25
46 1.4e-05 1.3e-02 9.1e-04 1.00e+00 2.536612924e+02 2.536967986e+02 8.0e-09 1.26
47 1.2e-05 1.2e-02 8.2e-04 1.00e+00 2.536638623e+02 2.536958179e+02 7.2e-09 1.27
48 1.1e-05 1.2e-02 7.4e-04 1.00e+00 2.536661750e+02 2.536949350e+02 6.5e-09 1.29
49 9.9e-06 1.1e-02 6.7e-04 1.00e+00 2.536682562e+02 2.536941402e+02 5.8e-09 1.30
50 8.9e-06 1.1e-02 6.0e-04 1.00e+00 2.536701290e+02 2.536934247e+02 5.2e-09 1.31
51 8.0e-06 1.0e-02 5.4e-04 1.00e+00 2.536718144e+02 2.536927806e+02 4.7e-09 1.32
52 7.2e-06 1.0e-02 4.9e-04 1.00e+00 2.536733312e+02 2.536922007e+02 4.2e-09 1.33
53 6.5e-06 9.9e-03 4.4e-04 1.00e+00 2.536746961e+02 2.536916788e+02 3.8e-09 1.35
54 5.9e-06 9.6e-03 3.9e-04 1.00e+00 2.536759245e+02 2.536912089e+02 3.4e-09 1.36
55 5.3e-06 9.4e-03 3.5e-04 1.00e+00 2.536770300e+02 2.536907860e+02 3.1e-09 1.37
56 4.7e-06 9.2e-03 3.2e-04 1.00e+00 2.536780248e+02 2.536904052e+02 2.8e-09 1.39
57 4.3e-06 9.0e-03 2.9e-04 1.00e+00 2.536789201e+02 2.536900625e+02 2.5e-09 1.43
58 3.8e-06 8.9e-03 2.6e-04 1.00e+00 2.536797258e+02 2.536897540e+02 2.3e-09 1.44
59 3.5e-06 8.7e-03 2.3e-04 1.00e+00 2.536804509e+02 2.536894763e+02 2.0e-09 1.48
60 3.1e-06 8.6e-03 2.1e-04 1.00e+00 2.536811034e+02 2.536892263e+02 1.8e-09 1.54
61 1.2e-06 3.3e-03 8.1e-05 1.00e+00 2.536846840e+02 2.536878533e+02 7.1e-10 1.57
62 1.1e-06 3.0e-03 7.3e-05 1.00e+00 2.536849137e+02 2.536877661e+02 6.4e-10 1.62
63 1.1e-06 3.0e-03 7.2e-05 1.00e+00 2.536849536e+02 2.536877507e+02 6.3e-10 1.67
64 9.7e-07 2.7e-03 6.5e-05 1.00e+00 2.536851456e+02 2.536876770e+02 5.7e-10 1.72
65 8.7e-07 2.4e-03 5.9e-05 1.00e+00 2.536853285e+02 2.536876068e+02 5.1e-10 1.78
66 8.5e-07 2.4e-03 5.7e-05 1.00e+00 2.536853604e+02 2.536875946e+02 5.0e-10 1.80
67 7.8e-07 2.2e-03 5.2e-05 1.00e+00 2.536855061e+02 2.536875387e+02 4.6e-10 1.88
68 1.6e-07 4.5e-04 1.1e-05 1.00e+00 2.536866722e+02 2.536870910e+02 9.4e-11 1.89
69 1.4e-07 4.1e-04 9.7e-06 1.00e+00 2.536867026e+02 2.536870795e+02 8.5e-11 1.91
70 1.4e-07 3.9e-04 9.3e-06 1.00e+00 2.536867146e+02 2.536870749e+02 8.1e-11 1.92
71 1.4e-07 3.9e-04 9.2e-06 1.00e+00 2.536867155e+02 2.536870745e+02 8.1e-11 1.93
72 1.4e-07 3.9e-04 9.2e-06 1.00e+00 2.536867165e+02 2.536870741e+02 8.0e-11 1.95
73 1.3e-07 3.6e-04 8.6e-06 1.00e+00 2.536867336e+02 2.536870675e+02 7.5e-11 1.96
74 1.2e-07 3.3e-04 7.8e-06 1.00e+00 2.536867565e+02 2.536870587e+02 6.8e-11 1.97
75 1.0e-07 3.0e-04 7.0e-06 1.00e+00 2.536867773e+02 2.536870507e+02 6.1e-11 1.98
76 1.0e-07 3.0e-04 7.0e-06 1.00e+00 2.536867780e+02 2.536870505e+02 6.1e-11 1.99
77 1.0e-07 2.9e-04 6.9e-06 1.00e+00 2.536867818e+02 2.536870490e+02 6.0e-11 2.01
78 1.0e-07 2.9e-04 6.8e-06 1.00e+00 2.536867825e+02 2.536870487e+02 6.0e-11 2.02
79 9.1e-08 2.6e-04 6.2e-06 1.00e+00 2.536868018e+02 2.536870413e+02 5.4e-11 2.03
80 8.4e-08 2.4e-04 5.7e-06 1.00e+00 2.536868158e+02 2.536870359e+02 4.9e-11 2.05
81 8.4e-08 2.4e-04 5.7e-06 1.00e+00 2.536868159e+02 2.536870359e+02 4.9e-11 2.06
82 7.6e-08 2.2e-04 5.1e-06 1.00e+00 2.536868317e+02 2.536870298e+02 4.4e-11 2.07
83 6.9e-08 2.0e-04 4.7e-06 1.00e+00 2.536868434e+02 2.536870253e+02 4.1e-11 2.09
84 6.2e-08 1.8e-04 4.2e-06 1.00e+00 2.536868565e+02 2.536870202e+02 3.7e-11 2.10
85 6.1e-08 1.7e-04 4.1e-06 1.00e+00 2.536868588e+02 2.536870193e+02 3.6e-11 2.11
86 6.1e-08 1.7e-04 4.1e-06 1.00e+00 2.536868588e+02 2.536870193e+02 3.6e-11 2.16
87 5.5e-08 1.6e-04 3.7e-06 1.00e+00 2.536868698e+02 2.536870151e+02 3.3e-11 2.21
88 5.5e-08 1.6e-04 3.7e-06 1.00e+00 2.536868698e+02 2.536870151e+02 3.3e-11 2.23
89 5.0e-08 1.4e-04 3.4e-06 1.00e+00 2.536868798e+02 2.536870112e+02 3.0e-11 2.24
90 4.5e-08 1.3e-04 3.1e-06 1.00e+00 2.536868888e+02 2.536870078e+02 2.7e-11 2.43
91 4.5e-08 1.3e-04 3.1e-06 1.00e+00 2.536868888e+02 2.536870078e+02 2.7e-11 2.48
92 4.1e-08 1.2e-04 2.8e-06 1.00e+00 2.536868974e+02 2.536870045e+02 2.4e-11 2.55
93 3.8e-08 1.1e-04 2.6e-06 1.00e+00 2.536869025e+02 2.536870025e+02 2.2e-11 2.60
94 3.8e-08 1.1e-04 2.6e-06 1.00e+00 2.536869025e+02 2.536870025e+02 2.2e-11 2.67
95 3.8e-08 1.1e-04 2.6e-06 1.00e+00 2.536869026e+02 2.536870025e+02 2.2e-11 2.73
96 3.4e-08 9.8e-05 2.3e-06 9.99e-01 2.536869098e+02 2.536869997e+02 2.0e-11 2.78
97 3.1e-08 8.8e-05 2.1e-06 1.00e+00 2.536869159e+02 2.536869973e+02 1.8e-11 2.80
98 3.1e-08 8.8e-05 2.1e-06 1.00e+00 2.536869159e+02 2.536869973e+02 1.8e-11 2.81
99 2.8e-08 8.0e-05 1.9e-06 9.99e-01 2.536869218e+02 2.536869951e+02 1.6e-11 2.82
100 2.7e-08 7.6e-05 1.8e-06 1.00e+00 2.536869241e+02 2.536869942e+02 1.6e-11 2.84
101 2.4e-08 6.8e-05 1.6e-06 1.00e+00 2.536869292e+02 2.536869922e+02 1.4e-11 2.99
102 2.2e-08 6.2e-05 1.5e-06 9.99e-01 2.536869337e+02 2.536869905e+02 1.3e-11 3.17
103 2.0e-08 5.6e-05 1.3e-06 9.99e-01 2.536869376e+02 2.536869890e+02 1.2e-11 3.34
104 1.8e-08 5.1e-05 1.2e-06 1.00e+00 2.536869406e+02 2.536869878e+02 1.1e-11 3.37
105 1.8e-08 5.1e-05 1.2e-06 1.00e+00 2.536869406e+02 2.536869878e+02 1.1e-11 3.44
106 1.6e-08 4.6e-05 1.1e-06 1.00e+00 2.536869440e+02 2.536869865e+02 9.5e-12 3.63
107 1.5e-08 4.2e-05 9.9e-07 1.00e+00 2.536869469e+02 2.536869853e+02 8.6e-12 3.77
108 1.4e-08 3.9e-05 9.2e-07 1.00e+00 2.536869488e+02 2.536869846e+02 8.1e-12 3.94
109 1.2e-08 3.5e-05 8.3e-07 1.00e+00 2.536869512e+02 2.536869837e+02 7.3e-12 4.07
110 1.2e-08 3.5e-05 8.3e-07 1.00e+00 2.536869512e+02 2.536869837e+02 7.3e-12 4.19
111 1.1e-08 3.2e-05 7.5e-07 1.00e+00 2.536869536e+02 2.536869828e+02 6.6e-12 4.43
112 1.0e-08 2.9e-05 6.8e-07 1.00e+00 2.536869557e+02 2.536869820e+02 5.9e-12 4.65
Interior-point optimizer terminated. Time: 4.65.
Optimizer terminated. Time: 4.66
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 2.5368695571e+02 Viol. con: 2e-07 var: 0e+00
Dual. obj: 2.5368698196e+02 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 4.68 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.02
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 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 : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.286636032e+05 2.000000000e+00 1.0e+00 0.05
1 1.1e+03 1.4e+03 6.0e+04 -9.71e-01 -1.264180260e+05 3.781070854e+00 4.7e-01 0.11
2 4.6e+02 6.0e+02 2.6e+04 -9.35e-01 -1.210471961e+05 9.871250675e+00 2.0e-01 0.15
3 2.9e+02 3.8e+02 1.6e+04 -8.50e-01 -1.158624976e+05 5.253701891e+01 1.3e-01 0.17
4 2.9e+02 3.8e+02 1.6e+04 -7.62e-01 -1.137381539e+05 1.863811989e+03 1.3e-01 0.18
5 8.3e+01 1.1e+02 4.6e+03 -7.57e-01 -7.842864608e+04 9.038469625e+03 3.6e-02 0.20
6 3.6e+01 4.7e+01 2.0e+03 -2.53e-01 -4.698030065e+04 1.010176986e+04 1.6e-02 0.21
7 1.8e+01 2.4e+01 1.0e+03 2.76e-01 -2.813348721e+04 6.397682980e+03 8.2e-03 0.22
8 9.2e+00 1.2e+01 5.1e+02 6.02e-01 -1.477869526e+04 4.004072554e+03 4.0e-03 0.23
9 5.7e+00 7.4e+00 3.2e+02 8.20e-01 -9.247829971e+03 2.776682029e+03 2.5e-03 0.24
10 1.9e+00 2.5e+00 1.1e+02 9.03e-01 -3.003060412e+03 1.154002790e+03 8.5e-04 0.25
11 1.6e+00 2.0e+00 8.8e+01 9.75e-01 -2.419019018e+03 1.010907137e+03 7.0e-04 0.27
12 1.0e+00 1.4e+00 5.7e+01 9.77e-01 -1.494909804e+03 7.263450153e+02 4.5e-04 0.28
13 4.7e-01 7.0e-01 2.7e+01 9.83e-01 -6.134620377e+02 4.375216351e+02 2.1e-04 0.29
14 2.5e-01 3.8e-01 1.4e+01 1.00e+00 -2.355955495e+02 3.290668990e+02 1.1e-04 0.30
15 1.0e-01 1.7e-01 5.9e+00 1.00e+00 7.317587883e+00 2.369834124e+02 4.7e-05 0.31
16 5.0e-02 1.0e-01 2.9e+00 1.00e+00 9.073386498e+01 2.038614809e+02 2.3e-05 0.32
17 1.0e-02 1.5e-01 6.3e-01 1.01e+00 1.546017193e+02 1.791070628e+02 5.2e-06 0.33
18 6.2e-03 1.0e-01 3.8e-01 1.01e+00 1.615121007e+02 1.764421344e+02 3.2e-06 0.34
19 1.6e-03 1.2e-01 1.0e-01 1.01e+00 1.694752257e+02 1.734658673e+02 8.7e-07 0.35
20 3.3e-04 1.5e-01 2.2e-02 1.01e+00 1.717779141e+02 1.726253081e+02 1.9e-07 0.39
21 1.4e-04 1.0e-01 9.3e-03 9.93e-01 1.721395923e+02 1.725021455e+02 8.2e-08 0.44
22 8.8e-05 8.3e-02 5.9e-03 1.00e+00 1.722353223e+02 1.724645586e+02 5.2e-08 0.48
23 7.9e-05 7.7e-02 5.3e-03 1.00e+00 1.722533711e+02 1.724597544e+02 4.7e-08 0.52
24 7.1e-05 7.0e-02 4.8e-03 1.00e+00 1.722685690e+02 1.724543185e+02 4.2e-08 0.53
25 6.4e-05 6.4e-02 4.3e-03 1.00e+00 1.722822901e+02 1.724494655e+02 3.8e-08 0.58
26 5.8e-05 5.8e-02 3.9e-03 1.00e+00 1.722946100e+02 1.724450675e+02 3.4e-08 0.63
27 5.2e-05 5.3e-02 3.5e-03 1.00e+00 1.723056850e+02 1.724410958e+02 3.1e-08 0.67
28 4.7e-05 4.9e-02 3.1e-03 1.00e+00 1.723156375e+02 1.724375061e+02 2.8e-08 0.68
29 4.2e-05 4.5e-02 2.8e-03 1.00e+00 1.723245812e+02 1.724342618e+02 2.5e-08 0.70
30 3.8e-05 4.1e-02 2.5e-03 1.00e+00 1.723326184e+02 1.724313298e+02 2.2e-08 0.71
31 3.4e-05 3.8e-02 2.3e-03 1.00e+00 1.723398411e+02 1.724286804e+02 2.0e-08 0.72
32 3.1e-05 3.5e-02 2.1e-03 1.00e+00 1.723463325e+02 1.724262871e+02 1.8e-08 0.73
33 2.8e-05 3.2e-02 1.9e-03 1.00e+00 1.723521673e+02 1.724241257e+02 1.6e-08 0.85
34 2.5e-05 3.0e-02 1.7e-03 1.00e+00 1.723574125e+02 1.724221744e+02 1.5e-08 0.89
35 2.2e-05 2.8e-02 1.5e-03 1.00e+00 1.723621282e+02 1.724204134e+02 1.3e-08 0.90
36 2.0e-05 2.6e-02 1.4e-03 1.00e+00 1.723663682e+02 1.724188245e+02 1.2e-08 0.92
37 1.8e-05 2.4e-02 1.2e-03 1.00e+00 1.723701808e+02 1.724173911e+02 1.1e-08 0.93
38 1.6e-05 2.2e-02 1.1e-03 1.00e+00 1.723736094e+02 1.724160984e+02 9.6e-09 0.94
39 1.5e-05 2.1e-02 9.9e-04 1.00e+00 1.723766927e+02 1.724149327e+02 8.6e-09 0.95
40 1.3e-05 1.9e-02 8.9e-04 1.00e+00 1.723794658e+02 1.724138818e+02 7.8e-09 0.97
41 1.2e-05 1.8e-02 8.0e-04 1.00e+00 1.723819600e+02 1.724129343e+02 7.0e-09 0.98
42 1.1e-05 1.7e-02 7.2e-04 1.00e+00 1.723842034e+02 1.724120802e+02 6.3e-09 0.99
43 9.6e-06 1.6e-02 6.5e-04 1.00e+00 1.723862213e+02 1.724113105e+02 5.7e-09 1.02
44 8.7e-06 1.5e-02 5.8e-04 1.00e+00 1.723880365e+02 1.724106167e+02 5.1e-09 1.07
45 7.8e-06 1.5e-02 5.2e-04 1.00e+00 1.723896694e+02 1.724099916e+02 4.6e-09 1.08
46 7.0e-06 1.4e-02 4.7e-04 1.00e+00 1.723911383e+02 1.724094283e+02 4.1e-09 1.13
47 6.3e-06 1.3e-02 4.3e-04 1.00e+00 1.723924598e+02 1.724089208e+02 3.7e-09 1.18
48 5.7e-06 1.3e-02 3.8e-04 1.00e+00 1.723936486e+02 1.724084637e+02 3.3e-09 1.21
49 5.1e-06 1.2e-02 3.4e-04 1.00e+00 1.723947182e+02 1.724080518e+02 3.0e-09 1.26
50 4.6e-06 1.2e-02 3.1e-04 1.00e+00 1.723956805e+02 1.724076808e+02 2.7e-09 1.28
51 4.2e-06 1.1e-02 2.8e-04 1.00e+00 1.723965462e+02 1.724073466e+02 2.4e-09 1.29
52 3.7e-06 1.1e-02 2.5e-04 1.00e+00 1.723973252e+02 1.724070456e+02 2.2e-09 1.30
53 3.4e-06 1.1e-02 2.3e-04 1.00e+00 1.723980261e+02 1.724067745e+02 2.0e-09 1.31
54 3.0e-06 1.0e-02 2.0e-04 1.00e+00 1.723986568e+02 1.724065303e+02 1.8e-09 1.33
55 2.7e-06 1.0e-02 1.8e-04 1.00e+00 1.723992242e+02 1.724063104e+02 1.6e-09 1.34
56 2.5e-06 9.7e-03 1.6e-04 1.00e+00 1.723997348e+02 1.724061124e+02 1.4e-09 1.35
57 2.2e-06 9.5e-03 1.5e-04 1.00e+00 1.724001943e+02 1.724059341e+02 1.3e-09 1.37
58 2.0e-06 9.3e-03 1.3e-04 1.00e+00 1.724006077e+02 1.724057736e+02 1.2e-09 1.38
59 1.8e-06 9.1e-03 1.2e-04 1.00e+00 1.724009797e+02 1.724056290e+02 1.1e-09 1.39
60 1.6e-06 9.0e-03 1.1e-04 1.00e+00 1.724013144e+02 1.724054988e+02 9.5e-10 1.40
61 1.4e-06 8.8e-03 9.7e-05 1.00e+00 1.724016156e+02 1.724053816e+02 8.5e-10 1.42
62 1.3e-06 8.7e-03 8.8e-05 1.00e+00 1.724018867e+02 1.724052760e+02 7.7e-10 1.43
63 1.2e-06 8.6e-03 7.9e-05 1.00e+00 1.724021306e+02 1.724051810e+02 6.9e-10 1.45
64 1.1e-06 8.5e-03 7.1e-05 1.00e+00 1.724023500e+02 1.724050954e+02 6.2e-10 1.46
65 9.5e-07 8.4e-03 6.4e-05 1.00e+00 1.724025475e+02 1.724050184e+02 5.6e-10 1.47
66 8.5e-07 8.3e-03 5.7e-05 1.00e+00 1.724027253e+02 1.724049490e+02 5.0e-10 1.48
67 7.7e-07 8.2e-03 5.2e-05 1.00e+00 1.724028852e+02 1.724048866e+02 4.5e-10 1.53
68 6.9e-07 8.1e-03 4.7e-05 1.00e+00 1.724030291e+02 1.724048304e+02 4.1e-10 1.57
69 6.2e-07 8.1e-03 4.2e-05 1.00e+00 1.724031586e+02 1.724047798e+02 3.7e-10 1.63
70 5.6e-07 8.0e-03 3.8e-05 1.00e+00 1.724032751e+02 1.724047342e+02 3.3e-10 1.65
71 5.0e-07 7.9e-03 3.4e-05 1.00e+00 1.724033800e+02 1.724046932e+02 3.0e-10 1.66
72 4.5e-07 7.9e-03 3.1e-05 1.00e+00 1.724034744e+02 1.724046562e+02 2.7e-10 1.67
73 4.1e-07 7.8e-03 2.7e-05 1.00e+00 1.724035593e+02 1.724046230e+02 2.4e-10 1.69
74 3.7e-07 7.8e-03 2.5e-05 1.00e+00 1.724036357e+02 1.724045930e+02 2.2e-10 1.70
75 3.3e-07 7.7e-03 2.2e-05 1.00e+00 1.724037045e+02 1.724045661e+02 1.9e-10 1.71
76 3.0e-07 7.7e-03 2.0e-05 1.00e+00 1.724037664e+02 1.724045418e+02 1.8e-10 1.73
77 2.7e-07 7.7e-03 1.8e-05 1.00e+00 1.724038221e+02 1.724045200e+02 1.6e-10 1.74
78 2.4e-07 7.6e-03 1.6e-05 1.00e+00 1.724038722e+02 1.724045003e+02 1.4e-10 1.75
79 2.2e-07 7.6e-03 1.5e-05 9.99e-01 1.724039173e+02 1.724044826e+02 1.3e-10 1.77
80 2.0e-07 7.6e-03 1.3e-05 9.99e-01 1.724039579e+02 1.724044667e+02 1.2e-10 1.78
81 1.8e-07 7.5e-03 1.2e-05 9.99e-01 1.724039944e+02 1.724044523e+02 1.0e-10 1.79
82 1.6e-07 7.5e-03 1.1e-05 1.00e+00 1.724040273e+02 1.724044394e+02 9.3e-11 1.80
83 1.4e-07 7.5e-03 9.6e-06 9.99e-01 1.724040568e+02 1.724044277e+02 8.4e-11 1.82
84 1.3e-07 7.5e-03 8.6e-06 1.00e+00 1.724040834e+02 1.724044173e+02 7.5e-11 1.83
85 1.2e-07 7.4e-03 7.8e-06 9.99e-01 1.724041074e+02 1.724044079e+02 6.8e-11 1.84
86 1.0e-07 7.4e-03 7.0e-06 1.00e+00 1.724041289e+02 1.724043993e+02 6.1e-11 1.86
87 9.4e-08 7.4e-03 6.3e-06 9.99e-01 1.724041483e+02 1.724043917e+02 5.5e-11 1.87
88 8.4e-08 7.4e-03 5.7e-06 9.96e-01 1.724041658e+02 1.724043849e+02 5.0e-11 1.88
89 7.6e-08 7.4e-03 5.1e-06 9.98e-01 1.724041815e+02 1.724043787e+02 4.5e-11 1.89
90 6.8e-08 7.3e-03 4.6e-06 9.97e-01 1.724041956e+02 1.724043731e+02 4.0e-11 1.90
91 6.1e-08 7.3e-03 4.1e-06 9.98e-01 1.724042083e+02 1.724043681e+02 3.6e-11 1.91
92 5.5e-08 7.3e-03 3.7e-06 1.00e+00 1.724042198e+02 1.724043636e+02 3.2e-11 1.92
93 5.0e-08 7.3e-03 3.3e-06 1.00e+00 1.724042301e+02 1.724043595e+02 2.9e-11 1.93
94 4.5e-08 7.3e-03 3.0e-06 1.00e+00 1.724042394e+02 1.724043558e+02 2.6e-11 1.97
95 4.0e-08 7.3e-03 2.7e-06 1.00e+00 1.724042477e+02 1.724043525e+02 2.4e-11 1.98
96 3.6e-08 7.3e-03 2.4e-06 9.93e-01 1.724042552e+02 1.724043496e+02 2.1e-11 2.02
97 3.3e-08 6.5e-03 2.2e-06 1.00e+00 1.724042620e+02 1.724043469e+02 1.9e-11 2.03
98 2.9e-08 5.9e-03 2.0e-06 1.00e+00 1.724042681e+02 1.724043445e+02 1.7e-11 2.05
99 2.6e-08 5.3e-03 1.8e-06 9.91e-01 1.724042735e+02 1.724043423e+02 1.6e-11 2.06
100 2.4e-08 4.8e-03 1.6e-06 1.01e+00 1.724042788e+02 1.724043402e+02 1.4e-11 2.08
101 2.1e-08 4.3e-03 1.4e-06 9.99e-01 1.724042832e+02 1.724043385e+02 1.3e-11 2.10
102 1.9e-08 3.9e-03 1.3e-06 1.01e+00 1.724042873e+02 1.724043368e+02 1.1e-11 2.11
103 1.7e-08 3.5e-03 1.2e-06 1.01e+00 1.724042910e+02 1.724043353e+02 1.0e-11 2.12
104 1.6e-08 3.1e-03 1.0e-06 1.00e+00 1.724042942e+02 1.724043341e+02 9.3e-12 2.13
105 4.4e-09 7.7e-04 2.6e-07 9.98e-01 1.724043157e+02 1.724043256e+02 2.3e-12 2.15
106 3.9e-09 7.0e-04 2.3e-07 1.03e+00 1.724043165e+02 1.724043253e+02 2.1e-12 2.16
107 1.3e-09 1.7e-04 5.8e-08 1.07e+00 1.724043212e+02 1.724043232e+02 4.9e-13 2.17
Interior-point optimizer terminated. Time: 2.17.
Optimizer terminated. Time: 2.18
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.7240432117e+02 Viol. con: 2e-08 var: 0e+00
Dual. obj: 1.7240432323e+02 Viol. con: 0e+00 var: 1e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.2 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
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.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 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 : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.289209279e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.267404395e+05 3.637047323e+00 4.8e-01 0.05
2 4.4e+02 5.7e+02 2.4e+04 -9.36e-01 -1.207993260e+05 1.004622010e+01 1.9e-01 0.06
3 2.9e+02 3.8e+02 1.6e+04 -8.43e-01 -1.160618628e+05 5.990662233e+01 1.3e-01 0.07
4 2.9e+02 3.8e+02 1.6e+04 -7.62e-01 -1.136045221e+05 2.136092785e+03 1.3e-01 0.10
5 8.1e+01 1.0e+02 4.5e+03 -7.56e-01 -7.752618955e+04 9.316590632e+03 3.5e-02 0.11
6 4.0e+01 5.2e+01 2.2e+03 -2.34e-01 -5.076741252e+04 1.003179833e+04 1.8e-02 0.12
7 3.0e+01 3.9e+01 1.7e+03 2.19e-01 -4.171035381e+04 8.294890628e+03 1.3e-02 0.15
8 1.9e+01 2.4e+01 1.0e+03 3.81e-01 -2.865141899e+04 5.387064689e+03 8.1e-03 0.17
9 7.9e+00 1.0e+01 4.4e+02 6.03e-01 -1.310597210e+04 3.143049736e+03 3.5e-03 0.18
10 4.0e+00 5.2e+00 2.2e+02 8.46e-01 -6.378101576e+03 2.128677120e+03 1.8e-03 0.21
11 2.2e+00 2.9e+00 1.3e+02 9.42e-01 -3.514555688e+03 1.314876543e+03 9.9e-04 0.27
12 9.1e-01 1.2e+00 5.1e+01 9.75e-01 -1.333953141e+03 6.456467148e+02 4.0e-04 0.28
13 8.2e-01 1.1e+00 4.6e+01 9.70e-01 -1.223648492e+03 5.999353713e+02 3.7e-04 0.29
14 5.9e-01 7.8e-01 3.3e+01 9.74e-01 -8.149794417e+02 4.893554429e+02 2.6e-04 0.30
15 2.2e-01 7.6e-01 1.2e+01 9.90e-01 -1.999795996e+02 2.844530000e+02 9.8e-05 0.32
16 1.1e-01 3.8e-01 6.1e+00 1.00e+00 -2.241201048e+01 2.161154382e+02 4.9e-05 0.33
17 7.7e-02 2.8e-01 4.5e+00 1.01e+00 2.681073930e+01 2.015603399e+02 3.6e-05 0.34
18 5.1e-02 2.0e-01 3.0e+00 1.02e+00 7.892007143e+01 1.950358756e+02 2.4e-05 0.35
19 1.4e-02 1.1e-01 8.5e-01 1.00e+00 1.414700276e+02 1.745815002e+02 6.9e-06 0.35
20 4.0e-03 2.2e-01 2.4e-01 1.02e+00 1.602704576e+02 1.696481183e+02 1.9e-06 0.36
21 2.7e-03 2.1e-01 1.6e-01 1.01e+00 1.624284108e+02 1.687369719e+02 1.3e-06 0.37
22 1.9e-03 1.5e-01 1.2e-01 1.00e+00 1.637170023e+02 1.683012331e+02 9.5e-07 0.38
23 7.5e-04 9.5e-02 4.7e-02 1.01e+00 1.658030249e+02 1.676006389e+02 3.8e-07 0.39
24 3.6e-04 7.9e-02 2.3e-02 1.01e+00 1.664694569e+02 1.673480746e+02 1.9e-07 0.40
25 3.3e-04 7.2e-02 2.1e-02 1.01e+00 1.665375736e+02 1.673287231e+02 1.7e-07 0.41
26 3.0e-04 6.6e-02 1.9e-02 1.01e+00 1.665946655e+02 1.673064407e+02 1.5e-07 0.42
27 2.7e-04 6.0e-02 1.7e-02 1.01e+00 1.666462522e+02 1.672866431e+02 1.4e-07 0.43
28 2.4e-04 5.5e-02 1.5e-02 1.01e+00 1.666924449e+02 1.672686263e+02 1.2e-07 0.45
29 2.2e-04 5.0e-02 1.4e-02 1.01e+00 1.667338925e+02 1.672523163e+02 1.1e-07 0.46
30 1.9e-04 4.6e-02 1.2e-02 1.01e+00 1.667710545e+02 1.672375218e+02 9.9e-08 0.47
31 1.7e-04 4.2e-02 1.1e-02 1.01e+00 1.668043755e+02 1.672241027e+02 8.9e-08 0.48
32 1.6e-04 3.8e-02 9.9e-03 1.01e+00 1.668342505e+02 1.672119290e+02 8.0e-08 0.50
33 1.4e-04 3.5e-02 8.9e-03 1.01e+00 1.668610362e+02 1.672008851e+02 7.2e-08 0.51
34 1.3e-04 3.3e-02 8.0e-03 1.01e+00 1.668850531e+02 1.671908670e+02 6.5e-08 0.52
35 1.1e-04 3.0e-02 7.2e-03 1.01e+00 1.669065896e+02 1.671817816e+02 5.8e-08 0.53
36 1.0e-04 2.8e-02 6.5e-03 1.00e+00 1.669259047e+02 1.671735449e+02 5.3e-08 0.54
37 9.3e-05 2.6e-02 5.8e-03 1.00e+00 1.669432306e+02 1.671660806e+02 4.7e-08 0.55
38 8.3e-05 2.4e-02 5.3e-03 1.00e+00 1.669587748e+02 1.671593190e+02 4.3e-08 0.56
39 7.5e-05 2.2e-02 4.7e-03 1.00e+00 1.669727231e+02 1.671531963e+02 3.8e-08 0.63
40 6.8e-05 2.1e-02 4.3e-03 1.00e+00 1.669852412e+02 1.671476540e+02 3.5e-08 0.69
41 6.1e-05 2.0e-02 3.8e-03 1.00e+00 1.669964774e+02 1.671426385e+02 3.1e-08 0.75
42 5.5e-05 1.8e-02 3.4e-03 1.00e+00 1.670065645e+02 1.671381014e+02 2.8e-08 0.80
43 4.9e-05 1.7e-02 3.1e-03 1.00e+00 1.670156210e+02 1.671339979e+02 2.5e-08 0.85
44 4.4e-05 1.6e-02 2.8e-03 1.00e+00 1.670237533e+02 1.671302877e+02 2.3e-08 0.88
45 4.0e-05 1.6e-02 2.5e-03 1.00e+00 1.670310565e+02 1.671269338e+02 2.0e-08 1.01
46 3.6e-05 1.5e-02 2.3e-03 1.00e+00 1.670376160e+02 1.671239028e+02 1.8e-08 1.24
47 3.2e-05 1.4e-02 2.0e-03 1.00e+00 1.670435081e+02 1.671211642e+02 1.7e-08 1.69
48 2.9e-05 1.4e-02 1.8e-03 1.00e+00 1.670488012e+02 1.671186902e+02 1.5e-08 2.05
49 2.6e-05 1.3e-02 1.7e-03 1.00e+00 1.670535568e+02 1.671164557e+02 1.3e-08 2.19
50 2.4e-05 1.3e-02 1.5e-03 1.00e+00 1.670578298e+02 1.671144381e+02 1.2e-08 2.36
51 2.1e-05 1.2e-02 1.3e-03 1.00e+00 1.670616696e+02 1.671126165e+02 1.1e-08 2.43
52 1.9e-05 1.2e-02 1.2e-03 1.00e+00 1.670651203e+02 1.671109722e+02 9.8e-09 2.73
53 1.7e-05 1.1e-02 1.1e-03 1.00e+00 1.670682217e+02 1.671094882e+02 8.8e-09 3.00
54 1.5e-05 1.1e-02 9.7e-04 1.00e+00 1.670710093e+02 1.671081491e+02 7.9e-09 3.42
55 1.4e-05 1.1e-02 8.8e-04 1.00e+00 1.670735151e+02 1.671069409e+02 7.1e-09 3.78
56 1.3e-05 1.0e-02 7.9e-04 1.00e+00 1.670757678e+02 1.671058510e+02 6.4e-09 3.93
57 1.1e-05 1.0e-02 7.1e-04 1.00e+00 1.670777930e+02 1.671048679e+02 5.8e-09 4.34
58 1.0e-05 1.0e-02 6.4e-04 1.00e+00 1.670796139e+02 1.671039814e+02 5.2e-09 4.72
59 9.1e-06 9.8e-03 5.8e-04 1.00e+00 1.670812512e+02 1.671031821e+02 4.7e-09 5.11
60 8.2e-06 9.6e-03 5.2e-04 1.00e+00 1.670827235e+02 1.671024614e+02 4.2e-09 5.64
61 7.4e-06 9.5e-03 4.7e-04 1.00e+00 1.670840476e+02 1.671018117e+02 3.8e-09 6.35
62 6.6e-06 9.3e-03 4.2e-04 1.00e+00 1.670852383e+02 1.671012261e+02 3.4e-09 6.67
63 6.0e-06 9.2e-03 3.8e-04 1.00e+00 1.670863093e+02 1.671006984e+02 3.1e-09 6.90
64 5.4e-06 9.1e-03 3.4e-04 1.00e+00 1.670872725e+02 1.671002229e+02 2.8e-09 7.16
65 2.0e-06 3.4e-03 1.3e-04 1.00e+00 1.670926183e+02 1.670975534e+02 1.1e-09 7.43
66 6.9e-07 1.2e-03 4.4e-05 1.00e+00 1.670947944e+02 1.670964651e+02 3.6e-10 7.69
67 6.2e-07 1.0e-03 3.9e-05 1.00e+00 1.670949088e+02 1.670964123e+02 3.2e-10 8.04
68 5.6e-07 9.4e-04 3.6e-05 1.00e+00 1.670950084e+02 1.670963615e+02 2.9e-10 8.33
69 5.0e-07 8.5e-04 3.2e-05 9.99e-01 1.670950982e+02 1.670963160e+02 2.6e-10 8.52
70 4.5e-07 7.6e-04 2.9e-05 1.00e+00 1.670951789e+02 1.670962750e+02 2.3e-10 8.98
71 4.1e-07 6.9e-04 2.6e-05 1.00e+00 1.670952516e+02 1.670962379e+02 2.1e-10 9.29
72 3.7e-07 6.2e-04 2.3e-05 1.00e+00 1.670953169e+02 1.670962046e+02 1.9e-10 9.54
73 3.3e-07 5.6e-04 2.1e-05 1.00e+00 1.670953757e+02 1.670961746e+02 1.7e-10 9.81
74 3.0e-07 5.0e-04 1.9e-05 1.00e+00 1.670954286e+02 1.670961476e+02 1.5e-10 10.28
75 2.7e-07 4.5e-04 1.7e-05 1.00e+00 1.670954762e+02 1.670961233e+02 1.4e-10 10.83
76 2.4e-07 4.1e-04 1.5e-05 1.00e+00 1.670955190e+02 1.670961013e+02 1.2e-10 11.39
77 2.2e-07 3.7e-04 1.4e-05 1.00e+00 1.670955575e+02 1.670960815e+02 1.1e-10 11.84
78 2.0e-07 3.3e-04 1.2e-05 1.00e+00 1.670955921e+02 1.670960638e+02 1.0e-10 12.12
79 1.8e-07 3.0e-04 1.1e-05 9.98e-01 1.670956233e+02 1.670960478e+02 9.1e-11 12.40
80 1.6e-07 2.7e-04 1.0e-05 1.00e+00 1.670956515e+02 1.670960333e+02 8.2e-11 12.67
81 1.4e-07 2.4e-04 9.0e-06 1.00e+00 1.670956767e+02 1.670960203e+02 7.3e-11 12.96
82 1.3e-07 2.2e-04 8.1e-06 1.00e+00 1.670956994e+02 1.670960087e+02 6.6e-11 13.03
83 1.2e-07 1.9e-04 7.3e-06 9.96e-01 1.670957199e+02 1.670959982e+02 5.9e-11 13.39
84 1.0e-07 1.7e-04 6.6e-06 1.00e+00 1.670957382e+02 1.670959887e+02 5.4e-11 13.62
85 9.3e-08 1.6e-04 5.9e-06 1.00e+00 1.670957548e+02 1.670959802e+02 4.8e-11 13.79
86 8.4e-08 1.4e-04 5.3e-06 1.01e+00 1.670957699e+02 1.670959724e+02 4.3e-11 13.94
87 7.6e-08 1.3e-04 4.8e-06 9.97e-01 1.670957833e+02 1.670959656e+02 3.9e-11 14.07
88 6.8e-08 1.1e-04 4.3e-06 1.00e+00 1.670957953e+02 1.670959594e+02 3.5e-11 14.22
89 6.1e-08 1.0e-04 3.9e-06 9.94e-01 1.670958061e+02 1.670959538e+02 3.2e-11 14.32
90 5.5e-08 9.3e-05 3.5e-06 9.94e-01 1.670958159e+02 1.670959489e+02 2.8e-11 14.45
91 5.0e-08 8.4e-05 3.2e-06 1.00e+00 1.670958247e+02 1.670959443e+02 2.6e-11 14.58
92 4.5e-08 7.5e-05 2.8e-06 1.00e+00 1.670958326e+02 1.670959402e+02 2.3e-11 14.68
93 4.0e-08 6.8e-05 2.6e-06 1.01e+00 1.670958399e+02 1.670959364e+02 2.1e-11 14.81
94 3.6e-08 6.1e-05 2.3e-06 9.83e-01 1.670958463e+02 1.670959332e+02 1.9e-11 14.99
95 3.3e-08 5.5e-05 2.1e-06 1.01e+00 1.670958522e+02 1.670959301e+02 1.7e-11 15.09
96 2.9e-08 4.9e-05 1.9e-06 1.02e+00 1.670958578e+02 1.670959272e+02 1.5e-11 15.15
97 2.6e-08 4.4e-05 1.7e-06 9.96e-01 1.670958623e+02 1.670959249e+02 1.4e-11 15.27
98 2.4e-08 4.0e-05 1.5e-06 9.76e-01 1.670958664e+02 1.670959228e+02 1.2e-11 15.40
99 2.1e-08 3.6e-05 1.4e-06 1.01e+00 1.670958703e+02 1.670959208e+02 1.1e-11 15.49
100 1.9e-08 3.2e-05 1.2e-06 9.94e-01 1.670958736e+02 1.670959191e+02 1.0e-11 15.80
101 1.7e-08 2.9e-05 1.1e-06 1.02e+00 1.670958768e+02 1.670959174e+02 9.2e-12 16.02
Interior-point optimizer terminated. Time: 16.03.
Optimizer terminated. Time: 16.04
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6709587681e+02 Viol. con: 3e-07 var: 0e+00
Dual. obj: 1.6709591743e+02 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 16.1 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
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.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 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 : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.286499298e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.264834069e+05 3.586695488e+00 4.8e-01 0.18
2 4.3e+02 5.6e+02 2.4e+04 -9.36e-01 -1.204818408e+05 1.001252852e+01 1.9e-01 0.44
3 2.9e+02 3.7e+02 1.6e+04 -8.42e-01 -1.157492292e+05 6.085649918e+01 1.3e-01 0.87
4 2.9e+02 3.7e+02 1.6e+04 -7.62e-01 -1.131499805e+05 2.257752192e+03 1.3e-01 1.49
5 7.4e+01 9.6e+01 4.1e+03 -7.55e-01 -7.449025152e+04 9.842634114e+03 3.3e-02 1.64
6 3.6e+01 4.7e+01 2.0e+03 -1.90e-01 -4.726343942e+04 1.026281828e+04 1.6e-02 1.87
7 2.2e+01 2.9e+01 1.3e+03 2.77e-01 -3.297733606e+04 7.148459883e+03 9.9e-03 2.21
8 1.4e+01 1.7e+01 7.5e+02 5.32e-01 -2.145913430e+04 4.808156211e+03 6.0e-03 2.59
9 5.3e+00 6.9e+00 3.0e+02 7.21e-01 -8.768077140e+03 2.417294393e+03 2.4e-03 2.86
10 2.4e+00 3.1e+00 1.3e+02 9.13e-01 -3.743298654e+03 1.405439341e+03 1.1e-03 3.11
11 1.7e+00 2.3e+00 9.8e+01 9.75e-01 -2.706783635e+03 1.075294761e+03 7.8e-04 3.43
12 8.2e-01 1.1e+00 4.6e+01 9.83e-01 -1.189758577e+03 5.993132962e+02 3.7e-04 3.77
13 7.5e-01 1.1e+00 4.2e+01 9.48e-01 -1.109365023e+03 5.596606911e+02 3.4e-04 4.09
14 6.3e-01 8.8e-01 3.5e+01 9.86e-01 -8.799127583e+02 5.072307533e+02 2.8e-04 4.58
15 1.8e-01 2.8e-01 1.0e+01 9.89e-01 -1.584747447e+02 2.542000438e+02 8.4e-05 5.04
16 1.0e-01 1.7e-01 5.9e+00 1.01e+00 -1.976707451e+01 2.098853099e+02 4.7e-05 5.33
17 1.0e-01 1.7e-01 5.8e+00 1.02e+00 -1.809004746e+01 2.102290929e+02 4.7e-05 5.60
18 8.6e-02 1.5e-01 5.0e+00 1.02e+00 1.591141088e+01 2.106371433e+02 4.0e-05 5.85
19 4.3e-02 9.6e-02 2.5e+00 1.01e+00 9.060665396e+01 1.877232512e+02 2.0e-05 6.02
20 1.2e-02 1.9e-01 6.8e-01 1.01e+00 1.471514505e+02 1.733932142e+02 5.5e-06 6.23
21 4.3e-03 3.5e-01 2.6e-01 1.01e+00 1.590258134e+02 1.689635190e+02 2.1e-06 6.26
22 1.2e-03 1.7e-01 7.5e-02 1.01e+00 1.645644512e+02 1.674295875e+02 6.1e-07 6.29
23 6.7e-04 1.2e-01 4.2e-02 9.81e-01 1.654779071e+02 1.670872399e+02 3.5e-07 6.80
24 2.0e-04 1.1e-01 1.3e-02 9.95e-01 1.662934708e+02 1.667797855e+02 1.1e-07 7.11
25 6.2e-05 1.1e-01 4.1e-03 1.01e+00 1.665280619e+02 1.666838915e+02 3.5e-08 7.38
26 2.0e-05 1.1e-01 1.4e-03 1.01e+00 1.666013411e+02 1.666531233e+02 1.2e-08 7.75
27 6.5e-06 1.1e-01 4.4e-04 1.00e+00 1.666261907e+02 1.666427298e+02 3.8e-09 7.98
28 2.2e-06 1.0e-01 1.5e-04 1.00e+00 1.666337612e+02 1.666395177e+02 1.3e-09 8.25
29 7.7e-07 9.7e-02 5.3e-05 1.00e+00 1.666363786e+02 1.666383683e+02 4.5e-10 8.41
30 3.4e-07 8.2e-02 2.3e-05 1.00e+00 1.666371513e+02 1.666380164e+02 2.0e-10 8.57
31 7.3e-08 1.8e-02 5.0e-06 1.00e+00 1.666376162e+02 1.666378047e+02 4.3e-11 8.59
32 6.6e-08 1.6e-02 4.5e-06 1.00e+00 1.666376302e+02 1.666377998e+02 3.9e-11 8.60
33 5.9e-08 1.6e-02 4.1e-06 1.01e+00 1.666376419e+02 1.666377943e+02 3.5e-11 8.66
34 5.3e-08 1.5e-02 3.7e-06 9.99e-01 1.666376523e+02 1.666377895e+02 3.1e-11 8.89
35 4.8e-08 1.4e-02 3.3e-06 1.01e+00 1.666376618e+02 1.666377850e+02 2.8e-11 9.13
36 4.3e-08 1.3e-02 3.0e-06 9.96e-01 1.666376702e+02 1.666377811e+02 2.6e-11 9.29
37 3.9e-08 1.3e-02 2.7e-06 9.99e-01 1.666376778e+02 1.666377776e+02 2.3e-11 9.43
38 3.5e-08 1.2e-02 2.4e-06 1.01e+00 1.666376847e+02 1.666377743e+02 2.1e-11 9.61
39 3.1e-08 1.2e-02 2.2e-06 1.00e+00 1.666376909e+02 1.666377715e+02 1.9e-11 9.75
40 2.8e-08 1.1e-02 1.9e-06 9.86e-01 1.666376963e+02 1.666377689e+02 1.7e-11 9.92
41 2.5e-08 1.1e-02 1.8e-06 1.01e+00 1.666377015e+02 1.666377665e+02 1.5e-11 9.99
42 2.3e-08 1.1e-02 1.6e-06 9.82e-01 1.666377059e+02 1.666377645e+02 1.4e-11 10.01
43 2.1e-08 1.0e-02 1.4e-06 1.01e+00 1.666377101e+02 1.666377625e+02 1.2e-11 10.06
44 1.9e-08 1.0e-02 1.3e-06 1.03e+00 1.666377141e+02 1.666377606e+02 1.1e-11 10.07
45 1.7e-08 1.0e-02 1.1e-06 9.68e-01 1.666377172e+02 1.666377592e+02 1.0e-11 10.08
46 1.5e-08 9.8e-03 1.0e-06 9.86e-01 1.666377201e+02 1.666377579e+02 9.1e-12 10.10
47 1.4e-08 9.6e-03 9.3e-07 9.92e-01 1.666377227e+02 1.666377567e+02 8.2e-12 10.11
48 1.2e-08 9.5e-03 8.4e-07 1.01e+00 1.666377251e+02 1.666377555e+02 7.4e-12 10.12
49 1.1e-08 9.2e-03 7.5e-07 9.72e-01 1.666377271e+02 1.666377546e+02 6.7e-12 10.13
50 9.9e-09 8.3e-03 6.8e-07 1.04e+00 1.666377294e+02 1.666377535e+02 6.1e-12 10.15
51 8.9e-09 8.1e-03 6.1e-07 9.70e-01 1.666377310e+02 1.666377528e+02 5.5e-12 10.18
52 8.0e-09 8.1e-03 5.5e-07 9.73e-01 1.666377325e+02 1.666377521e+02 5.0e-12 10.20
53 7.2e-09 7.8e-03 4.9e-07 9.01e-01 1.666377338e+02 1.666377515e+02 4.5e-12 10.21
54 4.7e-09 4.7e-04 3.0e-08 8.68e-01 1.666377455e+02 1.666377467e+02 5.1e-13 10.23
Interior-point optimizer terminated. Time: 10.23.
Optimizer terminated. Time: 10.24
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6663774551e+02 Viol. con: 2e-07 var: 0e+00
Dual. obj: 1.6663774666e+02 Viol. con: 0e+00 var: 4e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 10.3 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
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.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 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 : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.286106771e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.264423007e+05 3.580365222e+00 4.8e-01 0.06
2 4.3e+02 5.5e+02 2.4e+04 -9.36e-01 -1.203332335e+05 1.010636288e+01 1.9e-01 0.08
3 2.9e+02 3.7e+02 1.6e+04 -8.40e-01 -1.156664730e+05 6.247792604e+01 1.3e-01 0.10
4 2.9e+02 3.7e+02 1.6e+04 -7.61e-01 -1.130152826e+05 2.295884618e+03 1.3e-01 0.11
5 7.3e+01 9.4e+01 4.1e+03 -7.54e-01 -7.379597028e+04 9.860992526e+03 3.2e-02 0.14
6 3.6e+01 4.6e+01 2.0e+03 -1.80e-01 -4.641910319e+04 1.009611434e+04 1.6e-02 0.15
7 2.1e+01 2.7e+01 1.2e+03 2.91e-01 -3.097469823e+04 6.886219939e+03 9.2e-03 0.18
8 1.2e+01 1.6e+01 6.8e+02 5.65e-01 -1.945488591e+04 4.491373678e+03 5.4e-03 0.19
9 4.7e+00 6.1e+00 2.6e+02 7.53e-01 -7.765154187e+03 2.180676492e+03 2.1e-03 0.20
10 2.3e+00 3.0e+00 1.3e+02 9.26e-01 -3.530372780e+03 1.395530077e+03 1.0e-03 0.22
11 1.5e+00 1.9e+00 8.5e+01 9.77e-01 -2.301318826e+03 9.721205230e+02 6.7e-04 0.25
12 8.5e-01 1.1e+00 4.8e+01 9.85e-01 -1.230530091e+03 6.224921019e+02 3.8e-04 0.26
13 7.5e-01 1.0e+00 4.2e+01 9.54e-01 -1.093831153e+03 5.630529286e+02 3.4e-04 0.28
14 3.7e-01 5.0e-01 2.1e+01 9.85e-01 -4.359009575e+02 3.737949774e+02 1.6e-04 0.29
15 1.8e-01 2.5e-01 1.0e+01 9.98e-01 -1.439999276e+02 2.585348621e+02 8.2e-05 0.31
16 8.9e-02 1.6e-01 5.1e+00 1.01e+00 4.980078878e+00 2.043015061e+02 4.1e-05 0.32
17 8.6e-02 1.5e-01 4.9e+00 1.01e+00 1.398829009e+01 2.065699109e+02 4.0e-05 0.33
18 6.1e-02 1.1e-01 3.5e+00 1.01e+00 5.949224722e+01 1.948373534e+02 2.8e-05 0.35
19 3.0e-02 7.3e-02 1.7e+00 1.01e+00 1.152797946e+02 1.809927777e+02 1.4e-05 0.37
20 8.5e-03 1.8e-01 4.9e-01 1.01e+00 1.525612320e+02 1.716192008e+02 4.0e-06 0.38
21 2.5e-03 1.8e-01 1.5e-01 1.00e+00 1.622330892e+02 1.679611454e+02 1.2e-06 0.40
22 1.5e-03 1.2e-01 9.0e-02 1.00e+00 1.639702593e+02 1.674409743e+02 7.3e-07 0.51
23 5.1e-04 1.0e-01 3.2e-02 1.01e+00 1.656550168e+02 1.668671106e+02 2.6e-07 0.52
24 2.0e-04 9.6e-02 1.2e-02 1.01e+00 1.661959789e+02 1.666660332e+02 1.0e-07 0.54
25 1.8e-04 8.7e-02 1.1e-02 1.01e+00 1.662326077e+02 1.666555351e+02 9.2e-08 0.55
26 1.6e-04 7.9e-02 1.0e-02 1.01e+00 1.662628626e+02 1.666433552e+02 8.3e-08 0.57
27 1.4e-04 7.2e-02 9.0e-03 1.01e+00 1.662902734e+02 1.666326040e+02 7.5e-08 0.58
28 1.3e-04 6.6e-02 8.1e-03 1.01e+00 1.663148172e+02 1.666228211e+02 6.7e-08 0.61
29 1.2e-04 6.0e-02 7.3e-03 1.01e+00 1.663368438e+02 1.666139702e+02 6.0e-08 0.63
30 1.0e-04 5.5e-02 6.5e-03 1.01e+00 1.663566055e+02 1.666059557e+02 5.4e-08 0.64
31 9.4e-05 5.0e-02 5.9e-03 1.01e+00 1.663743370e+02 1.665987003e+02 4.9e-08 0.65
32 8.5e-05 4.6e-02 5.3e-03 1.01e+00 1.663902477e+02 1.665921324e+02 4.4e-08 0.66
33 7.6e-05 4.2e-02 4.8e-03 1.01e+00 1.664045257e+02 1.665861875e+02 4.0e-08 0.68
34 6.9e-05 3.8e-02 4.3e-03 1.01e+00 1.664173397e+02 1.665808074e+02 3.6e-08 0.69
35 6.2e-05 3.5e-02 3.9e-03 1.01e+00 1.664288411e+02 1.665759394e+02 3.2e-08 0.72
36 5.5e-05 3.3e-02 3.5e-03 1.00e+00 1.664391654e+02 1.665715357e+02 2.9e-08 0.73
37 5.0e-05 3.0e-02 3.1e-03 1.00e+00 1.664484343e+02 1.665675529e+02 2.6e-08 0.75
38 4.5e-05 2.8e-02 2.8e-03 1.00e+00 1.664567564e+02 1.665639514e+02 2.3e-08 0.76
39 4.0e-05 2.6e-02 2.5e-03 1.00e+00 1.664642293e+02 1.665606955e+02 2.1e-08 0.77
40 3.6e-05 2.4e-02 2.3e-03 1.00e+00 1.664709403e+02 1.665577525e+02 1.9e-08 0.78
41 3.3e-05 2.2e-02 2.1e-03 1.00e+00 1.664769679e+02 1.665550929e+02 1.7e-08 0.82
42 2.9e-05 2.1e-02 1.9e-03 1.00e+00 1.664823821e+02 1.665526899e+02 1.5e-08 0.84
43 2.7e-05 2.0e-02 1.7e-03 1.00e+00 1.664872457e+02 1.665505192e+02 1.4e-08 0.85
44 2.4e-05 1.8e-02 1.5e-03 1.00e+00 1.664916154e+02 1.665485586e+02 1.2e-08 0.87
45 2.1e-05 1.7e-02 1.3e-03 1.00e+00 1.664955415e+02 1.665467882e+02 1.1e-08 0.88
46 1.9e-05 1.6e-02 1.2e-03 1.00e+00 1.664990696e+02 1.665451899e+02 1.0e-08 0.89
47 1.7e-05 1.6e-02 1.1e-03 1.00e+00 1.665022403e+02 1.665437472e+02 9.1e-09 0.91
48 1.6e-05 1.5e-02 9.8e-04 1.00e+00 1.665050900e+02 1.665424452e+02 8.2e-09 0.92
49 1.4e-05 1.4e-02 8.9e-04 1.00e+00 1.665076517e+02 1.665412706e+02 7.4e-09 0.96
50 1.3e-05 1.3e-02 8.0e-04 1.00e+00 1.665099546e+02 1.665402111e+02 6.6e-09 1.00
51 1.1e-05 1.3e-02 7.2e-04 1.00e+00 1.665120251e+02 1.665392556e+02 6.0e-09 1.05
52 1.0e-05 1.2e-02 6.5e-04 1.00e+00 1.665138869e+02 1.665383940e+02 5.4e-09 1.08
53 9.3e-06 1.2e-02 5.8e-04 1.00e+00 1.665155611e+02 1.665376174e+02 4.8e-09 1.14
54 8.3e-06 1.2e-02 5.2e-04 1.00e+00 1.665170668e+02 1.665369173e+02 4.4e-09 1.20
55 7.5e-06 1.1e-02 4.7e-04 1.00e+00 1.665184211e+02 1.665362864e+02 3.9e-09 1.24
56 6.7e-06 1.1e-02 4.2e-04 1.00e+00 1.665196391e+02 1.665357179e+02 3.5e-09 1.25
57 6.1e-06 1.1e-02 3.8e-04 1.00e+00 1.665207348e+02 1.665352057e+02 3.2e-09 1.27
58 5.5e-06 1.0e-02 3.4e-04 1.00e+00 1.665217203e+02 1.665347442e+02 2.9e-09 1.34
59 4.9e-06 1.0e-02 3.1e-04 1.00e+00 1.665226069e+02 1.665343284e+02 2.6e-09 1.36
60 4.4e-06 9.9e-03 2.8e-04 1.00e+00 1.665234043e+02 1.665339537e+02 2.3e-09 1.42
61 4.0e-06 9.7e-03 2.5e-04 1.00e+00 1.665241217e+02 1.665336162e+02 2.1e-09 1.49
62 3.6e-06 9.5e-03 2.3e-04 1.00e+00 1.665247669e+02 1.665333120e+02 1.9e-09 1.51
63 3.2e-06 9.4e-03 2.0e-04 1.00e+00 1.665253472e+02 1.665330379e+02 1.7e-09 1.53
64 2.9e-06 9.2e-03 1.8e-04 1.00e+00 1.665258692e+02 1.665327909e+02 1.5e-09 1.56
65 2.6e-06 9.1e-03 1.6e-04 1.00e+00 1.665263387e+02 1.665325683e+02 1.4e-09 1.60
66 2.4e-06 9.0e-03 1.5e-04 1.00e+00 1.665267610e+02 1.665323677e+02 1.2e-09 1.64
67 2.1e-06 8.9e-03 1.3e-04 1.00e+00 1.665271409e+02 1.665321869e+02 1.1e-09 1.68
68 1.9e-06 8.8e-03 1.2e-04 1.00e+00 1.665274827e+02 1.665320241e+02 1.0e-09 1.75
69 1.7e-06 8.7e-03 1.1e-04 1.00e+00 1.665277901e+02 1.665318775e+02 9.0e-10 1.77
70 1.5e-06 8.6e-03 9.7e-05 1.00e+00 1.665280667e+02 1.665317454e+02 8.1e-10 1.85
71 1.4e-06 8.6e-03 8.7e-05 1.00e+00 1.665283155e+02 1.665316264e+02 7.3e-10 1.88
72 1.3e-06 8.5e-03 7.9e-05 1.00e+00 1.665285394e+02 1.665315192e+02 6.5e-10 1.88
73 1.1e-06 8.5e-03 7.1e-05 1.00e+00 1.665287408e+02 1.665314226e+02 5.9e-10 1.90
74 1.0e-06 8.4e-03 6.4e-05 1.00e+00 1.665289219e+02 1.665313356e+02 5.3e-10 1.91
75 9.1e-07 8.4e-03 5.7e-05 1.00e+00 1.665290848e+02 1.665312572e+02 4.8e-10 1.93
76 8.2e-07 8.3e-03 5.2e-05 1.00e+00 1.665292314e+02 1.665311865e+02 4.3e-10 1.97
77 7.4e-07 8.3e-03 4.6e-05 1.00e+00 1.665293632e+02 1.665311228e+02 3.9e-10 2.00
78 6.6e-07 8.2e-03 4.2e-05 1.00e+00 1.665294818e+02 1.665310655e+02 3.5e-10 2.06
79 6.0e-07 8.2e-03 3.8e-05 1.00e+00 1.665295884e+02 1.665310137e+02 3.1e-10 2.11
80 5.4e-07 8.2e-03 3.4e-05 1.00e+00 1.665296843e+02 1.665309671e+02 2.8e-10 2.12
81 4.8e-07 8.1e-03 3.0e-05 1.00e+00 1.665297706e+02 1.665309250e+02 2.5e-10 2.16
82 4.4e-07 8.1e-03 2.7e-05 9.98e-01 1.665298481e+02 1.665308872e+02 2.3e-10 2.20
83 3.9e-07 8.1e-03 2.5e-05 9.99e-01 1.665299178e+02 1.665308531e+02 2.1e-10 2.23
84 3.5e-07 8.0e-03 2.2e-05 9.98e-01 1.665299805e+02 1.665308223e+02 1.8e-10 2.26
85 3.2e-07 8.0e-03 2.0e-05 1.00e+00 1.665300369e+02 1.665307945e+02 1.7e-10 2.28
86 2.9e-07 8.0e-03 1.8e-05 1.00e+00 1.665300877e+02 1.665307695e+02 1.5e-10 2.35
87 2.6e-07 8.0e-03 1.6e-05 9.99e-01 1.665301333e+02 1.665307469e+02 1.3e-10 2.38
88 2.3e-07 7.9e-03 1.5e-05 9.96e-01 1.665301743e+02 1.665307267e+02 1.2e-10 2.40
89 2.1e-07 7.9e-03 1.3e-05 1.00e+00 1.665302113e+02 1.665307084e+02 1.1e-10 2.41
90 1.9e-07 7.9e-03 1.2e-05 9.95e-01 1.665302445e+02 1.665306920e+02 9.8e-11 2.46
91 1.7e-07 7.9e-03 1.1e-05 1.00e+00 1.665302743e+02 1.665306771e+02 8.8e-11 2.49
92 1.5e-07 7.1e-03 9.6e-06 1.01e+00 1.665303014e+02 1.665306635e+02 8.0e-11 2.55
93 1.4e-07 6.4e-03 8.6e-06 9.97e-01 1.665303256e+02 1.665306515e+02 7.2e-11 2.57
94 1.2e-07 5.7e-03 7.7e-06 9.98e-01 1.665303473e+02 1.665306407e+02 6.5e-11 2.63
95 1.1e-07 5.2e-03 7.0e-06 1.00e+00 1.665303669e+02 1.665306309e+02 5.8e-11 2.67
96 1.0e-07 4.7e-03 6.3e-06 1.00e+00 1.665303845e+02 1.665306221e+02 5.2e-11 2.72
97 9.0e-08 4.2e-03 5.6e-06 1.01e+00 1.665304008e+02 1.665306139e+02 4.7e-11 2.74
98 8.1e-08 3.8e-03 5.1e-06 1.01e+00 1.665304154e+02 1.665306066e+02 4.3e-11 2.78
99 7.3e-08 3.4e-03 4.6e-06 9.99e-01 1.665304282e+02 1.665306002e+02 3.8e-11 2.83
100 6.5e-08 3.1e-03 4.1e-06 9.92e-01 1.665304396e+02 1.665305946e+02 3.4e-11 2.92
101 5.9e-08 2.7e-03 3.7e-06 9.90e-01 1.665304500e+02 1.665305894e+02 3.1e-11 2.95
102 5.3e-08 2.5e-03 3.3e-06 1.01e+00 1.665304595e+02 1.665305847e+02 2.8e-11 2.97
103 4.8e-08 2.2e-03 3.0e-06 1.00e+00 1.665304678e+02 1.665305805e+02 2.5e-11 2.98
104 4.3e-08 2.0e-03 2.7e-06 9.89e-01 1.665304753e+02 1.665305768e+02 2.3e-11 3.00
105 3.9e-08 1.8e-03 2.4e-06 9.84e-01 1.665304821e+02 1.665305734e+02 2.0e-11 3.03
106 3.5e-08 1.6e-03 2.2e-06 9.89e-01 1.665304881e+02 1.665305704e+02 1.8e-11 3.07
107 3.1e-08 1.5e-03 2.0e-06 9.88e-01 1.665304936e+02 1.665305677e+02 1.7e-11 3.10
108 2.8e-08 1.3e-03 1.8e-06 1.01e+00 1.665304988e+02 1.665305650e+02 1.5e-11 3.11
109 2.5e-08 1.2e-03 1.6e-06 9.83e-01 1.665305032e+02 1.665305629e+02 1.3e-11 3.12
110 2.3e-08 1.1e-03 1.4e-06 1.01e+00 1.665305073e+02 1.665305608e+02 1.2e-11 3.14
111 2.1e-08 9.6e-04 1.3e-06 9.75e-01 1.665305108e+02 1.665305591e+02 1.1e-11 3.15
112 1.8e-08 8.6e-04 1.2e-06 1.00e+00 1.665305141e+02 1.665305574e+02 9.9e-12 3.16
113 1.7e-08 7.8e-04 1.0e-06 9.97e-01 1.665305170e+02 1.665305560e+02 8.9e-12 3.18
114 1.5e-08 7.0e-04 9.4e-07 1.10e+00 1.665305207e+02 1.665305539e+02 8.4e-12 3.19
115 1.3e-08 6.3e-04 8.5e-07 1.04e+00 1.665305233e+02 1.665305526e+02 7.7e-12 3.24
116 1.2e-08 5.7e-04 7.6e-07 1.07e+00 1.665305259e+02 1.665305512e+02 7.2e-12 3.29
117 1.1e-08 5.1e-04 6.9e-07 9.76e-01 1.665305276e+02 1.665305504e+02 6.4e-12 3.32
118 9.9e-09 4.6e-04 6.2e-07 9.72e-01 1.665305291e+02 1.665305497e+02 5.8e-12 3.38
119 8.9e-09 4.1e-04 5.6e-07 1.01e+00 1.665305305e+02 1.665305490e+02 5.2e-12 3.44
120 8.0e-09 3.7e-04 5.0e-07 9.23e-01 1.665305318e+02 1.665305484e+02 4.7e-12 3.48
121 7.2e-09 3.3e-04 4.5e-07 9.98e-01 1.665305329e+02 1.665305479e+02 4.2e-12 3.49
122 6.5e-09 3.0e-04 4.1e-07 1.05e+00 1.665305341e+02 1.665305472e+02 3.9e-12 3.55
123 6.0e-09 2.7e-04 3.6e-07 1.11e+00 1.665305354e+02 1.665305465e+02 3.7e-12 3.62
124 5.4e-09 2.4e-04 3.3e-07 9.17e-01 1.665305362e+02 1.665305462e+02 3.3e-12 3.67
125 4.9e-09 2.2e-04 3.0e-07 1.05e+00 1.665305370e+02 1.665305458e+02 3.1e-12 3.71
126 4.6e-09 2.0e-04 2.7e-07 9.62e-01 1.665305376e+02 1.665305455e+02 2.8e-12 3.76
127 4.7e-09 1.8e-04 2.4e-07 1.18e+00 1.665305385e+02 1.665305450e+02 2.7e-12 3.84
128 4.7e-09 1.6e-04 2.2e-07 1.20e+00 1.665305394e+02 1.665305445e+02 2.7e-12 3.89
129 4.3e-09 1.4e-04 1.9e-07 1.04e+00 1.665305398e+02 1.665305443e+02 2.5e-12 3.91
130 2.4e-09 8.2e-06 1.1e-08 1.00e+00 1.665305427e+02 1.665305430e+02 1.4e-13 3.92
Interior-point optimizer terminated. Time: 3.92.
Optimizer terminated. Time: 3.93
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6653054272e+02 Viol. con: 4e-08 var: 0e+00
Dual. obj: 1.6653054298e+02 Viol. con: 0e+00 var: 3e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.96 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
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.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 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 : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.286069766e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.264280190e+05 3.575761773e+00 4.8e-01 0.06
2 4.3e+02 5.5e+02 2.4e+04 -9.36e-01 -1.202642600e+05 1.018055901e+01 1.9e-01 0.07
3 2.9e+02 3.7e+02 1.6e+04 -8.40e-01 -1.155864699e+05 6.348057000e+01 1.2e-01 0.09
4 2.8e+02 3.7e+02 1.6e+04 -7.60e-01 -1.129604570e+05 2.275516183e+03 1.2e-01 0.16
5 7.5e+01 9.6e+01 4.2e+03 -7.53e-01 -7.467569926e+04 9.661818848e+03 3.3e-02 0.17
6 3.3e+01 4.2e+01 1.8e+03 -1.93e-01 -4.344555550e+04 1.030574895e+04 1.4e-02 0.19
7 1.9e+01 2.5e+01 1.1e+03 3.43e-01 -2.866888252e+04 6.921959471e+03 8.5e-03 0.20
8 1.1e+01 1.5e+01 6.3e+02 6.05e-01 -1.820597939e+04 4.395204082e+03 5.0e-03 0.21
9 4.5e+00 5.8e+00 2.5e+02 7.73e-01 -7.371166904e+03 2.103309766e+03 2.0e-03 0.23
10 2.1e+00 2.7e+00 1.2e+02 9.30e-01 -3.214990468e+03 1.325823099e+03 9.3e-04 0.25
11 1.3e+00 1.7e+00 7.5e+01 9.81e-01 -2.014767646e+03 8.899276566e+02 6.0e-04 0.26
12 8.1e-01 1.0e+00 4.5e+01 9.84e-01 -1.165870649e+03 6.060224068e+02 3.6e-04 0.28
13 6.4e-01 8.5e-01 3.6e+01 9.55e-01 -9.120507046e+02 5.060745857e+02 2.9e-04 0.29
14 3.6e-01 4.9e-01 2.0e+01 9.93e-01 -4.191575491e+02 3.802511459e+02 1.6e-04 0.30
15 1.8e-01 2.4e-01 1.0e+01 9.93e-01 -1.346795984e+02 2.582567727e+02 8.0e-05 0.31
16 7.9e-02 1.4e-01 4.6e+00 1.01e+00 2.126792483e+01 1.996179868e+02 3.7e-05 0.33
17 6.8e-02 1.2e-01 3.9e+00 1.02e+00 4.474499175e+01 1.978720383e+02 3.2e-05 0.34
18 2.8e-02 7.4e-02 1.6e+00 1.02e+00 1.178045934e+02 1.806433001e+02 1.3e-05 0.35
19 8.1e-03 2.0e-01 4.7e-01 1.01e+00 1.531909913e+02 1.714402073e+02 3.8e-06 0.54
20 2.9e-03 2.3e-01 1.7e-01 1.00e+00 1.613911991e+02 1.680582047e+02 1.4e-06 0.83
21 1.7e-03 1.4e-01 1.0e-01 1.01e+00 1.635874230e+02 1.674597121e+02 8.2e-07 0.99
22 5.0e-04 1.2e-01 3.1e-02 1.01e+00 1.656228560e+02 1.668056681e+02 2.5e-07 1.23
23 1.9e-04 1.0e-01 1.2e-02 1.01e+00 1.661602583e+02 1.666050994e+02 9.7e-08 1.46
24 8.5e-05 8.7e-02 5.4e-03 1.01e+00 1.663313715e+02 1.665357285e+02 4.5e-08 1.54
25 3.9e-05 7.9e-02 2.5e-03 1.01e+00 1.664099188e+02 1.665032835e+02 2.1e-08 1.63
26 3.5e-05 7.2e-02 2.2e-03 1.01e+00 1.664180564e+02 1.665021090e+02 1.9e-08 1.67
27 3.1e-05 6.6e-02 2.0e-03 1.01e+00 1.664237676e+02 1.664993862e+02 1.7e-08 1.74
28 2.8e-05 6.0e-02 1.8e-03 1.01e+00 1.664290361e+02 1.664970782e+02 1.5e-08 1.75
29 2.5e-05 5.5e-02 1.6e-03 1.01e+00 1.664337498e+02 1.664949751e+02 1.4e-08 1.76
30 2.3e-05 5.0e-02 1.5e-03 1.01e+00 1.664379869e+02 1.664930794e+02 1.2e-08 1.78
31 2.1e-05 4.6e-02 1.3e-03 1.00e+00 1.664417927e+02 1.664913676e+02 1.1e-08 1.80
32 1.8e-05 4.2e-02 1.2e-03 1.00e+00 1.664452121e+02 1.664898226e+02 1.0e-08 1.89
33 1.7e-05 3.9e-02 1.1e-03 1.00e+00 1.664482844e+02 1.664884284e+02 9.0e-09 2.23
34 1.5e-05 3.6e-02 9.6e-04 1.00e+00 1.664510454e+02 1.664871705e+02 8.1e-09 2.49
35 1.3e-05 3.3e-02 8.6e-04 1.00e+00 1.664535268e+02 1.664860357e+02 7.3e-09 2.59
36 1.2e-05 3.0e-02 7.8e-04 1.00e+00 1.664557571e+02 1.664850122e+02 6.5e-09 2.72
37 1.1e-05 2.8e-02 7.0e-04 1.00e+00 1.664577620e+02 1.664840892e+02 5.9e-09 3.23
38 9.8e-06 2.6e-02 6.3e-04 1.00e+00 1.664595644e+02 1.664832570e+02 5.3e-09 3.53
39 8.8e-06 2.4e-02 5.7e-04 1.00e+00 1.664611850e+02 1.664825068e+02 4.8e-09 3.72
40 8.0e-06 2.3e-02 5.1e-04 1.00e+00 1.664626422e+02 1.664818306e+02 4.3e-09 4.07
41 7.2e-06 2.1e-02 4.6e-04 1.00e+00 1.664639526e+02 1.664812212e+02 3.9e-09 4.37
42 6.4e-06 2.0e-02 4.1e-04 1.00e+00 1.664651312e+02 1.664806721e+02 3.5e-09 4.60
43 5.8e-06 1.9e-02 3.7e-04 1.00e+00 1.664661912e+02 1.664801774e+02 3.1e-09 4.90
44 5.2e-06 1.7e-02 3.3e-04 1.00e+00 1.664671446e+02 1.664797317e+02 2.8e-09 5.48
45 4.7e-06 1.6e-02 3.0e-04 1.00e+00 1.664680022e+02 1.664793303e+02 2.5e-09 5.81
46 4.2e-06 1.6e-02 2.7e-04 1.00e+00 1.664687737e+02 1.664789687e+02 2.3e-09 6.15
47 3.8e-06 1.5e-02 2.4e-04 1.00e+00 1.664694676e+02 1.664786429e+02 2.1e-09 6.48
48 3.4e-06 1.4e-02 2.2e-04 1.00e+00 1.664700919e+02 1.664783495e+02 1.8e-09 6.83
49 3.1e-06 1.3e-02 2.0e-04 1.00e+00 1.664706535e+02 1.664780852e+02 1.7e-09 7.22
50 2.8e-06 1.3e-02 1.8e-04 1.00e+00 1.664711587e+02 1.664778472e+02 1.5e-09 7.63
51 2.5e-06 1.2e-02 1.6e-04 1.00e+00 1.664716133e+02 1.664776328e+02 1.3e-09 7.96
52 2.2e-06 1.2e-02 1.4e-04 1.00e+00 1.664720223e+02 1.664774398e+02 1.2e-09 8.19
53 2.0e-06 1.1e-02 1.3e-04 1.00e+00 1.664723903e+02 1.664772661e+02 1.1e-09 8.39
54 1.8e-06 1.1e-02 1.2e-04 1.00e+00 1.664727215e+02 1.664771097e+02 9.8e-10 8.53
55 1.6e-06 1.1e-02 1.0e-04 1.00e+00 1.664730196e+02 1.664769689e+02 8.8e-10 8.61
56 1.5e-06 1.0e-02 9.4e-05 1.00e+00 1.664732878e+02 1.664768422e+02 8.0e-10 8.69
57 1.3e-06 1.0e-02 8.5e-05 1.00e+00 1.664735292e+02 1.664767281e+02 7.2e-10 8.93
58 1.2e-06 9.9e-03 7.6e-05 1.00e+00 1.664737464e+02 1.664766254e+02 6.5e-10 9.22
59 1.1e-06 9.6e-03 6.9e-05 1.00e+00 1.664739419e+02 1.664765330e+02 5.8e-10 9.59
60 9.7e-07 9.4e-03 6.2e-05 1.00e+00 1.664741178e+02 1.664764498e+02 5.2e-10 10.09
61 8.7e-07 9.2e-03 5.6e-05 1.00e+00 1.664742761e+02 1.664763749e+02 4.7e-10 10.43
62 7.8e-07 9.1e-03 5.0e-05 1.00e+00 1.664744185e+02 1.664763074e+02 4.2e-10 10.78
63 7.1e-07 8.9e-03 4.5e-05 1.00e+00 1.664745467e+02 1.664762467e+02 3.8e-10 11.04
64 6.3e-07 8.8e-03 4.1e-05 1.00e+00 1.664746620e+02 1.664761920e+02 3.4e-10 11.33
65 5.7e-07 8.7e-03 3.7e-05 1.00e+00 1.664747658e+02 1.664761427e+02 3.1e-10 11.70
66 5.1e-07 8.6e-03 3.3e-05 1.00e+00 1.664748591e+02 1.664760984e+02 2.8e-10 12.21
67 4.6e-07 8.5e-03 3.0e-05 1.00e+00 1.664749431e+02 1.664760584e+02 2.5e-10 12.55
68 4.2e-07 8.4e-03 2.7e-05 1.00e+00 1.664750186e+02 1.664760224e+02 2.2e-10 12.91
69 3.7e-07 8.3e-03 2.4e-05 1.00e+00 1.664750865e+02 1.664759899e+02 2.0e-10 13.16
70 3.4e-07 8.2e-03 2.2e-05 1.00e+00 1.664751477e+02 1.664759606e+02 1.8e-10 13.39
71 3.0e-07 8.2e-03 1.9e-05 9.99e-01 1.664752026e+02 1.664759344e+02 1.6e-10 13.72
72 2.7e-07 8.1e-03 1.7e-05 1.00e+00 1.664752521e+02 1.664759106e+02 1.5e-10 14.02
73 2.5e-07 8.1e-03 1.6e-05 1.00e+00 1.664752966e+02 1.664758893e+02 1.3e-10 14.56
74 2.2e-07 8.0e-03 1.4e-05 9.98e-01 1.664753366e+02 1.664758701e+02 1.2e-10 14.99
75 2.0e-07 8.0e-03 1.3e-05 1.00e+00 1.664753726e+02 1.664758528e+02 1.1e-10 15.34
76 1.8e-07 7.9e-03 1.1e-05 1.00e+00 1.664754052e+02 1.664758370e+02 9.7e-11 15.59
77 1.6e-07 7.9e-03 1.0e-05 1.00e+00 1.664754343e+02 1.664758230e+02 8.7e-11 15.80
78 1.5e-07 7.8e-03 9.3e-06 9.97e-01 1.664754605e+02 1.664758104e+02 7.8e-11 15.98
79 1.3e-07 7.8e-03 8.4e-06 1.00e+00 1.664754842e+02 1.664757990e+02 7.1e-11 16.07
80 1.2e-07 7.8e-03 7.5e-06 9.99e-01 1.664755054e+02 1.664757888e+02 6.4e-11 16.39
81 1.1e-07 7.8e-03 6.8e-06 1.00e+00 1.664755246e+02 1.664757795e+02 5.7e-11 16.94
82 9.5e-08 7.7e-03 6.1e-06 9.95e-01 1.664755418e+02 1.664757713e+02 5.2e-11 17.27
83 8.6e-08 7.7e-03 5.5e-06 1.00e+00 1.664755573e+02 1.664757638e+02 4.6e-11 17.67
84 7.7e-08 7.7e-03 4.9e-06 1.00e+00 1.664755712e+02 1.664757570e+02 4.2e-11 18.12
85 6.9e-08 7.7e-03 4.4e-06 9.95e-01 1.664755837e+02 1.664757510e+02 3.8e-11 18.52
86 6.2e-08 7.6e-03 4.0e-06 9.98e-01 1.664755950e+02 1.664757456e+02 3.4e-11 18.82
87 5.6e-08 7.6e-03 3.6e-06 1.00e+00 1.664756052e+02 1.664757406e+02 3.0e-11 19.22
88 5.1e-08 7.6e-03 3.2e-06 1.00e+00 1.664756143e+02 1.664757362e+02 2.7e-11 19.51
89 4.6e-08 7.6e-03 2.9e-06 1.00e+00 1.664756225e+02 1.664757322e+02 2.5e-11 19.97
90 4.1e-08 6.8e-03 2.6e-06 1.00e+00 1.664756300e+02 1.664757286e+02 2.2e-11 20.30
91 3.7e-08 6.1e-03 2.4e-06 9.94e-01 1.664756367e+02 1.664757254e+02 2.0e-11 20.73
92 3.3e-08 5.5e-03 2.1e-06 1.00e+00 1.664756426e+02 1.664757225e+02 1.8e-11 21.37
93 3.0e-08 5.0e-03 1.9e-06 9.95e-01 1.664756480e+02 1.664757199e+02 1.6e-11 21.73
94 2.7e-08 4.5e-03 1.7e-06 1.00e+00 1.664756529e+02 1.664757176e+02 1.5e-11 22.05
95 2.4e-08 4.0e-03 1.6e-06 1.01e+00 1.664756575e+02 1.664757153e+02 1.3e-11 22.41
96 2.2e-08 3.6e-03 1.4e-06 1.00e+00 1.664756614e+02 1.664757134e+02 1.2e-11 22.94
97 2.0e-08 3.3e-03 1.3e-06 1.02e+00 1.664756651e+02 1.664757116e+02 1.1e-11 23.59
98 1.8e-08 2.9e-03 1.1e-06 9.96e-01 1.664756683e+02 1.664757101e+02 9.7e-12 24.02
99 1.6e-08 2.6e-03 1.0e-06 1.02e+00 1.664756713e+02 1.664757086e+02 8.8e-12 24.47
100 1.4e-08 2.4e-03 9.2e-07 1.03e+00 1.664756742e+02 1.664757072e+02 8.0e-12 24.90
101 1.3e-08 2.1e-03 8.2e-07 9.72e-01 1.664756764e+02 1.664757061e+02 7.2e-12 25.37
102 1.2e-08 1.9e-03 7.4e-07 1.06e+00 1.664756789e+02 1.664757049e+02 6.7e-12 25.94
103 1.0e-08 1.7e-03 6.7e-07 1.01e+00 1.664756808e+02 1.664757040e+02 6.1e-12 26.38
104 9.4e-09 1.6e-03 6.0e-07 9.87e-01 1.664756823e+02 1.664757032e+02 5.5e-12 26.81
105 2.2e-09 1.6e-04 6.2e-08 9.90e-01 1.664756950e+02 1.664756972e+02 5.8e-13 27.13
Interior-point optimizer terminated. Time: 27.14.
Optimizer terminated. Time: 27.15
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6647569505e+02 Viol. con: 4e-08 var: 0e+00
Dual. obj: 1.6647569720e+02 Viol. con: 0e+00 var: 1e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 27.2 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.02
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3439 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 : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.285358117e+05 2.000000000e+00 1.0e+00 0.05
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.263542085e+05 3.574445468e+00 4.8e-01 0.06
2 4.3e+02 5.5e+02 2.4e+04 -9.36e-01 -1.201588472e+05 1.021567231e+01 1.9e-01 0.07
3 2.9e+02 3.7e+02 1.6e+04 -8.39e-01 -1.154718917e+05 6.399968046e+01 1.2e-01 0.09
4 2.8e+02 3.7e+02 1.6e+04 -7.59e-01 -1.128613765e+05 2.263785696e+03 1.2e-01 0.10
5 7.5e+01 9.7e+01 4.2e+03 -7.52e-01 -7.480743550e+04 9.600131301e+03 3.3e-02 0.12
6 3.0e+01 3.9e+01 1.7e+03 -1.96e-01 -4.068261743e+04 1.026881490e+04 1.3e-02 0.13
7 1.8e+01 2.3e+01 1.0e+03 3.91e-01 -2.712655858e+04 6.680853695e+03 7.9e-03 0.14
8 9.7e+00 1.2e+01 5.4e+02 6.31e-01 -1.569361656e+04 3.889214983e+03 4.3e-03 0.15
9 3.9e+00 5.0e+00 2.2e+02 8.12e-01 -6.429968337e+03 1.893873530e+03 1.7e-03 0.17
10 2.1e+00 2.7e+00 1.2e+02 9.41e-01 -3.286676875e+03 1.204165331e+03 9.2e-04 0.18
11 1.0e+00 1.3e+00 5.9e+01 9.80e-01 -1.544941282e+03 7.355115621e+02 4.7e-04 0.23
12 8.1e-01 1.0e+00 4.5e+01 9.78e-01 -1.184101277e+03 6.013207806e+02 3.6e-04 0.24
13 4.8e-01 6.2e-01 2.7e+01 9.74e-01 -6.380956895e+02 4.207594054e+02 2.1e-04 0.51
14 2.6e-01 3.6e-01 1.5e+01 1.00e+00 -2.718762467e+02 3.084915877e+02 1.2e-04 0.67
15 9.7e-02 1.5e-01 5.5e+00 1.00e+00 -1.010192524e+01 2.072399472e+02 4.5e-05 0.69
16 8.6e-02 1.3e-01 4.9e+00 1.02e+00 1.582480471e+01 2.085964057e+02 4.0e-05 0.71
17 5.3e-02 8.8e-02 3.1e+00 1.02e+00 7.252853999e+01 1.918878922e+02 2.5e-05 0.72
18 2.3e-02 6.9e-02 1.3e+00 1.02e+00 1.266655683e+02 1.778066257e+02 1.1e-05 0.73
19 6.2e-03 2.3e-01 3.7e-01 1.01e+00 1.562529231e+02 1.702799638e+02 2.9e-06 0.75
20 3.1e-03 3.1e-01 1.8e-01 1.00e+00 1.610359052e+02 1.681101297e+02 1.5e-06 0.76
21 1.6e-03 1.7e-01 9.8e-02 1.01e+00 1.636142750e+02 1.673814360e+02 8.0e-07 0.77
22 4.9e-04 1.4e-01 3.0e-02 1.01e+00 1.656242398e+02 1.667725437e+02 2.5e-07 0.78
23 3.1e-04 1.1e-01 1.9e-02 9.98e-01 1.659258400e+02 1.666521482e+02 1.6e-07 0.80
24 1.9e-04 7.7e-02 1.2e-02 9.85e-01 1.661267131e+02 1.665737826e+02 9.7e-08 0.81
25 1.7e-04 6.6e-02 1.0e-02 9.99e-01 1.661696325e+02 1.665612833e+02 8.5e-08 0.82
26 1.5e-04 6.0e-02 9.3e-03 1.01e+00 1.661982519e+02 1.665504953e+02 7.7e-08 0.83
27 1.3e-04 5.5e-02 8.4e-03 1.01e+00 1.662230712e+02 1.665399625e+02 6.9e-08 0.85
28 1.2e-04 5.0e-02 7.5e-03 1.01e+00 1.662455484e+02 1.665306826e+02 6.2e-08 0.86
29 1.1e-04 4.6e-02 6.8e-03 1.01e+00 1.662656857e+02 1.665222505e+02 5.6e-08 0.87
30 9.8e-05 4.2e-02 6.1e-03 1.01e+00 1.662837605e+02 1.665146234e+02 5.1e-08 0.89
31 8.8e-05 3.8e-02 5.5e-03 1.01e+00 1.662999797e+02 1.665077195e+02 4.5e-08 0.90
32 7.9e-05 3.5e-02 4.9e-03 1.01e+00 1.663145356e+02 1.665014716e+02 4.1e-08 0.91
33 7.1e-05 3.3e-02 4.4e-03 1.00e+00 1.663275992e+02 1.664958177e+02 3.7e-08 0.93
34 6.4e-05 3.0e-02 4.0e-03 1.00e+00 1.663393246e+02 1.664907020e+02 3.3e-08 0.94
35 5.8e-05 2.8e-02 3.6e-03 1.00e+00 1.663498497e+02 1.664860740e+02 3.0e-08 0.96
36 5.2e-05 2.6e-02 3.2e-03 1.00e+00 1.663592984e+02 1.664818880e+02 2.7e-08 0.97
37 4.7e-05 2.4e-02 2.9e-03 1.00e+00 1.663677816e+02 1.664781026e+02 2.4e-08 0.98
38 4.2e-05 2.2e-02 2.6e-03 1.00e+00 1.663753989e+02 1.664746801e+02 2.2e-08 1.00
39 3.8e-05 2.1e-02 2.4e-03 1.00e+00 1.663822394e+02 1.664715863e+02 2.0e-08 1.01
40 3.4e-05 1.9e-02 2.1e-03 1.00e+00 1.663883828e+02 1.664687903e+02 1.8e-08 1.02
41 3.1e-05 1.8e-02 1.9e-03 1.00e+00 1.663939007e+02 1.664662637e+02 1.6e-08 1.04
42 2.8e-05 1.7e-02 1.7e-03 1.00e+00 1.663988572e+02 1.664639809e+02 1.4e-08 1.05
43 2.5e-05 1.6e-02 1.6e-03 1.00e+00 1.664033097e+02 1.664619188e+02 1.3e-08 1.06
44 2.2e-05 1.5e-02 1.4e-03 1.00e+00 1.664073098e+02 1.664600563e+02 1.2e-08 1.07
45 2.0e-05 1.5e-02 1.3e-03 1.00e+00 1.664109036e+02 1.664583741e+02 1.0e-08 1.09
46 1.8e-05 1.4e-02 1.1e-03 1.00e+00 1.664141327e+02 1.664568551e+02 9.4e-09 1.10
47 1.6e-05 1.3e-02 1.0e-03 1.00e+00 1.664170342e+02 1.664554836e+02 8.4e-09 1.11
48 1.5e-05 1.3e-02 9.2e-04 1.00e+00 1.664196415e+02 1.664542454e+02 7.6e-09 1.13
49 1.3e-05 1.2e-02 8.2e-04 1.00e+00 1.664219846e+02 1.664531277e+02 6.8e-09 1.14
50 1.2e-05 1.2e-02 7.4e-04 1.00e+00 1.664240905e+02 1.664521190e+02 6.2e-09 1.15
51 1.1e-05 1.1e-02 6.7e-04 1.00e+00 1.664259832e+02 1.664512087e+02 5.5e-09 1.16
52 9.6e-06 1.1e-02 6.0e-04 1.00e+00 1.664276845e+02 1.664503874e+02 5.0e-09 1.18
53 8.6e-06 1.1e-02 5.4e-04 1.00e+00 1.664292138e+02 1.664496464e+02 4.5e-09 1.19
54 7.8e-06 1.0e-02 4.9e-04 1.00e+00 1.664305887e+02 1.664489780e+02 4.0e-09 1.21
55 7.0e-06 1.0e-02 4.4e-04 1.00e+00 1.664318247e+02 1.664483751e+02 3.6e-09 1.22
56 6.3e-06 9.9e-03 3.9e-04 1.00e+00 1.664329360e+02 1.664478314e+02 3.3e-09 1.24
57 5.7e-06 9.7e-03 3.5e-04 1.00e+00 1.664339352e+02 1.664473412e+02 2.9e-09 1.25
58 5.1e-06 9.6e-03 3.2e-04 1.00e+00 1.664348337e+02 1.664468991e+02 2.7e-09 1.26
59 4.6e-06 9.4e-03 2.9e-04 1.00e+00 1.664356416e+02 1.664465005e+02 2.4e-09 1.28
60 4.1e-06 9.2e-03 2.6e-04 1.00e+00 1.664363681e+02 1.664461412e+02 2.1e-09 1.29
61 3.7e-06 9.1e-03 2.3e-04 1.00e+00 1.664370213e+02 1.664458172e+02 1.9e-09 1.30
62 3.3e-06 9.0e-03 2.1e-04 1.00e+00 1.664376088e+02 1.664455251e+02 1.7e-09 1.32
63 3.0e-06 8.9e-03 1.9e-04 1.00e+00 1.664381370e+02 1.664452618e+02 1.6e-09 1.33
64 2.7e-06 8.7e-03 1.7e-04 1.00e+00 1.664386121e+02 1.664450245e+02 1.4e-09 1.35
65 2.4e-06 8.7e-03 1.5e-04 1.00e+00 1.664390394e+02 1.664448106e+02 1.3e-09 1.36
66 2.2e-06 8.6e-03 1.4e-04 1.00e+00 1.664394237e+02 1.664446179e+02 1.1e-09 1.37
67 2.0e-06 8.5e-03 1.2e-04 1.00e+00 1.664397695e+02 1.664444443e+02 1.0e-09 1.39
68 1.8e-06 8.4e-03 1.1e-04 1.00e+00 1.664400806e+02 1.664442879e+02 9.3e-10 1.40
69 1.6e-06 8.3e-03 1.0e-04 1.00e+00 1.664403604e+02 1.664441471e+02 8.3e-10 1.42
70 1.4e-06 8.3e-03 9.0e-05 1.00e+00 1.664406121e+02 1.664440202e+02 7.5e-10 1.43
71 1.3e-06 8.2e-03 8.1e-05 1.00e+00 1.664408386e+02 1.664439059e+02 6.7e-10 1.44
72 1.2e-06 8.2e-03 7.3e-05 1.00e+00 1.664410424e+02 1.664438030e+02 6.1e-10 1.46
73 1.1e-06 8.1e-03 6.6e-05 1.00e+00 1.664412257e+02 1.664437103e+02 5.5e-10 1.47
74 9.5e-07 8.1e-03 5.9e-05 1.00e+00 1.664413906e+02 1.664436268e+02 4.9e-10 1.48
75 8.5e-07 8.0e-03 5.3e-05 1.00e+00 1.664415390e+02 1.664435515e+02 4.4e-10 1.50
76 7.7e-07 8.0e-03 4.8e-05 1.00e+00 1.664416725e+02 1.664434838e+02 4.0e-10 1.51
77 6.9e-07 7.9e-03 4.3e-05 1.00e+00 1.664417926e+02 1.664434227e+02 3.6e-10 1.52
78 6.2e-07 7.9e-03 3.9e-05 1.00e+00 1.664419007e+02 1.664433677e+02 3.2e-10 1.54
79 5.6e-07 7.9e-03 3.5e-05 1.00e+00 1.664419978e+02 1.664433182e+02 2.9e-10 1.55
80 5.0e-07 7.8e-03 3.1e-05 1.00e+00 1.664420853e+02 1.664432736e+02 2.6e-10 1.56
81 4.5e-07 7.8e-03 2.8e-05 1.00e+00 1.664421639e+02 1.664432333e+02 2.4e-10 1.57
82 4.1e-07 7.8e-03 2.5e-05 1.00e+00 1.664422347e+02 1.664431972e+02 2.1e-10 1.76
83 3.7e-07 7.8e-03 2.3e-05 1.00e+00 1.664422983e+02 1.664431646e+02 1.9e-10 1.88
84 3.3e-07 7.7e-03 2.1e-05 1.00e+00 1.664423556e+02 1.664431352e+02 1.7e-10 1.97
85 3.0e-07 7.7e-03 1.9e-05 9.99e-01 1.664424071e+02 1.664431088e+02 1.5e-10 2.05
86 2.7e-07 7.7e-03 1.7e-05 1.00e+00 1.664424535e+02 1.664430850e+02 1.4e-10 2.06
87 2.4e-07 7.7e-03 1.5e-05 1.00e+00 1.664424952e+02 1.664430636e+02 1.3e-10 2.07
88 2.2e-07 7.7e-03 1.4e-05 1.00e+00 1.664425328e+02 1.664430443e+02 1.1e-10 2.09
89 1.9e-07 7.6e-03 1.2e-05 1.00e+00 1.664425666e+02 1.664430269e+02 1.0e-10 2.10
90 1.8e-07 7.6e-03 1.1e-05 1.00e+00 1.664425970e+02 1.664430113e+02 9.1e-11 2.11
91 1.6e-07 7.6e-03 9.9e-06 1.00e+00 1.664426244e+02 1.664429972e+02 8.2e-11 2.13
92 1.4e-07 7.6e-03 8.9e-06 1.00e+00 1.664426490e+02 1.664429846e+02 7.4e-11 2.14
93 1.3e-07 7.6e-03 8.0e-06 1.00e+00 1.664426712e+02 1.664429732e+02 6.6e-11 2.15
94 1.2e-07 7.6e-03 7.2e-06 9.97e-01 1.664426912e+02 1.664429630e+02 6.0e-11 2.17
95 1.0e-07 6.8e-03 6.5e-06 1.00e+00 1.664427092e+02 1.664429537e+02 5.4e-11 2.18
96 9.3e-08 6.1e-03 5.8e-06 9.98e-01 1.664427253e+02 1.664429454e+02 4.8e-11 2.19
97 8.4e-08 5.5e-03 5.2e-06 9.97e-01 1.664427399e+02 1.664429380e+02 4.4e-11 2.20
98 7.5e-08 5.0e-03 4.7e-06 9.91e-01 1.664427529e+02 1.664429313e+02 3.9e-11 2.22
99 6.8e-08 4.5e-03 4.3e-06 1.00e+00 1.664427647e+02 1.664429253e+02 3.5e-11 2.23
100 6.1e-08 4.0e-03 3.8e-06 1.00e+00 1.664427754e+02 1.664429198e+02 3.2e-11 2.25
101 5.5e-08 3.6e-03 3.4e-06 1.00e+00 1.664427850e+02 1.664429149e+02 2.9e-11 2.26
102 5.0e-08 3.3e-03 3.1e-06 1.00e+00 1.664427935e+02 1.664429104e+02 2.6e-11 2.27
103 4.5e-08 2.9e-03 2.8e-06 9.99e-01 1.664428013e+02 1.664429065e+02 2.3e-11 2.28
104 4.0e-08 2.6e-03 2.5e-06 9.87e-01 1.664428082e+02 1.664429030e+02 2.1e-11 2.30
105 3.6e-08 2.4e-03 2.3e-06 1.01e+00 1.664428147e+02 1.664428996e+02 1.9e-11 2.31
106 3.2e-08 2.1e-03 2.0e-06 9.95e-01 1.664428203e+02 1.664428967e+02 1.7e-11 2.32
107 2.9e-08 1.9e-03 1.8e-06 9.96e-01 1.664428254e+02 1.664428942e+02 1.5e-11 2.34
108 2.6e-08 1.7e-03 1.6e-06 1.00e+00 1.664428299e+02 1.664428918e+02 1.4e-11 2.35
109 2.4e-08 1.6e-03 1.5e-06 1.01e+00 1.664428341e+02 1.664428897e+02 1.2e-11 2.36
110 2.1e-08 1.4e-03 1.3e-06 1.00e+00 1.664428378e+02 1.664428878e+02 1.1e-11 2.37
111 1.9e-08 1.3e-03 1.2e-06 9.43e-01 1.664428411e+02 1.664428861e+02 1.0e-11 2.38
112 1.7e-08 1.1e-03 1.1e-06 1.04e+00 1.664428446e+02 1.664428842e+02 9.2e-12 2.40
113 1.6e-08 1.0e-03 9.7e-07 1.08e+00 1.664428481e+02 1.664428823e+02 8.6e-12 2.41
114 1.4e-08 9.2e-04 8.8e-07 1.02e+00 1.664428505e+02 1.664428811e+02 7.8e-12 2.42
115 1.3e-08 8.3e-04 7.9e-07 1.08e+00 1.664428533e+02 1.664428796e+02 7.3e-12 2.43
116 1.2e-08 7.5e-04 7.1e-07 8.82e-01 1.664428550e+02 1.664428787e+02 6.5e-12 2.45
117 1.1e-08 6.7e-04 6.4e-07 8.80e-01 1.664428566e+02 1.664428780e+02 5.9e-12 2.46
118 9.4e-09 6.0e-04 5.7e-07 9.29e-01 1.664428580e+02 1.664428774e+02 5.3e-12 2.47
119 8.5e-09 5.4e-04 5.2e-07 9.19e-01 1.664428593e+02 1.664428767e+02 4.8e-12 2.49
120 8.1e-09 4.9e-04 4.7e-07 1.04e+00 1.664428606e+02 1.664428760e+02 4.4e-12 2.50
121 7.5e-09 4.4e-04 4.2e-07 1.02e+00 1.664428617e+02 1.664428755e+02 4.0e-12 2.51
122 1.0e-08 4.0e-04 3.8e-07 1.20e+00 1.664428635e+02 1.664428743e+02 3.9e-12 2.52
123 1.0e-08 3.6e-04 3.4e-07 7.44e-01 1.664428643e+02 1.664428739e+02 3.5e-12 2.53
124 1.5e-08 3.2e-04 3.1e-07 1.19e+00 1.664428654e+02 1.664428731e+02 3.5e-12 2.55
125 1.7e-08 2.9e-04 2.8e-07 4.86e-01 1.664428661e+02 1.664428726e+02 3.1e-12 2.56
126 1.6e-08 2.6e-04 2.5e-07 1.29e+00 1.664428666e+02 1.664428724e+02 2.8e-12 2.57
127 1.3e-08 2.4e-04 2.3e-07 3.99e-01 1.664428670e+02 1.664428724e+02 2.5e-12 2.58
128 1.7e-08 2.1e-04 2.6e-07 1.00e+00 1.664428659e+02 1.664428722e+02 2.3e-12 2.59
129 1.8e-08 1.9e-04 2.4e-07 3.30e+00 1.664428658e+02 1.664428727e+02 2.0e-12 2.61
130 1.6e-08 1.7e-04 2.1e-07 7.03e-01 1.664428662e+02 1.664428726e+02 1.8e-12 2.62
131 1.4e-08 1.6e-04 1.9e-07 1.56e+00 1.664428666e+02 1.664428724e+02 1.6e-12 2.63
132 1.2e-08 1.4e-04 1.7e-07 1.67e+00 1.664428671e+02 1.664428722e+02 1.5e-12 2.65
133 1.3e-08 1.3e-04 1.9e-07 1.00e+00 1.664428666e+02 1.664428720e+02 1.3e-12 2.66
134 1.2e-08 1.1e-04 1.7e-07 7.76e-01 1.664428671e+02 1.664428719e+02 1.2e-12 2.68
135 1.1e-08 1.0e-04 1.5e-07 5.25e-01 1.664428674e+02 1.664428718e+02 1.1e-12 2.69
136 1.2e-08 9.2e-05 1.4e-07 9.92e-01 1.664428678e+02 1.664428717e+02 9.6e-13 2.70
Interior-point optimizer terminated. Time: 2.70.
Optimizer terminated. Time: 2.71
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6644286777e+02 Viol. con: 3e-07 var: 0e+00
Dual. obj: 1.6644287173e+02 Viol. con: 0e+00 var: 5e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.74 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
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.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3439 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 : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.285340957e+05 2.000000000e+00 1.0e+00 0.05
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.263517283e+05 3.573621329e+00 4.8e-01 0.06
2 4.3e+02 5.5e+02 2.4e+04 -9.36e-01 -1.201360090e+05 1.023272656e+01 1.8e-01 0.08
3 2.9e+02 3.7e+02 1.6e+04 -8.39e-01 -1.154380586e+05 6.426640353e+01 1.2e-01 0.09
4 2.8e+02 3.6e+02 1.6e+04 -7.59e-01 -1.128348628e+05 2.258318868e+03 1.2e-01 0.11
5 7.5e+01 9.6e+01 4.1e+03 -7.52e-01 -7.471880335e+04 9.598257258e+03 3.3e-02 0.12
6 3.0e+01 3.9e+01 1.7e+03 -1.95e-01 -4.050837111e+04 1.020869836e+04 1.3e-02 0.13
7 1.8e+01 2.3e+01 1.0e+03 3.94e-01 -2.711076981e+04 6.648787000e+03 7.9e-03 0.15
8 9.5e+00 1.2e+01 5.3e+02 6.30e-01 -1.542139758e+04 3.834874078e+03 4.2e-03 0.16
9 3.6e+00 4.7e+00 2.0e+02 8.16e-01 -5.933715770e+03 1.798172324e+03 1.6e-03 0.17
10 2.0e+00 2.6e+00 1.1e+02 9.47e-01 -3.130705089e+03 1.194463503e+03 8.9e-04 0.19
11 8.4e-01 1.1e+00 4.7e+01 9.81e-01 -1.229432961e+03 6.158762901e+02 3.8e-04 0.20
12 8.2e-01 1.1e+00 4.6e+01 9.50e-01 -1.213196380e+03 5.912535389e+02 3.7e-04 0.22
13 5.1e-01 6.6e-01 2.9e+01 9.72e-01 -7.067517247e+02 4.266802042e+02 2.3e-04 0.23
14 3.1e-01 4.2e-01 1.8e+01 1.00e+00 -3.527408526e+02 3.411005417e+02 1.4e-04 0.24
15 1.1e-01 1.7e-01 6.1e+00 9.98e-01 -2.763122075e+01 2.143698841e+02 5.0e-05 0.26
16 8.2e-02 1.3e-01 4.7e+00 1.02e+00 2.135848180e+01 2.045405480e+02 3.8e-05 0.27
17 4.1e-02 8.3e-02 2.4e+00 1.02e+00 9.501475880e+01 1.868885776e+02 1.9e-05 0.29
18 1.4e-02 8.3e-02 8.2e-01 1.02e+00 1.425019024e+02 1.741744387e+02 6.6e-06 0.30
19 6.2e-03 7.2e-02 3.6e-01 1.01e+00 1.557125030e+02 1.695765297e+02 2.9e-06 0.31
20 1.5e-03 1.6e-01 9.2e-02 1.01e+00 1.638758801e+02 1.673863259e+02 7.4e-07 0.33
21 8.0e-04 1.1e-01 4.9e-02 9.78e-01 1.650620557e+02 1.669373602e+02 4.0e-07 0.34
22 2.4e-04 1.1e-01 1.6e-02 9.90e-01 1.660031289e+02 1.665978524e+02 1.3e-07 0.35
23 1.1e-04 8.9e-02 7.5e-03 1.01e+00 1.662212758e+02 1.665057616e+02 6.3e-08 0.37
24 4.7e-05 8.5e-02 3.1e-03 1.01e+00 1.663394239e+02 1.664571338e+02 2.6e-08 0.38
25 2.2e-05 7.7e-02 1.5e-03 1.01e+00 1.663835790e+02 1.664385513e+02 1.2e-08 0.40
26 2.0e-05 7.1e-02 1.3e-03 1.00e+00 1.663881973e+02 1.664377015e+02 1.1e-08 0.41
27 1.8e-05 6.4e-02 1.2e-03 1.01e+00 1.663915598e+02 1.664361006e+02 1.0e-08 0.43
28 1.6e-05 5.9e-02 1.1e-03 1.00e+00 1.663946472e+02 1.664347271e+02 9.0e-09 0.44
29 1.4e-05 5.4e-02 9.6e-04 1.00e+00 1.663974102e+02 1.664334758e+02 8.1e-09 0.45
30 1.3e-05 4.9e-02 8.6e-04 1.00e+00 1.663998948e+02 1.664323489e+02 7.3e-09 0.47
31 1.2e-05 4.5e-02 7.7e-04 1.00e+00 1.664021273e+02 1.664313320e+02 6.5e-09 0.48
32 1.0e-05 4.1e-02 7.0e-04 1.00e+00 1.664041338e+02 1.664304146e+02 5.9e-09 0.49
33 9.4e-06 3.8e-02 6.3e-04 1.00e+00 1.664059371e+02 1.664295872e+02 5.3e-09 0.50
34 8.5e-06 3.5e-02 5.6e-04 1.00e+00 1.664075581e+02 1.664288411e+02 4.8e-09 0.52
35 7.7e-06 3.2e-02 5.1e-04 1.00e+00 1.664090153e+02 1.664281682e+02 4.3e-09 0.53
36 6.9e-06 3.0e-02 4.6e-04 1.00e+00 1.664103253e+02 1.664275615e+02 3.9e-09 0.54
37 6.2e-06 2.8e-02 4.1e-04 1.00e+00 1.664115031e+02 1.664270145e+02 3.5e-09 0.56
38 5.6e-06 2.6e-02 3.7e-04 1.00e+00 1.664125621e+02 1.664265215e+02 3.1e-09 0.57
39 5.0e-06 2.4e-02 3.3e-04 1.00e+00 1.664135144e+02 1.664260771e+02 2.8e-09 0.58
40 4.5e-06 2.2e-02 3.0e-04 1.00e+00 1.664143706e+02 1.664256765e+02 2.5e-09 0.60
41 4.1e-06 2.1e-02 2.7e-04 1.00e+00 1.664151406e+02 1.664253155e+02 2.3e-09 0.61
42 3.7e-06 2.0e-02 2.4e-04 1.00e+00 1.664158330e+02 1.664249900e+02 2.1e-09 0.62
43 3.3e-06 1.8e-02 2.2e-04 1.00e+00 1.664164557e+02 1.664246967e+02 1.8e-09 0.64
44 3.0e-06 1.7e-02 2.0e-04 1.00e+00 1.664170157e+02 1.664244324e+02 1.7e-09 0.66
45 2.7e-06 1.6e-02 1.8e-04 1.00e+00 1.664175193e+02 1.664241941e+02 1.5e-09 0.68
46 2.4e-06 1.5e-02 1.6e-04 1.00e+00 1.664179722e+02 1.664239795e+02 1.3e-09 0.69
47 2.2e-06 1.5e-02 1.4e-04 1.00e+00 1.664183797e+02 1.664237861e+02 1.2e-09 0.71
48 1.9e-06 1.4e-02 1.3e-04 1.00e+00 1.664187463e+02 1.664236119e+02 1.1e-09 0.72
49 1.8e-06 1.3e-02 1.2e-04 1.00e+00 1.664190761e+02 1.664234550e+02 9.8e-10 0.73
50 1.6e-06 1.3e-02 1.0e-04 1.00e+00 1.664193728e+02 1.664233138e+02 8.8e-10 0.75
51 1.4e-06 1.2e-02 9.4e-05 1.00e+00 1.664196397e+02 1.664231866e+02 8.0e-10 0.76
52 1.3e-06 1.2e-02 8.5e-05 1.00e+00 1.664198799e+02 1.664230721e+02 7.2e-10 0.78
53 1.1e-06 1.1e-02 7.6e-05 1.00e+00 1.664200959e+02 1.664229689e+02 6.4e-10 0.79
54 1.0e-06 1.1e-02 6.9e-05 1.00e+00 1.664202903e+02 1.664228759e+02 5.8e-10 0.80
55 9.3e-07 1.1e-02 6.2e-05 1.00e+00 1.664204652e+02 1.664227923e+02 5.2e-10 0.86
56 8.4e-07 1.0e-02 5.6e-05 1.00e+00 1.664206226e+02 1.664227169e+02 4.7e-10 0.87
57 7.5e-07 1.0e-02 5.0e-05 1.00e+00 1.664207642e+02 1.664226490e+02 4.2e-10 0.89
58 6.8e-07 9.9e-03 4.5e-05 1.00e+00 1.664208915e+02 1.664225879e+02 3.8e-10 0.90
59 6.1e-07 9.7e-03 4.1e-05 1.00e+00 1.664210061e+02 1.664225328e+02 3.4e-10 0.91
60 5.5e-07 9.5e-03 3.6e-05 1.00e+00 1.664211092e+02 1.664224831e+02 3.1e-10 0.93
61 4.9e-07 9.3e-03 3.3e-05 1.00e+00 1.664212019e+02 1.664224384e+02 2.8e-10 0.94
62 4.4e-07 9.1e-03 3.0e-05 1.00e+00 1.664212853e+02 1.664223981e+02 2.5e-10 0.95
63 4.0e-07 9.0e-03 2.7e-05 9.99e-01 1.664213603e+02 1.664223619e+02 2.2e-10 0.98
64 3.6e-07 8.8e-03 2.4e-05 9.99e-01 1.664214278e+02 1.664223292e+02 2.0e-10 1.03
65 3.2e-07 8.7e-03 2.2e-05 1.00e+00 1.664214885e+02 1.664222998e+02 1.8e-10 1.05
66 2.9e-07 8.6e-03 1.9e-05 9.99e-01 1.664215431e+02 1.664222733e+02 1.6e-10 1.06
67 2.6e-07 8.5e-03 1.7e-05 9.99e-01 1.664215922e+02 1.664222495e+02 1.5e-10 1.08
68 2.4e-07 8.4e-03 1.6e-05 1.00e+00 1.664216365e+02 1.664222280e+02 1.3e-10 1.09
69 2.1e-07 8.3e-03 1.4e-05 9.99e-01 1.664216763e+02 1.664222086e+02 1.2e-10 1.12
70 1.9e-07 8.3e-03 1.3e-05 1.00e+00 1.664217121e+02 1.664221912e+02 1.1e-10 1.14
71 1.7e-07 8.2e-03 1.1e-05 1.00e+00 1.664217443e+02 1.664221755e+02 9.7e-11 1.16
72 1.6e-07 8.1e-03 1.0e-05 9.99e-01 1.664217733e+02 1.664221614e+02 8.7e-11 1.17
73 1.4e-07 8.1e-03 9.3e-06 1.00e+00 1.664217995e+02 1.664221485e+02 7.8e-11 1.18
74 1.3e-07 8.0e-03 8.3e-06 1.00e+00 1.664218230e+02 1.664221371e+02 7.1e-11 1.22
75 1.1e-07 8.0e-03 7.5e-06 9.98e-01 1.664218441e+02 1.664221268e+02 6.4e-11 1.24
76 1.0e-07 8.0e-03 6.8e-06 1.01e+00 1.664218634e+02 1.664221174e+02 5.7e-11 1.26
77 9.2e-08 7.9e-03 6.1e-06 9.93e-01 1.664218804e+02 1.664221091e+02 5.2e-11 1.28
78 8.2e-08 7.9e-03 5.5e-06 9.92e-01 1.664218958e+02 1.664221017e+02 4.6e-11 1.30
79 7.4e-08 7.1e-03 4.9e-06 1.01e+00 1.664219100e+02 1.664220947e+02 4.2e-11 1.31
80 6.7e-08 6.4e-03 4.4e-06 1.00e+00 1.664219225e+02 1.664220886e+02 3.8e-11 1.35
81 6.0e-08 5.7e-03 4.0e-06 9.95e-01 1.664219336e+02 1.664220831e+02 3.4e-11 1.37
82 5.4e-08 5.2e-03 3.6e-06 9.95e-01 1.664219437e+02 1.664220783e+02 3.1e-11 1.39
83 4.9e-08 4.6e-03 3.2e-06 9.97e-01 1.664219527e+02 1.664220739e+02 2.7e-11 1.40
84 4.4e-08 4.2e-03 2.9e-06 1.00e+00 1.664219609e+02 1.664220699e+02 2.5e-11 1.42
85 3.9e-08 3.8e-03 2.6e-06 1.02e+00 1.664219688e+02 1.664220659e+02 2.2e-11 1.43
86 3.6e-08 3.4e-03 2.4e-06 9.94e-01 1.664219753e+02 1.664220628e+02 2.0e-11 1.44
87 3.2e-08 3.0e-03 2.1e-06 1.02e+00 1.664219817e+02 1.664220596e+02 1.8e-11 1.46
88 2.9e-08 2.7e-03 1.9e-06 9.86e-01 1.664219869e+02 1.664220571e+02 1.7e-11 1.48
89 2.6e-08 2.5e-03 1.7e-06 1.00e+00 1.664219917e+02 1.664220547e+02 1.5e-11 1.49
90 2.3e-08 2.2e-03 1.5e-06 1.02e+00 1.664219962e+02 1.664220525e+02 1.3e-11 1.50
91 2.1e-08 2.0e-03 1.4e-06 1.03e+00 1.664220005e+02 1.664220504e+02 1.2e-11 1.52
92 1.9e-08 1.8e-03 1.3e-06 1.01e+00 1.664220040e+02 1.664220486e+02 1.1e-11 1.55
93 1.7e-08 1.6e-03 1.1e-06 1.00e+00 1.664220071e+02 1.664220471e+02 1.0e-11 1.58
94 1.5e-08 1.5e-03 1.0e-06 9.96e-01 1.664220098e+02 1.664220458e+02 9.0e-12 1.60
95 1.4e-08 1.3e-03 9.1e-07 9.92e-01 1.664220122e+02 1.664220447e+02 8.1e-12 1.61
96 1.2e-08 1.2e-03 8.2e-07 9.80e-01 1.664220144e+02 1.664220436e+02 7.3e-12 1.63
97 1.1e-08 1.1e-03 7.4e-07 9.55e-01 1.664220163e+02 1.664220427e+02 6.6e-12 1.64
98 1.0e-08 9.6e-04 6.7e-07 9.59e-01 1.664220181e+02 1.664220419e+02 5.9e-12 1.69
99 9.2e-09 8.6e-04 6.0e-07 9.55e-01 1.664220197e+02 1.664220412e+02 5.3e-12 1.70
100 8.3e-09 7.7e-04 5.4e-07 1.06e+00 1.664220215e+02 1.664220402e+02 4.9e-12 1.75
101 7.5e-09 7.0e-04 4.9e-07 9.30e-01 1.664220227e+02 1.664220396e+02 4.5e-12 1.77
102 6.7e-09 6.3e-04 4.4e-07 9.15e-01 1.664220239e+02 1.664220391e+02 4.0e-12 1.78
103 6.1e-09 5.6e-04 3.9e-07 1.10e+00 1.664220253e+02 1.664220383e+02 3.8e-12 1.80
104 5.5e-09 5.1e-04 3.5e-07 1.16e+00 1.664220269e+02 1.664220375e+02 3.7e-12 1.81
105 2.8e-09 3.3e-05 2.3e-08 8.31e-01 1.664220339e+02 1.664220347e+02 4.9e-13 1.83
Interior-point optimizer terminated. Time: 1.83.
Optimizer terminated. Time: 1.84
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6642203391e+02 Viol. con: 6e-08 var: 0e+00
Dual. obj: 1.6642203466e+02 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.86 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
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.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3439 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 : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.285332508e+05 2.000000000e+00 1.0e+00 0.05
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.263506603e+05 3.573405890e+00 4.8e-01 0.08
2 4.3e+02 5.5e+02 2.4e+04 -9.36e-01 -1.201229629e+05 1.024109129e+01 1.8e-01 0.16
3 2.9e+02 3.7e+02 1.6e+04 -8.38e-01 -1.154146796e+05 6.438967965e+01 1.2e-01 0.17
4 2.8e+02 3.6e+02 1.6e+04 -7.58e-01 -1.128141998e+05 2.256492616e+03 1.2e-01 0.18
5 7.5e+01 9.6e+01 4.1e+03 -7.51e-01 -7.452159547e+04 9.623289244e+03 3.3e-02 0.23
6 3.0e+01 3.8e+01 1.7e+03 -1.92e-01 -4.039642979e+04 1.017306930e+04 1.3e-02 0.27
7 1.8e+01 2.3e+01 1.0e+03 3.96e-01 -2.710383498e+04 6.644076882e+03 7.9e-03 0.28
8 9.5e+00 1.2e+01 5.2e+02 6.30e-01 -1.529784967e+04 3.811651876e+03 4.1e-03 0.30
9 3.3e+00 4.2e+00 1.8e+02 8.18e-01 -5.370881759e+03 1.685460993e+03 1.5e-03 0.31
10 1.6e+00 2.1e+00 9.1e+01 9.54e-01 -2.488163715e+03 1.068021330e+03 7.3e-04 0.33
11 9.3e-01 1.2e+00 5.2e+01 9.86e-01 -1.337520843e+03 6.866519894e+02 4.1e-04 0.34
12 8.5e-01 1.1e+00 4.8e+01 9.60e-01 -1.253928796e+03 6.354852531e+02 3.8e-04 0.36
13 4.7e-01 6.1e-01 2.7e+01 9.77e-01 -6.373643163e+02 4.197161706e+02 2.1e-04 0.38
14 2.5e-01 3.3e-01 1.4e+01 1.00e+00 -2.541512711e+02 3.021241906e+02 1.1e-04 0.39
15 9.3e-02 1.5e-01 5.3e+00 1.00e+00 -3.966326849e+00 2.060664469e+02 4.3e-05 0.40
16 8.6e-02 1.3e-01 4.9e+00 1.02e+00 1.475304501e+01 2.084814275e+02 4.0e-05 0.41
17 6.0e-02 9.6e-02 3.4e+00 1.02e+00 6.117888995e+01 1.950767378e+02 2.8e-05 0.43
18 3.3e-02 7.2e-02 1.9e+00 1.02e+00 1.091859306e+02 1.824025378e+02 1.5e-05 0.44
19 9.2e-03 1.8e-01 5.3e-01 1.02e+00 1.513704968e+02 1.718413722e+02 4.3e-06 0.45
20 3.6e-03 2.1e-01 2.1e-01 1.01e+00 1.602182009e+02 1.683900226e+02 1.7e-06 0.46
21 1.3e-03 1.3e-01 7.6e-02 1.01e+00 1.642699975e+02 1.671903191e+02 6.2e-07 0.48
22 8.6e-04 1.0e-01 5.2e-02 9.84e-01 1.649681567e+02 1.669444025e+02 4.3e-07 0.56
23 2.6e-04 1.1e-01 1.6e-02 9.86e-01 1.659690902e+02 1.665864865e+02 1.3e-07 0.57
24 9.4e-05 1.0e-01 6.1e-03 1.01e+00 1.662459023e+02 1.664756911e+02 5.1e-08 0.59
25 3.7e-05 9.5e-02 2.4e-03 1.01e+00 1.663440798e+02 1.664350964e+02 2.0e-08 0.60
26 1.7e-05 8.1e-02 1.1e-03 1.00e+00 1.663785042e+02 1.664206580e+02 9.5e-09 0.61
27 1.5e-05 7.4e-02 1.0e-03 1.00e+00 1.663820223e+02 1.664199767e+02 8.5e-09 0.71
28 1.4e-05 6.7e-02 9.0e-04 1.01e+00 1.663846091e+02 1.664187607e+02 7.7e-09 0.72
29 1.2e-05 6.1e-02 8.1e-04 1.00e+00 1.663869810e+02 1.664177120e+02 6.9e-09 0.74
30 1.1e-05 5.6e-02 7.3e-04 1.00e+00 1.663891056e+02 1.664167591e+02 6.2e-09 0.78
31 1.0e-05 5.1e-02 6.6e-04 1.00e+00 1.663910162e+02 1.664159007e+02 5.6e-09 0.86
32 9.1e-06 4.7e-02 5.9e-04 1.00e+00 1.663927335e+02 1.664151266e+02 5.0e-09 0.97
33 8.1e-06 4.3e-02 5.3e-04 1.00e+00 1.663942773e+02 1.664144287e+02 4.5e-09 1.07
34 7.3e-06 3.9e-02 4.8e-04 1.00e+00 1.663956653e+02 1.664137995e+02 4.1e-09 1.08
35 6.6e-06 3.6e-02 4.3e-04 1.00e+00 1.663969132e+02 1.664132324e+02 3.7e-09 1.17
36 5.9e-06 3.3e-02 3.9e-04 1.00e+00 1.663980353e+02 1.664127212e+02 3.3e-09 1.19
37 5.3e-06 3.1e-02 3.5e-04 1.00e+00 1.663990443e+02 1.664122606e+02 3.0e-09 1.20
38 4.8e-06 2.9e-02 3.2e-04 1.00e+00 1.663999516e+02 1.664118455e+02 2.7e-09 1.21
39 4.3e-06 2.6e-02 2.8e-04 1.00e+00 1.664007676e+02 1.664114714e+02 2.4e-09 1.24
40 3.9e-06 2.5e-02 2.6e-04 1.00e+00 1.664015014e+02 1.664111343e+02 2.2e-09 1.26
41 3.5e-06 2.3e-02 2.3e-04 1.00e+00 1.664021613e+02 1.664108304e+02 2.0e-09 1.27
42 3.2e-06 2.1e-02 2.1e-04 1.00e+00 1.664027548e+02 1.664105566e+02 1.8e-09 1.29
43 2.8e-06 2.0e-02 1.9e-04 1.00e+00 1.664032885e+02 1.664103100e+02 1.6e-09 1.75
44 2.6e-06 1.9e-02 1.7e-04 1.00e+00 1.664037686e+02 1.664100877e+02 1.4e-09 1.89
45 2.3e-06 1.8e-02 1.5e-04 1.00e+00 1.664042005e+02 1.664098874e+02 1.3e-09 1.91
46 2.1e-06 1.7e-02 1.4e-04 1.00e+00 1.664045890e+02 1.664097071e+02 1.2e-09 1.93
47 1.9e-06 1.6e-02 1.2e-04 1.00e+00 1.664049385e+02 1.664095447e+02 1.0e-09 1.97
48 1.7e-06 1.5e-02 1.1e-04 1.00e+00 1.664052529e+02 1.664093984e+02 9.4e-10 1.98
49 1.5e-06 1.4e-02 9.9e-05 1.00e+00 1.664055358e+02 1.664092668e+02 8.4e-10 2.02
50 1.4e-06 1.4e-02 8.9e-05 1.00e+00 1.664057904e+02 1.664091482e+02 7.6e-10 2.04
51 1.2e-06 1.3e-02 8.0e-05 1.00e+00 1.664060194e+02 1.664090414e+02 6.8e-10 2.08
52 1.1e-06 1.2e-02 7.2e-05 1.00e+00 1.664062254e+02 1.664089452e+02 6.1e-10 2.14
53 9.9e-07 1.2e-02 6.5e-05 1.00e+00 1.664064108e+02 1.664088586e+02 5.5e-10 2.23
54 8.9e-07 1.2e-02 5.9e-05 1.00e+00 1.664065776e+02 1.664087805e+02 5.0e-10 2.28
55 8.0e-07 1.1e-02 5.3e-05 1.00e+00 1.664067277e+02 1.664087103e+02 4.5e-10 2.30
56 7.2e-07 1.1e-02 4.7e-05 1.00e+00 1.664068627e+02 1.664086471e+02 4.0e-10 2.31
57 6.5e-07 1.0e-02 4.3e-05 1.00e+00 1.664069841e+02 1.664085901e+02 3.6e-10 2.37
58 5.8e-07 1.0e-02 3.8e-05 1.00e+00 1.664070934e+02 1.664085387e+02 3.3e-10 2.38
59 5.3e-07 9.9e-03 3.5e-05 1.00e+00 1.664071917e+02 1.664084925e+02 2.9e-10 2.79
60 4.7e-07 9.7e-03 3.1e-05 1.00e+00 1.664072801e+02 1.664084508e+02 2.6e-10 2.81
61 4.3e-07 9.5e-03 2.8e-05 1.00e+00 1.664073596e+02 1.664084132e+02 2.4e-10 2.89
62 3.8e-07 9.3e-03 2.5e-05 1.00e+00 1.664074312e+02 1.664083794e+02 2.1e-10 2.90
63 3.5e-07 9.1e-03 2.3e-05 9.99e-01 1.664074955e+02 1.664083489e+02 1.9e-10 2.92
64 3.1e-07 9.0e-03 2.0e-05 1.00e+00 1.664075534e+02 1.664083215e+02 1.7e-10 3.01
65 2.8e-07 8.8e-03 1.8e-05 9.98e-01 1.664076055e+02 1.664082968e+02 1.6e-10 3.03
66 2.5e-07 8.7e-03 1.7e-05 1.00e+00 1.664076523e+02 1.664082745e+02 1.4e-10 3.04
67 2.3e-07 8.6e-03 1.5e-05 1.00e+00 1.664076945e+02 1.664082544e+02 1.3e-10 3.20
68 2.0e-07 8.5e-03 1.3e-05 1.00e+00 1.664077324e+02 1.664082364e+02 1.1e-10 3.25
69 1.8e-07 8.4e-03 1.2e-05 1.00e+00 1.664077666e+02 1.664082201e+02 1.0e-10 3.43
70 1.7e-07 8.3e-03 1.1e-05 1.01e+00 1.664077977e+02 1.664082052e+02 9.2e-11 3.50
71 1.5e-07 8.3e-03 9.8e-06 1.00e+00 1.664078255e+02 1.664081919e+02 8.3e-11 3.53
72 1.3e-07 8.2e-03 8.8e-06 1.01e+00 1.664078506e+02 1.664081798e+02 7.5e-11 3.72
73 1.2e-07 8.2e-03 7.9e-06 1.00e+00 1.664078729e+02 1.664081692e+02 6.7e-11 3.92
74 1.1e-07 8.1e-03 7.1e-06 9.98e-01 1.664078930e+02 1.664081597e+02 6.1e-11 4.24
75 9.8e-08 8.0e-03 6.4e-06 9.94e-01 1.664079110e+02 1.664081511e+02 5.5e-11 4.56
76 8.8e-08 8.0e-03 5.8e-06 9.99e-01 1.664079273e+02 1.664081434e+02 4.9e-11 4.73
77 7.9e-08 8.0e-03 5.2e-06 1.00e+00 1.664079420e+02 1.664081363e+02 4.4e-11 4.75
78 7.1e-08 7.9e-03 4.7e-06 1.00e+00 1.664079552e+02 1.664081300e+02 4.0e-11 4.76
79 6.4e-08 7.9e-03 4.2e-06 9.93e-01 1.664079670e+02 1.664081244e+02 3.6e-11 4.77
80 5.8e-08 7.9e-03 3.8e-06 1.00e+00 1.664079778e+02 1.664081193e+02 3.2e-11 4.78
81 5.2e-08 7.1e-03 3.4e-06 1.01e+00 1.664079875e+02 1.664081146e+02 2.9e-11 4.80
82 4.7e-08 6.4e-03 3.1e-06 1.00e+00 1.664079961e+02 1.664081105e+02 2.6e-11 4.81
83 4.2e-08 5.7e-03 2.8e-06 1.01e+00 1.664080043e+02 1.664081065e+02 2.4e-11 4.82
84 3.8e-08 5.2e-03 2.5e-06 1.01e+00 1.664080114e+02 1.664081031e+02 2.1e-11 4.83
85 3.4e-08 4.6e-03 2.2e-06 9.95e-01 1.664080176e+02 1.664081002e+02 1.9e-11 4.85
86 3.1e-08 4.2e-03 2.0e-06 1.01e+00 1.664080233e+02 1.664080974e+02 1.7e-11 4.86
87 2.8e-08 3.8e-03 1.8e-06 9.96e-01 1.664080283e+02 1.664080951e+02 1.6e-11 4.87
88 2.5e-08 3.4e-03 1.6e-06 9.84e-01 1.664080328e+02 1.664080929e+02 1.4e-11 4.89
89 2.2e-08 3.0e-03 1.5e-06 9.92e-01 1.664080369e+02 1.664080910e+02 1.3e-11 4.90
90 2.0e-08 2.7e-03 1.3e-06 9.81e-01 1.664080405e+02 1.664080893e+02 1.1e-11 4.91
91 1.8e-08 2.5e-03 1.2e-06 1.04e+00 1.664080444e+02 1.664080874e+02 1.0e-11 5.01
92 1.6e-08 2.2e-03 1.1e-06 9.20e-01 1.664080473e+02 1.664080861e+02 9.4e-12 5.02
93 1.5e-08 2.0e-03 9.6e-07 9.87e-01 1.664080499e+02 1.664080848e+02 8.5e-12 5.15
94 1.3e-08 1.8e-03 8.7e-07 9.59e-01 1.664080522e+02 1.664080838e+02 7.6e-12 5.22
95 1.2e-08 1.6e-03 7.8e-07 9.71e-01 1.664080543e+02 1.664080828e+02 6.9e-12 5.23
96 1.1e-08 1.5e-03 7.0e-07 9.83e-01 1.664080562e+02 1.664080818e+02 6.2e-12 5.24
97 9.7e-09 1.3e-03 6.3e-07 9.95e-01 1.664080580e+02 1.664080810e+02 5.6e-12 5.25
98 8.7e-09 1.2e-03 5.7e-07 1.08e+00 1.664080601e+02 1.664080799e+02 5.2e-12 5.26
99 7.8e-09 1.1e-03 5.1e-07 9.77e-01 1.664080614e+02 1.664080793e+02 4.7e-12 5.28
100 7.1e-09 9.5e-04 4.6e-07 8.48e-01 1.664080626e+02 1.664080788e+02 4.2e-12 5.29
101 6.4e-09 8.6e-04 4.1e-07 9.79e-01 1.664080637e+02 1.664080782e+02 3.8e-12 5.30
102 5.8e-09 7.7e-04 3.7e-07 1.21e+00 1.664080656e+02 1.664080771e+02 3.8e-12 5.31
103 5.3e-09 7.0e-04 3.4e-07 8.63e-01 1.664080664e+02 1.664080768e+02 3.4e-12 5.33
104 4.8e-09 6.3e-04 3.0e-07 1.03e+00 1.664080672e+02 1.664080764e+02 3.1e-12 5.34
105 4.5e-09 5.6e-04 2.7e-07 1.14e+00 1.664080682e+02 1.664080759e+02 3.0e-12 5.35
106 6.2e-09 6.7e-05 3.3e-08 7.54e-01 1.664080731e+02 1.664080742e+02 6.1e-13 5.54
Interior-point optimizer terminated. Time: 5.54.
Optimizer terminated. Time: 5.55
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6640807313e+02 Viol. con: 9e-08 var: 0e+00
Dual. obj: 1.6640807415e+02 Viol. con: 0e+00 var: 4e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 5.57 seconds.
Solving took 9 GP solves and 86.7 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: 1.495740870058179e+110 vs 1.49570172575e+110
GP iteration 0 has relaxed constants
Cost
----
1.496e+110
Free Variables
--------------
| Mission.Aircraft.Engine.Turbine.Relax
C_{p_{t2}} : 2.251 Cp Value for Combustion Products in LP Turbine
| Mission.Aircraft.Fuselage.Relax
l_{nose} : 1.042 Nose length
n_{pass} : [ 2.86 ] Number of passengers
| Mission.Aircraft.Relax
f_{L_{total/wing}} : 1.656 Total lift as a percentage of wing lift
| Mission.Aircraft.Wing.WingNoStruct.Relax
\tan(\Lambda) : 1.133 Tangent of quarter-chord sweep angle
| Mission.FlightState.Atmosphere.Relax
L_{atm} : [ 1.77 1 1 1 1 ] Temperature lapse rate
T_{sl} : [ 1 1 1.25 1 1 ] Temperature at sea level
| Mission.Relax
R_{req} : 2.362 Required Cruise Range
GP iteration 1 has relaxed constants
Cost
----
7.486e+74
Free Variables
--------------
| Mission.Aircraft.Engine.Combustor.Relax
hold_{4a} : 1.093 1+(gamma-1)/2 * M_4a**2
| Mission.Aircraft.Fuselage.Relax
n_{pass} : [ 1.03 ] Number of passengers
| Mission.Aircraft.LandingGear.Relax
h_{hold} : 1.006 Hold height
Solution check warning: Primal solution computed cost did not match solver-returned cost: 3.70539773406721e+72 vs 3.70524769429e+72
WEIGHT DIFFERENCES
Total Fuel Weight Percent Diff: [-92.94682341]
Total Aircraft Weight Percent Diff: [-21.48056538]
Engine Weight Percent Diff: -56.27822091678476
Fuselage Weight Percent Diff: -0.869725296853007
Payload Weight Percent Diff: [-0.04003557]
VT Weight Percent Diff: -8.6077263920923
HT Weight Percent Diff: -93.23325716227288
Wing Weight Percent Diff: 8.267439218976007
WING DIFFERENCES
Wing Span Percent Diff: -0.029994856793720385
Wing Area Percent Diff: 32.90010333250834
HORIZONTAL TAIL DIFFERENCES
HT Area Percent Diff: 40.48930585994106
VERTICAL TAIL DIFFERENCES
VT Span Percent Diff: -11.022337366369138
VT Area Percent Diff: -60.38683290529611
CRUISE SEGMENT 1 DRAG DIFFERENCES
Overall Cd Percent Diff: [-18.54730647]
L/D Percent Diff: [24.0102099]
Nacelle Cd Percent Diff: [-94.27641573]
HT Cd Percent Diff: [-80.76936701] dimensionless
Fuselage Cd Percent Diff: [108.78752887]
VT Cd Percent Diff: [-58.00304197] dimensionless
Wing Cd percent Diff: [-14.2292792]
Induced Drag Cd Percent Diff: [1.2194058]
CRUISE SEGMENT 1 TSFC DIFFERENCES
Initial Cruise TSFC Percent Diff: [-90.57035978]
FUSELAGE DIFFERENCES
Weight of HB material: -38.36021065314171
Weight of VB material: 87.82227997816754
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.71260519]
Mission1
========
Cost
----
W_{f_{total}}[:].sum()
Constraints
-----------
W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin}
PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:])
x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:])
x_{CG}[3] <= \Delta x_n + x_n
\Delta x_m + x_{CG}[3] >= x_m
\tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m
C_{D_{fuse}}[:] = 0.018081
M_{fuseD} = 0.72
W_{start}[0] = W_{total}[:]
W_{start}[:] >= W_{end}[:] + W_{burn}[:]
W_{start}[1:] = W_{end}[:4]
W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1]
W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2]
W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1]
hft[2] >= CruiseAlt
hft[1:5] = hft[:4] + dhft[1:5]
hft[0] = dhft[0]
dhft[1:3] = dhft[:2]
RC[0] >= 2.5e+03
RC[:3] >= RC_{min}[:3]
\theta[2] >= 0.015
hft[2] >= MinCruiseAlt
n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:]
R_{segment}[3:4] = R_{segment}[4:5]
M[3:5] >= M_{min}
0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req}
Fsafetyfac*F[0] = T_e
W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:]
V_2[:] = M_2[:]*a[:]
\alpha_{max,w}[:3] = 0.18
\alpha_{max,w}[3:] = 0.1
0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime
0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime
ClimbTime <= MaxClimbTime
T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}}
F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
OPR[:] <= OPR_{max}
Aircraft
Fuselage
W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on}
W_{pass}[:] >= n_{pass}[:]*W_{avg. pass}
W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo}
W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}}
W_{payload}[:] <= W_{payload_{max}}
n_{pass}[:] <= n_{seat}
n_{rows} = n_{seat}/SPR
l_{shell} = n_{rows}*p_s
\theta_{db} = w_{db}/R_{fuse}
R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db}
A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db}
(PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse}
A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin}
w_{floor} = w_{fuse}
R_{fuse} + w_{db} >= w_{fuse}
h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse}
t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell}
S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2
S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2
l_{fuse} = l_{nose} + l_{shell} + l_{cone}
l_{cone} = R_{fuse}/\lambda_{cone}
x_{shell1} = l_{nose}
x_{shell2} >= l_{nose} + l_{shell}
t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin}
t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin}
\sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell})
\sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin}
l_{floor} >= l_{shell} + 2*R_{fuse}
P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat})
A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor}
V_{floor} = 2*w_{floor}*A_{floor}
W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor}
\tau_{cone} = \sigma_{skin}
W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame})
x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone}
-2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}}
(PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}}
x_{hbend_{Land}} >= x_{wing}
x_{hbend_{Land}} <= l_{fuse}
x_{hbend_{MLF}} >= x_{wing}
x_{hbend_{MLF}} <= l_{fuse}
A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}})
A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}})
A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
A_{2h_{MLF}} >= Mission1.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2)
A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}}
A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}}
A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}}
A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}}
A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}}
A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}}
A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}}
A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}}
V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}}
W_{hbend} >= g*\rho_{bend}*V_{hbend}
x_{vbend} >= x_{wing}
x_{vbend} <= l_{fuse}
B_{0v} = B_{1v}*(x_{tail} - x_{vbend})
B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2)
B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}}
0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}}
V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}}
W_{vbend} >= \rho_{bend}*g*V_{vbend}
x_f = x_{wing} + 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
x_b = x_{wing} - 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
\sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h}
\sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v}
V_{cyl} = A_{skin}*l_{shell}
V_{nose} = S_{nose}*t_{skin}
V_{bulk} = S_{bulk}*t_{skin}
V_{db} = A_{db}*l_{shell}
V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse})
W_{apu} = W_{payload_{max}}*f_{apu}
W_{db} = \rho_{skin}*g*V_{db}
W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk})
W_{window} >= W'_{window}*l_{shell}
W_{padd} = W_{payload_{max}}*f_{padd}
W_{seat} >= W'_{seat}*n_{seat}
W_{seat} >= f_{seat}*W_{payload_{max}}
W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk})
W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db}
W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone})
Wing
WingNoStruct
A_{rect} = c_{tip}*b
0.5*(1 - \lambda)*c_{root}*b <= A_{tri}
p >= 1 + 2*\lambda
2*q >= 1 + p
y_{mac} = b/3*q/p
mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q
\lambda = c_{tip}/c_{root}
S = b*(c_{root} + c_{tip})/2
0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w)
e*(1 + f(\lambda_w)*AR) <= 1
\lambda >= 0.15
V_{fuel, max} <= 0.303*mac^2*b*\tau
W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g
b <= b_{max}
WingBox
AR = b^2/S
0.423*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5)
\tau <= \tau_{max_w}
W_{struct} >= W_{web} + W_{cap}
AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5)
Mission1.Aircraft.Wing.WingBox.N_{lift} = 3
Mission1.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8
\lambda = taper
W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt})
0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}}
Engine
Compressor
(no constraints)
Combustor
(no constraints)
Turbine
(no constraints)
Thrust
(no constraints)
FanMap
(no constraints)
LPCMap
(no constraints)
HPCMap
(no constraints)
Sizing
A_{2} >= A_{5} + A_{7}
FlightState
V[:] = V[:]
a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
V[:] = M[:]*a[:]
Altitude
h[:] = hft[:]
Atmosphere
(P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
\rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
\mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
EnginePerformance
CompressorPerformance
T_{t_0}[:] = T_{atm}[:]/c1[:]^-1
h_{t_0}[:] = C_{p_{air}*T_{t_0}[:]
P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:]
T_{t_{1.8}}[:] = T_{t_0}[:]
h_{t_{1.8}}[:] = h_{t_0}[:]
P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5
T_{T_{2}}[:] = T_{t_{1.8}}[:]
h_{T_{2}}[:] = h_{t_{1.8}}[:]
P_{T_{2}}[:] = P_{t_{1.8}}[:]
P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:]
T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016
h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:]
P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:]
T_{t_7}[:] = T_{t_{2.1}}[:]
h_{t_7}[:] = h_{t_{2.1}}[:]
P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:]
T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152
h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1}
P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:]
T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491
h_{t_3}[:] = C_{p_{2}*T_{t_3}[:]
CombustorPerformance
h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:]
h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:]
fp1[:] = f[:] + 1
M_{4a}[:] = 0.1025
fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5
T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]]
P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891
u_{4a}[:] = M_{4a}[:]*(1.31*Mission1.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a}
u_c[:] = r_{uc}*u_{4a}[:]
P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891
TurbinePerformance
h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:]
P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:]
\pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565
h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:]
P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:]
T_{t_5}[:] = T_{t_{4.9}}[:]
h_{t_5}[:] = h_{t_{4.9}}[:]
ThrustPerformance
P_{8}[:] = P_{atm}[:]
h_{8}[:] = C_{p_{fex}*T_{8}[:]
u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:]
(P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:]
h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:]
P_{6}[:] = P_{atm}[:]
(P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:]
u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:]
h_6[:] = C_{p_{tex}*T_{6}[:]
h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:]
\alpha[:] = m_{fan}[:]/m_{core}[:]
\alpha_{+1}[:] = \alpha[:] + 1
\alpha[:] <= \alpha_{max}
F[:] <= F_{6}[:] + F_{8}[:]
F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:])
TSFC[:] = 1/I_{sp}[:]
F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:]
FanMapPerformance
m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}}
LPCMapPerformance
m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D}
HPCMapPerformance
m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D}
SizingPerformance
P_{7}[:] >= P_{atm}[:]
M_7[:] <= 1
a_{7}[:] = (1.4*Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5
a_{7}[:]*M_7[:] = u_{7}[:]
\rho_7[:] = P_{7}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])
P_{5}[:] >= P_{atm}[:]
M_5[:] <= 1
a_{5}[:] = (1.39*Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5
a_{5}[:]*M_5[:] = u_{5}[:]
\rho_5[:] = P_{5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])
h_{2}[:] = C_{p_{1}*T_{2}[:]
\rho_{2}[:] = P_{2}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:])
u_{2}[:] = M_2[:]*(C_{p_{1}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:]/781)^0.5
h_{2.5}[:] = C_{p_{2}*T_{2.5}[:]
\rho_{2.5}[:] = P_{2.5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:])
u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/781)^0.5
m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine}
d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5
d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5
\eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]])
h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:]
P_{t_4}[:] = \pi_{b}*P_{t_3}[:]
M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]]
M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]])
P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:]
\pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013
\pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10
\pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10
\pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10
m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
\pi_{f}[:] >= 1
\pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10
\pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10
\pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10
\pi_{lc}[:] >= 1
m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
\pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10
\pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10
\pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10
m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref})
\pi_{hc}[:] >= 1
OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:]
P_{t_8}[:] = P_{t_7}[:]
T_{t_8}[:] = T_{t_7}[:]
P_{t_6}[:] = P_{t_5}[:]
T_{t_6}[:] = T_{t_5}[:]
F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:]
I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g)
N_{f}[:]*G_{f} = N_{1}[:]
N_{1}[:] <= 1.1
N_{2}[:] <= 1.1
fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD}
fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD}
P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5
(T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2
P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979
(T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2
M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:]
m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:]
m_{total}[:] = m_{fan}[:] + m_{core}[:]
P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512
T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1
m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2}
P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857
T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1
m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5}
1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD}
0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD}
1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD}
0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD}
m_{lc_D} >= 0.7*m_{coreD}/0.649
m_{lc_D} <= 1.3*m_{coreD}/0.649
m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23
m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23
\bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405
\bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405
F[:] = F_{spec}[:]
T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}}
OPR[:] <= OPR_{max}
VerticalTail
VerticalTailNoStruct
C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}}
L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}}
c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt}))
A_{vt} = b_{vt}^2/S_{vt}
b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt}
p_{vt} >= 1 + 2*\lambda_{vt}
2*q_{vt} >= 1 + p_{vt}
y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt}
\lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}}
\Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}}
\Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt}
\lambda_{vt} >= 0.25
V_{vt} >= V_{vt_{min}}
WingBox
AR_{vt} = (2*b_{vt})^2/(2*S_{vt})
0.423*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
\tau_{vt} <= 0.14
W_{struct} >= 0.5*(W_{web} + W_{cap})
Mission1.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24
AR_{vt}*2*L_{vt_{max}}*Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
Mission1.Aircraft.VerticalTail.WingBox.N_{lift} = 1
Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*Mission1.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8
\lambda_{vt} = taper
W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT})
HorizontalTail
HorizontalTailNoStruct
\Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht}
\Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}}
p_{ht} >= 1 + 2*\lambda_{ht}
2*q_{ht} >= 1 + p_{ht}
y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht}
0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht}
\lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}}
S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2
0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht})
e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1
AR_{ht} = b_{ht}^2/S_{ht}
\lambda_{ht} >= 0.2
\lambda_{ht} <= 1
WingBox
AR_{ht} = b_{ht}^2/S_{ht}
0.423*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
\tau_{ht} <= 0.14
W_{struct} >= W_{web} + W_{cap}
L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2
L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht})
2*AR_{ht}*L_{shear}*Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
Mission1.Aircraft.HorizontalTail.WingBox.N_{lift} = 1
Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission1.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8
L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht}
L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}}
W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht})
LandingGear
l_n + z_{wing} + y_m*\tan(\gamma) >= l_m
T = 2*y_m
x_m >= x_n + B
x_n >= 5
\tan(\phi) = \tan(\phi_{min})
(z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1
\tan(\psi) <= \tan(\psi_{max})
x_{up} - x_m <= l_m/\tan(\theta_{max})
y_m >= l_m
S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG})
l_{oleo} = 2.5*S_{sa}
d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5
l_m >= l_{oleo} + d_{t_m}/2
F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in])
W_{wa,m} = 1.2*F_{w_m}^0.609
F_{w_n} = L_{w_n}*d_{t_n}/1e+03
W_{wa,n} = 1.2*F_{w_n}^0.609
L_{w_m} = L_m/(n_{mg}*n_{wps})
L_{w_n} = L_n/n_{wps}
d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315
w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48
d_{t_n} = 0.8*d_{t_m}
w_{t_n} = 0.8*w_{t_m}
W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g
N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m
W_{mw} = n_{wps}*W_{wa,m}
W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g
\sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}})
W_{nw} >= n_{wps}*W_{wa,n}
L_m <= 9.87*E*I_m/(K*l_m)^2
I_m = PI*r_m^3*t_m
L_n <= 9.87*E*I_n/(K*l_n)^2
I_n = PI*r_n^3*t_n
2*r_m/t_m <= 40
2*r_m/t_n <= 40
h_{hold} >= 2*w_{t_m} + 2*r_m
0.8 >= 2*w_{t_n} + 2*r_n
W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m}))
W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n})
W_{lg} >= C_{lg}*(W_{mg} + W_{ng})
W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m
x_m >= x_{CG_{lg}}
c_{root} = c_0
Mission1.Aircraft.Wing.WingBox.r_{w/c} = Mission1.Aircraft.Fuselage.r_{w/c}
x_w = x_{wing}
Mission1.Aircraft.Fuselage.N_{lift} = Mission1.Aircraft.Wing.WingBox.N_{lift}
f_{L_{total/wing}}*L_{max} >= Mission1.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}}
W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc}
W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:]
W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:]
W_{total}[:] <= W_{total, max}
f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}}
W_{misc} >= W_{lg} + W_{hpesys}
W_{hpesys} = f_{hpesys}*W_{total, max}
x_n <= l_{nose}
x_m >= x_{wing}
\Delta x_{AC_{wing}} + x_{wing} >= x_m
x_{hpesys} = 1.1*l_{nose}
x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys}
d_{nacelle} >= d_{f} + 2*t_{nacelle}
E_{land} >= W_{total, max}/(2*g)*w_{ult}^2
x_{up} = x_{shell2}
L_n = W_{total, max}*\Delta x_m/B
L_m = W_{total, max}*\Delta x_n/B
L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max}
y_{eng} >= y_m
3*n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}}
V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse}
W_{tail} >= n_{vt}*W_{vt} + W_{ht}
2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db}
B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v})
m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht}
x_{CG_{ht}} <= l_{fuse}
V_{ht} = S_{ht}*l_{ht}/(S*mac)
L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}}
L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}}
x_{CG_{vt}} <= l_{fuse}
V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b)
n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max}
n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng}
D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}}
I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:]
I_{z}[:] <= I_{z, max}
S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2
l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}}
f_{S_{nacelle}} = S_{nacelle}*S^-1
A_{inlet} = 0.4*S_{nacelle}
A_{fancowl} = 0.2*S_{nacelle}
A_{exh} = 0.4*S_{nacelle}
A_{corecowl} = 3PI*d_{LPC}^2
W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl})
W_{eadd} = f_{eadd}*W_{engine}
W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon}
W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine})
y_{eng} = 0.5*w_{fuse}
(L_{max} - Mission1.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission1.Aircraft.Wing.WingBox.M_r*c_{root}
A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend})
A_{1h_{MLF}} >= (Mission1.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h})
I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16)
I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81
I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81)
x_{shell2} + l_{cone} >= x_{eng}
x_{eng} >= x_{shell2} + 0.75*l_{cone}
S_{floor} = 0.312*P_{floor}
M_{floor} = 0.0352*P_{floor}*w_{floor}
\Delta R_{fuse} = R_{fuse}*0.43/1.75
b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2
b_{ht_{out}} = 0.5*b_{ht} - w_{fuse}
L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}}
M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}}
L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}}
c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach}
\pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht})
FlightSegment
FlightState
V[:] = V[:]
a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
V[:] = M[:]*a[:]
Altitude
h[:] = hft[:]
Atmosphere
(P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
\rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
\mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
FlightP
P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:]
RC[:] = P_{excess}[:]/W_{avg}[:]
\theta[:]*V[:] = RC[:]
dhft[:] = tmin[:]*RC[:]
R_{segment}[:] = thr[:]*V[:]
WingPerformance
0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:]
\Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:]
\Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2
(AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2
C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:]
\alpha_w[:] <= \alpha_{max,w}[:]
D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:]
C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:]
C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR)
Re_w[:] = \rho[:]*V[:]*mac/\mu[:]
C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114
FuselagePerformance
(no constraints)
VerticalTailPerformance
D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:]
Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:]
C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577
HorizontalTailPerformance
L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:]
C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:]
\alpha_{ht}[:] <= \alpha_{ht,max}
C_{L_{\alpha,ht_0}}[:] = 6.28
D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:]
C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht})
Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:]
C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852
W_{burn}[:] = W_{burn}[:]
F_{fuel}[:] = F_{fuel}[:]
\rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:])
P_{cabin}[:] = 7.5e+04
T_{cabin}[:] = 297
V[:] >= V_{stall}[:]
W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:]
tmin[:] = thr[:]
L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:]
L_{total}[:] = f_{L_{total/wing}}*L_w[:]
L_{total}[:] >= W_{avg}[:] + L_{ht}[:]
D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2
D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:])
C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S)
L/D[:] = W_{avg}[:]/D[:]
W_{Load}[:] <= W_{Load_{max}}[:]
W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S
p_{o}[:] >= L_w[:]*c_{root}/S
\eta_{o}[:] = w_{fuse}/(b/2)
x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:]
c_{m_{w}}[:] = 1.9
x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2)
x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse}
x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}}
x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}}
C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht}
AR_{ht} >= 4
C_{L_{ht}}[:] >= 0.01
SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac
SM[:] >= SM_{min}
SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}}
x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:]
R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:]
C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2
V_{nacelle}[:] = r_{v_{nacelle}}*V[:]
V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]]
r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0)
C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0
D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S
\Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}}
M_2[:3] = M[:3]
M_{2.5}[:3] = 0.6
hold_{2}[:3] = 1.07164
hold_{2.5}[:3] = 1.06372
P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:]
c1[:] = 1 + 0.201*M[:]^2.0
M_2[3:] = M[3:]
M_{2.5}[3:] = 0.6
hold_{2}[3:] = 1.07164
hold_{2.5}[3:] = 1.06372
Beginning signomial solve.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
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.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3438 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 : 1.64e+04 after factor : 1.45e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 2.9e+03 1.3e+05 0.00e+00 -1.280976207e+05 2.000000000e+00 1.0e+00 0.05
1 1.1e+03 1.4e+03 6.3e+04 -9.71e-01 -1.260360597e+05 3.611424052e+00 4.9e-01 0.53
2 4.1e+02 5.3e+02 2.3e+04 -9.38e-01 -1.195206719e+05 1.063331153e+01 1.8e-01 0.62
3 2.9e+02 3.7e+02 1.6e+04 -8.34e-01 -1.151942168e+05 6.795829655e+01 1.3e-01 0.66
4 2.8e+02 3.7e+02 1.6e+04 -7.59e-01 -1.127212826e+05 2.109723808e+03 1.3e-01 1.38
5 8.8e+01 1.1e+02 5.0e+03 -7.53e-01 -8.071413615e+04 8.411072422e+03 3.9e-02 1.56
6 3.7e+01 4.8e+01 2.1e+03 -2.93e-01 -4.787028059e+04 1.016025756e+04 1.6e-02 1.76
7 2.1e+01 2.8e+01 1.2e+03 2.52e-01 -3.173778936e+04 7.155034269e+03 9.5e-03 1.78
8 9.4e+00 1.2e+01 5.3e+02 5.36e-01 -1.511150083e+04 4.167123567e+03 4.2e-03 1.79
9 5.5e+00 7.1e+00 3.1e+02 8.14e-01 -8.836155418e+03 2.832992813e+03 2.5e-03 1.80
10 1.3e+00 1.7e+00 7.6e+01 9.07e-01 -2.021517100e+03 9.278094940e+02 6.1e-04 1.82
11 7.0e-01 9.1e-01 4.0e+01 9.94e-01 -8.292899266e+02 7.204982019e+02 3.2e-04 1.83
12 4.7e-01 6.1e-01 2.7e+01 9.97e-01 -4.810408396e+02 5.632816117e+02 2.1e-04 1.84
13 3.5e-01 7.3e-01 2.0e+01 9.79e-01 -3.119899248e+02 4.857188935e+02 1.6e-04 1.86
14 1.7e-01 3.5e-01 9.8e+00 9.96e-01 -1.727746611e+01 3.656933383e+02 7.9e-05 1.87
15 5.5e-02 1.5e-01 3.2e+00 9.94e-01 1.624902967e+02 2.901499707e+02 2.7e-05 2.50
16 3.2e-02 1.3e-01 1.9e+00 1.00e+00 1.999027139e+02 2.746125040e+02 1.6e-05 2.73
17 5.1e-03 1.8e-01 3.2e-01 1.00e+00 2.445305033e+02 2.572371524e+02 2.8e-06 2.87
18 1.5e-03 1.3e-01 9.6e-02 1.00e+00 2.509424510e+02 2.546897023e+02 8.3e-07 3.61
19 4.8e-04 1.1e-01 3.2e-02 1.00e+00 2.527845502e+02 2.540210950e+02 2.8e-07 4.27
20 2.1e-04 8.6e-02 1.4e-02 1.00e+00 2.532880856e+02 2.538352203e+02 1.2e-07 4.74
21 1.9e-04 7.8e-02 1.3e-02 1.00e+00 2.533292209e+02 2.538216573e+02 1.1e-07 4.99
22 1.7e-04 7.1e-02 1.1e-02 1.00e+00 2.533650962e+02 2.538082643e+02 1.0e-07 5.11
23 1.5e-04 6.4e-02 1.0e-02 1.00e+00 2.533974267e+02 2.537962616e+02 9.0e-08 5.15
24 1.4e-04 5.9e-02 9.2e-03 1.00e+00 2.534264980e+02 2.537854354e+02 8.1e-08 5.25
25 1.2e-04 5.4e-02 8.3e-03 1.00e+00 2.534526435e+02 2.537756756e+02 7.3e-08 5.49
26 1.1e-04 4.9e-02 7.5e-03 1.00e+00 2.534761571e+02 2.537668763e+02 6.5e-08 5.82
27 1.0e-04 4.5e-02 6.7e-03 1.00e+00 2.534973060e+02 2.537589453e+02 5.9e-08 6.14
28 9.0e-05 4.1e-02 6.1e-03 1.00e+00 2.535163290e+02 2.537517977e+02 5.3e-08 6.95
29 8.1e-05 3.8e-02 5.4e-03 1.00e+00 2.535334405e+02 2.537453571e+02 4.8e-08 7.38
30 7.3e-05 3.5e-02 4.9e-03 1.00e+00 2.535488335e+02 2.537395540e+02 4.3e-08 7.44
31 6.6e-05 3.2e-02 4.4e-03 1.00e+00 2.535626808e+02 2.537343259e+02 3.9e-08 7.48
32 5.9e-05 3.0e-02 4.0e-03 1.00e+00 2.535751383e+02 2.537296160e+02 3.5e-08 7.53
33 5.3e-05 2.7e-02 3.6e-03 1.00e+00 2.535863455e+02 2.537253733e+02 3.1e-08 8.65
34 4.8e-05 2.5e-02 3.2e-03 1.00e+00 2.535964283e+02 2.537215515e+02 2.8e-08 9.04
35 4.3e-05 2.4e-02 2.9e-03 1.00e+00 2.536054996e+02 2.537181092e+02 2.5e-08 9.40
36 3.9e-05 2.2e-02 2.6e-03 1.00e+00 2.536136611e+02 2.537150086e+02 2.3e-08 9.57
37 3.5e-05 2.0e-02 2.3e-03 1.00e+00 2.536210042e+02 2.537122161e+02 2.1e-08 9.66
38 3.2e-05 1.9e-02 2.1e-03 1.00e+00 2.536276109e+02 2.537097011e+02 1.9e-08 9.69
39 2.8e-05 1.8e-02 1.9e-03 1.00e+00 2.536335554e+02 2.537074360e+02 1.7e-08 9.72
40 2.6e-05 1.7e-02 1.7e-03 1.00e+00 2.536389040e+02 2.537053963e+02 1.5e-08 9.74
41 2.3e-05 1.6e-02 1.5e-03 1.00e+00 2.536437166e+02 2.537035594e+02 1.3e-08 9.80
42 2.1e-05 1.5e-02 1.4e-03 1.00e+00 2.536480470e+02 2.537019053e+02 1.2e-08 9.82
43 1.9e-05 1.4e-02 1.2e-03 1.00e+00 2.536519435e+02 2.537004159e+02 1.1e-08 10.21
44 1.7e-05 1.4e-02 1.1e-03 1.00e+00 2.536554497e+02 2.536990747e+02 9.8e-09 11.09
45 1.5e-05 1.3e-02 1.0e-03 1.00e+00 2.536586047e+02 2.536978672e+02 8.9e-09 11.45
46 1.4e-05 1.3e-02 9.1e-04 1.00e+00 2.536614438e+02 2.536967800e+02 8.0e-09 11.92
47 1.2e-05 1.2e-02 8.2e-04 1.00e+00 2.536639986e+02 2.536958012e+02 7.2e-09 11.97
48 1.1e-05 1.2e-02 7.4e-04 1.00e+00 2.536662977e+02 2.536949200e+02 6.5e-09 12.01
49 9.9e-06 1.1e-02 6.6e-04 1.00e+00 2.536683666e+02 2.536941267e+02 5.8e-09 12.06
50 8.9e-06 1.1e-02 6.0e-04 1.00e+00 2.536702284e+02 2.536934125e+02 5.2e-09 12.56
51 8.0e-06 1.0e-02 5.4e-04 1.00e+00 2.536719038e+02 2.536927696e+02 4.7e-09 13.09
52 7.2e-06 1.0e-02 4.8e-04 1.00e+00 2.536734116e+02 2.536921909e+02 4.2e-09 14.19
53 6.5e-06 9.9e-03 4.3e-04 1.00e+00 2.536747686e+02 2.536916699e+02 3.8e-09 14.24
54 5.8e-06 9.6e-03 3.9e-04 1.00e+00 2.536759897e+02 2.536912009e+02 3.4e-09 14.32
55 5.3e-06 9.4e-03 3.5e-04 1.00e+00 2.536770886e+02 2.536907788e+02 3.1e-09 15.20
56 4.7e-06 9.2e-03 3.2e-04 1.00e+00 2.536780776e+02 2.536903988e+02 2.8e-09 15.60
57 4.3e-06 9.0e-03 2.9e-04 1.00e+00 2.536789676e+02 2.536900567e+02 2.5e-09 16.50
58 3.8e-06 8.9e-03 2.6e-04 1.00e+00 2.536797686e+02 2.536897487e+02 2.3e-09 17.95
59 3.4e-06 8.7e-03 2.3e-04 1.00e+00 2.536804894e+02 2.536894716e+02 2.0e-09 18.71
60 3.1e-06 8.6e-03 2.1e-04 1.00e+00 2.536811381e+02 2.536892221e+02 1.8e-09 19.67
61 1.2e-06 3.3e-03 8.1e-05 1.00e+00 2.536846983e+02 2.536878513e+02 7.1e-10 20.21
62 1.1e-06 3.0e-03 7.3e-05 1.00e+00 2.536849266e+02 2.536877643e+02 6.4e-10 21.00
63 3.9e-07 1.1e-03 2.6e-05 1.00e+00 2.536862390e+02 2.536872587e+02 2.3e-10 21.04
64 3.5e-07 9.7e-04 2.4e-05 1.00e+00 2.536863127e+02 2.536872303e+02 2.1e-10 21.12
65 3.2e-07 8.8e-04 2.1e-05 9.99e-01 2.536863789e+02 2.536872048e+02 1.9e-10 21.96
66 2.8e-07 7.9e-04 1.9e-05 1.00e+00 2.536864385e+02 2.536871818e+02 1.7e-10 22.97
67 2.6e-07 7.1e-04 1.7e-05 1.00e+00 2.536864921e+02 2.536871611e+02 1.5e-10 23.24
68 2.3e-07 6.4e-04 1.5e-05 1.00e+00 2.536865404e+02 2.536871425e+02 1.4e-10 23.29
69 2.1e-07 5.7e-04 1.4e-05 9.99e-01 2.536865838e+02 2.536871257e+02 1.2e-10 23.32
70 1.9e-07 5.2e-04 1.3e-05 9.99e-01 2.536866229e+02 2.536871106e+02 1.1e-10 24.57
71 1.7e-07 4.7e-04 1.1e-05 1.00e+00 2.536866581e+02 2.536870970e+02 9.9e-11 25.46
72 1.5e-07 4.2e-04 1.0e-05 1.00e+00 2.536866898e+02 2.536870848e+02 8.9e-11 25.50
73 1.4e-07 3.8e-04 9.1e-06 1.00e+00 2.536867183e+02 2.536870738e+02 8.0e-11 25.52
74 1.2e-07 3.4e-04 8.2e-06 1.00e+00 2.536867440e+02 2.536870638e+02 7.2e-11 25.62
75 1.1e-07 3.1e-04 7.4e-06 1.00e+00 2.536867671e+02 2.536870549e+02 6.5e-11 25.65
76 9.9e-08 2.7e-04 6.7e-06 1.00e+00 2.536867879e+02 2.536870469e+02 5.8e-11 26.17
77 8.9e-08 2.5e-04 6.0e-06 9.99e-01 2.536868066e+02 2.536870396e+02 5.3e-11 27.62
78 8.0e-08 2.2e-04 5.4e-06 1.00e+00 2.536868234e+02 2.536870331e+02 4.7e-11 27.74
79 7.2e-08 2.0e-04 4.9e-06 1.00e+00 2.536868385e+02 2.536870273e+02 4.3e-11 27.80
80 6.5e-08 1.8e-04 4.4e-06 1.00e+00 2.536868521e+02 2.536870220e+02 3.8e-11 27.87
81 5.9e-08 1.6e-04 3.9e-06 9.99e-01 2.536868644e+02 2.536870173e+02 3.5e-11 28.10
82 5.3e-08 1.5e-04 3.5e-06 1.00e+00 2.536868755e+02 2.536870130e+02 3.1e-11 29.45
83 4.8e-08 1.3e-04 3.2e-06 1.00e+00 2.536868855e+02 2.536870091e+02 2.8e-11 29.86
84 4.3e-08 1.2e-04 2.9e-06 9.98e-01 2.536868944e+02 2.536870057e+02 2.5e-11 30.10
85 3.8e-08 1.1e-04 2.6e-06 1.00e+00 2.536869025e+02 2.536870026e+02 2.3e-11 30.56
86 3.5e-08 9.6e-05 2.3e-06 9.96e-01 2.536869097e+02 2.536869998e+02 2.0e-11 31.80
87 3.1e-08 8.6e-05 2.1e-06 9.98e-01 2.536869162e+02 2.536869973e+02 1.8e-11 32.38
88 2.8e-08 7.8e-05 1.9e-06 9.93e-01 2.536869220e+02 2.536869950e+02 1.7e-11 33.86
89 2.5e-08 7.0e-05 1.7e-06 9.96e-01 2.536869273e+02 2.536869930e+02 1.5e-11 34.52
90 2.3e-08 6.3e-05 1.5e-06 9.98e-01 2.536869320e+02 2.536869912e+02 1.3e-11 34.64
91 2.0e-08 5.7e-05 1.4e-06 9.92e-01 2.536869363e+02 2.536869895e+02 1.2e-11 36.01
92 1.8e-08 5.1e-05 1.2e-06 1.01e+00 2.536869402e+02 2.536869880e+02 1.1e-11 36.84
93 1.7e-08 4.6e-05 1.1e-06 9.93e-01 2.536869437e+02 2.536869867e+02 9.8e-12 36.88
94 1.5e-08 4.1e-05 1.0e-06 9.99e-01 2.536869468e+02 2.536869855e+02 8.8e-12 36.95
95 1.3e-08 3.7e-05 9.0e-07 9.97e-01 2.536869495e+02 2.536869844e+02 7.9e-12 38.03
96 1.2e-08 3.3e-05 8.1e-07 9.93e-01 2.536869521e+02 2.536869834e+02 7.1e-12 39.09
97 1.1e-08 3.0e-05 7.3e-07 9.95e-01 2.536869543e+02 2.536869826e+02 6.4e-12 39.14
98 9.8e-09 2.7e-05 6.6e-07 1.01e+00 2.536869565e+02 2.536869817e+02 5.8e-12 39.16
Interior-point optimizer terminated. Time: 39.22.
Optimizer terminated. Time: 39.23
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 2.5368695647e+02 Viol. con: 2e-07 var: 0e+00
Dual. obj: 2.5368698170e+02 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 39.3 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 935
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 935
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.02
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 770
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 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 : 0.03
Factor - nonzeros before factor : 1.64e+04 after factor : 1.45e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.281787446e+05 2.000000000e+00 1.0e+00 0.06
1 1.1e+03 1.4e+03 6.0e+04 -9.71e-01 -1.259414228e+05 3.780941016e+00 4.7e-01 0.76
2 4.6e+02 5.9e+02 2.6e+04 -9.35e-01 -1.205918795e+05 9.868922463e+00 2.0e-01 0.78
3 2.9e+02 3.7e+02 1.6e+04 -8.50e-01 -1.154239527e+05 5.250197663e+01 1.3e-01 0.84
4 2.9e+02 3.7e+02 1.6e+04 -7.62e-01 -1.133019475e+05 1.862130071e+03 1.3e-01 0.88
5 8.3e+01 1.1e+02 4.6e+03 -7.57e-01 -7.812142135e+04 9.031239867e+03 3.6e-02 0.93
6 3.6e+01 4.6e+01 2.0e+03 -2.53e-01 -4.675648511e+04 1.010078026e+04 1.6e-02 1.38
7 1.9e+01 2.4e+01 1.0e+03 2.76e-01 -2.801894100e+04 6.402312541e+03 8.2e-03 1.54
8 9.2e+00 1.2e+01 5.1e+02 6.02e-01 -1.471216448e+04 4.005088022e+03 4.0e-03 2.06
9 5.7e+00 7.3e+00 3.2e+02 8.20e-01 -9.206577478e+03 2.776623636e+03 2.5e-03 2.28
10 1.9e+00 2.4e+00 1.1e+02 9.02e-01 -2.967188192e+03 1.150548899e+03 8.4e-04 2.56
11 1.6e+00 2.0e+00 8.8e+01 9.75e-01 -2.411824742e+03 1.013250409e+03 7.0e-04 2.91
12 1.0e+00 1.4e+00 5.6e+01 9.78e-01 -1.467425485e+03 7.220754945e+02 4.4e-04 3.12
13 4.6e-01 6.8e-01 2.6e+01 9.83e-01 -5.896881228e+02 4.319680952e+02 2.1e-04 4.53
14 2.5e-01 3.8e-01 1.4e+01 1.00e+00 -2.320840438e+02 3.288887895e+02 1.1e-04 5.26
15 1.0e-01 1.6e-01 5.7e+00 1.00e+00 1.044653981e+01 2.360029459e+02 4.6e-05 5.31
16 4.7e-02 1.0e-01 2.7e+00 1.00e+00 9.574907475e+01 2.020284071e+02 2.2e-05 5.44
17 1.0e-02 1.4e-01 6.2e-01 1.01e+00 1.548431163e+02 1.790677307e+02 5.2e-06 6.20
18 6.3e-03 1.0e-01 3.9e-01 1.01e+00 1.614292033e+02 1.765011127e+02 3.2e-06 6.70
19 1.6e-03 1.2e-01 1.0e-01 1.01e+00 1.695627756e+02 1.734405842e+02 8.5e-07 7.49
20 3.4e-04 1.4e-01 2.2e-02 1.01e+00 1.717721237e+02 1.726293361e+02 1.9e-07 7.54
21 1.4e-04 1.0e-01 9.5e-03 9.94e-01 1.721372136e+02 1.725037900e+02 8.3e-08 7.57
22 8.9e-05 8.2e-02 6.0e-03 1.00e+00 1.722347054e+02 1.724653290e+02 5.2e-08 7.63
23 8.0e-05 7.6e-02 5.4e-03 1.00e+00 1.722527902e+02 1.724604212e+02 4.7e-08 8.37
24 7.2e-05 6.9e-02 4.8e-03 1.00e+00 1.722680411e+02 1.724549097e+02 4.2e-08 9.41
25 6.5e-05 6.3e-02 4.3e-03 1.00e+00 1.722818157e+02 1.724499966e+02 3.8e-08 9.83
26 5.9e-05 5.7e-02 3.9e-03 1.00e+00 1.722941841e+02 1.724455455e+02 3.4e-08 9.93
27 5.3e-05 5.2e-02 3.5e-03 1.00e+00 1.723053032e+02 1.724415268e+02 3.1e-08 11.17
28 4.7e-05 4.8e-02 3.2e-03 1.00e+00 1.723152953e+02 1.724378950e+02 2.8e-08 11.93
29 4.3e-05 4.4e-02 2.8e-03 1.00e+00 1.723242746e+02 1.724346129e+02 2.5e-08 12.09
30 3.8e-05 4.0e-02 2.6e-03 1.00e+00 1.723323436e+02 1.724316468e+02 2.2e-08 12.13
31 3.5e-05 3.7e-02 2.3e-03 1.00e+00 1.723395949e+02 1.724289667e+02 2.0e-08 12.19
32 3.1e-05 3.4e-02 2Build was aborted
Cloning into 'solar'...
/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/jenkins3442355128258613857.sh: line 101: 44523 Terminated: 15 python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True)"
INFO: Starting to record.
INFO: Processing JUnit
INFO: [JUnit] - 5 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 ABORTED
INFO: Stopping recording.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: ABORTED