Started by upstream project "gpkit_PullRequest_Models" build number 402
originally caused by:
GitHub pull request #1429 of commit 88b46886deef3bf74587f14704b52108dca7ae93, no merge conflicts.
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on macys in workspace /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek
No credentials specified
Wiping out workspace first.
Cloning the remote Git repository
Cloning repository https://github.com/convexengineering/gpkit
> git init /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek # timeout=10
Fetching upstream changes from https://github.com/convexengineering/gpkit
> git --version # timeout=10
> git fetch --tags --progress https://github.com/convexengineering/gpkit +refs/heads/*:refs/remotes/origin/* # timeout=10
> git config remote.origin.url https://github.com/convexengineering/gpkit # timeout=10
> git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10
> git config remote.origin.url https://github.com/convexengineering/gpkit # timeout=10
Fetching upstream changes from https://github.com/convexengineering/gpkit
> git fetch --tags --progress https://github.com/convexengineering/gpkit +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master # timeout=10
Merging Revision 41ae9e4371d3a6e0e99433752ef71ae4749e78b6 (refs/remotes/origin/pr/1429/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='DEFAULT', fastForwardMode='FF'}
> git rev-parse origin/master^{commit} # timeout=10
> git config core.sparsecheckout # timeout=10
> git checkout -f origin/master # timeout=3
> git merge --ff 41ae9e4371d3a6e0e99433752ef71ae4749e78b6 # timeout=10
> git rev-parse HEAD^{commit} # timeout=10
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> git show-ref --tags -d # timeout=10
Checking out Revision 41ae9e4371d3a6e0e99433752ef71ae4749e78b6 (origin/pr/1429/merge, origin/master)
> git config core.sparsecheckout # timeout=10
> git checkout -f 41ae9e4371d3a6e0e99433752ef71ae4749e78b6 # timeout=3
Commit message: "Merge 88b46886deef3bf74587f14704b52108dca7ae93 into a96e0a00db0411574831cfe3a1d4dfb8889510b5"
Using 'Changelog to branch' strategy.
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[description-setter] Description set: PR 1429: remove ctyespgen dependency
[Execution node] check if [macys] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[mosek] $ /bin/bash -xe /var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/jenkins12606903914175171389.sh
+ [[ macys == *macys* ]]
+ export PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
+ PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
+ virtualenv --system-site-packages /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit
New python executable in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/python
Installing setuptools, pip, wheel...done.
+ . /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/activate
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ '[' -n /bin/bash ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH
++ '[' -z '' ']'
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ '[' x '!=' x ']'
+++ basename /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit
++ PS1='(venv2_gpkit) '
++ export PS1
++ alias pydoc
++ '[' -n /bin/bash ']'
++ hash -r
++ which pip
+ export PIP=/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip
+ PIP=/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip
+ pip_install pip
+ python /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade pip
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Requirement already up-to-date: pip in ./venv2_gpkit/lib/python2.7/site-packages (19.2.3)
+ [[ macys == *reynolds* ]]
+ [[ macys == *macys* ]]
+ [[ mosek == mosek ]]
+ [[ macys == macys ]]
+ export PATH=/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin
+ PATH=/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin
+ export DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin
+ DYLD_LIBRARY_PATH=:/Users/jenkins/mosek/8/tools/platform/osx64x86/bin
+ python /Users/jenkins/mosek/8/tools/platform/osx64x86/python/2/setup.py install
running install
running build
running build_py
running build_ext
copying mosek/_msk.so -> build/lib.macosx-10.13-intel-2.7/mosek
copying mosek/fusion/impl/fragments.so -> build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl
running install_lib
creating /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying build/lib.macosx-10.13-intel-2.7/mosek/__init__.py -> /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
copying build/lib.macosx-10.13-intel-2.7/mosek/_msk.so -> /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek
creating /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/__init__.py -> /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
creating /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl
copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl/__init__.py -> /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl
copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl/_implementation.py -> /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl
copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/impl/fragments.so -> /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl
copying build/lib.macosx-10.13-intel-2.7/mosek/fusion/Utils.py -> /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion
byte-compiling /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/__init__.py to __init__.pyc
byte-compiling /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/__init__.py to __init__.pyc
byte-compiling /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl/__init__.py to __init__.pyc
byte-compiling /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/impl/_implementation.py to _implementation.pyc
byte-compiling /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/Utils.py to Utils.pyc
running install_egg_info
Writing /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/Mosek-8.1.41-py2.7.egg-info
Fixing library paths
copying /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib -> /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/
copying /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libcilkrts.5.dylib -> /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/
+ [[ mosek == cvxopt ]]
+ [[ mosek == mosek ]]
+ python -c '__import__("mosek").Env()'
+ msktestlic
Mosek license manager: License path: /Users/jenkins/mosek/mosek.lic
Mosek license manager: Checkout license feature 'PTS' from flexlm.
Mosek license manager: Checkout time 0.01. r: 0 status: 0
Problem
Name :
Objective sense : min
Type : LO (linear optimization problem)
Constraints : 1
Cones : 0
Scalar variables : 5000
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Eliminator started.
Freed constraints in eliminator : 0
Eliminator terminated.
Eliminator - tries : 1 time : 0.00
Lin. dep. - tries : 0 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.00
Optimizer terminated. Time: 0.00
************************************
A license was checked out correctly.
************************************
+ export 'GPKITSOLVERS=mosek, mosek_cli'
+ GPKITSOLVERS='mosek, mosek_cli'
+ [[ mosek == cvxopt ]]
+ pip_install xmlrunner
+ python /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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
ERROR: matplotlib 1.3.1 requires nose, which is not installed.
ERROR: matplotlib 1.3.1 requires tornado, which is not installed.
Installing collected packages: numpy
Found existing installation: numpy 1.8.0rc1
Not uninstalling numpy at /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python, outside environment /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit
Can't uninstall 'numpy'. No files were found to uninstall.
Successfully installed numpy-1.16.5
+ pip_install scipy
+ python /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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
Found existing installation: scipy 0.13.0b1
Not uninstalling scipy at /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python, outside environment /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit
Can't uninstall 'scipy'. No files were found to uninstall.
Successfully installed scipy-1.2.2
+ pip_install ctypesgen
+ python /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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
Using cached https://files.pythonhosted.org/packages/77/e8/73c5636dd329bcb781e3fc8762342ce4c543c279ceab9eeb06f3f2a4b241/ctypesgen-1.0.0.post4-py2.py3-none-any.whl
Installing collected packages: ctypesgen
Successfully installed ctypesgen-1.0.0.post4
+ pip_install pandas
+ python /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade pandas
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting pandas
Using cached https://files.pythonhosted.org/packages/52/ff/912fe03a623a70bcf297d466013a0b4f4c68c3b60f86bf226682d061fc09/pandas-0.24.2-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl
Collecting python-dateutil>=2.5.0 (from pandas)
Using cached https://files.pythonhosted.org/packages/41/17/c62faccbfbd163c7f57f3844689e3a78bae1f403648a6afb1d0866d87fbb/python_dateutil-2.8.0-py2.py3-none-any.whl
Requirement already satisfied, skipping upgrade: numpy>=1.12.0 in ./venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5)
Requirement already satisfied, skipping upgrade: pytz>=2011k in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from pandas) (2013.7)
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
ERROR: matplotlib 1.3.1 requires nose, which is not installed.
ERROR: matplotlib 1.3.1 requires tornado, which is not installed.
Installing collected packages: six, python-dateutil, pandas
Found existing installation: six 1.4.1
Not uninstalling six at /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python, outside environment /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit
Can't uninstall 'six'. No files were found to uninstall.
Found existing installation: python-dateutil 1.5
Not uninstalling python-dateutil at /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python, outside environment /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit
Can't uninstall 'python-dateutil'. No files were found to uninstall.
Successfully installed pandas-0.24.2 python-dateutil-2.8.0 six-1.12.0
+ pip_install matplotlib
+ python /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade matplotlib
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting matplotlib
Using cached https://files.pythonhosted.org/packages/3e/d6/4c949597c4186599cc8be08cd11b1e83fe7966676aeee3868bf3e581d852/matplotlib-2.2.4-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl
Collecting kiwisolver>=1.0.1 (from matplotlib)
Using cached https://files.pythonhosted.org/packages/0d/15/ec5f70ac79f378ed0ef5ed8b71e8a04e382115426b2cda9a3ab5ffcf467f/kiwisolver-1.1.0-cp27-cp27m-macosx_10_6_intel.macosx_10_9_intel.macosx_10_9_x86_64.macosx_10_10_intel.macosx_10_10_x86_64.whl
Collecting cycler>=0.10 (from matplotlib)
Using cached https://files.pythonhosted.org/packages/f7/d2/e07d3ebb2bd7af696440ce7e754c59dd546ffe1bbe732c8ab68b9c834e61/cycler-0.10.0-py2.py3-none-any.whl
Collecting subprocess32 (from matplotlib)
Using cached https://files.pythonhosted.org/packages/35/f3/7cdeeef9cb05c42fadcc8aa040dd3b80d94e0f6a8dedc4bacebf796c2385/subprocess32-3.5.4-cp27-cp27m-macosx_10_6_intel.whl
Requirement already satisfied, skipping upgrade: pytz in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from matplotlib) (2013.7)
Requirement already satisfied, skipping upgrade: six>=1.10 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.12.0)
Collecting backports.functools-lru-cache (from matplotlib)
Using cached https://files.pythonhosted.org/packages/03/8e/2424c0e65c4a066e28f539364deee49b6451f8fcd4f718fefa50cc3dcf48/backports.functools_lru_cache-1.5-py2.py3-none-any.whl
Requirement already satisfied, skipping upgrade: numpy>=1.7.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.16.5)
Requirement already satisfied, skipping upgrade: pyparsing!=2.0.4,!=2.1.2,!=2.1.6,>=2.0.1 in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from matplotlib) (2.0.1)
Requirement already satisfied, skipping upgrade: python-dateutil>=2.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2.8.0)
Requirement already satisfied, skipping upgrade: setuptools in ./venv2_gpkit/lib/python2.7/site-packages (from kiwisolver>=1.0.1->matplotlib) (39.0.1)
Installing collected packages: kiwisolver, cycler, subprocess32, backports.functools-lru-cache, matplotlib
Found existing installation: matplotlib 1.3.1
Not uninstalling matplotlib at /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python, outside environment /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit
Can't uninstall 'matplotlib'. No files were found to uninstall.
Successfully installed backports.functools-lru-cache-1.5 cycler-0.10.0 kiwisolver-1.1.0 matplotlib-2.2.4 subprocess32-3.5.4
+ pip_install ad
+ python /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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 future
+ python /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --upgrade future
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting future
Installing collected packages: future
Successfully installed future-0.17.1
+ export GPKITBUILD=/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/build_gpkit
+ GPKITBUILD=/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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
+ python /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek
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 -c 'from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True)'
No filename given.
Usage:
mskexpopt FILENAME [-primal] [-dual] [-p parameterfile]
Return code: 1052
Description: MSK_RES_ERR_FILE_OPEN [An error occurred while opening a file.]
...................................................................................................................................................................................................................................................
----------------------------------------------------------------------
Ran 243 tests in 17.306s
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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/gplibrary
Installing collected packages: gpkitmodels
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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/robust
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek (from robust==0.0.0) (0.9.1.0)
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from robust==0.0.0) (1.16.5)
Requirement already satisfied: matplotlib in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from robust==0.0.0) (2.2.4)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->robust==0.0.0) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->robust==0.0.0) (1.12.0)
Requirement already satisfied: kiwisolver>=1.0.1 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (1.1.0)
Requirement already satisfied: cycler>=0.10 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (0.10.0)
Requirement already satisfied: subprocess32 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (3.5.4)
Requirement already satisfied: pytz in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from matplotlib->robust==0.0.0) (2013.7)
Requirement already satisfied: backports.functools-lru-cache in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (1.5)
Requirement already satisfied: pyparsing!=2.0.4,!=2.1.2,!=2.1.6,>=2.0.1 in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from matplotlib->robust==0.0.0) (2.0.1)
Requirement already satisfied: python-dateutil>=2.1 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from matplotlib->robust==0.0.0) (2.8.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from kiwisolver>=1.0.1->matplotlib->robust==0.0.0) (39.0.1)
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=218188 sha256=fd6d02caf29c65b10eb5acbbb8ff066ad17d59946650285e9ae848c5f1e6853d
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-lA0hPG/wheels/71/b1/d7/ddc0739b90757010d4d803ce99aff9322d53a77207baac1a9f
Successfully built robust
Installing collected packages: robust
Successfully installed robust-0.0.0
Running tests...
----------------------------------------------------------------------
................
----------------------------------------------------------------------
Ran 16 tests in 7.262s
OK
.................
----------------------------------------------------------------------
Ran 16 tests in 13.575s
OK
.
----------------------------------------------------------------------
Ran 2 tests in 21.058s
OK
Generating XML reports...
adding test for 'run_tests.py'
Cloning into 'shopping'...
Running tests...
----------------------------------------------------------------------
...
----------------------------------------------------------------------
Ran 3 tests in 0.175s
OK
Generating XML reports...
adding test for 'test.py'
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.011 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.00976 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.0743 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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.8.0)
Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5)
Requirement already satisfied: pytz>=2011k in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from pandas) (2013.7)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0)
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting git+https://github.com/hoburg/gpfit.git
Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-Xg4csZ
Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-Xg4csZ
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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=5a672c6ed605d38bb59122397e9f412790978943c77cc3808e85ccc2f83f7fb5
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-0ZdbBY/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/gassolar
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek (from gassolar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.12.0)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.8.0)
Requirement already satisfied: pytz>=2011k in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from pandas->gassolar==0.0.0.0) (2013.7)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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=0030c292e1845c93116679ffeec06263d9e889a89b669996bcd4f212ccb163e5
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-QyT5Wi/wheels/19/67/be/e67706cd5c57d9b18406a59a938edbc76dffdb4f94d5edae48
Successfully built gassolar
Installing collected packages: gassolar
Successfully installed gassolar-0.0.0.0
Running tests...
----------------------------------------------------------------------
/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
tau = np.exp(-0.175/costhsun)
..
----------------------------------------------------------------------
Ran 4 tests in 16.105s
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 0.0587 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 0.312 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 0.0559 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 0.309 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 0.303 seconds.
Warning: Variable Mission.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.3538 but bound is 150000.0000
Warning: Variable Mission.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.3827 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 1.33 seconds.
Warning: Variable Mission1.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103379.4301 but bound is 150000.0000
Warning: Variable Mission1.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103406.0835 but bound is 150000.0000
Using solver 'mosek_cli'
Solving for 1250 variables.
Solving took 0.268 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 1.68 seconds.
Warning: Variable Mission1.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103379.2971 but bound is 150000.0000
Warning: Variable Mission1.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103406.1793 but bound is 150000.0000
Cloning into 'jho'...
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Requirement already satisfied: pandas in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.8.0)
Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5)
Requirement already satisfied: pytz>=2011k in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from pandas) (2013.7)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0)
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting git+https://github.com/hoburg/gpfit.git
Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-h2lBwf
Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-h2lBwf
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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=3d9d0d0457a26e0618185e1cc47bf3be9c57ecb6918da8988cd57cef184afd9c
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-qDajxV/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
Running tests...
----------------------------------------------------------------------
/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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 17.391s
OK
Generating XML reports...
adding test for 'model/jho.py'
adding test for 'model/print_perf.py'
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.2566195913693567e-13.
Solving took 4 GP solves and 0.702 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.269612e-13.
Solving took 4 GP solves and 1.1 seconds.
Allowing negative dual variable(s) as small as -6.193960275235888e-13.
Allowing negative dual variable(s) as small as -1.3846424549469882e-13.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.626
design loiter speed [m/s] = 25.071
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.3846424549469882e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.356
optimum loiter speed for min power, end of loiter [m/s] = 25.000
optimum cruise speed, inbound [m/s] = 25.637
optimum cruise speed, outbound [m/s] = 36.421
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.171202259721421e-12.
Solving took 4 GP solves and 0.989 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 0.551 seconds.
Max payload weight [lbf] = 28.242
Max take off weight [lbf] = 166.638
Allowing negative dual variable(s) as small as -6.188938e-13.
Allowing negative dual variable(s) as small as -1.385335e-13.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.626
design loiter speed [m/s] = 25.071
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.385335e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.356
optimum loiter speed for min power, end of loiter [m/s] = 25.000
optimum cruise speed, inbound [m/s] = 25.637
optimum cruise speed, outbound [m/s] = 36.421
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.171066e-12.
Solving took 4 GP solves and 1.17 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 0.872 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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/turbofan
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.9)
Requirement already satisfied: future in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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=857b13b28f2341c7ff422b9340ed4a86d833f85b9aa1bc3c6ede3a3c94d02d46
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-X1iAOS/wheels/21/f3/3d/fc4b7a73fe968cb3e78bf516133a76d35546734c8e11a00fb8
Successfully built turbofan
Installing collected packages: turbofan
Successfully installed turbofan-0.0.0.0
Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 0.893s
OK
Generating XML reports...
adding test for 'turbofan/engine_test.py'
Beginning signomial solve.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.027 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0188 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0248 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.025 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0211 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0216 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0225 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0205 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0206 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0227 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0206 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0199 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.0254 seconds.
Solving took 13 GP solves and 0.617 seconds.
Cloning into 'SPaircraft'...
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting git+https://github.com/hoburg/turbofan.git
Cloning https://github.com/hoburg/turbofan.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-O1ki74
Running command git clone -q https://github.com/hoburg/turbofan.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-O1ki74
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.9)
Requirement already satisfied: future in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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=5adc91e64d3e0c9a90e88a09df1d2ebbcd7ad0283fbaf38bb2c2d7b4542b2f00
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-xdrJtg/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/SPaircraft
Requirement already satisfied: turbofan in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek (from SPaircraft==0.0.0) (0.9.1.0)
Requirement already satisfied: pint in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan->SPaircraft==0.0.0) (0.9)
Requirement already satisfied: future in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan->SPaircraft==0.0.0) (0.17.1)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan->SPaircraft==0.0.0) (1.2.2)
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan->SPaircraft==0.0.0) (1.16.5)
Requirement already satisfied: ad in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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=739ed4597ba6d2c3fb0722096182b4cd935c26206de87e48c257774b7d56be10
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-UrZZqr/wheels/01/56/88/5015f23f591bf3e1fd1a2acbd8d5d87f556ad5377f941ac33c
Successfully built SPaircraft
Installing collected packages: SPaircraft
Successfully installed SPaircraft-0.0.0
Running tests...
----------------------------------------------------------------------
adding test for 'SPaircraft.py'
Mission
=======
Cost
----
W_{f_{total}}[:].sum()
Constraints
-----------
W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin}
PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:])
x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:])
x_{CG}[3] <= \Delta x_n + x_n
\Delta x_m + x_{CG}[3] >= x_m
\tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m
C_{D_{fuse}}[:] = 0.018081
M_{fuseD} = 0.72
W_{start}[0] = W_{total}[:]
W_{start}[:] >= W_{end}[:] + W_{burn}[:]
W_{start}[1:] = W_{end}[:4]
W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1]
W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2]
W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1]
hft[2] >= CruiseAlt
hft[1:5] = hft[:4] + dhft[1:5]
hft[0] = dhft[0]
dhft[1:3] = dhft[:2]
RC[0] >= 2.5e+03
RC[:3] >= RC_{min}[:3]
\theta[2] >= 0.015
hft[2] >= MinCruiseAlt
n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:]
R_{segment}[3:4] = R_{segment}[4:5]
M[3:5] >= M_{min}
0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req}
Fsafetyfac*F[0] = T_e
W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:]
V_2[:] = M_2[:]*a[:]
\alpha_{max,w}[:3] = 0.18
\alpha_{max,w}[3:] = 0.1
0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime
0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime
ClimbTime <= MaxClimbTime
T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}}
F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
OPR[:] <= OPR_{max}
Aircraft
Fuselage
W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on}
W_{pass}[:] >= n_{pass}[:]*W_{avg. pass}
W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo}
W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}}
W_{payload}[:] <= W_{payload_{max}}
n_{pass}[:] <= n_{seat}
n_{rows} = n_{seat}/SPR
l_{shell} = n_{rows}*p_s
\theta_{db} = w_{db}/R_{fuse}
R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db}
A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db}
(PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse}
A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin}
w_{floor} = w_{fuse}
R_{fuse} + w_{db} >= w_{fuse}
h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse}
t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell}
S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2
S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2
l_{fuse} = l_{nose} + l_{shell} + l_{cone}
l_{cone} = R_{fuse}/\lambda_{cone}
x_{shell1} = l_{nose}
x_{shell2} >= l_{nose} + l_{shell}
t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin}
t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin}
\sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell})
\sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin}
l_{floor} >= l_{shell} + 2*R_{fuse}
P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat})
A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor}
V_{floor} = 2*w_{floor}*A_{floor}
W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor}
\tau_{cone} = \sigma_{skin}
W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame})
x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone}
-2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}}
(PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}}
x_{hbend_{Land}} >= x_{wing}
x_{hbend_{Land}} <= l_{fuse}
x_{hbend_{MLF}} >= x_{wing}
x_{hbend_{MLF}} <= l_{fuse}
A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}})
A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}})
A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
A_{2h_{MLF}} >= Mission.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2)
A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}}
A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}}
A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}}
A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}}
A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}}
A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}}
A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}}
A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}}
V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission.Aircraft.Fuselage.r_{w/c}
V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission.Aircraft.Fuselage.r_{w/c}
V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}}
W_{hbend} >= g*\rho_{bend}*V_{hbend}
x_{vbend} >= x_{wing}
x_{vbend} <= l_{fuse}
B_{0v} = B_{1v}*(x_{tail} - x_{vbend})
B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2)
B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}}
0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}}
V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission.Aircraft.Fuselage.r_{w/c}
V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}}
W_{vbend} >= \rho_{bend}*g*V_{vbend}
x_f = x_{wing} + 0.5*c_0*Mission.Aircraft.Fuselage.r_{w/c}
x_b = x_{wing} - 0.5*c_0*Mission.Aircraft.Fuselage.r_{w/c}
\sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h}
\sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v}
V_{cyl} = A_{skin}*l_{shell}
V_{nose} = S_{nose}*t_{skin}
V_{bulk} = S_{bulk}*t_{skin}
V_{db} = A_{db}*l_{shell}
V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse})
W_{apu} = W_{payload_{max}}*f_{apu}
W_{db} = \rho_{skin}*g*V_{db}
W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk})
W_{window} >= W'_{window}*l_{shell}
W_{padd} = W_{payload_{max}}*f_{padd}
W_{seat} >= W'_{seat}*n_{seat}
W_{seat} >= f_{seat}*W_{payload_{max}}
W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk})
W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db}
W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone})
Wing
WingNoStruct
A_{rect} = c_{tip}*b
0.5*(1 - \lambda)*c_{root}*b <= A_{tri}
p >= 1 + 2*\lambda
2*q >= 1 + p
y_{mac} = b/3*q/p
mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q
\lambda = c_{tip}/c_{root}
S = b*(c_{root} + c_{tip})/2
0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w)
e*(1 + f(\lambda_w)*AR) <= 1
\lambda >= 0.15
V_{fuel, max} <= 0.303*mac^2*b*\tau
W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g
b <= b_{max}
WingBox
AR = b^2/S
0.423*Mission.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5)
\tau <= \tau_{max_w}
W_{struct} >= W_{web} + W_{cap}
AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= 8*\rho_{cap}*g*Mission.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5)
Mission.Aircraft.Wing.WingBox.N_{lift} = 3
Mission.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8
\lambda = taper
W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt})
0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}}
Engine
Compressor
(no constraints)
Combustor
(no constraints)
Turbine
(no constraints)
Thrust
(no constraints)
FanMap
(no constraints)
LPCMap
(no constraints)
HPCMap
(no constraints)
Sizing
A_{2} >= A_{5} + A_{7}
FlightState
V[:] = V[:]
a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
V[:] = M[:]*a[:]
Altitude
h[:] = hft[:]
Atmosphere
(P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
\rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
\mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
EnginePerformance
CompressorPerformance
T_{t_0}[:] = T_{atm}[:]/c1[:]^-1
h_{t_0}[:] = C_{p_{air}*T_{t_0}[:]
P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:]
T_{t_{1.8}}[:] = T_{t_0}[:]
h_{t_{1.8}}[:] = h_{t_0}[:]
P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5
T_{T_{2}}[:] = T_{t_{1.8}}[:]
h_{T_{2}}[:] = h_{t_{1.8}}[:]
P_{T_{2}}[:] = P_{t_{1.8}}[:]
P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:]
T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016
h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:]
P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:]
T_{t_7}[:] = T_{t_{2.1}}[:]
h_{t_7}[:] = h_{t_{2.1}}[:]
P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:]
T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152
h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1}
P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:]
T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491
h_{t_3}[:] = C_{p_{2}*T_{t_3}[:]
CombustorPerformance
h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:]
h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:]
fp1[:] = f[:] + 1
M_{4a}[:] = 0.1025
fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5
T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]]
P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891
u_{4a}[:] = M_{4a}[:]*(1.31*Mission.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a}
u_c[:] = r_{uc}*u_{4a}[:]
P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891
TurbinePerformance
h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:]
P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:]
\pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565
h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:]
P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:]
T_{t_5}[:] = T_{t_{4.9}}[:]
h_{t_5}[:] = h_{t_{4.9}}[:]
ThrustPerformance
P_{8}[:] = P_{atm}[:]
h_{8}[:] = C_{p_{fex}*T_{8}[:]
u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:]
(P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:]
h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:]
P_{6}[:] = P_{atm}[:]
(P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:]
u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:]
h_6[:] = C_{p_{tex}*T_{6}[:]
h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:]
\alpha[:] = m_{fan}[:]/m_{core}[:]
\alpha_{+1}[:] = \alpha[:] + 1
\alpha[:] <= \alpha_{max}
F[:] <= F_{6}[:] + F_{8}[:]
F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:])
TSFC[:] = 1/I_{sp}[:]
F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:]
FanMapPerformance
m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}}
LPCMapPerformance
m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D}
HPCMapPerformance
m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D}
SizingPerformance
P_{7}[:] >= P_{atm}[:]
M_7[:] <= 1
a_{7}[:] = (1.4*Mission.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5
a_{7}[:]*M_7[:] = u_{7}[:]
\rho_7[:] = P_{7}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{7}[:])
P_{5}[:] >= P_{atm}[:]
M_5[:] <= 1
a_{5}[:] = (1.39*Mission.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5
a_{5}[:]*M_5[:] = u_{5}[:]
\rho_5[:] = P_{5}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{5}[:])
h_{2}[:] = C_{p_{1}*T_{2}[:]
\rho_{2}[:] = P_{2}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{2}[:])
u_{2}[:] = M_2[:]*(C_{p_{1}*Mission.Aircraft.Engine.EngineConstants.R*T_{2}[:]/781)^0.5
h_{2.5}[:] = C_{p_{2}*T_{2.5}[:]
\rho_{2.5}[:] = P_{2.5}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{2.5}[:])
u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/781)^0.5
m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine}
d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5
d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5
\eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]])
h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:]
P_{t_4}[:] = \pi_{b}*P_{t_3}[:]
M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]]
M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]])
P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:]
\pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013
\pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10
\pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10
\pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10
m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
\pi_{f}[:] >= 1
\pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10
\pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10
\pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10
\pi_{lc}[:] >= 1
m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
\pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10
\pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10
\pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10
m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref})
\pi_{hc}[:] >= 1
OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:]
P_{t_8}[:] = P_{t_7}[:]
T_{t_8}[:] = T_{t_7}[:]
P_{t_6}[:] = P_{t_5}[:]
T_{t_6}[:] = T_{t_5}[:]
F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:]
I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g)
N_{f}[:]*G_{f} = N_{1}[:]
N_{1}[:] <= 1.1
N_{2}[:] <= 1.1
fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD}
fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD}
P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5
(T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2
P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979
(T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2
M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:]
m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:]
m_{total}[:] = m_{fan}[:] + m_{core}[:]
P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512
T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1
m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2}
P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857
T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1
m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5}
1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD}
0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD}
1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD}
0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD}
m_{lc_D} >= 0.7*m_{coreD}/0.649
m_{lc_D} <= 1.3*m_{coreD}/0.649
m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23
m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23
\bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405
\bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405
F[:] = F_{spec}[:]
T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}}
OPR[:] <= OPR_{max}
VerticalTail
VerticalTailNoStruct
C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}}
L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}}
c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt}))
A_{vt} = b_{vt}^2/S_{vt}
b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt}
p_{vt} >= 1 + 2*\lambda_{vt}
2*q_{vt} >= 1 + p_{vt}
y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt}
\lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}}
\Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}}
\Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt}
\lambda_{vt} >= 0.25
V_{vt} >= V_{vt_{min}}
WingBox
AR_{vt} = (2*b_{vt})^2/(2*S_{vt})
0.423*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
\tau_{vt} <= 0.14
W_{struct} >= 0.5*(W_{web} + W_{cap})
Mission.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24
AR_{vt}*2*L_{vt_{max}}*Mission.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= 8*\rho_{cap}*g*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
Mission.Aircraft.VerticalTail.WingBox.N_{lift} = 1
Mission.Aircraft.VerticalTail.WingBox.N_{lift}*Mission.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8
\lambda_{vt} = taper
W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT})
HorizontalTail
HorizontalTailNoStruct
\Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht}
\Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}}
p_{ht} >= 1 + 2*\lambda_{ht}
2*q_{ht} >= 1 + p_{ht}
y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht}
0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht}
\lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}}
S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2
0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht})
e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1
AR_{ht} = b_{ht}^2/S_{ht}
\lambda_{ht} >= 0.2
\lambda_{ht} <= 1
WingBox
AR_{ht} = b_{ht}^2/S_{ht}
0.423*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
\tau_{ht} <= 0.14
W_{struct} >= W_{web} + W_{cap}
L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2
L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht})
2*AR_{ht}*L_{shear}*Mission.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
Mission.Aircraft.HorizontalTail.WingBox.N_{lift} = 1
Mission.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8
L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht}
L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}}
W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht})
LandingGear
l_n + z_{wing} + y_m*\tan(\gamma) >= l_m
T = 2*y_m
x_m >= x_n + B
x_n >= 5
\tan(\phi) = \tan(\phi_{min})
(z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1
\tan(\psi) <= \tan(\psi_{max})
x_{up} - x_m <= l_m/\tan(\theta_{max})
y_m >= l_m
S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG})
l_{oleo} = 2.5*S_{sa}
d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5
l_m >= l_{oleo} + d_{t_m}/2
F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in])
W_{wa,m} = 1.2*F_{w_m}^0.609
F_{w_n} = L_{w_n}*d_{t_n}/1e+03
W_{wa,n} = 1.2*F_{w_n}^0.609
L_{w_m} = L_m/(n_{mg}*n_{wps})
L_{w_n} = L_n/n_{wps}
d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315
w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48
d_{t_n} = 0.8*d_{t_m}
w_{t_n} = 0.8*w_{t_m}
W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g
N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m
W_{mw} = n_{wps}*W_{wa,m}
W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g
\sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}})
W_{nw} >= n_{wps}*W_{wa,n}
L_m <= 9.87*E*I_m/(K*l_m)^2
I_m = PI*r_m^3*t_m
L_n <= 9.87*E*I_n/(K*l_n)^2
I_n = PI*r_n^3*t_n
2*r_m/t_m <= 40
2*r_m/t_n <= 40
h_{hold} >= 2*w_{t_m} + 2*r_m
0.8 >= 2*w_{t_n} + 2*r_n
W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m}))
W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n})
W_{lg} >= C_{lg}*(W_{mg} + W_{ng})
W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m
x_m >= x_{CG_{lg}}
c_{root} = c_0
Mission.Aircraft.Wing.WingBox.r_{w/c} = Mission.Aircraft.Fuselage.r_{w/c}
x_w = x_{wing}
Mission.Aircraft.Fuselage.N_{lift} = Mission.Aircraft.Wing.WingBox.N_{lift}
f_{L_{total/wing}}*L_{max} >= Mission.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}}
W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc}
W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:]
W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:]
W_{total}[:] <= W_{total, max}
f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}}
W_{misc} >= W_{lg} + W_{hpesys}
W_{hpesys} = f_{hpesys}*W_{total, max}
x_n <= l_{nose}
x_m >= x_{wing}
\Delta x_{AC_{wing}} + x_{wing} >= x_m
x_{hpesys} = 1.1*l_{nose}
x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys}
d_{nacelle} >= d_{f} + 2*t_{nacelle}
E_{land} >= W_{total, max}/(2*g)*w_{ult}^2
x_{up} = x_{shell2}
L_n = W_{total, max}*\Delta x_m/B
L_m = W_{total, max}*\Delta x_n/B
L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max}
y_{eng} >= y_m
3*n_{vt}*Mission.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}}
V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse}
W_{tail} >= n_{vt}*W_{vt} + W_{ht}
2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db}
B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v})
m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht}
x_{CG_{ht}} <= l_{fuse}
V_{ht} = S_{ht}*l_{ht}/(S*mac)
L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}}
L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}}
x_{CG_{vt}} <= l_{fuse}
V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b)
n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max}
n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng}
D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}}
I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:]
I_{z}[:] <= I_{z, max}
S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2
l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}}
f_{S_{nacelle}} = S_{nacelle}*S^-1
A_{inlet} = 0.4*S_{nacelle}
A_{fancowl} = 0.2*S_{nacelle}
A_{exh} = 0.4*S_{nacelle}
A_{corecowl} = 3PI*d_{LPC}^2
W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl})
W_{eadd} = f_{eadd}*W_{engine}
W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon}
W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine})
y_{eng} = 0.5*w_{fuse}
(L_{max} - Mission.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission.Aircraft.Wing.WingBox.M_r*c_{root}
A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend})
A_{1h_{MLF}} >= (Mission.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h})
I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16)
I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81
I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81)
x_{shell2} + l_{cone} >= x_{eng}
x_{eng} >= x_{shell2} + 0.75*l_{cone}
S_{floor} = 0.312*P_{floor}
M_{floor} = 0.0352*P_{floor}*w_{floor}
\Delta R_{fuse} = R_{fuse}*0.43/1.75
b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2
b_{ht_{out}} = 0.5*b_{ht} - w_{fuse}
L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}}
M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}}
L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}}
c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach}
\pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht})
FlightSegment
FlightState
V[:] = V[:]
a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
V[:] = M[:]*a[:]
Altitude
h[:] = hft[:]
Atmosphere
(P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
\rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
\mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
FlightP
P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:]
RC[:] = P_{excess}[:]/W_{avg}[:]
\theta[:]*V[:] = RC[:]
dhft[:] = tmin[:]*RC[:]
R_{segment}[:] = thr[:]*V[:]
WingPerformance
0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:]
\Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:]
\Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2
(AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2
C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:]
\alpha_w[:] <= \alpha_{max,w}[:]
D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:]
C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:]
C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR)
Re_w[:] = \rho[:]*V[:]*mac/\mu[:]
C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114
FuselagePerformance
(no constraints)
VerticalTailPerformance
D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:]
Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:]
C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577
HorizontalTailPerformance
L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:]
C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:]
\alpha_{ht}[:] <= \alpha_{ht,max}
C_{L_{\alpha,ht_0}}[:] = 6.28
D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:]
C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht})
Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:]
C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852
W_{burn}[:] = W_{burn}[:]
F_{fuel}[:] = F_{fuel}[:]
\rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:])
P_{cabin}[:] = 7.5e+04
T_{cabin}[:] = 297
V[:] >= V_{stall}[:]
W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:]
tmin[:] = thr[:]
L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:]
L_{total}[:] = f_{L_{total/wing}}*L_w[:]
L_{total}[:] >= W_{avg}[:] + L_{ht}[:]
D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2
D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:])
C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S)
L/D[:] = W_{avg}[:]/D[:]
W_{Load}[:] <= W_{Load_{max}}[:]
W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S
p_{o}[:] >= L_w[:]*c_{root}/S
\eta_{o}[:] = w_{fuse}/(b/2)
x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:]
c_{m_{w}}[:] = 1.9
x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2)
x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse}
x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}}
x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}}
C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht}
AR_{ht} >= 4
C_{L_{ht}}[:] >= 0.01
SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac
SM[:] >= SM_{min}
SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}}
x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:]
R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:]
C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2
V_{nacelle}[:] = r_{v_{nacelle}}*V[:]
V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]]
r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0)
C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0
D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S
\Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}}
M_2[:3] = M[:3]
M_{2.5}[:3] = 0.6
hold_{2}[:3] = 1.07164
hold_{2.5}[:3] = 1.06372
P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:]
c1[:] = 1 + 0.201*M[:]^2.0
M_2[3:] = M[3:]
M_{2.5}[3:] = 0.6
hold_{2}[3:] = 1.07164
hold_{2.5}[3:] = 1.06372
Beginning signomial solve.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 867
Optimizer - Cones : 0
Optimizer - Scalar variables : 3449 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05
Factor - dense dim. : 0 flops : 2.91e+07
Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.240554640e+05 2.000000000e+00 1.0e+00 0.04
1 1.6e+03 2.5e+03 8.6e+04 -9.71e-01 -1.231748620e+05 2.768564203e+00 6.9e-01 0.04
2 8.3e+02 1.3e+03 4.5e+04 -9.57e-01 -1.207102576e+05 5.074539575e+00 3.6e-01 0.05
3 2.9e+02 4.6e+02 1.6e+04 -9.16e-01 -1.119695293e+05 2.152151786e+01 1.3e-01 0.06
4 2.9e+02 4.6e+02 1.6e+04 -7.71e-01 -1.100217009e+05 1.714527825e+03 1.3e-01 0.06
5 1.1e+02 1.8e+02 6.1e+03 -7.62e-01 -8.610790684e+04 6.695162483e+03 4.9e-02 0.07
6 3.8e+01 6.0e+01 2.0e+03 -4.15e-01 -4.645329796e+04 1.061030954e+04 1.7e-02 0.08
7 2.0e+01 3.2e+01 1.1e+03 2.49e-01 -2.881094530e+04 6.918992390e+03 8.9e-03 0.09
8 9.3e+00 1.5e+01 5.1e+02 5.72e-01 -1.414104026e+04 4.203941881e+03 4.1e-03 0.09
9 4.7e+00 7.4e+00 2.6e+02 8.28e-01 -7.062773964e+03 2.484854671e+03 2.1e-03 0.10
10 1.4e+00 2.2e+00 7.8e+01 9.34e-01 -2.018136909e+03 9.357817475e+02 6.3e-04 0.11
11 6.4e-01 1.0e+00 3.5e+01 9.94e-01 -6.982656505e+02 6.561046293e+02 2.9e-04 0.12
12 4.8e-01 7.6e-01 2.7e+01 9.96e-01 -4.637672981e+02 5.552260964e+02 2.2e-04 0.12
13 3.5e-01 7.8e-01 1.9e+01 9.80e-01 -2.759129050e+02 4.726371230e+02 1.6e-04 0.13
14 1.7e-01 3.9e-01 9.5e+00 9.96e-01 -5.042629419e+00 3.635650326e+02 7.9e-05 0.14
15 5.6e-02 1.6e-01 3.2e+00 9.94e-01 1.664733408e+02 2.896174723e+02 2.7e-05 0.15
16 3.2e-02 1.3e-01 1.9e+00 1.00e+00 2.020980643e+02 2.743670523e+02 1.6e-05 0.15
17 5.2e-03 1.8e-01 3.2e-01 1.00e+00 2.448158456e+02 2.572499035e+02 2.8e-06 0.16
18 1.5e-03 1.3e-01 9.5e-02 1.00e+00 2.510419816e+02 2.546930667e+02 8.5e-07 0.17
19 4.9e-04 1.1e-01 3.1e-02 1.00e+00 2.528147431e+02 2.540233778e+02 2.8e-07 0.18
20 2.1e-04 8.7e-02 1.4e-02 1.00e+00 2.533049609e+02 2.538348974e+02 1.2e-07 0.19
21 1.9e-04 7.9e-02 1.2e-02 1.00e+00 2.533443648e+02 2.538213184e+02 1.1e-07 0.19
22 1.7e-04 7.2e-02 1.1e-02 1.00e+00 2.533787262e+02 2.538079586e+02 1.0e-07 0.20
23 1.6e-04 6.6e-02 1.0e-02 1.00e+00 2.534096894e+02 2.537959814e+02 9.1e-08 0.21
24 1.4e-04 6.0e-02 9.1e-03 1.00e+00 2.534375306e+02 2.537851789e+02 8.2e-08 0.23
25 1.3e-04 5.4e-02 8.2e-03 1.00e+00 2.534625698e+02 2.537754412e+02 7.4e-08 0.24
26 1.1e-04 5.0e-02 7.3e-03 1.00e+00 2.534850882e+02 2.537666624e+02 6.6e-08 0.24
27 1.0e-04 4.6e-02 6.6e-03 1.00e+00 2.535053418e+02 2.537587504e+02 6.0e-08 0.25
28 9.2e-05 4.2e-02 5.9e-03 1.00e+00 2.535235593e+02 2.537516203e+02 5.4e-08 0.26
29 8.3e-05 3.8e-02 5.4e-03 1.00e+00 2.535399463e+02 2.537451957e+02 4.8e-08 0.27
30 7.4e-05 3.5e-02 4.8e-03 1.00e+00 2.535546874e+02 2.537394073e+02 4.4e-08 0.27
31 6.7e-05 3.2e-02 4.3e-03 1.00e+00 2.535679483e+02 2.537341927e+02 3.9e-08 0.28
32 6.0e-05 3.0e-02 3.9e-03 1.00e+00 2.535798780e+02 2.537294951e+02 3.5e-08 0.30
33 5.4e-05 2.8e-02 3.5e-03 1.00e+00 2.535906105e+02 2.537252636e+02 3.2e-08 0.31
34 4.9e-05 2.6e-02 3.2e-03 1.00e+00 2.536002661e+02 2.537214521e+02 2.9e-08 0.31
35 4.4e-05 2.4e-02 2.8e-03 1.00e+00 2.536089531e+02 2.537180190e+02 2.6e-08 0.32
36 4.0e-05 2.2e-02 2.6e-03 1.00e+00 2.536167687e+02 2.537149269e+02 2.3e-08 0.33
37 3.6e-05 2.1e-02 2.3e-03 1.00e+00 2.536238006e+02 2.537121421e+02 2.1e-08 0.33
38 3.2e-05 1.9e-02 2.1e-03 1.00e+00 2.536301274e+02 2.537096341e+02 1.9e-08 0.34
39 2.9e-05 1.8e-02 1.9e-03 1.00e+00 2.536358199e+02 2.537073754e+02 1.7e-08 0.35
40 2.6e-05 1.7e-02 1.7e-03 1.00e+00 2.536409418e+02 2.537053414e+02 1.5e-08 0.36
41 2.3e-05 1.6e-02 1.5e-03 1.00e+00 2.536455504e+02 2.537035098e+02 1.4e-08 0.36
42 2.1e-05 1.5e-02 1.4e-03 1.00e+00 2.536496972e+02 2.537018604e+02 1.2e-08 0.37
43 1.9e-05 1.5e-02 1.2e-03 1.00e+00 2.536534285e+02 2.537003753e+02 1.1e-08 0.38
44 1.7e-05 1.4e-02 1.1e-03 1.00e+00 2.536567861e+02 2.536990381e+02 1.0e-08 0.39
45 1.5e-05 1.3e-02 9.9e-04 1.00e+00 2.536598074e+02 2.536978341e+02 9.0e-09 0.39
46 1.4e-05 1.3e-02 8.9e-04 1.00e+00 2.536625261e+02 2.536967502e+02 8.1e-09 0.40
47 1.2e-05 1.2e-02 8.0e-04 1.00e+00 2.536649726e+02 2.536957743e+02 7.3e-09 0.41
48 1.1e-05 1.2e-02 7.2e-04 1.00e+00 2.536671742e+02 2.536948957e+02 6.5e-09 0.41
49 1.0e-05 1.1e-02 6.5e-04 1.00e+00 2.536691554e+02 2.536941047e+02 5.9e-09 0.42
50 9.0e-06 1.1e-02 5.9e-04 1.00e+00 2.536709383e+02 2.536933927e+02 5.3e-09 0.43
51 8.1e-06 1.1e-02 5.3e-04 1.00e+00 2.536725427e+02 2.536927517e+02 4.8e-09 0.44
52 7.3e-06 1.0e-02 4.7e-04 1.00e+00 2.536739866e+02 2.536921747e+02 4.3e-09 0.44
53 6.6e-06 1.0e-02 4.3e-04 1.00e+00 2.536752860e+02 2.536916553e+02 3.9e-09 0.45
54 5.9e-06 9.8e-03 3.8e-04 1.00e+00 2.536764553e+02 2.536911878e+02 3.5e-09 0.46
55 5.3e-06 9.6e-03 3.5e-04 1.00e+00 2.536775077e+02 2.536907669e+02 3.1e-09 0.47
56 4.8e-06 9.4e-03 3.1e-04 1.00e+00 2.536784547e+02 2.536903881e+02 2.8e-09 0.47
57 4.3e-06 9.2e-03 2.8e-04 1.00e+00 2.536793070e+02 2.536900470e+02 2.5e-09 0.48
58 3.9e-06 9.0e-03 2.5e-04 1.00e+00 2.536800740e+02 2.536897401e+02 2.3e-09 0.49
59 3.5e-06 8.9e-03 2.3e-04 1.00e+00 2.536807643e+02 2.536894637e+02 2.1e-09 0.50
60 3.2e-06 8.7e-03 2.0e-04 1.00e+00 2.536813855e+02 2.536892150e+02 1.8e-09 0.50
61 1.2e-06 3.4e-03 7.9e-05 1.00e+00 2.536848025e+02 2.536878456e+02 7.2e-10 0.51
62 1.1e-06 3.0e-03 7.1e-05 1.00e+00 2.536850202e+02 2.536877590e+02 6.5e-10 0.52
63 3.9e-07 1.1e-03 2.6e-05 1.00e+00 2.536862733e+02 2.536872564e+02 2.3e-10 0.52
64 3.6e-07 9.8e-04 2.3e-05 1.00e+00 2.536863436e+02 2.536872284e+02 2.1e-10 0.53
65 3.2e-07 8.9e-04 2.1e-05 1.00e+00 2.536864067e+02 2.536872030e+02 1.9e-10 0.54
66 2.9e-07 8.0e-04 1.9e-05 1.00e+00 2.536864635e+02 2.536871802e+02 1.7e-10 0.55
67 2.6e-07 7.2e-04 1.7e-05 1.00e+00 2.536865146e+02 2.536871596e+02 1.5e-10 0.55
68 2.3e-07 6.5e-04 1.5e-05 1.00e+00 2.536865606e+02 2.536871412e+02 1.4e-10 0.56
69 2.1e-07 5.8e-04 1.4e-05 1.00e+00 2.536866020e+02 2.536871245e+02 1.2e-10 0.57
70 1.9e-07 5.2e-04 1.2e-05 1.00e+00 2.536866393e+02 2.536871096e+02 1.1e-10 0.58
71 1.7e-07 4.7e-04 1.1e-05 1.00e+00 2.536866729e+02 2.536870961e+02 1.0e-10 0.58
72 1.5e-07 4.2e-04 9.9e-06 1.00e+00 2.536867031e+02 2.536870839e+02 9.0e-11 0.59
73 1.4e-07 3.8e-04 8.9e-06 1.00e+00 2.536867302e+02 2.536870730e+02 8.1e-11 0.60
74 1.2e-07 3.4e-04 8.1e-06 1.00e+00 2.536867547e+02 2.536870632e+02 7.3e-11 0.60
75 1.1e-07 3.1e-04 7.2e-06 1.00e+00 2.536867767e+02 2.536870544e+02 6.6e-11 0.61
76 1.0e-07 2.8e-04 6.5e-06 1.00e+00 2.536867965e+02 2.536870464e+02 5.9e-11 0.62
77 9.0e-08 2.5e-04 5.9e-06 1.00e+00 2.536868143e+02 2.536870392e+02 5.3e-11 0.63
78 8.1e-08 2.3e-04 5.3e-06 1.00e+00 2.536868303e+02 2.536870328e+02 4.8e-11 0.63
79 7.3e-08 2.0e-04 4.8e-06 1.00e+00 2.536868448e+02 2.536870270e+02 4.3e-11 0.64
80 6.6e-08 1.8e-04 4.3e-06 1.00e+00 2.536868578e+02 2.536870217e+02 3.9e-11 0.65
81 5.9e-08 1.6e-04 3.9e-06 1.00e+00 2.536868695e+02 2.536870170e+02 3.5e-11 0.65
82 5.3e-08 1.5e-04 3.5e-06 1.00e+00 2.536868800e+02 2.536870128e+02 3.1e-11 0.66
83 4.8e-08 1.3e-04 3.1e-06 1.00e+00 2.536868894e+02 2.536870090e+02 2.8e-11 0.67
84 4.3e-08 1.2e-04 2.8e-06 1.00e+00 2.536868980e+02 2.536870056e+02 2.5e-11 0.68
85 3.9e-08 1.1e-04 2.5e-06 1.00e+00 2.536869056e+02 2.536870025e+02 2.3e-11 0.68
86 3.5e-08 9.7e-05 2.3e-06 1.00e+00 2.536869125e+02 2.536869997e+02 2.1e-11 0.69
87 3.1e-08 8.7e-05 2.0e-06 1.00e+00 2.536869188e+02 2.536869972e+02 1.9e-11 0.71
88 2.8e-08 7.8e-05 1.8e-06 1.00e+00 2.536869243e+02 2.536869949e+02 1.7e-11 0.71
89 2.6e-08 7.1e-05 1.7e-06 1.00e+00 2.536869294e+02 2.536869929e+02 1.5e-11 0.72
90 2.3e-08 6.4e-05 1.5e-06 1.00e+00 2.536869339e+02 2.536869911e+02 1.3e-11 0.73
91 2.1e-08 5.7e-05 1.3e-06 1.00e+00 2.536869380e+02 2.536869894e+02 1.2e-11 0.74
92 1.9e-08 5.1e-05 1.2e-06 9.99e-01 2.536869416e+02 2.536869880e+02 1.1e-11 0.74
93 1.7e-08 4.6e-05 1.1e-06 1.00e+00 2.536869449e+02 2.536869866e+02 9.8e-12 0.75
94 1.5e-08 4.2e-05 9.8e-07 1.00e+00 2.536869479e+02 2.536869854e+02 8.9e-12 0.77
95 1.4e-08 3.8e-05 8.8e-07 1.00e+00 2.536869506e+02 2.536869843e+02 8.0e-12 0.77
96 1.2e-08 3.4e-05 7.9e-07 1.00e+00 2.536869530e+02 2.536869834e+02 7.2e-12 0.78
Optimizer terminated. Time: 0.78
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 2.5368695299e+02 nrm: 4e+01 Viol. con: 2e-07 var: 0e+00
Dual. obj: 2.5368698338e+02 nrm: 8e+02 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.808 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 868
Optimizer - Cones : 0
Optimizer - Scalar variables : 3451 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05
Factor - dense dim. : 0 flops : 2.93e+07
Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237120597e+05 2.000000000e+00 1.0e+00 0.03
1 1.6e+03 2.5e+03 8.6e+04 -9.71e-01 -1.228589965e+05 2.751831010e+00 7.0e-01 0.04
2 7.9e+02 1.2e+03 4.3e+04 -9.57e-01 -1.201055617e+05 5.326974937e+00 3.5e-01 0.05
3 3.0e+02 4.7e+02 1.6e+04 -9.12e-01 -1.116972905e+05 2.210725287e+01 1.3e-01 0.05
4 2.9e+02 4.7e+02 1.6e+04 -7.71e-01 -1.098007288e+05 1.669805666e+03 1.3e-01 0.06
5 1.2e+02 2.0e+02 6.8e+03 -7.63e-01 -8.914530211e+04 6.028487627e+03 5.5e-02 0.07
6 3.9e+01 6.2e+01 2.1e+03 -4.65e-01 -4.731075280e+04 1.101859429e+04 1.7e-02 0.07
7 2.3e+01 3.6e+01 1.2e+03 2.31e-01 -3.188986622e+04 7.305151537e+03 1.0e-02 0.08
8 9.1e+00 1.4e+01 4.9e+02 5.19e-01 -1.390726678e+04 3.970193410e+03 4.0e-03 0.09
9 6.1e+00 9.6e+00 3.3e+02 8.31e-01 -9.268556419e+03 2.859448056e+03 2.7e-03 0.10
10 2.1e+00 3.3e+00 1.2e+02 9.02e-01 -3.163867678e+03 1.208066659e+03 9.4e-04 0.10
11 1.5e+00 2.4e+00 8.2e+01 9.76e-01 -2.158354396e+03 9.713866924e+02 6.7e-04 0.11
12 8.2e-01 1.4e+00 4.5e+01 9.80e-01 -1.092111068e+03 6.286525202e+02 3.7e-04 0.12
13 4.2e-01 8.1e-01 2.3e+01 9.88e-01 -4.661197429e+02 4.147126547e+02 1.9e-04 0.13
14 2.0e-01 3.9e-01 1.1e+01 1.00e+00 -1.249220987e+02 2.924420143e+02 9.0e-05 0.13
15 7.1e-02 1.6e-01 4.0e+00 1.00e+00 6.301524973e+01 2.167838530e+02 3.4e-05 0.14
16 2.8e-02 1.2e-01 1.6e+00 1.01e+00 1.288290682e+02 1.894676038e+02 1.3e-05 0.15
17 9.0e-03 1.1e-01 5.3e-01 1.01e+00 1.578773200e+02 1.781360078e+02 4.6e-06 0.15
18 3.5e-03 9.5e-02 2.1e-01 1.00e+00 1.667254586e+02 1.745981914e+02 1.8e-06 0.16
19 8.9e-04 1.2e-01 5.5e-02 9.96e-01 1.708742732e+02 1.729794156e+02 4.9e-07 0.17
20 3.2e-04 9.8e-02 2.0e-02 9.84e-01 1.718440948e+02 1.726232491e+02 1.8e-07 0.18
21 1.3e-04 9.3e-02 8.1e-03 9.96e-01 1.721840324e+02 1.724937389e+02 7.2e-08 0.19
22 4.6e-05 9.0e-02 3.0e-03 9.80e-01 1.723224558e+02 1.724367754e+02 2.7e-08 0.20
23 4.2e-05 8.8e-02 2.7e-03 9.92e-01 1.723310420e+02 1.724347821e+02 2.4e-08 0.21
24 4.1e-05 8.5e-02 2.6e-03 9.83e-01 1.723333827e+02 1.724335011e+02 2.3e-08 0.21
25 3.0e-05 8.4e-02 2.0e-03 9.27e-01 1.723515646e+02 1.724203243e+02 1.7e-08 0.22
26 1.2e-05 6.4e-02 8.3e-04 5.08e-01 1.723804253e+02 1.724123065e+02 7.6e-09 0.23
27 1.1e-05 5.8e-02 7.7e-04 8.67e-01 1.723842833e+02 1.724130215e+02 7.0e-09 0.24
28 1.0e-05 5.5e-02 7.0e-04 1.00e+00 1.723862088e+02 1.724122141e+02 6.4e-09 0.25
29 9.1e-06 5.0e-02 6.3e-04 1.00e+00 1.723880259e+02 1.724114281e+02 5.7e-09 0.25
30 8.2e-06 4.6e-02 5.7e-04 1.00e+00 1.723896607e+02 1.724107219e+02 5.2e-09 0.26
31 7.4e-06 4.2e-02 5.1e-04 1.00e+00 1.723911307e+02 1.724100853e+02 4.7e-09 0.27
32 6.7e-06 3.9e-02 4.6e-04 1.00e+00 1.723924532e+02 1.724095118e+02 4.2e-09 0.27
33 6.0e-06 3.5e-02 4.1e-04 1.00e+00 1.723936429e+02 1.724089953e+02 3.8e-09 0.28
34 5.4e-06 3.3e-02 3.7e-04 1.00e+00 1.723947132e+02 1.724085300e+02 3.4e-09 0.29
35 4.9e-06 3.0e-02 3.4e-04 1.00e+00 1.723956761e+02 1.724081109e+02 3.1e-09 0.29
36 4.4e-06 2.8e-02 3.0e-04 1.00e+00 1.723965424e+02 1.724077335e+02 2.7e-09 0.30
37 3.9e-06 2.6e-02 2.7e-04 1.00e+00 1.723973218e+02 1.724073936e+02 2.5e-09 0.31
38 3.5e-06 2.4e-02 2.4e-04 1.00e+00 1.723980230e+02 1.724070875e+02 2.2e-09 0.31
39 3.2e-06 2.2e-02 2.2e-04 1.00e+00 1.723986539e+02 1.724068118e+02 2.0e-09 0.32
40 2.9e-06 2.1e-02 2.0e-04 1.00e+00 1.723992216e+02 1.724065636e+02 1.8e-09 0.33
41 2.6e-06 2.0e-02 1.8e-04 1.00e+00 1.723997324e+02 1.724063401e+02 1.6e-09 0.33
42 2.3e-06 1.8e-02 1.6e-04 1.00e+00 1.724001920e+02 1.724061388e+02 1.5e-09 0.34
43 2.1e-06 1.7e-02 1.4e-04 1.00e+00 1.724006056e+02 1.724059576e+02 1.3e-09 0.35
44 1.9e-06 1.6e-02 1.3e-04 1.00e+00 1.724009777e+02 1.724057945e+02 1.2e-09 0.35
45 1.7e-06 1.6e-02 1.2e-04 1.00e+00 1.724013125e+02 1.724056476e+02 1.1e-09 0.36
46 1.5e-06 1.5e-02 1.1e-04 1.00e+00 1.724016138e+02 1.724055153e+02 9.6e-10 0.37
47 1.4e-06 1.4e-02 9.5e-05 1.00e+00 1.724018849e+02 1.724053962e+02 8.6e-10 0.38
48 1.2e-06 1.3e-02 8.5e-05 1.00e+00 1.724021289e+02 1.724052890e+02 7.8e-10 0.38
49 1.1e-06 1.3e-02 7.7e-05 1.00e+00 1.724023484e+02 1.724051925e+02 7.0e-10 0.39
50 1.0e-06 1.2e-02 6.9e-05 1.00e+00 1.724025459e+02 1.724051056e+02 6.3e-10 0.40
51 9.0e-07 1.2e-02 6.2e-05 1.00e+00 1.724027237e+02 1.724050274e+02 5.7e-10 0.40
52 8.1e-07 1.1e-02 5.6e-05 1.00e+00 1.724028836e+02 1.724049570e+02 5.1e-10 0.41
53 7.3e-07 1.1e-02 5.0e-05 1.00e+00 1.724030276e+02 1.724048936e+02 4.6e-10 0.42
54 6.6e-07 1.1e-02 4.5e-05 1.00e+00 1.724031571e+02 1.724048365e+02 4.1e-10 0.42
55 5.9e-07 1.0e-02 4.1e-05 1.00e+00 1.724032737e+02 1.724047851e+02 3.7e-10 0.43
56 5.3e-07 1.0e-02 3.7e-05 1.00e+00 1.724033785e+02 1.724047388e+02 3.3e-10 0.44
57 4.8e-07 9.9e-03 3.3e-05 1.00e+00 1.724034729e+02 1.724046972e+02 3.0e-10 0.44
58 4.3e-07 9.7e-03 3.0e-05 1.00e+00 1.724035579e+02 1.724046597e+02 2.7e-10 0.45
59 3.9e-07 9.5e-03 2.7e-05 1.00e+00 1.724036343e+02 1.724046259e+02 2.4e-10 0.46
60 3.5e-07 9.3e-03 2.4e-05 1.00e+00 1.724037031e+02 1.724045956e+02 2.2e-10 0.47
61 3.1e-07 9.2e-03 2.2e-05 1.00e+00 1.724037650e+02 1.724045682e+02 2.0e-10 0.47
62 2.8e-07 9.0e-03 1.9e-05 1.00e+00 1.724038206e+02 1.724045436e+02 1.8e-10 0.48
63 2.5e-07 8.9e-03 1.8e-05 1.00e+00 1.724038708e+02 1.724045214e+02 1.6e-10 0.49
64 2.3e-07 8.7e-03 1.6e-05 1.00e+00 1.724039159e+02 1.724045014e+02 1.4e-10 0.49
65 2.1e-07 8.6e-03 1.4e-05 9.99e-01 1.724039565e+02 1.724044834e+02 1.3e-10 0.50
66 1.9e-07 8.5e-03 1.3e-05 1.00e+00 1.724039930e+02 1.724044673e+02 1.2e-10 0.51
67 1.7e-07 8.4e-03 1.2e-05 1.00e+00 1.724040259e+02 1.724044527e+02 1.0e-10 0.52
68 1.5e-07 8.4e-03 1.0e-05 9.97e-01 1.724040554e+02 1.724044396e+02 9.4e-11 0.52
69 1.4e-07 8.3e-03 9.3e-06 1.00e+00 1.724040820e+02 1.724044278e+02 8.5e-11 0.53
70 1.2e-07 8.2e-03 8.4e-06 9.99e-01 1.724041060e+02 1.724044171e+02 7.7e-11 0.54
71 1.1e-07 8.1e-03 7.6e-06 9.98e-01 1.724041276e+02 1.724044076e+02 6.9e-11 0.55
72 9.9e-08 8.1e-03 6.8e-06 1.00e+00 1.724041470e+02 1.724043989e+02 6.2e-11 0.55
73 8.9e-08 8.0e-03 6.1e-06 9.99e-01 1.724041644e+02 1.724043912e+02 5.6e-11 0.56
74 8.0e-08 7.2e-03 5.5e-06 1.01e+00 1.724041806e+02 1.724043840e+02 5.0e-11 0.57
75 7.2e-08 6.5e-03 5.0e-06 1.00e+00 1.724041947e+02 1.724043777e+02 4.5e-11 0.57
76 6.5e-08 5.9e-03 4.5e-06 9.99e-01 1.724042074e+02 1.724043721e+02 4.1e-11 0.58
77 5.8e-08 5.3e-03 4.0e-06 9.93e-01 1.724042188e+02 1.724043672e+02 3.7e-11 0.59
78 5.3e-08 4.8e-03 3.6e-06 1.00e+00 1.724042291e+02 1.724043626e+02 3.3e-11 0.59
79 4.8e-08 4.3e-03 3.3e-06 9.90e-01 1.724042383e+02 1.724043586e+02 3.0e-11 0.60
80 4.3e-08 3.8e-03 2.9e-06 1.03e+00 1.724042478e+02 1.724043542e+02 2.7e-11 0.61
81 3.8e-08 3.5e-03 2.6e-06 9.79e-01 1.724042552e+02 1.724043509e+02 2.4e-11 0.61
82 3.4e-08 3.1e-03 2.4e-06 1.02e+00 1.724042624e+02 1.724043476e+02 2.2e-11 0.62
83 3.1e-08 2.8e-03 2.1e-06 1.03e+00 1.724042690e+02 1.724043446e+02 2.0e-11 0.63
84 2.8e-08 2.5e-03 1.9e-06 9.12e-01 1.724042743e+02 1.724043422e+02 1.8e-11 0.63
85 4.5e-08 2.3e-03 1.7e-06 1.19e+00 1.724042829e+02 1.724043382e+02 1.8e-11 0.64
86 3.7e-08 2.0e-03 1.6e-06 1.04e+00 1.724042873e+02 1.724043365e+02 1.7e-11 0.65
87 2.2e-08 4.8e-04 3.7e-07 1.05e+00 1.724043138e+02 1.724043253e+02 4.2e-12 0.66
88 4.1e-08 2.2e-04 1.6e-07 2.36e-01 1.724043176e+02 1.724043220e+02 1.3e-12 0.66
89 2.9e-08 1.9e-04 1.5e-07 1.99e+00 1.724043178e+02 1.724043221e+02 1.2e-12 0.67
90 2.8e-08 1.7e-04 1.3e-07 8.57e-01 1.724043184e+02 1.724043219e+02 1.0e-12 0.68
91 3.0e-08 1.5e-04 1.1e-07 1.29e+00 1.724043178e+02 1.724043232e+02 8.8e-13 0.68
Optimizer terminated. Time: 0.69
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.7240431778e+02 nrm: 4e+01 Viol. con: 9e-07 var: 0e+00
Dual. obj: 1.7240432322e+02 nrm: 8e+02 Viol. con: 0e+00 var: 1e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.708 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 868
Optimizer - Cones : 0
Optimizer - Scalar variables : 3451 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05
Factor - dense dim. : 0 flops : 2.93e+07
Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.238236350e+05 2.000000000e+00 1.0e+00 0.03
1 1.6e+03 2.6e+03 8.9e+04 -9.71e-01 -1.230656737e+05 2.647019465e+00 7.2e-01 0.04
2 8.5e+02 1.3e+03 4.6e+04 -9.59e-01 -1.206096807e+05 4.826231613e+00 3.7e-01 0.05
3 2.9e+02 4.6e+02 1.6e+04 -9.19e-01 -1.118497077e+05 2.029621091e+01 1.3e-01 0.05
4 2.9e+02 4.6e+02 1.6e+04 -7.73e-01 -1.097490525e+05 1.850586108e+03 1.3e-01 0.06
5 1.2e+02 2.0e+02 6.7e+03 -7.63e-01 -8.916030429e+04 6.085082524e+03 5.5e-02 0.07
6 4.4e+01 6.9e+01 2.4e+03 -4.64e-01 -5.177804334e+04 1.031145337e+04 1.9e-02 0.07
7 2.6e+01 4.1e+01 1.4e+03 1.59e-01 -3.543323189e+04 7.187062739e+03 1.1e-02 0.08
8 1.3e+01 2.0e+01 6.9e+02 4.65e-01 -1.929026185e+04 4.600188328e+03 5.6e-03 0.09
9 4.5e+00 7.1e+00 2.4e+02 7.44e-01 -6.918526178e+03 2.202933527e+03 2.0e-03 0.09
10 3.2e+00 5.1e+00 1.8e+02 9.39e-01 -4.934163409e+03 1.735951750e+03 1.5e-03 0.10
11 1.1e+00 1.7e+00 6.0e+01 9.62e-01 -1.562948083e+03 7.020582355e+02 4.9e-04 0.11
12 8.7e-01 1.4e+00 4.8e+01 9.87e-01 -1.217636151e+03 6.233488377e+02 3.9e-04 0.11
13 7.0e-01 1.2e+00 3.9e+01 9.68e-01 -9.661564015e+02 5.337666482e+02 3.2e-04 0.12
14 3.7e-01 6.1e-01 2.0e+01 9.89e-01 -3.985115606e+02 3.850483742e+02 1.7e-04 0.13
15 1.9e-01 3.2e-01 1.1e+01 9.96e-01 -1.412662595e+02 2.691767565e+02 8.8e-05 0.14
16 8.6e-02 1.7e-01 4.8e+00 1.00e+00 1.778207455e+01 2.044312768e+02 4.0e-05 0.14
17 7.8e-02 1.6e-01 4.4e+00 1.01e+00 3.927330071e+01 2.075518436e+02 3.6e-05 0.15
18 3.1e-02 9.1e-02 1.7e+00 1.01e+00 1.160421338e+02 1.824337014e+02 1.4e-05 0.16
19 1.4e-02 1.2e-01 7.7e-01 1.02e+00 1.451390072e+02 1.745459003e+02 6.4e-06 0.17
20 6.5e-03 4.2e-01 3.7e-01 1.01e+00 1.561700198e+02 1.702886893e+02 3.1e-06 0.17
21 2.1e-03 1.6e-01 1.3e-01 1.01e+00 1.635809429e+02 1.683332990e+02 1.1e-06 0.18
22 1.7e-03 1.3e-01 9.8e-02 1.01e+00 1.644225804e+02 1.681013974e+02 8.2e-07 0.19
23 6.6e-04 9.4e-02 4.0e-02 1.01e+00 1.660456798e+02 1.675261264e+02 3.4e-07 0.19
24 4.1e-04 7.6e-02 2.4e-02 1.01e+00 1.664525288e+02 1.673655646e+02 2.1e-07 0.20
25 3.7e-04 7.0e-02 2.2e-02 1.01e+00 1.665206591e+02 1.673421416e+02 1.9e-07 0.21
26 3.3e-04 6.3e-02 2.0e-02 1.01e+00 1.665794090e+02 1.673184976e+02 1.7e-07 0.22
27 3.0e-04 5.8e-02 1.8e-02 1.01e+00 1.666325754e+02 1.672975734e+02 1.5e-07 0.22
28 2.7e-04 5.3e-02 1.6e-02 1.01e+00 1.666802184e+02 1.672785665e+02 1.4e-07 0.23
29 2.4e-04 4.8e-02 1.4e-02 1.01e+00 1.667229548e+02 1.672613467e+02 1.2e-07 0.24
30 2.2e-04 4.4e-02 1.3e-02 1.01e+00 1.667612707e+02 1.672457248e+02 1.1e-07 0.24
31 1.9e-04 4.1e-02 1.2e-02 1.01e+00 1.667956243e+02 1.672315526e+02 1.0e-07 0.25
32 1.8e-04 3.7e-02 1.1e-02 1.01e+00 1.668264232e+02 1.672186933e+02 9.0e-08 0.26
33 1.6e-04 3.4e-02 9.5e-03 1.01e+00 1.668540348e+02 1.672070251e+02 8.1e-08 0.26
34 1.4e-04 3.2e-02 8.5e-03 1.00e+00 1.668787897e+02 1.671964382e+02 7.3e-08 0.27
35 1.3e-04 2.9e-02 7.7e-03 1.00e+00 1.669009849e+02 1.671868358e+02 6.6e-08 0.28
36 1.2e-04 2.7e-02 6.9e-03 1.00e+00 1.669208870e+02 1.671781271e+02 5.9e-08 0.29
37 1.0e-04 2.5e-02 6.2e-03 1.00e+00 1.669387360e+02 1.671702309e+02 5.3e-08 0.30
38 9.3e-05 2.3e-02 5.6e-03 1.00e+00 1.669547475e+02 1.671630747e+02 4.8e-08 0.32
39 8.4e-05 2.2e-02 5.0e-03 1.00e+00 1.669691132e+02 1.671565940e+02 4.3e-08 0.33
40 7.5e-05 2.0e-02 4.5e-03 1.00e+00 1.669820037e+02 1.671507256e+02 3.9e-08 0.34
41 6.8e-05 1.9e-02 4.1e-03 1.00e+00 1.669935725e+02 1.671454125e+02 3.5e-08 0.35
42 6.1e-05 1.8e-02 3.7e-03 1.00e+00 1.670039573e+02 1.671406082e+02 3.1e-08 0.36
43 5.5e-05 1.7e-02 3.3e-03 1.00e+00 1.670132789e+02 1.671362608e+02 2.8e-08 0.37
44 5.0e-05 1.6e-02 3.0e-03 1.00e+00 1.670216485e+02 1.671323292e+02 2.5e-08 0.38
45 4.5e-05 1.5e-02 2.7e-03 1.00e+00 1.670291639e+02 1.671287745e+02 2.3e-08 0.40
46 4.0e-05 1.5e-02 2.4e-03 1.00e+00 1.670359132e+02 1.671255600e+02 2.1e-08 0.41
47 3.6e-05 1.4e-02 2.2e-03 1.00e+00 1.670419753e+02 1.671226558e+02 1.9e-08 0.42
48 3.2e-05 1.3e-02 2.0e-03 1.00e+00 1.670474206e+02 1.671200297e+02 1.7e-08 0.43
49 2.9e-05 1.3e-02 1.8e-03 1.00e+00 1.670523127e+02 1.671176570e+02 1.5e-08 0.43
50 2.6e-05 1.2e-02 1.6e-03 1.00e+00 1.670567081e+02 1.671155162e+02 1.4e-08 0.44
51 2.4e-05 1.2e-02 1.4e-03 1.00e+00 1.670606568e+02 1.671135837e+02 1.2e-08 0.45
52 2.1e-05 1.2e-02 1.3e-03 1.00e+00 1.670642048e+02 1.671118395e+02 1.1e-08 0.46
53 1.9e-05 1.1e-02 1.2e-03 1.00e+00 1.670673932e+02 1.671102652e+02 9.9e-09 0.48
54 1.7e-05 1.1e-02 1.0e-03 1.00e+00 1.670702588e+02 1.671088431e+02 8.9e-09 0.49
55 1.6e-05 1.1e-02 9.4e-04 1.00e+00 1.670728345e+02 1.671075617e+02 8.0e-09 0.50
56 1.4e-05 1.1e-02 8.4e-04 1.00e+00 1.670751497e+02 1.671064039e+02 7.2e-09 0.51
57 1.3e-05 1.0e-02 7.6e-04 1.00e+00 1.670772310e+02 1.671053606e+02 6.5e-09 0.51
58 1.1e-05 1.0e-02 6.8e-04 1.00e+00 1.670791022e+02 1.671044185e+02 5.8e-09 0.52
59 1.0e-05 1.0e-02 6.1e-04 1.00e+00 1.670807846e+02 1.671035703e+02 5.2e-09 0.53
60 9.2e-06 9.8e-03 5.5e-04 1.00e+00 1.670822972e+02 1.671028046e+02 4.7e-09 0.53
61 8.3e-06 9.6e-03 5.0e-04 1.00e+00 1.670836577e+02 1.671021134e+02 4.3e-09 0.54
62 7.4e-06 9.5e-03 4.5e-04 1.00e+00 1.670848812e+02 1.671014903e+02 3.8e-09 0.55
63 6.7e-06 9.4e-03 4.0e-04 1.00e+00 1.670859815e+02 1.671009293e+02 3.4e-09 0.56
64 6.0e-06 9.3e-03 3.6e-04 1.00e+00 1.670869709e+02 1.671004242e+02 3.1e-09 0.56
65 5.4e-06 9.2e-03 3.3e-04 9.99e-01 1.670878607e+02 1.670999696e+02 2.8e-09 0.57
66 2.1e-06 3.5e-03 1.3e-04 1.00e+00 1.670927599e+02 1.670974336e+02 1.1e-09 0.58
67 8.4e-07 1.4e-03 5.1e-05 1.00e+00 1.670945910e+02 1.670964807e+02 4.3e-10 0.59
68 7.6e-07 1.3e-03 4.6e-05 9.76e-01 1.670947193e+02 1.670964216e+02 3.9e-10 0.59
69 6.8e-07 1.2e-03 4.1e-05 9.78e-01 1.670948304e+02 1.670963642e+02 3.5e-10 0.60
70 6.1e-07 1.0e-03 3.7e-05 1.01e+00 1.670949327e+02 1.670963100e+02 3.2e-10 0.61
71 5.5e-07 9.3e-04 3.3e-05 1.01e+00 1.670950269e+02 1.670962602e+02 2.9e-10 0.62
72 5.0e-07 8.4e-04 3.0e-05 9.98e-01 1.670951078e+02 1.670962181e+02 2.6e-10 0.62
73 4.5e-07 7.6e-04 2.7e-05 1.00e+00 1.670951806e+02 1.670961797e+02 2.3e-10 0.63
74 4.0e-07 6.8e-04 2.4e-05 9.62e-01 1.670952457e+02 1.670961466e+02 2.1e-10 0.64
75 3.6e-07 6.1e-04 2.2e-05 1.00e+00 1.670953048e+02 1.670961152e+02 1.9e-10 0.64
76 3.3e-07 5.5e-04 2.0e-05 9.47e-01 1.670953574e+02 1.670960887e+02 1.7e-10 0.65
77 2.9e-07 5.0e-04 1.8e-05 9.83e-01 1.670954049e+02 1.670960640e+02 1.5e-10 0.66
78 2.6e-07 4.5e-04 1.6e-05 9.72e-01 1.670954477e+02 1.670960418e+02 1.4e-10 0.66
79 2.4e-07 4.0e-04 1.4e-05 9.74e-01 1.670954862e+02 1.670960216e+02 1.2e-10 0.67
80 2.1e-07 3.6e-04 1.3e-05 1.11e+00 1.670955379e+02 1.670959913e+02 1.2e-10 0.68
81 1.9e-07 3.3e-04 1.2e-05 1.05e+00 1.670955741e+02 1.670959712e+02 1.1e-10 0.69
82 1.7e-07 2.9e-04 1.1e-05 9.00e-01 1.670955997e+02 1.670959587e+02 9.7e-11 0.70
83 1.6e-07 2.6e-04 9.5e-06 9.56e-01 1.670956230e+02 1.670959468e+02 8.8e-11 0.71
84 1.4e-07 2.4e-04 8.5e-06 1.26e+00 1.670956449e+02 1.670959326e+02 7.9e-11 0.72
85 1.3e-07 2.1e-04 7.7e-06 1.02e+00 1.670956658e+02 1.670959215e+02 7.2e-11 0.73
86 1.1e-07 1.9e-04 6.9e-06 9.32e-01 1.670956824e+02 1.670959135e+02 6.5e-11 0.74
87 1.0e-07 1.7e-04 6.2e-06 9.84e-01 1.670956975e+02 1.670959055e+02 5.8e-11 0.75
88 9.2e-08 1.6e-04 5.6e-06 8.13e-01 1.670957107e+02 1.670958999e+02 5.2e-11 0.76
89 8.3e-08 1.4e-04 5.0e-06 8.80e-01 1.670957228e+02 1.670958941e+02 4.7e-11 0.77
90 7.6e-08 1.3e-04 4.5e-06 7.53e-01 1.670957335e+02 1.670958896e+02 4.2e-11 0.78
91 6.9e-08 1.1e-04 4.1e-06 7.15e-01 1.670957432e+02 1.670958858e+02 3.8e-11 0.79
92 6.1e-08 1.0e-04 3.7e-06 1.47e+00 1.670957529e+02 1.670958781e+02 3.4e-11 0.80
93 5.5e-08 9.2e-05 3.3e-06 8.63e-01 1.670957608e+02 1.670958741e+02 3.1e-11 0.81
94 4.9e-08 8.3e-05 3.0e-06 1.22e+00 1.670957685e+02 1.670958690e+02 2.8e-11 0.82
95 4.4e-08 7.5e-05 2.7e-06 1.18e+00 1.670957803e+02 1.670958618e+02 2.7e-11 0.83
96 4.3e-08 6.7e-05 2.4e-06 1.10e+00 1.670957883e+02 1.670958574e+02 2.6e-11 0.84
97 1.3e-07 6.5e-05 2.3e-06 2.34e+01 1.670957954e+02 1.670958412e+02 1.9e-11 0.84
98 1.2e-07 5.8e-05 2.1e-06 2.38e+00 1.670958013e+02 1.670958392e+02 1.7e-11 0.85
99 1.1e-07 5.3e-05 1.9e-06 9.21e-01 1.670958045e+02 1.670958387e+02 1.5e-11 0.86
100 1.0e-07 4.7e-05 1.7e-06 1.01e+00 1.670958077e+02 1.670958382e+02 1.4e-11 0.86
101 9.1e-08 4.3e-05 1.5e-06 9.95e-01 1.670958104e+02 1.670958377e+02 1.2e-11 0.87
102 8.1e-08 3.8e-05 1.4e-06 1.62e+00 1.670958132e+02 1.670958371e+02 1.1e-11 0.88
103 7.4e-08 3.5e-05 1.2e-06 1.22e+00 1.670958154e+02 1.670958367e+02 1.0e-11 0.89
Optimizer terminated. Time: 0.89
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6709581541e+02 nrm: 2e+01 Viol. con: 1e-06 var: 0e+00
Dual. obj: 1.6709583675e+02 nrm: 9e+02 Viol. con: 0e+00 var: 1e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.914 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.02
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 868
Optimizer - Cones : 0
Optimizer - Scalar variables : 3451 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.03 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05
Factor - dense dim. : 0 flops : 2.93e+07
Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237491052e+05 2.000000000e+00 1.0e+00 0.05
1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230051622e+05 2.628714936e+00 7.2e-01 0.06
2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.206769287e+05 4.656932367e+00 3.8e-01 0.07
3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.117660642e+05 2.006454280e+01 1.3e-01 0.08
4 2.9e+02 4.6e+02 1.6e+04 -7.73e-01 -1.095928583e+05 1.917273339e+03 1.3e-01 0.09
5 1.2e+02 1.9e+02 6.5e+03 -7.63e-01 -8.815406305e+04 6.301964476e+03 5.3e-02 0.09
6 4.0e+01 6.3e+01 2.2e+03 -4.50e-01 -4.810694490e+04 1.098450134e+04 1.8e-02 0.10
7 2.5e+01 3.9e+01 1.3e+03 2.23e-01 -3.417995100e+04 7.471100510e+03 1.1e-02 0.11
8 1.2e+01 1.9e+01 6.5e+02 4.89e-01 -1.841437506e+04 4.250327359e+03 5.3e-03 0.11
9 3.9e+00 6.2e+00 2.1e+02 7.62e-01 -6.079617169e+03 2.004072841e+03 1.8e-03 0.12
10 2.3e+00 3.6e+00 1.2e+02 9.51e-01 -3.348709564e+03 1.369385886e+03 1.0e-03 0.13
11 9.6e-01 1.5e+00 5.3e+01 9.83e-01 -1.341473639e+03 6.716781476e+02 4.4e-04 0.14
12 7.9e-01 1.3e+00 4.4e+01 9.79e-01 -1.108501626e+03 5.799282710e+02 3.6e-04 0.15
13 7.5e-01 1.2e+00 4.1e+01 9.86e-01 -1.026923381e+03 5.623532525e+02 3.4e-04 0.16
14 2.6e-01 4.5e-01 1.5e+01 9.85e-01 -2.677966215e+02 2.992138734e+02 1.2e-04 0.17
15 1.2e-01 3.5e-01 6.6e+00 1.01e+00 -3.926603929e+01 2.146631657e+02 5.5e-05 0.18
16 1.1e-01 3.3e-01 6.0e+00 1.01e+00 -1.198752865e+01 2.196214563e+02 5.0e-05 0.19
17 8.7e-02 4.3e-01 4.9e+00 1.01e+00 1.945767868e+01 2.094440827e+02 4.2e-05 0.20
18 3.7e-02 1.9e-01 2.1e+00 1.01e+00 1.045391567e+02 1.838693347e+02 1.7e-05 0.21
19 9.9e-03 1.9e-01 5.7e-01 1.02e+00 1.505055784e+02 1.721489517e+02 4.8e-06 0.22
20 3.9e-03 1.6e-01 2.3e-01 1.01e+00 1.603048687e+02 1.688286538e+02 1.9e-06 0.23
21 1.8e-03 9.1e-02 1.1e-01 1.01e+00 1.636747889e+02 1.677018607e+02 9.1e-07 0.24
22 6.6e-04 9.6e-02 4.0e-02 1.01e+00 1.655620826e+02 1.670587271e+02 3.4e-07 0.25
23 2.5e-04 9.7e-02 1.5e-02 1.01e+00 1.662322259e+02 1.668083553e+02 1.3e-07 0.26
24 2.3e-04 8.9e-02 1.4e-02 1.01e+00 1.662772825e+02 1.667957045e+02 1.2e-07 0.27
25 2.0e-04 8.1e-02 1.3e-02 1.01e+00 1.663139499e+02 1.667803791e+02 1.1e-07 0.29
26 1.8e-04 7.4e-02 1.1e-02 1.01e+00 1.663470167e+02 1.667666725e+02 9.7e-08 0.30
27 1.7e-04 6.7e-02 1.0e-02 1.01e+00 1.663766562e+02 1.667542395e+02 8.7e-08 0.31
28 1.5e-04 6.1e-02 9.1e-03 1.01e+00 1.664032653e+02 1.667430022e+02 7.9e-08 0.32
29 1.3e-04 5.6e-02 8.2e-03 1.01e+00 1.664271496e+02 1.667328408e+02 7.1e-08 0.33
30 1.2e-04 5.1e-02 7.4e-03 1.01e+00 1.664485904e+02 1.667236538e+02 6.4e-08 0.34
31 1.1e-04 4.7e-02 6.7e-03 1.01e+00 1.664678389e+02 1.667153482e+02 5.7e-08 0.34
32 9.8e-05 4.3e-02 6.0e-03 1.01e+00 1.664851201e+02 1.667078397e+02 5.2e-08 0.35
33 8.8e-05 3.9e-02 5.4e-03 1.00e+00 1.665006361e+02 1.667010524e+02 4.7e-08 0.36
34 7.9e-05 3.6e-02 4.9e-03 1.00e+00 1.665145680e+02 1.666949173e+02 4.2e-08 0.37
35 7.1e-05 3.3e-02 4.4e-03 1.00e+00 1.665270781e+02 1.666893721e+02 3.8e-08 0.37
36 6.4e-05 3.1e-02 3.9e-03 1.00e+00 1.665383122e+02 1.666843604e+02 3.4e-08 0.38
37 5.8e-05 2.9e-02 3.5e-03 1.00e+00 1.665484010e+02 1.666798312e+02 3.1e-08 0.39
38 5.2e-05 2.6e-02 3.2e-03 1.00e+00 1.665574617e+02 1.666757384e+02 2.7e-08 0.40
39 4.7e-05 2.5e-02 2.9e-03 1.00e+00 1.665655996e+02 1.666720402e+02 2.5e-08 0.40
40 4.2e-05 2.3e-02 2.6e-03 1.00e+00 1.665729091e+02 1.666686989e+02 2.2e-08 0.41
41 3.8e-05 2.1e-02 2.3e-03 1.00e+00 1.665794749e+02 1.666656804e+02 2.0e-08 0.42
42 3.4e-05 2.0e-02 2.1e-03 1.00e+00 1.665853730e+02 1.666629538e+02 1.8e-08 0.43
43 3.1e-05 1.9e-02 1.9e-03 1.00e+00 1.665906717e+02 1.666604911e+02 1.6e-08 0.43
44 2.8e-05 1.8e-02 1.7e-03 1.00e+00 1.665954321e+02 1.666582670e+02 1.5e-08 0.44
45 2.5e-05 1.7e-02 1.5e-03 1.00e+00 1.665997093e+02 1.666562586e+02 1.3e-08 0.45
46 2.2e-05 1.6e-02 1.4e-03 1.00e+00 1.666035525e+02 1.666544453e+02 1.2e-08 0.46
47 2.0e-05 1.5e-02 1.2e-03 1.00e+00 1.666070060e+02 1.666528083e+02 1.1e-08 0.46
48 1.8e-05 1.4e-02 1.1e-03 1.00e+00 1.666101095e+02 1.666513306e+02 9.6e-09 0.47
49 1.6e-05 1.4e-02 1.0e-03 1.00e+00 1.666128986e+02 1.666499970e+02 8.6e-09 0.48
50 1.5e-05 1.3e-02 9.0e-04 1.00e+00 1.666154055e+02 1.666487934e+02 7.8e-09 0.49
51 1.3e-05 1.3e-02 8.1e-04 1.00e+00 1.666176587e+02 1.666477075e+02 7.0e-09 0.50
52 1.2e-05 1.2e-02 7.3e-04 1.00e+00 1.666196841e+02 1.666467277e+02 6.3e-09 0.51
53 1.1e-05 1.2e-02 6.6e-04 1.00e+00 1.666215048e+02 1.666458439e+02 5.7e-09 0.52
54 9.6e-06 1.2e-02 5.9e-04 1.00e+00 1.666231416e+02 1.666450466e+02 5.1e-09 0.53
55 8.7e-06 1.1e-02 5.3e-04 1.00e+00 1.666246131e+02 1.666443276e+02 4.6e-09 0.54
56 7.8e-06 1.1e-02 4.8e-04 1.00e+00 1.666259362e+02 1.666436791e+02 4.1e-09 0.55
57 7.0e-06 1.1e-02 4.3e-04 1.00e+00 1.666271257e+02 1.666430944e+02 3.7e-09 0.56
58 6.3e-06 1.0e-02 3.9e-04 1.00e+00 1.666281953e+02 1.666425671e+02 3.3e-09 0.56
59 5.7e-06 1.0e-02 3.5e-04 1.00e+00 1.666291571e+02 1.666420917e+02 3.0e-09 0.57
60 5.1e-06 1.0e-02 3.1e-04 1.00e+00 1.666300219e+02 1.666416631e+02 2.7e-09 0.58
61 4.6e-06 9.8e-03 2.8e-04 1.00e+00 1.666307995e+02 1.666412766e+02 2.4e-09 0.58
62 4.2e-06 9.7e-03 2.5e-04 1.00e+00 1.666314988e+02 1.666409282e+02 2.2e-09 0.59
63 3.7e-06 9.5e-03 2.3e-04 1.00e+00 1.666321275e+02 1.666406140e+02 2.0e-09 0.60
64 3.4e-06 9.4e-03 2.1e-04 1.00e+00 1.666326929e+02 1.666403308e+02 1.8e-09 0.60
65 3.0e-06 9.3e-03 1.9e-04 1.00e+00 1.666332012e+02 1.666400754e+02 1.6e-09 0.61
66 2.7e-06 9.2e-03 1.7e-04 1.00e+00 1.666336584e+02 1.666398451e+02 1.4e-09 0.62
67 2.5e-06 9.1e-03 1.5e-04 1.00e+00 1.666340695e+02 1.666396376e+02 1.3e-09 0.62
68 2.2e-06 9.0e-03 1.4e-04 1.00e+00 1.666344393e+02 1.666394506e+02 1.2e-09 0.63
69 2.0e-06 8.9e-03 1.2e-04 1.00e+00 1.666347718e+02 1.666392821e+02 1.1e-09 0.64
70 1.8e-06 8.9e-03 1.1e-04 1.00e+00 1.666350710e+02 1.666391302e+02 9.5e-10 0.64
71 1.6e-06 8.8e-03 9.9e-05 1.00e+00 1.666353400e+02 1.666389933e+02 8.5e-10 0.65
72 1.4e-06 8.7e-03 8.9e-05 1.00e+00 1.666355820e+02 1.666388700e+02 7.7e-10 0.66
73 1.3e-06 8.7e-03 8.0e-05 1.00e+00 1.666357997e+02 1.666387589e+02 6.9e-10 0.66
74 1.2e-06 8.6e-03 7.2e-05 1.00e+00 1.666359954e+02 1.666386588e+02 6.2e-10 0.67
75 1.1e-06 8.6e-03 6.5e-05 1.00e+00 1.666361715e+02 1.666385685e+02 5.6e-10 0.68
76 9.5e-07 8.5e-03 5.8e-05 1.00e+00 1.666363299e+02 1.666384872e+02 5.0e-10 0.69
77 8.5e-07 8.5e-03 5.2e-05 1.00e+00 1.666364723e+02 1.666384139e+02 4.5e-10 0.69
78 7.7e-07 8.4e-03 4.7e-05 1.00e+00 1.666366004e+02 1.666383478e+02 4.1e-10 0.70
79 6.9e-07 8.4e-03 4.3e-05 1.00e+00 1.666367156e+02 1.666382883e+02 3.7e-10 0.71
80 6.2e-07 8.4e-03 3.8e-05 1.00e+00 1.666368191e+02 1.666382346e+02 3.3e-10 0.71
81 5.6e-07 8.3e-03 3.4e-05 1.00e+00 1.666369123e+02 1.666381862e+02 3.0e-10 0.72
82 5.0e-07 8.3e-03 3.1e-05 1.00e+00 1.666369960e+02 1.666381425e+02 2.7e-10 0.73
83 4.5e-07 8.3e-03 2.8e-05 1.00e+00 1.666370713e+02 1.666381032e+02 2.4e-10 0.73
84 4.1e-07 8.2e-03 2.5e-05 1.00e+00 1.666371390e+02 1.666380677e+02 2.2e-10 0.74
85 3.7e-07 8.2e-03 2.3e-05 1.00e+00 1.666371999e+02 1.666380357e+02 1.9e-10 0.75
86 3.3e-07 8.2e-03 2.0e-05 1.00e+00 1.666372547e+02 1.666380069e+02 1.8e-10 0.76
87 3.0e-07 8.2e-03 1.8e-05 1.00e+00 1.666373039e+02 1.666379810e+02 1.6e-10 0.78
88 2.7e-07 8.1e-03 1.6e-05 1.00e+00 1.666373482e+02 1.666379576e+02 1.4e-10 0.79
89 2.4e-07 8.1e-03 1.5e-05 1.00e+00 1.666373881e+02 1.666379365e+02 1.3e-10 0.80
90 2.2e-07 8.1e-03 1.3e-05 1.00e+00 1.666374239e+02 1.666379175e+02 1.2e-10 0.81
91 2.0e-07 8.1e-03 1.2e-05 1.00e+00 1.666374562e+02 1.666379004e+02 1.0e-10 0.82
92 1.8e-07 8.0e-03 1.1e-05 9.99e-01 1.666374852e+02 1.666378850e+02 9.3e-11 0.83
93 1.6e-07 8.0e-03 9.7e-06 1.00e+00 1.666375113e+02 1.666378711e+02 8.4e-11 0.84
94 1.4e-07 8.0e-03 8.8e-06 1.00e+00 1.666375348e+02 1.666378586e+02 7.6e-11 0.85
95 1.3e-07 8.0e-03 7.9e-06 1.00e+00 1.666375559e+02 1.666378474e+02 6.8e-11 0.87
96 1.2e-07 8.0e-03 7.1e-06 1.00e+00 1.666375750e+02 1.666378372e+02 6.1e-11 0.88
97 1.0e-07 8.0e-03 6.4e-06 1.00e+00 1.666375921e+02 1.666378281e+02 5.5e-11 0.89
98 9.4e-08 7.9e-03 5.7e-06 1.00e+00 1.666376075e+02 1.666378199e+02 5.0e-11 0.90
99 8.4e-08 7.9e-03 5.2e-06 1.00e+00 1.666376213e+02 1.666378126e+02 4.5e-11 0.91
100 7.6e-08 7.9e-03 4.7e-06 1.00e+00 1.666376338e+02 1.666378059e+02 4.0e-11 0.92
101 6.8e-08 7.9e-03 4.2e-06 1.00e+00 1.666376450e+02 1.666377999e+02 3.6e-11 0.93
102 6.1e-08 7.9e-03 3.8e-06 9.99e-01 1.666376551e+02 1.666377945e+02 3.3e-11 0.94
103 5.5e-08 7.8e-03 3.4e-06 1.00e+00 1.666376642e+02 1.666377897e+02 2.9e-11 0.95
104 5.0e-08 7.8e-03 3.1e-06 9.99e-01 1.666376724e+02 1.666377853e+02 2.6e-11 0.96
105 4.5e-08 7.8e-03 2.7e-06 9.99e-01 1.666376798e+02 1.666377814e+02 2.4e-11 0.97
106 4.0e-08 7.8e-03 2.5e-06 1.00e+00 1.666376864e+02 1.666377779e+02 2.1e-11 0.98
107 3.6e-08 7.0e-03 2.2e-06 1.00e+00 1.666376924e+02 1.666377747e+02 1.9e-11 0.99
108 3.3e-08 6.3e-03 2.0e-06 1.00e+00 1.666376978e+02 1.666377718e+02 1.7e-11 1.00
109 2.9e-08 5.7e-03 1.8e-06 1.00e+00 1.666377026e+02 1.666377692e+02 1.6e-11 1.01
110 2.6e-08 5.1e-03 1.6e-06 1.00e+00 1.666377069e+02 1.666377669e+02 1.4e-11 1.01
111 2.4e-08 4.6e-03 1.5e-06 1.00e+00 1.666377109e+02 1.666377648e+02 1.3e-11 1.02
112 2.1e-08 4.1e-03 1.3e-06 9.97e-01 1.666377144e+02 1.666377629e+02 1.1e-11 1.03
113 1.9e-08 3.7e-03 1.2e-06 9.99e-01 1.666377176e+02 1.666377612e+02 1.0e-11 1.04
114 1.7e-08 3.4e-03 1.1e-06 9.99e-01 1.666377204e+02 1.666377597e+02 9.2e-12 1.05
115 1.6e-08 3.0e-03 9.6e-07 9.99e-01 1.666377230e+02 1.666377583e+02 8.3e-12 1.06
116 1.4e-08 2.7e-03 8.6e-07 1.00e+00 1.666377253e+02 1.666377571e+02 7.5e-12 1.06
117 1.3e-08 2.4e-03 7.8e-07 9.90e-01 1.666377273e+02 1.666377561e+02 6.7e-12 1.07
118 1.1e-08 2.2e-03 7.0e-07 1.00e+00 1.666377292e+02 1.666377551e+02 6.0e-12 1.08
119 1.0e-08 2.0e-03 6.3e-07 9.96e-01 1.666377309e+02 1.666377542e+02 5.4e-12 1.09
120 9.3e-09 1.8e-03 5.7e-07 1.00e+00 1.666377324e+02 1.666377534e+02 4.9e-12 1.09
121 8.3e-09 1.6e-03 5.1e-07 1.00e+00 1.666377338e+02 1.666377526e+02 4.4e-12 1.10
122 7.5e-09 1.4e-03 4.6e-07 1.01e+00 1.666377350e+02 1.666377519e+02 4.0e-12 1.11
123 6.8e-09 1.3e-03 4.1e-07 1.01e+00 1.666377362e+02 1.666377513e+02 3.6e-12 1.13
124 6.1e-09 1.2e-03 3.7e-07 1.01e+00 1.666377372e+02 1.666377507e+02 3.3e-12 1.14
125 5.5e-09 1.1e-03 3.3e-07 9.99e-01 1.666377381e+02 1.666377503e+02 2.9e-12 1.15
126 5.0e-09 9.5e-04 3.0e-07 1.01e+00 1.666377389e+02 1.666377498e+02 2.7e-12 1.16
127 4.5e-09 8.5e-04 2.7e-07 1.02e+00 1.666377397e+02 1.666377494e+02 2.4e-12 1.17
128 5.6e-08 1.1e-05 3.5e-09 7.43e-01 1.666377472e+02 1.666377474e+02 4.8e-13 1.18
Optimizer terminated. Time: 1.18
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6663774725e+02 nrm: 2e+01 Viol. con: 2e-06 var: 0e+00
Dual. obj: 1.6663774741e+02 nrm: 9e+02 Viol. con: 0e+00 var: 1e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.22 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 868
Optimizer - Cones : 0
Optimizer - Scalar variables : 3451 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05
Factor - dense dim. : 0 flops : 2.93e+07
Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237753739e+05 2.000000000e+00 1.0e+00 0.03
1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230370335e+05 2.621294786e+00 7.3e-01 0.04
2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.207091912e+05 4.644578295e+00 3.8e-01 0.05
3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.117445296e+05 2.001309028e+01 1.3e-01 0.06
4 2.9e+02 4.6e+02 1.6e+04 -7.72e-01 -1.095031374e+05 1.974666468e+03 1.3e-01 0.07
5 1.2e+02 1.9e+02 6.4e+03 -7.62e-01 -8.799037449e+04 6.314305350e+03 5.3e-02 0.07
6 4.2e+01 6.6e+01 2.3e+03 -4.47e-01 -4.984556168e+04 1.081696070e+04 1.8e-02 0.08
7 2.5e+01 4.0e+01 1.4e+03 1.91e-01 -3.456473041e+04 7.453847367e+03 1.1e-02 0.09
8 1.3e+01 2.0e+01 7.0e+02 4.82e-01 -1.966103600e+04 4.634640429e+03 5.7e-03 0.10
9 4.9e+00 7.7e+00 2.7e+02 7.41e-01 -7.622087862e+03 2.281743691e+03 2.2e-03 0.11
10 2.3e+00 3.7e+00 1.3e+02 9.30e-01 -3.406598713e+03 1.397641560e+03 1.0e-03 0.11
11 1.5e+00 2.3e+00 8.1e+01 9.81e-01 -2.141147845e+03 9.482776310e+02 6.7e-04 0.12
12 8.6e-01 1.4e+00 4.7e+01 9.88e-01 -1.174998359e+03 6.210539829e+02 3.9e-04 0.13
13 7.5e-01 1.2e+00 4.1e+01 9.55e-01 -1.042162751e+03 5.605880191e+02 3.4e-04 0.13
14 3.8e-01 6.2e-01 2.1e+01 9.87e-01 -4.228247028e+02 3.771747290e+02 1.7e-04 0.14
15 1.8e-01 3.1e-01 1.0e+01 9.99e-01 -1.361354275e+02 2.593484518e+02 8.5e-05 0.15
16 9.2e-02 1.8e-01 5.2e+00 1.01e+00 7.062921614e+00 2.057327727e+02 4.3e-05 0.15
17 8.9e-02 1.7e-01 5.0e+00 1.01e+00 1.638500422e+01 2.077013944e+02 4.1e-05 0.16
18 6.2e-02 1.2e-01 3.5e+00 1.01e+00 6.254439192e+01 1.952098048e+02 2.9e-05 0.17
19 3.0e-02 7.9e-02 1.7e+00 1.01e+00 1.175697610e+02 1.808611984e+02 1.4e-05 0.18
20 8.5e-03 1.8e-01 4.9e-01 1.01e+00 1.531753702e+02 1.715704380e+02 4.0e-06 0.19
21 2.5e-03 1.9e-01 1.5e-01 1.00e+00 1.623486761e+02 1.679511923e+02 1.2e-06 0.20
22 1.5e-03 1.2e-01 8.6e-02 1.00e+00 1.641427991e+02 1.674087189e+02 7.3e-07 0.21
23 5.2e-04 1.0e-01 3.1e-02 1.01e+00 1.656943758e+02 1.668625159e+02 2.6e-07 0.22
24 1.9e-04 1.0e-01 1.2e-02 1.01e+00 1.662226038e+02 1.666602047e+02 1.0e-07 0.23
25 1.7e-04 9.1e-02 1.1e-02 1.01e+00 1.662565312e+02 1.666502281e+02 9.1e-08 0.25
26 1.5e-04 8.3e-02 9.5e-03 1.01e+00 1.662843877e+02 1.666385768e+02 8.2e-08 0.26
27 1.4e-04 7.5e-02 8.5e-03 1.01e+00 1.663096002e+02 1.666282610e+02 7.3e-08 0.27
28 1.2e-04 6.8e-02 7.7e-03 1.01e+00 1.663321764e+02 1.666188810e+02 6.6e-08 0.27
29 1.1e-04 6.2e-02 6.9e-03 1.01e+00 1.663524351e+02 1.666103947e+02 5.9e-08 0.28
30 1.0e-04 5.7e-02 6.2e-03 1.01e+00 1.663706092e+02 1.666027116e+02 5.4e-08 0.29
31 9.1e-05 5.2e-02 5.6e-03 1.01e+00 1.663869151e+02 1.665957570e+02 4.8e-08 0.31
32 8.2e-05 4.8e-02 5.0e-03 1.01e+00 1.664015458e+02 1.665894624e+02 4.3e-08 0.32
33 7.4e-05 4.4e-02 4.5e-03 1.01e+00 1.664146744e+02 1.665837659e+02 3.9e-08 0.33
34 6.6e-05 4.0e-02 4.1e-03 1.01e+00 1.664264566e+02 1.665786118e+02 3.5e-08 0.34
35 6.0e-05 3.7e-02 3.7e-03 1.01e+00 1.664370315e+02 1.665739492e+02 3.2e-08 0.35
36 5.4e-05 3.4e-02 3.3e-03 1.00e+00 1.664465241e+02 1.665697322e+02 2.8e-08 0.36
37 4.8e-05 3.1e-02 3.0e-03 1.00e+00 1.664550460e+02 1.665659190e+02 2.6e-08 0.37
38 4.4e-05 2.9e-02 2.7e-03 1.00e+00 1.664626974e+02 1.665624716e+02 2.3e-08 0.38
39 3.9e-05 2.7e-02 2.4e-03 1.00e+00 1.664695680e+02 1.665593556e+02 2.1e-08 0.40
40 3.5e-05 2.5e-02 2.2e-03 1.00e+00 1.664757382e+02 1.665565397e+02 1.9e-08 0.41
41 3.2e-05 2.3e-02 1.9e-03 1.00e+00 1.664812799e+02 1.665539954e+02 1.7e-08 0.42
42 2.9e-05 2.2e-02 1.8e-03 1.00e+00 1.664862576e+02 1.665516970e+02 1.5e-08 0.43
43 2.6e-05 2.0e-02 1.6e-03 1.00e+00 1.664907293e+02 1.665496211e+02 1.4e-08 0.44
44 2.3e-05 1.9e-02 1.4e-03 1.00e+00 1.664947468e+02 1.665477465e+02 1.2e-08 0.45
45 2.1e-05 1.8e-02 1.3e-03 1.00e+00 1.664983566e+02 1.665460541e+02 1.1e-08 0.46
46 1.9e-05 1.7e-02 1.2e-03 1.00e+00 1.665016004e+02 1.665445264e+02 9.9e-09 0.47
47 1.7e-05 1.6e-02 1.0e-03 1.00e+00 1.665045157e+02 1.665431477e+02 9.0e-09 0.48
48 1.5e-05 1.5e-02 9.3e-04 1.00e+00 1.665071361e+02 1.665419038e+02 8.1e-09 0.48
49 1.4e-05 1.5e-02 8.4e-04 1.00e+00 1.665094915e+02 1.665407817e+02 7.3e-09 0.49
50 1.2e-05 1.4e-02 7.6e-04 1.00e+00 1.665116092e+02 1.665397698e+02 6.5e-09 0.50
51 1.1e-05 1.3e-02 6.8e-04 1.00e+00 1.665135132e+02 1.665388573e+02 5.9e-09 0.50
52 1.0e-05 1.3e-02 6.1e-04 1.00e+00 1.665152253e+02 1.665380346e+02 5.3e-09 0.51
53 9.0e-06 1.2e-02 5.5e-04 1.00e+00 1.665167650e+02 1.665372932e+02 4.8e-09 0.52
54 8.1e-06 1.2e-02 5.0e-04 1.00e+00 1.665181497e+02 1.665366249e+02 4.3e-09 0.53
55 7.3e-06 1.1e-02 4.5e-04 1.00e+00 1.665193951e+02 1.665360228e+02 3.9e-09 0.54
56 6.5e-06 1.1e-02 4.0e-04 1.00e+00 1.665205154e+02 1.665354802e+02 3.5e-09 0.55
57 5.9e-06 1.1e-02 3.6e-04 1.00e+00 1.665215231e+02 1.665349914e+02 3.1e-09 0.56
58 5.3e-06 1.1e-02 3.3e-04 1.00e+00 1.665224295e+02 1.665345509e+02 2.8e-09 0.56
59 4.8e-06 1.0e-02 2.9e-04 1.00e+00 1.665232448e+02 1.665341542e+02 2.5e-09 0.57
60 4.3e-06 1.0e-02 2.6e-04 1.00e+00 1.665239782e+02 1.665337967e+02 2.3e-09 0.59
61 3.9e-06 9.9e-03 2.4e-04 1.00e+00 1.665246379e+02 1.665334746e+02 2.0e-09 0.60
62 3.5e-06 9.7e-03 2.1e-04 1.00e+00 1.665252313e+02 1.665331843e+02 1.8e-09 0.61
63 3.1e-06 9.6e-03 1.9e-04 1.00e+00 1.665257650e+02 1.665329227e+02 1.7e-09 0.62
64 2.8e-06 9.4e-03 1.7e-04 1.00e+00 1.665262450e+02 1.665326870e+02 1.5e-09 0.63
65 2.5e-06 9.3e-03 1.6e-04 1.00e+00 1.665266767e+02 1.665324746e+02 1.3e-09 0.64
66 2.3e-06 9.2e-03 1.4e-04 1.00e+00 1.665270651e+02 1.665322832e+02 1.2e-09 0.66
67 2.1e-06 9.1e-03 1.3e-04 1.00e+00 1.665274145e+02 1.665321108e+02 1.1e-09 0.67
68 1.8e-06 9.0e-03 1.1e-04 1.00e+00 1.665277288e+02 1.665319555e+02 9.8e-10 0.68
69 1.7e-06 8.9e-03 1.0e-04 1.00e+00 1.665280116e+02 1.665318156e+02 8.8e-10 0.69
70 1.5e-06 8.8e-03 9.2e-05 1.00e+00 1.665282659e+02 1.665316896e+02 7.9e-10 0.70
71 1.3e-06 8.7e-03 8.3e-05 1.00e+00 1.665284948e+02 1.665315761e+02 7.2e-10 0.70
72 1.2e-06 8.7e-03 7.4e-05 1.00e+00 1.665287006e+02 1.665314738e+02 6.4e-10 0.71
73 1.1e-06 8.6e-03 6.7e-05 1.00e+00 1.665288858e+02 1.665313817e+02 5.8e-10 0.72
74 9.8e-07 8.6e-03 6.0e-05 1.00e+00 1.665290524e+02 1.665312987e+02 5.2e-10 0.72
75 8.8e-07 8.5e-03 5.4e-05 1.00e+00 1.665292022e+02 1.665312239e+02 4.7e-10 0.73
76 7.9e-07 8.5e-03 4.9e-05 1.00e+00 1.665293369e+02 1.665311565e+02 4.2e-10 0.74
77 7.2e-07 8.4e-03 4.4e-05 1.00e+00 1.665294581e+02 1.665310958e+02 3.8e-10 0.74
78 6.4e-07 8.4e-03 4.0e-05 1.00e+00 1.665295672e+02 1.665310410e+02 3.4e-10 0.75
79 5.8e-07 8.3e-03 3.6e-05 1.00e+00 1.665296652e+02 1.665309917e+02 3.1e-10 0.76
80 5.2e-07 8.3e-03 3.2e-05 1.00e+00 1.665297533e+02 1.665309472e+02 2.8e-10 0.77
81 4.7e-07 8.3e-03 2.9e-05 1.00e+00 1.665298326e+02 1.665309071e+02 2.5e-10 0.77
82 4.2e-07 8.2e-03 2.6e-05 1.00e+00 1.665299039e+02 1.665308709e+02 2.2e-10 0.78
83 3.8e-07 8.2e-03 2.3e-05 1.00e+00 1.665299680e+02 1.665308384e+02 2.0e-10 0.79
84 3.4e-07 8.2e-03 2.1e-05 1.00e+00 1.665300257e+02 1.665308090e+02 1.8e-10 0.79
85 3.1e-07 8.2e-03 1.9e-05 1.00e+00 1.665300775e+02 1.665307825e+02 1.6e-10 0.80
86 2.8e-07 8.1e-03 1.7e-05 1.00e+00 1.665301241e+02 1.665307586e+02 1.5e-10 0.81
87 2.5e-07 8.1e-03 1.5e-05 1.00e+00 1.665301661e+02 1.665307371e+02 1.3e-10 0.82
88 2.2e-07 8.1e-03 1.4e-05 1.00e+00 1.665302038e+02 1.665307178e+02 1.2e-10 0.83
89 2.0e-07 8.1e-03 1.2e-05 1.00e+00 1.665302377e+02 1.665307003e+02 1.1e-10 0.83
90 1.8e-07 8.1e-03 1.1e-05 1.00e+00 1.665302683e+02 1.665306845e+02 9.7e-11 0.84
91 1.6e-07 8.0e-03 1.0e-05 1.00e+00 1.665302958e+02 1.665306704e+02 8.7e-11 0.85
92 1.5e-07 8.0e-03 9.1e-06 1.00e+00 1.665303205e+02 1.665306576e+02 7.8e-11 0.85
93 1.3e-07 8.0e-03 8.1e-06 1.00e+00 1.665303427e+02 1.665306462e+02 7.0e-11 0.86
94 1.2e-07 8.0e-03 7.3e-06 1.00e+00 1.665303627e+02 1.665306358e+02 6.3e-11 0.87
95 1.1e-07 7.9e-03 6.6e-06 1.00e+00 1.665303807e+02 1.665306265e+02 5.7e-11 0.88
96 9.7e-08 7.9e-03 5.9e-06 1.00e+00 1.665303969e+02 1.665306182e+02 5.1e-11 0.89
97 8.7e-08 7.9e-03 5.3e-06 1.00e+00 1.665304115e+02 1.665306106e+02 4.6e-11 0.91
98 7.8e-08 7.9e-03 4.8e-06 1.00e+00 1.665304246e+02 1.665306038e+02 4.2e-11 0.92
99 7.0e-08 7.9e-03 4.3e-06 1.00e+00 1.665304364e+02 1.665305977e+02 3.7e-11 0.93
100 6.3e-08 7.9e-03 3.9e-06 1.00e+00 1.665304471e+02 1.665305922e+02 3.4e-11 0.94
101 5.7e-08 7.8e-03 3.5e-06 9.99e-01 1.665304566e+02 1.665305873e+02 3.0e-11 0.95
102 5.1e-08 7.8e-03 3.2e-06 9.99e-01 1.665304652e+02 1.665305828e+02 2.7e-11 0.96
103 1.3e-07 7.6e-03 3.1e-06 9.90e-01 1.665304639e+02 1.665305917e+02 2.6e-11 0.97
104 1.3e-07 7.3e-03 2.8e-06 1.00e+00 1.665304717e+02 1.665305876e+02 2.4e-11 0.98
105 1.2e-07 7.3e-03 2.5e-06 9.99e-01 1.665304788e+02 1.665305831e+02 2.1e-11 0.99
106 1.1e-07 7.3e-03 2.2e-06 9.97e-01 1.665304851e+02 1.665305790e+02 1.9e-11 0.99
107 9.5e-08 7.2e-03 2.0e-06 1.00e+00 1.665304909e+02 1.665305754e+02 1.7e-11 1.00
108 8.5e-08 7.2e-03 1.8e-06 1.00e+00 1.665304961e+02 1.665305721e+02 1.6e-11 1.01
109 7.7e-08 7.1e-03 1.6e-06 9.97e-01 1.665305008e+02 1.665305691e+02 1.4e-11 1.01
110 6.9e-08 7.1e-03 1.5e-06 1.00e+00 1.665305050e+02 1.665305665e+02 1.3e-11 1.02
111 6.2e-08 7.1e-03 1.3e-06 9.99e-01 1.665305087e+02 1.665305641e+02 1.1e-11 1.03
112 5.6e-08 6.4e-03 1.2e-06 1.01e+00 1.665305122e+02 1.665305619e+02 1.0e-11 1.03
113 5.0e-08 5.7e-03 1.1e-06 1.00e+00 1.665305152e+02 1.665305600e+02 9.2e-12 1.04
114 4.6e-08 5.2e-03 9.7e-07 9.95e-01 1.665305180e+02 1.665305583e+02 8.3e-12 1.05
115 4.1e-08 4.6e-03 8.7e-07 1.00e+00 1.665305204e+02 1.665305567e+02 7.5e-12 1.05
116 3.7e-08 4.2e-03 7.8e-07 9.93e-01 1.665305227e+02 1.665305553e+02 6.7e-12 1.06
117 3.3e-08 3.8e-03 7.0e-07 1.00e+00 1.665305247e+02 1.665305540e+02 6.1e-12 1.07
118 8.3e-08 3.4e-03 6.3e-07 9.34e-01 1.665305257e+02 1.665305588e+02 5.3e-12 1.07
119 4.3e-08 3.0e-03 5.7e-07 1.01e+00 1.665305272e+02 1.665305547e+02 4.7e-12 1.08
120 4.3e-08 2.7e-03 5.1e-07 9.21e-01 1.665305288e+02 1.665305507e+02 4.1e-12 1.09
121 2.7e-08 2.5e-03 4.6e-07 9.95e-01 1.665305300e+02 1.665305510e+02 3.7e-12 1.10
122 2.5e-08 2.3e-03 4.2e-07 1.01e+00 1.665305312e+02 1.665305502e+02 3.4e-12 1.11
123 2.4e-08 2.0e-03 3.7e-07 9.96e-01 1.665305324e+02 1.665305495e+02 3.0e-12 1.12
124 2.2e-08 1.8e-03 3.4e-07 9.97e-01 1.665305334e+02 1.665305488e+02 2.7e-12 1.13
125 2.0e-08 1.6e-03 3.0e-07 1.00e+00 1.665305343e+02 1.665305482e+02 2.4e-12 1.13
126 1.8e-08 1.5e-03 2.7e-07 1.00e+00 1.665305352e+02 1.665305476e+02 2.2e-12 1.14
127 2.6e-08 1.3e-03 2.4e-07 1.00e+00 1.665305363e+02 1.665305471e+02 2.0e-12 1.15
128 5.3e-08 1.2e-03 2.2e-07 9.12e-01 1.665305367e+02 1.665305467e+02 1.9e-12 1.16
129 4.1e-08 1.1e-03 2.0e-07 1.01e+00 1.665305373e+02 1.665305462e+02 1.7e-12 1.17
130 3.7e-08 1.0e-03 1.8e-07 1.00e+00 1.665305380e+02 1.665305459e+02 1.5e-12 1.18
131 3.3e-08 9.1e-04 1.6e-07 1.00e+00 1.665305385e+02 1.665305455e+02 1.4e-12 1.19
132 3.0e-08 8.2e-04 1.4e-07 9.95e-01 1.665305389e+02 1.665305453e+02 1.2e-12 1.20
133 2.7e-08 7.4e-04 1.3e-07 1.00e+00 1.665305393e+02 1.665305450e+02 1.1e-12 1.21
134 2.5e-08 6.6e-04 1.2e-07 1.00e+00 1.665305396e+02 1.665305448e+02 9.9e-13 1.22
Optimizer terminated. Time: 1.22
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6653053960e+02 nrm: 2e+01 Viol. con: 7e-07 var: 0e+00
Dual. obj: 1.6653054477e+02 nrm: 1e+03 Viol. con: 0e+00 var: 6e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.25 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (312) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 868
Optimizer - Cones : 0
Optimizer - Scalar variables : 3451 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05
Factor - dense dim. : 0 flops : 2.93e+07
Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237723965e+05 2.000000000e+00 1.0e+00 0.04
1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230338911e+05 2.619367871e+00 7.3e-01 0.04
2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.207104755e+05 4.635090693e+00 3.8e-01 0.05
3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.116924132e+05 2.006515812e+01 1.3e-01 0.06
4 2.9e+02 4.6e+02 1.6e+04 -7.72e-01 -1.094707951e+05 1.962598695e+03 1.3e-01 0.06
5 1.2e+02 1.9e+02 6.4e+03 -7.62e-01 -8.788226104e+04 6.303856314e+03 5.2e-02 0.07
6 3.3e+01 5.2e+01 1.8e+03 -4.45e-01 -4.126301059e+04 1.179599132e+04 1.5e-02 0.08
7 2.0e+01 3.2e+01 1.1e+03 3.46e-01 -2.865074013e+04 7.420402322e+03 9.0e-03 0.08
8 1.0e+01 1.6e+01 5.5e+02 5.88e-01 -1.559269793e+04 4.104339917e+03 4.5e-03 0.09
9 3.8e+00 6.0e+00 2.1e+02 8.10e-01 -5.894597930e+03 1.898576709e+03 1.7e-03 0.10
10 2.1e+00 3.3e+00 1.1e+02 9.51e-01 -3.065562116e+03 1.212591869e+03 9.2e-04 0.10
11 8.8e-01 1.4e+00 4.8e+01 9.86e-01 -1.199429749e+03 6.419680197e+02 4.0e-04 0.11
12 8.4e-01 1.3e+00 4.6e+01 9.64e-01 -1.163808416e+03 6.115786890e+02 3.8e-04 0.12
13 5.3e-01 8.3e-01 2.9e+01 9.74e-01 -6.960284870e+02 4.363811472e+02 2.4e-04 0.12
14 3.5e-01 5.5e-01 1.9e+01 1.00e+00 -3.813368667e+02 3.597045054e+02 1.6e-04 0.13
15 1.4e-01 2.3e-01 7.7e+00 9.97e-01 -6.719842854e+01 2.314917281e+02 6.5e-05 0.14
16 8.5e-02 1.5e-01 4.7e+00 1.01e+00 2.005116100e+01 2.025960004e+02 4.0e-05 0.15
17 8.2e-02 1.4e-01 4.6e+00 1.02e+00 2.553737299e+01 2.015018767e+02 3.8e-05 0.15
18 5.7e-02 1.0e-01 3.2e+00 1.02e+00 7.030708921e+01 1.929667335e+02 2.7e-05 0.16
19 1.8e-02 8.3e-02 1.0e+00 1.02e+00 1.375642693e+02 1.754927782e+02 8.4e-06 0.17
20 5.4e-03 1.9e-01 3.1e-01 1.01e+00 1.579583233e+02 1.696376159e+02 2.6e-06 0.17
21 3.0e-03 2.2e-01 1.8e-01 1.01e+00 1.615621834e+02 1.681592421e+02 1.5e-06 0.18
22 1.1e-03 1.2e-01 6.4e-02 1.01e+00 1.647466837e+02 1.671515795e+02 5.4e-07 0.19
23 3.3e-04 1.2e-01 2.0e-02 1.01e+00 1.659527749e+02 1.666952723e+02 1.7e-07 0.19
24 1.5e-04 9.6e-02 9.0e-03 1.01e+00 1.662411411e+02 1.665782592e+02 7.8e-08 0.20
25 1.3e-04 8.8e-02 8.1e-03 1.01e+00 1.662670615e+02 1.665704340e+02 7.0e-08 0.21
26 1.2e-04 8.0e-02 7.3e-03 1.01e+00 1.662882724e+02 1.665611881e+02 6.3e-08 0.22
27 1.1e-04 7.2e-02 6.6e-03 1.01e+00 1.663074622e+02 1.665530014e+02 5.7e-08 0.22
28 9.6e-05 6.6e-02 5.9e-03 1.01e+00 1.663246400e+02 1.665455534e+02 5.1e-08 0.23
29 8.7e-05 6.0e-02 5.3e-03 1.01e+00 1.663400561e+02 1.665388193e+02 4.6e-08 0.24
30 7.8e-05 5.5e-02 4.8e-03 1.01e+00 1.663538858e+02 1.665327239e+02 4.2e-08 0.24
31 7.0e-05 5.0e-02 4.3e-03 1.01e+00 1.663662942e+02 1.665272085e+02 3.7e-08 0.25
32 6.3e-05 4.6e-02 3.9e-03 1.01e+00 1.663774282e+02 1.665222182e+02 3.4e-08 0.26
33 5.7e-05 4.2e-02 3.5e-03 1.01e+00 1.663874199e+02 1.665177040e+02 3.0e-08 0.27
34 5.1e-05 3.9e-02 3.2e-03 1.01e+00 1.663963874e+02 1.665136211e+02 2.7e-08 0.28
35 4.6e-05 3.6e-02 2.8e-03 1.01e+00 1.664044369e+02 1.665099292e+02 2.5e-08 0.29
36 4.1e-05 3.3e-02 2.6e-03 1.00e+00 1.664116630e+02 1.665065915e+02 2.2e-08 0.30
37 3.7e-05 3.0e-02 2.3e-03 1.00e+00 1.664181509e+02 1.665035746e+02 2.0e-08 0.31
38 3.4e-05 2.8e-02 2.1e-03 1.00e+00 1.664239766e+02 1.665008483e+02 1.8e-08 0.32
39 3.0e-05 2.6e-02 1.9e-03 1.00e+00 1.664292085e+02 1.664983851e+02 1.6e-08 0.33
40 2.7e-05 2.4e-02 1.7e-03 1.00e+00 1.664339074e+02 1.664961602e+02 1.5e-08 0.33
41 2.4e-05 2.3e-02 1.5e-03 1.00e+00 1.664381284e+02 1.664941507e+02 1.3e-08 0.34
42 2.2e-05 2.1e-02 1.4e-03 1.00e+00 1.664419202e+02 1.664923363e+02 1.2e-08 0.35
43 2.0e-05 2.0e-02 1.2e-03 1.00e+00 1.664453271e+02 1.664906982e+02 1.1e-08 0.35
44 1.8e-05 1.9e-02 1.1e-03 1.00e+00 1.664483883e+02 1.664892197e+02 9.5e-09 0.36
45 1.6e-05 1.8e-02 9.9e-04 1.00e+00 1.664511392e+02 1.664878854e+02 8.6e-09 0.37
46 1.4e-05 1.7e-02 8.9e-04 1.00e+00 1.664536115e+02 1.664866815e+02 7.7e-09 0.38
47 1.3e-05 1.6e-02 8.0e-04 1.00e+00 1.664558338e+02 1.664855955e+02 7.0e-09 0.38
48 1.2e-05 1.5e-02 7.2e-04 1.00e+00 1.664578313e+02 1.664846159e+02 6.3e-09 0.39
49 1.1e-05 1.4e-02 6.5e-04 1.00e+00 1.664596272e+02 1.664837325e+02 5.6e-09 0.40
50 9.5e-06 1.4e-02 5.9e-04 1.00e+00 1.664612418e+02 1.664829359e+02 5.1e-09 0.40
51 8.5e-06 1.3e-02 5.3e-04 1.00e+00 1.664626936e+02 1.664822179e+02 4.6e-09 0.41
52 7.7e-06 1.3e-02 4.7e-04 1.00e+00 1.664639992e+02 1.664815706e+02 4.1e-09 0.42
53 6.9e-06 1.2e-02 4.3e-04 1.00e+00 1.664651733e+02 1.664809873e+02 3.7e-09 0.43
54 6.2e-06 1.2e-02 3.8e-04 1.00e+00 1.664662292e+02 1.664804617e+02 3.3e-09 0.43
55 5.6e-06 1.1e-02 3.5e-04 1.00e+00 1.664671790e+02 1.664799881e+02 3.0e-09 0.44
56 5.0e-06 1.1e-02 3.1e-04 1.00e+00 1.664680333e+02 1.664795614e+02 2.7e-09 0.45
57 4.5e-06 1.1e-02 2.8e-04 1.00e+00 1.664688018e+02 1.664791770e+02 2.4e-09 0.45
58 4.1e-06 1.0e-02 2.5e-04 1.00e+00 1.664694931e+02 1.664788307e+02 2.2e-09 0.46
59 3.7e-06 1.0e-02 2.3e-04 1.00e+00 1.664701149e+02 1.664785187e+02 2.0e-09 0.47
60 3.3e-06 9.9e-03 2.0e-04 1.00e+00 1.664706742e+02 1.664782377e+02 1.8e-09 0.47
61 3.0e-06 9.7e-03 1.8e-04 1.00e+00 1.664711774e+02 1.664779845e+02 1.6e-09 0.48
62 2.7e-06 9.5e-03 1.7e-04 1.00e+00 1.664716301e+02 1.664777565e+02 1.4e-09 0.49
63 2.4e-06 9.4e-03 1.5e-04 1.00e+00 1.664720374e+02 1.664775512e+02 1.3e-09 0.49
64 2.2e-06 9.2e-03 1.3e-04 1.00e+00 1.664724039e+02 1.664773663e+02 1.2e-09 0.50
65 2.0e-06 9.1e-03 1.2e-04 1.00e+00 1.664727338e+02 1.664771999e+02 1.0e-09 0.51
66 1.8e-06 9.0e-03 1.1e-04 1.00e+00 1.664730306e+02 1.664770501e+02 9.4e-10 0.52
67 1.6e-06 8.9e-03 9.8e-05 1.00e+00 1.664732977e+02 1.664769153e+02 8.5e-10 0.52
68 1.4e-06 8.8e-03 8.8e-05 1.00e+00 1.664735380e+02 1.664767939e+02 7.6e-10 0.53
69 1.3e-06 8.7e-03 7.9e-05 1.00e+00 1.664737543e+02 1.664766846e+02 6.9e-10 0.54
70 1.2e-06 8.6e-03 7.1e-05 1.00e+00 1.664739490e+02 1.664765862e+02 6.2e-10 0.54
71 1.0e-06 8.5e-03 6.4e-05 1.00e+00 1.664741241e+02 1.664764977e+02 5.6e-10 0.55
72 9.3e-07 8.4e-03 5.8e-05 1.00e+00 1.664742818e+02 1.664764180e+02 5.0e-10 0.56
73 8.4e-07 8.4e-03 5.2e-05 1.00e+00 1.664744236e+02 1.664763462e+02 4.5e-10 0.57
74 7.6e-07 8.3e-03 4.7e-05 1.00e+00 1.664745512e+02 1.664762816e+02 4.0e-10 0.57
75 6.8e-07 8.3e-03 4.2e-05 1.00e+00 1.664746661e+02 1.664762234e+02 3.6e-10 0.58
76 6.1e-07 8.2e-03 3.8e-05 1.00e+00 1.664747694e+02 1.664761710e+02 3.3e-10 0.59
77 5.5e-07 8.2e-03 3.4e-05 1.00e+00 1.664748623e+02 1.664761238e+02 3.0e-10 0.60
78 5.0e-07 8.1e-03 3.1e-05 1.00e+00 1.664749459e+02 1.664760812e+02 2.7e-10 0.60
79 4.5e-07 8.1e-03 2.8e-05 1.00e+00 1.664750211e+02 1.664760429e+02 2.4e-10 0.61
80 4.0e-07 8.0e-03 2.5e-05 1.00e+00 1.664750888e+02 1.664760084e+02 2.2e-10 0.62
81 3.6e-07 8.0e-03 2.2e-05 1.00e+00 1.664751496e+02 1.664759773e+02 1.9e-10 0.62
82 3.3e-07 8.0e-03 2.0e-05 1.00e+00 1.664752044e+02 1.664759493e+02 1.7e-10 0.63
83 2.9e-07 8.0e-03 1.8e-05 1.00e+00 1.664752536e+02 1.664759240e+02 1.6e-10 0.64
84 2.6e-07 7.9e-03 1.6e-05 1.00e+00 1.664752979e+02 1.664759013e+02 1.4e-10 0.65
85 2.4e-07 7.9e-03 1.5e-05 1.00e+00 1.664753378e+02 1.664758808e+02 1.3e-10 0.66
86 2.1e-07 7.9e-03 1.3e-05 1.00e+00 1.664753737e+02 1.664758624e+02 1.1e-10 0.66
87 1.9e-07 7.9e-03 1.2e-05 1.00e+00 1.664754059e+02 1.664758458e+02 1.0e-10 0.67
88 1.7e-07 7.8e-03 1.1e-05 1.00e+00 1.664754350e+02 1.664758309e+02 9.3e-11 0.68
89 1.6e-07 7.8e-03 9.6e-06 1.00e+00 1.664754611e+02 1.664758175e+02 8.3e-11 0.68
90 1.4e-07 7.8e-03 8.7e-06 1.00e+00 1.664754846e+02 1.664758053e+02 7.5e-11 0.69
91 1.3e-07 7.0e-03 7.8e-06 1.00e+00 1.664755058e+02 1.664757942e+02 6.8e-11 0.70
92 1.1e-07 6.3e-03 7.0e-06 1.00e+00 1.664755248e+02 1.664757844e+02 6.1e-11 0.70
93 1.0e-07 5.7e-03 6.3e-06 1.00e+00 1.664755420e+02 1.664757756e+02 5.5e-11 0.71
94 9.2e-08 5.1e-03 5.7e-06 1.00e+00 1.664755574e+02 1.664757676e+02 4.9e-11 0.72
95 8.3e-08 4.6e-03 5.1e-06 9.99e-01 1.664755713e+02 1.664757605e+02 4.4e-11 0.73
96 7.4e-08 4.1e-03 4.6e-06 1.00e+00 1.664755837e+02 1.664757541e+02 4.0e-11 0.73
97 6.7e-08 3.7e-03 4.1e-06 1.00e+00 1.664755950e+02 1.664757483e+02 3.6e-11 0.74
98 6.0e-08 3.4e-03 3.7e-06 1.00e+00 1.664756051e+02 1.664757431e+02 3.2e-11 0.75
99 5.4e-08 3.0e-03 3.4e-06 9.99e-01 1.664756142e+02 1.664757384e+02 2.9e-11 0.75
100 4.9e-08 2.7e-03 3.0e-06 1.00e+00 1.664756224e+02 1.664757342e+02 2.6e-11 0.76
101 4.4e-08 2.4e-03 2.7e-06 1.00e+00 1.664756297e+02 1.664757304e+02 2.4e-11 0.77
102 4.0e-08 2.2e-03 2.4e-06 1.00e+00 1.664756364e+02 1.664757269e+02 2.1e-11 0.77
103 3.6e-08 2.0e-03 2.2e-06 1.00e+00 1.664756424e+02 1.664757238e+02 1.9e-11 0.78
104 3.2e-08 1.8e-03 2.0e-06 1.00e+00 1.664756477e+02 1.664757210e+02 1.7e-11 0.79
105 2.9e-08 1.6e-03 1.8e-06 1.00e+00 1.664756526e+02 1.664757185e+02 1.5e-11 0.79
106 2.6e-08 1.4e-03 1.6e-06 9.97e-01 1.664756569e+02 1.664757163e+02 1.4e-11 0.80
107 2.3e-08 1.3e-03 1.4e-06 9.98e-01 1.664756608e+02 1.664757143e+02 1.3e-11 0.81
108 2.1e-08 1.2e-03 1.3e-06 9.99e-01 1.664756644e+02 1.664757125e+02 1.1e-11 0.81
109 1.9e-08 1.1e-03 1.2e-06 1.00e+00 1.664756675e+02 1.664757108e+02 1.0e-11 0.82
110 1.7e-08 9.5e-04 1.1e-06 1.00e+00 1.664756704e+02 1.664757093e+02 9.1e-12 0.83
111 1.5e-08 8.5e-04 9.5e-07 1.00e+00 1.664756730e+02 1.664757080e+02 8.2e-12 0.84
112 1.4e-08 7.7e-04 8.5e-07 9.96e-01 1.664756753e+02 1.664757068e+02 7.4e-12 0.85
113 1.2e-08 6.9e-04 7.7e-07 1.01e+00 1.664756774e+02 1.664757057e+02 6.7e-12 0.85
114 1.1e-08 6.2e-04 6.9e-07 9.97e-01 1.664756793e+02 1.664757048e+02 6.0e-12 0.86
115 1.0e-08 5.6e-04 6.2e-07 1.01e+00 1.664756810e+02 1.664757039e+02 5.4e-12 0.87
116 9.1e-09 5.0e-04 5.6e-07 1.00e+00 1.664756825e+02 1.664757031e+02 4.9e-12 0.87
117 3.7e-09 5.2e-05 5.8e-08 1.00e+00 1.664756946e+02 1.664756968e+02 5.0e-13 0.88
Optimizer terminated. Time: 0.88
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6647569465e+02 nrm: 2e+01 Viol. con: 1e-07 var: 0e+00
Dual. obj: 1.6647569678e+02 nrm: 1e+03 Viol. con: 0e+00 var: 4e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.91 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (312) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 868
Optimizer - Cones : 0
Optimizer - Scalar variables : 3451 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05
Factor - dense dim. : 0 flops : 2.93e+07
Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237711052e+05 2.000000000e+00 1.0e+00 0.03
1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230327955e+05 2.618555380e+00 7.3e-01 0.04
2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.207105230e+05 4.631548915e+00 3.8e-01 0.05
3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.116593625e+05 2.009145839e+01 1.3e-01 0.06
4 2.9e+02 4.6e+02 1.6e+04 -7.71e-01 -1.094464055e+05 1.958106253e+03 1.3e-01 0.07
5 1.2e+02 1.9e+02 6.4e+03 -7.62e-01 -8.784887085e+04 6.286653597e+03 5.2e-02 0.08
6 2.8e+01 4.4e+01 1.5e+03 -4.45e-01 -3.521466166e+04 1.246995668e+04 1.2e-02 0.09
7 1.8e+01 2.8e+01 9.7e+02 4.59e-01 -2.555040771e+04 7.282601029e+03 8.0e-03 0.10
8 1.0e+01 1.6e+01 5.5e+02 6.44e-01 -1.530962368e+04 4.310256051e+03 4.5e-03 0.10
9 4.0e+00 6.3e+00 2.2e+02 8.15e-01 -6.206808585e+03 1.970157915e+03 1.8e-03 0.11
10 2.1e+00 3.3e+00 1.1e+02 9.47e-01 -3.076258621e+03 1.206432808e+03 9.2e-04 0.12
11 8.6e-01 1.4e+00 4.7e+01 9.86e-01 -1.172512749e+03 6.452584713e+02 3.9e-04 0.12
12 8.3e-01 1.3e+00 4.6e+01 9.58e-01 -1.152704090e+03 6.177874298e+02 3.8e-04 0.13
13 5.3e-01 8.4e-01 2.9e+01 9.71e-01 -6.979547615e+02 4.416984539e+02 2.4e-04 0.14
14 3.5e-01 5.6e-01 1.9e+01 1.00e+00 -3.846816526e+02 3.613124056e+02 1.6e-04 0.14
15 1.1e-01 2.1e-01 6.5e+00 9.97e-01 -3.287554343e+01 2.179223059e+02 5.4e-05 0.15
16 8.4e-02 1.5e-01 4.7e+00 1.02e+00 2.205475750e+01 2.043964349e+02 4.0e-05 0.16
17 5.0e-02 9.3e-02 2.8e+00 1.02e+00 8.341064309e+01 1.909653399e+02 2.4e-05 0.16
18 1.3e-02 1.6e-01 7.4e-01 1.02e+00 1.456020178e+02 1.736314114e+02 6.2e-06 0.17
19 4.1e-03 2.0e-01 2.4e-01 1.01e+00 1.597194211e+02 1.687954823e+02 2.0e-06 0.18
20 2.1e-03 2.3e-01 1.2e-01 1.01e+00 1.630439252e+02 1.676586776e+02 1.0e-06 0.18
21 6.3e-04 1.5e-01 3.8e-02 1.01e+00 1.654295900e+02 1.668596314e+02 3.2e-07 0.19
22 4.2e-04 1.1e-01 2.6e-02 9.98e-01 1.657668009e+02 1.667213273e+02 2.2e-07 0.20
23 2.5e-04 8.1e-02 1.5e-02 9.86e-01 1.660455576e+02 1.666106550e+02 1.3e-07 0.20
24 2.0e-04 6.9e-02 1.2e-02 9.99e-01 1.661253082e+02 1.665840040e+02 1.1e-07 0.21
25 1.8e-04 6.4e-02 1.1e-02 1.01e+00 1.661579659e+02 1.665705552e+02 9.5e-08 0.22
26 1.6e-04 5.8e-02 9.9e-03 1.01e+00 1.661869284e+02 1.665581251e+02 8.5e-08 0.22
27 1.5e-04 5.3e-02 8.9e-03 1.00e+00 1.662130795e+02 1.665471131e+02 7.7e-08 0.23
28 1.3e-04 4.8e-02 8.1e-03 1.00e+00 1.662365215e+02 1.665371132e+02 6.9e-08 0.24
29 1.2e-04 4.4e-02 7.2e-03 1.00e+00 1.662575651e+02 1.665280693e+02 6.2e-08 0.24
30 1.1e-04 4.0e-02 6.5e-03 1.00e+00 1.662764527e+02 1.665198850e+02 5.6e-08 0.25
31 9.5e-05 3.7e-02 5.9e-03 1.00e+00 1.662934068e+02 1.665124797e+02 5.0e-08 0.26
32 8.6e-05 3.4e-02 5.3e-03 1.00e+00 1.663086255e+02 1.665057792e+02 4.5e-08 0.27
33 7.7e-05 3.1e-02 4.8e-03 1.00e+00 1.663222870e+02 1.664997165e+02 4.1e-08 0.28
34 6.9e-05 2.9e-02 4.3e-03 1.00e+00 1.663345508e+02 1.664942311e+02 3.7e-08 0.29
35 6.2e-05 2.7e-02 3.9e-03 1.00e+00 1.663455607e+02 1.664892683e+02 3.3e-08 0.30
36 5.6e-05 2.5e-02 3.5e-03 1.00e+00 1.663554455e+02 1.664847790e+02 3.0e-08 0.31
37 5.1e-05 2.3e-02 3.1e-03 1.00e+00 1.663643208e+02 1.664807187e+02 2.7e-08 0.31
38 4.6e-05 2.2e-02 2.8e-03 1.00e+00 1.663722906e+02 1.664770470e+02 2.4e-08 0.32
39 4.1e-05 2.0e-02 2.5e-03 1.00e+00 1.663794477e+02 1.664737273e+02 2.2e-08 0.33
40 3.7e-05 1.9e-02 2.3e-03 1.00e+00 1.663858757e+02 1.664707266e+02 2.0e-08 0.33
41 3.3e-05 1.8e-02 2.0e-03 1.00e+00 1.663916493e+02 1.664680146e+02 1.8e-08 0.34
42 3.0e-05 1.7e-02 1.8e-03 1.00e+00 1.663968354e+02 1.664655639e+02 1.6e-08 0.35
43 2.7e-05 1.6e-02 1.7e-03 1.00e+00 1.664014943e+02 1.664633498e+02 1.4e-08 0.36
44 2.4e-05 1.5e-02 1.5e-03 1.00e+00 1.664056797e+02 1.664613496e+02 1.3e-08 0.36
45 2.2e-05 1.4e-02 1.3e-03 1.00e+00 1.664094400e+02 1.664595429e+02 1.2e-08 0.37
46 2.0e-05 1.4e-02 1.2e-03 1.00e+00 1.664128185e+02 1.664579112e+02 1.0e-08 0.38
47 1.8e-05 1.3e-02 1.1e-03 1.00e+00 1.664158542e+02 1.664564378e+02 9.4e-09 0.38
48 1.6e-05 1.3e-02 9.8e-04 1.00e+00 1.664185821e+02 1.664551074e+02 8.4e-09 0.39
49 1.4e-05 1.2e-02 8.8e-04 1.00e+00 1.664210334e+02 1.664539063e+02 7.6e-09 0.40
50 1.3e-05 1.2e-02 7.9e-04 1.00e+00 1.664232364e+02 1.664528222e+02 6.8e-09 0.41
51 1.2e-05 1.1e-02 7.2e-04 1.00e+00 1.664252163e+02 1.664518437e+02 6.1e-09 0.41
52 1.0e-05 1.1e-02 6.4e-04 1.00e+00 1.664269959e+02 1.664509607e+02 5.5e-09 0.42
53 9.4e-06 1.1e-02 5.8e-04 1.00e+00 1.664285955e+02 1.664501639e+02 5.0e-09 0.43
54 8.4e-06 1.0e-02 5.2e-04 1.00e+00 1.664300333e+02 1.664494451e+02 4.5e-09 0.43
55 7.6e-06 1.0e-02 4.7e-04 1.00e+00 1.664313259e+02 1.664487966e+02 4.0e-09 0.44
56 6.8e-06 9.9e-03 4.2e-04 1.00e+00 1.664324880e+02 1.664482118e+02 3.6e-09 0.45
57 6.2e-06 9.7e-03 3.8e-04 1.00e+00 1.664335328e+02 1.664476843e+02 3.3e-09 0.45
58 5.5e-06 9.6e-03 3.4e-04 1.00e+00 1.664344722e+02 1.664472086e+02 2.9e-09 0.46
59 5.0e-06 9.4e-03 3.1e-04 1.00e+00 1.664353168e+02 1.664467797e+02 2.6e-09 0.47
60 4.5e-06 9.3e-03 2.8e-04 1.00e+00 1.664360762e+02 1.664463929e+02 2.4e-09 0.48
61 4.0e-06 9.1e-03 2.5e-04 1.00e+00 1.664367591e+02 1.664460442e+02 2.1e-09 0.48
62 3.6e-06 9.0e-03 2.2e-04 1.00e+00 1.664373731e+02 1.664457298e+02 1.9e-09 0.49
63 3.3e-06 8.9e-03 2.0e-04 1.00e+00 1.664379253e+02 1.664454463e+02 1.7e-09 0.50
64 2.9e-06 8.8e-03 1.8e-04 1.00e+00 1.664384218e+02 1.664451908e+02 1.6e-09 0.51
65 2.6e-06 8.7e-03 1.6e-04 1.00e+00 1.664388683e+02 1.664449605e+02 1.4e-09 0.52
66 2.4e-06 8.7e-03 1.5e-04 1.00e+00 1.664392699e+02 1.664447529e+02 1.3e-09 0.53
67 2.1e-06 8.6e-03 1.3e-04 1.00e+00 1.664396311e+02 1.664445659e+02 1.1e-09 0.54
68 1.9e-06 8.5e-03 1.2e-04 1.00e+00 1.664399561e+02 1.664443974e+02 1.0e-09 0.55
69 1.7e-06 8.4e-03 1.1e-04 1.00e+00 1.664402485e+02 1.664442457e+02 9.2e-10 0.56
70 1.6e-06 8.4e-03 9.7e-05 1.00e+00 1.664405115e+02 1.664441090e+02 8.3e-10 0.57
71 1.4e-06 8.3e-03 8.7e-05 1.00e+00 1.664407481e+02 1.664439859e+02 7.5e-10 0.58
72 1.3e-06 8.3e-03 7.8e-05 1.00e+00 1.664409609e+02 1.664438750e+02 6.7e-10 0.58
73 1.1e-06 8.2e-03 7.0e-05 1.00e+00 1.664411524e+02 1.664437751e+02 6.1e-10 0.59
74 1.0e-06 8.2e-03 6.3e-05 1.00e+00 1.664413247e+02 1.664436851e+02 5.5e-10 0.60
75 9.2e-07 8.1e-03 5.7e-05 1.00e+00 1.664414797e+02 1.664436041e+02 4.9e-10 0.60
76 8.3e-07 8.1e-03 5.1e-05 1.00e+00 1.664416192e+02 1.664435311e+02 4.4e-10 0.61
77 7.5e-07 8.1e-03 4.6e-05 1.00e+00 1.664417446e+02 1.664434654e+02 4.0e-10 0.62
78 6.7e-07 8.0e-03 4.2e-05 1.00e+00 1.664418575e+02 1.664434062e+02 3.6e-10 0.62
79 6.1e-07 8.0e-03 3.7e-05 1.00e+00 1.664419590e+02 1.664433528e+02 3.2e-10 0.63
80 5.5e-07 8.0e-03 3.4e-05 1.00e+00 1.664420503e+02 1.664433048e+02 2.9e-10 0.64
81 4.9e-07 7.9e-03 3.0e-05 1.00e+00 1.664421325e+02 1.664432615e+02 2.6e-10 0.64
82 4.4e-07 7.9e-03 2.7e-05 1.00e+00 1.664422064e+02 1.664432225e+02 2.3e-10 0.65
83 4.0e-07 7.9e-03 2.5e-05 1.00e+00 1.664422728e+02 1.664431874e+02 2.1e-10 0.66
84 3.6e-07 7.9e-03 2.2e-05 1.00e+00 1.664423326e+02 1.664431558e+02 1.9e-10 0.66
85 3.2e-07 7.8e-03 2.0e-05 1.00e+00 1.664423865e+02 1.664431273e+02 1.7e-10 0.67
86 2.9e-07 7.8e-03 1.8e-05 1.00e+00 1.664424349e+02 1.664431016e+02 1.5e-10 0.68
87 2.6e-07 7.8e-03 1.6e-05 1.00e+00 1.664424785e+02 1.664430785e+02 1.4e-10 0.68
88 2.3e-07 7.8e-03 1.5e-05 1.00e+00 1.664425177e+02 1.664430577e+02 1.2e-10 0.69
89 2.1e-07 7.8e-03 1.3e-05 1.00e+00 1.664425530e+02 1.664430390e+02 1.1e-10 0.70
90 1.9e-07 7.7e-03 1.2e-05 1.00e+00 1.664425847e+02 1.664430222e+02 1.0e-10 0.70
91 1.7e-07 7.7e-03 1.1e-05 1.00e+00 1.664426133e+02 1.664430070e+02 9.1e-11 0.71
92 1.5e-07 7.7e-03 9.5e-06 1.00e+00 1.664426390e+02 1.664429934e+02 8.2e-11 0.72
93 1.4e-07 7.7e-03 8.6e-06 1.00e+00 1.664426622e+02 1.664429811e+02 7.4e-11 0.73
94 1.2e-07 7.7e-03 7.7e-06 1.00e+00 1.664426830e+02 1.664429701e+02 6.6e-11 0.73
95 1.1e-07 7.7e-03 6.9e-06 1.00e+00 1.664427018e+02 1.664429601e+02 6.0e-11 0.74
96 1.0e-07 7.7e-03 6.2e-06 1.00e+00 1.664427187e+02 1.664429512e+02 5.4e-11 0.75
97 9.1e-08 7.6e-03 5.6e-06 1.00e+00 1.664427339e+02 1.664429431e+02 4.8e-11 0.75
98 8.2e-08 7.6e-03 5.1e-06 1.00e+00 1.664427476e+02 1.664429359e+02 4.4e-11 0.76
99 7.4e-08 7.6e-03 4.6e-06 1.00e+00 1.664427599e+02 1.664429294e+02 3.9e-11 0.77
100 6.6e-08 6.9e-03 4.1e-06 1.00e+00 1.664427710e+02 1.664429234e+02 3.5e-11 0.78
101 6.0e-08 6.2e-03 3.7e-06 1.00e+00 1.664427809e+02 1.664429182e+02 3.2e-11 0.78
102 5.4e-08 5.6e-03 3.3e-06 1.00e+00 1.664427899e+02 1.664429134e+02 2.9e-11 0.79
103 4.8e-08 5.0e-03 3.0e-06 9.99e-01 1.664427980e+02 1.664429092e+02 2.6e-11 0.80
104 4.3e-08 4.5e-03 2.7e-06 1.00e+00 1.664428052e+02 1.664429053e+02 2.3e-11 0.80
105 3.9e-08 4.1e-03 2.4e-06 9.98e-01 1.664428118e+02 1.664429019e+02 2.1e-11 0.81
106 3.5e-08 3.6e-03 2.2e-06 1.00e+00 1.664428177e+02 1.664428987e+02 1.9e-11 0.82
107 3.2e-08 3.3e-03 2.0e-06 1.00e+00 1.664428230e+02 1.664428959e+02 1.7e-11 0.83
108 2.9e-08 3.0e-03 1.8e-06 1.00e+00 1.664428277e+02 1.664428934e+02 1.5e-11 0.84
109 2.6e-08 2.7e-03 1.6e-06 1.00e+00 1.664428320e+02 1.664428911e+02 1.4e-11 0.85
110 2.3e-08 2.4e-03 1.4e-06 9.97e-01 1.664428359e+02 1.664428891e+02 1.2e-11 0.86
111 2.1e-08 2.2e-03 1.3e-06 1.00e+00 1.664428394e+02 1.664428873e+02 1.1e-11 0.87
112 1.9e-08 1.9e-03 1.2e-06 9.98e-01 1.664428425e+02 1.664428857e+02 1.0e-11 0.88
113 1.7e-08 1.7e-03 1.0e-06 1.00e+00 1.664428453e+02 1.664428842e+02 9.0e-12 0.88
114 1.6e-08 1.6e-03 9.4e-07 9.77e-01 1.664428478e+02 1.664428830e+02 8.1e-12 0.89
115 1.4e-08 1.4e-03 8.4e-07 1.00e+00 1.664428501e+02 1.664428817e+02 7.3e-12 0.90
116 1.3e-08 1.3e-03 7.6e-07 9.88e-01 1.664428521e+02 1.664428807e+02 6.5e-12 0.90
117 1.2e-08 1.1e-03 6.8e-07 1.01e+00 1.664428541e+02 1.664428796e+02 5.9e-12 0.91
118 1.1e-08 1.0e-03 6.2e-07 1.00e+00 1.664428557e+02 1.664428787e+02 5.3e-12 0.92
119 9.6e-09 9.3e-04 5.5e-07 9.88e-01 1.664428572e+02 1.664428779e+02 4.8e-12 0.92
120 8.7e-09 8.3e-04 5.0e-07 9.93e-01 1.664428586e+02 1.664428772e+02 4.3e-12 0.93
121 1.9e-08 7.5e-04 4.5e-07 1.01e+00 1.664428598e+02 1.664428765e+02 3.9e-12 0.94
122 2.1e-08 6.8e-04 4.0e-07 1.01e+00 1.664428610e+02 1.664428759e+02 3.5e-12 0.94
123 1.9e-08 6.1e-04 3.6e-07 1.02e+00 1.664428620e+02 1.664428753e+02 3.2e-12 0.95
124 1.7e-08 5.5e-04 3.3e-07 1.00e+00 1.664428629e+02 1.664428748e+02 2.9e-12 0.96
125 1.5e-08 4.9e-04 2.9e-07 9.79e-01 1.664428637e+02 1.664428744e+02 2.6e-12 0.97
126 1.4e-08 4.4e-04 2.6e-07 1.02e+00 1.664428644e+02 1.664428740e+02 2.4e-12 0.97
127 1.3e-08 4.0e-04 2.4e-07 1.00e+00 1.664428650e+02 1.664428737e+02 2.1e-12 0.98
128 1.1e-08 3.6e-04 2.1e-07 1.02e+00 1.664428657e+02 1.664428734e+02 1.9e-12 0.98
129 1.1e-08 3.2e-04 1.9e-07 9.81e-01 1.664428662e+02 1.664428731e+02 1.7e-12 0.99
130 9.6e-09 2.9e-04 1.7e-07 9.92e-01 1.664428666e+02 1.664428729e+02 1.6e-12 1.00
131 8.7e-09 2.6e-04 1.6e-07 1.03e+00 1.664428671e+02 1.664428726e+02 1.4e-12 1.01
132 7.8e-09 2.4e-04 1.4e-07 9.97e-01 1.664428674e+02 1.664428724e+02 1.3e-12 1.01
133 6.9e-09 2.1e-04 1.3e-07 9.85e-01 1.664428677e+02 1.664428723e+02 1.2e-12 1.02
134 6.2e-09 1.9e-04 1.1e-07 9.94e-01 1.664428680e+02 1.664428721e+02 1.0e-12 1.03
135 5.6e-09 1.7e-04 1.0e-07 9.91e-01 1.664428683e+02 1.664428720e+02 9.3e-13 1.03
Optimizer terminated. Time: 1.03
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6644286830e+02 nrm: 2e+01 Viol. con: 2e-07 var: 0e+00
Dual. obj: 1.6644287195e+02 nrm: 1e+03 Viol. con: 0e+00 var: 1e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.06 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 868
Optimizer - Cones : 0
Optimizer - Scalar variables : 3451 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05
Factor - dense dim. : 0 flops : 2.93e+07
Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237706206e+05 2.000000000e+00 1.0e+00 0.03
1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230321596e+05 2.618476980e+00 7.3e-01 0.04
2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.207092172e+05 4.631299788e+00 3.8e-01 0.05
3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.116388875e+05 2.010679045e+01 1.3e-01 0.05
4 2.9e+02 4.5e+02 1.6e+04 -7.71e-01 -1.094230997e+05 1.962291865e+03 1.3e-01 0.06
5 1.2e+02 1.9e+02 6.4e+03 -7.61e-01 -8.785793218e+04 6.263182648e+03 5.2e-02 0.07
6 2.6e+01 4.1e+01 1.4e+03 -4.45e-01 -3.316835220e+04 1.269767615e+04 1.2e-02 0.07
7 1.7e+01 2.7e+01 9.2e+02 4.98e-01 -2.422632748e+04 7.083733147e+03 7.5e-03 0.08
8 1.0e+01 1.6e+01 5.4e+02 6.67e-01 -1.518713164e+04 4.349438842e+03 4.4e-03 0.09
9 4.0e+00 6.3e+00 2.2e+02 8.16e-01 -6.253806240e+03 1.985800338e+03 1.8e-03 0.09
10 2.1e+00 3.3e+00 1.1e+02 9.46e-01 -3.093879792e+03 1.203594049e+03 9.3e-04 0.10
11 8.4e-01 1.3e+00 4.6e+01 9.86e-01 -1.145500547e+03 6.338782408e+02 3.8e-04 0.11
12 8.2e-01 1.3e+00 4.5e+01 9.50e-01 -1.137960646e+03 6.093711314e+02 3.7e-04 0.11
13 5.2e-01 8.3e-01 2.9e+01 9.70e-01 -6.844600457e+02 4.368156380e+02 2.4e-04 0.12
14 3.3e-01 5.4e-01 1.9e+01 1.00e+00 -3.665602888e+02 3.537892051e+02 1.5e-04 0.13
15 1.1e-01 2.0e-01 6.3e+00 9.97e-01 -2.732814371e+01 2.163541368e+02 5.3e-05 0.14
16 8.4e-02 1.5e-01 4.7e+00 1.02e+00 2.245602987e+01 2.054082491e+02 4.0e-05 0.14
17 4.4e-02 9.1e-02 2.5e+00 1.02e+00 9.404505834e+01 1.878214886e+02 2.1e-05 0.15
18 1.5e-02 8.6e-02 8.4e-01 1.02e+00 1.425020548e+02 1.744453424e+02 7.1e-06 0.16
19 6.8e-03 7.5e-02 3.9e-01 1.01e+00 1.551720364e+02 1.698416553e+02 3.3e-06 0.16
20 1.6e-03 1.6e-01 9.8e-02 1.01e+00 1.637887523e+02 1.674579832e+02 8.2e-07 0.17
21 9.3e-04 1.1e-01 5.6e-02 9.78e-01 1.649100104e+02 1.670143929e+02 4.7e-07 0.18
22 2.9e-04 1.1e-01 1.8e-02 9.88e-01 1.659434069e+02 1.666331473e+02 1.6e-07 0.19
23 1.3e-04 9.3e-02 8.0e-03 1.01e+00 1.662132718e+02 1.665137253e+02 6.9e-08 0.20
24 1.1e-04 8.6e-02 7.2e-03 1.01e+00 1.662362811e+02 1.665066924e+02 6.2e-08 0.21
25 1.0e-04 7.8e-02 6.5e-03 1.01e+00 1.662550118e+02 1.664982554e+02 5.6e-08 0.22
26 9.1e-05 7.1e-02 5.9e-03 1.01e+00 1.662720854e+02 1.664909344e+02 5.1e-08 0.23
27 8.2e-05 6.4e-02 5.3e-03 1.01e+00 1.662873803e+02 1.664842821e+02 4.6e-08 0.24
28 7.4e-05 5.9e-02 4.7e-03 1.01e+00 1.663011123e+02 1.664782724e+02 4.1e-08 0.25
29 6.6e-05 5.3e-02 4.3e-03 1.01e+00 1.663134330e+02 1.664728330e+02 3.7e-08 0.25
30 6.0e-05 4.9e-02 3.8e-03 1.01e+00 1.663244890e+02 1.664679121e+02 3.3e-08 0.26
31 5.4e-05 4.5e-02 3.5e-03 1.01e+00 1.663344111e+02 1.664634611e+02 3.0e-08 0.27
32 4.8e-05 4.1e-02 3.1e-03 1.01e+00 1.663433169e+02 1.664594363e+02 2.7e-08 0.27
33 4.4e-05 3.8e-02 2.8e-03 1.01e+00 1.663513115e+02 1.664557980e+02 2.4e-08 0.28
34 3.9e-05 3.5e-02 2.5e-03 1.01e+00 1.663584889e+02 1.664525096e+02 2.2e-08 0.29
35 3.5e-05 3.2e-02 2.3e-03 1.01e+00 1.663649336e+02 1.664495382e+02 2.0e-08 0.30
36 3.2e-05 3.0e-02 2.0e-03 1.00e+00 1.663707209e+02 1.664468536e+02 1.8e-08 0.31
37 2.9e-05 2.7e-02 1.8e-03 1.00e+00 1.663759184e+02 1.664444285e+02 1.6e-08 0.31
38 2.6e-05 2.5e-02 1.7e-03 1.00e+00 1.663805867e+02 1.664422382e+02 1.4e-08 0.32
39 2.3e-05 2.4e-02 1.5e-03 1.00e+00 1.663847800e+02 1.664402602e+02 1.3e-08 0.33
40 2.1e-05 2.2e-02 1.3e-03 1.00e+00 1.663885470e+02 1.664384742e+02 1.2e-08 0.34
41 1.9e-05 2.1e-02 1.2e-03 1.00e+00 1.663919312e+02 1.664368618e+02 1.0e-08 0.34
42 1.7e-05 1.9e-02 1.1e-03 1.00e+00 1.663949719e+02 1.664354061e+02 9.4e-09 0.35
43 1.5e-05 1.8e-02 9.8e-04 1.00e+00 1.663977039e+02 1.664340922e+02 8.5e-09 0.36
44 1.4e-05 1.7e-02 8.8e-04 1.00e+00 1.664001590e+02 1.664329064e+02 7.6e-09 0.37
45 1.2e-05 1.6e-02 7.9e-04 1.00e+00 1.664023653e+02 1.664318363e+02 6.9e-09 0.37
46 1.1e-05 1.6e-02 7.1e-04 1.00e+00 1.664043481e+02 1.664308707e+02 6.2e-09 0.38
47 1.0e-05 1.5e-02 6.4e-04 1.00e+00 1.664061303e+02 1.664299996e+02 5.6e-09 0.39
48 9.0e-06 1.4e-02 5.8e-04 1.00e+00 1.664077322e+02 1.664292138e+02 5.0e-09 0.39
49 8.1e-06 1.4e-02 5.2e-04 1.00e+00 1.664091722e+02 1.664285050e+02 4.5e-09 0.40
50 7.3e-06 1.3e-02 4.7e-04 1.00e+00 1.664104668e+02 1.664278658e+02 4.1e-09 0.41
51 6.5e-06 1.2e-02 4.2e-04 1.00e+00 1.664116306e+02 1.664272894e+02 3.6e-09 0.42
52 5.9e-06 1.2e-02 3.8e-04 1.00e+00 1.664126770e+02 1.664267697e+02 3.3e-09 0.42
53 5.3e-06 1.2e-02 3.4e-04 1.00e+00 1.664136179e+02 1.664263011e+02 3.0e-09 0.43
54 4.8e-06 1.1e-02 3.1e-04 1.00e+00 1.664144640e+02 1.664258787e+02 2.7e-09 0.44
55 4.3e-06 1.1e-02 2.8e-04 1.00e+00 1.664152247e+02 1.664254979e+02 2.4e-09 0.44
56 3.9e-06 1.1e-02 2.5e-04 1.00e+00 1.664159088e+02 1.664251546e+02 2.2e-09 0.46
57 3.5e-06 1.0e-02 2.2e-04 1.00e+00 1.664165240e+02 1.664248452e+02 1.9e-09 0.47
58 3.1e-06 1.0e-02 2.0e-04 1.00e+00 1.664170772e+02 1.664245662e+02 1.7e-09 0.47
59 2.8e-06 1.0e-02 1.8e-04 1.00e+00 1.664175747e+02 1.664243148e+02 1.6e-09 0.48
60 2.5e-06 9.8e-03 1.6e-04 1.00e+00 1.664180222e+02 1.664240883e+02 1.4e-09 0.49
61 2.3e-06 9.7e-03 1.5e-04 1.00e+00 1.664184247e+02 1.664238842e+02 1.3e-09 0.49
62 2.1e-06 9.5e-03 1.3e-04 1.00e+00 1.664187868e+02 1.664237003e+02 1.1e-09 0.50
63 1.8e-06 9.4e-03 1.2e-04 1.00e+00 1.664191125e+02 1.664235347e+02 1.0e-09 0.51
64 1.7e-06 9.2e-03 1.1e-04 1.00e+00 1.664194056e+02 1.664233856e+02 9.3e-10 0.52
65 1.5e-06 9.1e-03 9.6e-05 1.00e+00 1.664196692e+02 1.664232513e+02 8.3e-10 0.52
66 1.3e-06 9.0e-03 8.7e-05 1.00e+00 1.664199064e+02 1.664231303e+02 7.5e-10 0.53
67 1.2e-06 8.9e-03 7.8e-05 1.00e+00 1.664201198e+02 1.664230213e+02 6.8e-10 0.54
68 1.1e-06 8.8e-03 7.0e-05 1.00e+00 1.664203118e+02 1.664229232e+02 6.1e-10 0.55
69 9.8e-07 8.7e-03 6.3e-05 1.00e+00 1.664204846e+02 1.664228348e+02 5.5e-10 0.56
70 8.8e-07 8.6e-03 5.7e-05 1.00e+00 1.664206400e+02 1.664227552e+02 4.9e-10 0.57
71 8.0e-07 8.6e-03 5.1e-05 1.00e+00 1.664207798e+02 1.664226835e+02 4.4e-10 0.57
72 7.2e-07 8.5e-03 4.6e-05 1.00e+00 1.664209056e+02 1.664226189e+02 4.0e-10 0.59
73 6.4e-07 8.4e-03 4.2e-05 1.00e+00 1.664210187e+02 1.664225608e+02 3.6e-10 0.60
74 5.8e-07 8.4e-03 3.7e-05 1.00e+00 1.664211205e+02 1.664225084e+02 3.2e-10 0.60
75 5.2e-07 8.3e-03 3.4e-05 1.00e+00 1.664212121e+02 1.664224611e+02 2.9e-10 0.61
76 4.7e-07 8.3e-03 3.0e-05 1.00e+00 1.664212945e+02 1.664224186e+02 2.6e-10 0.62
77 4.2e-07 8.2e-03 2.7e-05 1.00e+00 1.664213686e+02 1.664223803e+02 2.4e-10 0.63
78 3.8e-07 8.2e-03 2.5e-05 1.00e+00 1.664214352e+02 1.664223458e+02 2.1e-10 0.64
79 3.4e-07 8.1e-03 2.2e-05 1.00e+00 1.664214952e+02 1.664223147e+02 1.9e-10 0.65
80 3.1e-07 8.1e-03 2.0e-05 1.00e+00 1.664215491e+02 1.664222867e+02 1.7e-10 0.66
81 2.8e-07 8.1e-03 1.8e-05 1.00e+00 1.664215977e+02 1.664222615e+02 1.5e-10 0.67
82 2.5e-07 8.0e-03 1.6e-05 1.00e+00 1.664216413e+02 1.664222387e+02 1.4e-10 0.67
83 2.2e-07 8.0e-03 1.4e-05 1.00e+00 1.664216806e+02 1.664222183e+02 1.3e-10 0.68
84 2.0e-07 8.0e-03 1.3e-05 1.00e+00 1.664217160e+02 1.664221999e+02 1.1e-10 0.69
85 1.8e-07 7.9e-03 1.2e-05 1.00e+00 1.664217478e+02 1.664221833e+02 1.0e-10 0.70
86 1.6e-07 7.9e-03 1.1e-05 1.00e+00 1.664217764e+02 1.664221684e+02 9.1e-11 0.70
87 1.5e-07 7.9e-03 9.5e-06 1.00e+00 1.664218022e+02 1.664221550e+02 8.2e-11 0.71
88 1.3e-07 7.9e-03 8.6e-06 1.00e+00 1.664218254e+02 1.664221429e+02 7.4e-11 0.72
89 1.2e-07 7.8e-03 7.7e-06 1.00e+00 1.664218463e+02 1.664221320e+02 6.7e-11 0.73
90 1.1e-07 7.8e-03 6.9e-06 1.00e+00 1.664218650e+02 1.664221222e+02 6.0e-11 0.73
91 9.7e-08 7.8e-03 6.2e-06 1.00e+00 1.664218819e+02 1.664221134e+02 5.4e-11 0.74
92 8.7e-08 7.8e-03 5.6e-06 1.00e+00 1.664218971e+02 1.664221055e+02 4.9e-11 0.75
93 7.8e-08 7.8e-03 5.1e-06 1.00e+00 1.664219108e+02 1.664220983e+02 4.4e-11 0.76
94 7.1e-08 7.8e-03 4.5e-06 1.00e+00 1.664219231e+02 1.664220919e+02 3.9e-11 0.77
95 6.4e-08 7.7e-03 4.1e-06 1.00e+00 1.664219342e+02 1.664220861e+02 3.5e-11 0.77
96 5.7e-08 7.0e-03 3.7e-06 1.00e+00 1.664219443e+02 1.664220807e+02 3.2e-11 0.78
97 5.1e-08 6.3e-03 3.3e-06 1.00e+00 1.664219532e+02 1.664220760e+02 2.9e-11 0.79
98 4.6e-08 5.6e-03 3.0e-06 1.00e+00 1.664219613e+02 1.664220718e+02 2.6e-11 0.80
99 4.2e-08 5.1e-03 2.7e-06 9.99e-01 1.664219686e+02 1.664220680e+02 2.3e-11 0.80
100 3.8e-08 4.6e-03 2.4e-06 1.00e+00 1.664219751e+02 1.664220646e+02 2.1e-11 0.81
101 3.4e-08 4.1e-03 2.2e-06 9.99e-01 1.664219810e+02 1.664220616e+02 1.9e-11 0.82
102 3.0e-08 3.7e-03 2.0e-06 1.00e+00 1.664219863e+02 1.664220588e+02 1.7e-11 0.83
103 2.7e-08 3.3e-03 1.8e-06 9.97e-01 1.664219910e+02 1.664220564e+02 1.5e-11 0.83
104 2.5e-08 3.0e-03 1.6e-06 1.00e+00 1.664219953e+02 1.664220542e+02 1.4e-11 0.84
105 2.2e-08 2.7e-03 1.4e-06 9.98e-01 1.664219992e+02 1.664220521e+02 1.2e-11 0.85
106 2.0e-08 2.4e-03 1.3e-06 1.00e+00 1.664220027e+02 1.664220503e+02 1.1e-11 0.86
107 1.8e-08 2.2e-03 1.2e-06 1.00e+00 1.664220058e+02 1.664220487e+02 1.0e-11 0.87
108 1.6e-08 2.0e-03 1.0e-06 1.00e+00 1.664220086e+02 1.664220472e+02 9.0e-12 0.87
109 1.5e-08 1.8e-03 9.4e-07 9.97e-01 1.664220112e+02 1.664220459e+02 8.1e-12 0.88
110 1.3e-08 1.6e-03 8.4e-07 1.00e+00 1.664220134e+02 1.664220447e+02 7.3e-12 0.89
111 1.2e-08 1.4e-03 7.6e-07 9.96e-01 1.664220155e+02 1.664220437e+02 6.6e-12 0.90
112 1.1e-08 1.3e-03 6.8e-07 9.99e-01 1.664220173e+02 1.664220427e+02 5.9e-12 0.91
113 9.6e-09 1.2e-03 6.1e-07 9.97e-01 1.664220190e+02 1.664220418e+02 5.3e-12 0.91
114 8.6e-09 1.0e-03 5.5e-07 9.91e-01 1.664220205e+02 1.664220410e+02 4.8e-12 0.92
115 7.8e-09 9.4e-04 5.0e-07 1.01e+00 1.664220219e+02 1.664220403e+02 4.3e-12 0.93
116 7.0e-09 8.5e-04 4.5e-07 9.92e-01 1.664220231e+02 1.664220397e+02 3.9e-12 0.94
117 1.4e-08 7.6e-04 4.0e-07 1.02e+00 1.664220242e+02 1.664220394e+02 3.5e-12 0.94
118 2.0e-08 6.9e-04 3.6e-07 9.99e-01 1.664220252e+02 1.664220387e+02 3.2e-12 0.95
119 1.8e-08 6.2e-04 3.3e-07 1.01e+00 1.664220261e+02 1.664220382e+02 2.9e-12 0.96
120 3.3e-08 5.6e-04 2.9e-07 9.98e-01 1.664220268e+02 1.664220382e+02 2.6e-12 0.97
121 2.2e-08 5.0e-04 2.6e-07 9.99e-01 1.664220276e+02 1.664220373e+02 2.3e-12 0.97
122 2.0e-08 4.5e-04 2.4e-07 1.01e+00 1.664220282e+02 1.664220370e+02 2.1e-12 0.98
123 1.8e-08 4.1e-04 2.1e-07 1.00e+00 1.664220288e+02 1.664220367e+02 1.9e-12 0.99
124 1.7e-08 3.7e-04 1.9e-07 1.02e+00 1.664220294e+02 1.664220364e+02 1.7e-12 1.00
125 1.5e-08 3.3e-04 1.7e-07 1.01e+00 1.664220298e+02 1.664220361e+02 1.5e-12 1.01
126 1.3e-08 3.0e-04 1.6e-07 1.00e+00 1.664220303e+02 1.664220359e+02 1.4e-12 1.01
127 1.2e-08 2.7e-04 1.4e-07 9.96e-01 1.664220306e+02 1.664220357e+02 1.2e-12 1.02
128 1.1e-08 2.4e-04 1.3e-07 1.01e+00 1.664220310e+02 1.664220355e+02 1.1e-12 1.03
129 9.9e-09 2.2e-04 1.1e-07 1.00e+00 1.664220313e+02 1.664220354e+02 1.0e-12 1.04
130 1.0e-09 2.2e-05 1.2e-08 1.00e+00 1.664220337e+02 1.664220341e+02 1.0e-13 1.05
Optimizer terminated. Time: 1.05
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6642203368e+02 nrm: 2e+01 Viol. con: 2e-08 var: 0e+00
Dual. obj: 1.6642203410e+02 nrm: 1e+03 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.07 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (312) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 868
Optimizer - Cones : 0
Optimizer - Scalar variables : 3451 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 1.48e+04 after factor : 1.48e+05
Factor - dense dim. : 0 flops : 2.93e+07
Factor - GP saved nzs : 3.33e+04 GP saved flops : 9.12e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.6e+03 1.2e+05 0.00e+00 -1.237697757e+05 2.000000000e+00 1.0e+00 0.03
1 1.7e+03 2.6e+03 9.0e+04 -9.71e-01 -1.230310708e+05 2.618658392e+00 7.3e-01 0.04
2 8.7e+02 1.4e+03 4.7e+04 -9.59e-01 -1.207072283e+05 4.631967602e+00 3.8e-01 0.05
3 2.9e+02 4.6e+02 1.6e+04 -9.21e-01 -1.116239239e+05 2.011668198e+01 1.3e-01 0.06
4 2.9e+02 4.5e+02 1.6e+04 -7.71e-01 -1.094044853e+05 1.966473714e+03 1.3e-01 0.06
5 1.2e+02 1.9e+02 6.4e+03 -7.61e-01 -8.784053867e+04 6.251650733e+03 5.2e-02 0.07
6 2.6e+01 4.1e+01 1.4e+03 -4.45e-01 -3.306603809e+04 1.270142506e+04 1.2e-02 0.08
7 1.7e+01 2.7e+01 9.1e+02 4.99e-01 -2.410345416e+04 7.059532995e+03 7.5e-03 0.09
8 9.9e+00 1.6e+01 5.4e+02 6.69e-01 -1.509576583e+04 4.325329085e+03 4.4e-03 0.10
9 3.9e+00 6.2e+00 2.1e+02 8.17e-01 -6.165428475e+03 1.962599328e+03 1.8e-03 0.11
10 2.0e+00 3.2e+00 1.1e+02 9.46e-01 -3.034895445e+03 1.193153232e+03 9.1e-04 0.11
11 8.5e-01 1.3e+00 4.7e+01 9.86e-01 -1.168555856e+03 6.294711099e+02 3.9e-04 0.12
12 8.2e-01 1.3e+00 4.5e+01 9.51e-01 -1.158089507e+03 6.045830226e+02 3.8e-04 0.13
13 5.2e-01 8.3e-01 2.9e+01 9.70e-01 -6.910803073e+02 4.348560115e+02 2.4e-04 0.14
14 3.3e-01 5.3e-01 1.8e+01 1.00e+00 -3.582552166e+02 3.500458516e+02 1.5e-04 0.14
15 1.1e-01 2.0e-01 6.2e+00 9.97e-01 -2.527655392e+01 2.158431403e+02 5.2e-05 0.15
16 8.3e-02 1.5e-01 4.7e+00 1.02e+00 2.363102125e+01 2.049700552e+02 3.9e-05 0.16
17 4.1e-02 8.8e-02 2.3e+00 1.02e+00 9.799313343e+01 1.868005351e+02 1.9e-05 0.17
18 1.1e-02 1.7e-01 6.3e-01 1.02e+00 1.487956591e+02 1.727754642e+02 5.3e-06 0.18
19 3.5e-03 2.0e-01 2.1e-01 1.01e+00 1.605532700e+02 1.683301713e+02 1.7e-06 0.18
20 1.3e-03 1.4e-01 8.0e-02 1.01e+00 1.642277735e+02 1.672301862e+02 6.8e-07 0.19
21 8.8e-04 1.0e-01 5.3e-02 9.84e-01 1.649840636e+02 1.669558345e+02 4.5e-07 0.21
22 2.6e-04 1.1e-01 1.7e-02 9.86e-01 1.659721215e+02 1.665916548e+02 1.4e-07 0.22
23 9.3e-05 1.1e-01 6.0e-03 1.01e+00 1.662531933e+02 1.664754263e+02 5.2e-08 0.22
24 3.5e-05 1.0e-01 2.3e-03 1.01e+00 1.663489963e+02 1.664340420e+02 2.0e-08 0.23
25 1.6e-05 8.4e-02 1.1e-03 1.00e+00 1.663808103e+02 1.664201668e+02 9.4e-09 0.24
26 1.5e-05 7.7e-02 9.6e-04 1.00e+00 1.663840618e+02 1.664194962e+02 8.4e-09 0.25
27 1.3e-05 7.0e-02 8.6e-04 1.01e+00 1.663864463e+02 1.664183305e+02 7.6e-09 0.26
28 1.2e-05 6.3e-02 7.7e-04 1.00e+00 1.663886321e+02 1.664173227e+02 6.8e-09 0.27
29 1.1e-05 5.8e-02 7.0e-04 1.00e+00 1.663905903e+02 1.664164076e+02 6.2e-09 0.28
30 9.6e-06 5.3e-02 6.3e-04 1.00e+00 1.663923512e+02 1.664155833e+02 5.5e-09 0.28
31 8.7e-06 4.8e-02 5.6e-04 1.00e+00 1.663939340e+02 1.664148400e+02 5.0e-09 0.30
32 7.8e-06 4.4e-02 5.1e-04 1.00e+00 1.663953569e+02 1.664141700e+02 4.5e-09 0.31
33 7.0e-06 4.1e-02 4.6e-04 1.00e+00 1.663966362e+02 1.664135660e+02 4.0e-09 0.31
34 6.3e-06 3.7e-02 4.1e-04 1.00e+00 1.663977864e+02 1.664130217e+02 3.6e-09 0.32
35 5.7e-06 3.5e-02 3.7e-04 1.00e+00 1.663988207e+02 1.664125312e+02 3.3e-09 0.33
36 5.1e-06 3.2e-02 3.3e-04 1.00e+00 1.663997507e+02 1.664120891e+02 2.9e-09 0.34
37 4.6e-06 2.9e-02 3.0e-04 1.00e+00 1.664005870e+02 1.664116908e+02 2.6e-09 0.34
38 4.1e-06 2.7e-02 2.7e-04 1.00e+00 1.664013391e+02 1.664113318e+02 2.4e-09 0.35
39 3.7e-06 2.5e-02 2.4e-04 1.00e+00 1.664020155e+02 1.664110084e+02 2.1e-09 0.36
40 3.4e-06 2.4e-02 2.2e-04 1.00e+00 1.664026238e+02 1.664107169e+02 1.9e-09 0.37
41 3.0e-06 2.2e-02 2.0e-04 1.00e+00 1.664031708e+02 1.664104542e+02 1.7e-09 0.38
42 2.7e-06 2.1e-02 1.8e-04 1.00e+00 1.664036628e+02 1.664102176e+02 1.6e-09 0.39
43 2.4e-06 1.9e-02 1.6e-04 1.00e+00 1.664041053e+02 1.664100044e+02 1.4e-09 0.39
44 2.2e-06 1.8e-02 1.4e-04 1.00e+00 1.664045034e+02 1.664098124e+02 1.3e-09 0.41
45 2.0e-06 1.7e-02 1.3e-04 1.00e+00 1.664048615e+02 1.664096395e+02 1.1e-09 0.42
46 1.8e-06 1.6e-02 1.2e-04 1.00e+00 1.664051837e+02 1.664094838e+02 1.0e-09 0.42
47 1.6e-06 1.5e-02 1.0e-04 1.00e+00 1.664054736e+02 1.664093436e+02 9.2e-10 0.44
48 1.4e-06 1.5e-02 9.4e-05 1.00e+00 1.664057344e+02 1.664092173e+02 8.3e-10 0.45
49 1.3e-06 1.4e-02 8.5e-05 1.00e+00 1.664059691e+02 1.664091036e+02 7.5e-10 0.45
50 1.2e-06 1.3e-02 7.6e-05 1.00e+00 1.664061802e+02 1.664090012e+02 6.7e-10 0.47
51 1.1e-06 1.3e-02 6.9e-05 1.00e+00 1.664063701e+02 1.664089090e+02 6.1e-10 0.48
52 9.5e-07 1.2e-02 6.2e-05 1.00e+00 1.664065410e+02 1.664088260e+02 5.5e-10 0.48
53 8.5e-07 1.2e-02 5.6e-05 1.00e+00 1.664066948e+02 1.664087512e+02 4.9e-10 0.50
54 7.7e-07 1.1e-02 5.0e-05 1.00e+00 1.664068331e+02 1.664086839e+02 4.4e-10 0.51
55 6.9e-07 1.1e-02 4.5e-05 1.00e+00 1.664069575e+02 1.664086232e+02 4.0e-10 0.52
56 6.2e-07 1.1e-02 4.1e-05 1.00e+00 1.664070695e+02 1.664085686e+02 3.6e-10 0.53
57 5.6e-07 1.0e-02 3.7e-05 1.00e+00 1.664071702e+02 1.664085194e+02 3.2e-10 0.54
58 5.0e-07 1.0e-02 3.3e-05 1.00e+00 1.664072608e+02 1.664084750e+02 2.9e-10 0.54
59 4.5e-07 9.9e-03 3.0e-05 1.00e+00 1.664073423e+02 1.664084351e+02 2.6e-10 0.55
60 4.1e-07 9.7e-03 2.7e-05 1.00e+00 1.664074156e+02 1.664083991e+02 2.4e-10 0.56
61 3.7e-07 9.5e-03 2.4e-05 1.00e+00 1.664074815e+02 1.664083667e+02 2.1e-10 0.57
62 3.3e-07 9.3e-03 2.2e-05 1.00e+00 1.664075408e+02 1.664083374e+02 1.9e-10 0.58
63 3.0e-07 9.2e-03 1.9e-05 1.00e+00 1.664075942e+02 1.664083111e+02 1.7e-10 0.59
64 2.7e-07 9.0e-03 1.7e-05 1.00e+00 1.664076422e+02 1.664082874e+02 1.5e-10 0.60
65 2.4e-07 8.9e-03 1.6e-05 1.00e+00 1.664076853e+02 1.664082661e+02 1.4e-10 0.61
66 2.2e-07 8.8e-03 1.4e-05 1.00e+00 1.664077242e+02 1.664082469e+02 1.2e-10 0.61
67 2.0e-07 8.7e-03 1.3e-05 1.00e+00 1.664077592e+02 1.664082296e+02 1.1e-10 0.62
68 1.8e-07 8.6e-03 1.1e-05 1.00e+00 1.664077906e+02 1.664082140e+02 1.0e-10 0.64
69 1.6e-07 8.5e-03 1.0e-05 1.00e+00 1.664078190e+02 1.664082000e+02 9.1e-11 0.64
70 1.4e-07 8.4e-03 9.3e-06 1.00e+00 1.664078444e+02 1.664081874e+02 8.2e-11 0.65
71 1.3e-07 8.3e-03 8.4e-06 1.00e+00 1.664078674e+02 1.664081760e+02 7.4e-11 0.66
72 1.2e-07 8.2e-03 7.5e-06 1.00e+00 1.664078880e+02 1.664081658e+02 6.6e-11 0.67
73 1.0e-07 8.2e-03 6.8e-06 1.00e+00 1.664079065e+02 1.664081567e+02 6.0e-11 0.68
74 9.3e-08 8.1e-03 6.1e-06 1.00e+00 1.664079232e+02 1.664081484e+02 5.4e-11 0.69
75 8.4e-08 8.1e-03 5.5e-06 1.00e+00 1.664079383e+02 1.664081409e+02 4.8e-11 0.70
76 7.6e-08 8.0e-03 4.9e-06 1.00e+00 1.664079518e+02 1.664081342e+02 4.4e-11 0.71
77 6.8e-08 8.0e-03 4.4e-06 1.00e+00 1.664079640e+02 1.664081281e+02 3.9e-11 0.72
78 6.1e-08 7.9e-03 4.0e-06 1.00e+00 1.664079750e+02 1.664081227e+02 3.5e-11 0.73
79 5.5e-08 7.9e-03 3.6e-06 1.00e+00 1.664079848e+02 1.664081178e+02 3.2e-11 0.73
80 5.0e-08 7.9e-03 3.2e-06 1.00e+00 1.664079937e+02 1.664081134e+02 2.9e-11 0.74
81 4.5e-08 7.9e-03 2.9e-06 1.00e+00 1.664080017e+02 1.664081094e+02 2.6e-11 0.75
82 4.0e-08 7.8e-03 2.6e-06 1.00e+00 1.664080089e+02 1.664081058e+02 2.3e-11 0.76
83 3.6e-08 7.8e-03 2.4e-06 1.00e+00 1.664080153e+02 1.664081026e+02 2.1e-11 0.77
84 3.3e-08 7.8e-03 2.1e-06 1.00e+00 1.664080212e+02 1.664080997e+02 1.9e-11 0.78
85 2.9e-08 7.8e-03 1.9e-06 1.00e+00 1.664080264e+02 1.664080970e+02 1.7e-11 0.79
86 2.6e-08 7.7e-03 1.7e-06 1.00e+00 1.664080311e+02 1.664080947e+02 1.5e-11 0.80
87 2.4e-08 7.7e-03 1.5e-06 9.99e-01 1.664080354e+02 1.664080926e+02 1.4e-11 0.81
88 2.1e-08 7.7e-03 1.4e-06 1.00e+00 1.664080392e+02 1.664080907e+02 1.2e-11 0.82
89 1.9e-08 7.7e-03 1.3e-06 1.00e+00 1.664080426e+02 1.664080890e+02 1.1e-11 0.83
90 1.7e-08 7.6e-03 1.1e-06 9.93e-01 1.664080457e+02 1.664080875e+02 1.0e-11 0.84
91 1.6e-08 7.6e-03 1.0e-06 9.96e-01 1.664080485e+02 1.664080861e+02 9.0e-12 0.85
92 1.4e-08 7.6e-03 9.1e-07 1.00e+00 1.664080510e+02 1.664080848e+02 8.1e-12 0.86
93 1.3e-08 6.8e-03 8.2e-07 1.01e+00 1.664080533e+02 1.664080837e+02 7.3e-12 0.87
94 1.2e-08 6.2e-03 7.4e-07 9.98e-01 1.664080553e+02 1.664080827e+02 6.6e-12 0.88
95 1.0e-08 5.5e-03 6.7e-07 9.97e-01 1.664080571e+02 1.664080818e+02 5.9e-12 0.89
96 9.4e-09 5.0e-03 6.0e-07 9.95e-01 1.664080588e+02 1.664080810e+02 5.3e-12 0.90
97 8.4e-09 4.5e-03 5.4e-07 1.00e+00 1.664080603e+02 1.664080802e+02 4.8e-12 0.91
98 7.5e-09 4.0e-03 4.9e-07 9.83e-01 1.664080616e+02 1.664080795e+02 4.3e-12 0.92
99 6.8e-09 3.6e-03 4.4e-07 9.99e-01 1.664080628e+02 1.664080789e+02 3.9e-12 0.93
100 6.1e-09 3.3e-03 3.9e-07 1.02e+00 1.664080639e+02 1.664080784e+02 3.5e-12 0.94
101 5.5e-09 2.9e-03 3.5e-07 1.01e+00 1.664080649e+02 1.664080779e+02 3.2e-12 0.95
102 4.9e-09 2.6e-03 3.2e-07 1.02e+00 1.664080658e+02 1.664080774e+02 2.9e-12 0.96
103 4.4e-09 2.4e-03 2.9e-07 1.01e+00 1.664080666e+02 1.664080770e+02 2.6e-12 0.98
104 4.0e-09 2.1e-03 2.6e-07 1.04e+00 1.664080674e+02 1.664080765e+02 2.4e-12 0.99
105 3.7e-09 1.9e-03 2.3e-07 1.00e+00 1.664080680e+02 1.664080763e+02 2.1e-12 1.00
106 3.3e-09 1.7e-03 2.1e-07 1.04e+00 1.664080687e+02 1.664080759e+02 2.0e-12 1.01
107 2.9e-09 1.6e-03 1.9e-07 9.99e-01 1.664080692e+02 1.664080757e+02 1.8e-12 1.02
108 2.6e-09 1.4e-03 1.7e-07 9.99e-01 1.664080696e+02 1.664080755e+02 1.6e-12 1.03
109 2.4e-09 1.3e-03 1.5e-07 1.00e+00 1.664080700e+02 1.664080753e+02 1.4e-12 1.03
110 2.2e-09 1.1e-03 1.4e-07 1.00e+00 1.664080704e+02 1.664080751e+02 1.3e-12 1.04
111 1.9e-09 1.0e-03 1.2e-07 1.01e+00 1.664080707e+02 1.664080749e+02 1.2e-12 1.05
112 1.7e-09 9.2e-04 1.1e-07 9.94e-01 1.664080710e+02 1.664080748e+02 1.0e-12 1.06
113 1.6e-09 8.3e-04 1.0e-07 1.00e+00 1.664080712e+02 1.664080747e+02 9.5e-13 1.06
Optimizer terminated. Time: 1.07
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6640807123e+02 nrm: 2e+01 Viol. con: 2e-08 var: 0e+00
Dual. obj: 1.6640807466e+02 nrm: 1e+03 Viol. con: 0e+00 var: 5e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.09 seconds.
Solving took 9 GP solves and 16.7 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: 1.495742457694431e+110 vs 1.4956976656e+110
GP iteration 0 has relaxed constants
Cost
----
1.496e+110
Free Variables
--------------
| Mission.Aircraft.Engine.Turbine.Relax
C_{p_{t2}} : 2.251 Cp Value for Combustion Products in LP Turbine
| Mission.Aircraft.Fuselage.Relax
l_{nose} : 1.042 Nose length
n_{pass} : [ 2.86 ] Number of passengers
| Mission.Aircraft.Relax
f_{L_{total/wing}} : 1.656 Total lift as a percentage of wing lift
| Mission.Aircraft.Wing.WingNoStruct.Relax
\tan(\Lambda) : 1.133 Tangent of quarter-chord sweep angle
| Mission.FlightState.Atmosphere.Relax
L_{atm} : [ 1.77 1 1 1 1 ] Temperature lapse rate
T_{sl} : [ 1 1 1.25 1 1 ] Temperature at sea level
| Mission.Relax
R_{req} : 2.362 Required Cruise Range
GP iteration 1 has relaxed constants
Cost
----
7.486e+74
Free Variables
--------------
| Mission.Aircraft.Engine.Combustor.Relax
hold_{4a} : 1.093 1+(gamma-1)/2 * M_4a**2
| Mission.Aircraft.Fuselage.Relax
n_{pass} : [ 1.03 ] Number of passengers
| Mission.Aircraft.LandingGear.Relax
h_{hold} : 1.006 Hold height
Solution check warning: Primal solution computed cost did not match solver-returned cost: 3.7050980759335926e+72 vs 3.70502020539e+72
WEIGHT DIFFERENCES
Total Fuel Weight Percent Diff: [-92.94682113]
Total Aircraft Weight Percent Diff: [-21.48054877]
Engine Weight Percent Diff: -56.278166751133654
Fuselage Weight Percent Diff: -0.8697062242189039
Payload Weight Percent Diff: [-0.04003553]
VT Weight Percent Diff: -8.607369318686331
HT Weight Percent Diff: -93.23322032086058
Wing Weight Percent Diff: 8.26743549310153
WING DIFFERENCES
Wing Span Percent Diff: -0.029997996845333903
Wing Area Percent Diff: 32.90022842687177
HORIZONTAL TAIL DIFFERENCES
HT Area Percent Diff: 40.489576650137494
VERTICAL TAIL DIFFERENCES
VT Span Percent Diff: -11.022306825728005
VT Area Percent Diff: -60.38680571118094
CRUISE SEGMENT 1 DRAG DIFFERENCES
Overall Cd Percent Diff: [-18.54737792]
L/D Percent Diff: [24.01020217]
Nacelle Cd Percent Diff: [-94.27640436]
HT Cd Percent Diff: [-80.76934841] dimensionless
Fuselage Cd Percent Diff: [108.78752887]
VT Cd Percent Diff: [-58.00304986] dimensionless
Wing Cd percent Diff: [-14.22936117]
Induced Drag Cd Percent Diff: [1.21931584]
CRUISE SEGMENT 1 TSFC DIFFERENCES
Initial Cruise TSFC Percent Diff: [-90.57035921]
FUSELAGE DIFFERENCES
Weight of HB material: -38.35923841364424
Weight of VB material: 87.8307550215667
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.71260527]
Mission1
========
Cost
----
W_{f_{total}}[:].sum()
Constraints
-----------
W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin}
PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:])
x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:])
x_{CG}[3] <= \Delta x_n + x_n
\Delta x_m + x_{CG}[3] >= x_m
\tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m
C_{D_{fuse}}[:] = 0.018081
M_{fuseD} = 0.72
W_{start}[0] = W_{total}[:]
W_{start}[:] >= W_{end}[:] + W_{burn}[:]
W_{start}[1:] = W_{end}[:4]
W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1]
W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2]
W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1]
hft[2] >= CruiseAlt
hft[1:5] = hft[:4] + dhft[1:5]
hft[0] = dhft[0]
dhft[1:3] = dhft[:2]
RC[0] >= 2.5e+03
RC[:3] >= RC_{min}[:3]
\theta[2] >= 0.015
hft[2] >= MinCruiseAlt
n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:]
R_{segment}[3:4] = R_{segment}[4:5]
M[3:5] >= M_{min}
0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req}
Fsafetyfac*F[0] = T_e
W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:]
V_2[:] = M_2[:]*a[:]
\alpha_{max,w}[:3] = 0.18
\alpha_{max,w}[3:] = 0.1
0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime
0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime
ClimbTime <= MaxClimbTime
T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}}
F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
OPR[:] <= OPR_{max}
Aircraft
Fuselage
W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on}
W_{pass}[:] >= n_{pass}[:]*W_{avg. pass}
W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo}
W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}}
W_{payload}[:] <= W_{payload_{max}}
n_{pass}[:] <= n_{seat}
n_{rows} = n_{seat}/SPR
l_{shell} = n_{rows}*p_s
\theta_{db} = w_{db}/R_{fuse}
R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db}
A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db}
(PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse}
A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin}
w_{floor} = w_{fuse}
R_{fuse} + w_{db} >= w_{fuse}
h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse}
t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell}
S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2
S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2
l_{fuse} = l_{nose} + l_{shell} + l_{cone}
l_{cone} = R_{fuse}/\lambda_{cone}
x_{shell1} = l_{nose}
x_{shell2} >= l_{nose} + l_{shell}
t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin}
t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin}
\sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell})
\sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin}
l_{floor} >= l_{shell} + 2*R_{fuse}
P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat})
A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor}
V_{floor} = 2*w_{floor}*A_{floor}
W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor}
\tau_{cone} = \sigma_{skin}
W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame})
x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone}
-2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}}
(PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}}
x_{hbend_{Land}} >= x_{wing}
x_{hbend_{Land}} <= l_{fuse}
x_{hbend_{MLF}} >= x_{wing}
x_{hbend_{MLF}} <= l_{fuse}
A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}})
A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}})
A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
A_{2h_{MLF}} >= Mission1.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2)
A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}}
A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}}
A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}}
A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}}
A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}}
A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}}
A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}}
A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}}
V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}}
W_{hbend} >= g*\rho_{bend}*V_{hbend}
x_{vbend} >= x_{wing}
x_{vbend} <= l_{fuse}
B_{0v} = B_{1v}*(x_{tail} - x_{vbend})
B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2)
B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}}
0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}}
V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}}
W_{vbend} >= \rho_{bend}*g*V_{vbend}
x_f = x_{wing} + 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
x_b = x_{wing} - 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
\sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h}
\sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v}
V_{cyl} = A_{skin}*l_{shell}
V_{nose} = S_{nose}*t_{skin}
V_{bulk} = S_{bulk}*t_{skin}
V_{db} = A_{db}*l_{shell}
V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse})
W_{apu} = W_{payload_{max}}*f_{apu}
W_{db} = \rho_{skin}*g*V_{db}
W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk})
W_{window} >= W'_{window}*l_{shell}
W_{padd} = W_{payload_{max}}*f_{padd}
W_{seat} >= W'_{seat}*n_{seat}
W_{seat} >= f_{seat}*W_{payload_{max}}
W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk})
W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db}
W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone})
Wing
WingNoStruct
A_{rect} = c_{tip}*b
0.5*(1 - \lambda)*c_{root}*b <= A_{tri}
p >= 1 + 2*\lambda
2*q >= 1 + p
y_{mac} = b/3*q/p
mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q
\lambda = c_{tip}/c_{root}
S = b*(c_{root} + c_{tip})/2
0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w)
e*(1 + f(\lambda_w)*AR) <= 1
\lambda >= 0.15
V_{fuel, max} <= 0.303*mac^2*b*\tau
W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g
b <= b_{max}
WingBox
AR = b^2/S
0.423*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5)
\tau <= \tau_{max_w}
W_{struct} >= W_{web} + W_{cap}
AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5)
Mission1.Aircraft.Wing.WingBox.N_{lift} = 3
Mission1.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8
\lambda = taper
W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt})
0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}}
Engine
Compressor
(no constraints)
Combustor
(no constraints)
Turbine
(no constraints)
Thrust
(no constraints)
FanMap
(no constraints)
LPCMap
(no constraints)
HPCMap
(no constraints)
Sizing
A_{2} >= A_{5} + A_{7}
FlightState
V[:] = V[:]
a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
V[:] = M[:]*a[:]
Altitude
h[:] = hft[:]
Atmosphere
(P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
\rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
\mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
EnginePerformance
CompressorPerformance
T_{t_0}[:] = T_{atm}[:]/c1[:]^-1
h_{t_0}[:] = C_{p_{air}*T_{t_0}[:]
P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:]
T_{t_{1.8}}[:] = T_{t_0}[:]
h_{t_{1.8}}[:] = h_{t_0}[:]
P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5
T_{T_{2}}[:] = T_{t_{1.8}}[:]
h_{T_{2}}[:] = h_{t_{1.8}}[:]
P_{T_{2}}[:] = P_{t_{1.8}}[:]
P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:]
T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016
h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:]
P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:]
T_{t_7}[:] = T_{t_{2.1}}[:]
h_{t_7}[:] = h_{t_{2.1}}[:]
P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:]
T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152
h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1}
P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:]
T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491
h_{t_3}[:] = C_{p_{2}*T_{t_3}[:]
CombustorPerformance
h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:]
h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:]
fp1[:] = f[:] + 1
M_{4a}[:] = 0.1025
fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5
T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]]
P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891
u_{4a}[:] = M_{4a}[:]*(1.31*Mission1.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a}
u_c[:] = r_{uc}*u_{4a}[:]
P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891
TurbinePerformance
h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:]
P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:]
\pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565
h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:]
P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:]
T_{t_5}[:] = T_{t_{4.9}}[:]
h_{t_5}[:] = h_{t_{4.9}}[:]
ThrustPerformance
P_{8}[:] = P_{atm}[:]
h_{8}[:] = C_{p_{fex}*T_{8}[:]
u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:]
(P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:]
h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:]
P_{6}[:] = P_{atm}[:]
(P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:]
u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:]
h_6[:] = C_{p_{tex}*T_{6}[:]
h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:]
\alpha[:] = m_{fan}[:]/m_{core}[:]
\alpha_{+1}[:] = \alpha[:] + 1
\alpha[:] <= \alpha_{max}
F[:] <= F_{6}[:] + F_{8}[:]
F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:])
TSFC[:] = 1/I_{sp}[:]
F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:]
FanMapPerformance
m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}}
LPCMapPerformance
m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D}
HPCMapPerformance
m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D}
SizingPerformance
P_{7}[:] >= P_{atm}[:]
M_7[:] <= 1
a_{7}[:] = (1.4*Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5
a_{7}[:]*M_7[:] = u_{7}[:]
\rho_7[:] = P_{7}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])
P_{5}[:] >= P_{atm}[:]
M_5[:] <= 1
a_{5}[:] = (1.39*Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5
a_{5}[:]*M_5[:] = u_{5}[:]
\rho_5[:] = P_{5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])
h_{2}[:] = C_{p_{1}*T_{2}[:]
\rho_{2}[:] = P_{2}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:])
u_{2}[:] = M_2[:]*(C_{p_{1}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:]/781)^0.5
h_{2.5}[:] = C_{p_{2}*T_{2.5}[:]
\rho_{2.5}[:] = P_{2.5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:])
u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/781)^0.5
m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine}
d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5
d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5
\eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]])
h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:]
P_{t_4}[:] = \pi_{b}*P_{t_3}[:]
M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]]
M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]])
P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:]
\pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013
\pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10
\pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10
\pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10
m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
\pi_{f}[:] >= 1
\pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10
\pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10
\pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10
\pi_{lc}[:] >= 1
m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
\pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10
\pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10
\pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10
m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref})
\pi_{hc}[:] >= 1
OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:]
P_{t_8}[:] = P_{t_7}[:]
T_{t_8}[:] = T_{t_7}[:]
P_{t_6}[:] = P_{t_5}[:]
T_{t_6}[:] = T_{t_5}[:]
F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:]
I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g)
N_{f}[:]*G_{f} = N_{1}[:]
N_{1}[:] <= 1.1
N_{2}[:] <= 1.1
fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD}
fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD}
P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5
(T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2
P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979
(T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2
M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:]
m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:]
m_{total}[:] = m_{fan}[:] + m_{core}[:]
P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512
T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1
m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2}
P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857
T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1
m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5}
1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD}
0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD}
1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD}
0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD}
m_{lc_D} >= 0.7*m_{coreD}/0.649
m_{lc_D} <= 1.3*m_{coreD}/0.649
m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23
m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23
\bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405
\bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405
F[:] = F_{spec}[:]
T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}}
OPR[:] <= OPR_{max}
VerticalTail
VerticalTailNoStruct
C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}}
L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}}
c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt}))
A_{vt} = b_{vt}^2/S_{vt}
b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt}
p_{vt} >= 1 + 2*\lambda_{vt}
2*q_{vt} >= 1 + p_{vt}
y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt}
\lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}}
\Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}}
\Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt}
\lambda_{vt} >= 0.25
V_{vt} >= V_{vt_{min}}
WingBox
AR_{vt} = (2*b_{vt})^2/(2*S_{vt})
0.423*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
\tau_{vt} <= 0.14
W_{struct} >= 0.5*(W_{web} + W_{cap})
Mission1.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24
AR_{vt}*2*L_{vt_{max}}*Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
Mission1.Aircraft.VerticalTail.WingBox.N_{lift} = 1
Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*Mission1.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8
\lambda_{vt} = taper
W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT})
HorizontalTail
HorizontalTailNoStruct
\Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht}
\Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}}
p_{ht} >= 1 + 2*\lambda_{ht}
2*q_{ht} >= 1 + p_{ht}
y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht}
0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht}
\lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}}
S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2
0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht})
e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1
AR_{ht} = b_{ht}^2/S_{ht}
\lambda_{ht} >= 0.2
\lambda_{ht} <= 1
WingBox
AR_{ht} = b_{ht}^2/S_{ht}
0.423*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
\tau_{ht} <= 0.14
W_{struct} >= W_{web} + W_{cap}
L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2
L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht})
2*AR_{ht}*L_{shear}*Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
Mission1.Aircraft.HorizontalTail.WingBox.N_{lift} = 1
Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission1.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8
L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht}
L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}}
W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht})
LandingGear
l_n + z_{wing} + y_m*\tan(\gamma) >= l_m
T = 2*y_m
x_m >= x_n + B
x_n >= 5
\tan(\phi) = \tan(\phi_{min})
(z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1
\tan(\psi) <= \tan(\psi_{max})
x_{up} - x_m <= l_m/\tan(\theta_{max})
y_m >= l_m
S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG})
l_{oleo} = 2.5*S_{sa}
d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5
l_m >= l_{oleo} + d_{t_m}/2
F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in])
W_{wa,m} = 1.2*F_{w_m}^0.609
F_{w_n} = L_{w_n}*d_{t_n}/1e+03
W_{wa,n} = 1.2*F_{w_n}^0.609
L_{w_m} = L_m/(n_{mg}*n_{wps})
L_{w_n} = L_n/n_{wps}
d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315
w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48
d_{t_n} = 0.8*d_{t_m}
w_{t_n} = 0.8*w_{t_m}
W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g
N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m
W_{mw} = n_{wps}*W_{wa,m}
W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g
\sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}})
W_{nw} >= n_{wps}*W_{wa,n}
L_m <= 9.87*E*I_m/(K*l_m)^2
I_m = PI*r_m^3*t_m
L_n <= 9.87*E*I_n/(K*l_n)^2
I_n = PI*r_n^3*t_n
2*r_m/t_m <= 40
2*r_m/t_n <= 40
h_{hold} >= 2*w_{t_m} + 2*r_m
0.8 >= 2*w_{t_n} + 2*r_n
W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m}))
W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n})
W_{lg} >= C_{lg}*(W_{mg} + W_{ng})
W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m
x_m >= x_{CG_{lg}}
c_{root} = c_0
Mission1.Aircraft.Wing.WingBox.r_{w/c} = Mission1.Aircraft.Fuselage.r_{w/c}
x_w = x_{wing}
Mission1.Aircraft.Fuselage.N_{lift} = Mission1.Aircraft.Wing.WingBox.N_{lift}
f_{L_{total/wing}}*L_{max} >= Mission1.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}}
W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc}
W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:]
W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:]
W_{total}[:] <= W_{total, max}
f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}}
W_{misc} >= W_{lg} + W_{hpesys}
W_{hpesys} = f_{hpesys}*W_{total, max}
x_n <= l_{nose}
x_m >= x_{wing}
\Delta x_{AC_{wing}} + x_{wing} >= x_m
x_{hpesys} = 1.1*l_{nose}
x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys}
d_{nacelle} >= d_{f} + 2*t_{nacelle}
E_{land} >= W_{total, max}/(2*g)*w_{ult}^2
x_{up} = x_{shell2}
L_n = W_{total, max}*\Delta x_m/B
L_m = W_{total, max}*\Delta x_n/B
L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max}
y_{eng} >= y_m
3*n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}}
V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse}
W_{tail} >= n_{vt}*W_{vt} + W_{ht}
2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db}
B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v})
m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht}
x_{CG_{ht}} <= l_{fuse}
V_{ht} = S_{ht}*l_{ht}/(S*mac)
L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}}
L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}}
x_{CG_{vt}} <= l_{fuse}
V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b)
n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max}
n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng}
D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}}
I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:]
I_{z}[:] <= I_{z, max}
S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2
l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}}
f_{S_{nacelle}} = S_{nacelle}*S^-1
A_{inlet} = 0.4*S_{nacelle}
A_{fancowl} = 0.2*S_{nacelle}
A_{exh} = 0.4*S_{nacelle}
A_{corecowl} = 3PI*d_{LPC}^2
W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl})
W_{eadd} = f_{eadd}*W_{engine}
W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon}
W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine})
y_{eng} = 0.5*w_{fuse}
(L_{max} - Mission1.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission1.Aircraft.Wing.WingBox.M_r*c_{root}
A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend})
A_{1h_{MLF}} >= (Mission1.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h})
I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16)
I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81
I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81)
x_{shell2} + l_{cone} >= x_{eng}
x_{eng} >= x_{shell2} + 0.75*l_{cone}
S_{floor} = 0.312*P_{floor}
M_{floor} = 0.0352*P_{floor}*w_{floor}
\Delta R_{fuse} = R_{fuse}*0.43/1.75
b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2
b_{ht_{out}} = 0.5*b_{ht} - w_{fuse}
L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}}
M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}}
L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}}
c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach}
\pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht})
FlightSegment
FlightState
V[:] = V[:]
a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
V[:] = M[:]*a[:]
Altitude
h[:] = hft[:]
Atmosphere
(P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
\rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
\mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
FlightP
P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:]
RC[:] = P_{excess}[:]/W_{avg}[:]
\theta[:]*V[:] = RC[:]
dhft[:] = tmin[:]*RC[:]
R_{segment}[:] = thr[:]*V[:]
WingPerformance
0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:]
\Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:]
\Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2
(AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2
C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:]
\alpha_w[:] <= \alpha_{max,w}[:]
D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:]
C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:]
C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR)
Re_w[:] = \rho[:]*V[:]*mac/\mu[:]
C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114
FuselagePerformance
(no constraints)
VerticalTailPerformance
D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:]
Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:]
C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577
HorizontalTailPerformance
L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:]
C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:]
\alpha_{ht}[:] <= \alpha_{ht,max}
C_{L_{\alpha,ht_0}}[:] = 6.28
D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:]
C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht})
Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:]
C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852
W_{burn}[:] = W_{burn}[:]
F_{fuel}[:] = F_{fuel}[:]
\rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:])
P_{cabin}[:] = 7.5e+04
T_{cabin}[:] = 297
V[:] >= V_{stall}[:]
W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:]
tmin[:] = thr[:]
L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:]
L_{total}[:] = f_{L_{total/wing}}*L_w[:]
L_{total}[:] >= W_{avg}[:] + L_{ht}[:]
D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2
D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:])
C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S)
L/D[:] = W_{avg}[:]/D[:]
W_{Load}[:] <= W_{Load_{max}}[:]
W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S
p_{o}[:] >= L_w[:]*c_{root}/S
\eta_{o}[:] = w_{fuse}/(b/2)
x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:]
c_{m_{w}}[:] = 1.9
x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2)
x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse}
x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}}
x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}}
C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht}
AR_{ht} >= 4
C_{L_{ht}}[:] >= 0.01
SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac
SM[:] >= SM_{min}
SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}}
x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:]
R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:]
C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2
V_{nacelle}[:] = r_{v_{nacelle}}*V[:]
V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]]
r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0)
C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0
D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S
\Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}}
M_2[:3] = M[:3]
M_{2.5}[:3] = 0.6
hold_{2}[:3] = 1.07164
hold_{2.5}[:3] = 1.06372
P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:]
c1[:] = 1 + 0.201*M[:]^2.0
M_2[3:] = M[3:]
M_{2.5}[3:] = 0.6
hold_{2}[3:] = 1.07164
hold_{2.5}[3:] = 1.06372
Beginning signomial solve.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 869
Optimizer - Cones : 0
Optimizer - Scalar variables : 3451 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.03 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.48e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 2.87e+07
Factor - GP saved nzs : 3.32e+04 GP saved flops : 9.06e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.1e+03 1.2e+05 0.00e+00 -1.225677090e+05 2.000000000e+00 1.0e+00 0.04
1 1.6e+03 2.1e+03 8.4e+04 -9.71e-01 -1.216848616e+05 2.766603376e+00 6.9e-01 0.05
2 8.2e+02 1.1e+03 4.4e+04 -9.57e-01 -1.192284454e+05 5.074629256e+00 3.6e-01 0.05
3 2.9e+02 3.9e+02 1.6e+04 -9.16e-01 -1.104950334e+05 2.156321042e+01 1.3e-01 0.06
4 2.9e+02 3.9e+02 1.6e+04 -7.68e-01 -1.085357608e+05 1.724066982e+03 1.3e-01 0.07
5 1.1e+02 1.5e+02 6.0e+03 -7.59e-01 -8.496747542e+04 6.645584441e+03 4.9e-02 0.08
6 3.8e+01 5.0e+01 2.0e+03 -4.14e-01 -4.573108853e+04 1.064008602e+04 1.7e-02 0.08
7 2.0e+01 2.7e+01 1.1e+03 2.50e-01 -2.853524473e+04 6.956951010e+03 9.0e-03 0.09
8 9.4e+00 1.3e+01 5.1e+02 5.70e-01 -1.401680654e+04 4.219068590e+03 4.2e-03 0.10
9 4.7e+00 6.4e+00 2.6e+02 8.27e-01 -7.046366663e+03 2.497942694e+03 2.1e-03 0.11
10 1.4e+00 1.9e+00 7.8e+01 9.33e-01 -2.013352976e+03 9.403827672e+02 6.4e-04 0.11
11 6.4e-01 8.6e-01 3.5e+01 9.93e-01 -6.804485566e+02 6.596896968e+02 2.9e-04 0.12
12 4.8e-01 6.5e-01 2.6e+01 9.96e-01 -4.518204661e+02 5.573058292e+02 2.2e-04 0.13
13 3.5e-01 7.3e-01 1.9e+01 9.80e-01 -2.686036694e+02 4.735665754e+02 1.6e-04 0.14
14 1.7e-01 3.6e-01 9.5e+00 9.96e-01 -1.706351213e+00 3.632401846e+02 7.9e-05 0.14
15 5.7e-02 1.5e-01 3.2e+00 9.94e-01 1.663588588e+02 2.900324402e+02 2.7e-05 0.15
16 3.3e-02 1.3e-01 1.9e+00 1.00e+00 2.025528074e+02 2.744117059e+02 1.6e-05 0.16
17 5.1e-03 1.9e-01 3.2e-01 1.00e+00 2.450077405e+02 2.572047198e+02 2.8e-06 0.17
18 1.5e-03 1.3e-01 9.4e-02 1.00e+00 2.510860215e+02 2.546831567e+02 8.5e-07 0.17
19 4.8e-04 1.1e-01 3.1e-02 1.00e+00 2.528335324e+02 2.540184841e+02 2.8e-07 0.18
20 2.1e-04 8.8e-02 1.3e-02 1.00e+00 2.533175848e+02 2.538309261e+02 1.2e-07 0.19
21 1.9e-04 8.0e-02 1.2e-02 1.00e+00 2.533556918e+02 2.538177109e+02 1.1e-07 0.20
22 1.7e-04 7.3e-02 1.1e-02 1.00e+00 2.533889178e+02 2.538047106e+02 9.9e-08 0.20
23 1.5e-04 6.6e-02 9.8e-03 1.00e+00 2.534188561e+02 2.537930533e+02 9.0e-08 0.21
24 1.4e-04 6.0e-02 8.8e-03 1.00e+00 2.534457755e+02 2.537825390e+02 8.1e-08 0.22
25 1.2e-04 5.5e-02 7.9e-03 1.00e+00 2.534699859e+02 2.537730615e+02 7.3e-08 0.23
26 1.1e-04 5.0e-02 7.1e-03 1.00e+00 2.534917592e+02 2.537645177e+02 6.5e-08 0.23
27 1.0e-04 4.6e-02 6.4e-03 1.00e+00 2.535113429e+02 2.537568176e+02 5.9e-08 0.24
28 9.0e-05 4.2e-02 5.8e-03 1.00e+00 2.535289580e+02 2.537498787e+02 5.3e-08 0.25
29 8.1e-05 3.9e-02 5.2e-03 1.00e+00 2.535448032e+02 2.537436266e+02 4.8e-08 0.26
30 7.3e-05 3.6e-02 4.7e-03 1.00e+00 2.535590570e+02 2.537379938e+02 4.3e-08 0.27
31 6.6e-05 3.3e-02 4.2e-03 1.00e+00 2.535718796e+02 2.537329193e+02 3.9e-08 0.27
32 5.9e-05 3.0e-02 3.8e-03 1.00e+00 2.535834151e+02 2.537283480e+02 3.5e-08 0.28
33 5.3e-05 2.8e-02 3.4e-03 1.00e+00 2.535937929e+02 2.537242304e+02 3.1e-08 0.29
34 4.8e-05 2.6e-02 3.1e-03 1.00e+00 2.536031295e+02 2.537205215e+02 2.8e-08 0.30
35 4.3e-05 2.4e-02 2.8e-03 1.00e+00 2.536115294e+02 2.537171809e+02 2.5e-08 0.30
36 3.9e-05 2.2e-02 2.5e-03 1.00e+00 2.536190868e+02 2.537141721e+02 2.3e-08 0.31
37 3.5e-05 2.1e-02 2.2e-03 1.00e+00 2.536258864e+02 2.537114623e+02 2.0e-08 0.32
38 3.1e-05 2.0e-02 2.0e-03 1.00e+00 2.536320042e+02 2.537090219e+02 1.8e-08 0.33
39 2.8e-05 1.8e-02 1.8e-03 1.00e+00 2.536375087e+02 2.537068241e+02 1.7e-08 0.33
40 2.5e-05 1.7e-02 1.6e-03 1.00e+00 2.536424614e+02 2.537048450e+02 1.5e-08 0.34
41 2.3e-05 1.6e-02 1.5e-03 1.00e+00 2.536469178e+02 2.537030627e+02 1.3e-08 0.35
42 2.1e-05 1.6e-02 1.3e-03 1.00e+00 2.536509277e+02 2.537014579e+02 1.2e-08 0.36
43 1.9e-05 1.5e-02 1.2e-03 1.00e+00 2.536545358e+02 2.537000129e+02 1.1e-08 0.37
44 1.7e-05 1.4e-02 1.1e-03 1.00e+00 2.536577825e+02 2.536987118e+02 9.8e-09 0.37
45 1.5e-05 1.3e-02 9.6e-04 1.00e+00 2.536607040e+02 2.536975404e+02 8.8e-09 0.38
46 1.3e-05 1.3e-02 8.7e-04 1.00e+00 2.536633330e+02 2.536964857e+02 7.9e-09 0.39
47 1.2e-05 1.2e-02 7.8e-04 1.00e+00 2.536656987e+02 2.536955361e+02 7.1e-09 0.40
48 1.1e-05 1.2e-02 7.0e-04 1.00e+00 2.536678276e+02 2.536946813e+02 6.4e-09 0.40
49 9.8e-06 1.1e-02 6.3e-04 1.00e+00 2.536697434e+02 2.536939118e+02 5.8e-09 0.41
50 8.9e-06 1.1e-02 5.7e-04 1.00e+00 2.536714675e+02 2.536932190e+02 5.2e-09 0.42
51 8.0e-06 1.1e-02 5.1e-04 1.00e+00 2.536730190e+02 2.536925954e+02 4.7e-09 0.43
52 7.2e-06 1.0e-02 4.6e-04 1.00e+00 2.536744152e+02 2.536920340e+02 4.2e-09 0.43
53 6.5e-06 1.0e-02 4.1e-04 1.00e+00 2.536756717e+02 2.536915286e+02 3.8e-09 0.44
54 5.8e-06 9.8e-03 3.7e-04 1.00e+00 2.536768025e+02 2.536910737e+02 3.4e-09 0.45
55 5.2e-06 9.6e-03 3.4e-04 1.00e+00 2.536778201e+02 2.536906643e+02 3.1e-09 0.46
56 4.7e-06 9.4e-03 3.0e-04 1.00e+00 2.536787359e+02 2.536902957e+02 2.8e-09 0.46
57 4.2e-06 9.2e-03 2.7e-04 1.00e+00 2.536795600e+02 2.536899639e+02 2.5e-09 0.47
58 3.8e-06 9.0e-03 2.5e-04 1.00e+00 2.536803017e+02 2.536896652e+02 2.2e-09 0.48
59 3.4e-06 8.9e-03 2.2e-04 1.00e+00 2.536809692e+02 2.536893963e+02 2.0e-09 0.49
60 3.1e-06 8.8e-03 2.0e-04 1.00e+00 2.536815699e+02 2.536891543e+02 1.8e-09 0.49
61 1.2e-06 3.4e-03 7.7e-05 1.00e+00 2.536848849e+02 2.536878177e+02 7.0e-10 0.50
62 1.1e-06 3.0e-03 6.9e-05 1.00e+00 2.536850944e+02 2.536877339e+02 6.3e-10 0.51
63 3.8e-07 1.1e-03 2.5e-05 1.00e+00 2.536863010e+02 2.536872470e+02 2.3e-10 0.52
64 3.5e-07 9.8e-04 2.2e-05 1.00e+00 2.536863685e+02 2.536872198e+02 2.0e-10 0.53
65 3.1e-07 8.8e-04 2.0e-05 1.00e+00 2.536864291e+02 2.536871953e+02 1.8e-10 0.53
66 2.8e-07 7.9e-04 1.8e-05 1.00e+00 2.536864836e+02 2.536871733e+02 1.7e-10 0.54
67 2.5e-07 7.1e-04 1.6e-05 1.00e+00 2.536865328e+02 2.536871534e+02 1.5e-10 0.55
68 2.3e-07 6.4e-04 1.5e-05 1.00e+00 2.536865770e+02 2.536871356e+02 1.3e-10 0.56
69 2.0e-07 5.8e-04 1.3e-05 1.00e+00 2.536866167e+02 2.536871195e+02 1.2e-10 0.56
70 1.8e-07 5.2e-04 1.2e-05 1.00e+00 2.536866525e+02 2.536871050e+02 1.1e-10 0.57
71 1.7e-07 4.7e-04 1.1e-05 1.00e+00 2.536866848e+02 2.536870920e+02 9.8e-11 0.58
72 1.5e-07 4.2e-04 9.6e-06 1.00e+00 2.536867138e+02 2.536870803e+02 8.8e-11 0.59
73 1.3e-07 3.8e-04 8.6e-06 1.00e+00 2.536867399e+02 2.536870697e+02 7.9e-11 0.59
74 1.2e-07 3.4e-04 7.8e-06 1.00e+00 2.536867634e+02 2.536870602e+02 7.1e-11 0.60
75 1.1e-07 3.1e-04 7.0e-06 1.00e+00 2.536867845e+02 2.536870517e+02 6.4e-11 0.61
76 9.8e-08 2.8e-04 6.3e-06 1.00e+00 2.536868035e+02 2.536870440e+02 5.8e-11 0.62
77 8.8e-08 2.5e-04 5.7e-06 1.00e+00 2.536868206e+02 2.536870371e+02 5.2e-11 0.63
78 7.9e-08 2.2e-04 5.1e-06 1.00e+00 2.536868360e+02 2.536870308e+02 4.7e-11 0.63
79 7.1e-08 2.0e-04 4.6e-06 1.00e+00 2.536868499e+02 2.536870252e+02 4.2e-11 0.64
80 6.4e-08 1.8e-04 4.1e-06 1.00e+00 2.536868624e+02 2.536870202e+02 3.8e-11 0.65
81 5.8e-08 1.6e-04 3.7e-06 1.00e+00 2.536868736e+02 2.536870156e+02 3.4e-11 0.66
82 5.2e-08 1.5e-04 3.3e-06 1.00e+00 2.536868837e+02 2.536870115e+02 3.1e-11 0.67
83 4.7e-08 1.3e-04 3.0e-06 1.00e+00 2.536868928e+02 2.536870078e+02 2.8e-11 0.67
84 4.2e-08 1.2e-04 2.7e-06 1.00e+00 2.536869010e+02 2.536870045e+02 2.5e-11 0.68
85 3.8e-08 1.1e-04 2.4e-06 1.00e+00 2.536869084e+02 2.536870015e+02 2.2e-11 0.69
86 3.4e-08 9.7e-05 2.2e-06 1.00e+00 2.536869150e+02 2.536869988e+02 2.0e-11 0.70
87 3.1e-08 8.7e-05 2.0e-06 1.00e+00 2.536869210e+02 2.536869964e+02 1.8e-11 0.70
88 2.8e-08 7.8e-05 1.8e-06 9.99e-01 2.536869263e+02 2.536869943e+02 1.6e-11 0.71
89 2.5e-08 7.0e-05 1.6e-06 1.00e+00 2.536869312e+02 2.536869923e+02 1.5e-11 0.72
90 2.2e-08 6.3e-05 1.4e-06 1.00e+00 2.536869355e+02 2.536869905e+02 1.3e-11 0.73
91 2.0e-08 5.7e-05 1.3e-06 1.00e+00 2.536869394e+02 2.536869889e+02 1.2e-11 0.74
92 1.8e-08 5.1e-05 1.2e-06 9.99e-01 2.536869429e+02 2.536869875e+02 1.1e-11 0.74
93 1.6e-08 4.6e-05 1.0e-06 1.00e+00 2.536869461e+02 2.536869862e+02 9.6e-12 0.75
94 1.5e-08 4.2e-05 9.4e-07 1.00e+00 2.536869490e+02 2.536869851e+02 8.6e-12 0.76
95 1.3e-08 3.7e-05 8.5e-07 9.99e-01 2.536869515e+02 2.536869840e+02 7.8e-12 0.77
96 1.2e-08 3.4e-05 7.7e-07 9.98e-01 2.536869538e+02 2.536869831e+02 7.0e-12 0.78
97 1.1e-08 3.0e-05 6.9e-07 9.99e-01 2.536869559e+02 2.536869822e+02 6.3e-12 0.78
Optimizer terminated. Time: 0.79
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 2.5368695593e+02 nrm: 4e+01 Viol. con: 2e-07 var: 0e+00
Dual. obj: 2.5368698225e+02 nrm: 8e+02 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.811 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 870
Optimizer - Cones : 0
Optimizer - Scalar variables : 3453 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.03 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.48e+04 after factor : 1.47e+05
Factor - dense dim. : 0 flops : 2.89e+07
Factor - GP saved nzs : 3.32e+04 GP saved flops : 9.06e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.1e+03 1.2e+05 0.00e+00 -1.222298263e+05 2.000000000e+00 1.0e+00 0.04
1 1.6e+03 2.1e+03 8.5e+04 -9.71e-01 -1.213710455e+05 2.752982256e+00 6.9e-01 0.05
2 7.8e+02 1.0e+03 4.2e+04 -9.57e-01 -1.186217467e+05 5.334792787e+00 3.4e-01 0.05
3 2.9e+02 3.9e+02 1.6e+04 -9.11e-01 -1.102259194e+05 2.219994521e+01 1.3e-01 0.06
4 2.9e+02 3.9e+02 1.6e+04 -7.68e-01 -1.083267789e+05 1.672821615e+03 1.3e-01 0.07
5 1.2e+02 1.6e+02 6.6e+03 -7.60e-01 -8.749626988e+04 6.083313951e+03 5.4e-02 0.08
6 3.9e+01 5.3e+01 2.1e+03 -4.56e-01 -4.677954462e+04 1.085256007e+04 1.7e-02 0.08
7 2.3e+01 3.0e+01 1.2e+03 2.29e-01 -3.113771930e+04 7.216008013e+03 1.0e-02 0.09
8 9.3e+00 1.2e+01 5.0e+02 5.24e-01 -1.393505869e+04 3.980814731e+03 4.1e-03 0.10
9 6.0e+00 8.0e+00 3.2e+02 8.27e-01 -9.009823590e+03 2.812604557e+03 2.7e-03 0.11
10 2.1e+00 2.8e+00 1.1e+02 9.04e-01 -3.057301137e+03 1.183564269e+03 9.3e-04 0.12
11 1.4e+00 1.9e+00 7.7e+01 9.76e-01 -1.997372761e+03 9.332543213e+02 6.4e-04 0.12
12 7.4e-01 1.0e+00 4.0e+01 9.81e-01 -9.699632101e+02 5.758019022e+02 3.3e-04 0.13
13 4.2e-01 7.2e-01 2.3e+01 9.89e-01 -4.606257868e+02 4.178451514e+02 1.9e-04 0.14
14 1.6e-01 2.8e-01 8.7e+00 9.97e-01 -6.512326323e+01 2.680538298e+02 7.3e-05 0.15
15 8.8e-02 1.6e-01 4.9e+00 1.00e+00 3.921207159e+01 2.264578862e+02 4.1e-05 0.15
16 3.1e-02 1.2e-01 1.7e+00 1.00e+00 1.252317814e+02 1.912713104e+02 1.5e-05 0.16
17 1.1e-02 9.8e-02 6.5e-01 1.01e+00 1.548024777e+02 1.794850661e+02 5.6e-06 0.17
18 6.0e-03 7.7e-02 3.5e-01 1.01e+00 1.628860752e+02 1.761840348e+02 3.0e-06 0.18
19 1.1e-03 1.5e-01 6.8e-02 1.01e+00 1.705511844e+02 1.731209203e+02 6.1e-07 0.18
20 4.2e-04 1.1e-01 2.6e-02 1.01e+00 1.716970465e+02 1.726831638e+02 2.4e-07 0.19
21 1.8e-04 9.1e-02 1.1e-02 1.00e+00 1.721010799e+02 1.725269096e+02 1.0e-07 0.20
22 1.0e-04 7.2e-02 6.3e-03 1.00e+00 1.722342738e+02 1.724717849e+02 5.7e-08 0.21
23 9.0e-05 6.5e-02 5.6e-03 1.00e+00 1.722520170e+02 1.724658133e+02 5.1e-08 0.21
24 8.1e-05 6.0e-02 5.1e-03 1.00e+00 1.722673117e+02 1.724597216e+02 4.6e-08 0.22
25 7.3e-05 5.5e-02 4.6e-03 1.00e+00 1.722811705e+02 1.724543346e+02 4.2e-08 0.23
26 6.6e-05 5.0e-02 4.1e-03 1.00e+00 1.722936134e+02 1.724494569e+02 3.7e-08 0.24
27 5.9e-05 4.6e-02 3.7e-03 1.00e+00 1.723047998e+02 1.724450554e+02 3.4e-08 0.24
28 5.3e-05 4.2e-02 3.3e-03 1.00e+00 1.723148518e+02 1.724410789e+02 3.0e-08 0.25
29 4.8e-05 3.9e-02 3.0e-03 1.00e+00 1.723238843e+02 1.724374861e+02 2.7e-08 0.26
30 4.3e-05 3.6e-02 2.7e-03 1.00e+00 1.723320001e+02 1.724342397e+02 2.5e-08 0.27
31 3.9e-05 3.3e-02 2.4e-03 1.00e+00 1.723392924e+02 1.724313064e+02 2.2e-08 0.28
32 3.5e-05 3.0e-02 2.2e-03 1.00e+00 1.723458452e+02 1.724286563e+02 2.0e-08 0.28
33 3.1e-05 2.8e-02 2.0e-03 1.00e+00 1.723517339e+02 1.724262629e+02 1.8e-08 0.29
34 2.8e-05 2.6e-02 1.8e-03 1.00e+00 1.723570267e+02 1.724241018e+02 1.6e-08 0.30
35 2.5e-05 2.4e-02 1.6e-03 1.00e+00 1.723617843e+02 1.724221513e+02 1.5e-08 0.31
36 2.3e-05 2.3e-02 1.4e-03 1.00e+00 1.723660614e+02 1.724203911e+02 1.3e-08 0.31
37 2.1e-05 2.1e-02 1.3e-03 1.00e+00 1.723699069e+02 1.724188032e+02 1.2e-08 0.32
38 1.9e-05 2.0e-02 1.2e-03 1.00e+00 1.723733647e+02 1.724173710e+02 1.1e-08 0.33
39 1.7e-05 1.9e-02 1.0e-03 1.00e+00 1.723764740e+02 1.724160795e+02 9.5e-09 0.34
40 1.5e-05 1.8e-02 9.4e-04 1.00e+00 1.723792702e+02 1.724149150e+02 8.6e-09 0.35
41 1.4e-05 1.7e-02 8.5e-04 1.00e+00 1.723817850e+02 1.724138651e+02 7.7e-09 0.36
42 1.2e-05 1.6e-02 7.6e-04 1.00e+00 1.723840467e+02 1.724129188e+02 6.9e-09 0.37
43 1.1e-05 1.5e-02 6.9e-04 1.00e+00 1.723860810e+02 1.724120658e+02 6.2e-09 0.37
44 9.9e-06 1.4e-02 6.2e-04 1.00e+00 1.723879108e+02 1.724112971e+02 5.6e-09 0.38
45 8.9e-06 1.4e-02 5.6e-04 1.00e+00 1.723895567e+02 1.724106044e+02 5.1e-09 0.39
46 8.0e-06 1.3e-02 5.0e-04 1.00e+00 1.723910373e+02 1.724099802e+02 4.6e-09 0.40
47 7.2e-06 1.3e-02 4.5e-04 1.00e+00 1.723923692e+02 1.724094178e+02 4.1e-09 0.40
48 6.5e-06 1.2e-02 4.1e-04 1.00e+00 1.723935674e+02 1.724089112e+02 3.7e-09 0.41
49 5.8e-06 1.2e-02 3.6e-04 1.00e+00 1.723946453e+02 1.724084548e+02 3.3e-09 0.42
50 5.2e-06 1.1e-02 3.3e-04 1.00e+00 1.723956151e+02 1.724080436e+02 3.0e-09 0.43
51 4.7e-06 1.1e-02 3.0e-04 1.00e+00 1.723964875e+02 1.724076733e+02 2.7e-09 0.44
52 4.2e-06 1.1e-02 2.7e-04 1.00e+00 1.723972725e+02 1.724073397e+02 2.4e-09 0.44
53 3.8e-06 1.0e-02 2.4e-04 1.00e+00 1.723979788e+02 1.724070393e+02 2.2e-09 0.45
54 3.4e-06 1.0e-02 2.2e-04 1.00e+00 1.723986142e+02 1.724067687e+02 2.0e-09 0.46
55 3.1e-06 9.9e-03 1.9e-04 1.00e+00 1.723991860e+02 1.724065251e+02 1.8e-09 0.47
56 2.8e-06 9.7e-03 1.7e-04 1.00e+00 1.723997005e+02 1.724063056e+02 1.6e-09 0.47
57 2.5e-06 9.5e-03 1.6e-04 1.00e+00 1.724001634e+02 1.724061080e+02 1.4e-09 0.48
58 2.3e-06 9.3e-03 1.4e-04 1.00e+00 1.724005799e+02 1.724059301e+02 1.3e-09 0.49
59 2.0e-06 9.2e-03 1.3e-04 1.00e+00 1.724009547e+02 1.724057699e+02 1.2e-09 0.50
60 1.8e-06 9.0e-03 1.1e-04 1.00e+00 1.724012919e+02 1.724056257e+02 1.0e-09 0.50
61 1.6e-06 8.9e-03 1.0e-04 1.00e+00 1.724015954e+02 1.724054958e+02 9.4e-10 0.51
62 1.5e-06 8.8e-03 9.3e-05 1.00e+00 1.724018684e+02 1.724053788e+02 8.4e-10 0.52
63 1.3e-06 8.7e-03 8.4e-05 1.00e+00 1.724021142e+02 1.724052735e+02 7.6e-10 0.53
64 1.2e-06 8.6e-03 7.5e-05 1.00e+00 1.724023353e+02 1.724051787e+02 6.8e-10 0.53
65 1.1e-06 8.5e-03 6.8e-05 1.00e+00 1.724025342e+02 1.724050933e+02 6.2e-10 0.54
66 9.7e-07 8.4e-03 6.1e-05 1.00e+00 1.724027133e+02 1.724050165e+02 5.5e-10 0.55
67 8.7e-07 8.3e-03 5.5e-05 1.00e+00 1.724028744e+02 1.724049473e+02 5.0e-10 0.56
68 7.9e-07 8.3e-03 4.9e-05 1.00e+00 1.724030194e+02 1.724048850e+02 4.5e-10 0.57
69 7.1e-07 8.2e-03 4.4e-05 1.00e+00 1.724031498e+02 1.724048289e+02 4.0e-10 0.57
70 6.4e-07 8.1e-03 4.0e-05 1.00e+00 1.724032672e+02 1.724047784e+02 3.6e-10 0.58
71 5.7e-07 8.1e-03 3.6e-05 1.00e+00 1.724033729e+02 1.724047329e+02 3.3e-10 0.59
72 5.2e-07 8.0e-03 3.2e-05 1.00e+00 1.724034679e+02 1.724046920e+02 2.9e-10 0.60
73 4.6e-07 8.0e-03 2.9e-05 1.00e+00 1.724035535e+02 1.724046551e+02 2.7e-10 0.61
74 4.2e-07 7.9e-03 2.6e-05 1.00e+00 1.724036305e+02 1.724046220e+02 2.4e-10 0.61
75 3.8e-07 7.9e-03 2.4e-05 1.00e+00 1.724036997e+02 1.724045921e+02 2.1e-10 0.62
76 3.4e-07 7.9e-03 2.1e-05 1.00e+00 1.724037621e+02 1.724045652e+02 1.9e-10 0.63
77 3.1e-07 7.8e-03 1.9e-05 1.00e+00 1.724038182e+02 1.724045410e+02 1.7e-10 0.64
78 2.7e-07 7.8e-03 1.7e-05 1.00e+00 1.724038687e+02 1.724045192e+02 1.6e-10 0.64
79 2.5e-07 7.8e-03 1.5e-05 1.00e+00 1.724039141e+02 1.724044996e+02 1.4e-10 0.65
80 2.2e-07 7.7e-03 1.4e-05 1.00e+00 1.724039550e+02 1.724044819e+02 1.3e-10 0.66
81 2.0e-07 7.7e-03 1.3e-05 1.00e+00 1.724039918e+02 1.724044660e+02 1.1e-10 0.67
82 1.8e-07 7.7e-03 1.1e-05 1.00e+00 1.7240402E
======================================================================
ERROR [28.771s]: test_SPaircraft_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/gpkit/tests/from_paths.py", line 51, in
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/gpkit/tests/from_paths.py", line 40, in test_fn
mod.test()
File "SPaircraft.py", line 87, in test
sol = optimize_aircraft(m, substitutions, fixedBPR, pRatOpt, mutategparg)
File "SPaircraft.py", line 62, in optimize_aircraft
sol = m_relax.localsolve(verbosity=4, iteration_limit=200, reltol=0.01, mutategp=mutategparg, x0 = x0)
File "/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/gpkit/constraints/prog_factories.py", line 124, in solvefn
result = progsolve(solver, verbosity, **kwargs)
File "/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/gpkit/constraints/sgp.py", line 149, in localsolve
feas_constrs, None)
File "/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/gpkit/constraints/gp.py", line 112, in __init__
+ boundstrs)
ValueError: Geometric Program is not fully bounded:
Mission1.Aircraft.Engine.EngineConstants.Relax1.R has no lower bound
Mission1.Aircraft.Engine.EngineConstants.Relax1.g has no lower bound
----------------------------------------------------------------------
Ran 1 test in 28.771s
FAILED (errors=1)
Generating XML reports...
49e+02 1.724044517e+02 1.0e-10 0.67
83 1.6e-07 7.7e-03 1.0e-05 1.00e+00 1.724040546e+02 1.724044388e+02 9.2e-11 0.68
84 1.5e-07 7.7e-03 9.1e-06 1.00e+00 1.724040815e+02 1.724044272e+02 8.3e-11 0.69
85 1.3e-07 7.6e-03 8.2e-06 1.00e+00 1.724041056e+02 1.724044167e+02 7.5e-11 0.70
86 1.2e-07 7.6e-03 7.4e-06 1.00e+00 1.724041273e+02 1.724044073e+02 6.7e-11 0.71
87 1.1e-07 7.6e-03 6.7e-06 1.00e+00 1.724041470e+02 1.724043988e+02 6.1e-11 0.71
88 9.6e-08 7.6e-03 6.0e-06 1.00e+00 1.724041646e+02 1.724043912e+02 5.5e-11 0.72
89 8.6e-08 7.6e-03 5.4e-06 1.00e+00 1.724041804e+02 1.724043843e+02 4.9e-11 0.73
90 7.8e-08 7.6e-03 4.9e-06 9.97e-01 1.724041946e+02 1.724043781e+02 4.4e-11 0.74
91 7.0e-08 7.5e-03 4.4e-06 1.00e+00 1.724042074e+02 1.724043726e+02 4.0e-11 0.74
92 6.3e-08 7.5e-03 3.9e-06 9.99e-01 1.724042189e+02 1.724043676e+02 3.6e-11 0.75
93 5.7e-08 6.8e-03 3.5e-06 1.02e+00 1.724042300e+02 1.724043628e+02 3.3e-11 0.76
94 5.1e-08 6.1e-03 3.2e-06 1.01e+00 1.724042398e+02 1.724043585e+02 2.9e-11 0.77
95 4.6e-08 5.5e-03 2.9e-06 1.01e+00 1.724042484e+02 1.724043549e+02 2.7e-11 0.77
96 4.2e-08 4.9e-03 2.6e-06 1.02e+00 1.724042564e+02 1.724043515e+02 2.4e-11 0.78
97 3.8e-08 4.4e-03 2.3e-06 9.97e-01 1.724042630e+02 1.724043486e+02 2.2e-11 0.79
98 3.4e-08 4.0e-03 2.1e-06 9.95e-01 1.724042689e+02 1.724043460e+02 2.0e-11 0.80
99 3.1e-08 3.6e-03 1.9e-06 9.91e-01 1.724042743e+02 1.724043436e+02 1.8e-11 0.81
100 2.8e-08 3.2e-03 1.7e-06 9.09e-01 1.724042791e+02 1.724043415e+02 1.6e-11 0.81
101 3.9e-08 7.7e-04 4.0e-07 1.00e+00 1.724043125e+02 1.724043276e+02 4.0e-12 0.82
102 1.1e-07 6.9e-04 3.6e-07 -7.72e-01 1.724043128e+02 1.724043312e+02 3.4e-12 0.83
103 1.1e-07 6.9e-04 3.6e-07 -3.73e+00 1.724043128e+02 1.724043312e+02 3.4e-12 0.84
Optimizer terminated. Time: 0.84
solsta = 7, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : NEAR_OPTIMAL
Primal. obj: 1.7240431284e+02 nrm: 4e+01 Viol. con: 3e-06 var: 0e+00
Dual. obj: 1.7240433117e+02 nrm: 8e+02 Viol. con: 0e+00 var: 7e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.863 seconds.
Cloning into 'solar'...
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Requirement already satisfied: pandas in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.8.0)
Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5)
Requirement already satisfied: pytz>=2011k in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from pandas) (2013.7)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0)
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting git+https://github.com/convexengineering/gpfit.git
Cloning https://github.com/convexengineering/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-V4F5Cj
Running command git clone -q https://github.com/convexengineering/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-V4F5Cj
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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=e558e72020ff084cd80b0e8d7a6baa7203c300e986a759809837922f3daa1934
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-CgUI_a/wheels/d5/94/ac/b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting git+https://github.com/convexengineering/gassolar.git
Cloning https://github.com/convexengineering/gassolar.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-VWv3eb
Running command git clone -q https://github.com/convexengineering/gassolar.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-VWv3eb
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek (from gassolar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.12.0)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.8.0)
Requirement already satisfied: pytz>=2011k in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from pandas->gassolar==0.0.0.0) (2013.7)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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=4b2709a42b17fbff26ae0fc8051e5111d4c917e5756f68cd4f2d66be07443e8c
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-h0qhb4/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Processing /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/solar
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek (from solar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.24.2)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/gplibrary (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.12.0)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2.8.0)
Requirement already satisfied: pytz>=2011k in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from pandas->solar==0.0.0.0) (2013.7)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->solar==0.0.0.0) (1.0.2)
Building wheels for collected packages: solar
Building wheel for solar (setup.py): started
Building wheel for solar (setup.py): finished with status 'done'
Created wheel for solar: filename=solar-0.0.0.0-cp27-none-any.whl size=14811 sha256=1003d06bfe318d283643c84ac043a0b2f60734fd4380f8f3bed814549af922a4
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-ShrBiI/wheels/c5/7c/ab/d5d14ab6469ea1bbff2179d6144368b7affd362fb7225dc095
Successfully built solar
Installing collected packages: solar
Successfully installed solar-0.0.0.0
Running tests...
----------------------------------------------------------------------
/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
tau = np.exp(-0.175/costhsun)
/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
tau = np.exp(-0.175/costhsun)
....
----------------------------------------------------------------------
Ran 6 tests in 181.700s
OK
Generating XML reports...
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
adding test for 'solar/npod_trade.py'
N=1
Beginning signomial solve.
Solving took 5 GP solves and 0.979 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 0.8904 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1632916.9435 but bound is 600000.0000
Warning: Variable Mission.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1259333.2960 but bound is 1000000.0000
N=3
Beginning signomial solve.
Solving took 5 GP solves and 0.865 seconds.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1135 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1036204.4449 but bound is 600000.0000
Warning: Variable Mission1.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1006645.3573 but bound is 1000000.0000
N=5
Beginning signomial solve.
Solving took 5 GP solves and 0.979 seconds.
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1487 but bound is 0.9465
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 989673.4666 but bound is 600000.0000
Warning: Variable Mission2.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1019678.5408 but bound is 1000000.0000
N=7
Beginning signomial solve.
Solving took 5 GP solves and 1.05 seconds.
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 976142.1475 but bound is 600000.0000
Warning: Variable Mission3.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1042059.4123 but bound is 1000000.0000
N=9
Beginning signomial solve.
Solving took 5 GP solves and 1.22 seconds.
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1567 but bound is 0.9465
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1007400.4785 but bound is 600000.0000
Warning: Variable Mission4.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1092545.5150 but bound is 1000000.0000
N=0
Beginning signomial solve.
Solving took 4 GP solves and 0.634 seconds.
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2078 but bound is 600000.0000
N=1
Beginning signomial solve.
Solving took 5 GP solves and 1.32 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 0.8904 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1632919.3776 but bound is 600000.0000
Warning: Variable Mission.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1259329.5070 but bound is 1000000.0000
N=3
Beginning signomial solve.
Solving took 5 GP solves and 1.21 seconds.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1135 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1036209.6021 but bound is 600000.0000
Warning: Variable Mission1.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1006641.3990 but bound is 1000000.0000
N=5
Beginning signomial solve.
Solving took 5 GP solves and 1.25 seconds.
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1487 but bound is 0.9465
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 989673.1341 but bound is 600000.0000
Warning: Variable Mission2.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1019680.6011 but bound is 1000000.0000
N=7
Beginning signomial solve.
Solving took 5 GP solves and 1.46 seconds.
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 976138.7332 but bound is 600000.0000
Warning: Variable Mission3.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1042059.9154 but bound is 1000000.0000
N=9
Beginning signomial solve.
Solving took 5 GP solves and 1.72 seconds.
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1567 but bound is 0.9465
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1007396.6632 but bound is 600000.0000
Warning: Variable Mission4.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1092544.5684 but bound is 1000000.0000
N=0
Beginning signomial solve.
Solving took 4 GP solves and 0.965 seconds.
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119116.3963 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 4.25 seconds.
Allowing negative dual variable(s) as small as -3.6246815899639153e-11.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.3227 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 671709.7480 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 3.98 seconds.
Allowing negative dual variable(s) as small as -5.780984487322902e-10.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2812 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 729183.6293 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 3.22 seconds.
Allowing negative dual variable(s) as small as -7.486587934225628e-12.
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2258 but bound is 0.9465
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 802959.5997 but bound is 600000.0000
Using solver 'mosek'
Solving for 7672 variables.
Solving took 1.51 seconds.
Allowing negative dual variable(s) as small as -1.2634497534364602e-11.
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2008 but bound is 0.9465
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 839122.5079 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 3.48 seconds.
Allowing negative dual variable(s) as small as -3.6246815899639153e-11.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.3227 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 671709.7480 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 3.63 seconds.
Allowing negative dual variable(s) as small as -5.780984487322902e-10.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2812 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 729183.6293 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 3.46 seconds.
Allowing negative dual variable(s) as small as -7.486587934225628e-12.
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2258 but bound is 0.9465
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 802959.5997 but bound is 600000.0000
Using solver 'mosek'
Solving for 7672 variables.
Solving took 1.64 seconds.
Allowing negative dual variable(s) as small as -1.2634497534364602e-11.
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2008 but bound is 0.9465
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 839122.5079 but bound is 600000.0000
Beginning signomial solve.
Solving took 4 GP solves and 0.549 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2076 but bound is 600000.0000
Beginning signomial solve.
Solving took 4 GP solves and 0.582 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2076 but bound is 600000.0000
fatal: destination path 'gplibrary' already exists and is not an empty directory.
fatal: destination path 'gplibrary' already exists and is not an empty directory.
fatal: destination path 'gplibrary' already exists and is not an empty directory.
fatal: destination path 'gplibrary' already exists and is not an empty directory.
fatal: destination path 'gplibrary' already exists and is not an empty directory.
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Requirement already satisfied: pandas in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.8.0)
Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.5)
Requirement already satisfied: pytz>=2011k in /System/Library/Frameworks/Python.framework/Versions/2.7/Extras/lib/python (from pandas) (2013.7)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0)
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting git+https://github.com/hoburg/gpfit.git
Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-HZ8bne
Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-HZ8bne
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/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/gpkit_PullRequest_Models/buildnode/macys/optimizer/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=404298cc1fad2910a919c93e2a1d42700661f56502f24e6f61203d103257f9d9
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-0_V343/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Processing /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/gplibrary
Requirement already satisfied: numpy>=1.12 in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.16.5)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.9)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint->gpkitmodels==0.0.0.0) (1.0.2)
Building wheels for collected packages: gpkitmodels
Building wheel for gpkitmodels (setup.py): started
Building wheel for gpkitmodels (setup.py): finished with status 'done'
Created wheel for gpkitmodels: filename=gpkitmodels-0.0.0.0-cp27-none-any.whl size=65697 sha256=e2b91055a2831206cd1207204e015078173495d9a125828d5a2248d34742410d
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-gbx0gY/wheels/41/dd/09/efaabd52c0fc91a3ab7827d0449f3cca33f90b69e85ad4dd27
Successfully built gpkitmodels
Installing collected packages: gpkitmodels
Found existing installation: gpkitmodels 0.0.0.0
Uninstalling gpkitmodels-0.0.0.0:
Successfully uninstalled gpkitmodels-0.0.0.0
Successfully installed gpkitmodels-0.0.0.0
Running tests...
----------------------------------------------------------------------
../Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped.
warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning)
..............
----------------------------------------------------------------------
Ran 16 tests in 6.803s
OK
Generating XML reports...
adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py'
adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py'
adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py'
adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py'
adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py'
adding test for 'gpkitmodels/SP/SimPleAC/SimPleAC.py'
adding test for 'gpkitmodels/SP/SimPleAC/SimPleAC_mission.py'
adding test for 'gpkitmodels/SP/SimPleAC/SimPleAC_multimission.py'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.0106 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.0306 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.00977 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.00928 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.00953 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 0.415 seconds.
Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.031 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.0306 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.0311 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 0.857 seconds.
Using solver 'mosek'
Solving for 13 variables.
Solving took 0.00995 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 0.291 seconds.
Warning: Variable BladeElementProp.BladeElementPerf.cl[:] could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable BladeElementProp.BladeElementPerf.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1619898.0180 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.0308 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 0.588 seconds.
Warning: Variable BladeElementProp.BladeElementPerf.cl[:] could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable BladeElementProp.BladeElementPerf.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000
Warning: Variable TailAero.Re could cause inaccurate result because it is above upper bound. Solution is 2220953.3838 but bound is 1000000.0000
Warning: Variable TailAero1.Re could cause inaccurate result because it is above upper bound. Solution is 2499787.9776 but bound is 1000000.0000
Warning: Variable TailAero2.Re could cause inaccurate result because it is above upper bound. Solution is 2223878.3883 but bound is 1000000.0000
Warning: Variable TailAero3.Re could cause inaccurate result because it is above upper bound. Solution is 2223877.9590 but bound is 1000000.0000
Warning: Variable TailAero4.Re could cause inaccurate result because it is above upper bound. Solution is 1853897.1004 but bound is 1000000.0000
Warning: Variable TailAero5.Re could cause inaccurate result because it is above upper bound. Solution is 1853897.1004 but bound is 1000000.0000
Warning: Variable TailAero.Re could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000
Warning: Variable TailAero1.Re could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000
Warning: Variable TailAero2.Re could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable TailAero3.Re could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable TailAero4.Re could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable TailAero5.Re could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable WingAero.Re could cause inaccurate result because it is above upper bound. Solution is 1884891.6332 but bound is 700000.0000
Warning: Variable WingAero1.Re could cause inaccurate result because it is above upper bound. Solution is 1910419.6195 but bound is 700000.0000
Warning: Variable WingAero.Re could cause inaccurate result because it is above upper bound. Solution is 1910412.9866 but bound is 700000.0000
Warning: Variable WingAero1.Re could cause inaccurate result because it is above upper bound. Solution is 1910412.9866 but bound is 700000.0000
SP is not converging! Last GP iteration had a higher cost (3e+03) than the previous one (2.7e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (3e+03) than the previous one (2.7e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (3.4e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (3.4e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
Beginning signomial solve.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.0104 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.0091 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.00942 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.00938 seconds.
Solving took 4 GP solves and 0.0427 seconds.
Beginning signomial solve.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.0399 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.0346 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.159 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.0326 seconds.
Solving took 4 GP solves and 0.274 seconds.
Cloning into 'eVTOL'...
Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 3.563s
OK
Generating XML reports...
adding test for 'models/model_tests.py'
Found no installed solvers, beginning a build.
# Moving to the directory from which GPkit was imported.
Started building gpkit...
Attempting to find and build solvers:
# Looking for mosek
# Found /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h
# Found /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib
# Found /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.c
# Found /Users/jenkins/mosek/8/tools/examples/c/expopt.c
# Found /Users/jenkins/mosek/8/tools/examples/c/dgopt.c
# Found /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.h
# Found /Users/jenkins/mosek/8/tools/examples/c/expopt.h
# Found /Users/jenkins/mosek/8/tools/examples/c/dgopt.h
# Found /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h
# Found mosek version 8, installed to /Users/jenkins/mosek
#
# Building mosek...
# Replacing directory _mosek/build
# Replacing directory /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/build_gpkit
#
# Copying expopt library files to _mosek/build
# Copying /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.c
# Copying /Users/jenkins/mosek/8/tools/examples/c/expopt.c
# Copying /Users/jenkins/mosek/8/tools/examples/c/dgopt.c
# Copying /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.h
# Copying /Users/jenkins/mosek/8/tools/examples/c/expopt.h
# Copying /Users/jenkins/mosek/8/tools/examples/c/dgopt.h
# Copying /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h
#
# Applying expopt patches...
#
# Change in _mosek/build/dgopt.con line 651
# -- printf("Number of Hessian non-zeros: %d\n",nlh[0]->numhesnz);
# ++ MSK_echotask(task,MSK_STREAM_MSG,"Number of Hessian non-zeros: %d\n",n
#
# Change in _mosek/build/expopt.con line 566
# -- printf("Warning: The variable with index '%d' has only positiv
# ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in
#
# Change in _mosek/build/expopt.con line 579
# -- printf("Warning: The variable with index '%d' has only negativ
# ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in
#
# Change in _mosek/build/expopt.con line 1115
# -- printf ("solsta = %d, prosta = %d\n", (int)*solsta,(int)*prosta);
# ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "solsta = %d, prosta = %d\n",
#
# Building expopt library...
# Calling 'gcc -fpic -shared -Wl,-rpath "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin" _mosek/build/scopt-ext.c _mosek/build/expopt.c _mosek/build/dgopt.c "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib" -o /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/build_gpkit/expopt.so'
##
### CALL BEGINS
### CALL ENDS
##
# Calling 'install_name_tool -change libmosek64.8.1.dylib /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib /Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/build_gpkit/expopt.so'
##
### CALL BEGINS
### CALL ENDS
##
# Calling 'install_name_tool -change libmosek64.8.1.dylib @executable_path/libmosek64.8.1.dylib /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/mskexpopt'
##
### CALL BEGINS
### CALL ENDS
##
# Done building mosek
# Looking for mosek_cli
# Trying to run mskexpopt...
# Calling 'mskexpopt'
##
### CALL BEGINS
### CALL ENDS
##
# Found mosek_cli in system path
# Looking for cvxopt
# Trying to import cvxopt...
# Found cvxopt in Python path
...finished building gpkit.
Replaced found solvers ([u'mosek', u'mosek_cli', u'cvxopt']) with environment var GPKITSOLVERS (mosek, mosek_cli)
Found the following solvers: mosek, mosek_cli
# Replacing directory env
x[:] <= w
GPkit is now installed with solver(s) [u'mosek', u'mosek_cli']
To incorporate new solvers at a later date, run `gpkit.build()`.
If any tests didn't pass, please post the output above
(starting from "Found no installed solvers, beginning a build.")
to gpkit@mit.edu or https://github.com/convexengineering/gpkit/issues/new
so we can prevent others from having these errors.
The same goes for any other bugs you encounter with GPkit:
send 'em our way, along with any interesting models, speculative features,
comments, discussions, or clarifications you feel like sharing.
Finally, we hope you find our documentation (https://gpkit.readthedocs.io/)
and engineering-design models (https://github.com/convexengineering/gplibrary/)
to be useful resources for your own applications.
Enjoy!
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gplibrary']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/robust.git']
attempt 1
SETTINGS
defaultdict(, {})
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git']
attempt 1
SETTINGS
defaultdict(, {})
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git']
attempt 1
SETTINGS
defaultdict(, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
attempt 1
SETTINGS
defaultdict(, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
attempt 1
SETTINGS
defaultdict(, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
attempt 1
SETTINGS
defaultdict(, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git']
attempt 1
SETTINGS
defaultdict(, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
attempt 1
attempt 2
attempt 3
attempt 4
attempt 5
SETTINGS
defaultdict(, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'})
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
attempt 1
SETTINGS
defaultdict(, {})
[Execution node] check if [macys] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
Build step 'Console output (build log) parsing' changed build result to FAILURE
INFO: Starting to record.
INFO: Processing JUnit
INFO: [JUnit] - 9 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/macys/optimizer/mosek' for the testing framework 'JUnit'.
INFO: Check 'Failed Tests' threshold.
INFO: Check 'Skipped Tests' threshold.
INFO: Setting the build status to FAILURE
INFO: Stopping recording.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: FAILURE