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Started by upstream project "gplibrary_Push_Models" build number 187
originally caused by:
 Started by upstream project "gpkit_Push" build number 654
 originally caused by:
  Started by GitHub push by bqpd
  Started by GitHub push by bqpd
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on windows7x64 in workspace D:\jenkins\workspace\gplibrary_Push_Models\mosek
No credentials specified
Wiping out workspace first.
Cloning the remote Git repository
Cloning repository https://github.com/convexengineering/gplibrary
 > git init D:\jenkins\workspace\gplibrary_Push_Models\mosek # timeout=10
Fetching upstream changes from https://github.com/convexengineering/gplibrary
 > git --version # timeout=10
 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* # timeout=10
 > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10
 > git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10
 > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10
Fetching upstream changes from https://github.com/convexengineering/gplibrary
 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master # timeout=10
Checking out Revision 62fd801e15375d0c0a052852b3f9d7633674eda8 (origin/master)
 > git config core.sparsecheckout # timeout=10
 > git checkout -f 62fd801e15375d0c0a052852b3f9d7633674eda8 # timeout=3
Commit message: "SimPleAC update (new model that doesn't solve on cvxopt)  (#175)"
 > git rev-list --no-walk 62fd801e15375d0c0a052852b3f9d7633674eda8 # timeout=10
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [windows7x64] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [windows7x64] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] enabling perform for step [Execute Windows batch command]
[mosek] $ cmd /c call C:\Users\jenkins\AppData\Local\Temp\jenkins4782068486941405003.bat

D:\jenkins\workspace\gplibrary_Push_Models\mosek>echo C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd 
C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd

D:\jenkins\workspace\gplibrary_Push_Models\mosek>REM turn on the anaconda console 

D:\jenkins\workspace\gplibrary_Push_Models\mosek>call activate.bat   || exit /b 666 

(base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>REM Create a virtualenv to install everything into 

(base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>SET VENV=D:\jenkins\workspace\gplibrary_Push_Models\mosek\venv2_gpkit 

(base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>virtualenv --system-site-packages D:\jenkins\workspace\gplibrary_Push_Models\mosek\venv2_gpkit    || exit /b 666 
New python executable in D:\jenkins\workspace\gplibrary_Push_Models\mosek\venv2_gpkit\Scripts\python.exe
Installing setuptools, pip, wheel...done.

(base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>call D:\jenkins\workspace\gplibrary_Push_Models\mosek\venv2_gpkit\Scripts\activate.bat    || exit /b 666 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>set PATH=C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;D:\jenkins\workspace\gplibrary_Push_Models\mosek\venv2_gpkit\Scripts;D:\Anaconda2;D:\Anaconda2\Library\mingw-w64\bin;D:\Anaconda2\Library\usr\bin;D:\Anaconda2\Library\bin;D:\Anaconda2\Scripts;D:\Anaconda2\bin;D:\Anaconda2\condabin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0;C:\Windows\System32\WindowsPowerShell\v1.0;C:\Program Files\Microsoft SQL Server\110\Tools\Binn;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0;C:\Program Files\Microsoft\Web Platform Installer;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>REM set PATH=C:\mingw-w64\x86_64-7.3.0-posix-seh-rt_v5-rev0\mingw64\bin;C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;D:\jenkins\workspace\gplibrary_Push_Models\mosek\venv2_gpkit\Scripts;D:\Anaconda2;D:\Anaconda2\Library\mingw-w64\bin;D:\Anaconda2\Library\usr\bin;D:\Anaconda2\Library\bin;D:\Anaconda2\Scripts;D:\Anaconda2\bin;D:\Anaconda2\condabin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0;C:\Windows\System32\WindowsPowerShell\v1.0;C:\Program Files\Microsoft SQL Server\110\Tools\Binn;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0;C:\Program Files\Microsoft\Web Platform Installer;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;D:\Git\cmd 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>gcc --version 
gcc (x86_64-posix-seh-rev0, Built by MinGW-W64 project) 6.4.0
Copyright (C) 2017 Free Software Foundation, Inc.
This is free software; see the source for copying conditions.  There is NO
warranty; not even for MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.


(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>REM Update pip 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>python -m 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 d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages (19.2.3)

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>REM Install dependencies 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>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
Requirement already up-to-date: xmlrunner in d:\anaconda2\lib\site-packages (1.7.7)

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>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
Requirement already up-to-date: pint in d:\anaconda2\lib\site-packages (0.9)
Requirement already satisfied, skipping upgrade: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint) (1.0.2)

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>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
Requirement already up-to-date: numpy in d:\anaconda2\lib\site-packages (1.16.4)

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>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
Requirement already up-to-date: scipy in d:\anaconda2\lib\site-packages (1.2.2)
Requirement already satisfied, skipping upgrade: numpy>=1.8.2 in d:\anaconda2\lib\site-packages (from scipy) (1.16.4)

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>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
Requirement already up-to-date: ctypesgen in d:\anaconda2\lib\site-packages (0.post125)

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>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
Requirement already up-to-date: pandas in d:\anaconda2\lib\site-packages (0.24.2)
Requirement already satisfied, skipping upgrade: numpy>=1.12.0 in d:\anaconda2\lib\site-packages (from pandas) (1.16.4)
Requirement already satisfied, skipping upgrade: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2019.2)
Requirement already satisfied, skipping upgrade: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas) (2.8.0)
Requirement already satisfied, skipping upgrade: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0)

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>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
Requirement already up-to-date: matplotlib in d:\anaconda2\lib\site-packages (2.2.4)
Requirement already satisfied, skipping upgrade: python-dateutil>=2.1 in d:\anaconda2\lib\site-packages (from matplotlib) (2.8.0)
Requirement already satisfied, skipping upgrade: pyparsing!=2.0.4,!=2.1.2,!=2.1.6,>=2.0.1 in d:\anaconda2\lib\site-packages (from matplotlib) (2.4.2)
Requirement already satisfied, skipping upgrade: numpy>=1.7.1 in d:\anaconda2\lib\site-packages (from matplotlib) (1.16.4)
Requirement already satisfied, skipping upgrade: pytz in d:\anaconda2\lib\site-packages (from matplotlib) (2019.2)
Requirement already satisfied, skipping upgrade: backports.functools-lru-cache in d:\anaconda2\lib\site-packages (from matplotlib) (1.5)
Requirement already satisfied, skipping upgrade: six>=1.10 in d:\anaconda2\lib\site-packages (from matplotlib) (1.12.0)
Requirement already satisfied, skipping upgrade: cycler>=0.10 in d:\anaconda2\lib\site-packages (from matplotlib) (0.10.0)
Requirement already satisfied, skipping upgrade: kiwisolver>=1.0.1 in d:\anaconda2\lib\site-packages (from matplotlib) (1.1.0)
Requirement already satisfied, skipping upgrade: setuptools in d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages (from kiwisolver>=1.0.1->matplotlib) (41.2.0)

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>if mosek == mosek msktestlic   || exit /b 666 
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : min             
  Type                   : LO (linear optimization problem)
  Constraints            : 1               
  Cones                  : 0               
  Scalar variables       : 5000            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator - tries                  : 0                 time                   : 0.00            
Eliminator - elim's                 : 0               
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Interior-point optimizer terminated. Time: 0.01. 

Optimizer terminated. Time: 0.47    
************************************
A license was checked out correctly.
************************************

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>SET GPKITBUILD=D:\jenkins\workspace\gplibrary_Push_Models\mosek\build_gpkit 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>gcc --version   || exit /b 666 
gcc (x86_64-posix-seh-rev0, Built by MinGW-W64 project) 6.4.0
Copyright (C) 2017 Free Software Foundation, Inc.
This is free software; see the source for copying conditions.  There is NO
warranty; not even for MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.


(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>if mosek == mosek (
msktestlic   || exit /b 666  
 python -c "__import__('mosek').Env()"   || exit /b 666  
 set GPKITSOLVERS=mosek, mosek_cli 
) 
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : min             
  Type                   : LO (linear optimization problem)
  Constraints            : 1               
  Cones                  : 0               
  Scalar variables       : 5000            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator - tries                  : 0                 time                   : 0.00            
Eliminator - elim's                 : 0               
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.00    
Interior-point optimizer terminated. Time: 0.00. 

Optimizer terminated. Time: 0.03    
************************************
A license was checked out correctly.
************************************

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>if mosek == cvxopt (
pip install --upgrade cvxopt   || exit /b 666  
 set GPKITSOLVERS=cvxopt 
) 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>python -c "import scipy; print scipy.__version__"   || exit /b 666 
1.2.1

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>python -c "import numpy; print numpy.__version__"   || exit /b 666 
1.16.3

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>python -c "import pint; print pint.__version__"   || exit /b 666 
0.9

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>REM Install gpkit to run the documentation examples 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>git clone --depth 1 https://github.com/convexengineering/gpkit.git   || exit /b 666 
Cloning into 'gpkit'...
Checking out files:  54% (102/188)   
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Checking out files: 100% (188/188)   
Checking out files: 100% (188/188), done.

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>pip install -e D:\jenkins\workspace\gplibrary_Push_Models\mosek\gpkit   || exit /b 666 
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:///D:/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit
Requirement already satisfied: numpy>=1.13.3 in d:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (1.16.4)
Requirement already satisfied: pint>=0.8.1 in d:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (0.9)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (1.2.2)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in d:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (1.2.3)
Requirement already satisfied: six in d:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit==0.9.1.0) (1.0.2)
Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt>=1.1.8->gpkit==0.9.1.0) (2018.0.0)
Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt>=1.1.8->gpkit==0.9.1.0) (2018.0.0)
Installing collected packages: gpkit
  Running setup.py develop for gpkit
Successfully installed gpkit

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>pip install -e D:\jenkins\workspace\gplibrary_Push_Models\mosek   || exit /b 666 
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:///D:/jenkins/workspace/gplibrary_Push_Models/mosek
Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.9)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint->gpkitmodels==0.0.0.0) (1.0.2)
Installing collected packages: gpkitmodels
  Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>REM Show the settings file 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>REM type D:\jenkins\workspace\gplibrary_Push_Models\mosek\gpkit\env\settings 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>REM dir D:\jenkins\workspace\gplibrary_Push_Models\mosek\build_gpkit 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>REM Limit number of threads that be can used 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>set MSK_IPAR_NUM_THREADS=2 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>set MKL_NUM_THREADS=2 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>set NUMEXPR_NUM_THREADS=2 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>set OPENBLAS_NUM_THREADS=2 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>set OMP_NUM_THREADS=2 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True)"   || exit /b 666 
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.]
...................................................................................................................................................................................................................................................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 C:\Program Files\Mosek\7\tools\platform\win64x86\h\mosek.h
#     Found C:\Program Files\Mosek\7\tools\platform\win64x86\bin\mosek64_7_1.dll
#     Found C:\Program Files\Mosek\7\tools\examples\c\scopt-ext.c
#     Found C:\Program Files\Mosek\7\tools\examples\c\expopt.c
#     Found C:\Program Files\Mosek\7\tools\examples\c\dgopt.c
#     Found C:\Program Files\Mosek\7\tools\examples\c\scopt-ext.h
#     Found C:\Program Files\Mosek\7\tools\examples\c\expopt.h
#     Found C:\Program Files\Mosek\7\tools\examples\c\dgopt.h
#     Found C:\Program Files\Mosek\7\tools\platform\win64x86\h\mosek.h
# Found mosek version 7, installed to C:\Program Files\Mosek
#
# Building mosek...
#     Replacing directory _mosek\lib
#     Replacing directory _mosek\build
#     Replacing directory D:\jenkins\workspace\gplibrary_Push_Models\mosek\build_gpkit
#
#   Copying expopt library files to _mosek\build
#     Copying C:\Program Files\Mosek\7\tools\examples\c\scopt-ext.c
#     Copying C:\Program Files\Mosek\7\tools\examples\c\expopt.c
#     Copying C:\Program Files\Mosek\7\tools\examples\c\dgopt.c
#     Copying C:\Program Files\Mosek\7\tools\examples\c\scopt-ext.h
#     Copying C:\Program Files\Mosek\7\tools\examples\c\expopt.h
#     Copying C:\Program Files\Mosek\7\tools\examples\c\dgopt.h
#     Copying C:\Program Files\Mosek\7\tools\platform\win64x86\h\mosek.h
#
#   Applying expopt patches...
#
#     Change in _mosek\build\dgopt.con line 683
#     --           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 569
#     --       printf("Warning: The variable with index '%d' has only positive 
#     ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in
#
#     Change in _mosek\build\expopt.con line 582
#     --       printf("Warning: The variable with index '%d' has only negative 
#     ++ 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,--export-all-symbols,-R "C:\Program Files\Mosek\7\tools\platform\win64x86\bin"    _mosek\build\scopt-ext.c _mosek\build\expopt.c _mosek\build\dgopt.c   "C:\Program Files\Mosek\7\tools\platform\win64x86\bin\mosek64_7_1.dll" -o D:\jenkins\workspace\gplibrary_Push_Models\mosek\build_gpkit\expopt.so'
##
### CALL BEGINS
### CALL ENDS
##
#
#   Building Python bindings for expopt and Mosek...
#   (if this fails on Windows, verify the mingw version)
#     Calling 'python modified_ctypesgen.py -a -l D:/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit/expopt.so -l "C:/Program Files/Mosek/7/tools/platform/win64x86/bin/mosek64_7_1.dll" -o _mosek\lib\expopt_h.py    _mosek\build\expopt.h'
##
### CALL BEGINS
### CALL ENDS
##
# Done building mosek
# Looking for mosek_cli
#   Trying to run mskexpopt...
#     Calling 'mskexpopt'
##
### CALL BEGINS
### CALL ENDS
##
# Found mosek_cli in system path
# Looking for cvxopt
#   Trying to import cvxopt...
# Found cvxopt in Python path
...finished building gpkit.
Replaced found solvers ([u'mosek', u'mosek_cli', u'cvxopt']) with environment var GPKITSOLVERS (mosek, mosek_cli)

Found the following solvers: mosek, mosek_cli
#     Replacing directory env
x[:] <= w

GPkit is now installed with solver(s) [u'mosek', u'mosek_cli']
To incorporate new solvers at a later date, run `gpkit.build()`.

If any tests didn't pass, please post the output above
(starting from "Found no installed solvers, beginning a build.")
to gpkit@mit.edu or https://github.com/convexengineering/gpkit/issues/new
so we can prevent others from having these errors.

TheCloning into 'gplibrary'...
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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:///D:/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary
Installing collected packages: gpkitmodels
  Found existing installation: gpkitmodels 0.0.0.0
    Uninstalling gpkitmodels-0.0.0.0:
      Successfully uninstalled gpkitmodels-0.0.0.0
  Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels
Cloning into 'shopping'...
adding test for 'test.py'
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.037 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.022 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.116 seconds.

Running tests...
----------------------------------------------------------------------
...
----------------------------------------------------------------------
Ran 3 tests in 0.592s

OK

Generating XML reports...
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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 d:\anaconda2\lib\site-packages (0.24.2)
Requirement already satisfied: numpy>=1.12.0 in d:\anaconda2\lib\site-packages (from pandas) (1.16.4)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas) (2.8.0)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\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 c:\users\jenkins\appdata\local\temp\pip-req-build-saopev
  Running command git clone -q https://github.com/hoburg/gpfit.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-saopev'
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_push_models\mosek\gpkit (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt>=1.1.8->gpkit->gpfit==0.1) (2018.0.0)
Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt>=1.1.8->gpkit->gpfit==0.1) (2018.0.0)
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=25428 sha256=891e58533a561956016cb32a7ff6efd823216cb2e36bfdfda78cc2317def097f
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-ftcgq1\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 d:\jenkins\workspace\gplibrary_push_models\mosek\gassolar
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.2.2)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_push_models\mosek\gpkit (from gassolar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.24.2)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.8.1 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.9)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.2.3)
Requirement already satisfied: six in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.12.0)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.8.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gassolar==0.0.0.0) (1.0.2)
Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt>=1.1.8->gpkit->gassolar==0.0.0.0) (2018.0.0)
Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt>=1.1.8->gpkit->gassolar==0.0.0.0) (2018.0.0)
Building wheels for collected packages: gassolar
  Building wheel for gassolar (setup.py): started
  Building wheel for gassolar (setup.py): still running...
  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=4895585 sha256=947e0eda65c06f5ffb60685f39aafe8aa6d19619823e88ef2c681968ec212896
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-ertjx2\wheels\c8\04\cf\c7930fbaf20d02c2a1bf8e7f1e428ba917da53d01905cc6931
Successfully built gassolar
Installing collected packages: gassolar
Successfully installed gassolar-0.0.0.0
adding test for 'gassolar/gas/gas.py'
adding test for 'gassolar/solar/solar.py'
Using solver 'mosek'
Solving for 592 variables.
Solving took 3.09 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 3.46 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 0.169 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 0.466 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 0.376 seconds.
Warning: Variable Mission.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.3537 but bound is 150000.0000
Warning: Variable Mission.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.3827 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 17.7 seconds.
Warning: Variable Mission1.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103406.0510 but bound is 150000.0000
Using solver 'mosek_cli'
Solving for 1250 variables.
Solving took 2.73 seconds.
Warning: Variable Mission.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.6388 but bound is 150000.0000
Warning: Variable Mission.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.6388 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 2.57 seconds.
Warning: Variable Mission1.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103406.1793 but bound is 150000.0000

Running tests...
----------------------------------------------------------------------
D:\Anaconda2\lib\site-packages\pint\quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped.
  warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning)
..D:\jenkins\workspace\gplibrary_Push_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
..
----------------------------------------------------------------------
Ran 4 tests in 50.485s

OK

Generating XML reports...
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 d:\anaconda2\lib\site-packages (0.24.2)
Requirement already satisfied: numpy>=1.12.0 in d:\anaconda2\lib\site-packages (from pandas) (1.16.4)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas) (2.8.0)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\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 c:\users\jenkins\appdata\local\temp\pip-req-build-pjspnq
  Running command git clone -q https://github.com/hoburg/gpfit.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-pjspnq'
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_push_models\mosek\gpkit (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt>=1.1.8->gpkit->gpfit==0.1) (2018.0.0)
Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt>=1.1.8->gpkit->gpfit==0.1) (2018.0.0)
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=25428 sha256=4e4fd5bc9529bb855875645b312a7667a72b6cbb3c8b929ffad26032be7cb182
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-bkpiqb\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
adding test for 'model/jho.py'
adding test for 'model/print_perf.py'
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.8082800881669137e-13.
Solving took 4 GP solves and 22.2 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.822401e-13.
Solving took 4 GP solves and 5.17 seconds.
Allowing negative dual variable(s) as small as -8.34027812091076e-12.
Allowing negative dual variable(s) as small as -1.2592341449083055e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.626
design loiter speed [m/s] = 25.071
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.2593344336092605e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.356
optimum loiter speed for min power, end of loiter [m/s] = 25.000
optimum cruise speed, inbound [m/s] = 25.637
optimum cruise speed, outbound [m/s] = 36.421
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.259767952301696e-11.
Solving took 4 GP solves and 6.48 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.15 seconds.
Max payload weight [lbf] = 28.242
Max take off weight [lbf] = 166.638
Allowing negative dual variable(s) as small as -8.34142e-12.
Allowing negative dual variable(s) as small as -1.260031e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.626
design loiter speed [m/s] = 25.071
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.257939e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.356
optimum loiter speed for min power, end of loiter [m/s] = 25.000
optimum cruise speed, inbound [m/s] = 25.637
optimum cruise speed, outbound [m/s] = 36.421
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.259772e-11.
Solving took 4 GP solves and 11.5 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 43.1 seconds.
Max payload weight [lbf] = 28.242
Max take off weight [lbf] = 166.638

Running tests...
----------------------------------------------------------------------
D:\Anaconda2\lib\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 130.756s

OK

Generating XML reports...
Cloning into 'turbofan'...
Checking out files:  97% (110/113)   
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Checking out files: 100% (113/113), done.
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 d:\jenkins\workspace\gplibrary_push_models\mosek\turbofan
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.9)
Requirement already satisfied: future in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.17.1)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\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=45480 sha256=35ecbc31588a4f165b7f2a88dabfc0d9306654481e283591a32ff6fadd5ac40f
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-ulf_sc\wheels\fd\eb\c7\cc8c21b792dd5ace3356cb5d7a5004c37932940e290e168145
Successfully built turbofan
Installing collected packages: turbofan
Successfully installed turbofan-0.0.0.0
adding test for 'turbofan/engine_test.py'
Beginning signomial solve.
Using solver 'mosek'
Solving for 327 variables.
Solving took 8.32 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 1.27 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.398 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 1.52 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.662 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.476 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.281 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.082 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.08 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.067 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.072 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.077 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.058 seconds.
Solving took 13 GP solves and 13.9 seconds.

Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 14.479s

OK

Generating XML reports...
Cloning into 'SPaircraft'...
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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 c:\users\jenkins\appdata\local\temp\pip-req-build-njiytl
  Running command git clone -q https://github.com/hoburg/turbofan.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-njiytl'
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.9)
Requirement already satisfied: future in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.17.1)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\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=45480 sha256=0e5a3d8abe69217141e1c563194a88db2cbcd9bd984db5f5dd049ddba54a4ccf
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-dm44ou\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 d:\jenkins\workspace\gplibrary_push_models\mosek\spaircraft
Requirement already satisfied: turbofan in d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages (from SPaircraft==0.0.0) (0.0.0.0)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_push_models\mosek\gpkit (from SPaircraft==0.0.0) (0.9.1.0)
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan->SPaircraft==0.0.0) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan->SPaircraft==0.0.0) (1.2.2)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan->SPaircraft==0.0.0) (0.9)
Requirement already satisfied: future in d:\anaconda2\lib\site-packages (from turbofan->SPaircraft==0.0.0) (0.17.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->SPaircraft==0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in d:\anaconda2\lib\site-packages (from gpkit->SPaircraft==0.0.0) (1.2.3)
Requirement already satisfied: six in d:\anaconda2\lib\site-packages (from gpkit->SPaircraft==0.0.0) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint->turbofan->SPaircraft==0.0.0) (1.0.2)
Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt>=1.1.8->gpkit->SPaircraft==0.0.0) (2018.0.0)
Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt>=1.1.8->gpkit->SPaircraft==0.0.0) (2018.0.0)
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=1857 sha256=2ada454a858d00d23f778bbed9a1b7cab62002bc63e2a225921bb8b4923059a8
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-6zpnrn\wheels\5a\85\02\bbec505cff1eea0765543219a0ea15a5ddec7c9686120c35d7
Successfully built SPaircraft
Installing collected packages: SPaircraft
Successfully installed SPaircraft-0.0.0
adding test for 'SPaircraft.py'
Mission
=======

Cost
----
 W_{f_{total}}[:].sum()

Constraints
-----------
   W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin}
   PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:])
   x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:])
   x_{CG}[3] <= \Delta x_n + x_n
   \Delta x_m + x_{CG}[3] >= x_m
   \tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m
   C_{D_{fuse}}[:] = 0.018081
   M_{fuseD} = 0.72
   W_{start}[0] = W_{total}[:]
   W_{start}[:] >= W_{end}[:] + W_{burn}[:]
   W_{start}[1:] = W_{end}[:4]
   W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1]
   W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2]
   W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1]
   hft[2] >= CruiseAlt
   hft[1:5] = hft[:4] + dhft[1:5]
   hft[0] = dhft[0]
   dhft[1:3] = dhft[:2]
   RC[0] >= 2.5e+03
   RC[:3] >= RC_{min}[:3]
   \theta[2] >= 0.015
   hft[2] >= MinCruiseAlt
   n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:]
   R_{segment}[3:4] = R_{segment}[4:5]
   M[3:5] >= M_{min}
   0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req}
   Fsafetyfac*F[0] = T_e
   W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:]
   V_2[:] = M_2[:]*a[:]
   \alpha_{max,w}[:3] = 0.18
   \alpha_{max,w}[3:] = 0.1
   0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime
   0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime
   ClimbTime <= MaxClimbTime
   T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}}
   F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   OPR[:] <= OPR_{max}
 
 Aircraft
     Fuselage
       W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on}
       W_{pass}[:] >= n_{pass}[:]*W_{avg. pass}
       W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo}
       W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}}
       W_{payload}[:] <= W_{payload_{max}}
       n_{pass}[:] <= n_{seat}
       n_{rows} = n_{seat}/SPR
       l_{shell} = n_{rows}*p_s
       \theta_{db} = w_{db}/R_{fuse}
       R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db}
       A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db}
       (PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse}
       A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin}
       w_{floor} = w_{fuse}
       R_{fuse} + w_{db} >= w_{fuse}
       h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse}
       t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell}
       S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2
       S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2
       l_{fuse} = l_{nose} + l_{shell} + l_{cone}
       l_{cone} = R_{fuse}/\lambda_{cone}
       x_{shell1} = l_{nose}
       x_{shell2} >= l_{nose} + l_{shell}
       t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin}
       t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin}
       \sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell})
       \sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin}
       l_{floor} >= l_{shell} + 2*R_{fuse}
       P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat})
       A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor}
       V_{floor} = 2*w_{floor}*A_{floor}
       W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor}
       \tau_{cone} = \sigma_{skin}
       W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame})
       x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone}
       -2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}}
       (PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}}
       x_{hbend_{Land}} >= x_{wing}
       x_{hbend_{Land}} <= l_{fuse}
       x_{hbend_{MLF}} >= x_{wing}
       x_{hbend_{MLF}} <= l_{fuse}
       A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}})
       A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}})
       A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
       A_{2h_{MLF}} >= Mission.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
       A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2)
       A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}}
       A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}}
       A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}}
       A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}}
       A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}}
       A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}}
       A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}}
       A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}}
       V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission.Aircraft.Fuselage.r_{w/c}
       V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission.Aircraft.Fuselage.r_{w/c}
       V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}}
       W_{hbend} >= g*\rho_{bend}*V_{hbend}
       x_{vbend} >= x_{wing}
       x_{vbend} <= l_{fuse}
       B_{0v} = B_{1v}*(x_{tail} - x_{vbend})
       B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2)
       B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}}
       0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}}
       V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission.Aircraft.Fuselage.r_{w/c}
       V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}}
       W_{vbend} >= \rho_{bend}*g*V_{vbend}
       x_f = x_{wing} + 0.5*c_0*Mission.Aircraft.Fuselage.r_{w/c}
       x_b = x_{wing} - 0.5*c_0*Mission.Aircraft.Fuselage.r_{w/c}
       \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h}
       \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v}
       V_{cyl} = A_{skin}*l_{shell}
       V_{nose} = S_{nose}*t_{skin}
       V_{bulk} = S_{bulk}*t_{skin}
       V_{db} = A_{db}*l_{shell}
       V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse})
       W_{apu} = W_{payload_{max}}*f_{apu}
       W_{db} = \rho_{skin}*g*V_{db}
       W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk})
       W_{window} >= W'_{window}*l_{shell}
       W_{padd} = W_{payload_{max}}*f_{padd}
       W_{seat} >= W'_{seat}*n_{seat}
       W_{seat} >= f_{seat}*W_{payload_{max}}
       W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk})
       W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db}
       W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone})
     
     Wing
       WingNoStruct
         A_{rect} = c_{tip}*b
         0.5*(1 - \lambda)*c_{root}*b <= A_{tri}
         p >= 1 + 2*\lambda
         2*q >= 1 + p
         y_{mac} = b/3*q/p
         mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q
         \lambda = c_{tip}/c_{root}
         S = b*(c_{root} + c_{tip})/2
         0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w)
         e*(1 + f(\lambda_w)*AR) <= 1
         \lambda >= 0.15
         V_{fuel, max} <= 0.303*mac^2*b*\tau
         W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g
         b <= b_{max}
       
       WingBox
         AR = b^2/S
         0.423*Mission.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5)
         \tau <= \tau_{max_w}
         W_{struct} >= W_{web} + W_{cap}
         AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= 8*\rho_{cap}*g*Mission.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5)
         Mission.Aircraft.Wing.WingBox.N_{lift} = 3
         Mission.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8
         \lambda = taper
         W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt})
         0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}}
     
     Engine
         Compressor
           (no constraints)
         
         Combustor
           (no constraints)
         
         Turbine
           (no constraints)
         
         Thrust
           (no constraints)
         
         FanMap
           (no constraints)
         
         LPCMap
           (no constraints)
         
         HPCMap
           (no constraints)
         
         Sizing
           A_{2} >= A_{5} + A_{7}
         
         FlightState
             V[:] = V[:]
             a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
             V[:] = M[:]*a[:]
           
           Altitude
             h[:] = hft[:]
           
           Atmosphere
             (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
             \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
             T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
             \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
         
         EnginePerformance
           CompressorPerformance
               T_{t_0}[:] = T_{atm}[:]/c1[:]^-1
               h_{t_0}[:] = C_{p_{air}*T_{t_0}[:]
               P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:]
               T_{t_{1.8}}[:] = T_{t_0}[:]
               h_{t_{1.8}}[:] = h_{t_0}[:]
               P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5
               T_{T_{2}}[:] = T_{t_{1.8}}[:]
               h_{T_{2}}[:] = h_{t_{1.8}}[:]
               P_{T_{2}}[:] = P_{t_{1.8}}[:]
               P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:]
               T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016
               h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:]
               P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:]
               T_{t_7}[:] = T_{t_{2.1}}[:]
               h_{t_7}[:] = h_{t_{2.1}}[:]
               P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:]
               T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152
               h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1}
               P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:]
               T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491
               h_{t_3}[:] = C_{p_{2}*T_{t_3}[:]
           
           CombustorPerformance
             h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:]
             h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:]
             fp1[:] = f[:] + 1
             M_{4a}[:] = 0.1025
             fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5
             T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]]
             P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891
             u_{4a}[:] = M_{4a}[:]*(1.31*Mission.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a}
             u_c[:] = r_{uc}*u_{4a}[:]
             P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891
           
           TurbinePerformance
             h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:]
             P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:]
             \pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565
             h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:]
             P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:]
             T_{t_5}[:] = T_{t_{4.9}}[:]
             h_{t_5}[:] = h_{t_{4.9}}[:]
           
           ThrustPerformance
             P_{8}[:] = P_{atm}[:]
             h_{8}[:] = C_{p_{fex}*T_{8}[:]
             u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:]
             (P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:]
             h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:]
             P_{6}[:] = P_{atm}[:]
             (P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:]
             u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:]
             h_6[:] = C_{p_{tex}*T_{6}[:]
             h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:]
             \alpha[:] = m_{fan}[:]/m_{core}[:]
             \alpha_{+1}[:] = \alpha[:] + 1
             \alpha[:] <= \alpha_{max}
             F[:] <= F_{6}[:] + F_{8}[:]
             F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:])
             TSFC[:] = 1/I_{sp}[:]
             F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:]
           
           FanMapPerformance
             m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}}
           
           LPCMapPerformance
             m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D}
           
           HPCMapPerformance
             m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D}
           
           SizingPerformance
             P_{7}[:] >= P_{atm}[:]
             M_7[:] <= 1
             a_{7}[:] = (1.4*Mission.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5
             a_{7}[:]*M_7[:] = u_{7}[:]
             \rho_7[:] = P_{7}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{7}[:])
             P_{5}[:] >= P_{atm}[:]
             M_5[:] <= 1
             a_{5}[:] = (1.39*Mission.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5
             a_{5}[:]*M_5[:] = u_{5}[:]
             \rho_5[:] = P_{5}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{5}[:])
             h_{2}[:] = C_{p_{1}*T_{2}[:]
             \rho_{2}[:] = P_{2}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{2}[:])
             u_{2}[:] = M_2[:]*(C_{p_{1}*Mission.Aircraft.Engine.EngineConstants.R*T_{2}[:]/781)^0.5
             h_{2.5}[:] = C_{p_{2}*T_{2.5}[:]
             \rho_{2.5}[:] = P_{2.5}[:]/(Mission.Aircraft.Engine.EngineConstants.R*T_{2.5}[:])
             u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/781)^0.5
         m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine}
           d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5
           d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5
           \eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]])
           h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:]
           P_{t_4}[:] = \pi_{b}*P_{t_3}[:]
           M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]]
           M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]])
           P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:]
           \pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013
           \pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10
           \pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10
           \pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10
           m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
           \pi_{f}[:] >= 1
           \pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10
           \pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10
           \pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10
           \pi_{lc}[:] >= 1
           m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
           \pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10
           \pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10
           \pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10
           m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref})
           \pi_{hc}[:] >= 1
         OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:]
           P_{t_8}[:] = P_{t_7}[:]
           T_{t_8}[:] = T_{t_7}[:]
           P_{t_6}[:] = P_{t_5}[:]
           T_{t_6}[:] = T_{t_5}[:]
           F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:]
           I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g)
           N_{f}[:]*G_{f} = N_{1}[:]
           N_{1}[:] <= 1.1
           N_{2}[:] <= 1.1
         fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD}
         fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD}
           P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5
           (T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2
           P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979
           (T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2
           M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:]
           m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:]
           m_{total}[:] = m_{fan}[:] + m_{core}[:]
           P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512
           T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1
           m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2}
           P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857
           T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1
           m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5}
           1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD}
           0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD}
           1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD}
           0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD}
           m_{lc_D} >= 0.7*m_{coreD}/0.649
           m_{lc_D} <= 1.3*m_{coreD}/0.649
           m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23
           m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23
           \bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405
           \bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405
           F[:] = F_{spec}[:]
           T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}}
           OPR[:] <= OPR_{max}
     
     VerticalTail
       VerticalTailNoStruct
         C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}}
         L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}}
         c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt}))
         A_{vt} = b_{vt}^2/S_{vt}
         b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt}
         p_{vt} >= 1 + 2*\lambda_{vt}
         2*q_{vt} >= 1 + p_{vt}
         y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
         z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
         0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt}
         \lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}}
         \Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}}
         \Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt}
         \lambda_{vt} >= 0.25
         V_{vt} >= V_{vt_{min}}
       
       WingBox
         AR_{vt} = (2*b_{vt})^2/(2*S_{vt})
         0.423*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
         \tau_{vt} <= 0.14
         W_{struct} >= 0.5*(W_{web} + W_{cap})
         Mission.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24
         AR_{vt}*2*L_{vt_{max}}*Mission.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= 8*\rho_{cap}*g*Mission.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
         Mission.Aircraft.VerticalTail.WingBox.N_{lift} = 1
         Mission.Aircraft.VerticalTail.WingBox.N_{lift}*Mission.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8
         \lambda_{vt} = taper
         W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT})
     
     HorizontalTail
       HorizontalTailNoStruct
         \Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht}
         \Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}}
         p_{ht} >= 1 + 2*\lambda_{ht}
         2*q_{ht} >= 1 + p_{ht}
         y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht}
         0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht}
         \lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}}
         S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2
         0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht})
         e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1
         AR_{ht} = b_{ht}^2/S_{ht}
         \lambda_{ht} >= 0.2
         \lambda_{ht} <= 1
       
       WingBox
         AR_{ht} = b_{ht}^2/S_{ht}
         0.423*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
         \tau_{ht} <= 0.14
         W_{struct} >= W_{web} + W_{cap}
         L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2
         L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht})
         2*AR_{ht}*L_{shear}*Mission.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
         Mission.Aircraft.HorizontalTail.WingBox.N_{lift} = 1
         Mission.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8
         L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht}
         L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}}
         W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht})
     
     LandingGear
       l_n + z_{wing} + y_m*\tan(\gamma) >= l_m
       T = 2*y_m
       x_m >= x_n + B
       x_n >= 5
       \tan(\phi) = \tan(\phi_{min})
       (z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1
       \tan(\psi) <= \tan(\psi_{max})
       x_{up} - x_m <= l_m/\tan(\theta_{max})
       y_m >= l_m
       S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG})
       l_{oleo} = 2.5*S_{sa}
       d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5
       l_m >= l_{oleo} + d_{t_m}/2
       F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in])
       W_{wa,m} = 1.2*F_{w_m}^0.609
       F_{w_n} = L_{w_n}*d_{t_n}/1e+03
       W_{wa,n} = 1.2*F_{w_n}^0.609
       L_{w_m} = L_m/(n_{mg}*n_{wps})
       L_{w_n} = L_n/n_{wps}
       d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315
       w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48
       d_{t_n} = 0.8*d_{t_m}
       w_{t_n} = 0.8*w_{t_m}
       W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g
       N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m
       W_{mw} = n_{wps}*W_{wa,m}
       W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g
       \sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}})
       W_{nw} >= n_{wps}*W_{wa,n}
       L_m <= 9.87*E*I_m/(K*l_m)^2
       I_m = PI*r_m^3*t_m
       L_n <= 9.87*E*I_n/(K*l_n)^2
       I_n = PI*r_n^3*t_n
       2*r_m/t_m <= 40
       2*r_m/t_n <= 40
       h_{hold} >= 2*w_{t_m} + 2*r_m
       0.8 >= 2*w_{t_n} + 2*r_n
       W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m}))
       W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n})
       W_{lg} >= C_{lg}*(W_{mg} + W_{ng})
       W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m
       x_m >= x_{CG_{lg}}
     c_{root} = c_0
     Mission.Aircraft.Wing.WingBox.r_{w/c} = Mission.Aircraft.Fuselage.r_{w/c}
     x_w = x_{wing}
     Mission.Aircraft.Fuselage.N_{lift} = Mission.Aircraft.Wing.WingBox.N_{lift}
     f_{L_{total/wing}}*L_{max} >= Mission.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}}
     W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc}
     W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
     W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
     W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:]
     W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:]
     W_{total}[:] <= W_{total, max}
     f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}}
     W_{misc} >= W_{lg} + W_{hpesys}
     W_{hpesys} = f_{hpesys}*W_{total, max}
     x_n <= l_{nose}
     x_m >= x_{wing}
     \Delta x_{AC_{wing}} + x_{wing} >= x_m
     x_{hpesys} = 1.1*l_{nose}
     x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys}
     d_{nacelle} >= d_{f} + 2*t_{nacelle}
     E_{land} >= W_{total, max}/(2*g)*w_{ult}^2
     x_{up} = x_{shell2}
     L_n = W_{total, max}*\Delta x_m/B
     L_m = W_{total, max}*\Delta x_n/B
     L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max}
     y_{eng} >= y_m
     3*n_{vt}*Mission.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}}
     V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse}
     W_{tail} >= n_{vt}*W_{vt} + W_{ht}
     2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db}
     B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v})
     m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht}
     x_{CG_{ht}} <= l_{fuse}
     V_{ht} = S_{ht}*l_{ht}/(S*mac)
     L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}}
     L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}}
     x_{CG_{vt}} <= l_{fuse}
     V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b)
     n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max}
     n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng}
     D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}}
     I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:]
     I_{z}[:] <= I_{z, max}
     S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2
     l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}}
     f_{S_{nacelle}} = S_{nacelle}*S^-1
     A_{inlet} = 0.4*S_{nacelle}
     A_{fancowl} = 0.2*S_{nacelle}
     A_{exh} = 0.4*S_{nacelle}
     A_{corecowl} = 3PI*d_{LPC}^2
       W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl})
       W_{eadd} = f_{eadd}*W_{engine}
     W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon}
     W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine})
     y_{eng} = 0.5*w_{fuse}
     (L_{max} - Mission.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission.Aircraft.Wing.WingBox.M_r*c_{root}
     A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend})
     A_{1h_{MLF}} >= (Mission.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h})
     I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16)
     I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81
     I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81)
     x_{shell2} + l_{cone} >= x_{eng}
     x_{eng} >= x_{shell2} + 0.75*l_{cone}
     S_{floor} = 0.312*P_{floor}
     M_{floor} = 0.0352*P_{floor}*w_{floor}
     \Delta R_{fuse} = R_{fuse}*0.43/1.75
     b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2
     b_{ht_{out}} = 0.5*b_{ht} - w_{fuse}
     L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}}
     M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}}
     L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}}
     c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach}
     \pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht})
 
 FlightSegment
   FlightState
       V[:] = V[:]
       a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
       V[:] = M[:]*a[:]
     
     Altitude
       h[:] = hft[:]
     
     Atmosphere
       (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
       \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
       T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
       \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
   
   FlightP
     P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:]
     RC[:] = P_{excess}[:]/W_{avg}[:]
     \theta[:]*V[:] = RC[:]
     dhft[:] = tmin[:]*RC[:]
     R_{segment}[:] = thr[:]*V[:]
       WingPerformance
         0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:]
         \Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:]
         \Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2
         (AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2
         C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:]
         \alpha_w[:] <= \alpha_{max,w}[:]
         D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:]
         C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:]
         C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR)
         Re_w[:] = \rho[:]*V[:]*mac/\mu[:]
         C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114
       
       FuselagePerformance
         (no constraints)
       
       VerticalTailPerformance
         D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:]
         Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:]
         C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577
       
       HorizontalTailPerformance
         L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:]
         C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:]
         \alpha_{ht}[:] <= \alpha_{ht,max}
         C_{L_{\alpha,ht_0}}[:] = 6.28
         D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:]
         C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht})
         Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:]
         C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852
       W_{burn}[:] = W_{burn}[:]
       F_{fuel}[:] = F_{fuel}[:]
       \rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:])
       P_{cabin}[:] = 7.5e+04
       T_{cabin}[:] = 297
       V[:] >= V_{stall}[:]
       W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:]
       tmin[:] = thr[:]
       L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:]
       L_{total}[:] = f_{L_{total/wing}}*L_w[:]
       L_{total}[:] >= W_{avg}[:] + L_{ht}[:]
       D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2
       D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:])
       C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S)
       L/D[:] = W_{avg}[:]/D[:]
       W_{Load}[:] <= W_{Load_{max}}[:]
       W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S
       p_{o}[:] >= L_w[:]*c_{root}/S
       \eta_{o}[:] = w_{fuse}/(b/2)
       x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:]
       c_{m_{w}}[:] = 1.9
       x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2)
       x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse}
       x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}}
       x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}}
       C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht}
       AR_{ht} >= 4
       C_{L_{ht}}[:] >= 0.01
       SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac
       SM[:] >= SM_{min}
       SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}}
       x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:]
       R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:]
       C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2
       V_{nacelle}[:] = r_{v_{nacelle}}*V[:]
       V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]]
       r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0)
       C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0
       D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S
       \Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}}
   M_2[:3] = M[:3]
   M_{2.5}[:3] = 0.6
   hold_{2}[:3] = 1.07164
   hold_{2.5}[:3] = 1.06372
   P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:]
   c1[:] = 1 + 0.201*M[:]^2.0
   M_2[3:] = M[3:]
   M_{2.5}[3:] = 0.6
   hold_{2}[3:] = 1.07164
   hold_{2.5}[3:] = 1.06372
Beginning signomial solve.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 937
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 937             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 768
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3438              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.08              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.46e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.285824792e+005 2.000000000e+000  1.0e+000 0.11  
1   1.1e+003 1.5e+003 6.3e+004 -9.71e-001 -1.265132514e+005 3.611589420e+000  4.9e-001 0.97  
2   4.1e+002 5.4e+002 2.3e+004 -9.38e-001 -1.199666169e+005 1.064041138e+001  1.8e-001 1.01  
3   2.9e+002 3.7e+002 1.6e+004 -8.34e-001 -1.156309126e+005 6.812702963e+001  1.3e-001 1.03  
4   2.8e+002 3.7e+002 1.6e+004 -7.60e-001 -1.131522901e+005 2.113211995e+003  1.3e-001 1.08  
5   8.8e+001 1.2e+002 5.0e+003 -7.53e-001 -8.096538237e+004 8.430204037e+003  3.9e-002 1.15  
6   3.7e+001 4.8e+001 2.1e+003 -2.92e-001 -4.806295568e+004 1.015705753e+004  1.6e-002 1.17  
7   2.1e+001 2.8e+001 1.2e+003 2.53e-001  -3.183959973e+004 7.147574260e+003  9.5e-003 1.19  
8   9.4e+000 1.2e+001 5.3e+002 5.37e-001  -1.516213576e+004 4.167067597e+003  4.2e-003 1.22  
9   5.5e+000 7.2e+000 3.1e+002 8.14e-001  -8.873654488e+003 2.833843752e+003  2.5e-003 1.23  
10  1.3e+000 1.8e+000 7.7e+001 9.07e-001  -2.032976954e+003 9.282385087e+002  6.1e-004 1.26  
11  7.0e-001 9.2e-001 4.0e+001 9.94e-001  -8.350002142e+002 7.206024908e+002  3.2e-004 1.28  
12  4.7e-001 6.2e-001 2.7e+001 9.97e-001  -4.846306076e+002 5.632460213e+002  2.1e-004 1.31  
13  3.5e-001 7.3e-001 2.0e+001 9.79e-001  -3.148957258e+002 4.857769751e+002  1.6e-004 1.33  
14  1.7e-001 3.5e-001 9.8e+000 9.96e-001  -1.857417116e+001 3.656902710e+002  7.9e-005 1.36  
15  5.5e-002 1.5e-001 3.3e+000 9.94e-001  1.620485362e+002  2.901550655e+002  2.6e-005 1.39  
16  3.2e-002 1.3e-001 1.9e+000 1.00e+000  1.996394651e+002  2.746181590e+002  1.6e-005 1.40  
17  5.1e-003 1.8e-001 3.3e-001 1.00e+000  2.444824012e+002  2.572405213e+002  2.8e-006 1.44  
18  1.5e-003 1.3e-001 9.6e-002 1.00e+000  2.509288752e+002  2.546905409e+002  8.3e-007 1.45  
19  4.8e-004 1.1e-001 3.2e-002 1.00e+000  2.527800442e+002  2.540213968e+002  2.8e-007 1.48  
20  2.1e-004 8.6e-002 1.4e-002 1.00e+000  2.532857302e+002  2.538354980e+002  1.2e-007 1.81  
21  1.9e-004 7.8e-002 1.3e-002 1.00e+000  2.533271035e+002  2.538219096e+002  1.1e-007 1.84  
22  1.7e-004 7.1e-002 1.1e-002 1.00e+000  2.533631908e+002  2.538084914e+002  1.0e-007 1.87  
23  1.5e-004 6.4e-002 1.0e-002 1.00e+000  2.533957124e+002  2.537964664e+002  9.0e-008 1.90  
24  1.4e-004 5.9e-002 9.3e-003 1.00e+000  2.534249555e+002  2.537856200e+002  8.1e-008 1.93  
25  1.2e-004 5.4e-002 8.3e-003 1.00e+000  2.534512557e+002  2.537758421e+002  7.3e-008 1.97  
26  1.1e-004 4.9e-002 7.5e-003 1.00e+000  2.534749084e+002  2.537670264e+002  6.6e-008 2.00  
27  1.0e-004 4.5e-002 6.8e-003 1.00e+000  2.534961824e+002  2.537590805e+002  5.9e-008 2.03  
28  9.1e-005 4.1e-002 6.1e-003 1.00e+000  2.535153179e+002  2.537519196e+002  5.3e-008 2.06  
29  8.2e-005 3.8e-002 5.5e-003 1.00e+000  2.535325308e+002  2.537454669e+002  4.8e-008 2.09  
30  7.3e-005 3.5e-002 4.9e-003 1.00e+000  2.535480148e+002  2.537396530e+002  4.3e-008 2.12  
31  6.6e-005 3.2e-002 4.4e-003 1.00e+000  2.535619442e+002  2.537344150e+002  3.9e-008 2.15  
32  5.9e-005 2.9e-002 4.0e-003 1.00e+000  2.535744754e+002  2.537296963e+002  3.5e-008 2.18  
33  5.3e-005 2.7e-002 3.6e-003 1.00e+000  2.535857490e+002  2.537254456e+002  3.1e-008 2.20  
34  4.8e-005 2.5e-002 3.2e-003 1.00e+000  2.535958915e+002  2.537216167e+002  2.8e-008 2.23  
35  4.3e-005 2.4e-002 2.9e-003 1.00e+000  2.536050166e+002  2.537181679e+002  2.5e-008 2.26  
36  3.9e-005 2.2e-002 2.6e-003 1.00e+000  2.536132264e+002  2.537150615e+002  2.3e-008 2.29  
37  3.5e-005 2.0e-002 2.4e-003 1.00e+000  2.536206130e+002  2.537122637e+002  2.1e-008 2.32  
38  3.2e-005 1.9e-002 2.1e-003 1.00e+000  2.536272589e+002  2.537097440e+002  1.9e-008 2.36  
39  2.8e-005 1.8e-002 1.9e-003 1.00e+000  2.536332386e+002  2.537074747e+002  1.7e-008 2.39  
40  2.6e-005 1.7e-002 1.7e-003 1.00e+000  2.536386189e+002  2.537054310e+002  1.5e-008 2.42  
41  2.3e-005 1.6e-002 1.5e-003 1.00e+000  2.536434601e+002  2.537035907e+002  1.4e-008 2.45  
42  2.1e-005 1.5e-002 1.4e-003 1.00e+000  2.536478161e+002  2.537019335e+002  1.2e-008 2.48  
43  1.9e-005 1.4e-002 1.3e-003 1.00e+000  2.536517357e+002  2.537004413e+002  1.1e-008 2.53  
44  1.7e-005 1.4e-002 1.1e-003 1.00e+000  2.536552627e+002  2.536990976e+002  9.8e-009 2.56  
45  1.5e-005 1.3e-002 1.0e-003 1.00e+000  2.536584365e+002  2.536978878e+002  8.9e-009 3.73  
46  1.4e-005 1.3e-002 9.1e-004 1.00e+000  2.536612924e+002  2.536967986e+002  8.0e-009 3.74  
47  1.2e-005 1.2e-002 8.2e-004 1.00e+000  2.536638623e+002  2.536958179e+002  7.2e-009 3.77  
48  1.1e-005 1.2e-002 7.4e-004 1.00e+000  2.536661750e+002  2.536949350e+002  6.5e-009 3.79  
49  9.9e-006 1.1e-002 6.7e-004 1.00e+000  2.536682562e+002  2.536941402e+002  5.8e-009 3.81  
50  8.9e-006 1.1e-002 6.0e-004 1.00e+000  2.536701290e+002  2.536934247e+002  5.2e-009 3.84  
51  8.0e-006 1.0e-002 5.4e-004 1.00e+000  2.536718144e+002  2.536927806e+002  4.7e-009 3.85  
52  7.2e-006 1.0e-002 4.9e-004 1.00e+000  2.536733312e+002  2.536922007e+002  4.2e-009 3.88  
53  6.5e-006 9.9e-003 4.4e-004 1.00e+000  2.536746961e+002  2.536916788e+002  3.8e-009 3.90  
54  5.9e-006 9.6e-003 3.9e-004 1.00e+000  2.536759245e+002  2.536912089e+002  3.4e-009 3.92  
55  5.3e-006 9.4e-003 3.5e-004 1.00e+000  2.536770300e+002  2.536907860e+002  3.1e-009 3.95  
56  4.7e-006 9.2e-003 3.2e-004 1.00e+000  2.536780248e+002  2.536904052e+002  2.8e-009 3.99  
57  4.3e-006 9.0e-003 2.9e-004 1.00e+000  2.536789201e+002  2.536900625e+002  2.5e-009 4.01  
58  3.8e-006 8.9e-003 2.6e-004 1.00e+000  2.536797258e+002  2.536897540e+002  2.3e-009 4.03  
59  3.5e-006 8.7e-003 2.3e-004 1.00e+000  2.536804509e+002  2.536894763e+002  2.0e-009 4.06  
60  3.1e-006 8.6e-003 2.1e-004 1.00e+000  2.536811034e+002  2.536892263e+002  1.8e-009 4.07  
61  1.2e-006 3.3e-003 8.1e-005 1.00e+000  2.536846840e+002  2.536878533e+002  7.1e-010 4.10  
62  1.1e-006 3.0e-003 7.3e-005 1.00e+000  2.536849136e+002  2.536877661e+002  6.4e-010 4.12  
63  1.1e-006 3.0e-003 7.2e-005 1.00e+000  2.536849536e+002  2.536877507e+002  6.3e-010 4.15  
64  9.7e-007 2.7e-003 6.5e-005 1.00e+000  2.536851456e+002  2.536876770e+002  5.7e-010 4.17  
65  9.5e-007 2.7e-003 6.4e-005 1.00e+000  2.536851810e+002  2.536876634e+002  5.6e-010 4.18  
66  8.5e-007 2.4e-003 5.7e-005 1.00e+000  2.536853604e+002  2.536875946e+002  5.0e-010 4.21  
67  8.4e-007 2.4e-003 5.6e-005 1.00e+000  2.536853917e+002  2.536875826e+002  4.9e-010 4.23  
68  1.7e-007 4.9e-004 1.2e-005 1.00e+000  2.536866463e+002  2.536871009e+002  1.0e-010 4.26  
69  1.6e-007 4.5e-004 1.1e-005 1.00e+000  2.536866776e+002  2.536870891e+002  9.2e-011 4.27  
70  1.6e-007 4.5e-004 1.1e-005 1.00e+000  2.536866787e+002  2.536870887e+002  9.2e-011 4.31  
71  1.4e-007 4.1e-004 9.7e-006 1.00e+000  2.536867028e+002  2.536870794e+002  8.5e-011 4.32  
72  1.3e-007 3.7e-004 8.7e-006 1.00e+000  2.536867300e+002  2.536870689e+002  7.6e-011 4.34  
73  1.2e-007 3.3e-004 7.9e-006 1.00e+000  2.536867533e+002  2.536870600e+002  6.9e-011 4.37  
74  1.1e-007 3.0e-004 7.1e-006 1.00e+000  2.536867754e+002  2.536870514e+002  6.2e-011 4.38  
75  1.0e-007 3.0e-004 7.1e-006 1.00e+000  2.536867762e+002  2.536870511e+002  6.2e-011 4.42  
76  9.4e-008 2.7e-004 6.4e-006 1.00e+000  2.536867960e+002  2.536870435e+002  5.6e-011 4.43  
77  8.5e-008 2.4e-004 5.7e-006 1.00e+000  2.536868139e+002  2.536870366e+002  5.0e-011 4.46  
78  8.5e-008 2.4e-004 5.7e-006 1.00e+000  2.536868145e+002  2.536870364e+002  5.0e-011 4.48  
79  7.7e-008 2.2e-004 5.2e-006 1.00e+000  2.536868297e+002  2.536870305e+002  4.5e-011 4.51  
80  7.2e-008 2.1e-004 4.8e-006 1.00e+000  2.536868393e+002  2.536870268e+002  4.2e-011 4.52  
81  7.2e-008 2.1e-004 4.8e-006 1.00e+000  2.536868394e+002  2.536870268e+002  4.2e-011 4.55  
82  6.4e-008 1.8e-004 4.3e-006 1.00e+000  2.536868529e+002  2.536870216e+002  3.8e-011 4.57  
83  5.8e-008 1.7e-004 3.9e-006 1.00e+000  2.536868651e+002  2.536870169e+002  3.4e-011 4.59  
84  5.8e-008 1.7e-004 3.9e-006 1.00e+000  2.536868655e+002  2.536870168e+002  3.4e-011 4.62  
85  5.8e-008 1.7e-004 3.9e-006 1.00e+000  2.536868655e+002  2.536870167e+002  3.4e-011 4.63  
86  5.2e-008 1.5e-004 3.5e-006 1.00e+000  2.536868759e+002  2.536870128e+002  3.1e-011 4.66  
87  5.2e-008 1.5e-004 3.5e-006 1.00e+000  2.536868759e+002  2.536870127e+002  3.1e-011 4.68  
88  4.7e-008 1.3e-004 3.2e-006 1.00e+000  2.536868858e+002  2.536870089e+002  2.8e-011 4.71  
89  4.7e-008 1.3e-004 3.2e-006 1.00e+000  2.536868861e+002  2.536870088e+002  2.8e-011 4.73  
90  4.3e-008 1.2e-004 2.9e-006 1.00e+000  2.536868941e+002  2.536870057e+002  2.5e-011 4.76  
91  4.3e-008 1.2e-004 2.9e-006 9.99e-001  2.536868941e+002  2.536870057e+002  2.5e-011 4.77  
92  3.8e-008 1.1e-004 2.6e-006 1.00e+000  2.536869022e+002  2.536870026e+002  2.3e-011 4.80  
93  3.5e-008 1.0e-004 2.4e-006 1.00e+000  2.536869081e+002  2.536870003e+002  2.1e-011 4.82  
94  3.2e-008 9.1e-005 2.1e-006 1.00e+000  2.536869144e+002  2.536869979e+002  1.9e-011 4.84  
95  3.2e-008 9.1e-005 2.1e-006 1.00e+000  2.536869144e+002  2.536869979e+002  1.9e-011 4.87  
96  2.9e-008 8.2e-005 1.9e-006 1.00e+000  2.536869204e+002  2.536869956e+002  1.7e-011 4.90  
97  2.6e-008 7.4e-005 1.7e-006 1.00e+000  2.536869256e+002  2.536869936e+002  1.5e-011 4.91  
98  2.3e-008 6.7e-005 1.6e-006 1.00e+000  2.536869302e+002  2.536869918e+002  1.4e-011 4.95  
99  2.2e-008 6.2e-005 1.5e-006 9.98e-001  2.536869339e+002  2.536869904e+002  1.3e-011 4.96  
100 2.2e-008 6.2e-005 1.5e-006 1.00e+000  2.536869339e+002  2.536869904e+002  1.3e-011 4.99  
101 1.9e-008 5.6e-005 1.3e-006 9.99e-001  2.536869379e+002  2.536869888e+002  1.1e-011 5.01  
102 1.7e-008 5.0e-005 1.2e-006 1.00e+000  2.536869416e+002  2.536869874e+002  1.0e-011 5.02  
103 1.6e-008 4.5e-005 1.1e-006 1.00e+000  2.536869449e+002  2.536869861e+002  9.3e-012 5.05  
104 1.6e-008 4.5e-005 1.1e-006 9.98e-001  2.536869449e+002  2.536869861e+002  9.3e-012 5.07  
105 1.6e-008 4.5e-005 1.1e-006 9.99e-001  2.536869450e+002  2.536869861e+002  9.2e-012 5.10  
106 1.6e-008 4.5e-005 1.1e-006 9.98e-001  2.536869450e+002  2.536869861e+002  9.2e-012 5.13  
107 1.4e-008 4.1e-005 9.6e-007 1.00e+000  2.536869478e+002  2.536869850e+002  8.3e-012 5.16  
108 1.3e-008 3.7e-005 8.6e-007 9.98e-001  2.536869505e+002  2.536869840e+002  7.5e-012 5.18  
109 1.2e-008 3.4e-005 7.9e-007 1.00e+000  2.536869525e+002  2.536869832e+002  6.9e-012 5.21  
110 1.2e-008 3.4e-005 7.9e-007 1.00e+000  2.536869525e+002  2.536869832e+002  6.9e-012 5.23  
111 1.2e-008 3.4e-005 7.9e-007 1.00e+000  2.536869525e+002  2.536869832e+002  6.9e-012 5.26  
112 1.1e-008 3.0e-005 7.1e-007 9.98e-001  2.536869546e+002  2.536869824e+002  6.2e-012 5.27  
113 9.6e-009 2.8e-005 6.5e-007 1.00e+000  2.536869565e+002  2.536869817e+002  5.6e-012 5.29  
Interior-point optimizer terminated. Time: 5.30. 

Optimizer terminated. Time: 5.32    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 2.5368695650e+002   Viol.  con: 2e-007   var: 0e+000 
  Dual.    obj: 2.5368698165e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 5.35 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 936             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 769
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3440              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.06              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.05            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.46e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.286636032e+005 2.000000000e+000  1.0e+000 0.09  
1   1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.264180260e+005 3.781070854e+000  4.7e-001 0.12  
2   4.6e+002 6.0e+002 2.6e+004 -9.35e-001 -1.210471961e+005 9.871250668e+000  2.0e-001 0.14  
3   2.9e+002 3.8e+002 1.6e+004 -8.50e-001 -1.158624976e+005 5.253701881e+001  1.3e-001 0.17  
4   2.9e+002 3.8e+002 1.6e+004 -7.62e-001 -1.137381539e+005 1.863811988e+003  1.3e-001 0.20  
5   8.3e+001 1.1e+002 4.6e+003 -7.57e-001 -7.842864603e+004 9.038469633e+003  3.6e-002 0.22  
6   3.6e+001 4.7e+001 2.0e+003 -2.53e-001 -4.698030125e+004 1.010176987e+004  1.6e-002 0.25  
7   1.8e+001 2.4e+001 1.0e+003 2.76e-001  -2.813348785e+004 6.397683045e+003  8.2e-003 0.27  
8   9.2e+000 1.2e+001 5.1e+002 6.02e-001  -1.477869522e+004 4.004072532e+003  4.0e-003 0.30  
9   5.7e+000 7.4e+000 3.2e+002 8.20e-001  -9.247830188e+003 2.776682075e+003  2.5e-003 0.31  
10  1.9e+000 2.5e+000 1.1e+002 9.03e-001  -3.003060519e+003 1.154002816e+003  8.5e-004 0.34  
11  1.6e+000 2.0e+000 8.8e+001 9.75e-001  -2.419019181e+003 1.010907178e+003  7.0e-004 0.36  
12  1.0e+000 1.4e+000 5.7e+001 9.77e-001  -1.494909905e+003 7.263450535e+002  4.5e-004 0.39  
13  4.7e-001 7.0e-001 2.7e+001 9.83e-001  -6.134621319e+002 4.375216650e+002  2.1e-004 0.41  
14  2.5e-001 3.8e-001 1.4e+001 1.00e+000  -2.355955618e+002 3.290669028e+002  1.1e-004 0.44  
15  1.0e-001 1.7e-001 5.9e+000 1.00e+000  7.317576511e+000  2.369834178e+002  4.7e-005 0.47  
16  5.0e-002 1.0e-001 2.9e+000 1.00e+000  9.073384410e+001  2.038614896e+002  2.3e-005 0.48  
17  1.0e-002 1.5e-001 6.3e-001 1.01e+000  1.546017188e+002  1.791070633e+002  5.2e-006 0.50  
18  6.2e-003 1.0e-001 3.8e-001 1.01e+000  1.615121015e+002  1.764421345e+002  3.2e-006 0.53  
19  1.6e-003 1.2e-001 1.0e-001 1.01e+000  1.694752255e+002  1.734658678e+002  8.7e-007 0.56  
20  3.3e-004 1.5e-001 2.2e-002 1.01e+000  1.717779154e+002  1.726253081e+002  1.9e-007 0.58  
21  1.4e-004 1.0e-001 9.3e-003 9.93e-001  1.721395928e+002  1.725021457e+002  8.2e-008 0.59  
22  8.8e-005 8.3e-002 5.9e-003 1.00e+000  1.722353228e+002  1.724645588e+002  5.2e-008 0.62  
23  7.9e-005 7.7e-002 5.3e-003 1.00e+000  1.722533715e+002  1.724597547e+002  4.7e-008 0.64  
24  7.1e-005 7.0e-002 4.8e-003 1.00e+000  1.722685694e+002  1.724543188e+002  4.2e-008 0.67  
25  6.4e-005 6.4e-002 4.3e-003 1.00e+000  1.722822906e+002  1.724494658e+002  3.8e-008 0.70  
26  5.8e-005 5.8e-002 3.9e-003 1.00e+000  1.722946104e+002  1.724450677e+002  3.4e-008 0.72  
27  5.2e-005 5.3e-002 3.5e-003 1.00e+000  1.723056854e+002  1.724410961e+002  3.1e-008 0.75  
28  4.7e-005 4.9e-002 3.1e-003 1.00e+000  1.723156379e+002  1.724375064e+002  2.8e-008 0.76  
29  4.2e-005 4.5e-002 2.8e-003 1.00e+000  1.723245816e+002  1.724342621e+002  2.5e-008 0.80  
30  3.8e-005 4.1e-002 2.5e-003 1.00e+000  1.723326187e+002  1.724313301e+002  2.2e-008 0.81  
31  3.4e-005 3.8e-002 2.3e-003 1.00e+000  1.723398415e+002  1.724286807e+002  2.0e-008 0.84  
32  3.1e-005 3.5e-002 2.1e-003 1.00e+000  1.723463329e+002  1.724262874e+002  1.8e-008 0.86  
33  2.8e-005 3.2e-002 1.9e-003 1.00e+000  1.723521677e+002  1.724241260e+002  1.6e-008 0.90  
34  2.5e-005 3.0e-002 1.7e-003 1.00e+000  1.723574129e+002  1.724221748e+002  1.5e-008 0.94  
35  2.2e-005 2.8e-002 1.5e-003 1.00e+000  1.723621285e+002  1.724204137e+002  1.3e-008 0.97  
36  2.0e-005 2.6e-002 1.4e-003 1.00e+000  1.723663685e+002  1.724188248e+002  1.2e-008 1.00  
37  1.8e-005 2.4e-002 1.2e-003 1.00e+000  1.723701811e+002  1.724173915e+002  1.1e-008 1.01  
38  1.6e-005 2.2e-002 1.1e-003 1.00e+000  1.723736097e+002  1.724160988e+002  9.6e-009 1.04  
39  1.5e-005 2.1e-002 9.9e-004 1.00e+000  1.723766931e+002  1.724149331e+002  8.6e-009 1.06  
40  1.3e-005 1.9e-002 8.9e-004 1.00e+000  1.723794662e+002  1.724138821e+002  7.8e-009 1.09  
41  1.2e-005 1.8e-002 8.0e-004 1.00e+000  1.723819603e+002  1.724129347e+002  7.0e-009 1.11  
42  1.1e-005 1.7e-002 7.2e-004 1.00e+000  1.723842037e+002  1.724120806e+002  6.3e-009 1.14  
43  9.6e-006 1.6e-002 6.5e-004 1.00e+000  1.723862217e+002  1.724113108e+002  5.7e-009 1.19  
44  8.7e-006 1.5e-002 5.8e-004 1.00e+000  1.723880368e+002  1.724106171e+002  5.1e-009 1.22  
45  7.8e-006 1.5e-002 5.2e-004 1.00e+000  1.723896697e+002  1.724099919e+002  4.6e-009 1.25  
46  7.0e-006 1.4e-002 4.7e-004 1.00e+000  1.723911386e+002  1.724094286e+002  4.1e-009 1.28  
47  6.3e-006 1.3e-002 4.3e-004 1.00e+000  1.723924601e+002  1.724089211e+002  3.7e-009 1.29  
48  5.7e-006 1.3e-002 3.8e-004 1.00e+000  1.723936490e+002  1.724084639e+002  3.3e-009 1.33  
49  5.1e-006 1.2e-002 3.4e-004 1.00e+000  1.723947185e+002  1.724080521e+002  3.0e-009 1.34  
50  4.6e-006 1.2e-002 3.1e-004 1.00e+000  1.723956808e+002  1.724076811e+002  2.7e-009 1.37  
51  4.2e-006 1.1e-002 2.8e-004 1.00e+000  1.723965466e+002  1.724073469e+002  2.4e-009 1.39  
52  3.7e-006 1.1e-002 2.5e-004 1.00e+000  1.723973256e+002  1.724070459e+002  2.2e-009 1.42  
53  3.4e-006 1.1e-002 2.3e-004 1.00e+000  1.723980265e+002  1.724067748e+002  2.0e-009 1.44  
54  3.0e-006 1.0e-002 2.0e-004 1.00e+000  1.723986571e+002  1.724065306e+002  1.8e-009 1.47  
55  2.7e-006 1.0e-002 1.8e-004 1.00e+000  1.723992246e+002  1.724063108e+002  1.6e-009 1.48  
56  2.5e-006 9.7e-003 1.6e-004 1.00e+000  1.723997352e+002  1.724061127e+002  1.4e-009 1.51  
57  2.2e-006 9.5e-003 1.5e-004 1.00e+000  1.724001946e+002  1.724059344e+002  1.3e-009 1.53  
58  2.0e-006 9.3e-003 1.3e-004 1.00e+000  1.724006080e+002  1.724057739e+002  1.2e-009 1.56  
59  1.8e-006 9.1e-003 1.2e-004 1.00e+000  1.724009800e+002  1.724056293e+002  1.1e-009 1.58  
60  1.6e-006 9.0e-003 1.1e-004 1.00e+000  1.724013147e+002  1.724054991e+002  9.5e-010 1.61  
61  1.4e-006 8.8e-003 9.7e-005 1.00e+000  1.724016159e+002  1.724053819e+002  8.5e-010 1.62  
62  1.3e-006 8.7e-003 8.8e-005 1.00e+000  1.724018870e+002  1.724052764e+002  7.7e-010 1.65  
63  1.2e-006 8.6e-003 7.9e-005 1.00e+000  1.724021309e+002  1.724051814e+002  6.9e-010 1.67  
64  1.1e-006 8.5e-003 7.1e-005 1.00e+000  1.724023504e+002  1.724050958e+002  6.2e-010 1.70  
65  9.5e-007 8.4e-003 6.4e-005 1.00e+000  1.724025479e+002  1.724050187e+002  5.6e-010 1.72  
66  8.5e-007 8.3e-003 5.7e-005 1.00e+000  1.724027256e+002  1.724049494e+002  5.0e-010 1.75  
67  7.7e-007 8.2e-003 5.2e-005 1.00e+000  1.724028855e+002  1.724048869e+002  4.5e-010 1.76  
68  6.9e-007 8.1e-003 4.7e-005 1.00e+000  1.724030294e+002  1.724048307e+002  4.1e-010 1.79  
69  6.2e-007 8.0e-003 4.2e-005 1.00e+000  1.724031589e+002  1.724047801e+002  3.7e-010 1.83  
70  5.6e-007 8.0e-003 3.8e-005 1.00e+000  1.724032755e+002  1.724047346e+002  3.3e-010 1.86  
71  5.0e-007 7.9e-003 3.4e-005 1.00e+000  1.724033803e+002  1.724046935e+002  3.0e-010 1.87  
72  4.5e-007 7.9e-003 3.1e-005 1.00e+000  1.724034747e+002  1.724046566e+002  2.7e-010 1.90  
73  4.1e-007 7.8e-003 2.7e-005 1.00e+000  1.724035596e+002  1.724046233e+002  2.4e-010 1.93  
74  3.7e-007 7.8e-003 2.5e-005 1.00e+000  1.724036361e+002  1.724045934e+002  2.2e-010 1.95  
75  3.3e-007 7.7e-003 2.2e-005 1.00e+000  1.724037048e+002  1.724045664e+002  1.9e-010 1.98  
76  3.0e-007 7.7e-003 2.0e-005 1.00e+000  1.724037667e+002  1.724045421e+002  1.8e-010 2.01  
77  2.7e-007 7.7e-003 1.8e-005 1.00e+000  1.724038224e+002  1.724045203e+002  1.6e-010 2.04  
78  2.4e-007 7.6e-003 1.6e-005 1.00e+000  1.724038725e+002  1.724045006e+002  1.4e-010 2.06  
79  2.2e-007 7.6e-003 1.5e-005 9.99e-001  1.724039176e+002  1.724044829e+002  1.3e-010 2.09  
80  2.0e-007 7.6e-003 1.3e-005 9.99e-001  1.724039582e+002  1.724044670e+002  1.2e-010 2.11  
81  1.8e-007 7.5e-003 1.2e-005 1.00e+000  1.724039947e+002  1.724044526e+002  1.0e-010 2.12  
82  1.6e-007 7.5e-003 1.1e-005 1.00e+000  1.724040276e+002  1.724044397e+002  9.3e-011 2.15  
83  1.4e-007 7.5e-003 9.6e-006 1.00e+000  1.724040572e+002  1.724044280e+002  8.4e-011 2.17  
84  1.3e-007 7.5e-003 8.6e-006 1.00e+000  1.724040838e+002  1.724044176e+002  7.5e-011 2.20  
85  1.2e-007 7.4e-003 7.8e-006 9.98e-001  1.724041077e+002  1.724044082e+002  6.8e-011 2.21  
86  1.0e-007 7.4e-003 7.0e-006 9.99e-001  1.724041293e+002  1.724043997e+002  6.1e-011 2.23  
87  9.4e-008 7.4e-003 6.3e-006 9.98e-001  1.724041487e+002  1.724043921e+002  5.5e-011 2.26  
88  8.4e-008 7.4e-003 5.7e-006 9.99e-001  1.724041661e+002  1.724043852e+002  5.0e-011 2.28  
89  7.6e-008 7.4e-003 5.1e-006 1.00e+000  1.724041818e+002  1.724043790e+002  4.5e-011 2.29  
90  6.8e-008 7.4e-003 4.6e-006 1.00e+000  1.724041960e+002  1.724043734e+002  4.0e-011 4.26  
91  6.1e-008 7.3e-003 4.1e-006 1.00e+000  1.724042087e+002  1.724043684e+002  3.6e-011 4.29  
92  5.5e-008 7.3e-003 3.7e-006 9.98e-001  1.724042201e+002  1.724043639e+002  3.2e-011 4.32  
93  5.0e-008 7.3e-003 3.3e-006 1.00e+000  1.724042304e+002  1.724043598e+002  2.9e-011 4.34  
94  4.5e-008 6.6e-003 3.0e-006 1.00e+000  1.724042398e+002  1.724043561e+002  2.6e-011 4.37  
95  4.0e-008 5.9e-003 2.7e-006 1.01e+000  1.724042483e+002  1.724043527e+002  2.4e-011 4.38  
96  3.6e-008 5.3e-003 2.4e-006 1.01e+000  1.724042559e+002  1.724043497e+002  2.1e-011 4.41  
97  3.3e-008 4.8e-003 2.2e-006 1.01e+000  1.724042629e+002  1.724043469e+002  1.9e-011 4.45  
98  2.9e-008 4.3e-003 2.0e-006 9.96e-001  1.724042689e+002  1.724043445e+002  1.7e-011 4.46  
99  2.6e-008 3.9e-003 1.8e-006 1.00e+000  1.724042743e+002  1.724043424e+002  1.6e-011 4.49  
100 2.4e-008 3.5e-003 1.6e-006 1.01e+000  1.724042794e+002  1.724043404e+002  1.4e-011 4.51  
101 2.1e-008 3.1e-003 1.4e-006 1.00e+000  1.724042838e+002  1.724043386e+002  1.3e-011 4.54  
102 1.9e-008 2.8e-003 1.3e-006 1.00e+000  1.724042878e+002  1.724043370e+002  1.1e-011 4.57  
103 1.7e-008 2.6e-003 1.2e-006 1.00e+000  1.724042913e+002  1.724043356e+002  1.0e-011 4.59  
104 1.6e-008 2.3e-003 1.0e-006 1.01e+000  1.724042946e+002  1.724043343e+002  9.4e-012 4.62  
105 3.9e-009 5.6e-004 2.6e-007 9.94e-001  1.724043161e+002  1.724043259e+002  2.3e-012 4.63  
106 3.5e-009 5.1e-004 2.3e-007 1.04e+000  1.724043169e+002  1.724043256e+002  2.1e-012 4.66  
107 1.7e-009 1.3e-004 6.0e-008 1.09e+000  1.724043215e+002  1.724043235e+002  5.0e-013 4.70  
Interior-point optimizer terminated. Time: 4.70. 

Optimizer terminated. Time: 4.71    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.7240432146e+002   Viol.  con: 4e-008   var: 0e+000 
  Dual.    obj: 1.7240432353e+002   Viol.  con: 0e+000   var: 9e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 4.74 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 936             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 769
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3440              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.05              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.46e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.289209295e+005 2.000000000e+000  1.0e+000 0.09  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.267404409e+005 3.637047596e+000  4.8e-001 0.14  
2   4.4e+002 5.7e+002 2.4e+004 -9.36e-001 -1.207993266e+005 1.004622041e+001  1.9e-001 0.19  
3   2.9e+002 3.8e+002 1.6e+004 -8.43e-001 -1.160618624e+005 5.990661859e+001  1.3e-001 0.22  
4   2.9e+002 3.8e+002 1.6e+004 -7.62e-001 -1.136045227e+005 2.136091938e+003  1.3e-001 0.25  
5   8.1e+001 1.0e+002 4.5e+003 -7.56e-001 -7.752618540e+004 9.316590062e+003  3.5e-002 0.28  
6   4.0e+001 5.2e+001 2.2e+003 -2.34e-001 -5.076740394e+004 1.003179681e+004  1.8e-002 0.58  
7   3.0e+001 3.9e+001 1.7e+003 2.19e-001  -4.171035603e+004 8.294891379e+003  1.3e-002 1.69  
8   1.9e+001 2.4e+001 1.0e+003 3.81e-001  -2.865144900e+004 5.387067742e+003  8.1e-003 1.90  
9   7.9e+000 1.0e+001 4.4e+002 6.03e-001  -1.310598994e+004 3.143052779e+003  3.5e-003 2.23  
10  4.0e+000 5.2e+000 2.2e+002 8.46e-001  -6.378104244e+003 2.128676893e+003  1.8e-003 2.56  
11  2.2e+000 2.9e+000 1.3e+002 9.42e-001  -3.514564173e+003 1.314879025e+003  9.9e-004 2.95  
12  9.1e-001 1.2e+000 5.1e+001 9.75e-001  -1.333956042e+003 6.456473822e+002  4.0e-004 3.40  
13  8.2e-001 1.1e+000 4.6e+001 9.70e-001  -1.223648571e+003 5.999353608e+002  3.7e-004 3.77  
14  5.9e-001 7.8e-001 3.3e+001 9.74e-001  -8.149798235e+002 4.893556589e+002  2.6e-004 4.10  
15  2.2e-001 7.6e-001 1.2e+001 9.90e-001  -1.999790707e+002 2.844527361e+002  9.8e-005 4.43  
16  1.1e-001 3.8e-001 6.1e+000 1.00e+000  -2.241182742e+001 2.161153577e+002  4.9e-005 4.76  
17  7.7e-002 2.8e-001 4.5e+000 1.01e+000  2.681099786e+001  2.015602373e+002  3.6e-005 5.09  
18  5.1e-002 2.0e-001 3.0e+000 1.02e+000  7.892010908e+001  1.950358603e+002  2.4e-005 5.40  
19  1.4e-002 1.1e-001 8.5e-001 1.00e+000  1.414702401e+002  1.745814524e+002  6.9e-006 5.72  
20  4.0e-003 2.2e-001 2.4e-001 1.02e+000  1.602704839e+002  1.696481054e+002  1.9e-006 6.05  
21  2.7e-003 2.1e-001 1.6e-001 1.01e+000  1.624284486e+002  1.687369615e+002  1.3e-006 6.38  
22  1.9e-003 1.5e-001 1.2e-001 1.00e+000  1.637170157e+002  1.683012316e+002  9.5e-007 7.30  
23  7.5e-004 9.5e-002 4.7e-002 1.01e+000  1.658030319e+002  1.676006389e+002  3.8e-007 7.61  
24  3.6e-004 7.9e-002 2.3e-002 1.01e+000  1.664694730e+002  1.673480712e+002  1.9e-007 7.92  
25  3.3e-004 7.2e-002 2.1e-002 1.01e+000  1.665375881e+002  1.673287202e+002  1.7e-007 8.28  
26  3.0e-004 6.6e-002 1.9e-002 1.01e+000  1.665946786e+002  1.673064382e+002  1.5e-007 8.61  
27  2.7e-004 6.0e-002 1.7e-002 1.01e+000  1.666462641e+002  1.672866410e+002  1.4e-007 8.94  
28  2.4e-004 5.5e-002 1.5e-002 1.01e+000  1.666924558e+002  1.672686246e+002  1.2e-007 9.27  
29  2.2e-004 5.0e-002 1.4e-002 1.01e+000  1.667339024e+002  1.672523149e+002  1.1e-007 9.61  
30  1.9e-004 4.6e-002 1.2e-002 1.01e+000  1.667710636e+002  1.672375207e+002  9.9e-008 9.94  
31  1.7e-004 4.2e-002 1.1e-002 1.01e+000  1.668043837e+002  1.672241019e+002  8.9e-008 10.27 
32  1.6e-004 3.8e-002 9.9e-003 1.01e+000  1.668342581e+002  1.672119284e+002  8.0e-008 10.61 
33  1.4e-004 3.5e-002 8.9e-003 1.01e+000  1.668610432e+002  1.672008847e+002  7.2e-008 10.94 
34  1.3e-004 3.3e-002 8.0e-003 1.01e+000  1.668850596e+002  1.671908667e+002  6.5e-008 11.26 
35  1.1e-004 3.0e-002 7.2e-003 1.00e+000  1.669065956e+002  1.671817816e+002  5.8e-008 11.57 
36  1.0e-004 2.8e-002 6.5e-003 1.00e+000  1.669259102e+002  1.671735451e+002  5.3e-008 11.90 
37  9.3e-005 2.6e-002 5.8e-003 1.00e+000  1.669432357e+002  1.671660809e+002  4.7e-008 12.22 
38  8.3e-005 2.4e-002 5.3e-003 1.00e+000  1.669587796e+002  1.671593195e+002  4.3e-008 13.10 
39  7.5e-005 2.2e-002 4.7e-003 1.00e+000  1.669727275e+002  1.671531969e+002  3.8e-008 13.39 
40  6.7e-005 2.1e-002 4.3e-003 1.00e+000  1.669852453e+002  1.671476546e+002  3.5e-008 13.68 
41  6.1e-005 2.0e-002 3.8e-003 1.00e+000  1.669964813e+002  1.671426394e+002  3.1e-008 13.96 
42  5.5e-005 1.8e-002 3.4e-003 1.00e+000  1.670065681e+002  1.671381023e+002  2.8e-008 14.27 
43  4.9e-005 1.7e-002 3.1e-003 1.00e+000  1.670156244e+002  1.671339988e+002  2.5e-008 14.57 
44  4.4e-005 1.6e-002 2.8e-003 1.00e+000  1.670237565e+002  1.671302887e+002  2.3e-008 14.88 
45  4.0e-005 1.6e-002 2.5e-003 1.00e+000  1.670310596e+002  1.671269349e+002  2.0e-008 15.19 
46  3.6e-005 1.5e-002 2.3e-003 1.00e+000  1.670376190e+002  1.671239039e+002  1.8e-008 15.52 
47  3.2e-005 1.4e-002 2.0e-003 1.00e+000  1.670435109e+002  1.671211653e+002  1.7e-008 15.85 
48  2.9e-005 1.4e-002 1.8e-003 1.00e+000  1.670488040e+002  1.671186914e+002  1.5e-008 16.16 
49  2.6e-005 1.3e-002 1.7e-003 1.00e+000  1.670535594e+002  1.671164570e+002  1.3e-008 16.50 
50  2.4e-005 1.3e-002 1.5e-003 1.00e+000  1.670578323e+002  1.671144394e+002  1.2e-008 16.83 
51  2.1e-005 1.2e-002 1.3e-003 1.00e+000  1.670616720e+002  1.671126178e+002  1.1e-008 17.16 
52  1.9e-005 1.2e-002 1.2e-003 1.00e+000  1.670651226e+002  1.671109736e+002  9.8e-009 17.92 
53  1.7e-005 1.1e-002 1.1e-003 1.00e+000  1.670682240e+002  1.671094896e+002  8.8e-009 18.24 
54  1.5e-005 1.1e-002 9.7e-004 1.00e+000  1.670710115e+002  1.671081505e+002  7.9e-009 18.56 
55  1.4e-005 1.1e-002 8.8e-004 1.00e+000  1.670735173e+002  1.671069423e+002  7.1e-009 18.89 
56  1.3e-005 1.0e-002 7.9e-004 1.00e+000  1.670757699e+002  1.671058524e+002  6.4e-009 19.22 
57  1.1e-005 1.0e-002 7.1e-004 1.00e+000  1.670777951e+002  1.671048694e+002  5.8e-009 19.53 
58  1.0e-005 1.0e-002 6.4e-004 1.00e+000  1.670796160e+002  1.671039828e+002  5.2e-009 19.83 
59  9.1e-006 9.8e-003 5.8e-004 1.00e+000  1.670812532e+002  1.671031835e+002  4.7e-009 20.16 
60  8.2e-006 9.6e-003 5.2e-004 1.00e+000  1.670827255e+002  1.671024629e+002  4.2e-009 20.50 
61  7.4e-006 9.5e-003 4.7e-004 1.00e+000  1.670840495e+002  1.671018131e+002  3.8e-009 20.83 
62  6.6e-006 9.3e-003 4.2e-004 1.00e+000  1.670852403e+002  1.671012276e+002  3.4e-009 21.15 
63  6.0e-006 9.2e-003 3.8e-004 1.00e+000  1.670863112e+002  1.671006998e+002  3.1e-009 21.50 
64  5.4e-006 9.1e-003 3.4e-004 1.00e+000  1.670872745e+002  1.671002243e+002  2.8e-009 21.82 
65  2.0e-006 3.4e-003 1.3e-004 1.00e+000  1.670926202e+002  1.670975550e+002  1.1e-009 22.15 
66  6.9e-007 1.2e-003 4.4e-005 1.00e+000  1.670947963e+002  1.670964668e+002  3.6e-010 22.57 
67  6.2e-007 1.0e-003 3.9e-005 9.99e-001  1.670949107e+002  1.670964141e+002  3.2e-010 22.78 
68  5.6e-007 9.4e-004 3.6e-005 1.00e+000  1.670950102e+002  1.670963633e+002  2.9e-010 23.82 
69  5.0e-007 8.5e-004 3.2e-005 1.00e+000  1.670951000e+002  1.670963178e+002  2.6e-010 23.90 
70  4.5e-007 7.6e-004 2.9e-005 9.99e-001  1.670951808e+002  1.670962767e+002  2.3e-010 24.13 
71  4.1e-007 6.9e-004 2.6e-005 1.00e+000  1.670952534e+002  1.670962398e+002  2.1e-010 24.15 
72  3.7e-007 6.2e-004 2.3e-005 1.00e+000  1.670953187e+002  1.670962064e+002  1.9e-010 24.18 
73  3.3e-007 5.6e-004 2.1e-005 9.98e-001  1.670953775e+002  1.670961765e+002  1.7e-010 25.80 
74  3.0e-007 5.0e-004 1.9e-005 9.99e-001  1.670954303e+002  1.670961495e+002  1.5e-010 26.19 
75  2.7e-007 4.5e-004 1.7e-005 9.99e-001  1.670954779e+002  1.670961252e+002  1.4e-010 26.43 
76  2.4e-007 4.1e-004 1.5e-005 9.98e-001  1.670955206e+002  1.670961033e+002  1.2e-010 26.63 
77  2.2e-007 3.7e-004 1.4e-005 9.99e-001  1.670955591e+002  1.670960835e+002  1.1e-010 26.82 
78  2.0e-007 3.3e-004 1.2e-005 1.00e+000  1.670955938e+002  1.670960658e+002  1.0e-010 27.14 
79  1.8e-007 3.0e-004 1.1e-005 1.00e+000  1.670956250e+002  1.670960497e+002  9.1e-011 27.30 
80  1.6e-007 2.7e-004 1.0e-005 1.00e+000  1.670956530e+002  1.670960353e+002  8.2e-011 27.44 
81  1.4e-007 2.4e-004 9.0e-006 9.98e-001  1.670956783e+002  1.670960223e+002  7.3e-011 27.55 
82  1.3e-007 2.2e-004 8.1e-006 1.00e+000  1.670957010e+002  1.670960106e+002  6.6e-011 27.78 
83  1.2e-007 1.9e-004 7.3e-006 1.00e+000  1.670957214e+002  1.670960001e+002  5.9e-011 27.82 
84  1.0e-007 1.7e-004 6.6e-006 9.99e-001  1.670957398e+002  1.670959906e+002  5.4e-011 27.88 
85  9.3e-008 1.6e-004 5.9e-006 1.00e+000  1.670957564e+002  1.670959821e+002  4.8e-011 28.33 
86  8.4e-008 1.4e-004 5.3e-006 1.00e+000  1.670957713e+002  1.670959744e+002  4.3e-011 28.94 
87  7.6e-008 1.3e-004 4.8e-006 9.97e-001  1.670957847e+002  1.670959675e+002  3.9e-011 28.97 
88  6.8e-008 1.1e-004 4.3e-006 1.01e+000  1.670957970e+002  1.670959612e+002  3.5e-011 29.00 
89  6.1e-008 1.0e-004 3.9e-006 9.97e-001  1.670958078e+002  1.670959556e+002  3.2e-011 29.03 
90  5.5e-008 9.3e-005 3.5e-006 1.01e+000  1.670958179e+002  1.670959504e+002  2.9e-011 29.06 
91  5.0e-008 8.4e-005 3.1e-006 1.00e+000  1.670958266e+002  1.670959459e+002  2.6e-011 29.09 
92  4.5e-008 7.5e-005 2.8e-006 1.01e+000  1.670958347e+002  1.670959417e+002  2.3e-011 29.11 
93  4.0e-008 6.8e-005 2.6e-006 9.87e-001  1.670958417e+002  1.670959381e+002  2.1e-011 29.14 
94  3.6e-008 6.1e-005 2.3e-006 1.01e+000  1.670958482e+002  1.670959347e+002  1.9e-011 29.17 
95  3.3e-008 5.5e-005 2.1e-006 1.00e+000  1.670958539e+002  1.670959318e+002  1.7e-011 29.20 
96  2.9e-008 4.9e-005 1.9e-006 9.87e-001  1.670958590e+002  1.670959292e+002  1.5e-011 29.23 
97  2.6e-008 4.4e-005 1.7e-006 1.01e+000  1.670958638e+002  1.670959267e+002  1.4e-011 29.27 
98  2.4e-008 4.0e-005 1.5e-006 9.93e-001  1.670958679e+002  1.670959246e+002  1.2e-011 29.30 
99  2.1e-008 3.6e-005 1.4e-006 1.00e+000  1.670958717e+002  1.670959227e+002  1.1e-011 29.31 
100 1.9e-008 3.2e-005 1.2e-006 1.03e+000  1.670958754e+002  1.670959207e+002  1.0e-011 29.34 
101 1.7e-008 2.9e-005 1.1e-006 1.02e+000  1.670958786e+002  1.670959190e+002  9.2e-012 29.38 
Interior-point optimizer terminated. Time: 29.38. 

Optimizer terminated. Time: 29.75   
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6709587862e+002   Viol.  con: 3e-007   var: 0e+000 
  Dual.    obj: 1.6709591899e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 29.8 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 936             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 769
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3440              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.05              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.46e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.286499296e+005 2.000000000e+000  1.0e+000 0.09  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.264834068e+005 3.586695421e+000  4.8e-001 0.14  
2   4.3e+002 5.6e+002 2.4e+004 -9.36e-001 -1.204818392e+005 1.001252982e+001  1.9e-001 0.39  
3   2.9e+002 3.7e+002 1.6e+004 -8.42e-001 -1.157492293e+005 6.085652497e+001  1.3e-001 0.72  
4   2.9e+002 3.7e+002 1.6e+004 -7.62e-001 -1.131499808e+005 2.257752003e+003  1.3e-001 1.65  
5   7.4e+001 9.6e+001 4.1e+003 -7.55e-001 -7.449025341e+004 9.842634555e+003  3.3e-002 2.17  
6   3.6e+001 4.7e+001 2.0e+003 -1.90e-001 -4.726343643e+004 1.026281927e+004  1.6e-002 2.40  
7   2.2e+001 2.9e+001 1.3e+003 2.77e-001  -3.297732476e+004 7.148458349e+003  9.9e-003 2.61  
8   1.4e+001 1.7e+001 7.5e+002 5.32e-001  -2.145913301e+004 4.808156551e+003  6.0e-003 2.79  
9   5.3e+000 6.9e+000 3.0e+002 7.21e-001  -8.768077363e+003 2.417294283e+003  2.4e-003 2.95  
10  2.4e+000 3.1e+000 1.3e+002 9.13e-001  -3.743297563e+003 1.405439141e+003  1.1e-003 3.17  
11  1.7e+000 2.3e+000 9.8e+001 9.75e-001  -2.706782709e+003 1.075294540e+003  7.8e-004 3.46  
12  8.2e-001 1.1e+000 4.6e+001 9.83e-001  -1.189758834e+003 5.993133985e+002  3.7e-004 3.65  
13  7.5e-001 1.1e+000 4.2e+001 9.48e-001  -1.109365139e+003 5.596607327e+002  3.4e-004 3.92  
14  6.3e-001 8.8e-001 3.5e+001 9.86e-001  -8.799128249e+002 5.072307769e+002  2.8e-004 4.23  
15  1.8e-001 2.8e-001 1.0e+001 9.89e-001  -1.584746310e+002 2.541999835e+002  8.4e-005 4.24  
16  1.0e-001 1.7e-001 5.9e+000 1.01e+000  -1.976710167e+001 2.098853145e+002  4.7e-005 4.27  
17  1.0e-001 1.7e-001 5.8e+000 1.02e+000  -1.809007688e+001 2.102290965e+002  4.7e-005 4.62  
18  8.6e-002 1.5e-001 5.0e+000 1.02e+000  1.591137127e+001  2.106371573e+002  4.0e-005 4.85  
19  4.3e-002 9.6e-002 2.5e+000 1.01e+000  9.060679234e+001  1.877232109e+002  2.0e-005 4.87  
20  1.2e-002 1.9e-001 6.8e-001 1.01e+000  1.471515213e+002  1.733931978e+002  5.5e-006 4.90  
21  4.3e-003 3.5e-001 2.6e-001 1.01e+000  1.590309677e+002  1.689623316e+002  2.1e-006 4.91  
22  1.2e-003 1.7e-001 7.5e-002 1.01e+000  1.645645226e+002  1.674294489e+002  6.1e-007 4.93  
23  6.7e-004 1.2e-001 4.2e-002 9.81e-001  1.654775941e+002  1.670873260e+002  3.5e-007 4.96  
24  2.0e-004 1.1e-001 1.3e-002 9.95e-001  1.662934781e+002  1.667797762e+002  1.1e-007 4.98  
25  6.2e-005 1.1e-001 4.1e-003 1.01e+000  1.665280220e+002  1.666839062e+002  3.5e-008 4.99  
26  2.0e-005 1.1e-001 1.4e-003 1.01e+000  1.666013277e+002  1.666531285e+002  1.2e-008 5.02  
27  6.5e-006 1.1e-001 4.4e-004 1.00e+000  1.666261868e+002  1.666427315e+002  3.8e-009 5.04  
28  2.2e-006 1.0e-001 1.5e-004 1.00e+000  1.666337604e+002  1.666395181e+002  1.3e-009 5.07  
29  7.7e-007 9.7e-002 5.3e-005 1.00e+000  1.666363789e+002  1.666383685e+002  4.5e-010 5.09  
30  3.4e-007 8.2e-002 2.3e-005 1.00e+000  1.666371512e+002  1.666380167e+002  2.0e-010 5.10  
31  7.3e-008 1.8e-002 5.0e-006 1.00e+000  1.666376165e+002  1.666378051e+002  4.3e-011 5.13  
32  6.6e-008 1.6e-002 4.5e-006 9.99e-001  1.666376305e+002  1.666378003e+002  3.9e-011 5.15  
33  5.9e-008 1.6e-002 4.1e-006 1.01e+000  1.666376425e+002  1.666377946e+002  3.5e-011 5.18  
34  5.3e-008 1.5e-002 3.7e-006 1.01e+000  1.666376534e+002  1.666377895e+002  3.2e-011 5.21  
35  4.8e-008 1.4e-002 3.3e-006 9.96e-001  1.666376626e+002  1.666377851e+002  2.9e-011 5.23  
36  4.3e-008 1.4e-002 3.0e-006 1.01e+000  1.666376714e+002  1.666377810e+002  2.6e-011 5.24  
37  3.9e-008 1.3e-002 2.7e-006 9.73e-001  1.666376789e+002  1.666377776e+002  2.3e-011 5.27  
38  3.5e-008 1.2e-002 2.4e-006 1.00e+000  1.666376856e+002  1.666377744e+002  2.1e-011 5.29  
39  3.1e-008 1.2e-002 2.2e-006 9.92e-001  1.666376916e+002  1.666377716e+002  1.9e-011 5.35  
40  2.8e-008 1.1e-002 1.9e-006 9.68e-001  1.666376970e+002  1.666377691e+002  1.7e-011 5.38  
41  2.5e-008 1.1e-002 1.8e-006 9.95e-001  1.666377019e+002  1.666377668e+002  1.5e-011 5.40  
42  2.3e-008 1.1e-002 1.6e-006 1.02e+000  1.666377068e+002  1.666377645e+002  1.4e-011 5.43  
43  2.1e-008 1.1e-002 1.4e-006 1.02e+000  1.666377110e+002  1.666377624e+002  1.3e-011 5.44  
44  1.9e-008 1.1e-002 1.3e-006 1.01e+000  1.666377147e+002  1.666377607e+002  1.1e-011 5.46  
45  1.7e-008 1.0e-002 1.1e-006 9.44e-001  1.666377178e+002  1.666377593e+002  1.0e-011 5.49  
46  1.5e-008 9.9e-003 1.0e-006 9.72e-001  1.666377206e+002  1.666377580e+002  9.3e-012 5.51  
47  1.4e-008 8.9e-003 9.3e-007 1.05e+000  1.666377238e+002  1.666377565e+002  8.6e-012 5.52  
48  1.2e-008 8.6e-003 8.4e-007 9.54e-001  1.666377260e+002  1.666377555e+002  7.7e-012 5.55  
49  1.1e-008 7.8e-003 7.5e-007 1.03e+000  1.666377282e+002  1.666377544e+002  7.0e-012 5.57  
50  9.9e-009 7.0e-003 6.8e-007 1.02e+000  1.666377302e+002  1.666377534e+002  6.4e-012 5.59  
51  8.9e-009 6.3e-003 6.1e-007 1.08e+000  1.666377324e+002  1.666377523e+002  6.0e-012 5.62  
52  8.1e-009 5.7e-003 5.5e-007 1.11e+000  1.666377344e+002  1.666377513e+002  5.7e-012 5.63  
53  7.3e-009 5.1e-003 4.9e-007 9.89e-001  1.666377356e+002  1.666377508e+002  5.1e-012 5.66  
54  4.0e-009 3.0e-004 2.9e-008 9.01e-001  1.666377456e+002  1.666377466e+002  5.0e-013 5.68  
Interior-point optimizer terminated. Time: 5.68. 

Optimizer terminated. Time: 5.99    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6663774564e+002   Viol.  con: 9e-008   var: 0e+000 
  Dual.    obj: 1.6663774657e+002   Viol.  con: 0e+000   var: 2e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 6.03 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 936             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.02    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 769
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3440              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.01            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.46e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.286106758e+005 2.000000000e+000  1.0e+000 0.05  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.264422999e+005 3.580364804e+000  4.8e-001 0.08  
2   4.3e+002 5.5e+002 2.4e+004 -9.36e-001 -1.203332259e+005 1.010636748e+001  1.9e-001 0.11  
3   2.9e+002 3.7e+002 1.6e+004 -8.40e-001 -1.156664724e+005 6.247805138e+001  1.3e-001 0.14  
4   2.9e+002 3.7e+002 1.6e+004 -7.61e-001 -1.130152820e+005 2.295884552e+003  1.3e-001 0.17  
5   7.3e+001 9.4e+001 4.1e+003 -7.54e-001 -7.379603980e+004 9.860981649e+003  3.2e-002 0.19  
6   3.6e+001 4.6e+001 2.0e+003 -1.80e-001 -4.641913697e+004 1.009611465e+004  1.6e-002 0.22  
7   2.1e+001 2.7e+001 1.2e+003 2.91e-001  -3.097467487e+004 6.886212178e+003  9.2e-003 0.23  
8   1.2e+001 1.6e+001 6.8e+002 5.65e-001  -1.945486896e+004 4.491372578e+003  5.4e-003 0.27  
9   4.7e+000 6.1e+000 2.6e+002 7.53e-001  -7.765152023e+003 2.180676629e+003  2.1e-003 0.28  
10  2.3e+000 3.0e+000 1.3e+002 9.26e-001  -3.530371960e+003 1.395529612e+003  1.0e-003 0.31  
11  1.5e+000 1.9e+000 8.5e+001 9.77e-001  -2.301317592e+003 9.721200706e+002  6.7e-004 0.33  
12  8.5e-001 1.1e+000 4.8e+001 9.85e-001  -1.230530014e+003 6.224921147e+002  3.8e-004 0.34  
13  7.5e-001 1.0e+000 4.2e+001 9.54e-001  -1.093830861e+003 5.630528500e+002  3.4e-004 0.38  
14  3.7e-001 5.0e-001 2.1e+001 9.85e-001  -4.359009450e+002 3.737951005e+002  1.6e-004 0.39  
15  1.8e-001 2.5e-001 1.0e+001 9.98e-001  -1.440000235e+002 2.585349403e+002  8.2e-005 0.41  
16  8.9e-002 1.6e-001 5.1e+000 1.01e+000  4.980050053e+000  2.043015279e+002  4.1e-005 0.44  
17  8.6e-002 1.5e-001 4.9e+000 1.01e+000  1.398830804e+001  2.065699361e+002  4.0e-005 0.45  
18  6.1e-002 1.1e-001 3.5e+000 1.01e+000  5.949227238e+001  1.948373544e+002  2.8e-005 0.48  
19  3.0e-002 7.3e-002 1.7e+000 1.01e+000  1.152798301e+002  1.809927698e+002  1.4e-005 0.50  
20  8.5e-003 1.8e-001 4.9e-001 1.01e+000  1.525612471e+002  1.716191967e+002  4.0e-006 0.52  
21  2.5e-003 1.8e-001 1.5e-001 1.00e+000  1.622330959e+002  1.679611398e+002  1.2e-006 0.55  
22  1.5e-003 1.2e-001 9.0e-002 1.00e+000  1.639702664e+002  1.674409711e+002  7.3e-007 0.56  
23  5.1e-004 1.0e-001 3.2e-002 1.01e+000  1.656550190e+002  1.668671096e+002  2.6e-007 0.58  
24  2.0e-004 9.6e-002 1.2e-002 1.01e+000  1.661959803e+002  1.666660326e+002  1.0e-007 0.61  
25  1.8e-004 8.7e-002 1.1e-002 1.01e+000  1.662326089e+002  1.666555345e+002  9.2e-008 0.62  
26  1.6e-004 7.9e-002 1.0e-002 1.01e+000  1.662628637e+002  1.666433548e+002  8.3e-008 0.64  
27  1.4e-004 7.2e-002 9.0e-003 1.01e+000  1.662902744e+002  1.666326036e+002  7.5e-008 0.67  
28  1.3e-004 6.6e-002 8.1e-003 1.01e+000  1.663148181e+002  1.666228208e+002  6.7e-008 0.69  
29  1.2e-004 6.0e-002 7.3e-003 1.01e+000  1.663368446e+002  1.666139698e+002  6.0e-008 0.72  
30  1.0e-004 5.5e-002 6.5e-003 1.01e+000  1.663566061e+002  1.666059555e+002  5.4e-008 0.75  
31  9.4e-005 5.0e-002 5.9e-003 1.01e+000  1.663743376e+002  1.665987001e+002  4.9e-008 0.77  
32  8.5e-005 4.6e-002 5.3e-003 1.01e+000  1.663902483e+002  1.665921321e+002  4.4e-008 0.80  
33  7.6e-005 4.2e-002 4.8e-003 1.01e+000  1.664045262e+002  1.665861873e+002  4.0e-008 0.81  
34  6.9e-005 3.8e-002 4.3e-003 1.01e+000  1.664173402e+002  1.665808072e+002  3.6e-008 0.83  
35  6.2e-005 3.5e-002 3.9e-003 1.01e+000  1.664288415e+002  1.665759392e+002  3.2e-008 0.86  
36  5.5e-005 3.3e-002 3.5e-003 1.00e+000  1.664391658e+002  1.665715356e+002  2.9e-008 0.87  
37  5.0e-005 3.0e-002 3.1e-003 1.00e+000  1.664484346e+002  1.665675527e+002  2.6e-008 0.91  
38  4.5e-005 2.8e-002 2.8e-003 1.00e+000  1.664567567e+002  1.665639513e+002  2.3e-008 0.92  
39  4.0e-005 2.6e-002 2.5e-003 1.00e+000  1.664642295e+002  1.665606954e+002  2.1e-008 0.94  
40  3.6e-005 2.4e-002 2.3e-003 1.00e+000  1.664709406e+002  1.665577524e+002  1.9e-008 0.97  
41  3.3e-005 2.2e-002 2.1e-003 1.00e+000  1.664769681e+002  1.665550928e+002  1.7e-008 0.98  
42  2.9e-005 2.1e-002 1.9e-003 1.00e+000  1.664823823e+002  1.665526898e+002  1.5e-008 1.00  
43  2.7e-005 2.0e-002 1.7e-003 1.00e+000  1.664872459e+002  1.665505191e+002  1.4e-008 1.03  
44  2.4e-005 1.8e-002 1.5e-003 1.00e+000  1.664916155e+002  1.665485585e+002  1.2e-008 1.05  
45  2.1e-005 1.7e-002 1.3e-003 1.00e+000  1.664955417e+002  1.665467881e+002  1.1e-008 1.06  
46  1.9e-005 1.6e-002 1.2e-003 1.00e+000  1.664990697e+002  1.665451898e+002  1.0e-008 1.09  
47  1.7e-005 1.6e-002 1.1e-003 1.00e+000  1.665022404e+002  1.665437471e+002  9.1e-009 1.11  
48  1.6e-005 1.5e-002 9.8e-004 1.00e+000  1.665050901e+002  1.665424452e+002  8.2e-009 1.12  
49  1.4e-005 1.4e-002 8.9e-004 1.00e+000  1.665076518e+002  1.665412705e+002  7.4e-009 1.16  
50  1.3e-005 1.3e-002 8.0e-004 1.00e+000  1.665099547e+002  1.665402110e+002  6.6e-009 1.17  
51  1.1e-005 1.3e-002 7.2e-004 1.00e+000  1.665120252e+002  1.665392555e+002  6.0e-009 1.19  
52  1.0e-005 1.2e-002 6.5e-004 1.00e+000  1.665138870e+002  1.665383940e+002  5.4e-009 1.22  
53  9.3e-006 1.2e-002 5.8e-004 1.00e+000  1.665155612e+002  1.665376173e+002  4.8e-009 1.23  
54  8.3e-006 1.2e-002 5.2e-004 1.00e+000  1.665170669e+002  1.665369173e+002  4.4e-009 1.25  
55  7.5e-006 1.1e-002 4.7e-004 1.00e+000  1.665184211e+002  1.665362864e+002  3.9e-009 1.28  
56  6.7e-006 1.1e-002 4.2e-004 1.00e+000  1.665196392e+002  1.665357179e+002  3.5e-009 1.29  
57  6.1e-006 1.1e-002 3.8e-004 1.00e+000  1.665207348e+002  1.665352057e+002  3.2e-009 1.31  
58  5.5e-006 1.0e-002 3.4e-004 1.00e+000  1.665217204e+002  1.665347442e+002  2.9e-009 1.34  
59  4.9e-006 1.0e-002 3.1e-004 1.00e+000  1.665226069e+002  1.665343284e+002  2.6e-009 1.36  
60  4.4e-006 9.9e-003 2.8e-004 1.00e+000  1.665234044e+002  1.665339538e+002  2.3e-009 1.37  
61  4.0e-006 9.7e-003 2.5e-004 1.00e+000  1.665241217e+002  1.665336162e+002  2.1e-009 1.40  
62  3.6e-006 9.5e-003 2.3e-004 1.00e+000  1.665247669e+002  1.665333121e+002  1.9e-009 1.42  
63  3.2e-006 9.4e-003 2.0e-004 1.00e+000  1.665253472e+002  1.665330379e+002  1.7e-009 1.44  
64  2.9e-006 9.2e-003 1.8e-004 1.00e+000  1.665258692e+002  1.665327909e+002  1.5e-009 1.47  
65  2.6e-006 9.1e-003 1.6e-004 1.00e+000  1.665263387e+002  1.665325682e+002  1.4e-009 1.48  
66  2.4e-006 9.0e-003 1.5e-004 1.00e+000  1.665267610e+002  1.665323677e+002  1.2e-009 1.50  
67  2.1e-006 8.9e-003 1.3e-004 1.00e+000  1.665271409e+002  1.665321870e+002  1.1e-009 1.51  
68  1.9e-006 8.8e-003 1.2e-004 1.00e+000  1.665274827e+002  1.665320241e+002  1.0e-009 1.54  
69  1.7e-006 8.7e-003 1.1e-004 1.00e+000  1.665277902e+002  1.665318775e+002  9.0e-010 1.56  
70  1.5e-006 8.6e-003 9.7e-005 1.00e+000  1.665280668e+002  1.665317454e+002  8.1e-010 1.58  
71  1.4e-006 8.6e-003 8.7e-005 1.00e+000  1.665283156e+002  1.665316263e+002  7.3e-010 1.61  
72  1.3e-006 8.5e-003 7.9e-005 1.00e+000  1.665285394e+002  1.665315191e+002  6.5e-010 1.62  
73  1.1e-006 8.5e-003 7.1e-005 1.00e+000  1.665287408e+002  1.665314225e+002  5.9e-010 1.64  
74  1.0e-006 8.4e-003 6.4e-005 1.00e+000  1.665289219e+002  1.665313355e+002  5.3e-010 1.67  
75  9.1e-007 8.4e-003 5.7e-005 1.00e+000  1.665290849e+002  1.665312571e+002  4.8e-010 1.69  
76  8.2e-007 8.3e-003 5.2e-005 1.00e+000  1.665292314e+002  1.665311865e+002  4.3e-010 1.70  
77  7.4e-007 8.3e-003 4.6e-005 1.00e+000  1.665293633e+002  1.665311228e+002  3.9e-010 1.73  
78  6.6e-007 8.2e-003 4.2e-005 9.99e-001  1.665294818e+002  1.665310655e+002  3.5e-010 1.75  
79  6.0e-007 8.2e-003 3.8e-005 1.00e+000  1.665295884e+002  1.665310138e+002  3.1e-010 1.76  
80  5.4e-007 8.2e-003 3.4e-005 1.00e+000  1.665296843e+002  1.665309671e+002  2.8e-010 1.78  
81  4.8e-007 8.1e-003 3.0e-005 1.00e+000  1.665297706e+002  1.665309251e+002  2.5e-010 1.84  
82  4.4e-007 8.1e-003 2.7e-005 1.00e+000  1.665298481e+002  1.665308872e+002  2.3e-010 1.86  
83  3.9e-007 8.1e-003 2.5e-005 1.00e+000  1.665299179e+002  1.665308530e+002  2.1e-010 1.87  
84  3.5e-007 8.0e-003 2.2e-005 1.00e+000  1.665299806e+002  1.665308222e+002  1.8e-010 1.90  
85  3.2e-007 8.0e-003 2.0e-005 1.00e+000  1.665300370e+002  1.665307945e+002  1.7e-010 1.92  
86  2.9e-007 8.0e-003 1.8e-005 1.00e+000  1.665300877e+002  1.665307694e+002  1.5e-010 1.94  
87  2.6e-007 8.0e-003 1.6e-005 9.97e-001  1.665301333e+002  1.665307470e+002  1.3e-010 1.97  
88  2.3e-007 7.9e-003 1.5e-005 1.00e+000  1.665301744e+002  1.665307266e+002  1.2e-010 1.98  
89  2.1e-007 7.9e-003 1.3e-005 1.00e+000  1.665302113e+002  1.665307083e+002  1.1e-010 2.01  
90  1.9e-007 7.9e-003 1.2e-005 1.00e+000  1.665302445e+002  1.665306918e+002  9.8e-011 2.03  
91  1.7e-007 7.9e-003 1.1e-005 9.89e-001  1.665302743e+002  1.665306771e+002  8.8e-011 2.04  
92  1.5e-007 7.9e-003 9.6e-006 9.99e-001  1.665303012e+002  1.665306638e+002  8.0e-011 2.08  
93  1.4e-007 7.8e-003 8.6e-006 9.95e-001  1.665303254e+002  1.665306518e+002  7.2e-011 2.09  
94  1.2e-007 7.8e-003 7.7e-006 1.00e+000  1.665303472e+002  1.665306409e+002  6.4e-011 2.11  
95  1.1e-007 7.8e-003 7.0e-006 9.99e-001  1.665303668e+002  1.665306311e+002  5.8e-011 2.14  
96  1.0e-007 7.8e-003 6.3e-006 1.00e+000  1.665303844e+002  1.665306223e+002  5.2e-011 2.15  
97  9.0e-008 7.7e-003 5.6e-006 9.94e-001  1.665304002e+002  1.665306144e+002  4.7e-011 2.17  
98  8.1e-008 7.0e-003 5.1e-006 1.01e+000  1.665304147e+002  1.665306071e+002  4.2e-011 2.20  
99  7.3e-008 6.3e-003 4.6e-006 9.93e-001  1.665304275e+002  1.665306008e+002  3.8e-011 2.22  
100 6.5e-008 5.6e-003 4.1e-006 1.01e+000  1.665304393e+002  1.665305948e+002  3.4e-011 2.23  
101 5.9e-008 5.1e-003 3.7e-006 9.83e-001  1.665304497e+002  1.665305897e+002  3.1e-011 2.26  
102 5.3e-008 4.6e-003 3.3e-006 9.94e-001  1.665304590e+002  1.665305851e+002  2.8e-011 2.28  
103 4.8e-008 4.1e-003 3.0e-006 9.91e-001  1.665304674e+002  1.665305809e+002  2.5e-011 2.29  
104 4.3e-008 3.7e-003 2.7e-006 9.96e-001  1.665304749e+002  1.665305771e+002  2.3e-011 2.33  
105 3.9e-008 3.3e-003 2.4e-006 1.00e+000  1.665304817e+002  1.665305737e+002  2.0e-011 2.34  
106 3.5e-008 3.0e-003 2.2e-006 9.90e-001  1.665304878e+002  1.665305706e+002  1.8e-011 2.36  
107 3.1e-008 2.7e-003 2.0e-006 9.88e-001  1.665304933e+002  1.665305679e+002  1.6e-011 2.37  
108 2.8e-008 2.4e-003 1.8e-006 9.94e-001  1.665304983e+002  1.665305654e+002  1.5e-011 2.40  
109 2.5e-008 2.2e-003 1.6e-006 9.72e-001  1.665305027e+002  1.665305632e+002  1.3e-011 2.42  
110 2.3e-008 2.0e-003 1.4e-006 1.04e+000  1.665305074e+002  1.665305608e+002  1.2e-011 2.43  
111 2.1e-008 1.8e-003 1.3e-006 1.05e+000  1.665305118e+002  1.665305585e+002  1.1e-011 2.46  
112 1.8e-008 1.6e-003 1.2e-006 1.00e+000  1.665305149e+002  1.665305569e+002  1.0e-011 2.48  
113 1.7e-008 1.4e-003 1.0e-006 1.07e+000  1.665305186e+002  1.665305550e+002  9.4e-012 2.50  
114 1.5e-008 1.3e-003 9.4e-007 1.04e+000  1.665305215e+002  1.665305535e+002  8.7e-012 2.53  
115 1.4e-008 1.2e-003 8.5e-007 1.01e+000  1.665305237e+002  1.665305524e+002  7.8e-012 2.54  
116 1.2e-008 1.0e-003 7.6e-007 9.80e-001  1.665305256e+002  1.665305515e+002  7.1e-012 2.56  
117 1.1e-008 9.4e-004 6.9e-007 9.40e-001  1.665305273e+002  1.665305507e+002  6.4e-012 2.57  
118 9.9e-009 8.5e-004 6.2e-007 8.60e-001  1.665305288e+002  1.665305501e+002  5.7e-012 2.61  
119 8.9e-009 7.6e-004 5.6e-007 9.51e-001  1.665305302e+002  1.665305494e+002  5.2e-012 2.62  
120 8.0e-009 6.9e-004 5.0e-007 1.09e+000  1.665305320e+002  1.665305484e+002  4.8e-012 2.64  
121 7.2e-009 6.2e-004 4.5e-007 9.84e-001  1.665305331e+002  1.665305479e+002  4.4e-012 2.67  
122 6.5e-009 5.6e-004 4.1e-007 9.02e-001  1.665305341e+002  1.665305474e+002  3.9e-012 2.68  
123 5.9e-009 5.0e-004 3.6e-007 8.92e-001  1.665305349e+002  1.665305470e+002  3.5e-012 2.71  
124 5.3e-009 4.5e-004 3.3e-007 1.23e+000  1.665305358e+002  1.665305465e+002  3.2e-012 2.73  
125 4.7e-009 4.1e-004 3.0e-007 9.97e-001  1.665305365e+002  1.665305462e+002  2.9e-012 2.76  
126 4.3e-009 3.7e-004 2.7e-007 9.66e-001  1.665305371e+002  1.665305458e+002  2.6e-012 2.78  
127 4.0e-009 3.3e-004 2.4e-007 1.73e+000  1.665305378e+002  1.665305453e+002  2.3e-012 2.79  
128 3.6e-009 3.0e-004 2.2e-007 9.79e-001  1.665305383e+002  1.665305451e+002  2.1e-012 2.82  
129 3.6e-009 2.7e-004 1.9e-007 1.90e+000  1.665305388e+002  1.665305447e+002  1.9e-012 2.84  
130 3.3e-009 2.4e-004 1.7e-007 1.06e+000  1.665305393e+002  1.665305444e+002  1.7e-012 2.87  
131 5.3e-010 2.4e-005 1.8e-008 9.77e-001  1.665305426e+002  1.665305431e+002  1.9e-013 2.90  
Interior-point optimizer terminated. Time: 2.90. 

Optimizer terminated. Time: 2.92    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6653054256e+002   Viol.  con: 9e-009   var: 0e+000 
  Dual.    obj: 1.6653054309e+002   Viol.  con: 0e+000   var: 1e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.95 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 936             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 769
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3440              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.01            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.46e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.286069770e+005 2.000000000e+000  1.0e+000 0.05  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.264280194e+005 3.575761900e+000  4.8e-001 0.08  
2   4.3e+002 5.5e+002 2.4e+004 -9.36e-001 -1.202642627e+005 1.018055693e+001  1.9e-001 0.09  
3   2.9e+002 3.7e+002 1.6e+004 -8.40e-001 -1.155864707e+005 6.348052521e+001  1.2e-001 0.14  
4   2.8e+002 3.7e+002 1.6e+004 -7.60e-001 -1.129604575e+005 2.275516326e+003  1.2e-001 0.17  
5   7.5e+001 9.6e+001 4.2e+003 -7.53e-001 -7.467564990e+004 9.661827672e+003  3.3e-002 0.20  
6   3.3e+001 4.2e+001 1.8e+003 -1.93e-001 -4.344556400e+004 1.030574624e+004  1.4e-002 0.22  
7   1.9e+001 2.5e+001 1.1e+003 3.43e-001  -2.866889632e+004 6.921959950e+003  8.5e-003 0.25  
8   1.1e+001 1.5e+001 6.3e+002 6.05e-001  -1.820598622e+004 4.395202865e+003  5.0e-003 0.28  
9   4.5e+000 5.8e+000 2.5e+002 7.73e-001  -7.371169122e+003 2.103309466e+003  2.0e-003 0.30  
10  2.1e+000 2.7e+000 1.2e+002 9.30e-001  -3.214989961e+003 1.325823009e+003  9.3e-004 0.33  
11  1.3e+000 1.7e+000 7.5e+001 9.81e-001  -2.014768597e+003 8.899280405e+002  6.0e-004 0.34  
12  8.1e-001 1.0e+000 4.5e+001 9.84e-001  -1.165870766e+003 6.060224825e+002  3.6e-004 0.37  
13  6.4e-001 8.5e-001 3.6e+001 9.55e-001  -9.120511289e+002 5.060747563e+002  2.9e-004 0.39  
14  3.6e-001 4.9e-001 2.0e+001 9.93e-001  -4.191573995e+002 3.802510508e+002  1.6e-004 0.42  
15  1.8e-001 2.4e-001 1.0e+001 9.93e-001  -1.346794360e+002 2.582566953e+002  8.0e-005 0.45  
16  7.9e-002 1.4e-001 4.6e+000 1.01e+000  2.126778969e+001  1.996180346e+002  3.7e-005 0.47  
17  6.8e-002 1.2e-001 3.9e+000 1.02e+000  4.474501802e+001  1.978721674e+002  3.2e-005 0.50  
18  2.8e-002 7.4e-002 1.6e+000 1.02e+000  1.178043198e+002  1.806433133e+002  1.3e-005 0.51  
19  8.1e-003 2.0e-001 4.7e-001 1.01e+000  1.531908827e+002  1.714402349e+002  3.8e-006 0.55  
20  2.9e-003 2.3e-001 1.7e-001 1.00e+000  1.613912476e+002  1.680581928e+002  1.4e-006 0.58  
21  1.7e-003 1.4e-001 1.0e-001 1.01e+000  1.635874339e+002  1.674597102e+002  8.2e-007 0.59  
22  5.0e-004 1.2e-001 3.1e-002 1.01e+000  1.656228581e+002  1.668056673e+002  2.5e-007 0.62  
23  1.9e-004 1.0e-001 1.2e-002 1.01e+000  1.661602516e+002  1.666051019e+002  9.7e-008 0.64  
24  8.5e-005 8.7e-002 5.4e-003 1.01e+000  1.663313691e+002  1.665357293e+002  4.5e-008 0.67  
25  3.9e-005 7.9e-002 2.5e-003 1.01e+000  1.664099173e+002  1.665032839e+002  2.1e-008 0.70  
26  3.5e-005 7.2e-002 2.2e-003 1.01e+000  1.664180551e+002  1.665021095e+002  1.9e-008 0.72  
27  3.1e-005 6.6e-002 2.0e-003 1.01e+000  1.664237665e+002  1.664993866e+002  1.7e-008 0.75  
28  2.8e-005 6.0e-002 1.8e-003 1.01e+000  1.664290350e+002  1.664970786e+002  1.5e-008 0.76  
29  2.5e-005 5.5e-002 1.6e-003 1.01e+000  1.664337489e+002  1.664949754e+002  1.4e-008 0.80  
30  2.3e-005 5.0e-002 1.5e-003 1.01e+000  1.664379861e+002  1.664930797e+002  1.2e-008 0.81  
31  2.1e-005 4.6e-002 1.3e-003 1.00e+000  1.664417920e+002  1.664913678e+002  1.1e-008 0.84  
32  1.8e-005 4.2e-002 1.2e-003 1.00e+000  1.664452114e+002  1.664898228e+002  1.0e-008 0.86  
33  1.7e-005 3.9e-002 1.1e-003 1.00e+000  1.664482838e+002  1.664884286e+002  9.0e-009 0.89  
34  1.5e-005 3.6e-002 9.6e-004 1.00e+000  1.664510449e+002  1.664871706e+002  8.1e-009 0.92  
35  1.3e-005 3.3e-002 8.6e-004 1.00e+000  1.664535263e+002  1.664860359e+002  7.3e-009 0.94  
36  1.2e-005 3.0e-002 7.8e-004 1.00e+000  1.664557566e+002  1.664850123e+002  6.5e-009 0.97  
37  1.1e-005 2.8e-002 7.0e-004 1.00e+000  1.664577616e+002  1.664840893e+002  5.9e-009 0.98  
38  9.8e-006 2.6e-002 6.3e-004 1.00e+000  1.664595641e+002  1.664832571e+002  5.3e-009 1.01  
39  8.8e-006 2.4e-002 5.7e-004 1.00e+000  1.664611847e+002  1.664825069e+002  4.8e-009 1.03  
40  8.0e-006 2.3e-002 5.1e-004 1.00e+000  1.664626419e+002  1.664818307e+002  4.3e-009 1.06  
41  7.2e-006 2.1e-002 4.6e-004 1.00e+000  1.664639524e+002  1.664812213e+002  3.9e-009 1.08  
42  6.4e-006 2.0e-002 4.1e-004 1.00e+000  1.664651309e+002  1.664806722e+002  3.5e-009 1.09  
43  5.8e-006 1.9e-002 3.7e-004 1.00e+000  1.664661909e+002  1.664801775e+002  3.1e-009 1.12  
44  5.2e-006 1.7e-002 3.3e-004 1.00e+000  1.664671444e+002  1.664797318e+002  2.8e-009 1.14  
45  4.7e-006 1.6e-002 3.0e-004 1.00e+000  1.664680020e+002  1.664793303e+002  2.5e-009 1.17  
46  4.2e-006 1.6e-002 2.7e-004 1.00e+000  1.664687735e+002  1.664789687e+002  2.3e-009 1.19  
47  3.8e-006 1.5e-002 2.4e-004 1.00e+000  1.664694675e+002  1.664786429e+002  2.1e-009 1.20  
48  3.4e-006 1.4e-002 2.2e-004 1.00e+000  1.664700918e+002  1.664783495e+002  1.8e-009 1.23  
49  3.1e-006 1.3e-002 2.0e-004 1.00e+000  1.664706534e+002  1.664780852e+002  1.7e-009 1.25  
50  2.8e-006 1.3e-002 1.8e-004 1.00e+000  1.664711587e+002  1.664778471e+002  1.5e-009 1.26  
51  2.5e-006 1.2e-002 1.6e-004 1.00e+000  1.664716132e+002  1.664776328e+002  1.3e-009 1.29  
52  2.2e-006 1.2e-002 1.4e-004 1.00e+000  1.664720222e+002  1.664774397e+002  1.2e-009 1.31  
53  2.0e-006 1.1e-002 1.3e-004 1.00e+000  1.664723903e+002  1.664772660e+002  1.1e-009 1.33  
54  1.8e-006 1.1e-002 1.2e-004 1.00e+000  1.664727215e+002  1.664771096e+002  9.8e-010 1.36  
55  1.6e-006 1.1e-002 1.0e-004 1.00e+000  1.664730195e+002  1.664769688e+002  8.8e-010 1.37  
56  1.5e-006 1.0e-002 9.4e-005 1.00e+000  1.664732878e+002  1.664768420e+002  8.0e-010 1.39  
57  1.3e-006 1.0e-002 8.5e-005 1.00e+000  1.664735292e+002  1.664767280e+002  7.2e-010 1.47  
58  1.2e-006 9.9e-003 7.6e-005 1.00e+000  1.664737464e+002  1.664766253e+002  6.5e-010 1.50  
59  1.1e-006 9.6e-003 6.9e-005 1.00e+000  1.664739419e+002  1.664765329e+002  5.8e-010 1.51  
60  9.7e-007 9.4e-003 6.2e-005 1.00e+000  1.664741178e+002  1.664764497e+002  5.2e-010 1.53  
61  8.7e-007 9.2e-003 5.6e-005 1.00e+000  1.664742761e+002  1.664763748e+002  4.7e-010 1.56  
62  7.8e-007 9.1e-003 5.0e-005 1.00e+000  1.664744185e+002  1.664763074e+002  4.2e-010 1.58  
63  7.1e-007 8.9e-003 4.5e-005 1.00e+000  1.664745467e+002  1.664762467e+002  3.8e-010 1.61  
64  6.3e-007 8.8e-003 4.1e-005 1.00e+000  1.664746620e+002  1.664761920e+002  3.4e-010 1.62  
65  5.7e-007 8.7e-003 3.7e-005 1.00e+000  1.664747658e+002  1.664761427e+002  3.1e-010 1.64  
66  5.1e-007 8.6e-003 3.3e-005 1.00e+000  1.664748591e+002  1.664760983e+002  2.8e-010 1.67  
67  4.6e-007 8.5e-003 3.0e-005 1.00e+000  1.664749431e+002  1.664760584e+002  2.5e-010 1.68  
68  4.2e-007 8.4e-003 2.7e-005 1.00e+000  1.664750186e+002  1.664760223e+002  2.3e-010 1.70  
69  3.7e-007 8.3e-003 2.4e-005 1.00e+000  1.664750865e+002  1.664759899e+002  2.0e-010 1.73  
70  3.4e-007 8.2e-003 2.2e-005 9.99e-001  1.664751476e+002  1.664759607e+002  1.8e-010 1.75  
71  3.0e-007 8.2e-003 1.9e-005 1.00e+000  1.664752026e+002  1.664759343e+002  1.6e-010 1.76  
72  2.7e-007 8.1e-003 1.7e-005 1.00e+000  1.664752521e+002  1.664759106e+002  1.5e-010 1.79  
73  2.5e-007 8.1e-003 1.6e-005 9.99e-001  1.664752966e+002  1.664758893e+002  1.3e-010 1.81  
74  2.2e-007 8.0e-003 1.4e-005 1.00e+000  1.664753366e+002  1.664758700e+002  1.2e-010 1.83  
75  2.0e-007 8.0e-003 1.3e-005 1.00e+000  1.664753726e+002  1.664758527e+002  1.1e-010 1.86  
76  1.8e-007 7.9e-003 1.1e-005 1.00e+000  1.664754050e+002  1.664758371e+002  9.7e-011 1.87  
77  1.6e-007 7.9e-003 1.0e-005 1.00e+000  1.664754342e+002  1.664758231e+002  8.7e-011 1.90  
78  1.5e-007 7.8e-003 9.3e-006 9.98e-001  1.664754605e+002  1.664758104e+002  7.8e-011 1.92  
79  1.3e-007 7.8e-003 8.4e-006 1.00e+000  1.664754841e+002  1.664757991e+002  7.1e-011 1.93  
80  1.2e-007 7.8e-003 7.5e-006 1.00e+000  1.664755054e+002  1.664757887e+002  6.4e-011 1.97  
81  1.1e-007 7.8e-003 6.8e-006 9.97e-001  1.664755245e+002  1.664757795e+002  5.7e-011 1.98  
82  9.5e-008 7.7e-003 6.1e-006 1.00e+000  1.664755417e+002  1.664757712e+002  5.2e-011 2.00  
83  8.6e-008 7.7e-003 5.5e-006 1.00e+000  1.664755572e+002  1.664757638e+002  4.6e-011 2.03  
84  7.7e-008 7.7e-003 4.9e-006 1.00e+000  1.664755711e+002  1.664757570e+002  4.2e-011 2.06  
85  6.9e-008 7.6e-003 4.4e-006 9.91e-001  1.664755837e+002  1.664757510e+002  3.8e-011 2.07  
86  6.2e-008 7.6e-003 4.0e-006 1.00e+000  1.664755949e+002  1.664757456e+002  3.4e-011 2.11  
87  5.6e-008 7.6e-003 3.6e-006 9.94e-001  1.664756051e+002  1.664757407e+002  3.0e-011 2.12  
88  5.1e-008 6.8e-003 3.2e-006 1.01e+000  1.664756145e+002  1.664757361e+002  2.7e-011 2.14  
89  4.6e-008 6.2e-003 2.9e-006 1.00e+000  1.664756228e+002  1.664757321e+002  2.5e-011 2.17  
90  4.1e-008 5.5e-003 2.6e-006 1.01e+000  1.664756304e+002  1.664757284e+002  2.2e-011 2.18  
91  3.7e-008 5.0e-003 2.4e-006 1.00e+000  1.664756370e+002  1.664757252e+002  2.0e-011 2.21  
92  3.3e-008 4.5e-003 2.1e-006 1.01e+000  1.664756430e+002  1.664757223e+002  1.8e-011 2.23  
93  3.0e-008 4.0e-003 1.9e-006 1.01e+000  1.664756485e+002  1.664757196e+002  1.6e-011 2.25  
94  2.7e-008 3.6e-003 1.7e-006 9.73e-001  1.664756532e+002  1.664757174e+002  1.5e-011 2.28  
95  2.4e-008 3.3e-003 1.6e-006 1.02e+000  1.664756579e+002  1.664757151e+002  1.3e-011 2.29  
96  2.2e-008 2.9e-003 1.4e-006 9.96e-001  1.664756617e+002  1.664757132e+002  1.2e-011 2.31  
97  2.0e-008 2.7e-003 1.3e-006 1.01e+000  1.664756654e+002  1.664757115e+002  1.1e-011 2.34  
98  1.8e-008 2.4e-003 1.1e-006 1.02e+000  1.664756687e+002  1.664757098e+002  9.8e-012 2.36  
99  1.6e-008 2.1e-003 1.0e-006 1.02e+000  1.664756717e+002  1.664757084e+002  8.9e-012 2.39  
100 1.4e-008 1.9e-003 9.2e-007 1.02e+000  1.664756744e+002  1.664757070e+002  8.1e-012 2.40  
101 1.3e-008 1.7e-003 8.2e-007 9.72e-001  1.664756766e+002  1.664757060e+002  7.3e-012 2.42  
102 1.2e-008 1.6e-003 7.4e-007 1.02e+000  1.664756787e+002  1.664757050e+002  6.6e-012 2.45  
103 1.0e-008 1.4e-003 6.7e-007 1.00e+000  1.664756805e+002  1.664757041e+002  6.0e-012 2.46  
104 9.4e-009 1.3e-003 6.0e-007 1.06e+000  1.664756825e+002  1.664757031e+002  5.5e-012 2.48  
105 3.0e-009 1.3e-004 6.2e-008 9.82e-001  1.664756951e+002  1.664756972e+002  6.1e-013 2.51  
Interior-point optimizer terminated. Time: 2.51. 

Optimizer terminated. Time: 2.53    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6647569509e+002   Viol.  con: 8e-008   var: 0e+000 
  Dual.    obj: 1.6647569721e+002   Viol.  con: 0e+000   var: 8e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.55 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 936             
Lin. dep.  - tries                  : 1                 time                   : 0.02            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.02    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 769
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3439              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.05              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.46e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.285358117e+005 2.000000000e+000  1.0e+000 0.06  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.263542085e+005 3.574445480e+000  4.8e-001 0.09  
2   4.3e+002 5.5e+002 2.4e+004 -9.36e-001 -1.201588476e+005 1.021567204e+001  1.9e-001 0.13  
3   2.9e+002 3.7e+002 1.6e+004 -8.39e-001 -1.154718918e+005 6.399967500e+001  1.2e-001 0.14  
4   2.8e+002 3.7e+002 1.6e+004 -7.59e-001 -1.128613766e+005 2.263785743e+003  1.2e-001 0.17  
5   7.5e+001 9.7e+001 4.2e+003 -7.52e-001 -7.480742550e+004 9.600133203e+003  3.3e-002 0.20  
6   3.0e+001 3.9e+001 1.7e+003 -1.96e-001 -4.068261326e+004 1.026881509e+004  1.3e-002 0.22  
7   1.8e+001 2.3e+001 1.0e+003 3.91e-001  -2.712656131e+004 6.680855315e+003  7.9e-003 0.25  
8   9.7e+000 1.2e+001 5.4e+002 6.31e-001  -1.569362005e+004 3.889215582e+003  4.3e-003 0.27  
9   3.9e+000 5.0e+000 2.2e+002 8.12e-001  -6.429970792e+003 1.893874007e+003  1.7e-003 0.30  
10  2.1e+000 2.7e+000 1.2e+002 9.41e-001  -3.286677032e+003 1.204165219e+003  9.2e-004 0.33  
11  1.0e+000 1.3e+000 5.9e+001 9.80e-001  -1.544943804e+003 7.355125157e+002  4.7e-004 0.34  
12  8.1e-001 1.0e+000 4.5e+001 9.78e-001  -1.184098380e+003 6.013199113e+002  3.6e-004 0.38  
13  4.8e-001 6.2e-001 2.7e+001 9.74e-001  -6.380902206e+002 4.207580323e+002  2.1e-004 0.39  
14  2.6e-001 3.6e-001 1.5e+001 1.00e+000  -2.718696692e+002 3.084890132e+002  1.2e-004 0.42  
15  9.7e-002 1.5e-001 5.5e+000 1.00e+000  -1.010318706e+001 2.072405059e+002  4.5e-005 0.45  
16  8.6e-002 1.3e-001 4.9e+000 1.02e+000  1.582576693e+001  2.085964054e+002  4.0e-005 0.47  
17  5.3e-002 8.8e-002 3.1e+000 1.02e+000  7.253972466e+001  1.918847502e+002  2.5e-005 0.50  
18  2.3e-002 6.9e-002 1.3e+000 1.02e+000  1.266761042e+002  1.778039792e+002  1.1e-005 0.52  
19  6.2e-003 2.3e-001 3.7e-001 1.01e+000  1.562550550e+002  1.702791212e+002  2.9e-006 0.55  
20  3.1e-003 3.1e-001 1.8e-001 1.00e+000  1.610362877e+002  1.681100435e+002  1.5e-006 0.56  
21  1.6e-003 1.7e-001 9.8e-002 1.01e+000  1.636144561e+002  1.673813822e+002  8.0e-007 0.59  
22  4.9e-004 1.4e-001 3.0e-002 1.01e+000  1.656242739e+002  1.667725326e+002  2.5e-007 0.61  
23  3.1e-004 1.1e-001 1.9e-002 9.98e-001  1.659258651e+002  1.666521402e+002  1.6e-007 0.64  
24  1.9e-004 7.7e-002 1.2e-002 9.85e-001  1.661267262e+002  1.665737789e+002  9.7e-008 0.66  
25  1.7e-004 6.6e-002 1.0e-002 9.99e-001  1.661696462e+002  1.665612797e+002  8.5e-008 0.67  
26  1.5e-004 6.0e-002 9.3e-003 1.01e+000  1.661982639e+002  1.665504923e+002  7.7e-008 0.70  
27  1.3e-004 5.5e-002 8.4e-003 1.01e+000  1.662230820e+002  1.665399599e+002  6.9e-008 0.72  
28  1.2e-004 5.0e-002 7.5e-003 1.01e+000  1.662455581e+002  1.665306802e+002  6.2e-008 0.75  
29  1.1e-004 4.6e-002 6.8e-003 1.01e+000  1.662656944e+002  1.665222483e+002  5.6e-008 0.77  
30  9.8e-005 4.2e-002 6.1e-003 1.01e+000  1.662837683e+002  1.665146214e+002  5.0e-008 0.78  
31  8.8e-005 3.8e-002 5.5e-003 1.01e+000  1.662999867e+002  1.665077177e+002  4.5e-008 0.81  
32  7.9e-005 3.5e-002 4.9e-003 1.01e+000  1.663145419e+002  1.665014700e+002  4.1e-008 0.83  
33  7.1e-005 3.3e-002 4.4e-003 1.00e+000  1.663276049e+002  1.664958163e+002  3.7e-008 0.86  
34  6.4e-005 3.0e-002 4.0e-003 1.00e+000  1.663393297e+002  1.664907007e+002  3.3e-008 0.87  
35  5.8e-005 2.8e-002 3.6e-003 1.00e+000  1.663498543e+002  1.664860728e+002  3.0e-008 0.89  
36  5.2e-005 2.6e-002 3.2e-003 1.00e+000  1.663593025e+002  1.664818869e+002  2.7e-008 0.92  
37  4.7e-005 2.4e-002 2.9e-003 1.00e+000  1.663677854e+002  1.664781016e+002  2.4e-008 0.94  
38  4.2e-005 2.2e-002 2.6e-003 1.00e+000  1.663754023e+002  1.664746792e+002  2.2e-008 0.95  
39  3.8e-005 2.1e-002 2.4e-003 1.00e+000  1.663822424e+002  1.664715855e+002  2.0e-008 0.98  
40  3.4e-005 1.9e-002 2.1e-003 1.00e+000  1.663883855e+002  1.664687895e+002  1.8e-008 1.00  
41  3.1e-005 1.8e-002 1.9e-003 1.00e+000  1.663939031e+002  1.664662630e+002  1.6e-008 1.03  
42  2.8e-005 1.7e-002 1.7e-003 1.00e+000  1.663988594e+002  1.664639804e+002  1.4e-008 1.05  
43  2.5e-005 1.6e-002 1.6e-003 1.00e+000  1.664033117e+002  1.664619183e+002  1.3e-008 1.08  
44  2.2e-005 1.5e-002 1.4e-003 1.00e+000  1.664073115e+002  1.664600558e+002  1.2e-008 1.09  
45  2.0e-005 1.5e-002 1.3e-003 1.00e+000  1.664109052e+002  1.664583737e+002  1.0e-008 1.12  
46  1.8e-005 1.4e-002 1.1e-003 1.00e+000  1.664141341e+002  1.664568547e+002  9.4e-009 1.14  
47  1.6e-005 1.3e-002 1.0e-003 1.00e+000  1.664170354e+002  1.664554832e+002  8.4e-009 1.16  
48  1.5e-005 1.3e-002 9.2e-004 1.00e+000  1.664196426e+002  1.664542451e+002  7.6e-009 1.19  
49  1.3e-005 1.2e-002 8.2e-004 1.00e+000  1.664219856e+002  1.664531274e+002  6.8e-009 1.20  
50  1.2e-005 1.2e-002 7.4e-004 1.00e+000  1.664240914e+002  1.664521187e+002  6.2e-009 1.23  
51  1.1e-005 1.1e-002 6.7e-004 1.00e+000  1.664259840e+002  1.664512085e+002  5.5e-009 1.25  
52  9.6e-006 1.1e-002 6.0e-004 1.00e+000  1.664276853e+002  1.664503871e+002  5.0e-009 1.26  
53  8.6e-006 1.1e-002 5.4e-004 1.00e+000  1.664292145e+002  1.664496462e+002  4.5e-009 1.28  
54  7.8e-006 1.0e-002 4.9e-004 1.00e+000  1.664305893e+002  1.664489778e+002  4.0e-009 1.31  
55  7.0e-006 1.0e-002 4.4e-004 1.00e+000  1.664318253e+002  1.664483749e+002  3.6e-009 1.33  
56  6.3e-006 9.9e-003 3.9e-004 1.00e+000  1.664329365e+002  1.664478313e+002  3.3e-009 1.36  
57  5.7e-006 9.7e-003 3.5e-004 1.00e+000  1.664339357e+002  1.664473410e+002  2.9e-009 1.37  
58  5.1e-006 9.6e-003 3.2e-004 1.00e+000  1.664348341e+002  1.664468990e+002  2.7e-009 1.39  
59  4.6e-006 9.4e-003 2.9e-004 1.00e+000  1.664356420e+002  1.664465004e+002  2.4e-009 1.42  
60  4.1e-006 9.2e-003 2.6e-004 1.00e+000  1.664363684e+002  1.664461411e+002  2.1e-009 1.44  
61  3.7e-006 9.1e-003 2.3e-004 1.00e+000  1.664370216e+002  1.664458171e+002  1.9e-009 1.45  
62  3.3e-006 9.0e-003 2.1e-004 1.00e+000  1.664376090e+002  1.664455250e+002  1.7e-009 1.48  
63  3.0e-006 8.9e-003 1.9e-004 1.00e+000  1.664381373e+002  1.664452617e+002  1.6e-009 1.50  
64  2.7e-006 8.7e-003 1.7e-004 1.00e+000  1.664386123e+002  1.664450244e+002  1.4e-009 1.51  
65  2.4e-006 8.7e-003 1.5e-004 1.00e+000  1.664390396e+002  1.664448105e+002  1.3e-009 1.54  
66  2.2e-006 8.6e-003 1.4e-004 1.00e+000  1.664394239e+002  1.664446178e+002  1.1e-009 1.56  
67  2.0e-006 8.5e-003 1.2e-004 1.00e+000  1.664397697e+002  1.664444442e+002  1.0e-009 1.58  
68  1.8e-006 8.4e-003 1.1e-004 1.00e+000  1.664400807e+002  1.664442879e+002  9.3e-010 1.61  
69  1.6e-006 8.3e-003 1.0e-004 1.00e+000  1.664403605e+002  1.664441470e+002  8.3e-010 1.62  
70  1.4e-006 8.3e-003 9.0e-005 1.00e+000  1.664406122e+002  1.664440201e+002  7.5e-010 1.65  
71  1.3e-006 8.2e-003 8.1e-005 1.00e+000  1.664408387e+002  1.664439059e+002  6.7e-010 1.67  
72  1.2e-006 8.2e-003 7.3e-005 1.00e+000  1.664410425e+002  1.664438029e+002  6.1e-010 1.69  
73  1.1e-006 8.1e-003 6.6e-005 1.00e+000  1.664412258e+002  1.664437102e+002  5.5e-010 1.72  
74  9.5e-007 8.1e-003 5.9e-005 1.00e+000  1.664413907e+002  1.664436267e+002  4.9e-010 1.73  
75  8.5e-007 8.0e-003 5.3e-005 1.00e+000  1.664415391e+002  1.664435515e+002  4.4e-010 1.75  
76  7.7e-007 8.0e-003 4.8e-005 1.00e+000  1.664416726e+002  1.664434837e+002  4.0e-010 1.78  
77  6.9e-007 7.9e-003 4.3e-005 1.00e+000  1.664417927e+002  1.664434227e+002  3.6e-010 1.79  
78  6.2e-007 7.9e-003 3.9e-005 1.00e+000  1.664419007e+002  1.664433677e+002  3.2e-010 1.81  
79  5.6e-007 7.9e-003 3.5e-005 1.00e+000  1.664419979e+002  1.664433182e+002  2.9e-010 1.84  
80  5.0e-007 7.8e-003 3.1e-005 1.00e+000  1.664420853e+002  1.664432736e+002  2.6e-010 1.86  
81  4.5e-007 7.8e-003 2.8e-005 1.00e+000  1.664421639e+002  1.664432334e+002  2.4e-010 1.87  
82  4.1e-007 7.8e-003 2.5e-005 1.00e+000  1.664422347e+002  1.664431972e+002  2.1e-010 1.90  
83  3.7e-007 7.8e-003 2.3e-005 1.00e+000  1.664422983e+002  1.664431646e+002  1.9e-010 1.92  
84  3.3e-007 7.7e-003 2.1e-005 1.00e+000  1.664423556e+002  1.664431352e+002  1.7e-010 1.94  
85  3.0e-007 7.7e-003 1.9e-005 1.00e+000  1.664424071e+002  1.664431088e+002  1.5e-010 1.97  
86  2.7e-007 7.7e-003 1.7e-005 9.98e-001  1.664424535e+002  1.664430851e+002  1.4e-010 1.98  
87  2.4e-007 7.7e-003 1.5e-005 9.99e-001  1.664424952e+002  1.664430637e+002  1.3e-010 2.00  
88  2.2e-007 7.7e-003 1.4e-005 9.99e-001  1.664425328e+002  1.664430444e+002  1.1e-010 2.03  
89  1.9e-007 7.6e-003 1.2e-005 9.99e-001  1.664425666e+002  1.664430270e+002  1.0e-010 2.04  
90  1.8e-007 7.6e-003 1.1e-005 1.00e+000  1.664425970e+002  1.664430114e+002  9.1e-011 2.06  
91  1.6e-007 7.6e-003 9.9e-006 1.00e+000  1.664426244e+002  1.664429973e+002  8.2e-011 2.09  
92  1.4e-007 7.6e-003 8.9e-006 1.00e+000  1.664426490e+002  1.664429847e+002  7.4e-011 2.12  
93  1.3e-007 7.6e-003 8.0e-006 1.00e+000  1.664426712e+002  1.664429732e+002  6.6e-011 2.14  
94  1.2e-007 7.6e-003 7.2e-006 1.00e+000  1.664426912e+002  1.664429629e+002  6.0e-011 2.15  
95  1.0e-007 7.6e-003 6.5e-006 9.98e-001  1.664427091e+002  1.664429538e+002  5.4e-011 2.18  
96  9.3e-008 7.5e-003 5.8e-006 9.98e-001  1.664427253e+002  1.664429455e+002  4.8e-011 2.20  
97  8.4e-008 7.5e-003 5.2e-006 9.94e-001  1.664427398e+002  1.664429381e+002  4.4e-011 2.23  
98  7.5e-008 6.8e-003 4.7e-006 1.00e+000  1.664427529e+002  1.664429313e+002  3.9e-011 2.25  
99  6.8e-008 6.1e-003 4.3e-006 1.00e+000  1.664427647e+002  1.664429252e+002  3.5e-011 2.26  
100 6.1e-008 5.5e-003 3.8e-006 1.01e+000  1.664427755e+002  1.664429197e+002  3.2e-011 2.29  
101 5.5e-008 4.9e-003 3.4e-006 9.92e-001  1.664427851e+002  1.664429148e+002  2.9e-011 2.31  
102 4.9e-008 4.4e-003 3.1e-006 9.98e-001  1.664427936e+002  1.664429104e+002  2.6e-011 2.33  
103 4.5e-008 4.0e-003 2.8e-006 1.01e+000  1.664428016e+002  1.664429063e+002  2.3e-011 2.36  
104 4.0e-008 3.6e-003 2.5e-006 9.94e-001  1.664428085e+002  1.664429028e+002  2.1e-011 2.37  
105 3.6e-008 3.2e-003 2.3e-006 9.92e-001  1.664428147e+002  1.664428996e+002  1.9e-011 2.39  
106 3.2e-008 2.9e-003 2.0e-006 1.01e+000  1.664428204e+002  1.664428967e+002  1.7e-011 2.42  
107 2.9e-008 2.6e-003 1.8e-006 1.02e+000  1.664428258e+002  1.664428939e+002  1.5e-011 2.43  
108 2.6e-008 2.4e-003 1.6e-006 1.03e+000  1.664428308e+002  1.664428913e+002  1.4e-011 2.45  
109 2.4e-008 2.1e-003 1.5e-006 1.02e+000  1.664428351e+002  1.664428890e+002  1.3e-011 2.48  
110 2.1e-008 1.9e-003 1.3e-006 1.06e+000  1.664428396e+002  1.664428866e+002  1.2e-011 2.50  
111 1.9e-008 1.7e-003 1.2e-006 9.86e-001  1.664428427e+002  1.664428851e+002  1.1e-011 2.51  
112 1.7e-008 1.5e-003 1.1e-006 1.02e+000  1.664428457e+002  1.664428835e+002  9.6e-012 2.54  
113 1.6e-008 1.4e-003 9.7e-007 1.08e+000  1.664428492e+002  1.664428816e+002  9.0e-012 2.56  
114 1.4e-008 1.3e-003 8.8e-007 1.02e+000  1.664428515e+002  1.664428805e+002  8.2e-012 2.57  
115 1.3e-008 1.1e-003 7.9e-007 9.43e-001  1.664428534e+002  1.664428795e+002  7.3e-012 2.61  
116 1.2e-008 1.0e-003 7.1e-007 1.09e+000  1.664428559e+002  1.664428781e+002  6.9e-012 2.62  
117 1.1e-008 9.1e-004 6.4e-007 1.03e+000  1.664428576e+002  1.664428773e+002  6.3e-012 2.64  
118 1.0e-008 8.2e-004 5.7e-007 1.03e+000  1.664428591e+002  1.664428765e+002  5.7e-012 2.67  
119 9.2e-009 7.4e-004 5.2e-007 8.75e-001  1.664428603e+002  1.664428760e+002  5.2e-012 2.68  
120 8.3e-009 6.7e-004 4.7e-007 7.91e-001  1.664428613e+002  1.664428755e+002  4.7e-012 2.70  
121 9.1e-009 6.0e-004 4.2e-007 1.04e+000  1.664428624e+002  1.664428749e+002  4.3e-012 2.73  
122 8.9e-009 5.4e-004 3.8e-007 5.48e-001  1.664428634e+002  1.664428742e+002  3.8e-012 2.75  
123 1.3e-008 4.9e-004 3.4e-007 1.03e+000  1.664428642e+002  1.664428738e+002  3.5e-012 2.78  
124 1.2e-008 4.4e-004 3.1e-007 9.46e-001  1.664428649e+002  1.664428735e+002  3.1e-012 2.79  
125 1.5e-008 3.9e-004 2.7e-007 1.09e+000  1.664428657e+002  1.664428731e+002  3.0e-012 2.81  
126 1.2e-008 3.5e-004 2.5e-007 5.62e-001  1.664428663e+002  1.664428727e+002  2.6e-012 2.84  
127 1.2e-008 3.2e-004 2.2e-007 4.67e-001  1.664428667e+002  1.664428727e+002  2.4e-012 2.86  
128 9.1e-009 2.9e-004 2.0e-007 4.58e+000  1.664428672e+002  1.664428722e+002  2.1e-012 2.87  
129 9.8e-009 2.6e-004 1.8e-007 4.49e-001  1.664428675e+002  1.664428722e+002  1.9e-012 2.90  
130 7.2e-009 2.3e-004 1.6e-007 1.44e+000  1.664428679e+002  1.664428720e+002  1.7e-012 2.92  
131 1.1e-008 2.1e-004 1.5e-007 5.95e-001  1.664428681e+002  1.664428720e+002  1.5e-012 2.95  
132 1.1e-008 1.9e-004 1.3e-007 4.81e-001  1.664428684e+002  1.664428719e+002  1.4e-012 2.96  
133 1.0e-008 1.7e-004 1.2e-007 3.47e-001  1.664428686e+002  1.664428719e+002  1.3e-012 2.98  
134 1.9e-008 1.5e-004 1.1e-007 5.06e+000  1.664428689e+002  1.664428715e+002  1.1e-012 3.01  
135 2.6e-008 1.4e-004 1.2e-007 1.00e+000  1.664428685e+002  1.664428714e+002  9.9e-013 3.03  
Interior-point optimizer terminated. Time: 3.03. 

Optimizer terminated. Time: 3.04    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6644286854e+002   Viol.  con: 5e-007   var: 0e+000 
  Dual.    obj: 1.6644287143e+002   Viol.  con: 0e+000   var: 6e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.08 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 936             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 769
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3439              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.02            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.46e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.285340946e+005 2.000000000e+000  1.0e+000 0.06  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.263517281e+005 3.573621146e+000  4.8e-001 0.08  
2   4.3e+002 5.5e+002 2.4e+004 -9.36e-001 -1.201360051e+005 1.023272909e+001  1.8e-001 0.11  
3   2.9e+002 3.7e+002 1.6e+004 -8.39e-001 -1.154380590e+005 6.426647208e+001  1.2e-001 0.14  
4   2.8e+002 3.6e+002 1.6e+004 -7.59e-001 -1.128348628e+005 2.258319422e+003  1.2e-001 0.17  
5   7.5e+001 9.6e+001 4.1e+003 -7.52e-001 -7.471893770e+004 9.598234561e+003  3.3e-002 0.20  
6   3.0e+001 3.9e+001 1.7e+003 -1.95e-001 -4.050843656e+004 1.020870781e+004  1.3e-002 0.22  
7   1.8e+001 2.3e+001 1.0e+003 3.94e-001  -2.711070257e+004 6.648765634e+003  7.9e-003 0.25  
8   9.5e+000 1.2e+001 5.3e+002 6.30e-001  -1.542138348e+004 3.834872946e+003  4.2e-003 0.28  
9   3.6e+000 4.7e+000 2.0e+002 8.16e-001  -5.933740444e+003 1.798175583e+003  1.6e-003 0.31  
10  2.0e+000 2.6e+000 1.1e+002 9.47e-001  -3.130716156e+003 1.194464154e+003  8.9e-004 0.33  
11  8.4e-001 1.1e+000 4.7e+001 9.81e-001  -1.229433447e+003 6.158772227e+002  3.8e-004 0.36  
12  8.2e-001 1.1e+000 4.6e+001 9.50e-001  -1.213196727e+003 5.912544025e+002  3.7e-004 0.39  
13  5.1e-001 6.6e-001 2.9e+001 9.72e-001  -7.067537523e+002 4.266806667e+002  2.3e-004 0.42  
14  3.1e-001 4.2e-001 1.8e+001 1.00e+000  -3.527467675e+002 3.411029410e+002  1.4e-004 0.44  
15  1.1e-001 1.7e-001 6.1e+000 9.98e-001  -2.763223219e+001 2.143702446e+002  5.0e-005 0.47  
16  8.2e-002 1.3e-001 4.7e+000 1.02e+000  2.135828668e+001  2.045404312e+002  3.8e-005 0.50  
17  4.1e-002 8.3e-002 2.4e+000 1.02e+000  9.501305460e+001  1.868890709e+002  1.9e-005 0.52  
18  1.4e-002 8.3e-002 8.2e-001 1.02e+000  1.425011959e+002  1.741746608e+002  6.6e-006 0.55  
19  6.2e-003 7.2e-002 3.6e-001 1.01e+000  1.557117228e+002  1.695767424e+002  2.9e-006 0.58  
20  1.5e-003 1.6e-001 9.2e-002 1.01e+000  1.638758053e+002  1.673863654e+002  7.4e-007 0.61  
21  8.0e-004 1.1e-001 4.9e-002 9.78e-001  1.650618539e+002  1.669374382e+002  4.0e-007 0.62  
22  2.4e-004 1.1e-001 1.6e-002 9.90e-001  1.660030870e+002  1.665978756e+002  1.3e-007 0.66  
23  1.1e-004 8.9e-002 7.5e-003 1.01e+000  1.662212529e+002  1.665057714e+002  6.3e-008 0.69  
24  4.7e-005 8.5e-002 3.1e-003 1.01e+000  1.663394250e+002  1.664571335e+002  2.6e-008 0.70  
25  2.2e-005 7.7e-002 1.5e-003 1.01e+000  1.663835785e+002  1.664385514e+002  1.2e-008 0.73  
26  2.0e-005 7.1e-002 1.3e-003 1.00e+000  1.663881968e+002  1.664377016e+002  1.1e-008 0.76  
27  1.8e-005 6.4e-002 1.2e-003 1.01e+000  1.663915594e+002  1.664361007e+002  1.0e-008 0.78  
28  1.6e-005 5.9e-002 1.1e-003 1.00e+000  1.663946469e+002  1.664347272e+002  9.0e-009 0.81  
29  1.4e-005 5.4e-002 9.6e-004 1.00e+000  1.663974099e+002  1.664334760e+002  8.1e-009 0.84  
30  1.3e-005 4.9e-002 8.6e-004 1.00e+000  1.663998945e+002  1.664323491e+002  7.3e-009 0.86  
31  1.2e-005 4.5e-002 7.7e-004 1.00e+000  1.664021270e+002  1.664313321e+002  6.5e-009 0.89  
32  1.0e-005 4.1e-002 7.0e-004 1.00e+000  1.664041335e+002  1.664304148e+002  5.9e-009 0.91  
33  9.4e-006 3.8e-002 6.3e-004 1.00e+000  1.664059369e+002  1.664295874e+002  5.3e-009 0.94  
34  8.5e-006 3.5e-002 5.6e-004 1.00e+000  1.664075579e+002  1.664288412e+002  4.8e-009 0.95  
35  7.7e-006 3.2e-002 5.1e-004 1.00e+000  1.664090152e+002  1.664281683e+002  4.3e-009 0.97  
36  6.9e-006 3.0e-002 4.6e-004 1.00e+000  1.664103252e+002  1.664275616e+002  3.9e-009 1.00  
37  6.2e-006 2.8e-002 4.1e-004 1.00e+000  1.664115030e+002  1.664270146e+002  3.5e-009 1.01  
38  5.6e-006 2.6e-002 3.7e-004 1.00e+000  1.664125620e+002  1.664265215e+002  3.1e-009 1.04  
39  5.0e-006 2.4e-002 3.3e-004 1.00e+000  1.664135142e+002  1.664260771e+002  2.8e-009 1.06  
40  4.5e-006 2.2e-002 3.0e-004 1.00e+000  1.664143705e+002  1.664256765e+002  2.5e-009 1.08  
41  4.1e-006 2.1e-002 2.7e-004 1.00e+000  1.664151405e+002  1.664253154e+002  2.3e-009 1.11  
42  3.7e-006 2.0e-002 2.4e-004 1.00e+000  1.664158329e+002  1.664249900e+002  2.1e-009 1.12  
43  3.3e-006 1.8e-002 2.2e-004 1.00e+000  1.664164556e+002  1.664246967e+002  1.8e-009 1.14  
44  3.0e-006 1.7e-002 2.0e-004 1.00e+000  1.664170156e+002  1.664244323e+002  1.7e-009 1.17  
45  2.7e-006 1.6e-002 1.8e-004 1.00e+000  1.664175192e+002  1.664241941e+002  1.5e-009 1.19  
46  2.4e-006 1.5e-002 1.6e-004 1.00e+000  1.664179722e+002  1.664239795e+002  1.3e-009 1.20  
47  2.2e-006 1.5e-002 1.4e-004 1.00e+000  1.664183797e+002  1.664237861e+002  1.2e-009 1.23  
48  1.9e-006 1.4e-002 1.3e-004 1.00e+000  1.664187463e+002  1.664236119e+002  1.1e-009 1.25  
49  1.8e-006 1.3e-002 1.2e-004 1.00e+000  1.664190761e+002  1.664234550e+002  9.8e-010 1.26  
50  1.6e-006 1.3e-002 1.0e-004 1.00e+000  1.664193728e+002  1.664233137e+002  8.8e-010 1.29  
51  1.4e-006 1.2e-002 9.4e-005 1.00e+000  1.664196397e+002  1.664231865e+002  8.0e-010 1.31  
52  1.3e-006 1.2e-002 8.5e-005 1.00e+000  1.664198798e+002  1.664230720e+002  7.2e-010 1.33  
53  1.1e-006 1.1e-002 7.6e-005 1.00e+000  1.664200959e+002  1.664229688e+002  6.4e-010 1.36  
54  1.0e-006 1.1e-002 6.9e-005 1.00e+000  1.664202903e+002  1.664228758e+002  5.8e-010 1.37  
55  9.3e-007 1.1e-002 6.2e-005 1.00e+000  1.664204652e+002  1.664227922e+002  5.2e-010 1.40  
56  8.4e-007 1.0e-002 5.6e-005 1.00e+000  1.664206226e+002  1.664227168e+002  4.7e-010 1.42  
57  7.5e-007 1.0e-002 5.0e-005 1.00e+000  1.664207641e+002  1.664226490e+002  4.2e-010 1.44  
58  6.8e-007 9.9e-003 4.5e-005 1.00e+000  1.664208915e+002  1.664225878e+002  3.8e-010 1.47  
59  6.1e-007 9.7e-003 4.1e-005 1.00e+000  1.664210061e+002  1.664225327e+002  3.4e-010 1.48  
60  5.5e-007 9.5e-003 3.6e-005 1.00e+000  1.664211091e+002  1.664224831e+002  3.1e-010 1.50  
61  4.9e-007 9.3e-003 3.3e-005 1.00e+000  1.664212019e+002  1.664224384e+002  2.8e-010 1.53  
62  4.4e-007 9.1e-003 3.0e-005 1.00e+000  1.664212853e+002  1.664223982e+002  2.5e-010 1.54  
63  4.0e-007 9.0e-003 2.7e-005 9.98e-001  1.664213603e+002  1.664223620e+002  2.2e-010 1.56  
64  3.6e-007 8.8e-003 2.4e-005 9.98e-001  1.664214277e+002  1.664223293e+002  2.0e-010 1.59  
65  3.2e-007 8.7e-003 2.2e-005 9.99e-001  1.664214884e+002  1.664222999e+002  1.8e-010 1.62  
66  2.9e-007 8.6e-003 1.9e-005 9.99e-001  1.664215431e+002  1.664222734e+002  1.6e-010 1.64  
67  2.6e-007 8.5e-003 1.7e-005 1.00e+000  1.664215922e+002  1.664222495e+002  1.5e-010 1.65  
68  2.4e-007 8.4e-003 1.6e-005 9.99e-001  1.664216364e+002  1.664222280e+002  1.3e-010 1.69  
69  2.1e-007 8.3e-003 1.4e-005 9.99e-001  1.664216762e+002  1.664222087e+002  1.2e-010 1.70  
70  1.9e-007 8.2e-003 1.3e-005 9.96e-001  1.664217120e+002  1.664221913e+002  1.1e-010 1.73  
71  1.7e-007 8.2e-003 1.1e-005 1.00e+000  1.664217442e+002  1.664221756e+002  9.7e-011 1.75  
72  1.6e-007 8.1e-003 1.0e-005 1.00e+000  1.664217732e+002  1.664221615e+002  8.7e-011 1.76  
73  1.4e-007 8.1e-003 9.3e-006 1.00e+000  1.664217993e+002  1.664221487e+002  7.8e-011 1.79  
74  1.3e-007 8.0e-003 8.3e-006 1.00e+000  1.664218228e+002  1.664221372e+002  7.1e-011 1.81  
75  1.1e-007 8.0e-003 7.5e-006 1.00e+000  1.664218440e+002  1.664221269e+002  6.3e-011 1.83  
76  1.0e-007 7.9e-003 6.8e-006 1.00e+000  1.664218631e+002  1.664221175e+002  5.7e-011 1.86  
77  9.2e-008 7.9e-003 6.1e-006 9.91e-001  1.664218802e+002  1.664221093e+002  5.1e-011 1.87  
78  8.2e-008 7.1e-003 5.5e-006 1.01e+000  1.664218958e+002  1.664221016e+002  4.6e-011 1.89  
79  7.4e-008 6.4e-003 4.9e-006 1.00e+000  1.664219096e+002  1.664220948e+002  4.2e-011 1.92  
80  6.7e-008 5.7e-003 4.4e-006 1.00e+000  1.664219221e+002  1.664220888e+002  3.8e-011 1.93  
81  6.0e-008 5.2e-003 4.0e-006 1.01e+000  1.664219338e+002  1.664220830e+002  3.4e-011 1.95  
82  5.4e-008 4.7e-003 3.6e-006 1.01e+000  1.664219442e+002  1.664220779e+002  3.1e-011 1.98  
83  4.9e-008 4.2e-003 3.2e-006 9.93e-001  1.664219531e+002  1.664220735e+002  2.8e-011 2.00  
84  4.4e-008 3.8e-003 2.9e-006 1.00e+000  1.664219613e+002  1.664220695e+002  2.5e-011 2.01  
85  3.9e-008 3.4e-003 2.6e-006 1.01e+000  1.664219690e+002  1.664220657e+002  2.3e-011 2.04  
86  3.6e-008 3.1e-003 2.4e-006 1.00e+000  1.664219756e+002  1.664220625e+002  2.0e-011 2.06  
87  3.2e-008 2.7e-003 2.1e-006 1.01e+000  1.664219816e+002  1.664220596e+002  1.8e-011 2.08  
88  2.9e-008 2.5e-003 1.9e-006 9.66e-001  1.664219868e+002  1.664220571e+002  1.6e-011 2.09  
89  2.6e-008 2.2e-003 1.7e-006 9.62e-001  1.664219915e+002  1.664220549e+002  1.5e-011 2.12  
90  2.3e-008 2.0e-003 1.5e-006 9.97e-001  1.664219958e+002  1.664220528e+002  1.3e-011 2.15  
91  2.1e-008 1.8e-003 1.4e-006 1.00e+000  1.664219996e+002  1.664220509e+002  1.2e-011 2.18  
92  1.9e-008 1.6e-003 1.3e-006 9.78e-001  1.664220030e+002  1.664220493e+002  1.1e-011 2.21  
93  1.7e-008 1.5e-003 1.1e-006 1.01e+000  1.664220062e+002  1.664220477e+002  9.8e-012 2.25  
94  1.5e-008 1.3e-003 1.0e-006 1.02e+000  1.664220092e+002  1.664220462e+002  8.9e-012 2.28  
95  1.4e-008 1.2e-003 9.1e-007 9.87e-001  1.664220117e+002  1.664220450e+002  8.0e-012 2.29  
96  1.2e-008 1.1e-003 8.2e-007 9.11e-001  1.664220139e+002  1.664220440e+002  7.2e-012 2.32  
97  1.1e-008 9.6e-004 7.4e-007 9.90e-001  1.664220159e+002  1.664220430e+002  6.5e-012 2.34  
98  1.0e-008 8.6e-004 6.7e-007 9.99e-001  1.664220177e+002  1.664220421e+002  5.8e-012 2.37  
99  9.1e-009 7.8e-004 6.0e-007 9.60e-001  1.664220194e+002  1.664220414e+002  5.2e-012 2.40  
100 8.2e-009 7.0e-004 5.4e-007 9.29e-001  1.664220208e+002  1.664220407e+002  4.7e-012 2.42  
101 7.5e-009 6.3e-004 4.9e-007 1.03e+000  1.664220223e+002  1.664220399e+002  4.3e-012 2.45  
102 6.8e-009 5.7e-004 4.4e-007 1.00e+000  1.664220235e+002  1.664220393e+002  3.9e-012 2.46  
103 6.1e-009 5.1e-004 3.9e-007 9.72e-001  1.664220245e+002  1.664220388e+002  3.5e-012 2.48  
104 5.4e-009 4.6e-004 3.5e-007 9.68e-001  1.664220255e+002  1.664220383e+002  3.1e-012 2.51  
105 5.0e-009 4.1e-004 3.2e-007 8.80e-001  1.664220263e+002  1.664220380e+002  2.8e-012 2.53  
106 4.6e-009 3.7e-004 2.9e-007 9.69e-001  1.664220271e+002  1.664220376e+002  2.5e-012 2.56  
107 4.1e-009 3.3e-004 2.6e-007 1.30e+000  1.664220278e+002  1.664220371e+002  2.3e-012 2.57  
108 3.7e-009 3.0e-004 2.3e-007 1.02e+000  1.664220285e+002  1.664220368e+002  2.1e-012 2.61  
109 3.7e-009 2.1e-005 1.6e-008 6.79e-001  1.664220342e+002  1.664220348e+002  3.9e-013 2.64  
Interior-point optimizer terminated. Time: 2.64. 

Optimizer terminated. Time: 2.65    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6642203418e+002   Viol.  con: 1e-007   var: 0e+000 
  Dual.    obj: 1.6642203485e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.66 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 936             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 769
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3439              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.01            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.46e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.285332517e+005 2.000000000e+000  1.0e+000 0.05  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.263506611e+005 3.573406056e+000  4.8e-001 0.08  
2   4.3e+002 5.5e+002 2.4e+004 -9.36e-001 -1.201229664e+005 1.024108894e+001  1.8e-001 0.09  
3   2.9e+002 3.7e+002 1.6e+004 -8.38e-001 -1.154146805e+005 6.438962157e+001  1.2e-001 0.12  
4   2.8e+002 3.6e+002 1.6e+004 -7.58e-001 -1.128142010e+005 2.256492322e+003  1.2e-001 0.14  
5   7.5e+001 9.6e+001 4.1e+003 -7.51e-001 -7.452149401e+004 9.623307072e+003  3.3e-002 0.19  
6   3.0e+001 3.8e+001 1.7e+003 -1.92e-001 -4.039638311e+004 1.017306508e+004  1.3e-002 0.22  
7   1.8e+001 2.3e+001 1.0e+003 3.96e-001  -2.710388119e+004 6.644093446e+003  7.9e-003 0.25  
8   9.5e+000 1.2e+001 5.2e+002 6.30e-001  -1.529786089e+004 3.811653387e+003  4.1e-003 0.27  
9   3.3e+000 4.2e+000 1.8e+002 8.18e-001  -5.370899192e+003 1.685464737e+003  1.5e-003 0.30  
10  1.6e+000 2.1e+000 9.1e+001 9.54e-001  -2.488182556e+003 1.068025853e+003  7.3e-004 0.33  
11  9.3e-001 1.2e+000 5.2e+001 9.86e-001  -1.337509586e+003 6.866474084e+002  4.1e-004 0.36  
12  8.5e-001 1.1e+000 4.8e+001 9.60e-001  -1.253924359e+003 6.354830031e+002  3.8e-004 0.39  
13  4.7e-001 6.1e-001 2.7e+001 9.77e-001  -6.373611310e+002 4.197149212e+002  2.1e-004 0.42  
14  2.5e-001 3.3e-001 1.4e+001 1.00e+000  -2.541480273e+002 3.021229249e+002  1.1e-004 0.44  
15  9.3e-002 1.5e-001 5.3e+000 1.00e+000  -3.966564290e+000 2.060665550e+002  4.3e-005 0.47  
16  8.6e-002 1.3e-001 4.9e+000 1.02e+000  1.475243314e+001  2.084814907e+002  4.0e-005 0.48  
17  6.0e-002 9.6e-002 3.4e+000 1.02e+000  6.117845031e+001  1.950767972e+002  2.8e-005 0.51  
18  3.3e-002 7.2e-002 1.9e+000 1.02e+000  1.091855256e+002  1.824026620e+002  1.5e-005 0.55  
19  9.2e-003 1.8e-001 5.3e-001 1.02e+000  1.513703858e+002  1.718414076e+002  4.3e-006 0.56  
20  3.6e-003 2.1e-001 2.1e-001 1.01e+000  1.602183047e+002  1.683899795e+002  1.7e-006 0.59  
21  1.3e-003 1.3e-001 7.6e-002 1.01e+000  1.642699983e+002  1.671903166e+002  6.2e-007 0.61  
22  8.6e-004 1.0e-001 5.2e-002 9.84e-001  1.649681572e+002  1.669444014e+002  4.3e-007 0.64  
23  2.6e-004 1.1e-001 1.6e-002 9.86e-001  1.659690900e+002  1.665864863e+002  1.3e-007 0.67  
24  9.4e-005 1.0e-001 6.1e-003 1.01e+000  1.662459008e+002  1.664756915e+002  5.1e-008 0.69  
25  3.7e-005 9.5e-002 2.4e-003 1.01e+000  1.663440792e+002  1.664350964e+002  2.0e-008 0.72  
26  1.7e-005 8.1e-002 1.1e-003 1.00e+000  1.663785039e+002  1.664206580e+002  9.5e-009 0.73  
27  1.5e-005 7.4e-002 1.0e-003 1.00e+000  1.663820220e+002  1.664199768e+002  8.5e-009 0.76  
28  1.4e-005 6.7e-002 9.0e-004 1.01e+000  1.663846088e+002  1.664187607e+002  7.7e-009 0.78  
29  1.2e-005 6.1e-002 8.1e-004 1.00e+000  1.663869808e+002  1.664177120e+002  6.9e-009 0.81  
30  1.1e-005 5.6e-002 7.3e-004 1.00e+000  1.663891053e+002  1.664167591e+002  6.2e-009 0.83  
31  1.0e-005 5.1e-002 6.6e-004 1.00e+000  1.663910160e+002  1.664159007e+002  5.6e-009 0.86  
32  9.1e-006 4.7e-002 5.9e-004 1.00e+000  1.663927333e+002  1.664151266e+002  5.0e-009 0.87  
33  8.1e-006 4.3e-002 5.3e-004 1.00e+000  1.663942771e+002  1.664144287e+002  4.5e-009 0.90  
34  7.3e-006 3.9e-002 4.8e-004 1.00e+000  1.663956651e+002  1.664137996e+002  4.1e-009 0.92  
35  6.6e-006 3.6e-002 4.3e-004 1.00e+000  1.663969130e+002  1.664132325e+002  3.7e-009 0.95  
36  5.9e-006 3.3e-002 3.9e-004 1.00e+000  1.663980351e+002  1.664127213e+002  3.3e-009 0.97  
37  5.3e-006 3.1e-002 3.5e-004 1.00e+000  1.663990441e+002  1.664122607e+002  3.0e-009 0.98  
38  4.8e-006 2.9e-002 3.2e-004 1.00e+000  1.663999515e+002  1.664118455e+002  2.7e-009 1.01  
39  4.3e-006 2.6e-002 2.8e-004 1.00e+000  1.664007675e+002  1.664114714e+002  2.4e-009 1.03  
40  3.9e-006 2.5e-002 2.6e-004 1.00e+000  1.664015013e+002  1.664111343e+002  2.2e-009 1.06  
41  3.5e-006 2.3e-002 2.3e-004 1.00e+000  1.664021612e+002  1.664108304e+002  2.0e-009 1.08  
42  3.2e-006 2.1e-002 2.1e-004 1.00e+000  1.664027547e+002  1.664105566e+002  1.8e-009 1.09  
43  2.8e-006 2.0e-002 1.9e-004 1.00e+000  1.664032885e+002  1.664103099e+002  1.6e-009 1.12  
44  2.6e-006 1.9e-002 1.7e-004 1.00e+000  1.664037685e+002  1.664100876e+002  1.4e-009 1.14  
45  2.3e-006 1.8e-002 1.5e-004 1.00e+000  1.664042004e+002  1.664098874e+002  1.3e-009 1.17  
46  2.1e-006 1.7e-002 1.4e-004 1.00e+000  1.664045889e+002  1.664097071e+002  1.2e-009 1.19  
47  1.9e-006 1.6e-002 1.2e-004 1.00e+000  1.664049384e+002  1.664095447e+002  1.0e-009 1.20  
48  1.7e-006 1.5e-002 1.1e-004 1.00e+000  1.664052529e+002  1.664093984e+002  9.4e-010 1.23  
49  1.5e-006 1.4e-002 9.9e-005 1.00e+000  1.664055358e+002  1.664092668e+002  8.4e-010 1.25  
50  1.4e-006 1.4e-002 8.9e-005 1.00e+000  1.664057903e+002  1.664091481e+002  7.6e-010 1.28  
51  1.2e-006 1.3e-002 8.0e-005 1.00e+000  1.664060193e+002  1.664090413e+002  6.8e-010 1.29  
52  1.1e-006 1.2e-002 7.2e-005 1.00e+000  1.664062254e+002  1.664089451e+002  6.1e-010 1.31  
53  9.9e-007 1.2e-002 6.5e-005 1.00e+000  1.664064108e+002  1.664088584e+002  5.5e-010 1.34  
54  8.9e-007 1.2e-002 5.9e-005 1.00e+000  1.664065776e+002  1.664087805e+002  5.0e-010 1.36  
55  8.0e-007 1.1e-002 5.3e-005 1.00e+000  1.664067277e+002  1.664087103e+002  4.5e-010 1.39  
56  7.2e-007 1.1e-002 4.7e-005 1.00e+000  1.664068626e+002  1.664086470e+002  4.0e-010 1.40  
57  6.5e-007 1.0e-002 4.3e-005 1.00e+000  1.664069841e+002  1.664085900e+002  3.6e-010 1.44  
58  5.8e-007 1.0e-002 3.8e-005 1.00e+000  1.664070934e+002  1.664085386e+002  3.3e-010 1.45  
59  5.3e-007 9.9e-003 3.5e-005 1.00e+000  1.664071917e+002  1.664084924e+002  2.9e-010 1.48  
60  4.7e-007 9.7e-003 3.1e-005 1.00e+000  1.664072801e+002  1.664084508e+002  2.6e-010 1.50  
61  4.3e-007 9.5e-003 2.8e-005 1.00e+000  1.664073596e+002  1.664084132e+002  2.4e-010 1.53  
62  3.8e-007 9.3e-003 2.5e-005 1.00e+000  1.664074311e+002  1.664083794e+002  2.1e-010 1.54  
63  3.5e-007 9.1e-003 2.3e-005 1.00e+000  1.664074955e+002  1.664083489e+002  1.9e-010 1.58  
64  3.1e-007 9.0e-003 2.0e-005 1.00e+000  1.664075534e+002  1.664083214e+002  1.7e-010 1.59  
65  2.8e-007 8.8e-003 1.8e-005 9.99e-001  1.664076055e+002  1.664082967e+002  1.6e-010 1.62  
66  2.5e-007 8.7e-003 1.7e-005 1.00e+000  1.664076523e+002  1.664082744e+002  1.4e-010 1.64  
67  2.3e-007 8.6e-003 1.5e-005 9.99e-001  1.664076945e+002  1.664082544e+002  1.3e-010 1.67  
68  2.0e-007 8.5e-003 1.3e-005 9.99e-001  1.664077324e+002  1.664082364e+002  1.1e-010 1.68  
69  1.8e-007 8.4e-003 1.2e-005 1.00e+000  1.664077665e+002  1.664082201e+002  1.0e-010 1.72  
70  1.7e-007 8.3e-003 1.1e-005 1.00e+000  1.664077973e+002  1.664082054e+002  9.2e-011 1.73  
71  1.5e-007 8.2e-003 9.8e-006 1.00e+000  1.664078249e+002  1.664081922e+002  8.3e-011 1.76  
72  1.3e-007 8.2e-003 8.8e-006 1.00e+000  1.664078498e+002  1.664081804e+002  7.5e-011 1.78  
73  1.2e-007 8.1e-003 7.9e-006 9.99e-001  1.664078722e+002  1.664081697e+002  6.7e-011 1.81  
74  1.1e-007 8.1e-003 7.1e-006 1.00e+000  1.664078924e+002  1.664081600e+002  6.1e-011 1.83  
75  9.8e-008 8.0e-003 6.4e-006 9.98e-001  1.664079105e+002  1.664081514e+002  5.4e-011 1.86  
76  8.8e-008 7.9e-003 5.8e-006 1.00e+000  1.664079268e+002  1.664081436e+002  4.9e-011 1.87  
77  7.9e-008 7.2e-003 5.2e-006 1.01e+000  1.664079421e+002  1.664081362e+002  4.4e-011 1.89  
78  7.1e-008 6.4e-003 4.7e-006 1.01e+000  1.664079555e+002  1.664081298e+002  4.0e-011 1.92  
79  6.4e-008 5.8e-003 4.2e-006 9.95e-001  1.664079673e+002  1.664081242e+002  3.6e-011 1.93  
80  5.8e-008 5.2e-003 3.8e-006 1.00e+000  1.664079779e+002  1.664081191e+002  3.2e-011 1.97  
81  5.2e-008 4.7e-003 3.4e-006 1.00e+000  1.664079875e+002  1.664081146e+002  2.9e-011 1.98  
82  4.7e-008 4.2e-003 3.1e-006 9.84e-001  1.664079961e+002  1.664081105e+002  2.6e-011 2.01  
83  4.2e-008 3.8e-003 2.8e-006 1.01e+000  1.664080039e+002  1.664081067e+002  2.4e-011 2.03  
84  3.8e-008 3.4e-003 2.5e-006 1.02e+000  1.664080116e+002  1.664081030e+002  2.2e-011 2.04  
85  3.4e-008 3.1e-003 2.2e-006 1.00e+000  1.664080178e+002  1.664081001e+002  1.9e-011 2.07  
86  3.1e-008 2.8e-003 2.0e-006 1.00e+000  1.664080233e+002  1.664080974e+002  1.7e-011 2.09  
87  2.8e-008 2.5e-003 1.8e-006 1.01e+000  1.664080285e+002  1.664080949e+002  1.6e-011 2.12  
88  2.5e-008 2.2e-003 1.6e-006 9.87e-001  1.664080330e+002  1.664080928e+002  1.4e-011 2.14  
89  2.2e-008 2.0e-003 1.5e-006 1.04e+000  1.664080378e+002  1.664080904e+002  1.3e-011 2.17  
90  2.0e-008 1.8e-003 1.3e-006 9.99e-001  1.664080414e+002  1.664080887e+002  1.2e-011 2.18  
91  1.8e-008 1.6e-003 1.2e-006 1.00e+000  1.664080446e+002  1.664080871e+002  1.1e-011 2.20  
92  1.6e-008 1.5e-003 1.1e-006 9.22e-001  1.664080475e+002  1.664080859e+002  9.5e-012 2.23  
93  1.5e-008 1.3e-003 9.6e-007 1.01e+000  1.664080502e+002  1.664080845e+002  8.6e-012 2.25  
94  1.3e-008 1.2e-003 8.7e-007 9.74e-001  1.664080525e+002  1.664080835e+002  7.7e-012 2.28  
95  1.2e-008 1.1e-003 7.8e-007 9.88e-001  1.664080546e+002  1.664080825e+002  7.0e-012 2.29  
96  1.1e-008 9.7e-004 7.0e-007 1.01e+000  1.664080566e+002  1.664080815e+002  6.3e-012 2.32  
97  9.7e-009 8.7e-004 6.3e-007 9.67e-001  1.664080583e+002  1.664080807e+002  5.7e-012 2.34  
98  8.7e-009 7.8e-004 5.7e-007 8.47e-001  1.664080598e+002  1.664080801e+002  5.1e-012 2.37  
99  7.9e-009 7.0e-004 5.1e-007 9.13e-001  1.664080611e+002  1.664080795e+002  4.6e-012 2.39  
100 7.2e-009 6.3e-004 4.6e-007 9.03e-001  1.664080623e+002  1.664080790e+002  4.1e-012 2.40  
101 6.5e-009 5.7e-004 4.1e-007 1.02e+000  1.664080636e+002  1.664080783e+002  3.8e-012 2.43  
102 5.9e-009 5.1e-004 3.7e-007 9.14e-001  1.664080645e+002  1.664080779e+002  3.4e-012 2.45  
103 5.6e-009 4.6e-004 3.4e-007 1.12e+000  1.664080659e+002  1.664080771e+002  3.2e-012 2.48  
104 5.0e-009 4.2e-004 3.0e-007 8.89e-001  1.664080667e+002  1.664080768e+002  2.9e-012 2.50  
105 4.7e-009 3.7e-004 2.7e-007 1.17e+000  1.664080679e+002  1.664080761e+002  2.9e-012 2.53  
106 4.3e-009 3.4e-004 2.4e-007 9.92e-001  1.664080684e+002  1.664080758e+002  2.6e-012 2.54  
107 3.7e-009 3.0e-004 2.2e-007 1.01e+000  1.664080690e+002  1.664080756e+002  2.3e-012 2.57  
108 3.7e-009 3.0e-004 2.2e-007 1.09e+000  1.664080690e+002  1.664080756e+002  2.3e-012 2.61  
109 3.7e-009 3.0e-004 2.2e-007 1.15e+000  1.664080690e+002  1.664080756e+002  2.3e-012 2.62  
110 3.4e-009 2.7e-004 2.0e-007 8.23e-001  1.664080694e+002  1.664080754e+002  2.1e-012 2.65  
111 3.4e-009 2.7e-004 2.0e-007 1.14e+000  1.664080694e+002  1.664080754e+002  2.1e-012 2.67  
112 3.4e-009 2.7e-004 2.0e-007 1.15e+000  1.664080694e+002  1.664080754e+002  2.1e-012 2.70  
113 3.4e-009 2.7e-004 2.0e-007 1.14e+000  1.664080694e+002  1.664080754e+002  2.1e-012 2.71  
114 3.2e-009 2.5e-004 1.8e-007 8.88e-001  1.664080698e+002  1.664080752e+002  1.9e-012 2.75  
115 3.5e-009 2.8e-005 2.0e-008 7.99e-001  1.664080732e+002  1.664080739e+002  3.5e-013 2.76  
Interior-point optimizer terminated. Time: 2.78. 

Optimizer terminated. Time: 2.79    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6640807319e+002   Viol.  con: 1e-007   var: 0e+000 
  Dual.    obj: 1.6640807388e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.81 seconds.
Solving took 9 GP solves and 72.1 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: 1.4957404149493179e+110 vs 1.49570291522e+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: 3.705403527142521e+72 vs 3.70525441629e+72
WEIGHT DIFFERENCES


Total Fuel Weight Percent Diff: [-92.94682466]


Total Aircraft Weight Percent Diff: [-21.48057113]


Engine Weight Percent Diff: -56.27821902807174


Fuselage Weight Percent Diff: -0.869732519197598


Payload Weight Percent Diff: [-0.0400356]


VT Weight Percent Diff: -8.607874288596456


HT Weight Percent Diff: -93.23327145187311


Wing Weight Percent Diff: 8.267424927424548




WING DIFFERENCES


Wing Span Percent Diff: -0.029993482109050847


Wing Area Percent Diff: 32.90012304693212




HORIZONTAL TAIL DIFFERENCES


HT Area Percent Diff: 40.48932226813156




VERTICAL TAIL DIFFERENCES




VT Span Percent Diff: -11.022348185151118


VT Area Percent Diff: -60.38684253848517




CRUISE SEGMENT 1 DRAG DIFFERENCES


Overall Cd Percent Diff: [-18.54730529]


L/D Percent Diff: [24.01021227]


Nacelle Cd Percent Diff: [-94.27642167]


HT Cd Percent Diff: [-80.76937396] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-58.00306014] dimensionless


Wing Cd percent Diff: [-14.22927727]
Induced Drag Cd Percent Diff: [1.21942295]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-90.57036082]




FUSELAGE DIFFERENCES




Weight of HB material: -38.3605168101039 


Weight of VB material: 87.81882373011766 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.71260522]
Mission1
========

Cost
----
 W_{f_{total}}[:].sum()

Constraints
-----------
   W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin}
   PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:])
   x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:])
   x_{CG}[3] <= \Delta x_n + x_n
   \Delta x_m + x_{CG}[3] >= x_m
   \tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m
   C_{D_{fuse}}[:] = 0.018081
   M_{fuseD} = 0.72
   W_{start}[0] = W_{total}[:]
   W_{start}[:] >= W_{end}[:] + W_{burn}[:]
   W_{start}[1:] = W_{end}[:4]
   W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1]
   W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2]
   W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1]
   hft[2] >= CruiseAlt
   hft[1:5] = hft[:4] + dhft[1:5]
   hft[0] = dhft[0]
   dhft[1:3] = dhft[:2]
   RC[0] >= 2.5e+03
   RC[:3] >= RC_{min}[:3]
   \theta[2] >= 0.015
   hft[2] >= MinCruiseAlt
   n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:]
   R_{segment}[3:4] = R_{segment}[4:5]
   M[3:5] >= M_{min}
   0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req}
   Fsafetyfac*F[0] = T_e
   W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:]
   V_2[:] = M_2[:]*a[:]
   \alpha_{max,w}[:3] = 0.18
   \alpha_{max,w}[3:] = 0.1
   0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime
   0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime
   ClimbTime <= MaxClimbTime
   T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}}
   F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   OPR[:] <= OPR_{max}
 
 Aircraft
     Fuselage
       W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on}
       W_{pass}[:] >= n_{pass}[:]*W_{avg. pass}
       W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo}
       W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}}
       W_{payload}[:] <= W_{payload_{max}}
       n_{pass}[:] <= n_{seat}
       n_{rows} = n_{seat}/SPR
       l_{shell} = n_{rows}*p_s
       \theta_{db} = w_{db}/R_{fuse}
       R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db}
       A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db}
       (PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse}
       A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin}
       w_{floor} = w_{fuse}
       R_{fuse} + w_{db} >= w_{fuse}
       h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse}
       t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell}
       S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2
       S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2
       l_{fuse} = l_{nose} + l_{shell} + l_{cone}
       l_{cone} = R_{fuse}/\lambda_{cone}
       x_{shell1} = l_{nose}
       x_{shell2} >= l_{nose} + l_{shell}
       t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin}
       t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin}
       \sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell})
       \sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin}
       l_{floor} >= l_{shell} + 2*R_{fuse}
       P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat})
       A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor}
       V_{floor} = 2*w_{floor}*A_{floor}
       W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor}
       \tau_{cone} = \sigma_{skin}
       W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame})
       x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone}
       -2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}}
       (PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}}
       x_{hbend_{Land}} >= x_{wing}
       x_{hbend_{Land}} <= l_{fuse}
       x_{hbend_{MLF}} >= x_{wing}
       x_{hbend_{MLF}} <= l_{fuse}
       A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}})
       A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}})
       A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
       A_{2h_{MLF}} >= Mission1.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
       A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2)
       A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}}
       A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}}
       A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}}
       A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}}
       A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}}
       A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}}
       A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}}
       A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}}
       V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}}
       W_{hbend} >= g*\rho_{bend}*V_{hbend}
       x_{vbend} >= x_{wing}
       x_{vbend} <= l_{fuse}
       B_{0v} = B_{1v}*(x_{tail} - x_{vbend})
       B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2)
       B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}}
       0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}}
       V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}}
       W_{vbend} >= \rho_{bend}*g*V_{vbend}
       x_f = x_{wing} + 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       x_b = x_{wing} - 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h}
       \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v}
       V_{cyl} = A_{skin}*l_{shell}
       V_{nose} = S_{nose}*t_{skin}
       V_{bulk} = S_{bulk}*t_{skin}
       V_{db} = A_{db}*l_{shell}
       V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse})
       W_{apu} = W_{payload_{max}}*f_{apu}
       W_{db} = \rho_{skin}*g*V_{db}
       W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk})
       W_{window} >= W'_{window}*l_{shell}
       W_{padd} = W_{payload_{max}}*f_{padd}
       W_{seat} >= W'_{seat}*n_{seat}
       W_{seat} >= f_{seat}*W_{payload_{max}}
       W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk})
       W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db}
       W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone})
     
     Wing
       WingNoStruct
         A_{rect} = c_{tip}*b
         0.5*(1 - \lambda)*c_{root}*b <= A_{tri}
         p >= 1 + 2*\lambda
         2*q >= 1 + p
         y_{mac} = b/3*q/p
         mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q
         \lambda = c_{tip}/c_{root}
         S = b*(c_{root} + c_{tip})/2
         0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w)
         e*(1 + f(\lambda_w)*AR) <= 1
         \lambda >= 0.15
         V_{fuel, max} <= 0.303*mac^2*b*\tau
         W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g
         b <= b_{max}
       
       WingBox
         AR = b^2/S
         0.423*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5)
         \tau <= \tau_{max_w}
         W_{struct} >= W_{web} + W_{cap}
         AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5)
         Mission1.Aircraft.Wing.WingBox.N_{lift} = 3
         Mission1.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8
         \lambda = taper
         W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt})
         0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}}
     
     Engine
         Compressor
           (no constraints)
         
         Combustor
           (no constraints)
         
         Turbine
           (no constraints)
         
         Thrust
           (no constraints)
         
         FanMap
           (no constraints)
         
         LPCMap
           (no constraints)
         
         HPCMap
           (no constraints)
         
         Sizing
           A_{2} >= A_{5} + A_{7}
         
         FlightState
             V[:] = V[:]
             a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
             V[:] = M[:]*a[:]
           
           Altitude
             h[:] = hft[:]
           
           Atmosphere
             (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
             \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
             T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
             \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
         
         EnginePerformance
           CompressorPerformance
               T_{t_0}[:] = T_{atm}[:]/c1[:]^-1
               h_{t_0}[:] = C_{p_{air}*T_{t_0}[:]
               P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:]
               T_{t_{1.8}}[:] = T_{t_0}[:]
               h_{t_{1.8}}[:] = h_{t_0}[:]
               P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5
               T_{T_{2}}[:] = T_{t_{1.8}}[:]
               h_{T_{2}}[:] = h_{t_{1.8}}[:]
               P_{T_{2}}[:] = P_{t_{1.8}}[:]
               P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:]
               T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016
               h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:]
               P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:]
               T_{t_7}[:] = T_{t_{2.1}}[:]
               h_{t_7}[:] = h_{t_{2.1}}[:]
               P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:]
               T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152
               h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1}
               P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:]
               T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491
               h_{t_3}[:] = C_{p_{2}*T_{t_3}[:]
           
           CombustorPerformance
             h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:]
             h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:]
             fp1[:] = f[:] + 1
             M_{4a}[:] = 0.1025
             fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5
             T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]]
             P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891
             u_{4a}[:] = M_{4a}[:]*(1.31*Mission1.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a}
             u_c[:] = r_{uc}*u_{4a}[:]
             P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891
           
           TurbinePerformance
             h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:]
             P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:]
             \pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565
             h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:]
             P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:]
             T_{t_5}[:] = T_{t_{4.9}}[:]
             h_{t_5}[:] = h_{t_{4.9}}[:]
           
           ThrustPerformance
             P_{8}[:] = P_{atm}[:]
             h_{8}[:] = C_{p_{fex}*T_{8}[:]
             u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:]
             (P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:]
             h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:]
             P_{6}[:] = P_{atm}[:]
             (P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:]
             u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:]
             h_6[:] = C_{p_{tex}*T_{6}[:]
             h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:]
             \alpha[:] = m_{fan}[:]/m_{core}[:]
             \alpha_{+1}[:] = \alpha[:] + 1
             \alpha[:] <= \alpha_{max}
             F[:] <= F_{6}[:] + F_{8}[:]
             F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:])
             TSFC[:] = 1/I_{sp}[:]
             F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:]
           
           FanMapPerformance
             m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}}
           
           LPCMapPerformance
             m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D}
           
           HPCMapPerformance
             m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D}
           
           SizingPerformance
             P_{7}[:] >= P_{atm}[:]
             M_7[:] <= 1
             a_{7}[:] = (1.4*Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5
             a_{7}[:]*M_7[:] = u_{7}[:]
             \rho_7[:] = P_{7}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])
             P_{5}[:] >= P_{atm}[:]
             M_5[:] <= 1
             a_{5}[:] = (1.39*Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5
             a_{5}[:]*M_5[:] = u_{5}[:]
             \rho_5[:] = P_{5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])
             h_{2}[:] = C_{p_{1}*T_{2}[:]
             \rho_{2}[:] = P_{2}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:])
             u_{2}[:] = M_2[:]*(C_{p_{1}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:]/781)^0.5
             h_{2.5}[:] = C_{p_{2}*T_{2.5}[:]
             \rho_{2.5}[:] = P_{2.5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:])
             u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/781)^0.5
         m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine}
           d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5
           d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5
           \eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]])
           h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:]
           P_{t_4}[:] = \pi_{b}*P_{t_3}[:]
           M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]]
           M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]])
           P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:]
           \pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013
           \pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10
           \pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10
           \pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10
           m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
           \pi_{f}[:] >= 1
           \pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10
           \pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10
           \pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10
           \pi_{lc}[:] >= 1
           m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
           \pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10
           \pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10
           \pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10
           m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref})
           \pi_{hc}[:] >= 1
         OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:]
           P_{t_8}[:] = P_{t_7}[:]
           T_{t_8}[:] = T_{t_7}[:]
           P_{t_6}[:] = P_{t_5}[:]
           T_{t_6}[:] = T_{t_5}[:]
           F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:]
           I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g)
           N_{f}[:]*G_{f} = N_{1}[:]
           N_{1}[:] <= 1.1
           N_{2}[:] <= 1.1
         fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD}
         fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD}
           P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5
           (T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2
           P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979
           (T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2
           M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:]
           m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:]
           m_{total}[:] = m_{fan}[:] + m_{core}[:]
           P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512
           T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1
           m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2}
           P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857
           T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1
           m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5}
           1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD}
           0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD}
           1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD}
           0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD}
           m_{lc_D} >= 0.7*m_{coreD}/0.649
           m_{lc_D} <= 1.3*m_{coreD}/0.649
           m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23
           m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23
           \bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405
           \bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405
           F[:] = F_{spec}[:]
           T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}}
           OPR[:] <= OPR_{max}
     
     VerticalTail
       VerticalTailNoStruct
         C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}}
         L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}}
         c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt}))
         A_{vt} = b_{vt}^2/S_{vt}
         b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt}
         p_{vt} >= 1 + 2*\lambda_{vt}
         2*q_{vt} >= 1 + p_{vt}
         y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
         z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
         0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt}
         \lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}}
         \Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}}
         \Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt}
         \lambda_{vt} >= 0.25
         V_{vt} >= V_{vt_{min}}
       
       WingBox
         AR_{vt} = (2*b_{vt})^2/(2*S_{vt})
         0.423*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
         \tau_{vt} <= 0.14
         W_{struct} >= 0.5*(W_{web} + W_{cap})
         Mission1.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24
         AR_{vt}*2*L_{vt_{max}}*Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
         Mission1.Aircraft.VerticalTail.WingBox.N_{lift} = 1
         Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*Mission1.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8
         \lambda_{vt} = taper
         W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT})
     
     HorizontalTail
       HorizontalTailNoStruct
         \Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht}
         \Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}}
         p_{ht} >= 1 + 2*\lambda_{ht}
         2*q_{ht} >= 1 + p_{ht}
         y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht}
         0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht}
         \lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}}
         S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2
         0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht})
         e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1
         AR_{ht} = b_{ht}^2/S_{ht}
         \lambda_{ht} >= 0.2
         \lambda_{ht} <= 1
       
       WingBox
         AR_{ht} = b_{ht}^2/S_{ht}
         0.423*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
         \tau_{ht} <= 0.14
         W_{struct} >= W_{web} + W_{cap}
         L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2
         L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht})
         2*AR_{ht}*L_{shear}*Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
         Mission1.Aircraft.HorizontalTail.WingBox.N_{lift} = 1
         Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission1.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8
         L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht}
         L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}}
         W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht})
     
     LandingGear
       l_n + z_{wing} + y_m*\tan(\gamma) >= l_m
       T = 2*y_m
       x_m >= x_n + B
       x_n >= 5
       \tan(\phi) = \tan(\phi_{min})
       (z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1
       \tan(\psi) <= \tan(\psi_{max})
       x_{up} - x_m <= l_m/\tan(\theta_{max})
       y_m >= l_m
       S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG})
       l_{oleo} = 2.5*S_{sa}
       d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5
       l_m >= l_{oleo} + d_{t_m}/2
       F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in])
       W_{wa,m} = 1.2*F_{w_m}^0.609
       F_{w_n} = L_{w_n}*d_{t_n}/1e+03
       W_{wa,n} = 1.2*F_{w_n}^0.609
       L_{w_m} = L_m/(n_{mg}*n_{wps})
       L_{w_n} = L_n/n_{wps}
       d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315
       w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48
       d_{t_n} = 0.8*d_{t_m}
       w_{t_n} = 0.8*w_{t_m}
       W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g
       N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m
       W_{mw} = n_{wps}*W_{wa,m}
       W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g
       \sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}})
       W_{nw} >= n_{wps}*W_{wa,n}
       L_m <= 9.87*E*I_m/(K*l_m)^2
       I_m = PI*r_m^3*t_m
       L_n <= 9.87*E*I_n/(K*l_n)^2
       I_n = PI*r_n^3*t_n
       2*r_m/t_m <= 40
       2*r_m/t_n <= 40
       h_{hold} >= 2*w_{t_m} + 2*r_m
       0.8 >= 2*w_{t_n} + 2*r_n
       W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m}))
       W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n})
       W_{lg} >= C_{lg}*(W_{mg} + W_{ng})
       W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m
       x_m >= x_{CG_{lg}}
     c_{root} = c_0
     Mission1.Aircraft.Wing.WingBox.r_{w/c} = Mission1.Aircraft.Fuselage.r_{w/c}
     x_w = x_{wing}
     Mission1.Aircraft.Fuselage.N_{lift} = Mission1.Aircraft.Wing.WingBox.N_{lift}
     f_{L_{total/wing}}*L_{max} >= Mission1.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}}
     W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc}
     W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
     W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
     W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:]
     W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:]
     W_{total}[:] <= W_{total, max}
     f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}}
     W_{misc} >= W_{lg} + W_{hpesys}
     W_{hpesys} = f_{hpesys}*W_{total, max}
     x_n <= l_{nose}
     x_m >= x_{wing}
     \Delta x_{AC_{wing}} + x_{wing} >= x_m
     x_{hpesys} = 1.1*l_{nose}
     x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys}
     d_{nacelle} >= d_{f} + 2*t_{nacelle}
     E_{land} >= W_{total, max}/(2*g)*w_{ult}^2
     x_{up} = x_{shell2}
     L_n = W_{total, max}*\Delta x_m/B
     L_m = W_{total, max}*\Delta x_n/B
     L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max}
     y_{eng} >= y_m
     3*n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}}
     V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse}
     W_{tail} >= n_{vt}*W_{vt} + W_{ht}
     2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db}
     B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v})
     m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht}
     x_{CG_{ht}} <= l_{fuse}
     V_{ht} = S_{ht}*l_{ht}/(S*mac)
     L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}}
     L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}}
     x_{CG_{vt}} <= l_{fuse}
     V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b)
     n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max}
     n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng}
     D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}}
     I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:]
     I_{z}[:] <= I_{z, max}
     S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2
     l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}}
     f_{S_{nacelle}} = S_{nacelle}*S^-1
     A_{inlet} = 0.4*S_{nacelle}
     A_{fancowl} = 0.2*S_{nacelle}
     A_{exh} = 0.4*S_{nacelle}
     A_{corecowl} = 3PI*d_{LPC}^2
       W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl})
       W_{eadd} = f_{eadd}*W_{engine}
     W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon}
     W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine})
     y_{eng} = 0.5*w_{fuse}
     (L_{max} - Mission1.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission1.Aircraft.Wing.WingBox.M_r*c_{root}
     A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend})
     A_{1h_{MLF}} >= (Mission1.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h})
     I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16)
     I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81
     I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81)
     x_{shell2} + l_{cone} >= x_{eng}
     x_{eng} >= x_{shell2} + 0.75*l_{cone}
     S_{floor} = 0.312*P_{floor}
     M_{floor} = 0.0352*P_{floor}*w_{floor}
     \Delta R_{fuse} = R_{fuse}*0.43/1.75
     b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2
     b_{ht_{out}} = 0.5*b_{ht} - w_{fuse}
     L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}}
     M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}}
     L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}}
     c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach}
     \pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht})
 
 FlightSegment
   FlightState
       V[:] = V[:]
       a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
       V[:] = M[:]*a[:]
     
     Altitude
       h[:] = hft[:]
     
     Atmosphere
       (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
       \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
       T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
       \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
   
   FlightP
     P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:]
     RC[:] = P_{excess}[:]/W_{avg}[:]
     \theta[:]*V[:] = RC[:]
     dhft[:] = tmin[:]*RC[:]
     R_{segment}[:] = thr[:]*V[:]
       WingPerformance
         0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:]
         \Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:]
         \Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2
         (AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2
         C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:]
         \alpha_w[:] <= \alpha_{max,w}[:]
         D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:]
         C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:]
         C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR)
         Re_w[:] = \rho[:]*V[:]*mac/\mu[:]
         C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114
       
       FuselagePerformance
         (no constraints)
       
       VerticalTailPerformance
         D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:]
         Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:]
         C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577
       
       HorizontalTailPerformance
         L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:]
         C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:]
         \alpha_{ht}[:] <= \alpha_{ht,max}
         C_{L_{\alpha,ht_0}}[:] = 6.28
         D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:]
         C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht})
         Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:]
         C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852
       W_{burn}[:] = W_{burn}[:]
       F_{fuel}[:] = F_{fuel}[:]
       \rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:])
       P_{cabin}[:] = 7.5e+04
       T_{cabin}[:] = 297
       V[:] >= V_{stall}[:]
       W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:]
       tmin[:] = thr[:]
       L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:]
       L_{total}[:] = f_{L_{total/wing}}*L_w[:]
       L_{total}[:] >= W_{avg}[:] + L_{ht}[:]
       D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2
       D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:])
       C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S)
       L/D[:] = W_{avg}[:]/D[:]
       W_{Load}[:] <= W_{Load_{max}}[:]
       W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S
       p_{o}[:] >= L_w[:]*c_{root}/S
       \eta_{o}[:] = w_{fuse}/(b/2)
       x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:]
       c_{m_{w}}[:] = 1.9
       x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2)
       x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse}
       x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}}
       x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}}
       C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht}
       AR_{ht} >= 4
       C_{L_{ht}}[:] >= 0.01
       SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac
       SM[:] >= SM_{min}
       SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}}
       x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:]
       R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:]
       C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2
       V_{nacelle}[:] = r_{v_{nacelle}}*V[:]
       V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]]
       r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0)
       C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0
       D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S
       \Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}}
   M_2[:3] = M[:3]
   M_{2.5}[:3] = 0.6
   hold_{2}[:3] = 1.07164
   hold_{2.5}[:3] = 1.06372
   P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:]
   c1[:] = 1 + 0.201*M[:]^2.0
   M_2[3:] = M[3:]
   M_{2.5}[3:] = 0.6
   hold_{2}[3:] = 1.07164
   hold_{2.5}[3:] = 1.06372
Beginning signomial solve.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 936             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 769
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3438              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.05              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.45e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 2.9e+003 1.3e+005 0.00e+000  -1.280976207e+005 2.000000000e+000  1.0e+000 0.09  
1   1.1e+003 1.4e+003 6.3e+004 -9.71e-001 -1.260360597e+005 3.611424052e+000  4.9e-001 0.14  
2   4.1e+002 5.3e+002 2.3e+004 -9.38e-001 -1.195206719e+005 1.063331153e+001  1.8e-001 0.17  
3   2.9e+002 3.7e+002 1.6e+004 -8.34e-001 -1.151942168e+005 6.795829655e+001  1.3e-001 0.20  
4   2.8e+002 3.7e+002 1.6e+004 -7.59e-001 -1.127212826e+005 2.109723808e+003  1.3e-001 0.23  
5   8.8e+001 1.1e+002 5.0e+003 -7.53e-001 -8.071413615e+004 8.411072422e+003  3.9e-002 0.27  
6   3.7e+001 4.8e+001 2.1e+003 -2.93e-001 -4.787028059e+004 1.016025756e+004  1.6e-002 0.28  
7   2.1e+001 2.8e+001 1.2e+003 2.52e-001  -3.173778936e+004 7.155034269e+003  9.5e-003 0.31  
8   9.4e+000 1.2e+001 5.3e+002 5.36e-001  -1.511150083e+004 4.167123567e+003  4.2e-003 0.33  
9   5.5e+000 7.1e+000 3.1e+002 8.14e-001  -8.836155418e+003 2.832992813e+003  2.5e-003 0.36  
10  1.3e+000 1.7e+000 7.6e+001 9.07e-001  -2.021517100e+003 9.278094940e+002  6.1e-004 0.38  
11  7.0e-001 9.1e-001 4.0e+001 9.94e-001  -8.292899266e+002 7.204982019e+002  3.2e-004 0.41  
12  4.7e-001 6.1e-001 2.7e+001 9.97e-001  -4.810408396e+002 5.632816117e+002  2.1e-004 0.42  
13  3.5e-001 7.3e-001 2.0e+001 9.79e-001  -3.119899248e+002 4.857188935e+002  1.6e-004 0.45  
14  1.7e-001 3.5e-001 9.8e+000 9.96e-001  -1.727746611e+001 3.656933383e+002  7.9e-005 0.48  
15  5.5e-002 1.5e-001 3.2e+000 9.94e-001  1.624902967e+002  2.901499707e+002  2.7e-005 0.50  
16  3.2e-002 1.3e-001 1.9e+000 1.00e+000  1.999027139e+002  2.746125040e+002  1.6e-005 0.53  
17  5.1e-003 1.8e-001 3.2e-001 1.00e+000  2.445305033e+002  2.572371524e+002  2.8e-006 0.56  
18  1.5e-003 1.3e-001 9.6e-002 1.00e+000  2.509424510e+002  2.546897023e+002  8.3e-007 0.58  
19  4.8e-004 1.1e-001 3.2e-002 1.00e+000  2.527845502e+002  2.540210950e+002  2.8e-007 0.61  
20  2.1e-004 8.6e-002 1.4e-002 1.00e+000  2.532880856e+002  2.538352203e+002  1.2e-007 0.64  
21  1.9e-004 7.8e-002 1.3e-002 1.00e+000  2.533292209e+002  2.538216573e+002  1.1e-007 0.66  
22  1.7e-004 7.1e-002 1.1e-002 1.00e+000  2.533650962e+002  2.538082643e+002  1.0e-007 0.69  
23  1.5e-004 6.4e-002 1.0e-002 1.00e+000  2.533974267e+002  2.537962616e+002  9.0e-008 0.72  
24  1.4e-004 5.9e-002 9.2e-003 1.00e+000  2.534264980e+002  2.537854354e+002  8.1e-008 0.75  
25  1.2e-004 5.4e-002 8.3e-003 1.00e+000  2.534526435e+002  2.537756756e+002  7.3e-008 0.77  
26  1.1e-004 4.9e-002 7.5e-003 1.00e+000  2.534761571e+002  2.537668763e+002  6.5e-008 0.80  
27  1.0e-004 4.5e-002 6.7e-003 1.00e+000  2.534973060e+002  2.537589453e+002  5.9e-008 0.83  
28  9.0e-005 4.1e-002 6.1e-003 1.00e+000  2.535163290e+002  2.537517977e+002  5.3e-008 0.84  
29  8.1e-005 3.8e-002 5.4e-003 1.00e+000  2.535334405e+002  2.537453571e+002  4.8e-008 0.87  
30  7.3e-005 3.5e-002 4.9e-003 1.00e+000  2.535488335e+002  2.537395540e+002  4.3e-008 0.91  
31  6.6e-005 3.2e-002 4.4e-003 1.00e+000  2.535626808e+002  2.537343259e+002  3.9e-008 0.92  
32  5.9e-005 3.0e-002 4.0e-003 1.00e+000  2.535751383e+002  2.537296160e+002  3.5e-008 0.95  
33  5.3e-005 2.7e-002 3.6e-003 1.00e+000  2.535863455e+002  2.537253733e+002  3.1e-008 0.97  
34  4.8e-005 2.5e-002 3.2e-003 1.00e+000  2.535964283e+002  2.537215515e+002  2.8e-008 1.00  
35  4.3e-005 2.4e-002 2.9e-003 1.00e+000  2.536054996e+002  2.537181092e+002  2.5e-008 1.01  
36  3.9e-005 2.2e-002 2.6e-003 1.00e+000  2.536136611e+002  2.537150086e+002  2.3e-008 1.04  
37  3.5e-005 2.0e-002 2.3e-003 1.00e+000  2.536210042e+002  2.537122161e+002  2.1e-008 1.06  
38  3.2e-005 1.9e-002 2.1e-003 1.00e+000  2.536276109e+002  2.537097011e+002  1.9e-008 1.08  
39  2.8e-005 1.8e-002 1.9e-003 1.00e+000  2.536335554e+002  2.537074360e+002  1.7e-008 1.11  
40  2.6e-005 1.7e-002 1.7e-003 1.00e+000  2.536389040e+002  2.537053963e+002  1.5e-008 1.14  
41  2.3e-005 1.6e-002 1.5e-003 1.00e+000  2.536437166e+002  2.537035594e+002  1.3e-008 1.16  
42  2.1e-005 1.5e-002 1.4e-003 1.00e+000  2.536480470e+002  2.537019053e+002  1.2e-008 1.19  
43  1.9e-005 1.4e-002 1.2e-003 1.00e+000  2.536519435e+002  2.537004158e+002  1.1e-008 1.20  
44  1.7e-005 1.4e-002 1.1e-003 1.00e+000  2.536554497e+002  2.536990747e+002  9.8e-009 1.23  
45  1.5e-005 1.3e-002 1.0e-003 1.00e+000  2.536586047e+002  2.536978672e+002  8.9e-009 1.26  
46  1.4e-005 1.3e-002 9.1e-004 1.00e+000  2.536614438e+002  2.536967800e+002  8.0e-009 1.29  
47  1.2e-005 1.2e-002 8.2e-004 1.00e+000  2.536639986e+002  2.536958012e+002  7.2e-009 1.33  
48  1.1e-005 1.2e-002 7.4e-004 1.00e+000  2.536662977e+002  2.536949200e+002  6.5e-009 1.34  
49  9.9e-006 1.1e-002 6.6e-004 1.00e+000  2.536683666e+002  2.536941267e+002  5.8e-009 1.37  
50  8.9e-006 1.1e-002 6.0e-004 1.00e+000  2.536702284e+002  2.536934125e+002  5.2e-009 1.40  
51  8.0e-006 1.0e-002 5.4e-004 1.00e+000  2.536719039e+002  2.536927696e+002  4.7e-009 1.44  
52  7.2e-006 1.0e-002 4.8e-004 1.00e+000  2.536734117e+002  2.536921909e+002  4.2e-009 1.47  
53  6.5e-006 9.9e-003 4.3e-004 1.00e+000  2.536747686e+002  2.536916699e+002  3.8e-009 1.48  
54  5.8e-006 9.6e-003 3.9e-004 1.00e+000  2.536759897e+002  2.536912009e+002  3.4e-009 1.51  
55  5.3e-006 9.4e-003 3.5e-004 1.00e+000  2.536770886e+002  2.536907787e+002  3.1e-009 1.54  
56  4.7e-006 9.2e-003 3.2e-004 1.00e+000  2.536780776e+002  2.536903987e+002  2.8e-009 1.56  
57  4.3e-006 9.0e-003 2.9e-004 1.00e+000  2.536789676e+002  2.536900566e+002  2.5e-009 1.59  
58  3.8e-006 8.9e-003 2.6e-004 1.00e+000  2.536797686e+002  2.536897487e+002  2.3e-009 1.61  
59  3.4e-006 8.7e-003 2.3e-004 1.00e+000  2.536804894e+002  2.536894716e+002  2.0e-009 1.62  
60  3.1e-006 8.6e-003 2.1e-004 1.00e+000  2.536811381e+002  2.536892221e+002  1.8e-009 1.65  
61  1.2e-006 3.3e-003 8.1e-005 1.00e+000  2.536846984e+002  2.536878513e+002  7.1e-010 1.67  
62  1.1e-006 3.0e-003 7.3e-005 1.00e+000  2.536849266e+002  2.536877643e+002  6.4e-010 1.70  
63  3.9e-007 1.1e-003 2.6e-005 1.00e+000  2.536862390e+002  2.536872587e+002  2.3e-010 1.72  
64  3.5e-007 9.7e-004 2.4e-005 1.00e+000  2.536863127e+002  2.536872304e+002  2.1e-010 1.73  
65  3.2e-007 8.8e-004 2.1e-005 1.00e+000  2.536863789e+002  2.536872048e+002  1.9e-010 1.76  
66  2.8e-007 7.9e-004 1.9e-005 1.00e+000  2.536864385e+002  2.536871818e+002  1.7e-010 1.78  
67  2.6e-007 7.1e-004 1.7e-005 1.00e+000  2.536864921e+002  2.536871611e+002  1.5e-010 1.81  
68  2.3e-007 6.4e-004 1.5e-005 1.00e+000  2.536865404e+002  2.536871425e+002  1.4e-010 1.83  
69  2.1e-007 5.7e-004 1.4e-005 9.99e-001  2.536865838e+002  2.536871257e+002  1.2e-010 1.84  
70  1.9e-007 5.2e-004 1.3e-005 1.00e+000  2.536866229e+002  2.536871106e+002  1.1e-010 1.87  
71  1.7e-007 4.7e-004 1.1e-005 1.00e+000  2.536866581e+002  2.536870971e+002  9.9e-011 1.89  
72  1.5e-007 4.2e-004 1.0e-005 1.00e+000  2.536866898e+002  2.536870848e+002  8.9e-011 1.92  
73  1.4e-007 3.8e-004 9.1e-006 9.99e-001  2.536867183e+002  2.536870738e+002  8.0e-011 1.94  
74  1.2e-007 3.4e-004 8.2e-006 1.00e+000  2.536867439e+002  2.536870639e+002  7.2e-011 1.97  
75  1.1e-007 3.1e-004 7.4e-006 1.00e+000  2.536867670e+002  2.536870550e+002  6.5e-011 1.98  
76  9.9e-008 2.7e-004 6.7e-006 1.00e+000  2.536867878e+002  2.536870470e+002  5.8e-011 2.00  
77  8.9e-008 2.5e-004 6.0e-006 9.99e-001  2.536868064e+002  2.536870398e+002  5.3e-011 2.03  
78  8.0e-008 2.2e-004 5.4e-006 1.00e+000  2.536868233e+002  2.536870332e+002  4.7e-011 2.04  
79  7.2e-008 2.0e-004 4.9e-006 9.98e-001  2.536868385e+002  2.536870274e+002  4.3e-011 2.08  
80  6.5e-008 1.8e-004 4.4e-006 1.00e+000  2.536868521e+002  2.536870221e+002  3.8e-011 2.09  
81  5.9e-008 1.6e-004 3.9e-006 9.98e-001  2.536868643e+002  2.536870174e+002  3.5e-011 2.12  
82  5.3e-008 1.5e-004 3.5e-006 1.00e+000  2.536868754e+002  2.536870131e+002  3.1e-011 2.14  
83  4.8e-008 1.3e-004 3.2e-006 9.96e-001  2.536868853e+002  2.536870093e+002  2.8e-011 2.15  
84  4.3e-008 1.2e-004 2.9e-006 1.00e+000  2.536868943e+002  2.536870058e+002  2.5e-011 2.18  
85  3.8e-008 1.1e-004 2.6e-006 9.96e-001  2.536869024e+002  2.536870027e+002  2.3e-011 2.21  
86  3.5e-008 9.6e-005 2.3e-006 1.01e+000  2.536869099e+002  2.536869997e+002  2.0e-011 2.23  
87  3.1e-008 8.6e-005 2.1e-006 1.00e+000  2.536869165e+002  2.536869972e+002  1.8e-011 2.26  
88  2.8e-008 7.8e-005 1.9e-006 1.00e+000  2.536869224e+002  2.536869949e+002  1.7e-011 2.28  
89  2.5e-008 7.0e-005 1.7e-006 9.99e-001  2.536869276e+002  2.536869929e+002  1.5e-011 2.31  
90  2.3e-008 6.3e-005 1.5e-006 9.99e-001  2.536869323e+002  2.536869910e+002  1.3e-011 2.33  
91  2.0e-008 5.7e-005 1.4e-006 1.00e+000  2.536869366e+002  2.536869894e+002  1.2e-011 2.34  
92  1.8e-008 5.1e-005 1.2e-006 1.01e+000  2.536869405e+002  2.536869879e+002  1.1e-011 2.37  
93  1.7e-008 4.6e-005 1.1e-006 1.01e+000  2.536869440e+002  2.536869865e+002  9.9e-012 2.39  
94  1.5e-008 4.1e-005 1.0e-006 1.00e+000  2.536869471e+002  2.536869853e+002  8.9e-012 2.42  
95  1.3e-008 3.7e-005 9.0e-007 1.01e+000  2.536869500e+002  2.536869842e+002  8.1e-012 2.43  
96  1.2e-008 3.3e-005 8.1e-007 1.00e+000  2.536869524e+002  2.536869832e+002  7.3e-012 2.45  
97  1.1e-008 3.0e-005 7.3e-007 1.00e+000  2.536869547e+002  2.536869824e+002  6.5e-012 2.48  
98  9.8e-009 2.7e-005 6.6e-007 9.94e-001  2.536869567e+002  2.536869816e+002  5.9e-012 2.50  
Interior-point optimizer terminated. Time: 2.50. 

Optimizer terminated. Time: 2.51    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 2.5368695666e+002   Viol.  con: 2e-007   var: 0e+000 
  Dual.    obj: 2.5368698159e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.53 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 935
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 935             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 770
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3440              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.45e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.281787446e+005 2.000000000e+000  1.0e+000 0.06  
1   1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.259414228e+005 3.780941016e+000  4.7e-001 0.09  
2   4.6e+002 5.9e+002 2.6e+004 -9.35e-001 -1.205918795e+005 9.868922462e+000  2.0e-001 0.11  
3   2.9e+002 3.7e+002 1.6e+004 -8.50e-001 -1.154239527e+005 5.250197659e+001  1.3e-001 0.14  
4   2.9e+002 3.7e+002 1.6e+004 -7.62e-001 -1.133019475e+005 1.862130071e+003  1.3e-001 0.16  
5   8.3e+001 1.1e+002 4.6e+003 -7.57e-001 -7.812142134e+004 9.031239869e+003  3.6e-002 0.19  
6   3.6e+001 4.6e+001 2.0e+003 -2.53e-001 -4.675648593e+004 1.010078030e+004  1.6e-002 0.22  
7   1.9e+001 2.4e+001 1.0e+003 2.76e-001  -2.801894191e+004 6.402312649e+003  8.2e-003 0.25  
8   9.2e+000 1.2e+001 5.1e+002 6.02e-001  -1.471216454e+004 4.005088019e+003  4.0e-003 0.28  
9   5.7e+000 7.3e+000 3.2e+002 8.20e-001  -9.206577814e+003 2.776623709e+003  2.5e-003 0.30  
10  1.9e+000 2.4e+000 1.1e+002 9.02e-001  -2.967188408e+003 1.150548957e+003  8.4e-004 0.33  
11  1.6e+000 2.0e+000 8.8e+001 9.75e-001  -2.411824662e+003 1.013250398e+003  7.0e-004 0.36  
12  1.0e+000 1.4e+000 5.6e+001 9.78e-001  -1.467425724e+003 7.220755517e+002  4.4e-004 0.37  
13  4.6e-001 6.8e-001 2.6e+001 9.83e-001  -5.896883404e+002 4.319681553e+002  2.1e-004 0.41  
14  2.5e-001 3.8e-001 1.4e+001 1.00e+000  -2.320840757e+002 3.288887967e+002  1.1e-004 0.44  
15  1.0e-001 1.6e-001 5.7e+000 1.00e+000  1.044651513e+001  2.360029562e+002  4.6e-005 0.45  
16  4.7e-002 1.0e-001 2.7e+000 1.00e+000  9.574902024e+001  2.020284288e+002  2.2e-005 0.48  
17  1.0e-002 1.4e-001 6.2e-001 1.01e+000  1.548431127e+002  1.790677319e+002  5.2e-006 0.50  
18  6.3e-003 1.0e-001 3.9e-001 1.01e+000  1.614292043e+002  1.765011124e+002  3.2e-006 0.53  
19  1.6e-003 1.2e-001 1.0e-001 1.01e+000  1.695627743e+002  1.734405848e+002  8.5e-007 0.56  
20  3.4e-004 1.4e-001 2.2e-002 1.01e+000  1.717721243e+002  1.726293360e+002  1.9e-007 0.58  
21  1.4e-004 1.0e-001 9.5e-003 9.94e-001  1.721372139e+002  1.725037900e+002  8.3e-008 0.61  
22  8.9e-005 8.2e-002 6.0e-003 1.00e+000  1.722347056e+002  1.724653291e+002  5.2e-008 0.62  
23  8.0e-005 7.6e-002 5.4e-003 1.00e+000  1.722527904e+002  1.724604213e+002  4.7e-008 0.66  
24  7.2e-005 6.9e-002 4.8e-003 1.00e+000  1.722680412e+002  1.724549098e+002  4.2e-008 0.69  
25  6.5e-005 6.3e-002 4.3e-003 1.00e+000  1.722818159e+002  1.724499967e+002  3.8e-008 0.70  
26  5.9e-005 5.7e-002 3.9e-003 1.00e+000  1.722941843e+002  1.724455456e+002  3.4e-008 0.73  
27  5.3e-005 5.2e-002 3.5e-003 1.00e+000  1.723053033e+002  1.724415269e+002  3.1e-008 0.76  
28  4.7e-005 4.8e-002 3.2e-003 1.00e+000  1.723152954e+002  1.724378951e+002  2.8e-008 0.78  
29  4.3e-005 4.4e-002 2.8e-003 1.00e+000  1.723242747e+002  1.724346130e+002  2.5e-008 0.81  
30  3.8e-005 4.0e-002 2.6e-003 1.00e+000  1.723323437e+002  1.724316469e+002  2.2e-008 0.83  
31  3.5e-005 3.7e-002 2.3e-003 1.00e+000  1.723395950e+002  1.724289668e+002  2.0e-008 0.84  
32  3.1e-005 3.4e-002 2.1e-003 1.00e+000  1.723461119e+002  1.724265457e+002  1.8e-008 0.87  
33  2.8e-005 3.2e-002 1.9e-003 1.00e+000  1.723519695e+002  1.724243592e+002  1.6e-008 0.89  
34  2.5e-005 2.9e-002 1.7e-003 1.00e+000  1.723572351e+002  1.724223852e+002  1.5e-008 0.92  
35  2.3e-005 2.7e-002 1.5e-003 1.00e+000  1.723619690e+002  1.724206036e+002  1.3e-008 0.94  
36  2.0e-005 2.5e-002 1.4e-003 1.00e+000  1.723662253e+002  1.724189962e+002  1.2e-008 0.95  
37  1.8e-005 2.4e-002 1.2e-003 1.00e+000  1.723700526e+002  1.724175461e+002  1.1e-008 0.98  
38  1.7e-005 2.2e-002 1.1e-003 1.00e+000  1.723734942e+002  1.724162382e+002  9.7e-009 1.00  
39  1.5e-005 2.1e-002 9.9e-004 1.00e+000  1.723765894e+002  1.724150588e+002  8.7e-009 1.03  
40  1.3e-005 1.9e-002 8.9e-004 1.00e+000  1.723793730e+002  1.724139955e+002  7.8e-009 1.04  
41  1.2e-005 1.8e-002 8.0e-004 1.00e+000  1.723818767e+002  1.724130368e+002  7.1e-009 1.06  
42  1.1e-005 1.7e-002 7.2e-004 1.00e+000  1.723841286e+002  1.724121727e+002  6.4e-009 1.09  
43  9.8e-006 1.6e-002 6.5e-004 1.00e+000  1.723861541e+002  1.724113938e+002  5.7e-009 1.12  
44  8.8e-006 1.5e-002 5.9e-004 1.00e+000  1.723879762e+002  1.724106919e+002  5.1e-009 1.14  
45  7.9e-006 1.5e-002 5.3e-004 1.00e+000  1.723896152e+002  1.724100594e+002  4.6e-009 1.17  
46  7.1e-006 1.4e-002 4.8e-004 1.00e+000  1.723910896e+002  1.724094894e+002  4.2e-009 1.19  
47  6.4e-006 1.3e-002 4.3e-004 1.00e+000  1.723924160e+002  1.724089759e+002  3.8e-009 1.22  
48  5.8e-006 1.3e-002 3.9e-004 1.00e+000  1.723936093e+002  1.724085133e+002  3.4e-009 1.23  
49  5.2e-006 1.2e-002 3.5e-004 1.00e+000  1.723946829e+002  1.724080965e+002  3.0e-009 1.25  
50  4.7e-006 1.2e-002 3.1e-004 1.00e+000  1.723956488e+002  1.724077211e+002  2.7e-009 1.28  
51  4.2e-006 1.1e-002 2.8e-004 1.00e+000  1.723965178e+002  1.724073829e+002  2.5e-009 1.29  
52  3.8e-006 1.1e-002 2.5e-004 1.00e+000  1.723972997e+002  1.724070784e+002  2.2e-009 1.33  
53  3.4e-006 1.1e-002 2.3e-004 1.00e+000  1.723980032e+002  1.724068040e+002  2.0e-009 1.34  
54  3.1e-006 1.0e-002 2.0e-004 1.00e+000  1.723986362e+002  1.724065570e+002  1.8e-009 1.36  
55  2.8e-006 1.0e-002 1.8e-004 1.00e+000  1.723992058e+002  1.724063345e+002  1.6e-009 1.39  
56  2.5e-006 9.7e-003 1.7e-004 1.00e+000  1.723997182e+002  1.724061342e+002  1.5e-009 1.40  
57  2.2e-006 9.5e-003 1.5e-004 1.00e+000  1.724001794e+002  1.724059537e+002  1.3e-009 1.44  
58  2.0e-006 9.3e-003 1.3e-004 1.00e+000  1.724005943e+002  1.724057913e+002  1.2e-009 1.45  
59  1.8e-006 9.1e-003 1.2e-004 1.00e+000  1.724009677e+002  1.724056450e+002  1.1e-009 1.47  
60  1.6e-006 9.0e-003 1.1e-004 1.00e+000  1.724013037e+002  1.724055132e+002  9.5e-010 1.50  
61  1.5e-006 8.8e-003 9.8e-005 1.00e+000  1.724016060e+002  1.724053946e+002  8.6e-010 1.51  
62  1.3e-006 8.7e-003 8.8e-005 1.00e+000  1.724018780e+002  1.724052878e+002  7.7e-010 1.54  
63  1.2e-006 8.6e-003 7.9e-005 1.00e+000  1.724021228e+002  1.724051917e+002  7.0e-010 1.56  
64  1.1e-006 8.5e-003 7.1e-005 1.00e+000  1.724023431e+002  1.724051051e+002  6.3e-010 1.58  
65  9.6e-007 8.4e-003 6.4e-005 1.00e+000  1.724025413e+002  1.724050271e+002  5.6e-010 1.61  
66  8.7e-007 8.3e-003 5.8e-005 1.00e+000  1.724027197e+002  1.724049570e+002  5.1e-010 1.62  
67  7.8e-007 8.2e-003 5.2e-005 1.00e+000  1.724028802e+002  1.724048938e+002  4.6e-010 1.65  
68  7.0e-007 8.1e-003 4.7e-005 1.00e+000  1.724030247e+002  1.724048369e+002  4.1e-010 1.67  
69  6.3e-007 8.0e-003 4.2e-005 1.00e+000  1.724031547e+002  1.724047856e+002  3.7e-010 1.70  
70  5.7e-007 8.0e-003 3.8e-005 1.00e+000  1.724032716e+002  1.724047395e+002  3.3e-010 1.72  
71  5.1e-007 7.9e-003 3.4e-005 1.00e+000  1.724033769e+002  1.724046980e+002  3.0e-010 1.73  
72  4.6e-007 7.9e-003 3.1e-005 1.00e+000  1.724034716e+002  1.724046606e+002  2.7e-010 1.76  
73  4.1e-007 7.8e-003 2.8e-005 1.00e+000  1.724035569e+002  1.724046270e+002  2.4e-010 1.78  
74  3.7e-007 7.8e-003 2.5e-005 1.00e+000  1.724036336e+002  1.724045967e+002  2.2e-010 1.81  
75  3.4e-007 7.7e-003 2.2e-005 1.00e+000  1.724037026e+002  1.724045694e+002  2.0e-010 1.83  
76  3.0e-007 7.7e-003 2.0e-005 1.00e+000  1.724037647e+002  1.724045448e+002  1.8e-010 1.84  
77  2.7e-007 7.7e-003 1.8e-005 1.00e+000  1.724038206e+002  1.724045227e+002  1.6e-010 1.87  
78  2.4e-007 7.6e-003 1.6e-005 1.00e+000  1.724038709e+002  1.724045028e+002  1.4e-010 1.89  
79  2.2e-007 7.6e-003 1.5e-005 1.00e+000  1.724039162e+002  1.724044849e+002  1.3e-010 1.92  
80  2.0e-007 7.6e-003 1.3e-005 1.00e+000  1.724039569e+002  1.724044687e+002  1.2e-010 1.93  
81  1.8e-007 7.5e-003 1.2e-005 1.00e+000  1.724039936e+002  1.724044542e+002  1.0e-010 1.97  
82  1.6e-007 7.5e-003 1.1e-005 1.00e+000  1.724040265e+002  1.724044411e+002  9.4e-011 1.98  
83  1.4e-007 7.5e-003 9.6e-006 1.00e+000  1.724040562e+002  1.724044294e+002  8.5e-011 2.00  
84  1.3e-007 7.5e-003 8.7e-006 1.00e+000  1.724040829e+002  1.724044188e+002  7.6e-011 2.03  
85  1.2e-007 7.5e-003 7.8e-006 1.00e+000  1.724041070e+002  1.724044092e+002  6.9e-011 2.04  
86  1.1e-007 7.4e-003 7.0e-006 1.00e+000  1.724041286e+002  1.724044006e+002  6.2e-011 2.07  
87  9.5e-008 7.4e-003 6.3e-006 1.00e+000  1.724041481e+002  1.724043929e+002  5.6e-011 2.09  
88  8.5e-008 7.4e-003 5.7e-006 9.99e-001  1.724041656e+002  1.724043859e+002  5.0e-011 2.11  
89  7.7e-008 7.4e-003 5.1e-006 1.00e+000  1.724041814e+002  1.724043797e+002  4.5e-011 2.14  
90  6.9e-008 7.4e-003 4.6e-006 1.00e+000  1.724041956e+002  1.724043740e+002  4.0e-011 2.15  
91  6.2e-008 7.4e-003 4.2e-006 1.00e+000  1.724042083e+002  1.724043689e+002  3.6e-011 2.18  
92  5.6e-008 7.3e-003 3.7e-006 1.00e+000  1.724042198e+002  1.724043644e+002  3.3e-011 2.21  
93  5.0e-008 7.3e-003 3.4e-006 1.00e+000  1.724042301e+002  1.724043603e+002  3.0e-011 2.23  
94  4.5e-008 7.3e-003 3.0e-006 1.00e+000  1.724042395e+002  1.724043565e+002  2.7e-011 2.25  
95  4.1e-008 7.3e-003 2.7e-006 9.98e-001  1.724042478e+002  1.724043532e+002  2.4e-011 2.28  
96  3.7e-008 7.3e-003 2.5e-006 9.99e-001  1.724042554e+002  1.724043502e+002  2.2e-011 2.29  
97  3.3e-008 7.3e-003 2.2e-006 1.00e+000  1.724042621e+002  1.724043475e+002  1.9e-011 2.32  
98  3.0e-008 7.3e-003 2.0e-006 9.99e-001  1.724042682e+002  1.724043451e+002  1.7e-011 2.34  
99  2.7e-008 7.3e-003 1.8e-006 1.00e+000  1.724042737e+002  1.724043429e+002  1.6e-011 2.36  
100 2.4e-008 7.2e-003 1.6e-006 1.00e+000  1.724042787e+002  1.724043409e+002  1.4e-011 2.39  
101 2.2e-008 7.2e-003 1.4e-006 1.00e+000  1.724042831e+002  1.724043391e+002  1.3e-011 2.40  
102 2.0e-008 7.2e-003 1.3e-006 9.98e-001  1.724042871e+002  1.724043375e+002  1.1e-011 2.42  
103 1.8e-008 7.2e-003 1.2e-006 9.99e-001  1.724042907e+002  1.724043361e+002  1.0e-011 2.45  
104 1.6e-008 7.2e-003 1.1e-006 9.98e-001  1.724042940e+002  1.724043348e+002  9.3e-012 2.46  
105 4.0e-009 1.8e-003 2.7e-007 1.01e+000  1.724043158e+002  1.724043260e+002  2.3e-012 2.48  
106 3.6e-009 1.6e-003 2.4e-007 1.01e+000  1.724043166e+002  1.724043257e+002  2.1e-012 2.51  
107 9.7e-010 3.5e-004 5.2e-008 9.92e-001  1.724043217e+002  1.724043237e+002  4.6e-013 2.53  
Interior-point optimizer terminated. Time: 2.54. 

Optimizer terminated. Time: 2.56    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.7240432170e+002   Viol.  con: 1e-008   var: 0e+000 
  Dual.    obj: 1.7240432369e+002   Viol.  con: 0e+000   var: 3e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.57 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 935
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 935             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.02    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 770
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3440              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.45e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.284360420e+005 2.000000000e+000  1.0e+000 0.05  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.262635412e+005 3.636950442e+000  4.8e-001 0.08  
2   4.4e+002 5.6e+002 2.4e+004 -9.36e-001 -1.203757411e+005 1.002085882e+001  1.9e-001 0.09  
3   2.9e+002 3.7e+002 1.6e+004 -8.43e-001 -1.156270477e+005 5.939196750e+001  1.3e-001 0.13  
4   2.9e+002 3.7e+002 1.6e+004 -7.62e-001 -1.131820433e+005 2.127606720e+003  1.3e-001 0.16  
5   8.1e+001 1.0e+002 4.5e+003 -7.56e-001 -7.750856797e+004 9.253344630e+003  3.6e-002 0.19  
6   4.0e+001 5.2e+001 2.2e+003 -2.39e-001 -5.068346157e+004 1.003935342e+004  1.8e-002 0.22  
7   3.0e+001 3.9e+001 1.7e+003 2.16e-001  -4.166687973e+004 8.310011522e+003  1.3e-002 0.25  
8   1.9e+001 2.4e+001 1.0e+003 3.78e-001  -2.878216349e+004 5.414761032e+003  8.2e-003 0.28  
9   8.0e+000 1.0e+001 4.4e+002 5.99e-001  -1.316010250e+004 3.160857189e+003  3.5e-003 0.31  
10  4.0e+000 5.1e+000 2.2e+002 8.45e-001  -6.347176213e+003 2.138436360e+003  1.8e-003 0.33  
11  2.2e+000 2.9e+000 1.3e+002 9.42e-001  -3.502090792e+003 1.318845329e+003  9.9e-004 0.36  
12  9.1e-001 1.2e+000 5.1e+001 9.75e-001  -1.332352653e+003 6.477137036e+002  4.1e-004 0.39  
13  8.3e-001 1.1e+000 4.6e+001 9.70e-001  -1.217518678e+003 6.005422671e+002  3.7e-004 0.41  
14  5.9e-001 7.7e-001 3.3e+001 9.74e-001  -8.114644924e+002 4.901671062e+002  2.6e-004 0.44  
15  2.1e-001 7.5e-001 1.2e+001 9.90e-001  -1.973607944e+002 2.838976848e+002  9.8e-005 0.45  
16  1.1e-001 3.8e-001 6.1e+000 1.00e+000  -2.194425166e+001 2.162391058e+002  4.9e-005 0.48  
17  7.7e-002 2.8e-001 4.4e+000 1.01e+000  2.773265252e+001  2.014223061e+002  3.6e-005 0.52  
18  5.2e-002 2.0e-001 3.0e+000 1.02e+000  7.871599114e+001  1.952109643e+002  2.4e-005 0.53  
19  1.5e-002 1.1e-001 8.7e-001 1.00e+000  1.409224792e+002  1.747335310e+002  7.0e-006 0.56  
20  4.0e-003 2.2e-001 2.5e-001 1.02e+000  1.602102570e+002  1.696952468e+002  2.0e-006 0.59  
21  2.7e-003 2.2e-001 1.7e-001 1.01e+000  1.623239075e+002  1.687770431e+002  1.3e-006 0.62  
22  2.0e-003 1.6e-001 1.2e-001 1.00e+000  1.636804090e+002  1.683151865e+002  9.6e-007 0.64  
23  7.7e-004 9.6e-002 4.8e-002 1.01e+000  1.657772227e+002  1.676105814e+002  3.9e-007 0.67  
24  3.6e-004 8.1e-002 2.3e-002 1.01e+000  1.664800830e+002  1.673455614e+002  1.8e-007 0.70  
25  1.5e-004 8.1e-002 9.6e-003 1.01e+000  1.668359782e+002  1.672046967e+002  7.9e-008 0.72  
26  1.4e-004 7.4e-002 8.7e-003 1.01e+000  1.668663976e+002  1.671983721e+002  7.1e-008 0.75  
27  1.2e-004 6.7e-002 7.8e-003 1.01e+000  1.668896219e+002  1.671882793e+002  6.4e-008 0.78  
28  1.1e-004 6.2e-002 7.0e-003 1.01e+000  1.669108059e+002  1.671795173e+002  5.8e-008 0.80  
29  1.0e-004 5.6e-002 6.3e-003 1.01e+000  1.669297034e+002  1.671714745e+002  5.2e-008 0.83  
30  9.0e-005 5.1e-002 5.7e-003 1.01e+000  1.669466561e+002  1.671641937e+002  4.7e-008 0.86  
31  8.1e-005 4.7e-002 5.1e-003 1.01e+000  1.669618594e+002  1.671575971e+002  4.2e-008 0.87  
32  7.3e-005 4.3e-002 4.6e-003 1.01e+000  1.669754999e+002  1.671516261e+002  3.8e-008 0.91  
33  6.5e-005 4.0e-002 4.2e-003 1.01e+000  1.669877404e+002  1.671462232e+002  3.4e-008 0.92  
34  5.9e-005 3.6e-002 3.7e-003 1.01e+000  1.669987263e+002  1.671413359e+002  3.1e-008 0.95  
35  5.3e-005 3.4e-002 3.4e-003 1.00e+000  1.670085877e+002  1.671369161e+002  2.8e-008 0.97  
36  4.8e-005 3.1e-002 3.0e-003 1.00e+000  1.670174409e+002  1.671329200e+002  2.5e-008 0.98  
37  4.3e-005 2.9e-002 2.7e-003 1.00e+000  1.670253901e+002  1.671293082e+002  2.2e-008 1.01  
38  3.9e-005 2.7e-002 2.5e-003 1.00e+000  1.670325285e+002  1.671260442e+002  2.0e-008 1.03  
39  3.5e-005 2.5e-002 2.2e-003 1.00e+000  1.670389395e+002  1.671230951e+002  1.8e-008 1.05  
40  3.1e-005 2.3e-002 2.0e-003 1.00e+000  1.670446980e+002  1.671204312e+002  1.6e-008 1.08  
41  2.8e-005 2.2e-002 1.8e-003 1.00e+000  1.670498709e+002  1.671180253e+002  1.5e-008 1.09  
42  2.5e-005 2.0e-002 1.6e-003 1.00e+000  1.670545182e+002  1.671158529e+002  1.3e-008 1.11  
43  2.3e-005 1.9e-002 1.5e-003 1.00e+000  1.670586939e+002  1.671138917e+002  1.2e-008 1.14  
44  2.1e-005 1.8e-002 1.3e-003 1.00e+000  1.670624461e+002  1.671121214e+002  1.1e-008 1.16  
45  1.8e-005 1.7e-002 1.2e-003 1.00e+000  1.670658181e+002  1.671105237e+002  9.6e-009 1.17  
46  1.7e-005 1.6e-002 1.1e-003 1.00e+000  1.670688487e+002  1.671090819e+002  8.7e-009 1.20  
47  1.5e-005 1.5e-002 9.5e-004 1.00e+000  1.670715727e+002  1.671077812e+002  7.8e-009 1.22  
48  1.3e-005 1.4e-002 8.6e-004 1.00e+000  1.670740213e+002  1.671066078e+002  7.0e-009 1.23  
49  1.2e-005 1.4e-002 7.7e-004 1.00e+000  1.670762224e+002  1.671055496e+002  6.3e-009 1.26  
50  1.1e-005 1.3e-002 6.9e-004 1.00e+000  1.670782014e+002  1.671045952e+002  5.7e-009 1.28  
51  9.8e-006 1.3e-002 6.2e-004 1.00e+000  1.670799807e+002  1.671037346e+002  5.1e-009 1.29  
52  8.8e-006 1.2e-002 5.6e-004 1.00e+000  1.670815806e+002  1.671029587e+002  4.6e-009 1.33  
53  8.0e-006 1.2e-002 5.1e-004 1.00e+000  1.670830192e+002  1.671022592e+002  4.2e-009 1.34  
54  7.2e-006 1.1e-002 4.6e-004 1.00e+000  1.670843130e+002  1.671016288e+002  3.7e-009 1.36  
55  6.4e-006 1.1e-002 4.1e-004 1.00e+000  1.670854766e+002  1.671010607e+002  3.4e-009 1.39  
56  5.8e-006 1.1e-002 3.7e-004 1.00e+000  1.670865231e+002  1.671005486e+002  3.0e-009 1.40  
57  5.2e-006 1.0e-002 3.3e-004 1.00e+000  1.670874644e+002  1.671000872e+002  2.7e-009 1.44  
58  1.6e-006 3.3e-003 1.1e-004 1.00e+000  1.670932319e+002  1.670972294e+002  8.6e-010 1.45  
59  1.5e-006 3.0e-003 9.5e-005 1.00e+000  1.670935008e+002  1.670970986e+002  7.8e-010 1.47  
60  1.3e-006 2.7e-003 8.5e-005 1.00e+000  1.670937446e+002  1.670969828e+002  7.0e-010 1.50  
61  5.3e-007 1.1e-003 3.4e-005 1.00e+000  1.670950404e+002  1.670963308e+002  2.8e-010 1.51  
62  4.8e-007 9.6e-004 3.1e-005 1.00e+000  1.670951288e+002  1.670962901e+002  2.5e-010 1.53  
63  4.3e-007 8.6e-004 2.8e-005 1.00e+000  1.670952060e+002  1.670962510e+002  2.3e-010 1.56  
64  3.9e-007 7.7e-004 2.5e-005 1.00e+000  1.670952755e+002  1.670962160e+002  2.0e-010 1.58  
65  3.5e-007 7.0e-004 2.2e-005 1.00e+000  1.670953380e+002  1.670961844e+002  1.8e-010 1.59  
66  3.1e-007 6.3e-004 2.0e-005 9.99e-001  1.670953942e+002  1.670961560e+002  1.6e-010 1.62  
67  2.8e-007 5.6e-004 1.8e-005 1.00e+000  1.670954447e+002  1.670961303e+002  1.5e-010 1.64  
68  2.5e-007 5.1e-004 1.6e-005 1.00e+000  1.670954902e+002  1.670961072e+002  1.3e-010 1.67  
69  2.3e-007 4.6e-004 1.5e-005 1.00e+000  1.670955311e+002  1.670960864e+002  1.2e-010 1.69  
70  2.1e-007 4.1e-004 1.3e-005 1.00e+000  1.670955679e+002  1.670960677e+002  1.1e-010 1.72  
71  1.8e-007 3.7e-004 1.2e-005 9.98e-001  1.670956010e+002  1.670960509e+002  9.7e-011 1.73  
72  1.7e-007 3.3e-004 1.1e-005 9.94e-001  1.670956308e+002  1.670960358e+002  8.7e-011 1.76  
73  1.5e-007 3.0e-004 9.6e-006 9.98e-001  1.670956576e+002  1.670960221e+002  7.9e-011 1.78  
74  1.3e-007 2.7e-004 8.6e-006 9.95e-001  1.670956818e+002  1.670960099e+002  7.1e-011 1.79  
75  1.2e-007 2.4e-004 7.8e-006 1.00e+000  1.670957035e+002  1.670959988e+002  6.4e-011 1.83  
76  1.1e-007 2.2e-004 7.0e-006 9.99e-001  1.670957230e+002  1.670959888e+002  5.7e-011 1.84  
77  9.8e-008 2.0e-004 6.3e-006 1.01e+000  1.670957410e+002  1.670959795e+002  5.2e-011 1.87  
78  8.8e-008 1.8e-004 5.7e-006 1.00e+000  1.670957568e+002  1.670959715e+002  4.7e-011 1.89  
79  8.0e-008 1.6e-004 5.1e-006 9.91e-001  1.670957710e+002  1.670959643e+002  4.2e-011 1.90  
80  7.2e-008 1.4e-004 4.6e-006 1.01e+000  1.670957845e+002  1.670959573e+002  3.8e-011 1.94  
81  6.4e-008 1.3e-004 4.1e-006 1.01e+000  1.670957964e+002  1.670959512e+002  3.4e-011 1.95  
82  5.8e-008 1.2e-004 3.7e-006 1.01e+000  1.670958068e+002  1.670959458e+002  3.1e-011 1.97  
83  5.2e-008 1.0e-004 3.3e-006 1.00e+000  1.670958161e+002  1.670959411e+002  2.8e-011 2.00  
84  4.7e-008 9.4e-005 3.0e-006 9.99e-001  1.670958243e+002  1.670959369e+002  2.5e-011 2.01  
85  4.2e-008 8.5e-005 2.7e-006 9.94e-001  1.670958318e+002  1.670959331e+002  2.3e-011 2.03  
86  3.8e-008 7.6e-005 2.4e-006 9.71e-001  1.670958385e+002  1.670959298e+002  2.0e-011 2.06  
87  3.4e-008 6.9e-005 2.2e-006 1.00e+000  1.670958445e+002  1.670959267e+002  1.8e-011 2.08  
88  3.1e-008 6.2e-005 2.0e-006 1.02e+000  1.670958503e+002  1.670959237e+002  1.7e-011 2.09  
89  2.8e-008 5.6e-005 1.8e-006 1.04e+000  1.670958560e+002  1.670959207e+002  1.5e-011 2.12  
90  2.5e-008 5.0e-005 1.6e-006 1.05e+000  1.670958612e+002  1.670959179e+002  1.4e-011 2.14  
91  2.3e-008 4.5e-005 1.4e-006 1.00e+000  1.670958650e+002  1.670959160e+002  1.3e-011 2.17  
92  2.0e-008 4.1e-005 1.3e-006 9.76e-001  1.670958684e+002  1.670959143e+002  1.1e-011 2.18  
93  1.8e-008 3.6e-005 1.2e-006 1.02e+000  1.670958717e+002  1.670959126e+002  1.0e-011 2.20  
94  1.6e-008 3.3e-005 1.0e-006 1.05e+000  1.670958750e+002  1.670959108e+002  9.5e-012 2.23  
95  1.5e-008 3.0e-005 9.4e-007 1.03e+000  1.670958778e+002  1.670959094e+002  8.7e-012 2.25  
Interior-point optimizer terminated. Time: 2.26. 

Optimizer terminated. Time: 2.28    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6709587777e+002   Viol.  con: 2e-007   var: 0e+000 
  Dual.    obj: 1.6709590942e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.3 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 935
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 935             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 770
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3440              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.06              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.05            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.45e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.281650039e+005 2.000000000e+000  1.0e+000 0.09  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.260064488e+005 3.586598412e+000  4.8e-001 0.12  
2   4.4e+002 5.6e+002 2.4e+004 -9.36e-001 -1.201036114e+005 9.955126089e+000  1.9e-001 0.16  
3   2.9e+002 3.7e+002 1.6e+004 -8.43e-001 -1.153209889e+005 5.962449873e+001  1.3e-001 0.17  
4   2.9e+002 3.7e+002 1.6e+004 -7.62e-001 -1.127512762e+005 2.237183959e+003  1.3e-001 0.19  
5   7.6e+001 9.7e+001 4.2e+003 -7.55e-001 -7.475663166e+004 9.749661547e+003  3.3e-002 0.22  
6   3.7e+001 4.7e+001 2.0e+003 -1.99e-001 -4.738443197e+004 1.028818944e+004  1.6e-002 0.23  
7   2.3e+001 3.0e+001 1.3e+003 2.71e-001  -3.362049222e+004 7.292006221e+003  1.0e-002 0.25  
8   1.4e+001 1.7e+001 7.6e+002 5.18e-001  -2.155826448e+004 4.842538249e+003  6.0e-003 0.28  
9   5.4e+000 6.9e+000 3.0e+002 7.18e-001  -8.872619581e+003 2.461230964e+003  2.4e-003 0.30  
10  2.4e+000 3.1e+000 1.4e+002 9.11e-001  -3.777344320e+003 1.422699345e+003  1.1e-003 0.31  
11  1.8e+000 2.3e+000 1.0e+002 9.74e-001  -2.754291107e+003 1.093078081e+003  7.9e-004 0.34  
12  8.1e-001 1.0e+000 4.6e+001 9.82e-001  -1.172185610e+003 5.956567944e+002  3.6e-004 0.36  
13  7.5e-001 1.1e+000 4.2e+001 9.46e-001  -1.100303482e+003 5.585000721e+002  3.4e-004 0.37  
14  6.2e-001 8.9e-001 3.5e+001 9.87e-001  -8.693260186e+002 5.054044315e+002  2.8e-004 0.41  
15  1.8e-001 2.9e-001 1.0e+001 9.89e-001  -1.579532331e+002 2.544988404e+002  8.4e-005 0.42  
16  1.0e-001 1.8e-001 5.8e+000 1.01e+000  -1.917029679e+001 2.099840067e+002  4.7e-005 0.45  
17  1.0e-001 1.8e-001 5.8e+000 1.02e+000  -1.750099774e+001 2.103208201e+002  4.7e-005 0.48  
18  8.6e-002 1.5e-001 5.0e+000 1.02e+000  1.630738501e+001  2.107226831e+002  4.0e-005 0.51  
19  4.3e-002 9.8e-002 2.5e+000 1.01e+000  9.144551162e+001  1.875633606e+002  2.0e-005 0.55  
20  1.2e-002 1.6e-001 7.1e-001 1.01e+000  1.464213362e+002  1.736014343e+002  5.7e-006 0.58  
21  4.7e-003 3.6e-001 2.8e-001 1.01e+000  1.584905705e+002  1.691033331e+002  2.3e-006 0.61  
22  1.2e-003 1.8e-001 7.5e-002 1.01e+000  1.645724845e+002  1.674403909e+002  6.1e-007 0.62  
23  6.6e-004 1.2e-001 4.1e-002 9.80e-001  1.655128476e+002  1.670779496e+002  3.4e-007 0.66  
24  2.0e-004 1.1e-001 1.3e-002 9.95e-001  1.662879387e+002  1.667831362e+002  1.1e-007 0.69  
25  6.9e-005 1.0e-001 4.5e-003 1.01e+000  1.665171029e+002  1.666889244e+002  3.8e-008 0.70  
26  3.1e-005 8.7e-002 2.1e-003 1.01e+000  1.665829618e+002  1.666610873e+002  1.8e-008 0.73  
27  2.8e-005 7.9e-002 1.9e-003 1.01e+000  1.665892620e+002  1.666595800e+002  1.6e-008 0.76  
28  2.5e-005 7.2e-002 1.7e-003 1.00e+000  1.665940973e+002  1.666573665e+002  1.4e-008 0.78  
29  2.3e-005 6.6e-002 1.5e-003 1.00e+000  1.665985131e+002  1.666554471e+002  1.3e-008 0.81  
30  2.0e-005 6.0e-002 1.4e-003 1.00e+000  1.666024747e+002  1.666537076e+002  1.1e-008 0.84  
31  1.8e-005 5.5e-002 1.2e-003 1.00e+000  1.666060358e+002  1.666521389e+002  1.0e-008 0.87  
32  1.7e-005 5.0e-002 1.1e-003 1.00e+000  1.666092358e+002  1.666507234e+002  9.3e-009 0.89  
33  1.5e-005 4.6e-002 9.9e-004 1.00e+000  1.666121119e+002  1.666494464e+002  8.4e-009 0.92  
34  1.3e-005 4.2e-002 8.9e-004 1.00e+000  1.666146970e+002  1.666482945e+002  7.5e-009 0.95  
35  1.2e-005 3.9e-002 8.0e-004 1.00e+000  1.666170207e+002  1.666472556e+002  6.8e-009 0.97  
36  1.1e-005 3.5e-002 7.2e-004 1.00e+000  1.666191096e+002  1.666463186e+002  6.1e-009 1.00  
37  9.8e-006 3.3e-002 6.5e-004 1.00e+000  1.666209875e+002  1.666454736e+002  5.5e-009 1.01  
38  8.8e-006 3.0e-002 5.9e-004 1.00e+000  1.666226758e+002  1.666447117e+002  5.0e-009 1.04  
39  7.9e-006 2.8e-002 5.3e-004 1.00e+000  1.666241937e+002  1.666440248e+002  4.5e-009 1.06  
40  7.1e-006 2.6e-002 4.7e-004 1.00e+000  1.666255585e+002  1.666434054e+002  4.0e-009 1.09  
41  6.4e-006 2.4e-002 4.3e-004 1.00e+000  1.666267857e+002  1.666428471e+002  3.6e-009 1.11  
42  5.8e-006 2.3e-002 3.8e-004 1.00e+000  1.666278892e+002  1.666423438e+002  3.3e-009 1.14  
43  5.2e-006 2.1e-002 3.5e-004 1.00e+000  1.666288815e+002  1.666418901e+002  2.9e-009 1.15  
44  4.7e-006 2.0e-002 3.1e-004 1.00e+000  1.666297738e+002  1.666414811e+002  2.6e-009 1.19  
45  4.2e-006 1.9e-002 2.8e-004 1.00e+000  1.666305762e+002  1.666411125e+002  2.4e-009 1.20  
46  3.8e-006 1.7e-002 2.5e-004 1.00e+000  1.666312978e+002  1.666407801e+002  2.1e-009 1.23  
47  3.4e-006 1.7e-002 2.3e-004 1.00e+000  1.666319467e+002  1.666404806e+002  1.9e-009 1.25  
48  3.1e-006 1.6e-002 2.0e-004 1.00e+000  1.666325302e+002  1.666402105e+002  1.7e-009 1.28  
49  2.8e-006 1.5e-002 1.8e-004 1.00e+000  1.666330549e+002  1.666399670e+002  1.6e-009 1.29  
50  2.5e-006 1.4e-002 1.7e-004 1.00e+000  1.666335267e+002  1.666397475e+002  1.4e-009 1.33  
51  2.2e-006 1.4e-002 1.5e-004 1.00e+000  1.666339511e+002  1.666395497e+002  1.3e-009 1.34  
52  2.0e-006 1.3e-002 1.3e-004 1.00e+000  1.666343328e+002  1.666393714e+002  1.1e-009 1.37  
53  1.8e-006 1.2e-002 1.2e-004 1.00e+000  1.666346761e+002  1.666392108e+002  1.0e-009 1.39  
54  1.6e-006 1.2e-002 1.1e-004 1.00e+000  1.666349849e+002  1.666390661e+002  9.2e-010 1.40  
55  1.5e-006 1.2e-002 9.8e-005 1.00e+000  1.666352626e+002  1.666389357e+002  8.3e-010 1.44  
56  1.3e-006 1.1e-002 8.8e-005 1.00e+000  1.666355124e+002  1.666388182e+002  7.4e-010 1.45  
57  1.2e-006 1.1e-002 7.9e-005 1.00e+000  1.666357371e+002  1.666387123e+002  6.7e-010 1.48  
58  1.1e-006 1.1e-002 7.1e-005 1.00e+000  1.666359393e+002  1.666386169e+002  6.0e-010 1.50  
59  9.6e-007 1.0e-002 6.4e-005 1.00e+000  1.666361211e+002  1.666385309e+002  5.4e-010 1.51  
60  8.7e-007 1.0e-002 5.8e-005 1.00e+000  1.666362846e+002  1.666384534e+002  4.9e-010 1.54  
61  7.8e-007 9.9e-003 5.2e-005 1.00e+000  1.666364316e+002  1.666383835e+002  4.4e-010 1.56  
62  7.0e-007 9.7e-003 4.7e-005 1.00e+000  1.666365638e+002  1.666383206e+002  4.0e-010 1.59  
63  6.3e-007 9.5e-003 4.2e-005 1.00e+000  1.666366828e+002  1.666382639e+002  3.6e-010 1.61  
64  5.7e-007 9.3e-003 3.8e-005 1.00e+000  1.666367897e+002  1.666382127e+002  3.2e-010 1.64  
65  5.1e-007 9.2e-003 3.4e-005 1.00e+000  1.666368859e+002  1.666381666e+002  2.9e-010 1.65  
66  4.6e-007 9.0e-003 3.1e-005 1.00e+000  1.666369724e+002  1.666381250e+002  2.6e-010 1.68  
67  4.1e-007 8.9e-003 2.8e-005 1.00e+000  1.666370501e+002  1.666380875e+002  2.3e-010 1.70  
68  3.7e-007 8.8e-003 2.5e-005 1.00e+000  1.666371201e+002  1.666380537e+002  2.1e-010 1.73  
69  3.4e-007 8.7e-003 2.2e-005 1.00e+000  1.666371829e+002  1.666380232e+002  1.9e-010 1.75  
70  3.0e-007 8.6e-003 2.0e-005 1.00e+000  1.666372395e+002  1.666379957e+002  1.7e-010 1.76  
71  2.7e-007 8.5e-003 1.8e-005 1.00e+000  1.666372904e+002  1.666379710e+002  1.5e-010 1.79  
72  2.4e-007 8.5e-003 1.6e-005 1.00e+000  1.666373361e+002  1.666379487e+002  1.4e-010 1.81  
73  2.2e-007 8.4e-003 1.5e-005 9.98e-001  1.666373773e+002  1.666379286e+002  1.2e-010 1.84  
74  2.0e-007 8.3e-003 1.3e-005 1.00e+000  1.666374143e+002  1.666379105e+002  1.1e-010 1.86  
75  1.8e-007 8.3e-003 1.2e-005 1.00e+000  1.666374476e+002  1.666378942e+002  1.0e-010 1.89  
76  1.6e-007 8.2e-003 1.1e-005 1.00e+000  1.666374776e+002  1.666378795e+002  9.1e-011 1.90  
77  1.4e-007 8.2e-003 9.6e-006 1.00e+000  1.666375045e+002  1.666378662e+002  8.1e-011 1.93  
78  1.3e-007 8.1e-003 8.7e-006 1.00e+000  1.666375288e+002  1.666378543e+002  7.3e-011 1.97  
79  1.2e-007 8.1e-003 7.8e-006 1.00e+000  1.666375506e+002  1.666378436e+002  6.6e-011 1.98  
80  1.1e-007 8.0e-003 7.0e-006 9.98e-001  1.666375703e+002  1.666378340e+002  5.9e-011 2.00  
81  9.5e-008 8.0e-003 6.3e-006 9.97e-001  1.666375879e+002  1.666378253e+002  5.3e-011 2.03  
82  8.5e-008 8.0e-003 5.7e-006 1.00e+000  1.666376039e+002  1.666378175e+002  4.8e-011 2.04  
83  7.7e-008 7.9e-003 5.1e-006 1.00e+000  1.666376183e+002  1.666378104e+002  4.3e-011 2.07  
84  6.9e-008 7.9e-003 4.6e-006 1.00e+000  1.666376311e+002  1.666378040e+002  3.9e-011 2.09  
85  6.2e-008 7.9e-003 4.1e-006 9.97e-001  1.666376427e+002  1.666377983e+002  3.5e-011 2.12  
86  5.6e-008 7.8e-003 3.7e-006 9.94e-001  1.666376531e+002  1.666377932e+002  3.2e-011 2.14  
87  5.0e-008 7.8e-003 3.4e-006 9.95e-001  1.666376625e+002  1.666377886e+002  2.8e-011 2.15  
88  4.5e-008 7.0e-003 3.0e-006 1.01e+000  1.666376711e+002  1.666377844e+002  2.6e-011 2.18  
89  4.1e-008 6.3e-003 2.7e-006 1.00e+000  1.666376788e+002  1.666377806e+002  2.3e-011 2.21  
90  3.7e-008 5.7e-003 2.4e-006 1.01e+000  1.666376859e+002  1.666377770e+002  2.1e-011 2.23  
91  3.3e-008 5.1e-003 2.2e-006 1.00e+000  1.666376920e+002  1.666377740e+002  1.9e-011 2.26  
92  3.0e-008 4.6e-003 2.0e-006 9.99e-001  1.666376975e+002  1.666377713e+002  1.7e-011 2.28  
93  2.7e-008 4.1e-003 1.8e-006 1.01e+000  1.666377026e+002  1.666377688e+002  1.5e-011 2.29  
94  2.4e-008 3.7e-003 1.6e-006 1.01e+000  1.666377072e+002  1.666377665e+002  1.4e-011 2.32  
95  2.2e-008 3.4e-003 1.4e-006 9.96e-001  1.666377112e+002  1.666377646e+002  1.2e-011 2.34  
96  2.0e-008 3.0e-003 1.3e-006 1.02e+000  1.666377151e+002  1.666377626e+002  1.1e-011 2.37  
97  1.8e-008 2.7e-003 1.2e-006 1.00e+000  1.666377183e+002  1.666377610e+002  1.0e-011 2.39  
98  1.6e-008 2.4e-003 1.1e-006 1.01e+000  1.666377212e+002  1.666377596e+002  9.2e-012 2.42  
99  1.4e-008 2.2e-003 9.5e-007 9.85e-001  1.666377238e+002  1.666377583e+002  8.3e-012 2.43  
100 1.3e-008 2.0e-003 8.5e-007 9.93e-001  1.666377261e+002  1.666377572e+002  7.4e-012 2.45  
101 1.2e-008 1.8e-003 7.7e-007 1.02e+000  1.666377284e+002  1.666377561e+002  6.7e-012 2.48  
102 1.0e-008 1.6e-003 6.9e-007 1.00e+000  1.666377303e+002  1.666377552e+002  6.1e-012 2.50  
103 9.4e-009 1.4e-003 6.2e-007 1.01e+000  1.666377320e+002  1.666377543e+002  5.5e-012 2.53  
104 8.4e-009 1.3e-003 5.6e-007 1.01e+000  1.666377335e+002  1.666377535e+002  5.0e-012 2.54  
105 7.6e-009 1.2e-003 5.0e-007 9.71e-001  1.666377349e+002  1.666377529e+002  4.5e-012 2.56  
106 6.9e-009 1.1e-003 4.5e-007 9.62e-001  1.666377361e+002  1.666377523e+002  4.0e-012 2.59  
107 6.2e-009 9.5e-004 4.1e-007 1.05e+000  1.666377374e+002  1.666377517e+002  3.7e-012 2.61  
108 5.5e-009 8.5e-004 3.7e-007 9.61e-001  1.666377383e+002  1.666377512e+002  3.3e-012 2.64  
109 5.1e-009 7.7e-004 3.3e-007 1.15e+000  1.666377398e+002  1.666377504e+002  3.2e-012 2.65  
110 4.6e-009 6.9e-004 3.0e-007 1.04e+000  1.666377407e+002  1.666377500e+002  3.0e-012 2.67  
111 4.1e-009 6.2e-004 2.7e-007 9.73e-001  1.666377413e+002  1.666377497e+002  2.7e-012 2.70  
112 2.3e-009 3.4e-005 1.5e-008 9.64e-001  1.666377467e+002  1.666377472e+002  1.9e-013 2.71  
Interior-point optimizer terminated. Time: 2.73. 

Optimizer terminated. Time: 2.75    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6663774670e+002   Viol.  con: 5e-008   var: 0e+000 
  Dual.    obj: 1.6663774717e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.76 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 935
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 935             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 770
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3440              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.45e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.281256834e+005 2.000000000e+000  1.0e+000 0.05  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.259652930e+005 3.580273350e+000  4.8e-001 0.08  
2   4.3e+002 5.5e+002 2.4e+004 -9.36e-001 -1.199460135e+005 1.005567772e+001  1.9e-001 0.11  
3   2.9e+002 3.7e+002 1.6e+004 -8.41e-001 -1.152369809e+005 6.134026226e+001  1.3e-001 0.14  
4   2.9e+002 3.7e+002 1.6e+004 -7.61e-001 -1.125938770e+005 2.293613946e+003  1.3e-001 0.17  
5   7.3e+001 9.4e+001 4.1e+003 -7.54e-001 -7.359810711e+004 9.834631471e+003  3.2e-002 0.20  
6   3.6e+001 4.5e+001 2.0e+003 -1.82e-001 -4.627586382e+004 1.009595081e+004  1.6e-002 0.23  
7   2.1e+001 2.7e+001 1.2e+003 2.90e-001  -3.084203836e+004 6.881649872e+003  9.2e-003 0.25  
8   1.2e+001 1.6e+001 6.7e+002 5.65e-001  -1.932393194e+004 4.483629534e+003  5.4e-003 0.28  
9   4.7e+000 6.0e+000 2.6e+002 7.54e-001  -7.701993694e+003 2.174748636e+003  2.1e-003 0.31  
10  2.3e+000 2.9e+000 1.3e+002 9.26e-001  -3.516865936e+003 1.397320866e+003  1.0e-003 0.34  
11  1.5e+000 1.9e+000 8.4e+001 9.76e-001  -2.278058155e+003 9.686747465e+002  6.7e-004 0.36  
12  8.5e-001 1.1e+000 4.7e+001 9.85e-001  -1.223620136e+003 6.225979300e+002  3.8e-004 0.39  
13  7.5e-001 9.9e-001 4.2e+001 9.54e-001  -1.085112150e+003 5.622488960e+002  3.3e-004 0.42  
14  3.7e-001 4.9e-001 2.1e+001 9.85e-001  -4.368185471e+002 3.757299569e+002  1.7e-004 0.44  
15  1.8e-001 2.5e-001 1.0e+001 9.98e-001  -1.425570957e+002 2.585351359e+002  8.2e-005 0.47  
16  8.9e-002 1.6e-001 5.1e+000 1.01e+000  5.484304986e+000  2.044128724e+002  4.1e-005 0.48  
17  8.6e-002 1.5e-001 4.9e+000 1.01e+000  1.455519356e+001  2.066563012e+002  4.0e-005 0.51  
18  6.1e-002 1.1e-001 3.5e+000 1.01e+000  6.001216926e+001  1.948456420e+002  2.8e-005 0.55  
19  2.9e-002 7.3e-002 1.7e+000 1.01e+000  1.156052379e+002  1.809648002e+002  1.4e-005 0.56  
20  8.5e-003 1.8e-001 4.9e-001 1.01e+000  1.526398199e+002  1.716139711e+002  4.0e-006 0.59  
21  2.5e-003 1.8e-001 1.5e-001 1.00e+000  1.622522100e+002  1.679613502e+002  1.2e-006 0.62  
22  1.5e-003 1.2e-001 9.0e-002 1.00e+000  1.639807316e+002  1.674413357e+002  7.3e-007 0.64  
23  5.1e-004 1.0e-001 3.2e-002 1.01e+000  1.656593398e+002  1.668669764e+002  2.6e-007 0.69  
24  2.0e-004 9.6e-002 1.2e-002 1.01e+000  1.661981690e+002  1.666657458e+002  1.0e-007 0.70  
25  1.8e-004 8.7e-002 1.1e-002 1.01e+000  1.662345733e+002  1.666552714e+002  9.2e-008 0.73  
26  1.6e-004 7.9e-002 9.9e-003 1.01e+000  1.662646308e+002  1.666431179e+002  8.3e-008 0.76  
27  1.4e-004 7.2e-002 8.9e-003 1.01e+000  1.662918626e+002  1.666323887e+002  7.5e-008 0.78  
28  1.3e-004 6.6e-002 8.0e-003 1.01e+000  1.663162459e+002  1.666226262e+002  6.7e-008 0.81  
29  1.2e-004 6.0e-002 7.2e-003 1.01e+000  1.663381281e+002  1.666137935e+002  6.0e-008 0.84  
30  1.0e-004 5.5e-002 6.5e-003 1.01e+000  1.663577600e+002  1.666057958e+002  5.4e-008 0.89  
31  9.4e-005 5.0e-002 5.9e-003 1.01e+000  1.663753750e+002  1.665985555e+002  4.9e-008 0.90  
32  8.4e-005 4.6e-002 5.3e-003 1.01e+000  1.663911809e+002  1.665920012e+002  4.4e-008 0.94  
33  7.6e-005 4.2e-002 4.7e-003 1.01e+000  1.664053647e+002  1.665860687e+002  4.0e-008 0.97  
34  6.8e-005 3.9e-002 4.3e-003 1.01e+000  1.664180941e+002  1.665806998e+002  3.6e-008 0.98  
35  6.2e-005 3.5e-002 3.8e-003 1.01e+000  1.664295194e+002  1.665758421e+002  3.2e-008 1.01  
36  5.5e-005 3.3e-002 3.5e-003 1.00e+000  1.664397754e+002  1.665714477e+002  2.9e-008 1.03  
37  5.0e-005 3.0e-002 3.1e-003 1.00e+000  1.664489827e+002  1.665674733e+002  2.6e-008 1.06  
38  4.5e-005 2.8e-002 2.8e-003 1.00e+000  1.664572496e+002  1.665638794e+002  2.3e-008 1.08  
39  4.0e-005 2.6e-002 2.5e-003 1.00e+000  1.664646728e+002  1.665606304e+002  2.1e-008 1.11  
40  3.6e-005 2.4e-002 2.3e-003 1.00e+000  1.664713393e+002  1.665576937e+002  1.9e-008 1.14  
41  3.3e-005 2.2e-002 2.0e-003 1.00e+000  1.664773267e+002  1.665550398e+002  1.7e-008 1.15  
42  2.9e-005 2.1e-002 1.8e-003 1.00e+000  1.664827048e+002  1.665526419e+002  1.5e-008 1.19  
43  2.6e-005 2.0e-002 1.7e-003 1.00e+000  1.664875360e+002  1.665504759e+002  1.4e-008 1.20  
44  2.4e-005 1.8e-002 1.5e-003 1.00e+000  1.664918765e+002  1.665485195e+002  1.2e-008 1.23  
45  2.1e-005 1.7e-002 1.3e-003 1.00e+000  1.664957764e+002  1.665467529e+002  1.1e-008 1.25  
46  1.9e-005 1.6e-002 1.2e-003 1.00e+000  1.664992809e+002  1.665451580e+002  1.0e-008 1.28  
47  1.7e-005 1.6e-002 1.1e-003 1.00e+000  1.665024304e+002  1.665437184e+002  9.1e-009 1.29  
48  1.6e-005 1.5e-002 9.8e-004 1.00e+000  1.665052611e+002  1.665424193e+002  8.2e-009 1.33  
49  1.4e-005 1.4e-002 8.8e-004 1.00e+000  1.665078056e+002  1.665412472e+002  7.4e-009 1.34  
50  1.3e-005 1.4e-002 7.9e-004 1.00e+000  1.665100931e+002  1.665401900e+002  6.6e-009 1.37  
51  1.1e-005 1.3e-002 7.1e-004 1.00e+000  1.665121498e+002  1.665392365e+002  6.0e-009 1.39  
52  1.0e-005 1.2e-002 6.4e-004 1.00e+000  1.665139991e+002  1.665383769e+002  5.4e-009 1.42  
53  9.2e-006 1.2e-002 5.8e-004 1.00e+000  1.665156621e+002  1.665376019e+002  4.8e-009 1.44  
54  8.3e-006 1.2e-002 5.2e-004 1.00e+000  1.665171577e+002  1.665369034e+002  4.3e-009 1.47  
55  7.5e-006 1.1e-002 4.7e-004 1.00e+000  1.665185029e+002  1.665362739e+002  3.9e-009 1.48  
56  6.7e-006 1.1e-002 4.2e-004 1.00e+000  1.665197128e+002  1.665357066e+002  3.5e-009 1.51  
57  6.1e-006 1.1e-002 3.8e-004 1.00e+000  1.665208011e+002  1.665351955e+002  3.2e-009 1.53  
58  5.5e-006 1.0e-002 3.4e-004 1.00e+000  1.665217800e+002  1.665347351e+002  2.9e-009 1.56  
59  4.9e-006 1.0e-002 3.1e-004 1.00e+000  1.665226606e+002  1.665343202e+002  2.6e-009 1.58  
60  4.4e-006 9.9e-003 2.8e-004 1.00e+000  1.665234527e+002  1.665339464e+002  2.3e-009 1.61  
61  4.0e-006 9.7e-003 2.5e-004 1.00e+000  1.665241652e+002  1.665336095e+002  2.1e-009 1.62  
62  3.6e-006 9.5e-003 2.2e-004 1.00e+000  1.665248061e+002  1.665333060e+002  1.9e-009 1.65  
63  3.2e-006 9.4e-003 2.0e-004 1.00e+000  1.665253825e+002  1.665330325e+002  1.7e-009 1.67  
64  2.9e-006 9.2e-003 1.8e-004 1.00e+000  1.665259010e+002  1.665327860e+002  1.5e-009 1.70  
65  2.6e-006 9.1e-003 1.6e-004 1.00e+000  1.665263673e+002  1.665325639e+002  1.4e-009 1.73  
66  2.3e-006 9.0e-003 1.5e-004 1.00e+000  1.665267868e+002  1.665323638e+002  1.2e-009 1.75  
67  2.1e-006 8.9e-003 1.3e-004 1.00e+000  1.665271642e+002  1.665321834e+002  1.1e-009 1.78  
68  1.9e-006 8.8e-003 1.2e-004 1.00e+000  1.665275036e+002  1.665320210e+002  1.0e-009 1.79  
69  1.7e-006 8.7e-003 1.1e-004 1.00e+000  1.665278090e+002  1.665318747e+002  9.0e-010 1.83  
70  1.5e-006 8.6e-003 9.6e-005 1.00e+000  1.665280838e+002  1.665317429e+002  8.1e-010 1.84  
71  1.4e-006 8.6e-003 8.7e-005 1.00e+000  1.665283309e+002  1.665316241e+002  7.3e-010 1.87  
72  1.2e-006 8.5e-003 7.8e-005 1.00e+000  1.665285532e+002  1.665315172e+002  6.5e-010 1.89  
73  1.1e-006 8.5e-003 7.0e-005 1.00e+000  1.665287533e+002  1.665314208e+002  5.9e-010 1.92  
74  1.0e-006 8.4e-003 6.3e-005 1.00e+000  1.665289332e+002  1.665313340e+002  5.3e-010 1.93  
75  9.1e-007 8.4e-003 5.7e-005 1.00e+000  1.665290950e+002  1.665312558e+002  4.8e-010 1.95  
76  8.2e-007 8.3e-003 5.1e-005 1.00e+000  1.665292406e+002  1.665311853e+002  4.3e-010 1.98  
77  7.4e-007 8.3e-003 4.6e-005 1.00e+000  1.665293715e+002  1.665311218e+002  3.9e-010 2.00  
78  6.6e-007 8.2e-003 4.2e-005 1.00e+000  1.665294893e+002  1.665310645e+002  3.5e-010 2.03  
79  6.0e-007 8.2e-003 3.7e-005 1.00e+000  1.665295952e+002  1.665310129e+002  3.1e-010 2.04  
80  5.4e-007 8.2e-003 3.4e-005 1.00e+000  1.665296904e+002  1.665309664e+002  2.8e-010 2.07  
81  4.8e-007 8.1e-003 3.0e-005 1.00e+000  1.665297761e+002  1.665309245e+002  2.5e-010 2.09  
82  4.4e-007 8.1e-003 2.7e-005 1.00e+000  1.665298531e+002  1.665308867e+002  2.3e-010 2.12  
83  3.9e-007 8.1e-003 2.5e-005 1.00e+000  1.665299224e+002  1.665308526e+002  2.1e-010 2.14  
84  3.5e-007 8.0e-003 2.2e-005 1.00e+000  1.665299846e+002  1.665308219e+002  1.8e-010 2.15  
85  3.2e-007 8.0e-003 2.0e-005 1.00e+000  1.665300407e+002  1.665307941e+002  1.7e-010 2.18  
86  2.9e-007 8.0e-003 1.8e-005 9.99e-001  1.665300910e+002  1.665307692e+002  1.5e-010 2.20  
87  2.6e-007 8.0e-003 1.6e-005 1.00e+000  1.665301364e+002  1.665307467e+002  1.3e-010 2.23  
88  2.3e-007 7.9e-003 1.4e-005 9.98e-001  1.665301771e+002  1.665307265e+002  1.2e-010 2.25  
89  2.1e-007 7.9e-003 1.3e-005 1.00e+000  1.665302138e+002  1.665307082e+002  1.1e-010 2.26  
90  1.9e-007 7.9e-003 1.2e-005 9.97e-001  1.665302468e+002  1.665306918e+002  9.8e-011 2.29  
91  1.7e-007 7.9e-003 1.1e-005 9.98e-001  1.665302764e+002  1.665306770e+002  8.8e-011 2.31  
92  1.5e-007 7.9e-003 9.5e-006 1.00e+000  1.665303031e+002  1.665306636e+002  7.9e-011 2.34  
93  1.4e-007 7.8e-003 8.6e-006 1.00e+000  1.665303272e+002  1.665306516e+002  7.2e-011 2.36  
94  1.2e-007 7.8e-003 7.7e-006 9.99e-001  1.665303488e+002  1.665306408e+002  6.4e-011 2.37  
95  1.1e-007 7.8e-003 6.9e-006 9.96e-001  1.665303682e+002  1.665306311e+002  5.8e-011 2.40  
96  1.0e-007 7.8e-003 6.2e-006 9.98e-001  1.665303857e+002  1.665306223e+002  5.2e-011 2.42  
97  9.0e-008 7.8e-003 5.6e-006 1.00e+000  1.665304015e+002  1.665306144e+002  4.7e-011 2.45  
98  8.1e-008 7.8e-003 5.1e-006 1.00e+000  1.665304157e+002  1.665306073e+002  4.2e-011 2.46  
99  7.3e-008 7.0e-003 4.5e-006 1.01e+000  1.665304286e+002  1.665306008e+002  3.8e-011 2.50  
100 6.5e-008 6.3e-003 4.1e-006 1.00e+000  1.665304400e+002  1.665305950e+002  3.4e-011 2.51  
101 5.9e-008 5.7e-003 3.7e-006 9.97e-001  1.665304503e+002  1.665305898e+002  3.1e-011 2.54  
102 5.3e-008 5.1e-003 3.3e-006 9.99e-001  1.665304596e+002  1.665305852e+002  2.8e-011 2.56  
103 4.8e-008 4.6e-003 3.0e-006 1.00e+000  1.665304680e+002  1.665305810e+002  2.5e-011 2.57  
104 4.3e-008 4.1e-003 2.7e-006 9.90e-001  1.665304755e+002  1.665305772e+002  2.2e-011 2.61  
105 3.9e-008 3.7e-003 2.4e-006 9.91e-001  1.665304822e+002  1.665305739e+002  2.0e-011 2.62  
106 3.5e-008 3.3e-003 2.2e-006 1.00e+000  1.665304883e+002  1.665305708e+002  1.8e-011 2.64  
107 3.1e-008 3.0e-003 2.0e-006 9.94e-001  1.665304938e+002  1.665305680e+002  1.6e-011 2.67  
108 2.8e-008 2.7e-003 1.8e-006 9.94e-001  1.665304987e+002  1.665305656e+002  1.5e-011 2.68  
109 2.5e-008 2.4e-003 1.6e-006 9.93e-001  1.665305032e+002  1.665305633e+002  1.3e-011 2.71  
110 2.3e-008 2.2e-003 1.4e-006 9.87e-001  1.665305072e+002  1.665305614e+002  1.2e-011 2.73  
111 2.1e-008 2.0e-003 1.3e-006 9.99e-001  1.665305108e+002  1.665305595e+002  1.1e-011 2.76  
112 1.8e-008 1.8e-003 1.2e-006 9.77e-001  1.665305140e+002  1.665305579e+002  9.7e-012 2.78  
113 1.7e-008 1.6e-003 1.0e-006 9.90e-001  1.665305169e+002  1.665305565e+002  8.7e-012 2.81  
114 1.5e-008 1.4e-003 9.4e-007 1.02e+000  1.665305197e+002  1.665305550e+002  7.9e-012 2.90  
115 1.3e-008 1.3e-003 8.4e-007 1.01e+000  1.665305222e+002  1.665305538e+002  7.1e-012 2.92  
116 1.2e-008 1.2e-003 7.6e-007 9.89e-001  1.665305243e+002  1.665305527e+002  6.4e-012 2.93  
117 1.1e-008 1.0e-003 6.8e-007 1.01e+000  1.665305263e+002  1.665305517e+002  5.8e-012 2.96  
118 9.8e-009 9.4e-004 6.1e-007 1.00e+000  1.665305280e+002  1.665305508e+002  5.2e-012 2.98  
119 8.9e-009 8.5e-004 5.5e-007 9.58e-001  1.665305295e+002  1.665305501e+002  4.7e-012 3.01  
120 8.0e-009 7.6e-004 5.0e-007 1.02e+000  1.665305310e+002  1.665305493e+002  4.3e-012 3.03  
121 7.2e-009 6.9e-004 4.5e-007 9.44e-001  1.665305322e+002  1.665305487e+002  3.9e-012 3.06  
122 6.5e-009 6.2e-004 4.0e-007 1.03e+000  1.665305334e+002  1.665305481e+002  3.5e-012 3.07  
123 5.9e-009 5.6e-004 3.6e-007 9.85e-001  1.665305344e+002  1.665305476e+002  3.2e-012 3.10  
124 5.3e-009 5.0e-004 3.3e-007 9.19e-001  1.665305353e+002  1.665305472e+002  2.9e-012 3.12  
125 4.8e-009 4.5e-004 2.9e-007 1.01e+000  1.665305361e+002  1.665305468e+002  2.6e-012 3.15  
126 4.3e-009 4.1e-004 2.6e-007 1.05e+000  1.665305370e+002  1.665305463e+002  2.4e-012 3.17  
127 3.9e-009 3.7e-004 2.4e-007 1.00e+000  1.665305376e+002  1.665305460e+002  2.1e-012 3.18  
128 3.5e-009 3.3e-004 2.1e-007 1.02e+000  1.665305382e+002  1.665305457e+002  1.9e-012 3.21  
129 3.2e-009 3.0e-004 1.9e-007 1.03e+000  1.665305388e+002  1.665305454e+002  1.8e-012 3.23  
130 3.1e-009 2.7e-004 1.7e-007 1.08e+000  1.665305394e+002  1.665305451e+002  1.7e-012 3.26  
131 2.7e-009 2.4e-004 1.6e-007 1.05e+000  1.665305398e+002  1.665305448e+002  1.5e-012 3.28  
132 6.9e-010 1.4e-005 9.2e-009 1.01e+000  1.665305430e+002  1.665305433e+002  8.7e-014 3.29  
Interior-point optimizer terminated. Time: 3.31. 

Optimizer terminated. Time: 3.32    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6653054296e+002   Viol.  con: 2e-008   var: 0e+000 
  Dual.    obj: 1.6653054325e+002   Viol.  con: 0e+000   var: 8e-005 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.35 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 935
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 935             
Lin. dep.  - tries                  : 1                 time                   : 0.02            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 770
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3440              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.06              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.05            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.45e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.281219220e+005 2.000000000e+000  1.0e+000 0.09  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.259510010e+005 3.575672435e+000  4.8e-001 0.13  
2   4.3e+002 5.5e+002 2.4e+004 -9.36e-001 -1.198706812e+005 1.013521083e+001  1.9e-001 0.16  
3   2.9e+002 3.7e+002 1.6e+004 -8.40e-001 -1.151566019e+005 6.243051359e+001  1.2e-001 0.19  
4   2.8e+002 3.6e+002 1.6e+004 -7.60e-001 -1.125384733e+005 2.273182374e+003  1.2e-001 0.20  
5   7.5e+001 9.6e+001 4.1e+003 -7.53e-001 -7.445610949e+004 9.639349102e+003  3.3e-002 0.23  
6   3.3e+001 4.2e+001 1.8e+003 -1.95e-001 -4.330178112e+004 1.030586811e+004  1.4e-002 0.25  
7   1.9e+001 2.5e+001 1.1e+003 3.42e-001  -2.853323737e+004 6.914886940e+003  8.5e-003 0.28  
8   1.1e+001 1.5e+001 6.3e+002 6.05e-001  -1.808894946e+004 4.388511490e+003  5.0e-003 0.30  
9   4.5e+000 5.7e+000 2.5e+002 7.74e-001  -7.326211542e+003 2.100234109e+003  2.0e-003 0.33  
10  2.1e+000 2.7e+000 1.2e+002 9.30e-001  -3.203277371e+003 1.327240789e+003  9.3e-004 0.36  
11  1.3e+000 1.7e+000 7.5e+001 9.81e-001  -2.002128650e+003 8.889969039e+002  6.0e-004 0.39  
12  8.1e-001 1.0e+000 4.5e+001 9.84e-001  -1.160052654e+003 6.061248328e+002  3.6e-004 0.42  
13  6.4e-001 8.5e-001 3.6e+001 9.55e-001  -9.074252422e+002 5.061566687e+002  2.9e-004 0.45  
14  3.6e-001 4.9e-001 2.0e+001 9.93e-001  -4.159488955e+002 3.800106575e+002  1.6e-004 0.48  
15  1.8e-001 2.4e-001 9.9e+000 9.93e-001  -1.329950382e+002 2.580942107e+002  8.0e-005 0.52  
16  7.9e-002 1.3e-001 4.5e+000 1.01e+000  2.194749319e+001  1.995887151e+002  3.7e-005 0.53  
17  6.8e-002 1.1e-001 3.9e+000 1.02e+000  4.516567574e+001  1.977874470e+002  3.2e-005 0.56  
18  2.8e-002 7.4e-002 1.6e+000 1.02e+000  1.183222920e+002  1.806141016e+002  1.3e-005 0.59  
19  8.1e-003 2.0e-001 4.7e-001 1.01e+000  1.533659978e+002  1.714095262e+002  3.8e-006 0.61  
20  2.9e-003 2.4e-001 1.7e-001 1.00e+000  1.613685361e+002  1.680688871e+002  1.4e-006 0.64  
21  1.7e-003 1.4e-001 1.0e-001 1.01e+000  1.635977454e+002  1.674592385e+002  8.2e-007 0.67  
22  5.0e-004 1.2e-001 3.1e-002 1.01e+000  1.656258720e+002  1.668059034e+002  2.6e-007 0.69  
23  1.8e-004 1.1e-001 1.1e-002 1.01e+000  1.661711765e+002  1.666014999e+002  9.5e-008 0.72  
24  8.3e-005 8.8e-002 5.3e-003 1.01e+000  1.663352911e+002  1.665344422e+002  4.4e-008 0.75  
25  3.7e-005 8.0e-002 2.4e-003 1.01e+000  1.664121377e+002  1.665025052e+002  2.0e-008 0.77  
26  3.4e-005 7.3e-002 2.2e-003 1.01e+000  1.664199856e+002  1.665013384e+002  1.8e-008 0.80  
27  3.0e-005 6.6e-002 1.9e-003 1.01e+000  1.664255069e+002  1.664986965e+002  1.6e-008 0.83  
28  2.7e-005 6.1e-002 1.7e-003 1.01e+000  1.664305978e+002  1.664964543e+002  1.5e-008 0.84  
29  2.5e-005 5.5e-002 1.6e-003 1.01e+000  1.664351531e+002  1.664944116e+002  1.3e-008 0.87  
30  2.2e-005 5.0e-002 1.4e-003 1.01e+000  1.664392478e+002  1.664925705e+002  1.2e-008 0.89  
31  2.0e-005 4.6e-002 1.3e-003 1.00e+000  1.664429257e+002  1.664909081e+002  1.1e-008 0.92  
32  1.8e-005 4.2e-002 1.1e-003 1.00e+000  1.664462303e+002  1.664894079e+002  9.7e-009 0.94  
33  1.6e-005 3.9e-002 1.0e-003 1.00e+000  1.664491996e+002  1.664880541e+002  8.7e-009 0.97  
34  1.5e-005 3.6e-002 9.3e-004 1.00e+000  1.664518680e+002  1.664868327e+002  7.8e-009 0.98  
35  1.3e-005 3.3e-002 8.3e-004 1.00e+000  1.664542662e+002  1.664857310e+002  7.1e-009 1.01  
36  1.2e-005 3.0e-002 7.5e-004 1.00e+000  1.664564219e+002  1.664847373e+002  6.4e-009 1.03  
37  1.1e-005 2.8e-002 6.8e-004 1.00e+000  1.664583597e+002  1.664838413e+002  5.7e-009 1.06  
38  9.5e-006 2.6e-002 6.1e-004 1.00e+000  1.664601019e+002  1.664830335e+002  5.2e-009 1.08  
39  8.6e-006 2.4e-002 5.5e-004 1.00e+000  1.664616684e+002  1.664823053e+002  4.6e-009 1.11  
40  7.7e-006 2.3e-002 4.9e-004 1.00e+000  1.664630769e+002  1.664816490e+002  4.2e-009 1.12  
41  6.9e-006 2.1e-002 4.4e-004 1.00e+000  1.664643436e+002  1.664810575e+002  3.8e-009 1.16  
42  6.3e-006 2.0e-002 4.0e-004 1.00e+000  1.664654829e+002  1.664805246e+002  3.4e-009 1.17  
43  5.6e-006 1.9e-002 3.6e-004 1.00e+000  1.664665075e+002  1.664800445e+002  3.0e-009 1.19  
44  5.1e-006 1.7e-002 3.2e-004 1.00e+000  1.664674292e+002  1.664796120e+002  2.7e-009 1.22  
45  4.6e-006 1.6e-002 2.9e-004 1.00e+000  1.664682582e+002  1.664792224e+002  2.5e-009 1.23  
46  4.1e-006 1.6e-002 2.6e-004 1.00e+000  1.664690040e+002  1.664788715e+002  2.2e-009 1.26  
47  3.7e-006 1.5e-002 2.4e-004 1.00e+000  1.664696749e+002  1.664785554e+002  2.0e-009 1.28  
48  3.3e-006 1.4e-002 2.1e-004 1.00e+000  1.664702783e+002  1.664782707e+002  1.8e-009 1.29  
49  3.0e-006 1.3e-002 1.9e-004 1.00e+000  1.664708212e+002  1.664780142e+002  1.6e-009 1.33  
50  2.7e-006 1.3e-002 1.7e-004 1.00e+000  1.664713096e+002  1.664777832e+002  1.5e-009 1.34  
51  2.4e-006 1.2e-002 1.5e-004 1.00e+000  1.664717491e+002  1.664775752e+002  1.3e-009 1.37  
52  2.2e-006 1.2e-002 1.4e-004 1.00e+000  1.664721445e+002  1.664773879e+002  1.2e-009 1.39  
53  2.0e-006 1.1e-002 1.3e-004 1.00e+000  1.664725003e+002  1.664772193e+002  1.1e-009 1.40  
54  1.8e-006 1.1e-002 1.1e-004 1.00e+000  1.664728205e+002  1.664770676e+002  9.6e-010 1.44  
55  1.6e-006 1.1e-002 1.0e-004 1.00e+000  1.664731087e+002  1.664769310e+002  8.6e-010 1.47  
56  1.4e-006 1.0e-002 9.1e-005 1.00e+000  1.664733680e+002  1.664768080e+002  7.7e-010 1.48  
57  1.3e-006 1.0e-002 8.2e-005 1.00e+000  1.664736013e+002  1.664766974e+002  7.0e-010 1.51  
58  1.2e-006 9.9e-003 7.4e-005 1.00e+000  1.664738113e+002  1.664765978e+002  6.3e-010 1.53  
59  1.0e-006 9.6e-003 6.7e-005 1.00e+000  1.664740003e+002  1.664765081e+002  5.6e-010 1.54  
60  9.4e-007 9.4e-003 6.0e-005 1.00e+000  1.664741704e+002  1.664764274e+002  5.1e-010 1.58  
61  8.4e-007 9.3e-003 5.4e-005 1.00e+000  1.664743234e+002  1.664763548e+002  4.6e-010 1.59  
62  7.6e-007 9.1e-003 4.9e-005 1.00e+000  1.664744611e+002  1.664762894e+002  4.1e-010 1.61  
63  6.8e-007 8.9e-003 4.4e-005 1.00e+000  1.664745850e+002  1.664762305e+002  3.7e-010 1.64  
64  6.2e-007 8.8e-003 3.9e-005 1.00e+000  1.664746965e+002  1.664761774e+002  3.3e-010 1.65  
65  5.5e-007 8.7e-003 3.5e-005 1.00e+000  1.664747968e+002  1.664761296e+002  3.0e-010 1.69  
66  5.0e-007 8.6e-003 3.2e-005 9.99e-001  1.664748870e+002  1.664760866e+002  2.7e-010 1.72  
67  4.5e-007 8.5e-003 2.9e-005 1.00e+000  1.664749682e+002  1.664760478e+002  2.4e-010 1.75  
68  4.0e-007 8.4e-003 2.6e-005 1.00e+000  1.664750412e+002  1.664760128e+002  2.2e-010 1.78  
69  3.6e-007 8.3e-003 2.3e-005 1.00e+000  1.664751069e+002  1.664759813e+002  2.0e-010 1.79  
70  3.3e-007 8.2e-003 2.1e-005 1.00e+000  1.664751659e+002  1.664759529e+002  1.8e-010 1.83  
71  2.9e-007 8.2e-003 1.9e-005 1.00e+000  1.664752191e+002  1.664759273e+002  1.6e-010 1.84  
72  2.7e-007 8.1e-003 1.7e-005 1.00e+000  1.664752669e+002  1.664759043e+002  1.4e-010 1.87  
73  2.4e-007 8.1e-003 1.5e-005 9.98e-001  1.664753099e+002  1.664758836e+002  1.3e-010 1.89  
74  2.1e-007 8.0e-003 1.4e-005 1.00e+000  1.664753486e+002  1.664758649e+002  1.2e-010 1.92  
75  1.9e-007 8.0e-003 1.2e-005 1.00e+000  1.664753835e+002  1.664758481e+002  1.0e-010 1.94  
76  1.7e-007 7.9e-003 1.1e-005 1.00e+000  1.664754148e+002  1.664758330e+002  9.4e-011 1.97  
77  1.6e-007 7.9e-003 1.0e-005 1.00e+000  1.664754430e+002  1.664758193e+002  8.5e-011 1.98  
78  1.4e-007 7.9e-003 9.0e-006 1.00e+000  1.664754685e+002  1.664758070e+002  7.6e-011 2.00  
79  1.3e-007 7.8e-003 8.1e-006 1.00e+000  1.664754913e+002  1.664757959e+002  6.9e-011 2.03  
80  1.1e-007 7.8e-003 7.3e-006 1.00e+000  1.664755118e+002  1.664757860e+002  6.2e-011 2.04  
81  1.0e-007 7.8e-003 6.6e-006 1.00e+000  1.664755303e+002  1.664757771e+002  5.6e-011 2.08  
82  9.2e-008 7.7e-003 5.9e-006 1.00e+000  1.664755469e+002  1.664757690e+002  5.0e-011 2.09  
83  8.3e-008 7.7e-003 5.3e-006 1.00e+000  1.664755619e+002  1.664757618e+002  4.5e-011 2.12  
84  7.5e-008 7.7e-003 4.8e-006 9.99e-001  1.664755754e+002  1.664757553e+002  4.1e-011 2.14  
85  6.7e-008 7.7e-003 4.3e-006 9.94e-001  1.664755875e+002  1.664757494e+002  3.6e-011 2.17  
86  6.1e-008 7.6e-003 3.9e-006 1.00e+000  1.664755984e+002  1.664757441e+002  3.3e-011 2.18  
87  5.5e-008 7.6e-003 3.5e-006 9.96e-001  1.664756082e+002  1.664757394e+002  3.0e-011 2.21  
88  4.9e-008 7.6e-003 3.1e-006 1.00e+000  1.664756170e+002  1.664757351e+002  2.7e-011 2.23  
89  4.4e-008 7.6e-003 2.8e-006 9.92e-001  1.664756250e+002  1.664757313e+002  2.4e-011 2.26  
90  4.0e-008 6.8e-003 2.5e-006 1.01e+000  1.664756323e+002  1.664757277e+002  2.2e-011 2.28  
91  3.6e-008 6.1e-003 2.3e-006 9.94e-001  1.664756387e+002  1.664757246e+002  1.9e-011 2.31  
92  3.2e-008 5.5e-003 2.1e-006 1.00e+000  1.664756445e+002  1.664757218e+002  1.7e-011 2.33  
93  2.9e-008 5.0e-003 1.9e-006 9.97e-001  1.664756497e+002  1.664757193e+002  1.6e-011 2.36  
94  2.6e-008 4.5e-003 1.7e-006 9.96e-001  1.664756544e+002  1.664757170e+002  1.4e-011 2.37  
95  2.4e-008 4.0e-003 1.5e-006 9.87e-001  1.664756586e+002  1.664757150e+002  1.3e-011 2.40  
96  2.1e-008 3.6e-003 1.4e-006 1.00e+000  1.664756624e+002  1.664757131e+002  1.1e-011 2.42  
97  1.9e-008 3.3e-003 1.2e-006 1.04e+000  1.664756664e+002  1.664757111e+002  1.1e-011 2.45  
98  1.7e-008 2.9e-003 1.1e-006 9.90e-001  1.664756694e+002  1.664757097e+002  9.5e-012 2.46  
99  1.5e-008 2.6e-003 9.8e-007 1.02e+000  1.664756723e+002  1.664757082e+002  8.6e-012 2.50  
100 1.4e-008 2.4e-003 8.9e-007 9.85e-001  1.664756747e+002  1.664757071e+002  7.7e-012 2.51  
101 1.2e-008 2.1e-003 8.0e-007 9.74e-001  1.664756769e+002  1.664757061e+002  7.0e-012 2.54  
102 1.1e-008 1.9e-003 7.2e-007 9.80e-001  1.664756789e+002  1.664757051e+002  6.3e-012 2.56  
103 1.0e-008 1.7e-003 6.5e-007 9.66e-001  1.664756806e+002  1.664757043e+002  5.6e-012 2.59  
104 9.1e-009 1.6e-003 5.8e-007 9.84e-001  1.664756822e+002  1.664757035e+002  5.1e-012 2.62  
105 2.1e-009 1.8e-004 6.6e-008 1.02e+000  1.664756948e+002  1.664756972e+002  5.4e-013 2.64  
Interior-point optimizer terminated. Time: 2.65. 

Optimizer terminated. Time: 2.67    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6647569483e+002   Viol.  con: 4e-008   var: 0e+000 
  Dual.    obj: 1.6647569722e+002   Viol.  con: 0e+000   var: 1e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.69 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 935
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 935             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.05    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 770
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3439              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.06              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.45e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 2.9e+003 1.3e+005 0.00e+000  -1.280507084e+005 2.000000000e+000  1.0e+000 0.11  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.258771623e+005 3.574359697e+000  4.8e-001 0.16  
2   4.3e+002 5.4e+002 2.4e+004 -9.36e-001 -1.197602093e+005 1.017425592e+001  1.9e-001 0.17  
3   2.9e+002 3.6e+002 1.6e+004 -8.40e-001 -1.150415152e+005 6.302666636e+001  1.2e-001 0.20  
4   2.8e+002 3.6e+002 1.6e+004 -7.59e-001 -1.124385251e+005 2.261511437e+003  1.2e-001 0.23  
5   7.5e+001 9.6e+001 4.2e+003 -7.52e-001 -7.457725847e+004 9.579684146e+003  3.3e-002 0.25  
6   3.0e+001 3.8e+001 1.7e+003 -1.97e-001 -4.046194550e+004 1.027494966e+004  1.3e-002 0.28  
7   1.8e+001 2.3e+001 1.0e+003 3.92e-001  -2.694173777e+004 6.671787866e+003  7.9e-003 0.30  
8   9.7e+000 1.2e+001 5.4e+002 6.31e-001  -1.557332433e+004 3.882110101e+003  4.3e-003 0.33  
9   3.9e+000 5.0e+000 2.2e+002 8.13e-001  -6.391548093e+003 1.890778101e+003  1.7e-003 0.36  
10  2.1e+000 2.6e+000 1.2e+002 9.41e-001  -3.269338876e+003 1.203686358e+003  9.2e-004 0.37  
11  1.0e+000 1.3e+000 5.8e+001 9.80e-001  -1.531728224e+003 7.332098087e+002  4.7e-004 0.41  
12  8.1e-001 1.0e+000 4.5e+001 9.78e-001  -1.183154167e+003 6.026765814e+002  3.6e-004 0.42  
13  4.8e-001 6.1e-001 2.7e+001 9.74e-001  -6.439291252e+002 4.230719844e+002  2.2e-004 0.45  
14  2.7e-001 3.5e-001 1.5e+001 1.00e+000  -2.812267411e+002 3.129614598e+002  1.2e-004 0.48  
15  9.6e-002 1.5e-001 5.4e+000 1.00e+000  -7.783480588e+000 2.065095619e+002  4.4e-005 0.52  
16  8.6e-002 1.3e-001 4.9e+000 1.02e+000  1.588822045e+001  2.085235860e+002  4.0e-005 0.53  
17  5.7e-002 9.1e-002 3.3e+000 1.02e+000  6.584695786e+001  1.938293533e+002  2.7e-005 0.56  
18  2.7e-002 7.0e-002 1.6e+000 1.02e+000  1.194039681e+002  1.796939544e+002  1.3e-005 0.59  
19  7.7e-003 1.9e-001 4.5e-001 1.02e+000  1.539666071e+002  1.710722805e+002  3.6e-006 0.61  
20  3.1e-003 2.3e-001 1.8e-001 1.01e+000  1.611159427e+002  1.680967614e+002  1.5e-006 0.64  
21  1.8e-003 1.4e-001 1.1e-001 1.01e+000  1.633748671e+002  1.674649269e+002  8.7e-007 0.67  
22  5.3e-004 1.3e-001 3.3e-002 1.01e+000  1.655449158e+002  1.667967010e+002  2.7e-007 0.69  
23  3.8e-004 1.1e-001 2.4e-002 9.97e-001  1.658044393e+002  1.666959342e+002  1.9e-007 0.72  
24  2.1e-004 7.7e-002 1.3e-002 9.85e-001  1.660854180e+002  1.665889092e+002  1.1e-007 0.75  
25  1.8e-004 6.6e-002 1.1e-002 1.00e+000  1.661391664e+002  1.665725862e+002  9.5e-008 0.76  
26  1.7e-004 6.0e-002 1.0e-002 1.01e+000  1.661713384e+002  1.665611543e+002  8.5e-008 0.80  
27  1.5e-004 5.5e-002 9.2e-003 1.01e+000  1.661989226e+002  1.665496352e+002  7.7e-008 0.81  
28  1.3e-004 5.0e-002 8.3e-003 1.01e+000  1.662238941e+002  1.665394604e+002  6.9e-008 0.84  
29  1.2e-004 4.6e-002 7.5e-003 1.01e+000  1.662462600e+002  1.665302095e+002  6.2e-008 0.87  
30  1.1e-004 4.2e-002 6.7e-003 1.01e+000  1.662663338e+002  1.665218393e+002  5.6e-008 0.89  
31  9.8e-005 3.9e-002 6.1e-003 1.01e+000  1.662843461e+002  1.665142612e+002  5.0e-008 0.92  
32  8.8e-005 3.5e-002 5.5e-003 1.01e+000  1.663005103e+002  1.665074016e+002  4.5e-008 0.94  
33  7.9e-005 3.3e-002 4.9e-003 1.00e+000  1.663150165e+002  1.665011925e+002  4.1e-008 0.97  
34  7.1e-005 3.0e-002 4.4e-003 1.00e+000  1.663280353e+002  1.664955727e+002  3.7e-008 0.98  
35  6.4e-005 2.8e-002 4.0e-003 1.00e+000  1.663397200e+002  1.664904867e+002  3.3e-008 1.00  
36  5.8e-005 2.6e-002 3.6e-003 1.00e+000  1.663502082e+002  1.664858847e+002  3.0e-008 1.03  
37  5.2e-005 2.4e-002 3.2e-003 1.00e+000  1.663596234e+002  1.664817214e+002  2.7e-008 1.04  
38  4.7e-005 2.2e-002 2.9e-003 1.00e+000  1.663680761e+002  1.664779557e+002  2.4e-008 1.08  
39  4.2e-005 2.1e-002 2.6e-003 1.00e+000  1.663756657e+002  1.664745505e+002  2.2e-008 1.09  
40  3.8e-005 2.0e-002 2.4e-003 1.00e+000  1.663824810e+002  1.664714719e+002  2.0e-008 1.12  
41  3.4e-005 1.8e-002 2.1e-003 1.00e+000  1.663886015e+002  1.664686891e+002  1.8e-008 1.14  
42  3.1e-005 1.7e-002 1.9e-003 1.00e+000  1.663940986e+002  1.664661741e+002  1.6e-008 1.17  
43  2.8e-005 1.6e-002 1.7e-003 1.00e+000  1.663990362e+002  1.664639016e+002  1.4e-008 1.19  
44  2.5e-005 1.5e-002 1.5e-003 1.00e+000  1.664034716e+002  1.664618485e+002  1.3e-008 1.20  
45  2.2e-005 1.5e-002 1.4e-003 1.00e+000  1.664074562e+002  1.664599939e+002  1.2e-008 1.23  
46  2.0e-005 1.4e-002 1.3e-003 1.00e+000  1.664110360e+002  1.664583188e+002  1.0e-008 1.25  
47  1.8e-005 1.3e-002 1.1e-003 1.00e+000  1.664142523e+002  1.664568060e+002  9.4e-009 1.28  
48  1.6e-005 1.3e-002 1.0e-003 1.00e+000  1.664171423e+002  1.664554399e+002  8.4e-009 1.31  
49  1.5e-005 1.2e-002 9.1e-004 1.00e+000  1.664197392e+002  1.664542066e+002  7.6e-009 1.33  
50  1.3e-005 1.2e-002 8.2e-004 1.00e+000  1.664220729e+002  1.664530933e+002  6.8e-009 1.36  
51  1.2e-005 1.1e-002 7.4e-004 1.00e+000  1.664241703e+002  1.664520884e+002  6.2e-009 1.39  
52  1.1e-005 1.1e-002 6.6e-004 1.00e+000  1.664260553e+002  1.664511815e+002  5.5e-009 1.42  
53  9.6e-006 1.1e-002 6.0e-004 1.00e+000  1.664277496e+002  1.664503631e+002  5.0e-009 1.44  
54  8.7e-006 1.0e-002 5.4e-004 1.00e+000  1.664292727e+002  1.664496248e+002  4.5e-009 1.47  
55  7.8e-006 1.0e-002 4.8e-004 1.00e+000  1.664306418e+002  1.664489588e+002  4.0e-009 1.48  
56  7.0e-006 1.0e-002 4.4e-004 1.00e+000  1.664318727e+002  1.664483580e+002  3.6e-009 1.51  
57  6.3e-006 9.8e-003 3.9e-004 1.00e+000  1.664329794e+002  1.664478161e+002  3.3e-009 1.53  
58  5.7e-006 9.6e-003 3.5e-004 1.00e+000  1.664339743e+002  1.664473275e+002  2.9e-009 1.56  
59  5.1e-006 9.4e-003 3.2e-004 1.00e+000  1.664348690e+002  1.664468869e+002  2.7e-009 1.58  
60  4.6e-006 9.3e-003 2.9e-004 1.00e+000  1.664356734e+002  1.664464896e+002  2.4e-009 1.61  
61  4.1e-006 9.1e-003 2.6e-004 1.00e+000  1.664363968e+002  1.664461314e+002  2.1e-009 1.62  
62  3.7e-006 9.0e-003 2.3e-004 1.00e+000  1.664370472e+002  1.664458084e+002  1.9e-009 1.65  
63  3.4e-006 8.9e-003 2.1e-004 1.00e+000  1.664376321e+002  1.664455173e+002  1.7e-009 1.69  
64  3.0e-006 8.8e-003 1.9e-004 1.00e+000  1.664381581e+002  1.664452548e+002  1.6e-009 1.70  
65  2.7e-006 8.7e-003 1.7e-004 1.00e+000  1.664386310e+002  1.664450182e+002  1.4e-009 1.73  
66  2.4e-006 8.6e-003 1.5e-004 1.00e+000  1.664390565e+002  1.664448050e+002  1.3e-009 1.75  
67  2.2e-006 8.5e-003 1.4e-004 1.00e+000  1.664394391e+002  1.664446129e+002  1.1e-009 1.78  
68  2.0e-006 8.4e-003 1.2e-004 1.00e+000  1.664397834e+002  1.664444397e+002  1.0e-009 1.79  
69  1.8e-006 8.4e-003 1.1e-004 1.00e+000  1.664400931e+002  1.664442838e+002  9.2e-010 1.83  
70  1.6e-006 8.3e-003 1.0e-004 1.00e+000  1.664403717e+002  1.664441434e+002  8.3e-010 1.84  
71  1.4e-006 8.2e-003 9.0e-005 1.00e+000  1.664406223e+002  1.664440169e+002  7.5e-010 1.87  
72  1.3e-006 8.2e-003 8.1e-005 1.00e+000  1.664408478e+002  1.664439029e+002  6.7e-010 1.89  
73  1.2e-006 8.1e-003 7.3e-005 1.00e+000  1.664410506e+002  1.664438003e+002  6.1e-010 1.92  
74  1.1e-006 8.1e-003 6.6e-005 1.00e+000  1.664412331e+002  1.664437079e+002  5.5e-010 1.93  
75  9.5e-007 8.0e-003 5.9e-005 1.00e+000  1.664413973e+002  1.664436246e+002  4.9e-010 1.97  
76  8.5e-007 8.0e-003 5.3e-005 1.00e+000  1.664415450e+002  1.664435497e+002  4.4e-010 1.98  
77  7.7e-007 8.0e-003 4.8e-005 1.00e+000  1.664416779e+002  1.664434821e+002  4.0e-010 2.01  
78  6.9e-007 7.9e-003 4.3e-005 1.00e+000  1.664417975e+002  1.664434213e+002  3.6e-010 2.03  
79  6.2e-007 7.9e-003 3.9e-005 1.00e+000  1.664419050e+002  1.664433665e+002  3.2e-010 2.06  
80  5.6e-007 7.9e-003 3.5e-005 1.00e+000  1.664420018e+002  1.664433171e+002  2.9e-010 2.08  
81  5.0e-007 7.8e-003 3.1e-005 1.00e+000  1.664420888e+002  1.664432726e+002  2.6e-010 2.11  
82  4.5e-007 7.8e-003 2.8e-005 1.00e+000  1.664421671e+002  1.664432325e+002  2.4e-010 2.12  
83  4.1e-007 7.8e-003 2.5e-005 1.00e+000  1.664422375e+002  1.664431964e+002  2.1e-010 2.15  
84  3.7e-007 7.8e-003 2.3e-005 1.00e+000  1.664423009e+002  1.664431639e+002  1.9e-010 2.17  
85  3.3e-007 7.7e-003 2.1e-005 1.00e+000  1.664423579e+002  1.664431346e+002  1.7e-010 2.20  
86  3.0e-007 7.7e-003 1.9e-005 9.99e-001  1.664424092e+002  1.664431083e+002  1.5e-010 2.21  
87  2.7e-007 7.7e-003 1.7e-005 1.00e+000  1.664424554e+002  1.664430845e+002  1.4e-010 2.25  
88  2.4e-007 7.7e-003 1.5e-005 9.98e-001  1.664424969e+002  1.664430632e+002  1.3e-010 2.26  
89  2.2e-007 7.7e-003 1.3e-005 1.00e+000  1.664425343e+002  1.664430440e+002  1.1e-010 2.28  
90  2.0e-007 7.6e-003 1.2e-005 1.00e+000  1.664425679e+002  1.664430266e+002  1.0e-010 2.31  
91  1.8e-007 7.6e-003 1.1e-005 9.99e-001  1.664425982e+002  1.664430111e+002  9.1e-011 2.32  
92  1.6e-007 7.6e-003 9.8e-006 1.00e+000  1.664426255e+002  1.664429970e+002  8.2e-011 2.36  
93  1.4e-007 7.6e-003 8.9e-006 1.00e+000  1.664426500e+002  1.664429844e+002  7.4e-011 2.39  
94  1.3e-007 7.6e-003 8.0e-006 1.00e+000  1.664426721e+002  1.664429730e+002  6.6e-011 2.43  
95  1.2e-007 7.6e-003 7.2e-006 9.98e-001  1.664426919e+002  1.664429628e+002  6.0e-011 2.46  
96  1.0e-007 7.6e-003 6.5e-006 1.00e+000  1.664427098e+002  1.664429536e+002  5.4e-011 2.48  
97  9.3e-008 7.5e-003 5.8e-006 1.00e+000  1.664427259e+002  1.664429453e+002  4.8e-011 2.51  
98  8.4e-008 7.5e-003 5.2e-006 9.95e-001  1.664427404e+002  1.664429379e+002  4.4e-011 2.53  
99  7.6e-008 7.5e-003 4.7e-006 9.97e-001  1.664427534e+002  1.664429312e+002  3.9e-011 2.56  
100 6.8e-008 7.5e-003 4.2e-006 1.00e+000  1.664427652e+002  1.664429252e+002  3.5e-011 2.59  
101 6.1e-008 6.8e-003 3.8e-006 1.01e+000  1.664427759e+002  1.664429196e+002  3.2e-011 2.61  
102 5.5e-008 6.1e-003 3.4e-006 1.01e+000  1.664427856e+002  1.664429146e+002  2.9e-011 2.64  
103 5.0e-008 5.5e-003 3.1e-006 1.00e+000  1.664427941e+002  1.664429102e+002  2.6e-011 2.65  
104 4.5e-008 4.9e-003 2.8e-006 9.91e-001  1.664428018e+002  1.664429063e+002  2.3e-011 2.68  
105 4.0e-008 4.4e-003 2.5e-006 9.98e-001  1.664428087e+002  1.664429028e+002  2.1e-011 2.70  
106 3.6e-008 4.0e-003 2.3e-006 1.00e+000  1.664428149e+002  1.664428996e+002  1.9e-011 2.73  
107 3.3e-008 3.6e-003 2.0e-006 1.02e+000  1.664428209e+002  1.664428965e+002  1.7e-011 2.75  
108 2.9e-008 3.2e-003 1.8e-006 9.89e-001  1.664428259e+002  1.664428939e+002  1.5e-011 2.78  
109 2.6e-008 2.9e-003 1.6e-006 9.71e-001  1.664428303e+002  1.664428917e+002  1.4e-011 2.79  
110 2.4e-008 2.6e-003 1.5e-006 1.00e+000  1.664428344e+002  1.664428896e+002  1.2e-011 2.82  
111 2.1e-008 2.4e-003 1.3e-006 9.91e-001  1.664428380e+002  1.664428877e+002  1.1e-011 2.84  
112 1.9e-008 2.1e-003 1.2e-006 1.04e+000  1.664428419e+002  1.664428857e+002  1.0e-011 2.87  
113 1.7e-008 1.9e-003 1.1e-006 1.02e+000  1.664428450e+002  1.664428840e+002  9.3e-012 2.89  
114 1.6e-008 1.7e-003 9.7e-007 9.86e-001  1.664428476e+002  1.664428827e+002  8.4e-012 2.92  
115 1.4e-008 1.5e-003 8.7e-007 9.75e-001  1.664428499e+002  1.664428816e+002  7.6e-012 2.95  
116 1.3e-008 1.4e-003 7.8e-007 1.09e+000  1.664428529e+002  1.664428798e+002  7.1e-012 2.96  
117 1.2e-008 1.3e-003 7.1e-007 1.12e+000  1.664428557e+002  1.664428783e+002  6.8e-012 3.00  
118 1.1e-008 1.1e-003 6.4e-007 9.87e-001  1.664428572e+002  1.664428776e+002  6.1e-012 3.01  
119 9.7e-009 1.0e-003 5.7e-007 9.46e-001  1.664428585e+002  1.664428769e+002  5.5e-012 3.04  
120 8.7e-009 9.1e-004 5.1e-007 8.13e-001  1.664428597e+002  1.664428764e+002  4.9e-012 3.06  
121 8.7e-009 8.2e-004 4.6e-007 9.71e-001  1.664428608e+002  1.664428759e+002  4.4e-012 3.09  
122 7.9e-009 7.4e-004 4.2e-007 8.01e-001  1.664428618e+002  1.664428754e+002  4.0e-012 3.10  
123 8.1e-009 6.6e-004 3.8e-007 9.26e-001  1.664428627e+002  1.664428750e+002  3.6e-012 3.14  
124 7.3e-009 6.0e-004 3.4e-007 8.30e-001  1.664428635e+002  1.664428746e+002  3.2e-012 3.15  
125 6.8e-009 5.4e-004 3.0e-007 8.87e-001  1.664428642e+002  1.664428742e+002  2.9e-012 3.18  
126 6.0e-009 4.8e-004 2.7e-007 8.57e-001  1.664428649e+002  1.664428739e+002  2.6e-012 3.20  
127 5.4e-009 4.4e-004 2.5e-007 6.43e-001  1.664428655e+002  1.664428736e+002  2.4e-012 3.23  
128 5.2e-009 3.9e-004 2.2e-007 2.48e+000  1.664428660e+002  1.664428733e+002  2.1e-012 3.25  
129 4.9e-009 3.5e-004 2.0e-007 7.09e-001  1.664428665e+002  1.664428732e+002  1.9e-012 3.26  
130 4.6e-009 3.2e-004 1.8e-007 3.47e+000  1.664428669e+002  1.664428731e+002  1.7e-012 3.29  
131 6.9e-009 2.9e-004 1.6e-007 7.97e-001  1.664428672e+002  1.664428730e+002  1.6e-012 3.31  
132 8.6e-009 2.6e-004 1.5e-007 1.04e+000  1.664428677e+002  1.664428727e+002  1.4e-012 3.34  
133 1.0e-008 2.3e-004 1.3e-007 2.04e+000  1.664428679e+002  1.664428729e+002  1.3e-012 3.35  
134 8.9e-009 2.1e-004 1.2e-007 6.21e-001  1.664428682e+002  1.664428729e+002  1.2e-012 3.38  
135 1.1e-008 1.9e-004 1.1e-007 1.22e+000  1.664428687e+002  1.664428723e+002  1.2e-012 3.40  
136 1.1e-008 1.7e-004 9.5e-008 4.13e-001  1.664428689e+002  1.664428719e+002  1.0e-012 3.42  
137 1.1e-008 1.5e-004 8.6e-008 5.28e-001  1.664428691e+002  1.664428719e+002  9.2e-013 3.45  
Interior-point optimizer terminated. Time: 3.45. 

Optimizer terminated. Time: 3.46    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6644286910e+002   Viol.  con: 3e-007   var: 0e+000 
  Dual.    obj: 1.6644287192e+002   Viol.  con: 0e+000   var: 9e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.49 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 935
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 935             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 770
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3439              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.05              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.45e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 2.9e+003 1.3e+005 0.00e+000  -1.280489612e+005 2.000000000e+000  1.0e+000 0.08  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.258746554e+005 3.573540236e+000  4.8e-001 0.09  
2   4.3e+002 5.4e+002 2.4e+004 -9.36e-001 -1.197248549e+005 1.020047660e+001  1.9e-001 0.13  
3   2.9e+002 3.6e+002 1.6e+004 -8.39e-001 -1.150061321e+005 6.350454843e+001  1.2e-001 0.14  
4   2.8e+002 3.6e+002 1.6e+004 -7.59e-001 -1.124090179e+005 2.256518439e+003  1.2e-001 0.16  
5   7.5e+001 9.5e+001 4.1e+003 -7.52e-001 -7.445946529e+004 9.583523617e+003  3.3e-002 0.19  
6   3.0e+001 3.8e+001 1.7e+003 -1.95e-001 -4.029027551e+004 1.021235565e+004  1.3e-002 0.20  
7   1.8e+001 2.3e+001 9.9e+002 3.95e-001  -2.693755987e+004 6.641979210e+003  7.9e-003 0.22  
8   9.5e+000 1.2e+001 5.2e+002 6.31e-001  -1.531787280e+004 3.830168849e+003  4.2e-003 0.25  
9   3.6e+000 4.6e+000 2.0e+002 8.16e-001  -5.905174613e+003 1.796571511e+003  1.6e-003 0.27  
10  2.0e+000 2.5e+000 1.1e+002 9.47e-001  -3.113317745e+003 1.193554747e+003  8.9e-004 0.28  
11  8.5e-001 1.1e+000 4.7e+001 9.81e-001  -1.224279515e+003 6.160622953e+002  3.8e-004 0.33  
12  8.2e-001 1.1e+000 4.6e+001 9.50e-001  -1.207775098e+003 5.913560028e+002  3.7e-004 0.34  
13  5.1e-001 6.6e-001 2.8e+001 9.72e-001  -7.035575654e+002 4.268397901e+002  2.3e-004 0.37  
14  3.1e-001 4.1e-001 1.7e+001 1.00e+000  -3.505781644e+002 3.411858720e+002  1.4e-004 0.41  
15  1.1e-001 1.7e-001 6.1e+000 9.98e-001  -2.684414631e+001 2.143800910e+002  5.0e-005 0.45  
16  8.2e-002 1.3e-001 4.7e+000 1.02e+000  2.198016847e+001  2.045205529e+002  3.8e-005 0.47  
17  4.1e-002 8.3e-002 2.4e+000 1.02e+000  9.510958201e+001  1.869519883e+002  1.9e-005 0.50  
18  1.4e-002 8.3e-002 8.2e-001 1.02e+000  1.425314864e+002  1.741990342e+002  6.7e-006 0.52  
19  6.3e-003 7.2e-002 3.6e-001 1.01e+000  1.556734721e+002  1.695990146e+002  2.9e-006 0.55  
20  1.5e-003 1.6e-001 9.2e-002 1.01e+000  1.638769426e+002  1.673910358e+002  7.5e-007 0.56  
21  8.1e-004 1.1e-001 5.0e-002 9.78e-001  1.650488580e+002  1.669447222e+002  4.1e-007 0.58  
22  2.5e-004 1.1e-001 1.6e-002 9.89e-001  1.659980764e+002  1.666010472e+002  1.3e-007 0.61  
23  1.2e-004 8.9e-002 7.5e-003 1.01e+000  1.662206457e+002  1.665064858e+002  6.3e-008 0.62  
24  4.6e-005 8.6e-002 3.0e-003 1.01e+000  1.663410619e+002  1.664565349e+002  2.6e-008 0.64  
25  2.1e-005 7.8e-002 1.4e-003 1.01e+000  1.663845711e+002  1.664381925e+002  1.2e-008 0.67  
26  1.9e-005 7.1e-002 1.3e-003 1.00e+000  1.663890815e+002  1.664373688e+002  1.1e-008 0.69  
27  1.7e-005 6.5e-002 1.2e-003 1.01e+000  1.663923561e+002  1.664358020e+002  9.7e-009 0.70  
28  1.6e-005 5.9e-002 1.0e-003 1.00e+000  1.663953626e+002  1.664344572e+002  8.8e-009 0.73  
29  1.4e-005 5.4e-002 9.3e-004 1.00e+000  1.663980533e+002  1.664332323e+002  7.9e-009 0.75  
30  1.3e-005 5.0e-002 8.4e-004 1.00e+000  1.664004729e+002  1.664321291e+002  7.1e-009 0.78  
31  1.1e-005 4.5e-002 7.5e-004 1.00e+000  1.664026469e+002  1.664311335e+002  6.4e-009 0.80  
32  1.0e-005 4.2e-002 6.8e-004 1.00e+000  1.664046009e+002  1.664302355e+002  5.8e-009 0.83  
33  9.2e-006 3.8e-002 6.1e-004 1.00e+000  1.664063571e+002  1.664294256e+002  5.2e-009 0.84  
34  8.3e-006 3.5e-002 5.5e-004 1.00e+000  1.664079358e+002  1.664286953e+002  4.7e-009 0.87  
35  7.5e-006 3.3e-002 5.0e-004 1.00e+000  1.664093549e+002  1.664280367e+002  4.2e-009 0.89  
36  6.7e-006 3.0e-002 4.5e-004 1.00e+000  1.664106307e+002  1.664274428e+002  3.8e-009 0.92  
37  6.1e-006 2.8e-002 4.0e-004 1.00e+000  1.664117777e+002  1.664269075e+002  3.4e-009 0.94  
38  5.5e-006 2.6e-002 3.6e-004 1.00e+000  1.664128090e+002  1.664264250e+002  3.1e-009 0.95  
39  4.9e-006 2.4e-002 3.3e-004 1.00e+000  1.664137364e+002  1.664259901e+002  2.8e-009 0.98  
40  4.4e-006 2.2e-002 2.9e-004 1.00e+000  1.664145703e+002  1.664255980e+002  2.5e-009 1.00  
41  4.0e-006 2.1e-002 2.6e-004 1.00e+000  1.664153202e+002  1.664252447e+002  2.2e-009 1.01  
42  3.6e-006 2.0e-002 2.4e-004 1.00e+000  1.664159945e+002  1.664249262e+002  2.0e-009 1.04  
43  3.2e-006 1.8e-002 2.1e-004 1.00e+000  1.664166010e+002  1.664246392e+002  1.8e-009 1.06  
44  2.9e-006 1.7e-002 1.9e-004 1.00e+000  1.664171463e+002  1.664243805e+002  1.6e-009 1.09  
45  2.6e-006 1.6e-002 1.7e-004 1.00e+000  1.664176368e+002  1.664241474e+002  1.5e-009 1.11  
46  2.3e-006 1.6e-002 1.6e-004 1.00e+000  1.664180780e+002  1.664239373e+002  1.3e-009 1.12  
47  2.1e-006 1.5e-002 1.4e-004 1.00e+000  1.664184749e+002  1.664237482e+002  1.2e-009 1.15  
48  1.9e-006 1.4e-002 1.3e-004 1.00e+000  1.664188319e+002  1.664235778e+002  1.1e-009 1.17  
49  1.7e-006 1.3e-002 1.1e-004 1.00e+000  1.664191531e+002  1.664234243e+002  9.6e-010 1.19  
50  1.5e-006 1.3e-002 1.0e-004 1.00e+000  1.664194420e+002  1.664232861e+002  8.6e-010 1.22  
51  1.4e-006 1.2e-002 9.2e-005 1.00e+000  1.664197020e+002  1.664231617e+002  7.8e-010 1.23  
52  1.2e-006 1.2e-002 8.3e-005 1.00e+000  1.664199359e+002  1.664230495e+002  7.0e-010 1.25  
53  1.1e-006 1.1e-002 7.4e-005 1.00e+000  1.664201464e+002  1.664229486e+002  6.3e-010 1.28  
54  1.0e-006 1.1e-002 6.7e-005 1.00e+000  1.664203357e+002  1.664228577e+002  5.7e-010 1.29  
55  9.1e-007 1.1e-002 6.0e-005 1.00e+000  1.664205060e+002  1.664227759e+002  5.1e-010 1.31  
56  8.2e-007 1.0e-002 5.4e-005 1.00e+000  1.664206593e+002  1.664227021e+002  4.6e-010 1.34  
57  7.4e-007 1.0e-002 4.9e-005 1.00e+000  1.664207972e+002  1.664226357e+002  4.1e-010 1.36  
58  6.6e-007 9.9e-003 4.4e-005 1.00e+000  1.664209212e+002  1.664225759e+002  3.7e-010 1.39  
59  6.0e-007 9.7e-003 4.0e-005 1.00e+000  1.664210328e+002  1.664225220e+002  3.3e-010 1.40  
60  5.4e-007 9.5e-003 3.6e-005 1.00e+000  1.664211332e+002  1.664224735e+002  3.0e-010 1.42  
61  4.8e-007 9.3e-003 3.2e-005 9.99e-001  1.664212235e+002  1.664224298e+002  2.7e-010 1.45  
62  4.4e-007 9.1e-003 2.9e-005 1.00e+000  1.664213047e+002  1.664223904e+002  2.4e-010 1.47  
63  3.9e-007 9.0e-003 2.6e-005 1.00e+000  1.664213778e+002  1.664223549e+002  2.2e-010 1.50  
64  3.5e-007 8.9e-003 2.3e-005 1.00e+000  1.664214435e+002  1.664223229e+002  2.0e-010 1.53  
65  3.2e-007 8.7e-003 2.1e-005 1.00e+000  1.664215026e+002  1.664222941e+002  1.8e-010 1.54  
66  2.9e-007 8.6e-003 1.9e-005 9.99e-001  1.664215558e+002  1.664222682e+002  1.6e-010 1.56  
67  2.6e-007 8.5e-003 1.7e-005 1.00e+000  1.664216037e+002  1.664222448e+002  1.4e-010 1.59  
68  2.3e-007 8.4e-003 1.5e-005 1.00e+000  1.664216468e+002  1.664222237e+002  1.3e-010 1.61  
69  2.1e-007 8.3e-003 1.4e-005 9.99e-001  1.664216855e+002  1.664222048e+002  1.2e-010 1.64  
70  1.9e-007 8.3e-003 1.2e-005 1.00e+000  1.664217204e+002  1.664221878e+002  1.1e-010 1.65  
71  1.7e-007 8.2e-003 1.1e-005 1.00e+000  1.664217518e+002  1.664221724e+002  9.5e-011 1.67  
72  1.5e-007 8.1e-003 1.0e-005 9.99e-001  1.664217800e+002  1.664221586e+002  8.5e-011 1.70  
73  1.4e-007 8.1e-003 9.0e-006 1.00e+000  1.664218055e+002  1.664221461e+002  7.7e-011 1.72  
74  1.2e-007 8.0e-003 8.1e-006 1.00e+000  1.664218283e+002  1.664221349e+002  6.9e-011 1.73  
75  1.1e-007 8.0e-003 7.3e-006 1.00e+000  1.664218490e+002  1.664221247e+002  6.2e-011 1.76  
76  1.0e-007 8.0e-003 6.6e-006 1.00e+000  1.664218677e+002  1.664221156e+002  5.6e-011 1.79  
77  9.0e-008 7.2e-003 5.9e-006 1.01e+000  1.664218847e+002  1.664221072e+002  5.0e-011 1.83  
78  8.1e-008 6.5e-003 5.3e-006 1.01e+000  1.664219000e+002  1.664220997e+002  4.6e-011 1.86  
79  7.3e-008 5.8e-003 4.8e-006 9.98e-001  1.664219134e+002  1.664220931e+002  4.1e-011 1.89  
80  6.5e-008 5.2e-003 4.3e-006 1.01e+000  1.664219258e+002  1.664220870e+002  3.7e-011 1.90  
81  5.9e-008 4.7e-003 3.9e-006 1.00e+000  1.664219367e+002  1.664220817e+002  3.3e-011 1.93  
82  5.3e-008 4.2e-003 3.5e-006 1.01e+000  1.664219467e+002  1.664220767e+002  3.0e-011 1.95  
83  4.8e-008 3.8e-003 3.2e-006 9.99e-001  1.664219554e+002  1.664220725e+002  2.7e-011 1.98  
84  4.3e-008 3.4e-003 2.8e-006 9.97e-001  1.664219633e+002  1.664220686e+002  2.4e-011 2.00  
85  3.9e-008 3.1e-003 2.6e-006 1.01e+000  1.664219707e+002  1.664220650e+002  2.2e-011 2.03  
86  3.5e-008 2.8e-003 2.3e-006 1.01e+000  1.664219773e+002  1.664220618e+002  2.0e-011 2.04  
87  3.1e-008 2.5e-003 2.1e-006 1.01e+000  1.664219830e+002  1.664220589e+002  1.8e-011 2.08  
88  2.8e-008 2.3e-003 1.9e-006 1.01e+000  1.664219883e+002  1.664220564e+002  1.6e-011 2.09  
89  2.5e-008 2.0e-003 1.7e-006 1.00e+000  1.664219929e+002  1.664220541e+002  1.5e-011 2.12  
90  2.3e-008 1.8e-003 1.5e-006 1.00e+000  1.664219970e+002  1.664220521e+002  1.3e-011 2.14  
91  2.0e-008 1.6e-003 1.4e-006 1.01e+000  1.664220009e+002  1.664220502e+002  1.2e-011 2.15  
92  1.8e-008 1.5e-003 1.2e-006 9.95e-001  1.664220042e+002  1.664220486e+002  1.1e-011 2.18  
93  1.7e-008 1.3e-003 1.1e-006 1.03e+000  1.664220076e+002  1.664220469e+002  9.8e-012 2.20  
94  1.5e-008 1.2e-003 9.9e-007 9.77e-001  1.664220103e+002  1.664220456e+002  8.8e-012 2.23  
95  1.3e-008 1.1e-003 8.9e-007 1.01e+000  1.664220127e+002  1.664220444e+002  7.9e-012 2.25  
96  1.2e-008 9.7e-004 8.0e-007 9.46e-001  1.664220149e+002  1.664220434e+002  7.2e-012 2.28  
97  1.1e-008 8.7e-004 7.2e-007 1.09e+000  1.664220176e+002  1.664220420e+002  6.7e-012 2.29  
98  9.9e-009 7.8e-004 6.5e-007 1.04e+000  1.664220196e+002  1.664220410e+002  6.2e-012 2.32  
99  8.9e-009 7.1e-004 5.8e-007 1.04e+000  1.664220213e+002  1.664220401e+002  5.7e-012 2.34  
100 8.0e-009 6.4e-004 5.3e-007 9.25e-001  1.664220226e+002  1.664220396e+002  5.1e-012 2.37  
101 7.2e-009 5.7e-004 4.7e-007 9.77e-001  1.664220237e+002  1.664220390e+002  4.6e-012 2.39  
102 6.5e-009 5.1e-004 4.3e-007 9.61e-001  1.664220247e+002  1.664220385e+002  4.2e-012 2.42  
103 5.8e-009 4.6e-004 3.8e-007 9.23e-001  1.664220257e+002  1.664220381e+002  3.7e-012 2.43  
104 5.2e-009 4.2e-004 3.5e-007 1.02e+000  1.664220266e+002  1.664220377e+002  3.4e-012 2.46  
105 4.7e-009 3.8e-004 3.1e-007 9.44e-001  1.664220273e+002  1.664220373e+002  3.1e-012 2.48  
106 4.2e-009 3.4e-004 2.8e-007 9.92e-001  1.664220280e+002  1.664220370e+002  2.8e-012 2.51  
107 3.8e-009 3.0e-004 2.5e-007 9.77e-001  1.664220286e+002  1.664220367e+002  2.5e-012 2.53  
108 3.6e-009 2.7e-004 2.3e-007 1.06e+000  1.664220293e+002  1.664220364e+002  2.3e-012 2.56  
109 3.2e-009 2.5e-004 2.0e-007 1.00e+000  1.664220298e+002  1.664220361e+002  2.1e-012 2.59  
110 1.9e-009 1.4e-005 1.2e-008 9.06e-001  1.664220339e+002  1.664220343e+002  2.0e-013 2.61  
Interior-point optimizer terminated. Time: 2.62. 

Optimizer terminated. Time: 2.64    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6642203390e+002   Viol.  con: 6e-008   var: 0e+000 
  Dual.    obj: 1.6642203429e+002   Viol.  con: 0e+000   var: 9e-005 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.65 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 935
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 935             
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 770
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3439              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.05              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.05            
Factor     - nonzeros before factor : 1.64e+004         after factor           : 1.45e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 2.9e+003 1.3e+005 0.00e+000  -1.280480912e+005 2.000000000e+000  1.0e+000 0.08  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.258735652e+005 3.573328892e+000  4.8e-001 0.11  
2   4.3e+002 5.4e+002 2.4e+004 -9.36e-001 -1.197006533e+005 1.021695034e+001  1.9e-001 0.13  
3   2.9e+002 3.6e+002 1.6e+004 -8.39e-001 -1.149813539e+005 6.382045194e+001  1.2e-001 0.16  
4   2.8e+002 3.6e+002 1.6e+004 -7.59e-001 -1.123855733e+005 2.255168080e+003  1.2e-001 0.19  
5   7.5e+001 9.5e+001 4.1e+003 -7.51e-001 -7.423640900e+004 9.613665884e+003  3.3e-002 0.22  
6   3.0e+001 3.8e+001 1.6e+003 -1.92e-001 -4.018136442e+004 1.017434432e+004  1.3e-002 0.25  
7   1.8e+001 2.3e+001 9.9e+002 3.96e-001  -2.694046022e+004 6.638991895e+003  7.9e-003 0.28  
8   9.5e+000 1.2e+001 5.2e+002 6.31e-001  -1.520613787e+004 3.808618254e+003  4.1e-003 0.31  
9   3.3e+000 4.2e+000 1.8e+002 8.18e-001  -5.318598512e+003 1.679725465e+003  1.4e-003 0.34  
10  1.6e+000 2.0e+000 8.9e+001 9.54e-001  -2.417061815e+003 1.055018156e+003  7.1e-004 0.38  
11  9.5e-001 1.2e+000 5.3e+001 9.86e-001  -1.370875317e+003 7.035305063e+002  4.2e-004 0.41  
12  8.6e-001 1.1e+000 4.8e+001 9.64e-001  -1.259042707e+003 6.421422591e+002  3.8e-004 0.42  
13  4.8e-001 6.1e-001 2.7e+001 9.77e-001  -6.392963992e+002 4.225710561e+002  2.1e-004 0.45  
14  2.6e-001 3.4e-001 1.4e+001 1.00e+000  -2.623575687e+002 3.061807194e+002  1.2e-004 0.47  
15  9.2e-002 1.5e-001 5.3e+000 1.00e+000  -2.395069185e+000 2.056350583e+002  4.3e-005 0.50  
16  8.6e-002 1.3e-001 4.9e+000 1.02e+000  1.576226327e+001  2.083372227e+002  4.0e-005 0.52  
17  6.0e-002 9.5e-002 3.4e+000 1.02e+000  6.107035269e+001  1.952046163e+002  2.8e-005 0.55  
18  3.4e-002 7.3e-002 1.9e+000 1.02e+000  1.081903654e+002  1.827220087e+002  1.6e-005 0.58  
19  9.3e-003 1.7e-001 5.4e-001 1.02e+000  1.512029308e+002  1.719128605e+002  4.3e-006 0.59  
20  3.4e-003 2.1e-001 2.0e-001 1.01e+000  1.605110604e+002  1.682874979e+002  1.7e-006 0.62  
21  1.3e-003 1.3e-001 7.6e-002 1.01e+000  1.642779607e+002  1.671863494e+002  6.2e-007 0.64  
22  8.5e-004 1.0e-001 5.1e-002 9.84e-001  1.649813507e+002  1.669397467e+002  4.2e-007 0.67  
23  2.6e-004 1.1e-001 1.6e-002 9.86e-001  1.659710717e+002  1.665859684e+002  1.3e-007 0.69  
24  9.4e-005 1.0e-001 6.0e-003 1.01e+000  1.662464778e+002  1.664756788e+002  5.1e-008 0.72  
25  3.7e-005 9.6e-002 2.4e-003 1.01e+000  1.663445762e+002  1.664349664e+002  2.0e-008 0.73  
26  1.7e-005 8.1e-002 1.1e-003 1.00e+000  1.663787299e+002  1.664206000e+002  9.5e-009 0.77  
27  1.5e-005 7.4e-002 1.0e-003 1.00e+000  1.663822232e+002  1.664199215e+002  8.5e-009 0.78  
28  1.4e-005 6.7e-002 9.0e-004 1.01e+000  1.663847897e+002  1.664187110e+002  7.7e-009 0.81  
29  1.2e-005 6.1e-002 8.1e-004 1.00e+000  1.663871434e+002  1.664176672e+002  6.9e-009 0.83  
30  1.1e-005 5.6e-002 7.3e-004 1.00e+000  1.663892516e+002  1.664167186e+002  6.2e-009 0.86  
31  1.0e-005 5.1e-002 6.6e-004 1.00e+000  1.663911475e+002  1.664158643e+002  5.6e-009 0.87  
32  9.0e-006 4.7e-002 5.9e-004 1.00e+000  1.663928516e+002  1.664150938e+002  5.0e-009 0.91  
33  8.1e-006 4.3e-002 5.3e-004 1.00e+000  1.663943835e+002  1.664143991e+002  4.5e-009 0.92  
34  7.3e-006 3.9e-002 4.8e-004 1.00e+000  1.663957608e+002  1.664137729e+002  4.1e-009 0.95  
35  6.6e-006 3.6e-002 4.3e-004 1.00e+000  1.663969991e+002  1.664132084e+002  3.7e-009 0.97  
36  5.9e-006 3.3e-002 3.9e-004 1.00e+000  1.663981125e+002  1.664126996e+002  3.3e-009 1.00  
37  5.3e-006 3.1e-002 3.5e-004 1.00e+000  1.663991138e+002  1.664122411e+002  3.0e-009 1.01  
38  4.8e-006 2.9e-002 3.1e-004 1.00e+000  1.664000141e+002  1.664118279e+002  2.7e-009 1.04  
39  4.3e-006 2.7e-002 2.8e-004 1.00e+000  1.664008238e+002  1.664114555e+002  2.4e-009 1.06  
40  3.9e-006 2.5e-002 2.5e-004 1.00e+000  1.664015520e+002  1.664111199e+002  2.2e-009 1.09  
41  3.5e-006 2.3e-002 2.3e-004 1.00e+000  1.664022068e+002  1.664108175e+002  2.0e-009 1.11  
42  3.1e-006 2.1e-002 2.1e-004 1.00e+000  1.664027957e+002  1.664105450e+002  1.8e-009 1.12  
43  2.8e-006 2.0e-002 1.9e-004 1.00e+000  1.664033254e+002  1.664102994e+002  1.6e-009 1.16  
44  2.5e-006 1.9e-002 1.7e-004 1.00e+000  1.664038018e+002  1.664100782e+002  1.4e-009 1.17  
45  2.3e-006 1.8e-002 1.5e-004 1.00e+000  1.664042303e+002  1.664098789e+002  1.3e-009 1.19  
46  2.1e-006 1.7e-002 1.4e-004 1.00e+000  1.664046158e+002  1.664096994e+002  1.2e-009 1.22  
47  1.9e-006 1.6e-002 1.2e-004 1.00e+000  1.664049626e+002  1.664095377e+002  1.0e-009 1.23  
48  1.7e-006 1.5e-002 1.1e-004 1.00e+000  1.664052747e+002  1.664093922e+002  9.3e-010 1.25  
49  1.5e-006 1.4e-002 9.8e-005 1.00e+000  1.664055554e+002  1.664092611e+002  8.4e-010 1.26  
50  1.4e-006 1.4e-002 8.9e-005 1.00e+000  1.664058080e+002  1.664091431e+002  7.6e-010 1.29  
51  1.2e-006 1.3e-002 8.0e-005 1.00e+000  1.664060352e+002  1.664090368e+002  6.8e-010 1.31  
52  1.1e-006 1.2e-002 7.2e-005 1.00e+000  1.664062397e+002  1.664089410e+002  6.1e-010 1.33  
53  9.9e-007 1.2e-002 6.5e-005 1.00e+000  1.664064236e+002  1.664088548e+002  5.5e-010 1.34  
54  8.9e-007 1.2e-002 5.8e-005 1.00e+000  1.664065892e+002  1.664087772e+002  5.0e-010 1.36  
55  8.0e-007 1.1e-002 5.2e-005 1.00e+000  1.664067381e+002  1.664087073e+002  4.5e-010 1.39  
56  7.2e-007 1.1e-002 4.7e-005 1.00e+000  1.664068720e+002  1.664086443e+002  4.0e-010 1.40  
57  6.5e-007 1.0e-002 4.2e-005 1.00e+000  1.664069925e+002  1.664085876e+002  3.6e-010 1.44  
58  5.8e-007 1.0e-002 3.8e-005 1.00e+000  1.664071010e+002  1.664085365e+002  3.3e-010 1.45  
59  5.2e-007 9.9e-003 3.4e-005 1.00e+000  1.664071985e+002  1.664084904e+002  2.9e-010 1.48  
60  4.7e-007 9.7e-003 3.1e-005 1.00e+000  1.664072862e+002  1.664084489e+002  2.6e-010 1.50  
61  4.2e-007 9.5e-003 2.8e-005 1.00e+000  1.664073651e+002  1.664084116e+002  2.4e-010 1.51  
62  3.8e-007 9.3e-003 2.5e-005 1.00e+000  1.664074361e+002  1.664083780e+002  2.1e-010 1.54  
63  3.4e-007 9.1e-003 2.3e-005 1.00e+000  1.664074999e+002  1.664083476e+002  1.9e-010 1.56  
64  3.1e-007 9.0e-003 2.0e-005 1.00e+000  1.664075574e+002  1.664083203e+002  1.7e-010 1.58  
65  2.8e-007 8.8e-003 1.8e-005 1.00e+000  1.664076091e+002  1.664082956e+002  1.6e-010 1.61  
66  2.5e-007 8.7e-003 1.6e-005 1.00e+000  1.664076556e+002  1.664082735e+002  1.4e-010 1.62  
67  2.3e-007 8.6e-003 1.5e-005 9.99e-001  1.664076974e+002  1.664082535e+002  1.3e-010 1.64  
68  2.0e-007 8.5e-003 1.3e-005 1.00e+000  1.664077351e+002  1.664082356e+002  1.1e-010 1.67  
69  1.8e-007 8.4e-003 1.2e-005 1.00e+000  1.664077689e+002  1.664082194e+002  1.0e-010 1.69  
70  1.6e-007 8.3e-003 1.1e-005 1.00e+000  1.664077994e+002  1.664082048e+002  9.2e-011 1.70  
71  1.5e-007 8.2e-003 9.7e-006 1.00e+000  1.664078268e+002  1.664081917e+002  8.3e-011 1.73  
72  1.3e-007 8.2e-003 8.7e-006 9.99e-001  1.664078515e+002  1.664081799e+002  7.5e-011 1.75  
73  1.2e-007 8.1e-003 7.9e-006 1.00e+000  1.664078737e+002  1.664081693e+002  6.7e-011 1.76  
74  1.1e-007 8.0e-003 7.1e-006 9.97e-001  1.664078937e+002  1.664081597e+002  6.0e-011 1.79  
75  9.7e-008 8.0e-003 6.4e-006 9.98e-001  1.664079117e+002  1.664081511e+002  5.4e-011 1.81  
76  8.7e-008 7.9e-003 5.7e-006 9.99e-001  1.664079279e+002  1.664081434e+002  4.9e-011 1.83  
77  7.9e-008 7.9e-003 5.2e-006 1.00e+000  1.664079425e+002  1.664081364e+002  4.4e-011 1.86  
78  7.1e-008 7.9e-003 4.6e-006 1.00e+000  1.664079556e+002  1.664081301e+002  4.0e-011 1.87  
79  6.4e-008 7.8e-003 4.2e-006 9.97e-001  1.664079674e+002  1.664081245e+002  3.6e-011 1.89  
80  5.7e-008 7.8e-003 3.8e-006 9.96e-001  1.664079780e+002  1.664081194e+002  3.2e-011 1.92  
81  5.2e-008 7.7e-003 3.4e-006 9.94e-001  1.664079875e+002  1.664081148e+002  2.9e-011 1.94  
82  4.6e-008 7.7e-003 3.0e-006 9.92e-001  1.664079961e+002  1.664081107e+002  2.6e-011 1.95  
83  4.2e-008 7.7e-003 2.7e-006 1.00e+000  1.664080038e+002  1.664081070e+002  2.3e-011 1.98  
84  3.8e-008 7.6e-003 2.5e-006 9.98e-001  1.664080108e+002  1.664081037e+002  2.1e-011 2.00  
85  3.4e-008 7.6e-003 2.2e-006 9.95e-001  1.664080171e+002  1.664081007e+002  1.9e-011 2.01  
86  3.0e-008 7.6e-003 2.0e-006 1.00e+000  1.664080227e+002  1.664080980e+002  1.7e-011 2.03  
87  2.7e-008 6.8e-003 1.8e-006 1.01e+000  1.664080279e+002  1.664080954e+002  1.5e-011 2.06  
88  2.5e-008 6.2e-003 1.6e-006 1.00e+000  1.664080325e+002  1.664080932e+002  1.4e-011 2.08  
89  2.2e-008 5.5e-003 1.5e-006 1.00e+000  1.664080366e+002  1.664080913e+002  1.2e-011 2.09  
90  2.0e-008 5.0e-003 1.3e-006 1.00e+000  1.664080402e+002  1.664080895e+002  1.1e-011 2.12  
91  1.8e-008 4.5e-003 1.2e-006 9.83e-001  1.664080436e+002  1.664080879e+002  1.0e-011 2.14  
92  1.6e-008 4.0e-003 1.1e-006 9.93e-001  1.664080465e+002  1.664080865e+002  9.1e-012 2.15  
93  1.5e-008 3.6e-003 9.6e-007 9.85e-001  1.664080492e+002  1.664080852e+002  8.2e-012 2.18  
94  1.3e-008 3.3e-003 8.6e-007 9.68e-001  1.664080516e+002  1.664080841e+002  7.4e-012 2.21  
95  1.2e-008 2.9e-003 7.7e-007 1.02e+000  1.664080540e+002  1.664080829e+002  6.7e-012 2.23  
96  1.1e-008 2.6e-003 7.0e-007 1.00e+000  1.664080559e+002  1.664080820e+002  6.0e-012 2.26  
97  9.6e-009 2.4e-003 6.3e-007 9.96e-001  1.664080577e+002  1.664080811e+002  5.4e-012 2.29  
98  8.7e-009 2.1e-003 5.6e-007 1.06e+000  1.664080597e+002  1.664080801e+002  5.0e-012 2.31  
99  7.9e-009 1.9e-003 5.1e-007 1.02e+000  1.664080612e+002  1.664080794e+002  4.5e-012 2.34  
100 7.1e-009 1.7e-003 4.6e-007 8.82e-001  1.664080624e+002  1.664080788e+002  4.1e-012 2.36  
101 6.4e-009 1.6e-003 4.1e-007 1.07e+000  1.664080639e+002  1.664080781e+002  3.8e-012 2.39  
102 5.8e-009 1.4e-003 3.7e-007 9.29e-001  1.664080648e+002  1.664080776e+002  3.4e-012 2.40  
103 5.2e-009 1.3e-003 3.3e-007 1.25e+000  1.664080657e+002  1.664080771e+002  3.1e-012 2.43  
104 5.2e-009 1.1e-003 3.0e-007 1.17e+000  1.664080671e+002  1.664080764e+002  3.0e-012 2.45  
105 4.7e-009 1.0e-003 2.7e-007 9.26e-001  1.664080677e+002  1.664080761e+002  2.7e-012 2.48  
106 4.0e-009 9.2e-004 2.4e-007 1.03e+000  1.664080684e+002  1.664080758e+002  2.5e-012 2.50  
107 3.6e-009 8.3e-004 2.2e-007 1.01e+000  1.664080689e+002  1.664080755e+002  2.2e-012 2.56  
108 3.3e-009 7.5e-004 2.0e-007 9.85e-001  1.664080693e+002  1.664080753e+002  2.0e-012 2.57  
109 3.0e-009 6.7e-004 1.8e-007 9.86e-001  1.664080697e+002  1.664080751e+002  1.8e-012 2.62  
110 2.9e-009 6.1e-004 1.6e-007 9.80e-001  1.664080701e+002  1.664080750e+002  1.6e-012 2.64  
111 2.7e-009 5.5e-004 1.4e-007 9.29e-001  1.664080704e+002  1.664080748e+002  1.5e-012 2.67  
112 2.2e-009 4.9e-004 1.3e-007 9.55e-001  1.664080707e+002  1.664080747e+002  1.3e-012 2.68  
113 1.9e-009 4.4e-004 1.2e-007 1.31e+000  1.664080710e+002  1.664080745e+002  1.2e-012 2.71  
114 1.8e-009 4.0e-004 1.0e-007 1.27e+000  1.664080713e+002  1.664080744e+002  1.1e-012 2.75  
115 2.0e-009 3.6e-004 9.4e-008 1.54e+000  1.664080715e+002  1.664080743e+002  9.5e-013 2.76  
Interior-point optimizer terminated. Time: 2.78. 

Optimizer terminated. Time: 2.79    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6640807152e+002   Viol.  con: 4e-008   var: 0e+000 
  Dual.    obj: 1.6640807426e+002   Viol.  con: 0e+000   var: 2e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.82 seconds.
Solving took 9 GP solves and 36.6 seconds.

Solves with these variables bounded:
   value near lower bound: Mission1.CruiseAlt
   value near upper bound: Mission1.T_{t_{4.1_{max-Cruise}}}, Mission1.Aircraft.Engine.Thrust.\alpha_{max}, Mission1.Aircraft.Wing.WingNoStruct.A_{tri}, Mission1.TotalTime, Mission1.Aircraft.HorizontalTail.WingBox.M_{r_{out}}, Mission1.Aircraft.LandingGear.d_{nacelle}

Checking for relaxed constants...
Solution check warning: Primal solution computed cost did not match solver-returned cost: 1.4957404423002604e+110 vs 1.49570315323e+110
GP iteration 0 has relaxed constants

Cost
----
 1.496e+110

Free Variables
--------------
                   | Mission1.Aircraft.Engine.Turbine.Relax1
        C_{p_{t2}} : 2.251                                                Cp Value for Combustion Products in LP Turbine

                   | Mission1.Aircraft.Fuselage.Relax1
          l_{nose} : 1.042                                                Nose length
          n_{pass} : [ 2.86     ]                                         Number of passengers

                   | Mission1.Aircraft.Relax1
f_{L_{total/wing}} : 1.656                                                Total lift as a percentage of wing lift

                   | Mission1.Aircraft.Wing.WingNoStruct.Relax1
     \tan(\Lambda) : 1.133                                                Tangent of quarter-chord sweep angle

                   | Mission1.FlightState.Atmosphere.Relax1
           L_{atm} : [ 1.77      1         1         1         1        ] Temperature lapse rate
            T_{sl} : [ 1         1         1.25      1         1        ] Temperature at sea level

                   | Mission1.Relax1
           R_{req} : 2.362                                                Required Cruise Range

GP iteration 1 has relaxed constants

Cost
----
 7.486e+74

Free Variables
--------------
          | Mission1.Aircraft.Engine.Combustor.Relax1
hold_{4a} : 1.093        1+(gamma-1)/2 * M_4a**2

          | Mission1.Aircraft.Fuselage.Relax1
 n_{pass} : [ 1.03     ] Number of passengers

          | Mission1.Aircraft.LandingGear.Relax1
 h_{hold} : 1.006        Hold height

Solution check warning: Primal solution computed cost did not match solver-returned cost: 3.7053685618089006e+72 vs 3.70525127556e+72
WEIGHT DIFFERENCES


Total Fuel Weight Percent Diff: [-92.94682299]


Total Aircraft Weight Percent Diff: [-21.48055841]


Engine Weight Percent Diff: -56.27821413978838


Fuselage Weight Percent Diff: -0.8697192866916202


Payload Weight Percent Diff: [-0.04003556]


VT Weight Percent Diff: -8.60758712182523


HT Weight Percent Diff: -93.23325222378857


Wing Weight Percent Diff: 8.267463545631589




WING DIFFERENCES


Wing Span Percent Diff: -0.029996083210493307


Wing Area Percent Diff: 32.90005291809683




HORIZONTAL TAIL DIFFERENCES


HT Area Percent Diff: 40.489239118989694




VERTICAL TAIL DIFFERENCES




VT Span Percent Diff: -11.02232568009664


VT Area Percent Diff: -60.386822499406826




CRUISE SEGMENT 1 DRAG DIFFERENCES


Overall Cd Percent Diff: [-18.5473063]


L/D Percent Diff: [24.01021344]


Nacelle Cd Percent Diff: [-94.27640965]


HT Cd Percent Diff: [-80.76936907] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-58.00301221] dimensionless


Wing Cd percent Diff: [-14.2292761]
Induced Drag Cd Percent Diff: [1.21937867]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-90.57035921]




FUSELAGE DIFFERENCES




Weight of HB material: -38.3599226491295 


Weight of VB material: 87.82532026626271 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.71260518]

Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 123.525s

OK

Generating XML reports...
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 d:\anaconda2\lib\site-packages (0.24.2)
Requirement already satisfied: numpy>=1.12.0 in d:\anaconda2\lib\site-packages (from pandas) (1.16.4)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas) (2.8.0)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\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 c:\users\jenkins\appdata\local\temp\pip-req-build-zfj0s9
  Running command git clone -q https://github.com/convexengineering/gpfit.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-zfj0s9'
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_push_models\mosek\gpkit (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt>=1.1.8->gpkit->gpfit==0.1) (2018.0.0)
Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt>=1.1.8->gpkit->gpfit==0.1) (2018.0.0)
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=25428 sha256=78d9bc1a71f54a3baf6996ab60e2806f2cc9a4aba8e1f7b78beccf0ad8f97d29
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-uap_t4\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 c:\users\jenkins\appdata\local\temp\pip-req-build-b9cixk
  Running command git clone -q https://github.com/convexengineering/gassolar.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-b9cixk'
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.2.2)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_push_models\mosek\gpkit (from gassolar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.24.2)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.8.1 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.9)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.2.3)
Requirement already satisfied: six in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.12.0)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.8.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gassolar==0.0.0.0) (1.0.2)
Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt>=1.1.8->gpkit->gassolar==0.0.0.0) (2018.0.0)
Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt>=1.1.8->gpkit->gassolar==0.0.0.0) (2018.0.0)
Building wheels for collected packages: gassolar
  Building wheel for gassolar (setup.py): started
  Building wheel for gassolar (setup.py): still running...
  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=4895585 sha256=aa3481939671f65c5819b0466c75009d1f839dc8c92d4d32c90aac19db72baa2
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-du63zw\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 d:\jenkins\workspace\gplibrary_push_models\mosek\solar
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.2.2)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_push_models\mosek\gpkit (from solar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.24.2)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in d:\jenkins\workspace\gplibrary_push_models\mosek\gplibrary (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.8.1 in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.9)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.2.3)
Requirement already satisfied: six in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.12.0)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.8.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->solar==0.0.0.0) (1.0.2)
Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt>=1.1.8->gpkit->solar==0.0.0.0) (2018.0.0)
Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt>=1.1.8->gpkit->solar==0.0.0.0) (2018.0.0)
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=14963 sha256=dd684a141442653c885f7feffba69a43f13e06f7d923ee6abaccf91924f978f6
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-k8vrl3\wheels\ce\3e\c7\684dc25c7e90a46c88fdf4c730f9fc06ebd99e02f86c9e22e3
Successfully built solar
Installing collected packages: solar
Successfully installed solar-0.0.0.0
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
adding test for 'solar/npod_trade.py'

N=1
Beginning signomial solve.
Solving took 5 GP solves and 1.53 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 1632916.9408 but bound is 600000.0000
Warning: Variable Mission.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1259333.2946 but bound is 1000000.0000

N=3
Beginning signomial solve.
rw: problem unsolved after 51 iterations.

    The last result is available in Model.program.gps[-1].result. If the gps
    appear to be converging, you may wish to increase the iteration limit by
    calling .localsolve(..., iteration_limit=NEWLIMIT).
e: The constraint CFRPFabric.Relax.tmin >= 1 is infeasible by 228.083990%

N=5
Beginning signomial solve.
Solving took 5 GP solves and 1.52 seconds.
Warning: Variable Mission3.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 Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 989673.4661 but bound is 600000.0000
Warning: Variable Mission3.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1019678.5407 but bound is 1000000.0000

N=7
Beginning signomial solve.
Solving took 5 GP solves and 1.65 seconds.
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 976142.1464 but bound is 600000.0000
Warning: Variable Mission4.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1042059.4119 but bound is 1000000.0000

N=9
Beginning signomial solve.
Solving took 5 GP solves and 1.95 seconds.
Warning: Variable Mission5.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 Mission5.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1007400.4745 but bound is 600000.0000
Warning: Variable Mission5.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1092545.5117 but bound is 1000000.0000

N=0
Beginning signomial solve.
Solving took 4 GP solves and 1.11 seconds.
Warning: Variable Mission6.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 Mission6.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2012 but bound is 600000.0000

N=1
Beginning signomial solve.
Solving took 5 GP solves and 2.49 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.
rw: problem unsolved after 51 iterations.

    The last result is available in Model.program.gps[-1].result. If the gps
    appear to be converging, you may wish to increase the iteration limit by
    calling .localsolve(..., iteration_limit=NEWLIMIT).
e: The constraint CFRPFabric.Relax.tmin >= 1 is infeasible by 228.083990%

N=5
Beginning signomial solve.
Solving took 5 GP solves and 2.81 seconds.
Warning: Variable Mission3.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 Mission3.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 Mission3.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 2.85 seconds.
Warning: Variable Mission4.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 Mission4.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 Mission4.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 3.19 seconds.
Warning: Variable Mission5.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 Mission5.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 Mission5.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 2.87 seconds.
Warning: Variable Mission6.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 Mission6.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119116.3963 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 5 seconds.
Allowing negative dual variable(s) as small as -7.283850822839555e-12.
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 671709.7359 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 4.61 seconds.
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 729183.6151 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 4.67 seconds.
Allowing negative dual variable(s) as small as -4.058001786162724e-11.
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 802959.5988 but bound is 600000.0000
Using solver 'mosek'
Solving for 7672 variables.
Solving took 2.49 seconds.
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 839122.5075 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 5.08 seconds.
Allowing negative dual variable(s) as small as -1.078991616106778e-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 671709.7359 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 4.63 seconds.
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 729183.6153 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 4.56 seconds.
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 802959.5990 but bound is 600000.0000
Using solver 'mosek'
Solving for 7672 variables.
Solving took 2.49 seconds.
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 839122.5076 but bound is 600000.0000
Beginning signomial solve.
Solving took 4 GP solves and 0.871 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 1119121.2013 but bound is 600000.0000
Beginning signomial solve.
Solving took 4 GP solves and 0.96 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 1119121.2013 but bound is 600000.0000

Running tests...
----------------------------------------------------------------------
D:\Anaconda2\lib\site-packages\pint\quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped.
  warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning)
..D:\jenkins\workspace\gplibrary_Push_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
D:\jenkins\workspace\gplibrary_Push_Models\mosek\venv2_gpkit\lib\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 306.638s

OK

Generating XML reports...
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 d:\anaconda2\lib\site-packages (0.24.2)
Requirement already satisfied: numpy>=1.12.0 in d:\anaconda2\lib\site-packages (from pandas) (1.16.4)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas) (2.8.0)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\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 c:\users\jenkins\appdata\local\temp\pip-req-build-haj0bc
  Running command git clone -q https://github.com/hoburg/gpfit.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-haj0bc'
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_push_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_push_models\mosek\gpkit (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt>=1.1.8->gpkit->gpfit==0.1) (2018.0.0)
Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt>=1.1.8->gpkit->gpfit==0.1) (2018.0.0)
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=25428 sha256=9e479b1cafe3f0a4d84ce08e181b3615bdd306295f0fcc1cecb95ade7d393066
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-yrktcy\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 d:\jenkins\workspace\gplibrary_push_models\mosek\gplibrary
Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.9)
Requirement already satisfied: funcsigs; python_version == "2.7" in d:\anaconda2\lib\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=66225 sha256=ce932bcb1806d17833a0aec6e90e13bef78988f5a1d4c3fe29393c0756842454
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-i_y2tq\wheels\7e\b9\8c\c001975c73314aa5cbad40b4ac5bd7134640e5d0e53f0a5710
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
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 0.034 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.115 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.052 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.039 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.023 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 1.08 seconds.
Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.081 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.09 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.14 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 3.74 seconds.
Using solver 'mosek'
Solving for 13 variables.
Solving took 0.035 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 0.815 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 1619897.4138 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.095 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 2.61 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 2220953.3481 but bound is 1000000.0000
Warning: Variable TailAero1.Re could cause inaccurate result because it is above upper bound. Solution is 2499787.9721 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 2223877.9562 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 1884891.2729 but bound is 700000.0000
Warning: Variable WingAero1.Re could cause inaccurate result because it is above upper bound. Solution is 1910419.4978 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 0.042 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.035 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.029 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.025 seconds.
Solving took 4 GP solves and 0.142 seconds.
Beginning signomial solve.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.1 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.095 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.112 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.152 seconds.
Solving took 4 GP solves and 0.475 seconds.

Running tests...
----------------------------------------------------------------------
..D:\Anaconda2\lib\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 21.048s

OK

Generating XML reports...
Cloning into 'eVTOL'...
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Checking out files: 100% (121/121), done.
adding test for 'models/model_tests.py'

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 7.397s

OK

Generating XML reports...

----------------------------------------------------------------------
Ran 243 tests in 67.825s

OK
 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 ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gplibrary']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {})

calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'})

calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
  attempt 1
  attempt 2
  attempt 3
  attempt 4
  attempt 5

SETTINGS
defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {})


(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_Push_Models\mosek>exit 0 
INFO: Starting to record.
INFO: Processing JUnit
INFO: [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'D:\jenkins\workspace\gplibrary_Push_Models\mosek' for the testing framework 'JUnit'.
INFO: Check 'Failed Tests' threshold.
INFO: Check 'Skipped Tests' threshold.
INFO: Setting the build status to SUCCESS
INFO: Stopping recording.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS