Console Output

Started by upstream project "gpkit_PullRequest_Models" build number 401
originally caused by:
 GitHub pull request #1428 of commit f31ccd680335f4d50ecec381d980d80b3aeb6433, no merge conflicts.
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on windows10x64 in workspace C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek
No credentials specified
Wiping out workspace first.
Cloning the remote Git repository
Cloning repository https://github.com/convexengineering/gpkit
 > C:\Program Files\Git\cmd\git init C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek # timeout=10
Fetching upstream changes from https://github.com/convexengineering/gpkit
 > C:\Program Files\Git\cmd\git --version # timeout=10
 > C:\Program Files\Git\cmd\git fetch --tags --progress https://github.com/convexengineering/gpkit +refs/heads/*:refs/remotes/origin/* # timeout=10
 > C:\Program Files\Git\cmd\git config remote.origin.url https://github.com/convexengineering/gpkit # timeout=10
 > C:\Program Files\Git\cmd\git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10
 > C:\Program Files\Git\cmd\git config remote.origin.url https://github.com/convexengineering/gpkit # timeout=10
Fetching upstream changes from https://github.com/convexengineering/gpkit
 > C:\Program Files\Git\cmd\git fetch --tags --progress https://github.com/convexengineering/gpkit +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master # timeout=10
Merging Revision 9701643602e871f73fa8233a58b228fcbc5d18ee (refs/remotes/origin/pr/1428/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='DEFAULT', fastForwardMode='FF'}
 > C:\Program Files\Git\cmd\git rev-parse "origin/master^{commit}" # timeout=10
 > C:\Program Files\Git\cmd\git config core.sparsecheckout # timeout=10
 > C:\Program Files\Git\cmd\git checkout -f origin/master # timeout=3
 > C:\Program Files\Git\cmd\git merge --ff 9701643602e871f73fa8233a58b228fcbc5d18ee # timeout=10
 > C:\Program Files\Git\cmd\git rev-parse "HEAD^{commit}" # timeout=10
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 > C:\Program Files\Git\cmd\git show-ref --tags -d # timeout=10
Checking out Revision 9701643602e871f73fa8233a58b228fcbc5d18ee (origin/pr/1428/merge, origin/master)
 > C:\Program Files\Git\cmd\git config core.sparsecheckout # timeout=10
 > C:\Program Files\Git\cmd\git checkout -f 9701643602e871f73fa8233a58b228fcbc5d18ee # timeout=3
Commit message: "Merge f31ccd680335f4d50ecec381d980d80b3aeb6433 into 4207f387028800de95fce7466a09f76a74455434"
Using 'Changelog to branch' strategy.
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[description-setter] Description set: <a title="python3 compatible parse_variables" href="https://github.com/convexengineering/gpkit/pull/1428">PR 1428</a>: python3 compatible parse_variables
[Execution node] check if [windows10x64] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [windows10x64] 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\jenkins6607863745258765786.bat

C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>echo C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps 
C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps

C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>REM turn on the anaconda console 

C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>call activate.bat   || exit /b 666 

(base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>REM Create a virtualenv to install everything into 

(base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>SET VENV=C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit 

(base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>virtualenv --system-site-packages C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit 
New python executable in C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts\python.exe
Installing setuptools, pip, wheel...done.

(base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>call C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts\activate.bat 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>REM Install coverage into the virtualenv to the coverage command blow uses the virtualenv python 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>pip install coverage 
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: coverage in c:\anaconda2\lib\site-packages (4.5.4)

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>pip install ad 
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (1.3.2)

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>pip install future 
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Requirement already satisfied: future in c:\anaconda2\lib\site-packages (0.17.1)

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>SET GPKITBUILD=C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\build_gpkit 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>set PATH=C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts;C:\Anaconda2;C:\Anaconda2\Library\mingw-w64\bin;C:\Anaconda2\Library\usr\bin;C:\Anaconda2\Library\bin;C:\Anaconda2\Scripts;C:\Anaconda2\bin;C:\Anaconda2\condabin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\WINDOWS\System32\OpenSSH;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\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;C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\Scripts;C:\Anaconda2;C:\Anaconda2\Library\mingw-w64\bin;C:\Anaconda2\Library\usr\bin;C:\Anaconda2\Library\bin;C:\Anaconda2\Scripts;C:\Anaconda2\bin;C:\Anaconda2\condabin;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\WINDOWS\System32\OpenSSH;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\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) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>if mosek == cvxopt pip install --upgrade cvxopt   || exit /b 666 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>if mosek == cvxopt python -c "import cvxopt; print cvxopt.__version__"   || exit /b 666 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>if mosek == cvxopt set GPKITSOLVERS=cvxopt 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>if mosek == mosek msktestlic   || exit /b 666 
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.
Mosek license manager: License path: C:\Users\jenkins\mosek\mosek.lic
Mosek license manager:  Checkout license feature 'PTS' from flexlm.
Mosek license manager:  Checkout time 0.02. r: 0 status: 0
Interior-point optimizer started.
Presolve started.
Eliminator started.
Freed constraints in eliminator : 0
Eliminator terminated.
Eliminator - tries                  : 1                 time                   : 0.00            
Lin. dep.  - tries                  : 0                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.00    
Interior-point optimizer terminated. Time: 0.00. 

Optimizer terminated. Time: 0.06    
************************************
A license was checked out correctly.
************************************

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>if mosek == mosek python -c "__import__('mosek').Env()"   || exit /b 666 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>if mosek == mosek set GPKITSOLVERS=mosek, mosek_cli 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>dir C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\build_gpkit 
 Volume in drive C has no label.
 Volume Serial Number is C4C9-8F11

 Directory of C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek

File Not Found

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>python -c "import scipy; print scipy.__version__" 
1.2.1

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>python -c "import numpy; print numpy.__version__" 
1.16.3

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>python -c "import pint; print pint.__version__" 
0.9

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>REM Install gpkit to run the documentation examples 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>pip install -e C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\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:///C:/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/windows10x64/optimizer/mosek
Requirement already satisfied: numpy>=1.13.3 in c:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (1.16.4)
Requirement already satisfied: pint>=0.8.1 in c:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (0.9)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (1.2.2)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in c:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (1.2.3)
Requirement already satisfied: six in c:\anaconda2\lib\site-packages (from gpkit==0.9.1.0) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit==0.9.1.0) (1.0.2)
Requirement already satisfied: mkl in c:\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 c:\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) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>REM Show the settings file 

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>type C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\gpkit\env\settings 
The system cannot find the path specified.

(venv2_gpkit) (base) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True)" 
No filename given.
Usage:
     mskexpopt FILENAME [-primal] [-dual] [-p parameterfile]
Return code: 1052
Description: MSK_RES_ERR_FILE_OPEN [An error occurred while opening a file.]
...................................................................................................................................................................................................................................................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\8\tools\platform\win64x86\h\mosek.h
#     Found C:\Program Files\Mosek\8\tools\platform\win64x86\bin\mosek64_8_0.dll
#     Found C:\Program Files\Mosek\8\tools\examples\c\scopt-ext.c
#     Found C:\Program Files\Mosek\8\tools\examples\c\expopt.c
#     Found C:\Program Files\Mosek\8\tools\examples\c\dgopt.c
#     Found C:\Program Files\Mosek\8\tools\examples\c\scopt-ext.h
#     Found C:\Program Files\Mosek\8\tools\examples\c\expopt.h
#     Found C:\Program Files\Mosek\8\tools\examples\c\dgopt.h
#     Found C:\Program Files\Mosek\8\tools\platform\win64x86\h\mosek.h
# Found mosek version 8, installed to C:\Program Files\Mosek
#
# Building mosek...
#     Replacing directory _mosek\lib
#     Replacing directory _mosek\build
#     Replacing directory C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\build_gpkit
#
#   Copying expopt library files to _mosek\build
#     Copying C:\Program Files\Mosek\8\tools\examples\c\scopt-ext.c
#     Copying C:\Program Files\Mosek\8\tools\examples\c\expopt.c
#     Copying C:\Program Files\Mosek\8\tools\examples\c\dgopt.c
#     Copying C:\Program Files\Mosek\8\tools\examples\c\scopt-ext.h
#     Copying C:\Program Files\Mosek\8\tools\examples\c\expopt.h
#     Copying C:\Program Files\Mosek\8\tools\examples\c\dgopt.h
#     Copying C:\Program Files\Mosek\8\tools\platform\win64x86\h\mosek.h
#
#   Applying expopt patches...
#
#     Change in _mosek\build\dgopt.con line 653
#     --         printf("Number of Hessian non-zeros: %d\n",nlh[0]->numhesnz);
#     ++ MSK_echotask(task,MSK_STREAM_MSG,"Number of Hessian non-zeros: %d\n",n
#
#     Change in _mosek\build\expopt.con line 566
#     --         printf("Warning: The variable with index '%d' has only positiv
#     ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in
#
#     Change in _mosek\build\expopt.con line 579
#     --         printf("Warning: The variable with index '%d' has only negativ
#     ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in
#
#     Change in _mosek\build\expopt.con line 1115
#     --     printf ("solsta = %d, prosta = %d\n", (int)*solsta,(int)*prosta);
#     ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "solsta = %d, prosta = %d\n", 
#
#   Building expopt library...
#     Calling 'gcc -fpic -shared -Wl,--export-all-symbols,-R "C:\Program Files\Mosek\8\tools\platform\win64x86\bin"    _mosek\build\scopt-ext.c _mosek\build\expopt.c _mosek\build\dgopt.c   "C:\Program Files\Mosek\8\tools\platform\win64x86\bin\mosek64_8_0.dll" -o C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\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 C:/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/windows10x64/optimizer/mosek/build_gpkit/expopt.so -l "C:/Program Files/Mosek/8/tools/platform/win64x86/bin/mosek64_8_0.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 gCloning into 'gplibrary'...
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Obtaining file:///C:/Users/jenkins/workspace/gpkit_PullRequest_Models/buildnode/windows10x64/optimizer/mosek/gplibrary
Installing collected packages: gpkitmodels
  Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels
Cloning into 'robust'...
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Processing c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\robust
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek (from robust==0.0.0) (0.9.1.0)
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from robust==0.0.0) (1.16.4)
Requirement already satisfied: matplotlib in c:\anaconda2\lib\site-packages (from robust==0.0.0) (2.2.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from robust==0.0.0) (1.2.2)
Requirement already satisfied: pint>=0.8.1 in c:\anaconda2\lib\site-packages (from gpkit->robust==0.0.0) (0.9)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->robust==0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in c:\anaconda2\lib\site-packages (from gpkit->robust==0.0.0) (1.2.3)
Requirement already satisfied: six in c:\anaconda2\lib\site-packages (from gpkit->robust==0.0.0) (1.12.0)
Requirement already satisfied: python-dateutil>=2.1 in c:\anaconda2\lib\site-packages (from matplotlib->robust==0.0.0) (2.8.0)
Requirement already satisfied: pyparsing!=2.0.4,!=2.1.2,!=2.1.6,>=2.0.1 in c:\anaconda2\lib\site-packages (from matplotlib->robust==0.0.0) (2.4.2)
Requirement already satisfied: pytz in c:\anaconda2\lib\site-packages (from matplotlib->robust==0.0.0) (2019.2)
Requirement already satisfied: backports.functools-lru-cache in c:\anaconda2\lib\site-packages (from matplotlib->robust==0.0.0) (1.5)
Requirement already satisfied: cycler>=0.10 in c:\anaconda2\lib\site-packages (from matplotlib->robust==0.0.0) (0.10.0)
Requirement already satisfied: kiwisolver>=1.0.1 in c:\anaconda2\lib\site-packages (from matplotlib->robust==0.0.0) (1.1.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->robust==0.0.0) (1.0.2)
Requirement already satisfied: mkl in c:\anaconda2\lib\site-packages (from cvxopt>=1.1.8->gpkit->robust==0.0.0) (2018.0.0)
Requirement already satisfied: setuptools in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from kiwisolver>=1.0.1->matplotlib->robust==0.0.0) (41.2.0)
Requirement already satisfied: intel-openmp==2018.0.0 in c:\anaconda2\lib\site-packages (from mkl->cvxopt>=1.1.8->gpkit->robust==0.0.0) (2018.0.0)
Building wheels for collected packages: robust
  Building wheel for robust (setup.py): started
  Building wheel for robust (setup.py): finished with status 'done'
  Created wheel for robust: filename=robust-0.0.0-cp27-none-any.whl size=219079 sha256=a7378a48a08e2e7646dc468e1337612855edb34351f2e3cefaab9e0815bfa3ec
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-i_d2no\wheels\63\42\8c\aba78dc7b7a1ee7d6698e31a4879b2c80be9b64f3a6578ce1c
Successfully built robust
Installing collected packages: robust
Successfully installed robust-0.0.0
adding test for 'robust/testing/t_linearization.py'
adding test for 'robust/testing/t_equivalent_posynomials.py'
adding test for 'robust/testing/t_two_term_approximation.py'
adding test for 'robust/testing/t_robust_gp_tools.py'
adding test for 'robust/testing/t_primitives.py'

Running tests...
----------------------------------------------------------------------
..........
----------------------------------------------------------------------
Ran 10 tests in 34.641s

OK

Generating XML reports...
Cloning into 'shopping'...
adding test for 'test.py'
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.051 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.021 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.083 seconds.

Running tests...
----------------------------------------------------------------------
...
----------------------------------------------------------------------
Ran 3 tests in 0.420s

OK

Generating XML reports...
Cloning into 'gassolar'...
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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 c:\anaconda2\lib\site-packages (0.24.2)
Requirement already satisfied: numpy>=1.12.0 in c:\anaconda2\lib\site-packages (from pandas) (1.16.4)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in c:\anaconda2\lib\site-packages (from pandas) (2.8.0)
Requirement already satisfied: six>=1.5 in c:\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-82dzlf
  Running command git clone -q https://github.com/hoburg/gpfit.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-82dzlf'
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Requirement already satisfied: mkl in c:\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 c:\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=d753b55dd34322587bf757f6a7e7e751f9fb529aeae21599715aa331c07788fb
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-9kw6bl\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 c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\gassolar
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.2.2)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek (from gassolar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.24.2)
Requirement already satisfied: gpfit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.8.1 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.9)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.2.3)
Requirement already satisfied: six in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.12.0)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.8.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gassolar==0.0.0.0) (1.0.2)
Requirement already satisfied: mkl in c:\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 c:\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): finished with status 'done'
  Created wheel for gassolar: filename=gassolar-0.0.0.0-cp27-none-any.whl size=4895585 sha256=fc36f3ac2d94c2238c49ff2d631a7b89d55c7e56647f5e152457a4be03d11467
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-ktzwfl\wheels\97\aa\da\f14cb30f8a30f7807dc0c251288a3f56e2299c77d2eb0b5498
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 0.251 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 0.984 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 0.367 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 0.727 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 0.438 seconds.
Warning: Variable Mission.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.3538 but bound is 150000.0000
Warning: Variable Mission.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 102558.3827 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 2.28 seconds.
Warning: Variable Mission1.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103379.4302 but bound is 150000.0000
Warning: Variable Mission1.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103406.0831 but bound is 150000.0000
Using solver 'mosek_cli'
Solving for 1250 variables.
Solving took 0.472 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 2.67 seconds.
Warning: Variable Mission1.FlightSegment.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103379.2971 but bound is 150000.0000
Warning: Variable Mission1.FlightSegment10.AircraftPerf.WingAero.Re could cause inaccurate result because it is below lower bound. Solution is 103406.1793 but bound is 150000.0000

Running tests...
----------------------------------------------------------------------
c:\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)
..C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\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 29.370s

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 c:\anaconda2\lib\site-packages (0.24.2)
Requirement already satisfied: numpy>=1.12.0 in c:\anaconda2\lib\site-packages (from pandas) (1.16.4)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in c:\anaconda2\lib\site-packages (from pandas) (2.8.0)
Requirement already satisfied: six>=1.5 in c:\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-nmgrbh
  Running command git clone -q https://github.com/hoburg/gpfit.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-nmgrbh'
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Requirement already satisfied: mkl in c:\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 c:\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=23bbd1ae1031d160aca69fceb45e5c6363894c9c76872bf495c530a22d8d3f11
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-q6r2zn\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 -1.297850715786808e-13.
Solving took 4 GP solves and 2.74 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.516593e-13.
Solving took 4 GP solves and 2.15 seconds.
Allowing negative dual variable(s) as small as -6.199129751194299e-13.
Allowing negative dual variable(s) as small as -1.377372879380473e-13.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.626
design loiter speed [m/s] = 25.071
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.384099540709116e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.356
optimum loiter speed for min power, end of loiter [m/s] = 25.000
optimum cruise speed, inbound [m/s] = 25.637
optimum cruise speed, outbound [m/s] = 36.421
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.171093747998145e-12.
Solving took 4 GP solves and 1.58 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.06 seconds.
Max payload weight [lbf] = 28.242
Max take off weight [lbf] = 166.638
Allowing negative dual variable(s) as small as -6.216017e-13.
Allowing negative dual variable(s) as small as -1.393956e-13.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.626
design loiter speed [m/s] = 25.071
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.384596e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.356
optimum loiter speed for min power, end of loiter [m/s] = 25.000
optimum cruise speed, inbound [m/s] = 25.637
optimum cruise speed, outbound [m/s] = 36.421
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.171055e-12.
Solving took 4 GP solves and 2.66 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.91 seconds.
Max payload weight [lbf] = 28.242
Max take off weight [lbf] = 166.638

Running tests...
----------------------------------------------------------------------
c:\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 34.174s

OK

Generating XML reports...
Cloning into 'turbofan'...
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Processing c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\turbofan
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.9)
Requirement already satisfied: future in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.17.1)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\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=ef59f7b486a21d663385067d4271e960f69e1e36a4e58c9342f71a4c0ef7e811
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-eb1scn\wheels\cb\74\b0\7dbe51588fa00064eb72033427061ca24f2fd137af6591418b
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 0.129 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.066 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.082 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.081 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.059 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.068 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.06 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.063 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.064 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.066 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.079 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.067 seconds.
Using solver 'mosek'
Solving for 327 variables.
Solving took 0.074 seconds.
Solving took 13 GP solves and 1.45 seconds.

Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 1.938s

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
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-ixld2m
  Running command git clone -q https://github.com/hoburg/turbofan.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-ixld2m'
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.9)
Requirement already satisfied: future in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.17.1)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\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=17262bbd5de441a25fde52611506a948880388f6f9d5d22682fe9913dde72fab
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-unzxj3\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 c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\spaircraft
Requirement already satisfied: turbofan in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from SPaircraft==0.0.0) (0.0.0.0)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek (from SPaircraft==0.0.0) (0.9.1.0)
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from turbofan->SPaircraft==0.0.0) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan->SPaircraft==0.0.0) (1.2.2)
Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan->SPaircraft==0.0.0) (0.9)
Requirement already satisfied: future in c:\anaconda2\lib\site-packages (from turbofan->SPaircraft==0.0.0) (0.17.1)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->SPaircraft==0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in c:\anaconda2\lib\site-packages (from gpkit->SPaircraft==0.0.0) (1.2.3)
Requirement already satisfied: six in c:\anaconda2\lib\site-packages (from gpkit->SPaircraft==0.0.0) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\anaconda2\lib\site-packages (from pint->turbofan->SPaircraft==0.0.0) (1.0.2)
Requirement already satisfied: mkl in c:\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 c:\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=a923095ef31ce8768ad0ab1d3864094f6a20864e5a22cceacdc0f30e628fbf7b
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-5by3hm\wheels\45\69\9f\3313207e241f667aa2b0d16b020d2b192066103a9d92062e07
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. *
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.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 867
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3450              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 : 1.48e+004         after factor           : 1.48e+005       
Factor     - dense dim.             : 0                 flops                  : 2.91e+007       
Factor     - GP saved nzs           : 3.33e+004         GP saved flops         : 9.12e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.229654184e+005 2.000000000e+000  1.0e+000 0.06  
1   1.6e+003 2.1e+003 8.5e+004 -9.71e-001 -1.220933662e+005 2.766906366e+000  6.9e-001 0.14  
2   8.2e+002 1.1e+003 4.5e+004 -9.57e-001 -1.196380037e+005 5.080922819e+000  3.6e-001 0.22  
3   2.9e+002 3.9e+002 1.6e+004 -9.16e-001 -1.109422977e+005 2.155821611e+001  1.3e-001 0.28  
4   2.9e+002 3.9e+002 1.6e+004 -7.70e-001 -1.089937613e+005 1.716633346e+003  1.3e-001 0.36  
5   1.1e+002 1.5e+002 6.0e+003 -7.61e-001 -8.527950662e+004 6.684630604e+003  4.9e-002 0.44  
6   3.8e+001 5.0e+001 2.0e+003 -4.15e-001 -4.589714486e+004 1.066199112e+004  1.7e-002 0.50  
7   2.0e+001 2.7e+001 1.1e+003 2.50e-001  -2.882346884e+004 7.006668007e+003  9.0e-003 0.58  
8   9.3e+000 1.2e+001 5.0e+002 5.67e-001  -1.399096273e+004 4.222492405e+003  4.1e-003 0.66  
9   4.8e+000 6.5e+000 2.6e+002 8.28e-001  -7.185408994e+003 2.539014185e+003  2.1e-003 0.72  
10  1.4e+000 1.9e+000 7.7e+001 9.31e-001  -2.008421594e+003 9.396575617e+002  6.4e-004 0.80  
11  6.5e-001 8.7e-001 3.6e+001 9.94e-001  -6.991135083e+002 6.660256052e+002  3.0e-004 0.86  
12  4.8e-001 6.5e-001 2.6e+001 9.96e-001  -4.541860724e+002 5.573962991e+002  2.2e-004 0.94  
13  3.5e-001 7.3e-001 1.9e+001 9.80e-001  -2.731372315e+002 4.753804548e+002  1.6e-004 1.02  
14  1.7e-001 3.7e-001 9.5e+000 9.96e-001  -3.782945803e+000 3.644269123e+002  8.0e-005 1.08  
15  5.6e-002 1.5e-001 3.2e+000 9.94e-001  1.674125439e+002  2.896430807e+002  2.7e-005 1.16  
16  3.3e-002 1.3e-001 1.9e+000 1.00e+000  2.025109590e+002  2.744449201e+002  1.6e-005 1.22  
17  5.2e-003 1.8e-001 3.2e-001 1.00e+000  2.448703769e+002  2.572667007e+002  2.9e-006 1.30  
18  1.5e-003 1.3e-001 9.5e-002 1.00e+000  2.510577709e+002  2.546974711e+002  8.5e-007 1.38  
19  4.9e-004 1.1e-001 3.1e-002 1.00e+000  2.528188946e+002  2.540251949e+002  2.9e-007 1.44  
20  2.2e-004 8.7e-002 1.4e-002 1.00e+000  2.533042080e+002  2.538367251e+002  1.3e-007 1.52  
21  1.9e-004 7.9e-002 1.2e-002 1.00e+000  2.533437043e+002  2.538229805e+002  1.1e-007 1.59  
22  1.7e-004 7.2e-002 1.1e-002 1.00e+000  2.533781329e+002  2.538094556e+002  1.0e-007 1.67  
23  1.6e-004 6.5e-002 1.0e-002 1.00e+000  2.534091579e+002  2.537973313e+002  9.2e-008 1.75  
24  1.4e-004 6.0e-002 9.1e-003 1.00e+000  2.534370547e+002  2.537863963e+002  8.3e-008 1.81  
25  1.3e-004 5.4e-002 8.2e-003 1.00e+000  2.534621433e+002  2.537765388e+002  7.5e-008 1.88  
26  1.1e-004 5.0e-002 7.4e-003 1.00e+000  2.534847060e+002  2.537676519e+002  6.7e-008 1.95  
27  1.0e-004 4.5e-002 6.6e-003 1.00e+000  2.535049991e+002  2.537596422e+002  6.1e-008 2.03  
28  9.3e-005 4.2e-002 6.0e-003 1.00e+000  2.535232519e+002  2.537524240e+002  5.4e-008 2.09  
29  8.4e-005 3.8e-002 5.4e-003 1.00e+000  2.535396705e+002  2.537459199e+002  4.9e-008 2.17  
30  7.5e-005 3.5e-002 4.8e-003 1.00e+000  2.535544399e+002  2.537400599e+002  4.4e-008 2.25  
31  6.8e-005 3.2e-002 4.4e-003 1.00e+000  2.535677261e+002  2.537347806e+002  4.0e-008 2.31  
32  6.1e-005 3.0e-002 3.9e-003 1.00e+000  2.535796786e+002  2.537300247e+002  3.6e-008 2.39  
33  5.5e-005 2.8e-002 3.5e-003 1.00e+000  2.535904314e+002  2.537257407e+002  3.2e-008 2.47  
34  4.9e-005 2.6e-002 3.2e-003 1.00e+000  2.536001053e+002  2.537218818e+002  2.9e-008 2.53  
35  4.4e-005 2.4e-002 2.9e-003 1.00e+000  2.536088086e+002  2.537184061e+002  2.6e-008 2.61  
36  4.0e-005 2.2e-002 2.6e-003 1.00e+000  2.536166390e+002  2.537152756e+002  2.3e-008 2.67  
37  3.6e-005 2.1e-002 2.3e-003 1.00e+000  2.536236840e+002  2.537124562e+002  2.1e-008 2.75  
38  3.2e-005 1.9e-002 2.1e-003 1.00e+000  2.536300227e+002  2.537099169e+002  1.9e-008 2.83  
39  2.9e-005 1.8e-002 1.9e-003 1.00e+000  2.536357258e+002  2.537076301e+002  1.7e-008 2.89  
40  2.6e-005 1.7e-002 1.7e-003 1.00e+000  2.536408572e+002  2.537055708e+002  1.5e-008 2.97  
41  2.4e-005 1.6e-002 1.5e-003 1.00e+000  2.536454744e+002  2.537037163e+002  1.4e-008 3.03  
42  2.1e-005 1.5e-002 1.4e-003 1.00e+000  2.536496289e+002  2.537020464e+002  1.2e-008 3.09  
43  1.9e-005 1.5e-002 1.2e-003 1.00e+000  2.536533671e+002  2.537005428e+002  1.1e-008 3.14  
44  1.7e-005 1.4e-002 1.1e-003 1.00e+000  2.536567309e+002  2.536991889e+002  1.0e-008 3.17  
45  1.5e-005 1.3e-002 1.0e-003 1.00e+000  2.536597578e+002  2.536979699e+002  9.1e-009 3.22  
46  1.4e-005 1.3e-002 9.0e-004 1.00e+000  2.536624815e+002  2.536968724e+002  8.2e-009 3.25  
47  1.3e-005 1.2e-002 8.1e-004 1.00e+000  2.536649325e+002  2.536958843e+002  7.4e-009 3.28  
48  1.1e-005 1.2e-002 7.3e-004 1.00e+000  2.536671381e+002  2.536949948e+002  6.6e-009 3.31  
49  1.0e-005 1.1e-002 6.5e-004 1.00e+000  2.536691229e+002  2.536941939e+002  6.0e-009 3.36  
50  9.1e-006 1.1e-002 5.9e-004 1.00e+000  2.536709091e+002  2.536934730e+002  5.4e-009 3.39  
51  8.2e-006 1.1e-002 5.3e-004 1.00e+000  2.536725165e+002  2.536928240e+002  4.8e-009 3.42  
52  7.4e-006 1.0e-002 4.8e-004 1.00e+000  2.536739630e+002  2.536922398e+002  4.3e-009 3.47  
53  6.7e-006 1.0e-002 4.3e-004 1.00e+000  2.536752647e+002  2.536917139e+002  3.9e-009 3.50  
54  6.0e-006 9.8e-003 3.9e-004 1.00e+000  2.536764362e+002  2.536912405e+002  3.5e-009 3.53  
55  5.4e-006 9.6e-003 3.5e-004 1.00e+000  2.536774905e+002  2.536908144e+002  3.2e-009 3.56  
56  4.9e-006 9.4e-003 3.1e-004 1.00e+000  2.536784393e+002  2.536904308e+002  2.9e-009 3.61  
57  4.4e-006 9.2e-003 2.8e-004 1.00e+000  2.536792931e+002  2.536900855e+002  2.6e-009 3.69  
58  3.9e-006 9.0e-003 2.5e-004 1.00e+000  2.536800615e+002  2.536897747e+002  2.3e-009 3.77  
59  3.5e-006 8.9e-003 2.3e-004 1.00e+000  2.536807530e+002  2.536894949e+002  2.1e-009 3.83  
60  3.2e-006 8.7e-003 2.1e-004 1.00e+000  2.536813753e+002  2.536892431e+002  1.9e-009 3.89  
61  1.2e-006 3.4e-003 8.0e-005 1.00e+000  2.536847926e+002  2.536878589e+002  7.3e-010 3.95  
62  1.1e-006 3.1e-003 7.2e-005 1.00e+000  2.536850113e+002  2.536877710e+002  6.6e-010 4.02  
63  4.0e-007 1.1e-003 2.6e-005 1.00e+000  2.536862696e+002  2.536872610e+002  2.4e-010 4.09  
64  3.6e-007 9.9e-004 2.3e-005 1.00e+000  2.536863402e+002  2.536872324e+002  2.1e-010 4.16  
65  3.2e-007 8.9e-004 2.1e-005 1.00e+000  2.536864036e+002  2.536872067e+002  1.9e-010 4.24  
66  2.9e-007 8.0e-004 1.9e-005 1.00e+000  2.536864607e+002  2.536871835e+002  1.7e-010 4.30  
67  2.6e-007 7.2e-004 1.7e-005 1.00e+000  2.536865121e+002  2.536871626e+002  1.5e-010 4.36  
68  2.4e-007 6.5e-004 1.5e-005 1.00e+000  2.536865584e+002  2.536871438e+002  1.4e-010 4.44  
69  2.1e-007 5.8e-004 1.4e-005 1.00e+000  2.536866000e+002  2.536871269e+002  1.3e-010 4.52  
70  1.9e-007 5.2e-004 1.2e-005 1.00e+000  2.536866375e+002  2.536871117e+002  1.1e-010 4.59  
71  1.7e-007 4.7e-004 1.1e-005 1.00e+000  2.536866712e+002  2.536870980e+002  1.0e-010 4.66  
72  1.6e-007 4.2e-004 1.0e-005 1.00e+000  2.536867016e+002  2.536870857e+002  9.1e-011 4.74  
73  1.4e-007 3.8e-004 9.0e-006 1.00e+000  2.536867289e+002  2.536870746e+002  8.2e-011 4.80  
74  1.3e-007 3.4e-004 8.1e-006 1.00e+000  2.536867535e+002  2.536870646e+002  7.4e-011 4.88  
75  1.1e-007 3.1e-004 7.3e-006 1.00e+000  2.536867756e+002  2.536870556e+002  6.7e-011 4.95  
76  1.0e-007 2.8e-004 6.6e-006 1.00e+000  2.536867955e+002  2.536870475e+002  6.0e-011 5.02  
77  9.2e-008 2.5e-004 5.9e-006 1.00e+000  2.536868134e+002  2.536870403e+002  5.4e-011 5.08  
78  8.3e-008 2.3e-004 5.3e-006 1.00e+000  2.536868296e+002  2.536870337e+002  4.9e-011 5.16  
79  7.4e-008 2.0e-004 4.8e-006 1.00e+000  2.536868441e+002  2.536870278e+002  4.4e-011 5.22  
80  6.7e-008 1.8e-004 4.3e-006 1.00e+000  2.536868571e+002  2.536870225e+002  3.9e-011 5.30  
81  6.0e-008 1.6e-004 3.9e-006 1.00e+000  2.536868689e+002  2.536870177e+002  3.5e-011 5.36  
82  5.4e-008 1.5e-004 3.5e-006 1.00e+000  2.536868795e+002  2.536870134e+002  3.2e-011 5.42  
83  4.9e-008 1.3e-004 3.1e-006 1.00e+000  2.536868890e+002  2.536870095e+002  2.9e-011 5.50  
84  4.4e-008 1.2e-004 2.8e-006 1.00e+000  2.536868976e+002  2.536870060e+002  2.6e-011 5.56  
85  4.0e-008 1.1e-004 2.5e-006 1.00e+000  2.536869053e+002  2.536870029e+002  2.3e-011 5.64  
86  3.6e-008 9.7e-005 2.3e-006 1.00e+000  2.536869122e+002  2.536870001e+002  2.1e-011 5.70  
87  3.2e-008 8.7e-005 2.1e-006 1.00e+000  2.536869185e+002  2.536869975e+002  1.9e-011 5.77  
88  2.9e-008 7.9e-005 1.9e-006 1.00e+000  2.536869241e+002  2.536869953e+002  1.7e-011 5.84  
89  2.6e-008 7.1e-005 1.7e-006 1.00e+000  2.536869291e+002  2.536869932e+002  1.5e-011 5.91  
90  2.3e-008 6.4e-005 1.5e-006 1.00e+000  2.536869337e+002  2.536869913e+002  1.4e-011 5.99  
91  2.1e-008 5.7e-005 1.4e-006 1.00e+000  2.536869378e+002  2.536869897e+002  1.2e-011 6.06  
92  1.9e-008 5.2e-005 1.2e-006 9.99e-001  2.536869415e+002  2.536869882e+002  1.1e-011 6.11  
93  1.7e-008 4.6e-005 1.1e-006 1.00e+000  2.536869448e+002  2.536869868e+002  1.0e-011 6.19  
94  1.5e-008 4.2e-005 9.9e-007 1.00e+000  2.536869478e+002  2.536869856e+002  9.0e-012 6.25  
95  1.4e-008 3.8e-005 8.9e-007 1.00e+000  2.536869505e+002  2.536869845e+002  8.1e-012 6.33  
96  1.2e-008 3.4e-005 8.0e-007 1.00e+000  2.536869529e+002  2.536869835e+002  7.3e-012 6.39  
97  1.1e-008 3.1e-005 7.2e-007 1.00e+000  2.536869551e+002  2.536869826e+002  6.6e-012 6.47  
Interior-point optimizer terminated. Time: 6.47. 

Optimizer terminated. Time: 6.51    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 2.5368695506e+002   nrm: 4e+001   Viol.  con: 2e-007   var: 0e+000 
  Dual.    obj: 2.5368698263e+002   nrm: 8e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 6.54 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (313) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 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.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.02    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 868
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3452              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 : 1.48e+004         after factor           : 1.48e+005       
Factor     - dense dim.             : 0                 flops                  : 2.93e+007       
Factor     - GP saved nzs           : 3.33e+004         GP saved flops         : 9.12e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.226217652e+005 2.000000000e+000  1.0e+000 0.05  
1   1.6e+003 2.1e+003 8.5e+004 -9.71e-001 -1.217757507e+005 2.751265607e+000  7.0e-001 0.13  
2   7.9e+002 1.1e+003 4.2e+004 -9.57e-001 -1.190373986e+005 5.330342286e+000  3.5e-001 0.19  
3   2.9e+002 3.9e+002 1.6e+004 -9.12e-001 -1.106678927e+005 2.214320615e+001  1.3e-001 0.25  
4   2.9e+002 3.9e+002 1.6e+004 -7.70e-001 -1.087706970e+005 1.671231613e+003  1.3e-001 0.33  
5   1.2e+002 1.7e+002 6.7e+003 -7.62e-001 -8.832741583e+004 6.011828880e+003  5.5e-002 0.41  
6   3.9e+001 5.2e+001 2.1e+003 -4.65e-001 -4.678232398e+004 1.101923718e+004  1.7e-002 0.47  
7   2.3e+001 3.1e+001 1.2e+003 2.31e-001  -3.153548321e+004 7.305431055e+003  1.0e-002 0.55  
8   9.1e+000 1.2e+001 4.9e+002 5.19e-001  -1.376407587e+004 3.968205216e+003  4.0e-003 0.63  
9   6.0e+000 8.1e+000 3.2e+002 8.31e-001  -9.139381105e+003 2.854016049e+003  2.7e-003 0.70  
10  2.1e+000 2.8e+000 1.1e+002 9.02e-001  -3.117012748e+003 1.205575374e+003  9.4e-004 0.77  
11  1.5e+000 2.0e+000 8.0e+001 9.76e-001  -2.106512099e+003 9.650781377e+002  6.6e-004 0.83  
12  8.1e-001 1.2e+000 4.4e+001 9.80e-001  -1.065816719e+003 6.236278493e+002  3.6e-004 0.86  
13  4.1e-001 7.3e-001 2.3e+001 9.88e-001  -4.563391396e+002 4.140752374e+002  1.9e-004 0.89  
14  1.9e-001 3.4e-001 1.0e+001 1.00e+000  -1.142020924e+002 2.896385168e+002  8.8e-005 0.92  
15  6.6e-002 1.5e-001 3.7e+000 1.00e+000  7.172342818e+001  2.137404199e+002  3.1e-005 0.97  
16  2.9e-002 1.2e-001 1.6e+000 1.01e+000  1.271309373e+002  1.901599088e+002  1.4e-005 1.00  
17  9.1e-003 1.1e-001 5.3e-001 1.01e+000  1.579841895e+002  1.781403643e+002  4.6e-006 1.03  
18  3.8e-003 9.0e-002 2.2e-001 1.01e+000  1.663150639e+002  1.748018185e+002  1.9e-006 1.08  
19  9.3e-004 1.3e-001 5.7e-002 1.01e+000  1.708421518e+002  1.729992040e+002  5.1e-007 1.11  
20  3.5e-004 9.8e-002 2.2e-002 1.00e+000  1.718083243e+002  1.726401689e+002  2.0e-007 1.17  
21  1.3e-004 1.0e-001 8.2e-003 1.00e+000  1.721836709e+002  1.724949683e+002  7.4e-008 1.25  
22  4.7e-005 9.5e-002 2.9e-003 1.00e+000  1.723246460e+002  1.724365755e+002  2.7e-008 1.31  
23  4.2e-005 8.7e-002 2.7e-003 1.00e+000  1.723332429e+002  1.724339881e+002  2.4e-008 1.38  
24  3.8e-005 8.0e-002 2.4e-003 1.00e+000  1.723404330e+002  1.724311003e+002  2.2e-008 1.44  
25  3.4e-005 7.2e-002 2.2e-003 1.00e+000  1.723468780e+002  1.724284758e+002  1.9e-008 1.50  
26  3.1e-005 6.6e-002 1.9e-003 1.00e+000  1.723526637e+002  1.724260989e+002  1.8e-008 1.56  
27  2.8e-005 6.0e-002 1.7e-003 1.00e+000  1.723578623e+002  1.724239514e+002  1.6e-008 1.64  
28  2.5e-005 5.5e-002 1.6e-003 1.00e+000  1.723625351e+002  1.724220129e+002  1.4e-008 1.70  
29  2.3e-005 5.0e-002 1.4e-003 1.00e+000  1.723667360e+002  1.724202641e+002  1.3e-008 1.77  
30  2.0e-005 4.6e-002 1.3e-003 1.00e+000  1.723705133e+002  1.724186869e+002  1.2e-008 1.83  
31  1.8e-005 4.2e-002 1.1e-003 1.00e+000  1.723739097e+002  1.724172646e+002  1.0e-008 1.89  
32  1.6e-005 3.9e-002 1.0e-003 1.00e+000  1.723769640e+002  1.724159823e+002  9.3e-009 1.95  
33  1.5e-005 3.6e-002 9.3e-004 1.00e+000  1.723797108e+002  1.724148263e+002  8.4e-009 2.02  
34  1.3e-005 3.3e-002 8.3e-004 1.00e+000  1.723821812e+002  1.724137843e+002  7.6e-009 2.08  
35  1.2e-005 3.0e-002 7.5e-004 1.00e+000  1.723844031e+002  1.724128453e+002  6.8e-009 2.14  
36  1.1e-005 2.8e-002 6.8e-004 1.00e+000  1.723864015e+002  1.724119990e+002  6.1e-009 2.20  
37  9.7e-006 2.6e-002 6.1e-004 1.00e+000  1.723881991e+002  1.724112364e+002  5.5e-009 2.27  
38  8.7e-006 2.4e-002 5.5e-004 1.00e+000  1.723898160e+002  1.724105492e+002  5.0e-009 2.33  
39  7.9e-006 2.3e-002 4.9e-004 1.00e+000  1.723912705e+002  1.724099302e+002  4.5e-009 2.39  
40  7.1e-006 2.1e-002 4.4e-004 1.00e+000  1.723925790e+002  1.724093724e+002  4.0e-009 2.45  
41  6.4e-006 2.0e-002 4.0e-004 1.00e+000  1.723937561e+002  1.724088700e+002  3.6e-009 2.52  
42  5.7e-006 1.9e-002 3.6e-004 1.00e+000  1.723948150e+002  1.724084175e+002  3.3e-009 2.58  
43  5.2e-006 1.7e-002 3.2e-004 1.00e+000  1.723957677e+002  1.724080098e+002  2.9e-009 2.64  
44  4.6e-006 1.6e-002 2.9e-004 1.00e+000  1.723966249e+002  1.724076427e+002  2.6e-009 2.70  
45  4.2e-006 1.6e-002 2.6e-004 1.00e+000  1.723973960e+002  1.724073120e+002  2.4e-009 2.77  
46  3.8e-006 1.5e-002 2.4e-004 1.00e+000  1.723980899e+002  1.724070142e+002  2.1e-009 2.84  
47  3.4e-006 1.4e-002 2.1e-004 1.00e+000  1.723987142e+002  1.724067460e+002  1.9e-009 2.89  
48  3.0e-006 1.3e-002 1.9e-004 1.00e+000  1.723992759e+002  1.724065045e+002  1.7e-009 2.95  
49  2.7e-006 1.3e-002 1.7e-004 1.00e+000  1.723997813e+002  1.724062871e+002  1.6e-009 3.03  
50  2.5e-006 1.2e-002 1.5e-004 1.00e+000  1.724002361e+002  1.724060913e+002  1.4e-009 3.09  
51  2.2e-006 1.2e-002 1.4e-004 1.00e+000  1.724006453e+002  1.724059149e+002  1.3e-009 3.17  
52  2.0e-006 1.1e-002 1.3e-004 1.00e+000  1.724010135e+002  1.724057562e+002  1.1e-009 3.23  
53  1.8e-006 1.1e-002 1.1e-004 1.00e+000  1.724013448e+002  1.724056132e+002  1.0e-009 3.30  
54  1.6e-006 1.1e-002 1.0e-004 1.00e+000  1.724016429e+002  1.724054845e+002  9.2e-010 3.36  
55  1.5e-006 1.0e-002 9.1e-005 1.00e+000  1.724019112e+002  1.724053686e+002  8.3e-010 3.42  
56  1.3e-006 1.0e-002 8.2e-005 1.00e+000  1.724021526e+002  1.724052643e+002  7.4e-010 3.48  
57  1.2e-006 9.9e-003 7.4e-005 1.00e+000  1.724023698e+002  1.724051704e+002  6.7e-010 3.55  
58  1.1e-006 9.7e-003 6.7e-005 1.00e+000  1.724025653e+002  1.724050858e+002  6.0e-010 3.61  
59  9.5e-007 9.5e-003 6.0e-005 1.00e+000  1.724027412e+002  1.724050096e+002  5.4e-010 3.67  
60  8.6e-007 9.3e-003 5.4e-005 1.00e+000  1.724028995e+002  1.724049411e+002  4.9e-010 3.73  
61  7.7e-007 9.1e-003 4.8e-005 1.00e+000  1.724030419e+002  1.724048794e+002  4.4e-010 3.80  
62  7.0e-007 9.0e-003 4.4e-005 1.00e+000  1.724031701e+002  1.724048238e+002  4.0e-010 3.86  
63  6.3e-007 8.8e-003 3.9e-005 1.00e+000  1.724032854e+002  1.724047738e+002  3.6e-010 3.94  
64  5.6e-007 8.7e-003 3.5e-005 1.00e+000  1.724033892e+002  1.724047287e+002  3.2e-010 3.98  
65  5.1e-007 8.6e-003 3.2e-005 1.00e+000  1.724034826e+002  1.724046882e+002  2.9e-010 4.05  
66  4.6e-007 8.5e-003 2.9e-005 1.00e+000  1.724035666e+002  1.724046517e+002  2.6e-010 4.11  
67  4.1e-007 8.4e-003 2.6e-005 1.00e+000  1.724036423e+002  1.724046188e+002  2.3e-010 4.19  
68  3.7e-007 8.3e-003 2.3e-005 1.00e+000  1.724037103e+002  1.724045892e+002  2.1e-010 4.25  
69  3.3e-007 8.2e-003 2.1e-005 1.00e+000  1.724037716e+002  1.724045626e+002  1.9e-010 4.31  
70  3.0e-007 8.1e-003 1.9e-005 1.00e+000  1.724038267e+002  1.724045386e+002  1.7e-010 4.38  
71  2.7e-007 8.1e-003 1.7e-005 1.00e+000  1.724038763e+002  1.724045170e+002  1.5e-010 4.44  
72  2.4e-007 8.0e-003 1.5e-005 9.99e-001  1.724039209e+002  1.724044976e+002  1.4e-010 4.50  
73  2.2e-007 8.0e-003 1.4e-005 1.00e+000  1.724039611e+002  1.724044800e+002  1.2e-010 4.56  
74  2.0e-007 7.9e-003 1.2e-005 1.00e+000  1.724039972e+002  1.724044643e+002  1.1e-010 4.63  
75  1.8e-007 7.9e-003 1.1e-005 1.00e+000  1.724040297e+002  1.724044501e+002  1.0e-010 4.69  
76  1.6e-007 7.8e-003 1.0e-005 9.98e-001  1.724040590e+002  1.724044374e+002  9.1e-011 4.75  
77  1.4e-007 7.8e-003 9.0e-006 1.00e+000  1.724040853e+002  1.724044259e+002  8.1e-011 4.81  
78  1.3e-007 7.7e-003 8.1e-006 1.00e+000  1.724041090e+002  1.724044155e+002  7.3e-011 4.88  
79  1.2e-007 7.7e-003 7.3e-006 1.00e+000  1.724041305e+002  1.724044061e+002  6.6e-011 4.94  
80  1.0e-007 7.7e-003 6.6e-006 9.99e-001  1.724041497e+002  1.724043978e+002  5.9e-011 5.00  
81  9.4e-008 7.7e-003 5.9e-006 9.93e-001  1.724041670e+002  1.724043902e+002  5.3e-011 5.06  
82  8.5e-008 7.6e-003 5.3e-006 1.00e+000  1.724041825e+002  1.724043834e+002  4.8e-011 5.13  
83  7.6e-008 6.9e-003 4.8e-006 1.01e+000  1.724041971e+002  1.724043771e+002  4.4e-011 5.19  
84  6.9e-008 6.2e-003 4.3e-006 1.02e+000  1.724042104e+002  1.724043712e+002  3.9e-011 5.25  
85  6.2e-008 5.6e-003 3.9e-006 9.95e-001  1.724042216e+002  1.724043663e+002  3.6e-011 5.33  
86  5.6e-008 5.0e-003 3.5e-006 9.89e-001  1.724042316e+002  1.724043619e+002  3.2e-011 5.39  
87  5.0e-008 4.5e-003 3.1e-006 9.75e-001  1.724042406e+002  1.724043581e+002  2.9e-011 5.45  
88  4.5e-008 4.1e-003 2.8e-006 9.71e-001  1.724042488e+002  1.724043545e+002  2.6e-011 5.52  
89  4.2e-008 3.7e-003 2.5e-006 9.86e-001  1.724042561e+002  1.724043514e+002  2.3e-011 5.58  
90  3.8e-008 3.3e-003 2.3e-006 9.99e-001  1.724042627e+002  1.724043485e+002  2.1e-011 5.64  
91  3.3e-008 3.0e-003 2.1e-006 1.01e+000  1.724042690e+002  1.724043455e+002  1.9e-011 5.70  
92  3.0e-008 2.7e-003 1.9e-006 9.88e-001  1.724042743e+002  1.724043433e+002  1.7e-011 5.77  
93  2.9e-008 2.4e-003 1.7e-006 9.65e-001  1.724042790e+002  1.724043413e+002  1.5e-011 5.83  
94  2.6e-008 2.2e-003 1.5e-006 9.80e-001  1.724042833e+002  1.724043394e+002  1.4e-011 5.89  
95  2.5e-008 1.9e-003 1.3e-006 1.03e+000  1.724042878e+002  1.724043369e+002  1.3e-011 5.95  
96  6.2e-008 5.0e-004 3.5e-007 7.89e-001  1.724043125e+002  1.724043244e+002  2.6e-012 6.02  
97  1.2e-007 4.8e-004 3.4e-007 8.84e-001  1.724043143e+002  1.724043227e+002  2.1e-012 6.08  
98  1.2e-007 4.8e-004 3.4e-007 1.00e+000  1.724043143e+002  1.724043227e+002  2.1e-012 6.13  
Interior-point optimizer terminated. Time: 6.14. 

Optimizer terminated. Time: 6.16    
solsta = 8, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : NEAR_OPTIMAL
  Primal.  obj: 1.7240431433e+002   nrm: 4e+001   Viol.  con: 2e-006   var: 0e+000 
  Dual.    obj: 1.7240432272e+002   nrm: 8e+002   Viol.  con: 0e+000   var: 2e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 6.18 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.02            
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            : 868
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3452              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 : 1.48e+004         after factor           : 1.48e+005       
Factor     - dense dim.             : 0                 flops                  : 2.93e+007       
Factor     - GP saved nzs           : 3.33e+004         GP saved flops         : 9.12e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.227329895e+005 2.000000000e+000  1.0e+000 0.05  
1   1.6e+003 2.2e+003 8.8e+004 -9.71e-001 -1.219819119e+005 2.645989959e+000  7.2e-001 0.09  
2   8.4e+002 1.1e+003 4.5e+004 -9.59e-001 -1.195380051e+005 4.830716767e+000  3.7e-001 0.13  
3   2.9e+002 3.9e+002 1.6e+004 -9.18e-001 -1.108216106e+005 2.032677367e+001  1.3e-001 0.17  
4   2.9e+002 3.9e+002 1.6e+004 -7.72e-001 -1.087186359e+005 1.854008088e+003  1.3e-001 0.20  
5   1.2e+002 1.7e+002 6.6e+003 -7.63e-001 -8.830307750e+004 6.076042731e+003  5.5e-002 0.23  
6   4.4e+001 5.8e+001 2.3e+003 -4.63e-001 -5.106761750e+004 1.035475360e+004  1.9e-002 0.27  
7   2.6e+001 3.5e+001 1.4e+003 1.62e-001  -3.516517247e+004 7.223163731e+003  1.1e-002 0.30  
8   1.3e+001 1.7e+001 6.8e+002 4.63e-001  -1.916964299e+004 4.619901604e+003  5.6e-003 0.33  
9   4.5e+000 6.0e+000 2.4e+002 7.42e-001  -6.813662207e+003 2.197894711e+003  2.0e-003 0.36  
10  3.3e+000 4.4e+000 1.8e+002 9.39e-001  -4.971325611e+003 1.758353481e+003  1.5e-003 0.39  
11  1.1e+000 1.5e+000 5.9e+001 9.61e-001  -1.543336712e+003 7.017437610e+002  4.9e-004 0.41  
12  8.7e-001 1.2e+000 4.8e+001 9.87e-001  -1.202281488e+003 6.244021558e+002  3.9e-004 0.44  
13  7.1e-001 1.0e+000 3.8e+001 9.68e-001  -9.556455581e+002 5.353933935e+002  3.2e-004 0.47  
14  3.7e-001 5.3e-001 2.0e+001 9.89e-001  -3.943857439e+002 3.866075045e+002  1.7e-004 0.50  
15  1.9e-001 2.8e-001 1.1e+001 9.96e-001  -1.394107308e+002 2.700325408e+002  8.8e-005 0.53  
16  8.6e-002 1.6e-001 4.8e+000 1.00e+000  1.968886509e+001  2.042784657e+002  4.0e-005 0.56  
17  7.8e-002 1.5e-001 4.3e+000 1.01e+000  4.067907588e+001  2.075436655e+002  3.6e-005 0.61  
18  3.1e-002 8.8e-002 1.8e+000 1.01e+000  1.154426718e+002  1.828320860e+002  1.5e-005 0.64  
19  1.4e-002 1.2e-001 7.9e-001 1.01e+000  1.448195123e+002  1.747380168e+002  6.6e-006 0.67  
20  6.7e-003 4.3e-001 3.8e-001 1.01e+000  1.559754187e+002  1.703750810e+002  3.2e-006 0.72  
21  2.2e-003 1.7e-001 1.3e-001 1.01e+000  1.635069791e+002  1.683733445e+002  1.1e-006 0.73  
22  1.7e-003 1.3e-001 1.0e-001 1.01e+000  1.643650640e+002  1.681283556e+002  8.5e-007 0.77  
23  7.3e-004 9.2e-002 4.3e-002 1.01e+000  1.659482019e+002  1.675662657e+002  3.7e-007 0.80  
24  4.3e-004 7.4e-002 2.5e-002 1.01e+000  1.664272587e+002  1.673731817e+002  2.2e-007 0.83  
25  3.8e-004 6.8e-002 2.3e-002 1.01e+000  1.665000264e+002  1.673517058e+002  2.0e-007 0.88  
26  3.4e-004 6.2e-002 2.1e-002 1.01e+000  1.665608964e+002  1.673271533e+002  1.8e-007 0.92  
27  3.1e-004 5.6e-002 1.9e-002 1.01e+000  1.666159758e+002  1.673054169e+002  1.6e-007 0.97  
28  2.8e-004 5.2e-002 1.7e-002 1.01e+000  1.666653053e+002  1.672856453e+002  1.4e-007 1.00  
29  2.5e-004 4.7e-002 1.5e-002 1.01e+000  1.667095743e+002  1.672677531e+002  1.3e-007 1.03  
30  2.3e-004 4.3e-002 1.3e-002 1.01e+000  1.667492633e+002  1.672515211e+002  1.2e-007 1.08  
31  2.0e-004 4.0e-002 1.2e-002 1.01e+000  1.667848468e+002  1.672367960e+002  1.0e-007 1.11  
32  1.8e-004 3.6e-002 1.1e-002 1.01e+000  1.668167463e+002  1.672234330e+002  9.4e-008 1.14  
33  1.7e-004 3.4e-002 9.8e-003 1.01e+000  1.668453437e+002  1.672113077e+002  8.5e-008 1.19  
34  1.5e-004 3.1e-002 8.9e-003 1.00e+000  1.668709798e+002  1.672003039e+002  7.6e-008 1.22  
35  1.3e-004 2.9e-002 8.0e-003 1.00e+000  1.668939631e+002  1.671903190e+002  6.9e-008 1.27  
36  1.2e-004 2.7e-002 7.2e-003 1.00e+000  1.669145707e+002  1.671812626e+002  6.2e-008 1.30  
37  1.1e-004 2.5e-002 6.5e-003 1.00e+000  1.669330506e+002  1.671730507e+002  5.6e-008 1.33  
38  9.7e-005 2.3e-002 5.8e-003 1.00e+000  1.669496258e+002  1.671656085e+002  5.0e-008 1.36  
39  8.8e-005 2.1e-002 5.2e-003 1.00e+000  1.669644946e+002  1.671588650e+002  4.5e-008 1.39  
40  7.9e-005 2.0e-002 4.7e-003 1.00e+000  1.669778359e+002  1.671527587e+002  4.1e-008 1.44  
41  7.1e-005 1.9e-002 4.2e-003 1.00e+000  1.669898080e+002  1.671472306e+002  3.7e-008 1.47  
42  6.4e-005 1.8e-002 3.8e-003 1.00e+000  1.670005531e+002  1.671422262e+002  3.3e-008 1.50  
43  5.8e-005 1.7e-002 3.4e-003 1.00e+000  1.670101989e+002  1.671376993e+002  3.0e-008 1.53  
44  5.2e-005 1.6e-002 3.1e-003 1.00e+000  1.670188584e+002  1.671336045e+002  2.7e-008 1.56  
45  4.7e-005 1.5e-002 2.8e-003 1.00e+000  1.670266334e+002  1.671299018e+002  2.4e-008 1.59  
46  4.2e-005 1.5e-002 2.5e-003 1.00e+000  1.670336153e+002  1.671265551e+002  2.2e-008 1.63  
47  3.8e-005 1.4e-002 2.3e-003 1.00e+000  1.670398855e+002  1.671235305e+002  1.9e-008 1.66  
48  3.4e-005 1.3e-002 2.0e-003 1.00e+000  1.670455173e+002  1.671207955e+002  1.7e-008 1.69  
49  3.1e-005 1.3e-002 1.8e-003 1.00e+000  1.670505766e+002  1.671183267e+002  1.6e-008 1.72  
50  2.8e-005 1.2e-002 1.6e-003 1.00e+000  1.670551212e+002  1.671160952e+002  1.4e-008 1.75  
51  2.5e-005 1.2e-002 1.5e-003 1.00e+000  1.670592047e+002  1.671140809e+002  1.3e-008 1.78  
52  2.2e-005 1.2e-002 1.3e-003 1.00e+000  1.670628736e+002  1.671122637e+002  1.1e-008 1.81  
53  2.0e-005 1.1e-002 1.2e-003 1.00e+000  1.670661704e+002  1.671106204e+002  1.0e-008 1.84  
54  1.8e-005 1.1e-002 1.1e-003 1.00e+000  1.670691338e+002  1.671091385e+002  9.3e-009 1.88  
55  1.6e-005 1.1e-002 9.7e-004 1.00e+000  1.670717968e+002  1.671078016e+002  8.4e-009 1.91  
56  1.5e-005 1.1e-002 8.7e-004 1.00e+000  1.670741903e+002  1.671065955e+002  7.5e-009 1.94  
57  1.3e-005 1.0e-002 7.9e-004 1.00e+000  1.670763421e+002  1.671055061e+002  6.8e-009 1.97  
58  1.2e-005 1.0e-002 7.1e-004 1.00e+000  1.670782767e+002  1.671045239e+002  6.1e-009 2.02  
59  1.1e-005 9.9e-003 6.4e-004 1.00e+000  1.670800157e+002  1.671036389e+002  5.5e-009 2.05  
60  9.6e-006 9.8e-003 5.7e-004 1.00e+000  1.670815792e+002  1.671028407e+002  4.9e-009 2.08  
61  8.6e-006 9.6e-003 5.2e-004 1.00e+000  1.670829853e+002  1.671021202e+002  4.4e-009 2.13  
62  7.8e-006 9.5e-003 4.6e-004 1.00e+000  1.670842497e+002  1.671014715e+002  4.0e-009 2.16  
63  7.0e-006 9.4e-003 4.2e-004 1.00e+000  1.670853867e+002  1.671008865e+002  3.6e-009 2.19  
64  6.3e-006 9.3e-003 3.8e-004 1.00e+000  1.670864093e+002  1.671003595e+002  3.2e-009 2.22  
65  5.7e-006 9.2e-003 3.4e-004 1.00e+000  1.670873290e+002  1.670998846e+002  2.9e-009 2.25  
66  2.2e-006 3.5e-003 1.3e-004 1.00e+000  1.670924289e+002  1.670972160e+002  1.1e-009 2.30  
67  8.7e-007 1.4e-003 5.2e-005 1.00e+000  1.670943032e+002  1.670962336e+002  4.5e-010 2.33  
68  7.8e-007 1.3e-003 4.7e-005 1.01e+000  1.670944364e+002  1.670961694e+002  4.0e-010 2.36  
69  7.0e-007 1.1e-003 4.2e-005 9.83e-001  1.670945494e+002  1.670961106e+002  3.6e-010 2.39  
70  6.3e-007 1.0e-003 3.8e-005 1.01e+000  1.670946538e+002  1.670960550e+002  3.3e-010 2.42  
71  5.7e-007 9.2e-004 3.4e-005 9.95e-001  1.670947456e+002  1.670960068e+002  3.0e-010 2.47  
72  5.1e-007 8.3e-004 3.1e-005 9.94e-001  1.670948281e+002  1.670959633e+002  2.7e-010 2.50  
73  4.6e-007 7.5e-004 2.8e-005 9.87e-001  1.670949021e+002  1.670959247e+002  2.4e-010 2.53  
74  4.1e-007 6.7e-004 2.5e-005 9.84e-001  1.670949687e+002  1.670958899e+002  2.2e-010 2.56  
75  3.7e-007 6.0e-004 2.2e-005 1.03e+000  1.670950364e+002  1.670958528e+002  2.0e-010 2.59  
76  3.4e-007 5.4e-004 2.0e-005 1.00e+000  1.670950897e+002  1.670958245e+002  1.8e-010 2.64  
77  3.0e-007 4.9e-004 1.8e-005 9.98e-001  1.670951376e+002  1.670957990e+002  1.6e-010 2.67  
78  2.7e-007 4.4e-004 1.6e-005 9.87e-001  1.670951807e+002  1.670957762e+002  1.4e-010 2.70  
79  2.4e-007 4.0e-004 1.5e-005 1.03e+000  1.670952241e+002  1.670957525e+002  1.3e-010 2.73  
80  2.2e-007 3.6e-004 1.3e-005 1.03e+000  1.670952624e+002  1.670957317e+002  1.2e-010 2.77  
81  2.0e-007 3.2e-004 1.2e-005 9.65e-001  1.670952929e+002  1.670957159e+002  1.1e-010 2.81  
82  1.8e-007 2.9e-004 1.1e-005 9.97e-001  1.670953204e+002  1.670957012e+002  9.6e-011 2.84  
83  1.6e-007 2.6e-004 9.7e-006 9.65e-001  1.670953451e+002  1.670956884e+002  8.7e-011 2.88  
84  1.5e-007 2.3e-004 8.7e-006 1.01e+000  1.670953684e+002  1.670956758e+002  7.8e-011 2.92  
85  1.3e-007 2.1e-004 7.8e-006 9.49e-001  1.670953882e+002  1.670956660e+002  7.1e-011 2.95  
86  1.2e-007 1.9e-004 7.0e-006 1.05e+000  1.670954104e+002  1.670956537e+002  6.5e-011 2.98  
87  1.1e-007 1.7e-004 6.3e-006 1.04e+000  1.670954293e+002  1.670956433e+002  6.0e-011 3.02  
88  1.0e-007 1.5e-004 5.7e-006 1.00e+000  1.670954432e+002  1.670956360e+002  5.4e-011 3.05  
89  9.0e-008 1.4e-004 5.1e-006 1.01e+000  1.670954563e+002  1.670956289e+002  4.9e-011 3.08  
90  8.0e-008 1.2e-004 4.6e-006 1.00e+000  1.670954676e+002  1.670956228e+002  4.4e-011 3.11  
91  7.1e-008 1.1e-004 4.2e-006 9.30e-001  1.670954776e+002  1.670956177e+002  3.9e-011 3.14  
92  6.3e-008 1.0e-004 3.7e-006 1.11e+000  1.670954912e+002  1.670956097e+002  3.7e-011 3.17  
93  5.6e-008 9.1e-005 3.4e-006 8.77e-001  1.670954988e+002  1.670956062e+002  3.4e-011 3.20  
94  5.1e-008 8.2e-005 3.0e-006 1.08e+000  1.670955084e+002  1.670956009e+002  3.2e-011 3.23  
95  4.5e-008 7.3e-005 2.7e-006 8.12e-001  1.670955142e+002  1.670955984e+002  2.9e-011 3.27  
96  8.9e-008 6.6e-005 2.5e-006 4.71e+000  1.670955225e+002  1.670955846e+002  2.4e-011 3.30  
97  7.9e-008 5.9e-005 2.2e-006 8.80e-001  1.670955270e+002  1.670955831e+002  2.1e-011 3.33  
98  7.5e-008 5.4e-005 2.0e-006 1.06e+000  1.670955323e+002  1.670955812e+002  2.0e-011 3.36  
99  7.9e-008 4.8e-005 1.8e-006 4.26e+000  1.670955389e+002  1.670955756e+002  1.7e-011 3.39  
100 6.9e-009 3.1e-006 1.1e-007 8.36e-001  1.670955673e+002  1.670955698e+002  2.2e-012 3.41  
Interior-point optimizer terminated. Time: 3.42. 

Optimizer terminated. Time: 3.45    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6709556727e+002   nrm: 2e+001   Viol.  con: 1e-007   var: 0e+000 
  Dual.    obj: 1.6709556981e+002   nrm: 9e+002   Viol.  con: 0e+000   var: 1e-005 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.48 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 868
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3452              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 : 1.48e+004         after factor           : 1.48e+005       
Factor     - dense dim.             : 0                 flops                  : 2.93e+007       
Factor     - GP saved nzs           : 3.33e+004         GP saved flops         : 9.12e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.226585484e+005 2.000000000e+000  1.0e+000 0.11  
1   1.7e+003 2.2e+003 8.9e+004 -9.71e-001 -1.219213872e+005 2.627749503e+000  7.2e-001 0.16  
2   8.7e+002 1.2e+003 4.7e+004 -9.59e-001 -1.196031120e+005 4.663152486e+000  3.8e-001 0.20  
3   2.9e+002 3.9e+002 1.6e+004 -9.21e-001 -1.107419751e+005 2.010365940e+001  1.3e-001 0.25  
4   2.9e+002 3.9e+002 1.6e+004 -7.72e-001 -1.085665984e+005 1.920496928e+003  1.3e-001 0.28  
5   1.2e+002 1.6e+002 6.4e+003 -7.63e-001 -8.729056822e+004 6.296508785e+003  5.3e-002 0.31  
6   4.0e+001 5.3e+001 2.1e+003 -4.49e-001 -4.763950705e+004 1.096723291e+004  1.8e-002 0.36  
7   2.5e+001 3.3e+001 1.3e+003 2.22e-001  -3.390534681e+004 7.487004240e+003  1.1e-002 0.39  
8   1.1e+001 1.5e+001 6.2e+002 4.87e-001  -1.760735587e+004 4.162567433e+003  5.1e-003 0.42  
9   4.0e+000 5.4e+000 2.2e+002 7.72e-001  -6.168782075e+003 2.053688664e+003  1.8e-003 0.45  
10  2.3e+000 3.1e+000 1.3e+002 9.48e-001  -3.390528359e+003 1.383516342e+003  1.0e-003 0.50  
11  1.0e+000 1.4e+000 5.6e+001 9.82e-001  -1.426283489e+003 7.076364442e+002  4.7e-004 0.55  
12  7.3e-001 9.8e-001 4.0e+001 9.83e-001  -9.961487239e+002 5.528661229e+002  3.3e-004 0.58  
13  7.0e-001 9.4e-001 3.8e+001 9.85e-001  -9.428432772e+002 5.417367208e+002  3.2e-004 0.61  
14  2.9e-001 4.2e-001 1.6e+001 9.84e-001  -2.921964085e+002 3.182866208e+002  1.3e-004 0.64  
15  1.7e-001 4.5e-001 9.5e+000 1.00e+000  -1.171840615e+002 2.513365970e+002  8.0e-005 0.67  
16  9.4e-002 2.5e-001 5.2e+000 1.01e+000  4.456305583e+000  2.058390058e+002  4.4e-005 0.70  
17  9.3e-002 2.5e-001 5.2e+000 1.02e+000  7.084701634e+000  2.058662629e+002  4.3e-005 0.73  
18  7.9e-002 2.1e-001 4.4e+000 1.02e+000  3.631563300e+001  2.044345805e+002  3.7e-005 0.78  
19  3.5e-002 1.1e-001 1.9e+000 1.01e+000  1.090774056e+002  1.830681095e+002  1.6e-005 0.81  
20  9.8e-003 1.8e-001 5.5e-001 1.01e+000  1.514853168e+002  1.723683138e+002  4.6e-006 0.84  
21  3.0e-003 1.9e-001 1.7e-001 1.00e+000  1.618226288e+002  1.682862587e+002  1.4e-006 0.88  
22  1.2e-003 1.4e-001 7.2e-002 1.01e+000  1.646754526e+002  1.673847390e+002  6.1e-007 0.91  
23  7.8e-004 1.0e-001 4.6e-002 9.78e-001  1.653898994e+002  1.671256172e+002  4.0e-007 0.94  
24  2.2e-004 1.1e-001 1.4e-002 9.85e-001  1.662723997e+002  1.667920708e+002  1.2e-007 0.98  
25  7.5e-005 1.1e-001 4.7e-003 1.01e+000  1.665147647e+002  1.666907444e+002  4.1e-008 1.01  
26  3.4e-005 9.0e-002 2.1e-003 1.01e+000  1.665822613e+002  1.666617800e+002  1.9e-008 1.05  
27  3.1e-005 8.4e-002 1.9e-003 1.01e+000  1.665884808e+002  1.666605441e+002  1.7e-008 1.08  
28  2.8e-005 7.5e-002 1.7e-003 1.00e+000  1.665934634e+002  1.666582979e+002  1.5e-008 1.11  
29  2.5e-005 6.8e-002 1.6e-003 1.00e+000  1.665979388e+002  1.666562833e+002  1.4e-008 1.16  
30  2.2e-005 6.2e-002 1.4e-003 1.00e+000  1.666019612e+002  1.666544632e+002  1.2e-008 1.19  
31  2.0e-005 5.7e-002 1.3e-003 1.00e+000  1.666055744e+002  1.666528193e+002  1.1e-008 1.22  
32  1.8e-005 5.2e-002 1.1e-003 1.00e+000  1.666088210e+002  1.666513357e+002  1.0e-008 1.25  
33  1.6e-005 4.8e-002 1.0e-003 1.00e+000  1.666117386e+002  1.666499970e+002  9.1e-009 1.28  
34  1.5e-005 4.4e-002 9.3e-004 1.00e+000  1.666143608e+002  1.666487895e+002  8.2e-009 1.31  
35  1.3e-005 4.0e-002 8.3e-004 1.00e+000  1.666167177e+002  1.666477003e+002  7.4e-009 1.34  
36  1.2e-005 3.7e-002 7.5e-004 1.00e+000  1.666188362e+002  1.666467179e+002  6.6e-009 1.38  
37  1.1e-005 3.4e-002 6.8e-004 1.00e+000  1.666207406e+002  1.666458320e+002  6.0e-009 1.41  
38  9.6e-006 3.1e-002 6.1e-004 1.00e+000  1.666224526e+002  1.666450331e+002  5.4e-009 1.44  
39  8.6e-006 2.9e-002 5.5e-004 1.00e+000  1.666239918e+002  1.666443128e+002  4.8e-009 1.47  
40  7.8e-006 2.7e-002 4.9e-004 1.00e+000  1.666253756e+002  1.666436634e+002  4.4e-009 1.50  
41  7.0e-006 2.5e-002 4.4e-004 1.00e+000  1.666266198e+002  1.666430779e+002  3.9e-009 1.53  
42  6.3e-006 2.3e-002 4.0e-004 1.00e+000  1.666277386e+002  1.666425501e+002  3.5e-009 1.56  
43  5.7e-006 2.2e-002 3.6e-004 1.00e+000  1.666287446e+002  1.666420744e+002  3.2e-009 1.59  
44  5.1e-006 2.0e-002 3.2e-004 1.00e+000  1.666296492e+002  1.666416455e+002  2.9e-009 1.63  
45  4.6e-006 1.9e-002 2.9e-004 1.00e+000  1.666304626e+002  1.666412589e+002  2.6e-009 1.66  
46  4.1e-006 1.8e-002 2.6e-004 1.00e+000  1.666311941e+002  1.666409105e+002  2.3e-009 1.69  
47  3.7e-006 1.7e-002 2.4e-004 1.00e+000  1.666318519e+002  1.666405964e+002  2.1e-009 1.73  
48  3.3e-006 1.6e-002 2.1e-004 1.00e+000  1.666324433e+002  1.666403132e+002  1.9e-009 1.76  
49  3.0e-006 1.5e-002 1.9e-004 1.00e+000  1.666329752e+002  1.666400579e+002  1.7e-009 1.80  
50  2.7e-006 1.5e-002 1.7e-004 1.00e+000  1.666334534e+002  1.666398277e+002  1.5e-009 1.83  
51  2.4e-006 1.4e-002 1.5e-004 1.00e+000  1.666338835e+002  1.666396203e+002  1.4e-009 1.86  
52  2.2e-006 1.3e-002 1.4e-004 1.00e+000  1.666342703e+002  1.666394333e+002  1.2e-009 1.89  
53  2.0e-006 1.3e-002 1.3e-004 1.00e+000  1.666346182e+002  1.666392649e+002  1.1e-009 1.92  
54  1.8e-006 1.2e-002 1.1e-004 1.00e+000  1.666349312e+002  1.666391131e+002  1.0e-009 1.95  
55  1.6e-006 1.2e-002 1.0e-004 1.00e+000  1.666352126e+002  1.666389763e+002  9.0e-010 1.98  
56  1.4e-006 1.1e-002 9.1e-005 1.00e+000  1.666354658e+002  1.666388531e+002  8.1e-010 2.02  
57  1.3e-006 1.1e-002 8.2e-005 1.00e+000  1.666356935e+002  1.666387420e+002  7.3e-010 2.06  
58  1.2e-006 1.1e-002 7.4e-005 1.00e+000  1.666358983e+002  1.666386420e+002  6.5e-010 2.09  
59  1.0e-006 1.1e-002 6.7e-005 1.00e+000  1.666360825e+002  1.666385518e+002  5.9e-010 2.13  
60  9.4e-007 1.0e-002 6.0e-005 1.00e+000  1.666362482e+002  1.666384705e+002  5.3e-010 2.16  
61  8.5e-007 1.0e-002 5.4e-005 1.00e+000  1.666363972e+002  1.666383973e+002  4.8e-010 2.19  
62  7.7e-007 9.9e-003 4.9e-005 1.00e+000  1.666365312e+002  1.666383313e+002  4.3e-010 2.22  
63  6.9e-007 9.7e-003 4.4e-005 1.00e+000  1.666366517e+002  1.666382718e+002  3.9e-010 2.27  
64  6.2e-007 9.5e-003 3.9e-005 1.00e+000  1.666367600e+002  1.666382181e+002  3.5e-010 2.30  
65  5.6e-007 9.3e-003 3.5e-005 1.00e+000  1.666368575e+002  1.666381698e+002  3.1e-010 2.33  
66  5.0e-007 9.2e-003 3.2e-005 1.00e+000  1.666369451e+002  1.666381262e+002  2.8e-010 2.36  
67  4.5e-007 9.1e-003 2.9e-005 1.00e+000  1.666370239e+002  1.666380868e+002  2.5e-010 2.39  
68  4.1e-007 9.0e-003 2.6e-005 1.00e+000  1.666370947e+002  1.666380514e+002  2.3e-010 2.42  
69  3.7e-007 8.9e-003 2.3e-005 1.00e+000  1.666371585e+002  1.666380194e+002  2.1e-010 2.45  
70  3.3e-007 8.8e-003 2.1e-005 1.00e+000  1.666372157e+002  1.666379906e+002  1.8e-010 2.48  
71  3.0e-007 8.7e-003 1.9e-005 1.00e+000  1.666372673e+002  1.666379646e+002  1.7e-010 2.52  
72  2.7e-007 8.6e-003 1.7e-005 1.00e+000  1.666373136e+002  1.666379412e+002  1.5e-010 2.55  
73  2.4e-007 8.5e-003 1.5e-005 1.00e+000  1.666373553e+002  1.666379202e+002  1.3e-010 2.58  
74  2.2e-007 8.5e-003 1.4e-005 1.00e+000  1.666373928e+002  1.666379012e+002  1.2e-010 2.61  
75  1.9e-007 8.4e-003 1.2e-005 1.00e+000  1.666374265e+002  1.666378841e+002  1.1e-010 2.66  
76  1.8e-007 8.4e-003 1.1e-005 9.99e-001  1.666374569e+002  1.666378687e+002  9.8e-011 2.69  
77  1.6e-007 8.3e-003 1.0e-005 1.00e+000  1.666374842e+002  1.666378548e+002  8.8e-011 2.72  
78  1.4e-007 8.3e-003 9.0e-006 1.00e+000  1.666375087e+002  1.666378423e+002  8.0e-011 2.75  
79  1.3e-007 8.2e-003 8.1e-006 1.00e+000  1.666375309e+002  1.666378311e+002  7.2e-011 2.80  
80  1.1e-007 8.2e-003 7.3e-006 9.99e-001  1.666375507e+002  1.666378209e+002  6.4e-011 2.83  
81  1.0e-007 8.1e-003 6.6e-006 1.00e+000  1.666375686e+002  1.666378118e+002  5.8e-011 2.88  
82  9.3e-008 8.1e-003 5.9e-006 1.00e+000  1.666375848e+002  1.666378036e+002  5.2e-011 2.91  
83  8.4e-008 8.1e-003 5.3e-006 9.99e-001  1.666375993e+002  1.666377962e+002  4.7e-011 2.94  
84  7.5e-008 8.0e-003 4.8e-006 1.00e+000  1.666376123e+002  1.666377896e+002  4.2e-011 2.98  
85  6.8e-008 8.0e-003 4.3e-006 1.00e+000  1.666376240e+002  1.666377836e+002  3.8e-011 3.02  
86  6.1e-008 8.0e-003 3.9e-006 9.99e-001  1.666376346e+002  1.666377782e+002  3.4e-011 3.06  
87  5.5e-008 7.9e-003 3.5e-006 1.00e+000  1.666376441e+002  1.666377733e+002  3.1e-011 3.11  
88  4.9e-008 7.9e-003 3.1e-006 1.00e+000  1.666376527e+002  1.666377690e+002  2.8e-011 3.14  
89  4.4e-008 7.9e-003 2.8e-006 9.98e-001  1.666376604e+002  1.666377650e+002  2.5e-011 3.17  
90  4.0e-008 7.9e-003 2.5e-006 1.00e+000  1.666376673e+002  1.666377615e+002  2.2e-011 3.22  
91  3.6e-008 7.8e-003 2.3e-006 1.00e+000  1.666376735e+002  1.666377583e+002  2.0e-011 3.25  
92  3.2e-008 7.8e-003 2.1e-006 1.00e+000  1.666376792e+002  1.666377554e+002  1.8e-011 3.28  
93  2.9e-008 7.8e-003 1.9e-006 1.00e+000  1.666376842e+002  1.666377528e+002  1.6e-011 3.33  
94  2.6e-008 7.8e-003 1.7e-006 9.99e-001  1.666376888e+002  1.666377505e+002  1.5e-011 3.36  
95  2.4e-008 7.0e-003 1.5e-006 1.00e+000  1.666376929e+002  1.666377484e+002  1.3e-011 3.39  
96  2.1e-008 6.3e-003 1.4e-006 9.98e-001  1.666376966e+002  1.666377465e+002  1.2e-011 3.44  
97  1.9e-008 5.7e-003 1.2e-006 9.98e-001  1.666376999e+002  1.666377449e+002  1.1e-011 3.47  
98  1.7e-008 5.1e-003 1.1e-006 1.00e+000  1.666377029e+002  1.666377433e+002  9.7e-012 3.50  
99  1.6e-008 4.6e-003 9.9e-007 9.95e-001  1.666377056e+002  1.666377420e+002  8.7e-012 3.53  
100 1.4e-008 4.1e-003 8.9e-007 9.99e-001  1.666377080e+002  1.666377407e+002  7.9e-012 3.56  
101 1.3e-008 3.7e-003 8.0e-007 1.00e+000  1.666377101e+002  1.666377396e+002  7.1e-012 3.61  
102 1.8e-008 3.6e-003 7.2e-007 9.80e-001  1.666377120e+002  1.666377391e+002  6.4e-012 3.64  
103 1.8e-008 3.2e-003 6.5e-007 9.99e-001  1.666377137e+002  1.666377382e+002  5.7e-012 3.67  
104 1.6e-008 2.9e-003 5.8e-007 1.00e+000  1.666377153e+002  1.666377374e+002  5.2e-012 3.70  
105 1.4e-008 2.6e-003 5.2e-007 1.01e+000  1.666377168e+002  1.666377366e+002  4.7e-012 3.75  
106 1.3e-008 2.4e-003 4.7e-007 1.03e+000  1.666377183e+002  1.666377358e+002  4.3e-012 3.78  
107 1.2e-008 2.1e-003 4.2e-007 1.01e+000  1.666377194e+002  1.666377351e+002  3.8e-012 3.81  
108 1.1e-008 1.9e-003 3.8e-007 9.96e-001  1.666377204e+002  1.666377346e+002  3.5e-012 3.86  
109 9.7e-009 1.7e-003 3.4e-007 1.02e+000  1.666377214e+002  1.666377341e+002  3.1e-012 3.89  
110 8.7e-009 1.5e-003 3.1e-007 1.00e+000  1.666377223e+002  1.666377336e+002  2.8e-012 3.92  
111 7.9e-009 1.4e-003 2.8e-007 9.94e-001  1.666377230e+002  1.666377333e+002  2.5e-012 3.95  
112 7.1e-009 1.3e-003 2.5e-007 9.96e-001  1.666377237e+002  1.666377329e+002  2.3e-012 3.98  
113 6.6e-009 1.1e-003 2.3e-007 9.98e-001  1.666377242e+002  1.666377326e+002  2.1e-012 4.01  
114 5.7e-009 1.0e-003 2.0e-007 9.68e-001  1.666377248e+002  1.666377323e+002  1.9e-012 4.05  
115 1.2e-009 5.6e-005 1.1e-008 9.62e-001  1.666377294e+002  1.666377298e+002  1.2e-013 4.08  
Interior-point optimizer terminated. Time: 4.08. 

Optimizer terminated. Time: 4.13    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6663772941e+002   nrm: 2e+001   Viol.  con: 3e-008   var: 0e+000 
  Dual.    obj: 1.6663772984e+002   nrm: 9e+002   Viol.  con: 0e+000   var: 4e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 4.15 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 868
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3452              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 : 1.48e+004         after factor           : 1.48e+005       
Factor     - dense dim.             : 0                 flops                  : 2.93e+007       
Factor     - GP saved nzs           : 3.33e+004         GP saved flops         : 9.12e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.226849239e+005 2.000000000e+000  1.0e+000 0.06  
1   1.7e+003 2.2e+003 8.9e+004 -9.71e-001 -1.219534294e+005 2.620225063e+000  7.3e-001 0.13  
2   8.7e+002 1.2e+003 4.7e+004 -9.59e-001 -1.196347191e+005 4.651232037e+000  3.8e-001 0.16  
3   2.9e+002 3.9e+002 1.6e+004 -9.21e-001 -1.107208228e+005 2.005392357e+001  1.3e-001 0.20  
4   2.9e+002 3.9e+002 1.6e+004 -7.72e-001 -1.084773393e+005 1.977849647e+003  1.3e-001 0.23  
5   1.2e+002 1.6e+002 6.4e+003 -7.62e-001 -8.711285036e+004 6.311703239e+003  5.2e-002 0.27  
6   4.2e+001 5.6e+001 2.2e+003 -4.46e-001 -4.936047090e+004 1.079796256e+004  1.9e-002 0.30  
7   2.5e+001 3.4e+001 1.3e+003 1.90e-001  -3.425875065e+004 7.462585720e+003  1.1e-002 0.33  
8   1.3e+001 1.7e+001 7.0e+002 4.81e-001  -1.968663943e+004 4.675777379e+003  5.8e-003 0.36  
9   4.9e+000 6.6e+000 2.7e+002 7.37e-001  -7.617325493e+003 2.298848291e+003  2.2e-003 0.39  
10  2.3e+000 3.2e+000 1.3e+002 9.29e-001  -3.398291800e+003 1.407277088e+003  1.0e-003 0.42  
11  1.5e+000 2.0e+000 8.2e+001 9.81e-001  -2.145200795e+003 9.589411243e+002  6.8e-004 0.45  
12  8.6e-001 1.2e+000 4.7e+001 9.88e-001  -1.159978720e+003 6.218748821e+002  3.9e-004 0.50  
13  7.6e-001 1.1e+000 4.1e+001 9.55e-001  -1.036813866e+003 5.640869372e+002  3.4e-004 0.53  
14  3.8e-001 5.6e-001 2.1e+001 9.86e-001  -4.218867577e+002 3.767872746e+002  1.7e-004 0.56  
15  1.9e-001 4.9e-001 1.0e+001 9.99e-001  -1.340640073e+002 2.592390609e+002  8.5e-005 0.61  
16  9.2e-002 2.6e-001 5.1e+000 1.01e+000  8.554917173e+000  2.056234335e+002  4.3e-005 0.64  
17  8.9e-002 2.5e-001 4.9e+000 1.01e+000  1.752038594e+001  2.076465550e+002  4.2e-005 0.67  
18  6.2e-002 1.7e-001 3.5e+000 1.01e+000  6.310350288e+001  1.953125443e+002  2.9e-005 0.72  
19  3.0e-002 9.7e-002 1.7e+000 1.01e+000  1.172653319e+002  1.810925603e+002  1.4e-005 0.75  
20  8.7e-003 1.8e-001 4.9e-001 1.01e+000  1.531505253e+002  1.716299670e+002  4.1e-006 0.78  
21  2.6e-003 1.9e-001 1.5e-001 1.00e+000  1.623849959e+002  1.679586883e+002  1.2e-006 0.83  
22  1.5e-003 1.2e-001 8.7e-002 1.00e+000  1.641429160e+002  1.674184684e+002  7.4e-007 0.86  
23  5.2e-004 1.0e-001 3.1e-002 1.01e+000  1.656902534e+002  1.668678096e+002  2.7e-007 0.89  
24  2.0e-004 9.7e-002 1.2e-002 1.01e+000  1.662107998e+002  1.666667299e+002  1.1e-007 0.94  
25  1.8e-004 8.9e-002 1.1e-002 1.01e+000  1.662459882e+002  1.666561861e+002  9.5e-008 0.97  
26  1.6e-004 8.1e-002 9.9e-003 1.01e+000  1.662749084e+002  1.666439448e+002  8.6e-008 1.00  
27  1.5e-004 7.4e-002 8.9e-003 1.01e+000  1.663011062e+002  1.666331281e+002  7.7e-008 1.03  
28  1.3e-004 6.7e-002 8.0e-003 1.01e+000  1.663245601e+002  1.666232880e+002  6.9e-008 1.06  
29  1.2e-004 6.1e-002 7.2e-003 1.01e+000  1.663456064e+002  1.666143858e+002  6.3e-008 1.09  
30  1.1e-004 5.6e-002 6.5e-003 1.01e+000  1.663644865e+002  1.666063257e+002  5.6e-008 1.11  
31  9.6e-005 5.1e-002 5.8e-003 1.01e+000  1.663814253e+002  1.665990296e+002  5.1e-008 1.14  
32  8.6e-005 4.7e-002 5.2e-003 1.01e+000  1.663966231e+002  1.665924254e+002  4.6e-008 1.16  
33  7.8e-005 4.3e-002 4.7e-003 1.01e+000  1.664102600e+002  1.665864482e+002  4.1e-008 1.17  
34  7.0e-005 3.9e-002 4.2e-003 1.01e+000  1.664224975e+002  1.665810395e+002  3.7e-008 1.20  
35  6.3e-005 3.6e-002 3.8e-003 1.01e+000  1.664334804e+002  1.665761461e+002  3.3e-008 1.22  
36  5.7e-005 3.3e-002 3.4e-003 1.00e+000  1.664433386e+002  1.665717197e+002  3.0e-008 1.25  
37  5.1e-005 3.1e-002 3.1e-003 1.00e+000  1.664521881e+002  1.665677168e+002  2.7e-008 1.26  
38  4.6e-005 2.8e-002 2.8e-003 1.00e+000  1.664601332e+002  1.665640975e+002  2.4e-008 1.28  
39  4.1e-005 2.6e-002 2.5e-003 1.00e+000  1.664672670e+002  1.665608257e+002  2.2e-008 1.31  
40  3.7e-005 2.5e-002 2.3e-003 1.00e+000  1.664736732e+002  1.665578687e+002  2.0e-008 1.33  
41  3.3e-005 2.3e-002 2.0e-003 1.00e+000  1.664794265e+002  1.665551966e+002  1.8e-008 1.36  
42  3.0e-005 2.1e-002 1.8e-003 1.00e+000  1.664845940e+002  1.665527826e+002  1.6e-008 1.38  
43  2.7e-005 2.0e-002 1.6e-003 1.00e+000  1.664892359e+002  1.665506020e+002  1.4e-008 1.42  
44  2.4e-005 1.9e-002 1.5e-003 1.00e+000  1.664934060e+002  1.665486327e+002  1.3e-008 1.45  
45  2.2e-005 1.8e-002 1.3e-003 1.00e+000  1.664971527e+002  1.665468546e+002  1.2e-008 1.48  
46  2.0e-005 1.7e-002 1.2e-003 1.00e+000  1.665005194e+002  1.665452494e+002  1.0e-008 1.51  
47  1.8e-005 1.6e-002 1.1e-003 1.00e+000  1.665035449e+002  1.665438006e+002  9.4e-009 1.53  
48  1.6e-005 1.5e-002 9.7e-004 1.00e+000  1.665062641e+002  1.665424932e+002  8.5e-009 1.56  
49  1.4e-005 1.4e-002 8.8e-004 1.00e+000  1.665087083e+002  1.665413138e+002  7.6e-009 1.58  
50  1.3e-005 1.4e-002 7.9e-004 1.00e+000  1.665109056e+002  1.665402500e+002  6.9e-009 1.59  
51  1.2e-005 1.3e-002 7.1e-004 1.00e+000  1.665128811e+002  1.665392906e+002  6.2e-009 1.63  
52  1.0e-005 1.3e-002 6.4e-004 1.00e+000  1.665146574e+002  1.665384257e+002  5.6e-009 1.64  
53  9.4e-006 1.2e-002 5.7e-004 1.00e+000  1.665162548e+002  1.665376460e+002  5.0e-009 1.66  
54  8.5e-006 1.2e-002 5.2e-004 1.00e+000  1.665176913e+002  1.665369433e+002  4.5e-009 1.69  
55  7.6e-006 1.1e-002 4.7e-004 1.00e+000  1.665189833e+002  1.665363100e+002  4.1e-009 1.70  
56  6.9e-006 1.1e-002 4.2e-004 1.00e+000  1.665201454e+002  1.665357394e+002  3.6e-009 1.73  
57  6.2e-006 1.1e-002 3.8e-004 1.00e+000  1.665211906e+002  1.665352252e+002  3.3e-009 1.75  
58  5.6e-006 1.1e-002 3.4e-004 1.00e+000  1.665221309e+002  1.665347620e+002  3.0e-009 1.76  
59  5.0e-006 1.0e-002 3.1e-004 1.00e+000  1.665229766e+002  1.665343447e+002  2.7e-009 1.80  
60  4.5e-006 1.0e-002 2.7e-004 1.00e+000  1.665237374e+002  1.665339687e+002  2.4e-009 1.81  
61  4.1e-006 9.9e-003 2.5e-004 1.00e+000  1.665244217e+002  1.665336299e+002  2.2e-009 1.83  
62  3.7e-006 9.7e-003 2.2e-004 1.00e+000  1.665250372e+002  1.665333246e+002  1.9e-009 1.86  
63  3.3e-006 9.6e-003 2.0e-004 1.00e+000  1.665255908e+002  1.665330495e+002  1.7e-009 1.88  
64  3.0e-006 9.4e-003 1.8e-004 1.00e+000  1.665260887e+002  1.665328016e+002  1.6e-009 1.91  
65  2.7e-006 9.3e-003 1.6e-004 1.00e+000  1.665265365e+002  1.665325782e+002  1.4e-009 1.92  
66  2.4e-006 9.2e-003 1.5e-004 1.00e+000  1.665269394e+002  1.665323769e+002  1.3e-009 1.95  
67  2.2e-006 9.1e-003 1.3e-004 1.00e+000  1.665273018e+002  1.665321956e+002  1.1e-009 1.97  
68  1.9e-006 9.0e-003 1.2e-004 1.00e+000  1.665276278e+002  1.665320322e+002  1.0e-009 2.00  
69  1.7e-006 8.9e-003 1.1e-004 1.00e+000  1.665279210e+002  1.665318851e+002  9.3e-010 2.02  
70  1.6e-006 8.8e-003 9.6e-005 1.00e+000  1.665281849e+002  1.665317525e+002  8.4e-010 2.05  
71  1.4e-006 8.7e-003 8.6e-005 1.00e+000  1.665284222e+002  1.665316331e+002  7.5e-010 2.06  
72  1.3e-006 8.7e-003 7.8e-005 1.00e+000  1.665286357e+002  1.665315256e+002  6.8e-010 2.08  
73  1.1e-006 8.6e-003 7.0e-005 1.00e+000  1.665288278e+002  1.665314287e+002  6.1e-010 2.11  
74  1.0e-006 8.6e-003 6.3e-005 1.00e+000  1.665290005e+002  1.665313414e+002  5.5e-010 2.13  
75  9.3e-007 8.5e-003 5.7e-005 1.00e+000  1.665291559e+002  1.665312627e+002  4.9e-010 2.16  
76  8.4e-007 8.5e-003 5.1e-005 1.00e+000  1.665292957e+002  1.665311918e+002  4.4e-010 2.17  
77  7.5e-007 8.4e-003 4.6e-005 1.00e+000  1.665294214e+002  1.665311279e+002  4.0e-010 2.19  
78  6.8e-007 8.4e-003 4.1e-005 1.00e+000  1.665295345e+002  1.665310704e+002  3.6e-010 2.22  
79  6.1e-007 8.3e-003 3.7e-005 1.00e+000  1.665296362e+002  1.665310185e+002  3.2e-010 2.23  
80  5.5e-007 8.3e-003 3.3e-005 1.00e+000  1.665297276e+002  1.665309717e+002  2.9e-010 2.25  
81  4.9e-007 8.3e-003 3.0e-005 1.00e+000  1.665298099e+002  1.665309295e+002  2.6e-010 2.28  
82  4.4e-007 8.3e-003 2.7e-005 1.00e+000  1.665298838e+002  1.665308915e+002  2.4e-010 2.30  
83  4.0e-007 8.2e-003 2.4e-005 1.00e+000  1.665299503e+002  1.665308572e+002  2.1e-010 2.33  
84  3.6e-007 8.2e-003 2.2e-005 1.00e+000  1.665300101e+002  1.665308263e+002  1.9e-010 2.34  
85  3.2e-007 8.2e-003 2.0e-005 1.00e+000  1.665300639e+002  1.665307985e+002  1.7e-010 2.36  
86  2.9e-007 8.1e-003 1.8e-005 1.00e+000  1.665301122e+002  1.665307734e+002  1.5e-010 2.39  
87  2.6e-007 8.1e-003 1.6e-005 1.00e+000  1.665301557e+002  1.665307508e+002  1.4e-010 2.41  
88  2.4e-007 8.1e-003 1.4e-005 1.00e+000  1.665301949e+002  1.665307304e+002  1.3e-010 2.44  
89  2.1e-007 8.1e-003 1.3e-005 1.00e+000  1.665302301e+002  1.665307121e+002  1.1e-010 2.45  
90  1.9e-007 8.1e-003 1.2e-005 1.00e+000  1.665302617e+002  1.665306955e+002  1.0e-010 2.48  
91  1.7e-007 8.0e-003 1.0e-005 1.00e+000  1.665302902e+002  1.665306806e+002  9.1e-011 2.50  
92  1.6e-007 8.0e-003 9.4e-006 1.00e+000  1.665303158e+002  1.665306672e+002  8.2e-011 2.52  
93  1.4e-007 8.0e-003 8.5e-006 1.00e+000  1.665303389e+002  1.665306551e+002  7.4e-011 2.55  
94  1.3e-007 8.0e-003 7.6e-006 1.00e+000  1.665303596e+002  1.665306443e+002  6.7e-011 2.56  
95  1.1e-007 8.0e-003 6.9e-006 9.99e-001  1.665303783e+002  1.665306345e+002  6.0e-011 2.59  
96  1.0e-007 7.9e-003 6.2e-006 9.99e-001  1.665303951e+002  1.665306257e+002  5.4e-011 2.61  
97  9.2e-008 7.9e-003 5.6e-006 1.00e+000  1.665304102e+002  1.665306177e+002  4.9e-011 2.64  
98  8.2e-008 7.9e-003 5.0e-006 9.99e-001  1.665304238e+002  1.665306106e+002  4.4e-011 2.66  
99  7.4e-008 7.9e-003 4.5e-006 1.00e+000  1.665304361e+002  1.665306042e+002  3.9e-011 2.69  
100 6.7e-008 7.9e-003 4.1e-006 9.99e-001  1.665304471e+002  1.665305984e+002  3.5e-011 2.70  
101 6.0e-008 7.8e-003 3.7e-006 9.99e-001  1.665304570e+002  1.665305932e+002  3.2e-011 2.73  
102 5.4e-008 7.8e-003 3.3e-006 1.00e+000  1.665304659e+002  1.665305885e+002  2.9e-011 2.75  
103 4.9e-008 7.8e-003 3.0e-006 1.00e+000  1.665304739e+002  1.665305842e+002  2.6e-011 2.78  
104 4.4e-008 7.8e-003 2.7e-006 9.98e-001  1.665304812e+002  1.665305804e+002  2.3e-011 2.81  
105 3.9e-008 7.8e-003 2.4e-006 1.00e+000  1.665304877e+002  1.665305770e+002  2.1e-011 2.83  
106 3.5e-008 7.8e-003 2.2e-006 9.99e-001  1.665304935e+002  1.665305739e+002  1.9e-011 2.86  
107 3.2e-008 7.7e-003 1.9e-006 1.00e+000  1.665304988e+002  1.665305712e+002  1.7e-011 2.88  
108 2.9e-008 7.7e-003 1.7e-006 1.00e+000  1.665305035e+002  1.665305687e+002  1.5e-011 2.91  
109 2.6e-008 7.7e-003 1.6e-006 1.00e+000  1.665305078e+002  1.665305664e+002  1.4e-011 2.92  
110 2.3e-008 7.7e-003 1.4e-006 9.98e-001  1.665305116e+002  1.665305644e+002  1.2e-011 2.95  
111 2.1e-008 7.7e-003 1.3e-006 9.98e-001  1.665305151e+002  1.665305626e+002  1.1e-011 2.97  
112 1.9e-008 7.7e-003 1.1e-006 9.98e-001  1.665305182e+002  1.665305610e+002  1.0e-011 2.98  
113 1.7e-008 7.7e-003 1.0e-006 9.99e-001  1.665305210e+002  1.665305595e+002  9.0e-012 3.02  
114 1.5e-008 7.6e-003 9.3e-007 9.95e-001  1.665305235e+002  1.665305582e+002  8.1e-012 3.03  
115 1.4e-008 7.6e-003 8.4e-007 9.99e-001  1.665305258e+002  1.665305570e+002  7.3e-012 3.06  
116 1.2e-008 7.6e-003 7.5e-007 1.00e+000  1.665305278e+002  1.665305559e+002  6.6e-012 3.08  
117 1.1e-008 6.8e-003 6.8e-007 1.01e+000  1.665305297e+002  1.665305549e+002  5.9e-012 3.11  
118 1.0e-008 6.2e-003 6.1e-007 1.00e+000  1.665305314e+002  1.665305540e+002  5.3e-012 3.13  
119 9.4e-009 5.5e-003 5.5e-007 1.01e+000  1.665305329e+002  1.665305533e+002  4.8e-012 3.16  
120 8.5e-009 5.0e-003 4.9e-007 9.72e-001  1.665305342e+002  1.665305526e+002  4.3e-012 3.17  
121 9.4e-009 4.5e-003 4.4e-007 9.76e-001  1.665305354e+002  1.665305518e+002  3.9e-012 3.19  
122 8.4e-009 4.0e-003 4.0e-007 9.99e-001  1.665305365e+002  1.665305513e+002  3.5e-012 3.22  
123 7.6e-009 3.6e-003 3.6e-007 9.99e-001  1.665305375e+002  1.665305508e+002  3.2e-012 3.23  
124 6.9e-009 3.3e-003 3.2e-007 9.90e-001  1.665305383e+002  1.665305503e+002  2.8e-012 3.25  
125 6.2e-009 2.9e-003 2.9e-007 1.02e+000  1.665305392e+002  1.665305499e+002  2.6e-012 3.28  
126 5.5e-009 2.7e-003 2.6e-007 9.84e-001  1.665305399e+002  1.665305495e+002  2.3e-012 3.30  
127 1.5e-007 2.4e-003 2.4e-007 8.44e-001  1.665305404e+002  1.665305498e+002  2.1e-012 3.33  
128 1.3e-007 2.1e-003 2.1e-007 1.02e+000  1.665305410e+002  1.665305494e+002  1.9e-012 3.34  
129 1.2e-007 1.9e-003 1.9e-007 9.78e-001  1.665305415e+002  1.665305491e+002  1.7e-012 3.36  
130 1.4e-007 1.9e-003 1.9e-007 1.35e+000  1.665305417e+002  1.665305482e+002  1.7e-012 3.39  
131 1.2e-007 1.7e-003 1.7e-007 1.47e+000  1.665305422e+002  1.665305480e+002  1.5e-012 3.41  
132 8.0e-009 9.7e-005 1.1e-008 1.00e+000  1.665305459e+002  1.665305463e+002  8.5e-014 3.44  
Interior-point optimizer terminated. Time: 3.44. 

Optimizer terminated. Time: 3.45    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6653054593e+002   nrm: 2e+001   Viol.  con: 1e-007   var: 0e+000 
  Dual.    obj: 1.6653054629e+002   nrm: 1e+003   Viol.  con: 0e+000   var: 6e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.49 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 868
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3452              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 : 1.48e+004         after factor           : 1.48e+005       
Factor     - dense dim.             : 0                 flops                  : 2.93e+007       
Factor     - GP saved nzs           : 3.33e+004         GP saved flops         : 9.12e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.226819507e+005 2.000000000e+000  1.0e+000 0.09  
1   1.7e+003 2.2e+003 8.9e+004 -9.71e-001 -1.219502494e+005 2.618325375e+000  7.3e-001 0.14  
2   8.7e+002 1.2e+003 4.7e+004 -9.59e-001 -1.196374201e+005 4.640470862e+000  3.8e-001 0.16  
3   2.9e+002 3.9e+002 1.6e+004 -9.21e-001 -1.106689816e+005 2.010085092e+001  1.3e-001 0.19  
4   2.9e+002 3.9e+002 1.5e+004 -7.71e-001 -1.084447201e+005 1.966197148e+003  1.3e-001 0.20  
5   1.2e+002 1.6e+002 6.3e+003 -7.61e-001 -8.700933758e+004 6.299125805e+003  5.2e-002 0.22  
6   3.3e+001 4.4e+001 1.8e+003 -4.45e-001 -4.090570829e+004 1.177146417e+004  1.5e-002 0.25  
7   2.0e+001 2.7e+001 1.1e+003 3.44e-001  -2.843133834e+004 7.437638444e+003  9.1e-003 0.27  
8   1.0e+001 1.4e+001 5.5e+002 5.87e-001  -1.544320219e+004 4.101945116e+003  4.5e-003 0.28  
9   3.8e+000 5.1e+000 2.0e+002 8.09e-001  -5.797857385e+003 1.892894033e+003  1.7e-003 0.30  
10  2.1e+000 2.8e+000 1.1e+002 9.52e-001  -3.027126002e+003 1.211769441e+003  9.2e-004 0.33  
11  8.8e-001 1.2e+000 4.8e+001 9.86e-001  -1.183747076e+003 6.420749036e+002  4.0e-004 0.34  
12  8.4e-001 1.1e+000 4.6e+001 9.64e-001  -1.148613590e+003 6.116856221e+002  3.8e-004 0.38  
13  5.3e-001 7.1e-001 2.9e+001 9.74e-001  -6.867170772e+002 4.366423918e+002  2.4e-004 0.39  
14  3.5e-001 4.7e-001 1.9e+001 1.00e+000  -3.747118852e+002 3.597751107e+002  1.6e-004 0.42  
15  1.4e-001 2.0e-001 7.6e+000 9.97e-001  -6.323407911e+001 2.309686009e+002  6.4e-005 0.44  
16  8.4e-002 1.3e-001 4.7e+000 1.01e+000  2.237492199e+001  2.024368767e+002  4.0e-005 0.47  
17  8.1e-002 1.2e-001 4.5e+000 1.02e+000  2.803491521e+001  2.012806020e+002  3.8e-005 0.50  
18  5.5e-002 8.5e-002 3.1e+000 1.02e+000  7.551177141e+001  1.919870231e+002  2.6e-005 0.53  
19  1.6e-002 8.7e-002 9.0e-001 1.02e+000  1.406137340e+002  1.747475957e+002  7.6e-006 0.55  
20  4.8e-003 2.0e-001 2.7e-001 1.01e+000  1.589424938e+002  1.692863227e+002  2.3e-006 0.58  
21  3.1e-003 2.2e-001 1.8e-001 1.01e+000  1.614585153e+002  1.682601653e+002  1.5e-006 0.59  
22  1.0e-003 1.3e-001 6.0e-002 1.00e+000  1.648742226e+002  1.671211405e+002  5.1e-007 0.63  
23  3.3e-004 1.1e-001 2.0e-002 1.01e+000  1.659556694e+002  1.666967868e+002  1.7e-007 0.64  
24  1.5e-004 9.3e-002 9.1e-003 1.01e+000  1.662395100e+002  1.665804363e+002  7.9e-008 0.67  
25  1.3e-004 8.5e-002 8.2e-003 1.01e+000  1.662655807e+002  1.665723911e+002  7.2e-008 0.69  
26  1.2e-004 7.7e-002 7.4e-003 1.01e+000  1.662869324e+002  1.665629435e+002  6.4e-008 0.72  
27  1.1e-004 7.0e-002 6.7e-003 1.01e+000  1.663062644e+002  1.665545917e+002  5.8e-008 0.73  
28  9.8e-005 6.4e-002 6.0e-003 1.01e+000  1.663235688e+002  1.665469933e+002  5.2e-008 0.77  
29  8.8e-005 5.8e-002 5.4e-003 1.01e+000  1.663390987e+002  1.665401233e+002  4.7e-008 0.78  
30  7.9e-005 5.3e-002 4.9e-003 1.01e+000  1.663530298e+002  1.665339046e+002  4.2e-008 0.80  
31  7.1e-005 4.9e-002 4.4e-003 1.01e+000  1.663655288e+002  1.665282774e+002  3.8e-008 0.83  
32  6.4e-005 4.5e-002 3.9e-003 1.01e+000  1.663767438e+002  1.665231856e+002  3.4e-008 0.84  
33  5.8e-005 4.1e-002 3.5e-003 1.01e+000  1.663868077e+002  1.665185793e+002  3.1e-008 0.88  
34  5.2e-005 3.8e-002 3.2e-003 1.01e+000  1.663958397e+002  1.665144130e+002  2.8e-008 0.89  
35  4.7e-005 3.5e-002 2.9e-003 1.01e+000  1.664039467e+002  1.665106453e+002  2.5e-008 0.92  
36  4.2e-005 3.2e-002 2.6e-003 1.00e+000  1.664112242e+002  1.665072390e+002  2.2e-008 0.94  
37  3.8e-005 3.0e-002 2.3e-003 1.00e+000  1.664177581e+002  1.665041599e+002  2.0e-008 0.97  
38  3.4e-005 2.7e-002 2.1e-003 1.00e+000  1.664236249e+002  1.665013773e+002  1.8e-008 0.98  
39  3.1e-005 2.6e-002 1.9e-003 1.00e+000  1.664288934e+002  1.664988632e+002  1.6e-008 1.02  
40  2.8e-005 2.4e-002 1.7e-003 1.00e+000  1.664336252e+002  1.664965921e+002  1.5e-008 1.03  
41  2.5e-005 2.2e-002 1.5e-003 1.00e+000  1.664378755e+002  1.664945409e+002  1.3e-008 1.06  
42  2.2e-005 2.1e-002 1.4e-003 1.00e+000  1.664416937e+002  1.664926887e+002  1.2e-008 1.09  
43  2.0e-005 1.9e-002 1.2e-003 1.00e+000  1.664451240e+002  1.664910165e+002  1.1e-008 1.11  
44  1.8e-005 1.8e-002 1.1e-003 1.00e+000  1.664482063e+002  1.664895070e+002  9.7e-009 1.14  
45  1.6e-005 1.7e-002 1.0e-003 1.00e+000  1.664509760e+002  1.664881448e+002  8.7e-009 1.16  
46  1.5e-005 1.6e-002 9.0e-004 1.00e+000  1.664534653e+002  1.664869157e+002  7.9e-009 1.17  
47  1.3e-005 1.6e-002 8.1e-004 1.00e+000  1.664557026e+002  1.664858068e+002  7.1e-009 1.20  
48  1.2e-005 1.5e-002 7.3e-004 1.00e+000  1.664577137e+002  1.664848066e+002  6.4e-009 1.22  
49  1.1e-005 1.4e-002 6.6e-004 1.00e+000  1.664595217e+002  1.664839046e+002  5.7e-009 1.25  
50  9.6e-006 1.3e-002 5.9e-004 1.00e+000  1.664611472e+002  1.664830913e+002  5.2e-009 1.27  
51  8.7e-006 1.3e-002 5.3e-004 1.00e+000  1.664626088e+002  1.664823580e+002  4.6e-009 1.30  
52  7.8e-006 1.2e-002 4.8e-004 1.00e+000  1.664639231e+002  1.664816971e+002  4.2e-009 1.31  
53  7.0e-006 1.2e-002 4.3e-004 1.00e+000  1.664651050e+002  1.664811014e+002  3.8e-009 1.33  
54  6.3e-006 1.2e-002 3.9e-004 1.00e+000  1.664661680e+002  1.664805646e+002  3.4e-009 1.36  
55  5.7e-006 1.1e-002 3.5e-004 1.00e+000  1.664671242e+002  1.664800810e+002  3.0e-009 1.38  
56  5.1e-006 1.1e-002 3.1e-004 1.00e+000  1.664679842e+002  1.664796452e+002  2.7e-009 1.41  
57  4.6e-006 1.1e-002 2.8e-004 1.00e+000  1.664687577e+002  1.664792527e+002  2.5e-009 1.42  
58  4.1e-006 1.0e-002 2.5e-004 1.00e+000  1.664694536e+002  1.664788990e+002  2.2e-009 1.45  
59  3.7e-006 1.0e-002 2.3e-004 1.00e+000  1.664700796e+002  1.664785804e+002  2.0e-009 1.47  
60  3.4e-006 9.9e-003 2.1e-004 1.00e+000  1.664706427e+002  1.664782934e+002  1.8e-009 1.49  
61  3.0e-006 9.7e-003 1.9e-004 1.00e+000  1.664711492e+002  1.664780349e+002  1.6e-009 1.52  
62  2.7e-006 9.5e-003 1.7e-004 1.00e+000  1.664716049e+002  1.664778020e+002  1.5e-009 1.53  
63  2.4e-006 9.3e-003 1.5e-004 1.00e+000  1.664720149e+002  1.664775923e+002  1.3e-009 1.56  
64  2.2e-006 9.2e-003 1.4e-004 1.00e+000  1.664723838e+002  1.664774035e+002  1.2e-009 1.58  
65  2.0e-006 9.1e-003 1.2e-004 1.00e+000  1.664727158e+002  1.664772335e+002  1.1e-009 1.61  
66  1.8e-006 8.9e-003 1.1e-004 1.00e+000  1.664730145e+002  1.664770805e+002  9.6e-010 1.63  
67  1.6e-006 8.8e-003 9.9e-005 1.00e+000  1.664732834e+002  1.664769428e+002  8.6e-010 1.66  
68  1.4e-006 8.7e-003 8.9e-005 1.00e+000  1.664735253e+002  1.664768188e+002  7.7e-010 1.67  
69  1.3e-006 8.6e-003 8.0e-005 1.00e+000  1.664737431e+002  1.664767072e+002  7.0e-010 1.70  
70  1.2e-006 8.6e-003 7.2e-005 1.00e+000  1.664739390e+002  1.664766068e+002  6.3e-010 1.72  
71  1.1e-006 8.5e-003 6.5e-005 1.00e+000  1.664741153e+002  1.664765163e+002  5.6e-010 1.75  
72  9.5e-007 8.4e-003 5.8e-005 1.00e+000  1.664742740e+002  1.664764349e+002  5.1e-010 1.77  
73  8.5e-007 8.4e-003 5.2e-005 1.00e+000  1.664744168e+002  1.664763616e+002  4.6e-010 1.78  
74  7.7e-007 8.3e-003 4.7e-005 1.00e+000  1.664745453e+002  1.664762956e+002  4.1e-010 1.81  
75  6.9e-007 8.2e-003 4.2e-005 1.00e+000  1.664746608e+002  1.664762362e+002  3.7e-010 1.84  
76  6.2e-007 8.2e-003 3.8e-005 1.00e+000  1.664747648e+002  1.664761826e+002  3.3e-010 1.86  
77  5.6e-007 8.2e-003 3.4e-005 1.00e+000  1.664748584e+002  1.664761345e+002  3.0e-010 1.89  
78  5.0e-007 8.1e-003 3.1e-005 1.00e+000  1.664749425e+002  1.664760910e+002  2.7e-010 1.91  
79  4.5e-007 8.1e-003 2.8e-005 1.00e+000  1.664750183e+002  1.664760519e+002  2.4e-010 1.94  
80  4.1e-007 8.0e-003 2.5e-005 1.00e+000  1.664750863e+002  1.664760166e+002  2.2e-010 1.95  
81  3.7e-007 8.0e-003 2.3e-005 1.00e+000  1.664751476e+002  1.664759848e+002  2.0e-010 1.99  
82  3.3e-007 8.0e-003 2.0e-005 1.00e+000  1.664752027e+002  1.664759562e+002  1.8e-010 2.00  
83  3.0e-007 7.9e-003 1.8e-005 1.00e+000  1.664752523e+002  1.664759304e+002  1.6e-010 2.03  
84  2.7e-007 7.9e-003 1.6e-005 1.00e+000  1.664752969e+002  1.664759072e+002  1.4e-010 2.05  
85  2.4e-007 7.9e-003 1.5e-005 1.00e+000  1.664753370e+002  1.664758863e+002  1.3e-010 2.08  
86  2.2e-007 7.9e-003 1.3e-005 1.00e+000  1.664753731e+002  1.664758675e+002  1.2e-010 2.09  
87  2.0e-007 7.9e-003 1.2e-005 1.00e+000  1.664754056e+002  1.664758505e+002  1.0e-010 2.11  
88  1.8e-007 7.8e-003 1.1e-005 1.00e+000  1.664754348e+002  1.664758353e+002  9.4e-011 2.14  
89  1.6e-007 7.8e-003 9.7e-006 1.00e+000  1.664754611e+002  1.664758215e+002  8.5e-011 2.16  
90  1.4e-007 7.8e-003 8.8e-006 1.00e+000  1.664754848e+002  1.664758091e+002  7.6e-011 2.19  
91  1.3e-007 7.8e-003 7.9e-006 9.99e-001  1.664755061e+002  1.664757980e+002  6.9e-011 2.20  
92  1.2e-007 7.8e-003 7.1e-006 1.00e+000  1.664755252e+002  1.664757880e+002  6.2e-011 2.22  
93  1.0e-007 7.8e-003 6.4e-006 1.00e+000  1.664755425e+002  1.664757790e+002  5.6e-011 2.25  
94  9.3e-008 7.7e-003 5.7e-006 1.00e+000  1.664755580e+002  1.664757708e+002  5.0e-011 2.27  
95  8.4e-008 7.7e-003 5.2e-006 1.00e+000  1.664755720e+002  1.664757635e+002  4.5e-011 2.30  
96  7.6e-008 7.7e-003 4.7e-006 1.00e+000  1.664755845e+002  1.664757569e+002  4.1e-011 2.31  
97  6.8e-008 7.7e-003 4.2e-006 1.00e+000  1.664755958e+002  1.664757510e+002  3.6e-011 2.33  
98  6.1e-008 7.7e-003 3.8e-006 1.00e+000  1.664756060e+002  1.664757457e+002  3.3e-011 2.36  
99  5.5e-008 7.7e-003 3.4e-006 1.00e+000  1.664756152e+002  1.664757409e+002  3.0e-011 2.38  
100 5.0e-008 7.7e-003 3.1e-006 1.00e+000  1.664756234e+002  1.664757365e+002  2.7e-011 2.39  
101 4.5e-008 7.6e-003 2.7e-006 1.00e+000  1.664756308e+002  1.664757326e+002  2.4e-011 2.42  
102 4.0e-008 7.6e-003 2.5e-006 1.00e+000  1.664756375e+002  1.664757291e+002  2.2e-011 2.44  
103 3.6e-008 7.6e-003 2.2e-006 9.99e-001  1.664756435e+002  1.664757260e+002  1.9e-011 2.47  
104 3.3e-008 7.6e-003 2.0e-006 1.00e+000  1.664756489e+002  1.664757231e+002  1.7e-011 2.48  
105 2.9e-008 7.6e-003 1.8e-006 1.00e+000  1.664756538e+002  1.664757206e+002  1.6e-011 2.50  
106 2.6e-008 7.6e-003 1.6e-006 1.00e+000  1.664756582e+002  1.664757183e+002  1.4e-011 2.53  
107 2.4e-008 7.6e-003 1.5e-006 1.00e+000  1.664756621e+002  1.664757162e+002  1.3e-011 2.55  
108 2.1e-008 7.6e-003 1.3e-006 9.98e-001  1.664756657e+002  1.664757144e+002  1.1e-011 2.58  
109 1.9e-008 7.6e-003 1.2e-006 9.98e-001  1.664756689e+002  1.664757127e+002  1.0e-011 2.59  
110 1.7e-008 7.6e-003 1.1e-006 9.99e-001  1.664756717e+002  1.664757112e+002  9.3e-012 2.63  
111 1.6e-008 6.8e-003 9.6e-007 1.00e+000  1.664756744e+002  1.664757098e+002  8.4e-012 2.64  
112 1.4e-008 6.1e-003 8.6e-007 1.01e+000  1.664756768e+002  1.664757085e+002  7.6e-012 2.67  
113 1.3e-008 5.5e-003 7.8e-007 9.99e-001  1.664756789e+002  1.664757074e+002  6.8e-012 2.69  
114 1.1e-008 5.0e-003 7.0e-007 1.00e+000  1.664756807e+002  1.664757065e+002  6.1e-012 2.72  
115 1.0e-008 4.5e-003 6.3e-007 1.00e+000  1.664756825e+002  1.664757056e+002  5.5e-012 2.73  
116 9.3e-009 4.0e-003 5.7e-007 1.01e+000  1.664756840e+002  1.664757047e+002  5.0e-012 2.75  
117 3.7e-009 4.4e-004 6.2e-008 1.02e+000  1.664756961e+002  1.664756983e+002  5.2e-013 2.78  
Interior-point optimizer terminated. Time: 2.78. 

Optimizer terminated. Time: 2.78    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6647569608e+002   nrm: 2e+001   Viol.  con: 1e-007   var: 0e+000 
  Dual.    obj: 1.6647569833e+002   nrm: 1e+003   Viol.  con: 0e+000   var: 3e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.82 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.05    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 868
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3452              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 : 1.48e+004         after factor           : 1.48e+005       
Factor     - dense dim.             : 0                 flops                  : 2.93e+007       
Factor     - GP saved nzs           : 3.33e+004         GP saved flops         : 9.12e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.226806720e+005 2.000000000e+000  1.0e+000 0.09  
1   1.7e+003 2.2e+003 8.9e+004 -9.71e-001 -1.219491848e+005 2.617495992e+000  7.3e-001 0.13  
2   8.7e+002 1.2e+003 4.7e+004 -9.59e-001 -1.196377261e+005 4.636685652e+000  3.8e-001 0.16  
3   2.9e+002 3.9e+002 1.5e+004 -9.21e-001 -1.106361529e+005 2.012612674e+001  1.3e-001 0.17  
4   2.9e+002 3.8e+002 1.5e+004 -7.71e-001 -1.084204318e+005 1.961777053e+003  1.3e-001 0.20  
5   1.2e+002 1.6e+002 6.3e+003 -7.61e-001 -8.697391411e+004 6.281938783e+003  5.2e-002 0.22  
6   2.8e+001 3.7e+001 1.5e+003 -4.44e-001 -3.497853422e+004 1.243733738e+004  1.2e-002 0.23  
7   1.8e+001 2.4e+001 9.7e+002 4.56e-001  -2.544128492e+004 7.282435834e+003  8.0e-003 0.27  
8   1.0e+001 1.4e+001 5.4e+002 6.41e-001  -1.522165589e+004 4.310637560e+003  4.5e-003 0.28  
9   4.0e+000 5.3e+000 2.2e+002 8.13e-001  -6.144883638e+003 1.969711650e+003  1.8e-003 0.30  
10  2.1e+000 2.8e+000 1.1e+002 9.47e-001  -3.044502970e+003 1.207457923e+003  9.3e-004 0.31  
11  8.6e-001 1.1e+000 4.7e+001 9.86e-001  -1.157996544e+003 6.459955188e+002  3.9e-004 0.34  
12  8.3e-001 1.1e+000 4.5e+001 9.58e-001  -1.138132235e+003 6.183835428e+002  3.8e-004 0.36  
13  5.3e-001 7.1e-001 2.9e+001 9.71e-001  -6.888562929e+002 4.420652301e+002  2.4e-004 0.38  
14  3.5e-001 4.7e-001 1.9e+001 1.00e+000  -3.794801659e+002 3.620429880e+002  1.6e-004 0.41  
15  1.2e-001 1.8e-001 6.4e+000 9.97e-001  -3.092661659e+001 2.180453123e+002  5.4e-005 0.42  
16  8.4e-002 1.3e-001 4.7e+000 1.02e+000  2.357132243e+001  2.044237343e+002  4.0e-005 0.44  
17  5.0e-002 8.3e-002 2.8e+000 1.02e+000  8.413080953e+001  1.910325595e+002  2.4e-005 0.47  
18  1.3e-002 1.6e-001 7.4e-001 1.02e+000  1.457940947e+002  1.736490331e+002  6.2e-006 0.48  
19  4.2e-003 2.0e-001 2.4e-001 1.01e+000  1.597513290e+002  1.688127797e+002  2.0e-006 0.52  
20  2.1e-003 2.3e-001 1.2e-001 1.01e+000  1.630959323e+002  1.676537467e+002  1.0e-006 0.53  
21  6.2e-004 1.5e-001 3.8e-002 1.01e+000  1.654452793e+002  1.668584758e+002  3.2e-007 0.55  
22  4.1e-004 1.1e-001 2.5e-002 9.98e-001  1.657900985e+002  1.667152215e+002  2.1e-007 0.58  
23  2.4e-004 8.1e-002 1.5e-002 9.86e-001  1.660526906e+002  1.666096241e+002  1.3e-007 0.59  
24  2.0e-004 6.7e-002 1.2e-002 9.99e-001  1.661292060e+002  1.665838658e+002  1.0e-007 0.63  
25  1.8e-004 6.2e-002 1.1e-002 1.01e+000  1.661615251e+002  1.665704642e+002  9.5e-008 0.64  
26  1.6e-004 5.7e-002 9.9e-003 1.01e+000  1.661901237e+002  1.665580434e+002  8.5e-008 0.66  
27  1.4e-004 5.2e-002 8.9e-003 1.00e+000  1.662159550e+002  1.665470383e+002  7.7e-008 0.69  
28  1.3e-004 4.7e-002 8.0e-003 1.00e+000  1.662391076e+002  1.665370450e+002  6.9e-008 0.70  
29  1.2e-004 4.3e-002 7.2e-003 1.00e+000  1.662598912e+002  1.665280069e+002  6.2e-008 0.72  
30  1.1e-004 4.0e-002 6.5e-003 1.00e+000  1.662785451e+002  1.665198280e+002  5.6e-008 0.75  
31  9.5e-005 3.6e-002 5.8e-003 1.00e+000  1.662952889e+002  1.665124278e+002  5.0e-008 0.77  
32  8.6e-005 3.3e-002 5.2e-003 1.00e+000  1.663103185e+002  1.665057318e+002  4.5e-008 0.78  
33  7.7e-005 3.1e-002 4.7e-003 1.00e+000  1.663238098e+002  1.664996733e+002  4.1e-008 0.81  
34  6.9e-005 2.9e-002 4.2e-003 1.00e+000  1.663359208e+002  1.664941917e+002  3.7e-008 0.83  
35  6.2e-005 2.6e-002 3.8e-003 1.00e+000  1.663467931e+002  1.664892325e+002  3.3e-008 0.86  
36  5.6e-005 2.5e-002 3.4e-003 1.00e+000  1.663565542e+002  1.664847465e+002  3.0e-008 0.88  
37  5.1e-005 2.3e-002 3.1e-003 1.00e+000  1.663653183e+002  1.664806891e+002  2.7e-008 0.89  
38  4.5e-005 2.1e-002 2.8e-003 1.00e+000  1.663731880e+002  1.664770202e+002  2.4e-008 0.92  
39  4.1e-005 2.0e-002 2.5e-003 1.00e+000  1.663802551e+002  1.664737030e+002  2.2e-008 0.94  
40  3.7e-005 1.9e-002 2.3e-003 1.00e+000  1.663866022e+002  1.664707046e+002  2.0e-008 0.97  
41  3.3e-005 1.8e-002 2.0e-003 1.00e+000  1.663923029e+002  1.664679946e+002  1.8e-008 0.98  
42  3.0e-005 1.7e-002 1.8e-003 1.00e+000  1.663974236e+002  1.664655459e+002  1.6e-008 1.01  
43  2.7e-005 1.6e-002 1.6e-003 1.00e+000  1.664020235e+002  1.664633334e+002  1.4e-008 1.03  
44  2.4e-005 1.5e-002 1.5e-003 1.00e+000  1.664061559e+002  1.664613348e+002  1.3e-008 1.05  
45  2.2e-005 1.4e-002 1.3e-003 1.00e+000  1.664098685e+002  1.664595295e+002  1.2e-008 1.08  
46  2.0e-005 1.4e-002 1.2e-003 1.00e+000  1.664132041e+002  1.664578991e+002  1.0e-008 1.09  
47  1.8e-005 1.3e-002 1.1e-003 1.00e+000  1.664162012e+002  1.664564269e+002  9.4e-009 1.11  
48  1.6e-005 1.2e-002 9.7e-004 1.00e+000  1.664188943e+002  1.664550976e+002  8.4e-009 1.14  
49  1.4e-005 1.2e-002 8.8e-004 1.00e+000  1.664213144e+002  1.664538975e+002  7.6e-009 1.16  
50  1.3e-005 1.2e-002 7.9e-004 1.00e+000  1.664234893e+002  1.664528142e+002  6.8e-009 1.19  
51  1.2e-005 1.1e-002 7.1e-004 1.00e+000  1.664254439e+002  1.664518365e+002  6.1e-009 1.20  
52  1.0e-005 1.1e-002 6.4e-004 1.00e+000  1.664272007e+002  1.664509542e+002  5.5e-009 1.22  
53  9.4e-006 1.1e-002 5.7e-004 1.00e+000  1.664287798e+002  1.664501581e+002  5.0e-009 1.25  
54  8.4e-006 1.0e-002 5.2e-004 1.00e+000  1.664301992e+002  1.664494398e+002  4.5e-009 1.26  
55  7.6e-006 1.0e-002 4.7e-004 1.00e+000  1.664314752e+002  1.664487919e+002  4.0e-009 1.30  
56  6.8e-006 9.9e-003 4.2e-004 1.00e+000  1.664326224e+002  1.664482075e+002  3.6e-009 1.31  
57  6.1e-006 9.7e-003 3.8e-004 1.00e+000  1.664336538e+002  1.664476805e+002  3.3e-009 1.33  
58  5.5e-006 9.6e-003 3.4e-004 1.00e+000  1.664345810e+002  1.664472052e+002  2.9e-009 1.36  
59  5.0e-006 9.4e-003 3.1e-004 1.00e+000  1.664354148e+002  1.664467766e+002  2.6e-009 1.38  
60  4.5e-006 9.3e-003 2.7e-004 1.00e+000  1.664361645e+002  1.664463902e+002  2.4e-009 1.39  
61  4.0e-006 9.1e-003 2.5e-004 1.00e+000  1.664368385e+002  1.664460418e+002  2.1e-009 1.42  
62  3.6e-006 9.0e-003 2.2e-004 1.00e+000  1.664374446e+002  1.664457277e+002  1.9e-009 1.44  
63  3.3e-006 8.9e-003 2.0e-004 1.00e+000  1.664379896e+002  1.664454444e+002  1.7e-009 1.45  
64  2.9e-006 8.8e-003 1.8e-004 1.00e+000  1.664384797e+002  1.664451891e+002  1.6e-009 1.47  
65  2.6e-006 8.7e-003 1.6e-004 1.00e+000  1.664389205e+002  1.664449590e+002  1.4e-009 1.50  
66  2.4e-006 8.7e-003 1.5e-004 1.00e+000  1.664393169e+002  1.664447516e+002  1.3e-009 1.51  
67  2.1e-006 8.6e-003 1.3e-004 1.00e+000  1.664396735e+002  1.664445647e+002  1.1e-009 1.53  
68  1.9e-006 8.5e-003 1.2e-004 1.00e+000  1.664399942e+002  1.664443964e+002  1.0e-009 1.56  
69  1.7e-006 8.4e-003 1.1e-004 1.00e+000  1.664402828e+002  1.664442448e+002  9.2e-010 1.58  
70  1.6e-006 8.4e-003 9.6e-005 1.00e+000  1.664405424e+002  1.664441082e+002  8.3e-010 1.59  
71  1.4e-006 8.3e-003 8.6e-005 1.00e+000  1.664407759e+002  1.664439852e+002  7.5e-010 1.63  
72  1.3e-006 8.3e-003 7.8e-005 1.00e+000  1.664409860e+002  1.664438744e+002  6.7e-010 1.64  
73  1.1e-006 8.2e-003 7.0e-005 1.00e+000  1.664411750e+002  1.664437746e+002  6.1e-010 1.66  
74  1.0e-006 8.2e-003 6.3e-005 1.00e+000  1.664413451e+002  1.664436847e+002  5.5e-010 1.69  
75  9.2e-007 8.1e-003 5.7e-005 1.00e+000  1.664414981e+002  1.664436038e+002  4.9e-010 1.70  
76  8.3e-007 8.1e-003 5.1e-005 1.00e+000  1.664416357e+002  1.664435308e+002  4.4e-010 1.73  
77  7.5e-007 8.1e-003 4.6e-005 1.00e+000  1.664417595e+002  1.664434652e+002  4.0e-010 1.75  
78  6.7e-007 8.0e-003 4.1e-005 1.00e+000  1.664418709e+002  1.664434060e+002  3.6e-010 1.76  
79  6.1e-007 8.0e-003 3.7e-005 1.00e+000  1.664419711e+002  1.664433527e+002  3.2e-010 1.80  
80  5.4e-007 8.0e-003 3.3e-005 1.00e+000  1.664420613e+002  1.664433047e+002  2.9e-010 1.81  
81  4.9e-007 7.9e-003 3.0e-005 1.00e+000  1.664421423e+002  1.664432615e+002  2.6e-010 1.84  
82  4.4e-007 7.9e-003 2.7e-005 1.00e+000  1.664422153e+002  1.664432225e+002  2.3e-010 1.86  
83  4.0e-007 7.9e-003 2.4e-005 1.00e+000  1.664422809e+002  1.664431874e+002  2.1e-010 1.89  
84  3.6e-007 7.9e-003 2.2e-005 1.00e+000  1.664423399e+002  1.664431558e+002  1.9e-010 1.91  
85  3.2e-007 7.8e-003 2.0e-005 1.00e+000  1.664423930e+002  1.664431273e+002  1.7e-010 1.94  
86  2.9e-007 7.8e-003 1.8e-005 1.00e+000  1.664424408e+002  1.664431017e+002  1.5e-010 1.97  
87  2.6e-007 7.8e-003 1.6e-005 1.00e+000  1.664424838e+002  1.664430786e+002  1.4e-010 1.98  
88  2.3e-007 7.8e-003 1.4e-005 1.00e+000  1.664425226e+002  1.664430579e+002  1.2e-010 2.02  
89  2.1e-007 7.8e-003 1.3e-005 1.00e+000  1.664425574e+002  1.664430392e+002  1.1e-010 2.03  
90  1.9e-007 7.7e-003 1.2e-005 1.00e+000  1.664425887e+002  1.664430224e+002  1.0e-010 2.06  
91  1.7e-007 7.7e-003 1.0e-005 1.00e+000  1.664426169e+002  1.664430072e+002  9.1e-011 2.08  
92  1.5e-007 7.7e-003 9.4e-006 1.00e+000  1.664426423e+002  1.664429936e+002  8.2e-011 2.11  
93  1.4e-007 7.7e-003 8.5e-006 1.00e+000  1.664426652e+002  1.664429813e+002  7.4e-011 2.13  
94  1.2e-007 7.7e-003 7.6e-006 1.00e+000  1.664426858e+002  1.664429703e+002  6.6e-011 2.16  
95  1.1e-007 7.7e-003 6.9e-006 1.00e+000  1.664427043e+002  1.664429603e+002  6.0e-011 2.17  
96  1.0e-007 7.7e-003 6.2e-006 1.00e+000  1.664427209e+002  1.664429514e+002  5.4e-011 2.19  
97  9.1e-008 7.6e-003 5.6e-006 1.00e+000  1.664427359e+002  1.664429434e+002  4.8e-011 2.22  
98  8.2e-008 7.6e-003 5.0e-006 9.99e-001  1.664427494e+002  1.664429362e+002  4.4e-011 2.23  
99  7.4e-008 7.6e-003 4.5e-006 1.00e+000  1.664427616e+002  1.664429296e+002  3.9e-011 2.27  
100 6.6e-008 7.6e-003 4.1e-006 9.99e-001  1.664427725e+002  1.664429238e+002  3.5e-011 2.28  
101 6.0e-008 7.6e-003 3.7e-006 1.00e+000  1.664427824e+002  1.664429185e+002  3.2e-011 2.31  
102 5.4e-008 7.6e-003 3.3e-006 1.00e+000  1.664427912e+002  1.664429138e+002  2.9e-011 2.33  
103 4.8e-008 7.6e-003 3.0e-006 1.00e+000  1.664427992e+002  1.664429095e+002  2.6e-011 2.34  
104 4.3e-008 7.6e-003 2.7e-006 1.00e+000  1.664428064e+002  1.664429056e+002  2.3e-011 2.38  
105 3.9e-008 7.6e-003 2.4e-006 1.00e+000  1.664428128e+002  1.664429022e+002  2.1e-011 2.39  
106 3.5e-008 7.6e-003 2.2e-006 1.00e+000  1.664428186e+002  1.664428990e+002  1.9e-011 2.42  
107 3.2e-008 7.6e-003 1.9e-006 1.00e+000  1.664428239e+002  1.664428962e+002  1.7e-011 2.44  
108 2.9e-008 6.8e-003 1.8e-006 1.00e+000  1.664428286e+002  1.664428937e+002  1.5e-011 2.47  
109 2.6e-008 6.1e-003 1.6e-006 1.00e+000  1.664428328e+002  1.664428914e+002  1.4e-011 2.48  
110 2.3e-008 5.5e-003 1.4e-006 1.00e+000  1.664428366e+002  1.664428894e+002  1.2e-011 2.52  
111 2.1e-008 5.0e-003 1.3e-006 1.00e+000  1.664428401e+002  1.664428875e+002  1.1e-011 2.53  
112 1.9e-008 4.5e-003 1.1e-006 9.99e-001  1.664428432e+002  1.664428859e+002  1.0e-011 2.55  
113 1.7e-008 4.0e-003 1.0e-006 1.00e+000  1.664428460e+002  1.664428844e+002  9.0e-012 2.58  
114 1.5e-008 3.6e-003 9.3e-007 1.00e+000  1.664428485e+002  1.664428830e+002  8.1e-012 2.59  
115 1.4e-008 3.3e-003 8.4e-007 1.01e+000  1.664428508e+002  1.664428818e+002  7.3e-012 2.63  
116 1.2e-008 2.9e-003 7.5e-007 1.00e+000  1.664428528e+002  1.664428807e+002  6.6e-012 2.64  
117 1.1e-008 2.6e-003 6.8e-007 9.98e-001  1.664428546e+002  1.664428798e+002  5.9e-012 2.66  
118 1.0e-008 2.4e-003 6.1e-007 9.99e-001  1.664428562e+002  1.664428789e+002  5.3e-012 2.69  
119 9.6e-009 2.1e-003 5.5e-007 9.67e-001  1.664428576e+002  1.664428783e+002  4.8e-012 2.70  
120 8.6e-009 1.9e-003 4.9e-007 1.02e+000  1.664428591e+002  1.664428775e+002  4.3e-012 2.73  
121 7.7e-009 1.7e-003 4.4e-007 1.02e+000  1.664428604e+002  1.664428767e+002  3.9e-012 2.75  
122 7.0e-009 1.6e-003 4.0e-007 9.80e-001  1.664428614e+002  1.664428761e+002  3.5e-012 2.78  
123 6.2e-009 1.4e-003 3.6e-007 1.00e+000  1.664428624e+002  1.664428756e+002  3.2e-012 2.80  
124 1.6e-008 1.4e-003 3.2e-007 8.48e-001  1.664428631e+002  1.664428758e+002  2.9e-012 2.83  
125 1.6e-008 1.2e-003 2.9e-007 1.04e+000  1.664428640e+002  1.664428753e+002  2.6e-012 2.84  
126 1.3e-008 1.1e-003 2.6e-007 9.47e-001  1.664428647e+002  1.664428749e+002  2.4e-012 2.88  
127 1.2e-008 1.1e-003 2.4e-007 9.06e-001  1.664428653e+002  1.664428747e+002  2.1e-012 2.89  
128 1.2e-008 9.6e-004 2.1e-007 1.07e+000  1.664428660e+002  1.664428742e+002  2.0e-012 2.92  
129 1.1e-008 8.7e-004 1.9e-007 9.13e-001  1.664428665e+002  1.664428739e+002  1.8e-012 2.94  
130 9.7e-009 7.8e-004 1.7e-007 9.77e-001  1.664428670e+002  1.664428736e+002  1.6e-012 2.97  
131 8.8e-009 7.0e-004 1.6e-007 9.99e-001  1.664428674e+002  1.664428734e+002  1.5e-012 2.98  
132 7.9e-009 6.3e-004 1.4e-007 1.01e+000  1.664428677e+002  1.664428731e+002  1.3e-012 3.02  
133 7.1e-009 5.7e-004 1.3e-007 9.96e-001  1.664428680e+002  1.664428729e+002  1.2e-012 3.03  
134 6.4e-009 5.1e-004 1.1e-007 1.03e+000  1.664428684e+002  1.664428727e+002  1.1e-012 3.06  
135 5.7e-009 4.6e-004 1.0e-007 9.62e-001  1.664428686e+002  1.664428725e+002  9.7e-013 3.08  
Interior-point optimizer terminated. Time: 3.08. 

Optimizer terminated. Time: 3.09    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6644286863e+002   nrm: 2e+001   Viol.  con: 1e-007   var: 0e+000 
  Dual.    obj: 1.6644287250e+002   nrm: 1e+003   Viol.  con: 0e+000   var: 3e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.13 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (312) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 868
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3452              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 : 1.48e+004         after factor           : 1.48e+005       
Factor     - dense dim.             : 0                 flops                  : 2.93e+007       
Factor     - GP saved nzs           : 3.33e+004         GP saved flops         : 9.12e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.226801879e+005 2.000000000e+000  1.0e+000 0.08  
1   1.7e+003 2.2e+003 8.9e+004 -9.71e-001 -1.219485528e+005 2.617414593e+000  7.3e-001 0.11  
2   8.7e+002 1.2e+003 4.7e+004 -9.59e-001 -1.196364657e+005 4.636401427e+000  3.8e-001 0.14  
3   2.9e+002 3.9e+002 1.5e+004 -9.21e-001 -1.106158286e+005 2.014129696e+001  1.3e-001 0.17  
4   2.9e+002 3.8e+002 1.5e+004 -7.70e-001 -1.083972792e+005 1.965947448e+003  1.3e-001 0.20  
5   1.2e+002 1.6e+002 6.3e+003 -7.61e-001 -8.697816667e+004 6.259175118e+003  5.2e-002 0.22  
6   2.6e+001 3.5e+001 1.4e+003 -4.45e-001 -3.295066978e+004 1.266446066e+004  1.2e-002 0.25  
7   1.7e+001 2.3e+001 9.2e+002 4.94e-001  -2.416410948e+004 7.106816742e+003  7.6e-003 0.28  
8   1.0e+001 1.3e+001 5.4e+002 6.63e-001  -1.508051712e+004 4.346566371e+003  4.5e-003 0.31  
9   4.0e+000 5.4e+000 2.2e+002 8.15e-001  -6.179967954e+003 1.982142317e+003  1.8e-003 0.34  
10  2.1e+000 2.8e+000 1.1e+002 9.46e-001  -3.054868182e+003 1.203017350e+003  9.2e-004 0.36  
11  8.4e-001 1.1e+000 4.6e+001 9.86e-001  -1.130707029e+003 6.332361926e+002  3.8e-004 0.39  
12  8.2e-001 1.1e+000 4.5e+001 9.51e-001  -1.123325353e+003 6.088012732e+002  3.7e-004 0.41  
13  5.2e-001 7.0e-001 2.8e+001 9.70e-001  -6.752902948e+002 4.367358081e+002  2.4e-004 0.44  
14  3.3e-001 4.6e-001 1.8e+001 1.00e+000  -3.600088349e+002 3.538069143e+002  1.5e-004 0.45  
15  1.1e-001 1.8e-001 6.2e+000 9.97e-001  -2.521086951e+001 2.163980822e+002  5.3e-005 0.48  
16  8.4e-002 1.4e-001 4.7e+000 1.02e+000  2.402948827e+001  2.054512383e+002  4.0e-005 0.50  
17  4.4e-002 8.3e-002 2.4e+000 1.02e+000  9.488613832e+001  1.878251676e+002  2.1e-005 0.53  
18  1.5e-002 8.5e-002 8.4e-001 1.02e+000  1.427846743e+002  1.744479100e+002  7.1e-006 0.56  
19  6.8e-003 7.5e-002 3.9e-001 1.01e+000  1.553129812e+002  1.698394498e+002  3.3e-006 0.58  
20  1.6e-003 1.6e-001 9.7e-002 1.01e+000  1.638198136e+002  1.674577497e+002  8.2e-007 0.61  
21  9.3e-004 1.1e-001 5.6e-002 9.78e-001  1.649298333e+002  1.670134668e+002  4.7e-007 0.63  
22  2.9e-004 1.1e-001 1.8e-002 9.88e-001  1.659498711e+002  1.666326685e+002  1.6e-007 0.66  
23  1.2e-004 9.3e-002 8.0e-003 1.01e+000  1.662161081e+002  1.665134991e+002  6.9e-008 0.67  
24  1.1e-004 8.6e-002 7.2e-003 1.01e+000  1.662388390e+002  1.665064963e+002  6.2e-008 0.70  
25  1.0e-004 7.8e-002 6.4e-003 1.01e+000  1.662573148e+002  1.664980817e+002  5.6e-008 0.72  
26  9.1e-005 7.1e-002 5.8e-003 1.01e+000  1.662741560e+002  1.664907768e+002  5.1e-008 0.75  
27  8.2e-005 6.4e-002 5.2e-003 1.01e+000  1.662892418e+002  1.664841392e+002  4.5e-008 0.77  
28  7.4e-005 5.9e-002 4.7e-003 1.01e+000  1.663027860e+002  1.664781428e+002  4.1e-008 0.80  
29  6.6e-005 5.4e-002 4.2e-003 1.01e+000  1.663149378e+002  1.664727157e+002  3.7e-008 0.81  
30  6.0e-005 4.9e-002 3.8e-003 1.01e+000  1.663258421e+002  1.664678058e+002  3.3e-008 0.84  
31  5.4e-005 4.5e-002 3.4e-003 1.01e+000  1.663356278e+002  1.664633648e+002  3.0e-008 0.88  
32  4.8e-005 4.1e-002 3.1e-003 1.01e+000  1.663444109e+002  1.664593492e+002  2.7e-008 0.89  
33  4.4e-005 3.8e-002 2.8e-003 1.01e+000  1.663522953e+002  1.664557191e+002  2.4e-008 0.91  
34  3.9e-005 3.5e-002 2.5e-003 1.01e+000  1.663593736e+002  1.664524382e+002  2.2e-008 0.94  
35  3.5e-005 3.2e-002 2.3e-003 1.01e+000  1.663657292e+002  1.664494735e+002  2.0e-008 0.97  
36  3.2e-005 3.0e-002 2.0e-003 1.00e+000  1.663714364e+002  1.664467950e+002  1.8e-008 0.98  
37  2.9e-005 2.7e-002 1.8e-003 1.00e+000  1.663765620e+002  1.664443755e+002  1.6e-008 1.02  
38  2.6e-005 2.5e-002 1.6e-003 1.00e+000  1.663811655e+002  1.664421903e+002  1.4e-008 1.03  
39  2.3e-005 2.4e-002 1.5e-003 1.00e+000  1.663853006e+002  1.664402169e+002  1.3e-008 1.05  
40  2.1e-005 2.2e-002 1.3e-003 1.00e+000  1.663890152e+002  1.664384351e+002  1.2e-008 1.08  
41  1.9e-005 2.1e-002 1.2e-003 1.00e+000  1.663923524e+002  1.664368263e+002  1.0e-008 1.11  
42  1.7e-005 1.9e-002 1.1e-003 1.00e+000  1.663953507e+002  1.664353741e+002  9.4e-009 1.13  
43  1.5e-005 1.8e-002 9.7e-004 1.00e+000  1.663980447e+002  1.664340633e+002  8.4e-009 1.16  
44  1.4e-005 1.7e-002 8.7e-004 1.00e+000  1.664004655e+002  1.664328802e+002  7.6e-009 1.17  
45  1.2e-005 1.6e-002 7.9e-004 1.00e+000  1.664026410e+002  1.664318126e+002  6.8e-009 1.20  
46  1.1e-005 1.6e-002 7.1e-004 1.00e+000  1.664045962e+002  1.664308494e+002  6.2e-009 1.23  
47  1.0e-005 1.5e-002 6.4e-004 1.00e+000  1.664063534e+002  1.664299803e+002  5.5e-009 1.27  
48  9.0e-006 1.4e-002 5.7e-004 1.00e+000  1.664079329e+002  1.664291963e+002  5.0e-009 1.28  
49  8.1e-006 1.4e-002 5.2e-004 1.00e+000  1.664093528e+002  1.664284892e+002  4.5e-009 1.30  
50  7.3e-006 1.3e-002 4.6e-004 1.00e+000  1.664106292e+002  1.664278516e+002  4.0e-009 1.33  
51  6.5e-006 1.2e-002 4.2e-004 1.00e+000  1.664117767e+002  1.664272765e+002  3.6e-009 1.34  
52  5.9e-006 1.2e-002 3.8e-004 1.00e+000  1.664128085e+002  1.664267580e+002  3.3e-009 1.38  
53  5.3e-006 1.2e-002 3.4e-004 1.00e+000  1.664137362e+002  1.664262906e+002  2.9e-009 1.39  
54  4.8e-006 1.1e-002 3.0e-004 1.00e+000  1.664145703e+002  1.664258692e+002  2.7e-009 1.42  
55  4.3e-006 1.1e-002 2.7e-004 1.00e+000  1.664153204e+002  1.664254893e+002  2.4e-009 1.44  
56  3.9e-006 1.1e-002 2.5e-004 1.00e+000  1.664159949e+002  1.664251468e+002  2.1e-009 1.45  
57  3.5e-006 1.0e-002 2.2e-004 1.00e+000  1.664166015e+002  1.664248381e+002  1.9e-009 1.48  
58  3.1e-006 1.0e-002 2.0e-004 1.00e+000  1.664171469e+002  1.664245599e+002  1.7e-009 1.50  
59  2.8e-006 1.0e-002 1.8e-004 1.00e+000  1.664176374e+002  1.664243091e+002  1.6e-009 1.53  
60  2.5e-006 9.8e-003 1.6e-004 1.00e+000  1.664180786e+002  1.664240831e+002  1.4e-009 1.55  
61  2.3e-006 9.7e-003 1.5e-004 1.00e+000  1.664184754e+002  1.664238794e+002  1.3e-009 1.58  
62  2.0e-006 9.5e-003 1.3e-004 1.00e+000  1.664188324e+002  1.664236960e+002  1.1e-009 1.59  
63  1.8e-006 9.4e-003 1.2e-004 1.00e+000  1.664191535e+002  1.664235308e+002  1.0e-009 1.61  
64  1.7e-006 9.2e-003 1.1e-004 1.00e+000  1.664194424e+002  1.664233820e+002  9.3e-010 1.64  
65  1.5e-006 9.1e-003 9.6e-005 1.00e+000  1.664197024e+002  1.664232480e+002  8.3e-010 1.66  
66  1.3e-006 9.0e-003 8.6e-005 1.00e+000  1.664199362e+002  1.664231273e+002  7.5e-010 1.69  
67  1.2e-006 8.9e-003 7.7e-005 1.00e+000  1.664201466e+002  1.664230186e+002  6.7e-010 1.70  
68  1.1e-006 8.8e-003 7.0e-005 1.00e+000  1.664203359e+002  1.664229207e+002  6.1e-010 1.72  
69  9.8e-007 8.7e-003 6.3e-005 1.00e+000  1.664205062e+002  1.664228326e+002  5.5e-010 1.75  
70  8.8e-007 8.6e-003 5.6e-005 1.00e+000  1.664206594e+002  1.664227532e+002  4.9e-010 1.77  
71  7.9e-007 8.6e-003 5.1e-005 1.00e+000  1.664207973e+002  1.664226816e+002  4.4e-010 1.80  
72  7.1e-007 8.5e-003 4.6e-005 1.00e+000  1.664209213e+002  1.664226172e+002  4.0e-010 1.81  
73  6.4e-007 8.4e-003 4.1e-005 1.00e+000  1.664210328e+002  1.664225592e+002  3.6e-010 1.84  
74  5.8e-007 8.4e-003 3.7e-005 1.00e+000  1.664211332e+002  1.664225069e+002  3.2e-010 1.86  
75  5.2e-007 8.3e-003 3.3e-005 1.00e+000  1.664212235e+002  1.664224598e+002  2.9e-010 1.89  
76  4.7e-007 8.3e-003 3.0e-005 1.00e+000  1.664213047e+002  1.664224174e+002  2.6e-010 1.91  
77  4.2e-007 8.2e-003 2.7e-005 1.00e+000  1.664213777e+002  1.664223792e+002  2.4e-010 1.94  
78  3.8e-007 8.2e-003 2.4e-005 1.00e+000  1.664214434e+002  1.664223448e+002  2.1e-010 1.95  
79  3.4e-007 8.1e-003 2.2e-005 1.00e+000  1.664215025e+002  1.664223137e+002  1.9e-010 1.98  
80  3.1e-007 8.1e-003 2.0e-005 1.00e+000  1.664215557e+002  1.664222858e+002  1.7e-010 2.00  
81  2.8e-007 8.1e-003 1.8e-005 1.00e+000  1.664216036e+002  1.664222606e+002  1.5e-010 2.03  
82  2.5e-007 8.0e-003 1.6e-005 1.00e+000  1.664216466e+002  1.664222380e+002  1.4e-010 2.05  
83  2.2e-007 8.0e-003 1.4e-005 1.00e+000  1.664216854e+002  1.664222176e+002  1.3e-010 2.06  
84  2.0e-007 8.0e-003 1.3e-005 1.00e+000  1.664217202e+002  1.664221992e+002  1.1e-010 2.09  
85  1.8e-007 7.9e-003 1.2e-005 1.00e+000  1.664217516e+002  1.664221827e+002  1.0e-010 2.11  
86  1.6e-007 7.9e-003 1.0e-005 1.00e+000  1.664217798e+002  1.664221678e+002  9.1e-011 2.14  
87  1.5e-007 7.9e-003 9.4e-006 1.00e+000  1.664218052e+002  1.664221544e+002  8.2e-011 2.16  
88  1.3e-007 7.9e-003 8.5e-006 1.00e+000  1.664218281e+002  1.664221424e+002  7.4e-011 2.19  
89  1.2e-007 7.9e-003 7.6e-006 1.00e+000  1.664218486e+002  1.664221315e+002  6.6e-011 2.20  
90  1.1e-007 7.1e-003 6.9e-006 1.00e+000  1.664218672e+002  1.664221216e+002  6.0e-011 2.22  
91  9.7e-008 6.4e-003 6.2e-006 1.00e+000  1.664218839e+002  1.664221128e+002  5.4e-011 2.25  
92  8.7e-008 5.7e-003 5.6e-006 1.00e+000  1.664218988e+002  1.664221049e+002  4.8e-011 2.27  
93  7.8e-008 5.2e-003 5.0e-006 1.00e+000  1.664219123e+002  1.664220978e+002  4.4e-011 2.30  
94  7.0e-008 4.6e-003 4.5e-006 1.00e+000  1.664219245e+002  1.664220914e+002  3.9e-011 2.31  
95  6.3e-008 4.2e-003 4.1e-006 1.00e+000  1.664219354e+002  1.664220856e+002  3.5e-011 2.34  
96  5.7e-008 3.8e-003 3.6e-006 1.00e+000  1.664219452e+002  1.664220804e+002  3.2e-011 2.36  
97  5.1e-008 3.4e-003 3.3e-006 1.00e+000  1.664219541e+002  1.664220758e+002  2.9e-011 2.39  
98  4.6e-008 3.0e-003 3.0e-006 9.99e-001  1.664219620e+002  1.664220715e+002  2.6e-011 2.41  
99  4.2e-008 2.7e-003 2.7e-006 1.00e+000  1.664219692e+002  1.664220678e+002  2.3e-011 2.44  
100 3.7e-008 2.5e-003 2.4e-006 1.00e+000  1.664219757e+002  1.664220644e+002  2.1e-011 2.45  
101 3.4e-008 2.2e-003 2.2e-006 1.00e+000  1.664219815e+002  1.664220613e+002  1.9e-011 2.47  
102 3.0e-008 2.0e-003 1.9e-006 9.99e-001  1.664219867e+002  1.664220585e+002  1.7e-011 2.50  
103 2.7e-008 1.8e-003 1.7e-006 9.98e-001  1.664219914e+002  1.664220560e+002  1.5e-011 2.52  
104 2.5e-008 1.6e-003 1.6e-006 9.98e-001  1.664219956e+002  1.664220538e+002  1.4e-011 2.55  
105 2.2e-008 1.5e-003 1.4e-006 1.00e+000  1.664219994e+002  1.664220518e+002  1.2e-011 2.56  
106 2.0e-008 1.3e-003 1.3e-006 9.97e-001  1.664220029e+002  1.664220500e+002  1.1e-011 2.58  
107 1.8e-008 1.2e-003 1.1e-006 9.98e-001  1.664220059e+002  1.664220484e+002  1.0e-011 2.61  
108 1.6e-008 1.1e-003 1.0e-006 1.00e+000  1.664220087e+002  1.664220469e+002  9.0e-012 2.63  
109 1.5e-008 9.5e-004 9.3e-007 1.00e+000  1.664220112e+002  1.664220456e+002  8.1e-012 2.66  
110 1.3e-008 8.6e-004 8.3e-007 9.97e-001  1.664220135e+002  1.664220444e+002  7.3e-012 2.67  
111 1.2e-008 7.7e-004 7.5e-007 1.00e+000  1.664220155e+002  1.664220433e+002  6.6e-012 2.69  
112 1.1e-008 7.0e-004 6.8e-007 1.00e+000  1.664220174e+002  1.664220423e+002  5.9e-012 2.72  
113 9.7e-009 6.3e-004 6.1e-007 1.00e+000  1.664220190e+002  1.664220415e+002  5.3e-012 2.73  
114 8.7e-009 5.6e-004 5.5e-007 1.01e+000  1.664220205e+002  1.664220406e+002  4.8e-012 2.77  
115 7.8e-009 5.1e-004 4.9e-007 9.95e-001  1.664220218e+002  1.664220399e+002  4.3e-012 2.78  
116 7.0e-009 4.6e-004 4.4e-007 1.00e+000  1.664220230e+002  1.664220393e+002  3.9e-012 2.80  
117 6.3e-009 4.1e-004 4.0e-007 9.99e-001  1.664220241e+002  1.664220387e+002  3.5e-012 2.83  
118 5.7e-009 3.7e-004 3.6e-007 1.00e+000  1.664220251e+002  1.664220382e+002  3.2e-012 2.84  
119 5.2e-009 3.3e-004 3.2e-007 1.01e+000  1.664220259e+002  1.664220378e+002  2.8e-012 2.86  
120 5.2e-009 3.0e-004 2.9e-007 9.86e-001  1.664220267e+002  1.664220374e+002  2.6e-012 2.89  
121 9.8e-009 5.7e-006 5.6e-009 7.73e-001  1.664220346e+002  1.664220348e+002  4.4e-013 2.91  
Interior-point optimizer terminated. Time: 2.91. 

Optimizer terminated. Time: 2.94    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6642203455e+002   nrm: 2e+001   Viol.  con: 4e-007   var: 0e+000 
  Dual.    obj: 1.6642203481e+002   nrm: 1e+003   Viol.  con: 0e+000   var: 5e-005 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.97 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 472
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.05    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 868
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3452              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 : 1.48e+004         after factor           : 1.48e+005       
Factor     - dense dim.             : 0                 flops                  : 2.93e+007       
Factor     - GP saved nzs           : 3.33e+004         GP saved flops         : 9.12e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.226793464e+005 2.000000000e+000  1.0e+000 0.09  
1   1.7e+003 2.2e+003 8.9e+004 -9.71e-001 -1.219475222e+005 2.617551325e+000  7.3e-001 0.13  
2   8.7e+002 1.2e+003 4.7e+004 -9.59e-001 -1.196332918e+005 4.638035495e+000  3.8e-001 0.16  
3   2.9e+002 3.9e+002 1.5e+004 -9.21e-001 -1.106010035e+005 2.015517241e+001  1.3e-001 0.19  
4   2.9e+002 3.8e+002 1.5e+004 -7.70e-001 -1.083789356e+005 1.970023149e+003  1.3e-001 0.20  
5   1.2e+002 1.6e+002 6.3e+003 -7.60e-001 -8.694904937e+004 6.250544788e+003  5.2e-002 0.22  
6   2.6e+001 3.5e+001 1.4e+003 -4.44e-001 -3.282677345e+004 1.266802161e+004  1.2e-002 0.25  
7   1.7e+001 2.3e+001 9.1e+002 4.96e-001  -2.402660040e+004 7.077439287e+003  7.5e-003 0.27  
8   9.9e+000 1.3e+001 5.3e+002 6.65e-001  -1.498800253e+004 4.322341725e+003  4.4e-003 0.28  
9   3.9e+000 5.3e+000 2.1e+002 8.16e-001  -6.094505188e+003 1.959604195e+003  1.8e-003 0.30  
10  2.0e+000 2.7e+000 1.1e+002 9.46e-001  -2.997047175e+003 1.192826209e+003  9.1e-004 0.33  
11  8.5e-001 1.1e+000 4.6e+001 9.86e-001  -1.153378430e+003 6.290976970e+002  3.9e-004 0.34  
12  8.2e-001 1.1e+000 4.5e+001 9.51e-001  -1.143155875e+003 6.042664843e+002  3.8e-004 0.36  
13  5.2e-001 7.1e-001 2.9e+001 9.70e-001  -6.817645781e+002 4.348849381e+002  2.4e-004 0.39  
14  3.3e-001 4.5e-001 1.8e+001 1.00e+000  -3.517991226e+002 3.500690488e+002  1.5e-004 0.41  
15  1.1e-001 1.8e-001 6.1e+000 9.97e-001  -2.317479485e+001 2.158838006e+002  5.2e-005 0.42  
16  8.3e-002 1.3e-001 4.6e+000 1.02e+000  2.519198500e+001  2.050142594e+002  3.9e-005 0.45  
17  4.1e-002 8.0e-002 2.3e+000 1.02e+000  9.882882516e+001  1.867924562e+002  1.9e-005 0.47  
18  1.1e-002 1.7e-001 6.3e-001 1.02e+000  1.490154947e+002  1.727744421e+002  5.3e-006 0.50  
19  3.5e-003 2.0e-001 2.0e-001 1.01e+000  1.606163004e+002  1.683314680e+002  1.7e-006 0.52  
20  1.3e-003 1.4e-001 7.9e-002 1.01e+000  1.642501142e+002  1.672313421e+002  6.8e-007 0.53  
21  8.9e-004 1.0e-001 5.3e-002 9.83e-001  1.649856280e+002  1.669612923e+002  4.5e-007 0.56  
22  2.7e-004 1.1e-001 1.7e-002 9.86e-001  1.659722667e+002  1.665936074e+002  1.4e-007 0.58  
23  9.3e-005 1.1e-001 5.9e-003 1.01e+000  1.662553702e+002  1.664752691e+002  5.2e-008 0.61  
24  3.5e-005 1.0e-001 2.3e-003 1.01e+000  1.663497958e+002  1.664339909e+002  2.0e-008 0.63  
25  1.6e-005 8.4e-002 1.1e-003 1.00e+000  1.663811885e+002  1.664201380e+002  9.3e-009 0.66  
26  1.5e-005 7.7e-002 9.5e-004 1.00e+000  1.663843952e+002  1.664194627e+002  8.4e-009 0.67  
27  1.3e-005 7.0e-002 8.5e-004 1.01e+000  1.663867462e+002  1.664183004e+002  7.6e-009 0.69  
28  1.2e-005 6.4e-002 7.7e-004 1.00e+000  1.663889017e+002  1.664172953e+002  6.8e-009 0.72  
29  1.1e-005 5.8e-002 6.9e-004 1.00e+000  1.663908327e+002  1.664163827e+002  6.1e-009 0.73  
30  9.6e-006 5.3e-002 6.2e-004 1.00e+000  1.663925692e+002  1.664155607e+002  5.5e-009 0.75  
31  8.6e-006 4.9e-002 5.6e-004 1.00e+000  1.663941299e+002  1.664148195e+002  5.0e-009 0.78  
32  7.8e-006 4.4e-002 5.0e-004 1.00e+000  1.663955331e+002  1.664141514e+002  4.5e-009 0.80  
33  7.0e-006 4.1e-002 4.5e-004 1.00e+000  1.663967946e+002  1.664135492e+002  4.0e-009 0.83  
34  6.3e-006 3.8e-002 4.1e-004 1.00e+000  1.663979288e+002  1.664130064e+002  3.6e-009 0.84  
35  5.7e-006 3.5e-002 3.7e-004 1.00e+000  1.663989486e+002  1.664125172e+002  3.3e-009 0.88  
36  5.1e-006 3.2e-002 3.3e-004 1.00e+000  1.663998657e+002  1.664120764e+002  2.9e-009 0.89  
37  4.6e-006 3.0e-002 3.0e-004 1.00e+000  1.664006904e+002  1.664116792e+002  2.6e-009 0.92  
38  4.1e-006 2.7e-002 2.7e-004 1.00e+000  1.664014320e+002  1.664113213e+002  2.4e-009 0.94  
39  3.7e-006 2.5e-002 2.4e-004 1.00e+000  1.664020990e+002  1.664109988e+002  2.1e-009 0.97  
40  3.3e-006 2.4e-002 2.2e-004 1.00e+000  1.664026987e+002  1.664107081e+002  1.9e-009 0.98  
41  3.0e-006 2.2e-002 1.9e-004 1.00e+000  1.664032381e+002  1.664104462e+002  1.7e-009 1.00  
42  2.7e-006 2.1e-002 1.8e-004 1.00e+000  1.664037232e+002  1.664102103e+002  1.6e-009 1.03  
43  2.4e-006 1.9e-002 1.6e-004 1.00e+000  1.664041596e+002  1.664099977e+002  1.4e-009 1.05  
44  2.2e-006 1.8e-002 1.4e-004 1.00e+000  1.664045521e+002  1.664098062e+002  1.3e-009 1.08  
45  2.0e-006 1.7e-002 1.3e-004 1.00e+000  1.664049053e+002  1.664096338e+002  1.1e-009 1.09  
46  1.8e-006 1.6e-002 1.2e-004 1.00e+000  1.664052230e+002  1.664094786e+002  1.0e-009 1.11  
47  1.6e-006 1.5e-002 1.0e-004 1.00e+000  1.664055088e+002  1.664093387e+002  9.2e-010 1.14  
48  1.4e-006 1.5e-002 9.3e-005 1.00e+000  1.664057660e+002  1.664092128e+002  8.3e-010 1.16  
49  1.3e-006 1.4e-002 8.4e-005 1.00e+000  1.664059974e+002  1.664090995e+002  7.5e-010 1.19  
50  1.2e-006 1.3e-002 7.6e-005 1.00e+000  1.664062055e+002  1.664089974e+002  6.7e-010 1.20  
51  1.0e-006 1.3e-002 6.8e-005 1.00e+000  1.664063928e+002  1.664089054e+002  6.0e-010 1.22  
52  9.4e-007 1.2e-002 6.1e-005 1.00e+000  1.664065613e+002  1.664088227e+002  5.4e-010 1.25  
53  8.5e-007 1.2e-002 5.5e-005 1.00e+000  1.664067129e+002  1.664087481e+002  4.9e-010 1.27  
54  7.6e-007 1.1e-002 5.0e-005 1.00e+000  1.664068493e+002  1.664086810e+002  4.4e-010 1.28  
55  6.9e-007 1.1e-002 4.5e-005 1.00e+000  1.664069720e+002  1.664086205e+002  4.0e-010 1.31  
56  6.2e-007 1.1e-002 4.0e-005 1.00e+000  1.664070824e+002  1.664085660e+002  3.6e-010 1.33  
57  5.6e-007 1.0e-002 3.6e-005 1.00e+000  1.664071817e+002  1.664085170e+002  3.2e-010 1.34  
58  5.0e-007 1.0e-002 3.3e-005 1.00e+000  1.664072710e+002  1.664084727e+002  2.9e-010 1.38  
59  4.5e-007 9.9e-003 2.9e-005 1.00e+000  1.664073514e+002  1.664084329e+002  2.6e-010 1.39  
60  4.1e-007 9.7e-003 2.6e-005 1.00e+000  1.664074236e+002  1.664083970e+002  2.3e-010 1.42  
61  3.7e-007 9.5e-003 2.4e-005 1.00e+000  1.664074886e+002  1.664083647e+002  2.1e-010 1.44  
62  3.3e-007 9.3e-003 2.1e-005 1.00e+000  1.664075471e+002  1.664083356e+002  1.9e-010 1.47  
63  3.0e-007 9.2e-003 1.9e-005 1.00e+000  1.664075997e+002  1.664083093e+002  1.7e-010 1.48  
64  2.7e-007 9.0e-003 1.7e-005 1.00e+000  1.664076471e+002  1.664082857e+002  1.5e-010 1.52  
65  2.4e-007 8.9e-003 1.6e-005 1.00e+000  1.664076896e+002  1.664082644e+002  1.4e-010 1.53  
66  2.2e-007 8.8e-003 1.4e-005 1.00e+000  1.664077280e+002  1.664082452e+002  1.2e-010 1.55  
67  1.9e-007 8.7e-003 1.3e-005 1.00e+000  1.664077624e+002  1.664082280e+002  1.1e-010 1.58  
68  1.7e-007 8.6e-003 1.1e-005 1.00e+000  1.664077935e+002  1.664082125e+002  1.0e-010 1.59  
69  1.6e-007 8.5e-003 1.0e-005 1.00e+000  1.664078214e+002  1.664081985e+002  9.1e-011 1.63  
70  1.4e-007 8.4e-003 9.2e-006 1.00e+000  1.664078465e+002  1.664081859e+002  8.2e-011 1.64  
71  1.3e-007 8.3e-003 8.3e-006 1.00e+000  1.664078691e+002  1.664081745e+002  7.4e-011 1.67  
72  1.1e-007 8.3e-003 7.4e-006 1.00e+000  1.664078895e+002  1.664081644e+002  6.6e-011 1.69  
73  1.0e-007 8.2e-003 6.7e-006 1.00e+000  1.664079078e+002  1.664081552e+002  6.0e-011 1.70  
74  9.3e-008 8.1e-003 6.0e-006 1.00e+000  1.664079242e+002  1.664081469e+002  5.4e-011 1.73  
75  8.4e-008 8.1e-003 5.4e-006 1.00e+000  1.664079391e+002  1.664081395e+002  4.8e-011 1.75  
76  7.5e-008 8.0e-003 4.9e-006 9.99e-001  1.664079524e+002  1.664081327e+002  4.3e-011 1.78  
77  6.8e-008 8.0e-003 4.4e-006 1.00e+000  1.664079644e+002  1.664081267e+002  3.9e-011 1.80  
78  6.1e-008 8.0e-003 4.0e-006 9.99e-001  1.664079752e+002  1.664081213e+002  3.5e-011 1.83  
79  5.5e-008 7.9e-003 3.6e-006 1.00e+000  1.664079849e+002  1.664081164e+002  3.2e-011 1.84  
80  4.9e-008 7.9e-003 3.2e-006 1.00e+000  1.664079937e+002  1.664081120e+002  2.9e-011 1.86  
81  4.4e-008 7.9e-003 2.9e-006 1.00e+000  1.664080016e+002  1.664081081e+002  2.6e-011 1.89  
82  4.0e-008 7.8e-003 2.6e-006 1.00e+000  1.664080087e+002  1.664081045e+002  2.3e-011 1.91  
83  3.6e-008 7.8e-003 2.3e-006 1.00e+000  1.664080151e+002  1.664081012e+002  2.1e-011 1.92  
84  3.2e-008 7.8e-003 2.1e-006 1.00e+000  1.664080208e+002  1.664080983e+002  1.9e-011 1.95  
85  2.9e-008 7.8e-003 1.9e-006 1.00e+000  1.664080260e+002  1.664080957e+002  1.7e-011 1.97  
86  2.6e-008 7.8e-003 1.7e-006 9.97e-001  1.664080306e+002  1.664080934e+002  1.5e-011 2.00  
87  2.4e-008 7.7e-003 1.5e-006 1.00e+000  1.664080348e+002  1.664080913e+002  1.4e-011 2.02  
88  2.1e-008 7.7e-003 1.4e-006 1.00e+000  1.664080385e+002  1.664080894e+002  1.2e-011 2.03  
89  1.9e-008 7.7e-003 1.2e-006 9.95e-001  1.664080419e+002  1.664080877e+002  1.1e-011 2.06  
90  1.7e-008 7.7e-003 1.1e-006 1.00e+000  1.664080450e+002  1.664080862e+002  9.9e-012 2.08  
91  1.6e-008 7.7e-003 1.0e-006 1.00e+000  1.664080477e+002  1.664080848e+002  8.9e-012 2.09  
92  1.4e-008 6.9e-003 9.0e-007 1.01e+000  1.664080503e+002  1.664080835e+002  8.1e-012 2.13  
93  1.3e-008 6.2e-003 8.1e-007 9.97e-001  1.664080525e+002  1.664080824e+002  7.3e-012 2.14  
94  1.1e-008 5.6e-003 7.3e-007 9.99e-001  1.664080545e+002  1.664080814e+002  6.5e-012 2.16  
95  1.0e-008 5.0e-003 6.6e-007 1.01e+000  1.664080563e+002  1.664080805e+002  5.9e-012 2.19  
96  9.2e-009 4.5e-003 5.9e-007 1.01e+000  1.664080580e+002  1.664080796e+002  5.3e-012 2.20  
97  8.3e-009 4.1e-003 5.3e-007 1.00e+000  1.664080594e+002  1.664080789e+002  4.8e-012 2.23  
98  7.4e-009 3.7e-003 4.8e-007 1.00e+000  1.664080607e+002  1.664080783e+002  4.3e-012 2.25  
99  6.8e-009 3.3e-003 4.3e-007 1.00e+000  1.664080619e+002  1.664080777e+002  3.9e-012 2.27  
100 6.1e-009 3.0e-003 3.9e-007 9.99e-001  1.664080629e+002  1.664080771e+002  3.5e-012 2.30  
101 5.5e-009 2.7e-003 3.5e-007 9.94e-001  1.664080639e+002  1.664080767e+002  3.2e-012 2.31  
102 4.9e-009 2.4e-003 3.2e-007 9.96e-001  1.664080647e+002  1.664080763e+002  2.8e-012 2.34  
103 5.0e-009 2.2e-003 2.8e-007 1.03e+000  1.664080656e+002  1.664080757e+002  2.6e-012 2.36  
104 4.4e-009 2.0e-003 2.6e-007 1.00e+000  1.664080663e+002  1.664080753e+002  2.3e-012 2.38  
105 4.1e-009 1.8e-003 2.3e-007 9.88e-001  1.664080669e+002  1.664080750e+002  2.1e-012 2.41  
106 3.6e-009 1.6e-003 2.1e-007 9.88e-001  1.664080675e+002  1.664080747e+002  1.9e-012 2.42  
107 3.3e-009 1.4e-003 1.9e-007 1.00e+000  1.664080680e+002  1.664080745e+002  1.7e-012 2.45  
108 2.9e-009 1.3e-003 1.7e-007 9.97e-001  1.664080684e+002  1.664080743e+002  1.5e-012 2.47  
109 2.6e-009 1.2e-003 1.5e-007 1.00e+000  1.664080688e+002  1.664080741e+002  1.4e-012 2.50  
110 2.4e-009 1.0e-003 1.4e-007 1.00e+000  1.664080692e+002  1.664080739e+002  1.2e-012 2.52  
111 2.1e-009 9.3e-004 1.2e-007 9.98e-001  1.664080695e+002  1.664080738e+002  1.1e-012 2.55  
112 1.9e-009 8.4e-004 1.1e-007 9.89e-001  1.664080698e+002  1.664080736e+002  1.0e-012 2.56  
113 1.7e-009 7.6e-004 9.9e-008 1.01e+000  1.664080701e+002  1.664080735e+002  9.1e-013 2.59  
Interior-point optimizer terminated. Time: 2.59. 

Optimizer terminated. Time: 2.61    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6640807005e+002   nrm: 2e+001   Viol.  con: 2e-008   var: 0e+000 
  Dual.    obj: 1.6640807349e+002   nrm: 1e+003   Viol.  con: 0e+000   var: 5e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.63 seconds.
Solving took 9 GP solves and 48.3 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: 1.4957417539192265e+110 vs 1.49570075379e+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

WEIGHT DIFFERENCES


Total Fuel Weight Percent Diff: [-92.94682932]


Total Aircraft Weight Percent Diff: [-21.48045673]


Engine Weight Percent Diff: -56.277768457037375


Fuselage Weight Percent Diff: -0.869702823500253


Payload Weight Percent Diff: [-0.04003553]


VT Weight Percent Diff: -8.6071426906855


HT Weight Percent Diff: -93.23323850050295


Wing Weight Percent Diff: 8.2676262686229




WING DIFFERENCES


Wing Span Percent Diff: -0.029997852700332565


Wing Area Percent Diff: 32.89994603486249




HORIZONTAL TAIL DIFFERENCES


HT Area Percent Diff: 40.489192479635626




VERTICAL TAIL DIFFERENCES




VT Span Percent Diff: -11.022229397058116


VT Area Percent Diff: -60.386736768091644




CRUISE SEGMENT 1 DRAG DIFFERENCES


Overall Cd Percent Diff: [-18.54744239]


L/D Percent Diff: [24.01023011]


Nacelle Cd Percent Diff: [-94.27639763]


HT Cd Percent Diff: [-80.76936069] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-58.00286276] dimensionless


Wing Cd percent Diff: [-14.22940233]
Induced Drag Cd Percent Diff: [1.21899649]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-90.57037122]




FUSELAGE DIFFERENCES




Weight of HB material: -38.359021299529935 


Weight of VB material: 87.82995488726316 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.71260575]
Mission1
========

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

Constraints
-----------
   W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin}
   PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:])
   x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:])
   x_{CG}[3] <= \Delta x_n + x_n
   \Delta x_m + x_{CG}[3] >= x_m
   \tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m
   C_{D_{fuse}}[:] = 0.018081
   M_{fuseD} = 0.72
   W_{start}[0] = W_{total}[:]
   W_{start}[:] >= W_{end}[:] + W_{burn}[:]
   W_{start}[1:] = W_{end}[:4]
   W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1]
   W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2]
   W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1]
   hft[2] >= CruiseAlt
   hft[1:5] = hft[:4] + dhft[1:5]
   hft[0] = dhft[0]
   dhft[1:3] = dhft[:2]
   RC[0] >= 2.5e+03
   RC[:3] >= RC_{min}[:3]
   \theta[2] >= 0.015
   hft[2] >= MinCruiseAlt
   n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:]
   R_{segment}[3:4] = R_{segment}[4:5]
   M[3:5] >= M_{min}
   0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req}
   Fsafetyfac*F[0] = T_e
   W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:]
   V_2[:] = M_2[:]*a[:]
   \alpha_{max,w}[:3] = 0.18
   \alpha_{max,w}[3:] = 0.1
   0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime
   0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime
   ClimbTime <= MaxClimbTime
   T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}}
   F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   OPR[:] <= OPR_{max}
 
 Aircraft
     Fuselage
       W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on}
       W_{pass}[:] >= n_{pass}[:]*W_{avg. pass}
       W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo}
       W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}}
       W_{payload}[:] <= W_{payload_{max}}
       n_{pass}[:] <= n_{seat}
       n_{rows} = n_{seat}/SPR
       l_{shell} = n_{rows}*p_s
       \theta_{db} = w_{db}/R_{fuse}
       R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db}
       A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db}
       (PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse}
       A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin}
       w_{floor} = w_{fuse}
       R_{fuse} + w_{db} >= w_{fuse}
       h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse}
       t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell}
       S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2
       S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2
       l_{fuse} = l_{nose} + l_{shell} + l_{cone}
       l_{cone} = R_{fuse}/\lambda_{cone}
       x_{shell1} = l_{nose}
       x_{shell2} >= l_{nose} + l_{shell}
       t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin}
       t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin}
       \sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell})
       \sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin}
       l_{floor} >= l_{shell} + 2*R_{fuse}
       P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat})
       A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor}
       V_{floor} = 2*w_{floor}*A_{floor}
       W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor}
       \tau_{cone} = \sigma_{skin}
       W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame})
       x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone}
       -2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}}
       (PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}}
       x_{hbend_{Land}} >= x_{wing}
       x_{hbend_{Land}} <= l_{fuse}
       x_{hbend_{MLF}} >= x_{wing}
       x_{hbend_{MLF}} <= l_{fuse}
       A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}})
       A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}})
       A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
       A_{2h_{MLF}} >= Mission1.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
       A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2)
       A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}}
       A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}}
       A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}}
       A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}}
       A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}}
       A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}}
       A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}}
       A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}}
       V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}}
       W_{hbend} >= g*\rho_{bend}*V_{hbend}
       x_{vbend} >= x_{wing}
       x_{vbend} <= l_{fuse}
       B_{0v} = B_{1v}*(x_{tail} - x_{vbend})
       B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2)
       B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}}
       0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}}
       V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}}
       W_{vbend} >= \rho_{bend}*g*V_{vbend}
       x_f = x_{wing} + 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       x_b = x_{wing} - 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h}
       \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v}
       V_{cyl} = A_{skin}*l_{shell}
       V_{nose} = S_{nose}*t_{skin}
       V_{bulk} = S_{bulk}*t_{skin}
       V_{db} = A_{db}*l_{shell}
       V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse})
       W_{apu} = W_{payload_{max}}*f_{apu}
       W_{db} = \rho_{skin}*g*V_{db}
       W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk})
       W_{window} >= W'_{window}*l_{shell}
       W_{padd} = W_{payload_{max}}*f_{padd}
       W_{seat} >= W'_{seat}*n_{seat}
       W_{seat} >= f_{seat}*W_{payload_{max}}
       W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk})
       W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db}
       W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone})
     
     Wing
       WingNoStruct
         A_{rect} = c_{tip}*b
         0.5*(1 - \lambda)*c_{root}*b <= A_{tri}
         p >= 1 + 2*\lambda
         2*q >= 1 + p
         y_{mac} = b/3*q/p
         mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q
         \lambda = c_{tip}/c_{root}
         S = b*(c_{root} + c_{tip})/2
         0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w)
         e*(1 + f(\lambda_w)*AR) <= 1
         \lambda >= 0.15
         V_{fuel, max} <= 0.303*mac^2*b*\tau
         W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g
         b <= b_{max}
       
       WingBox
         AR = b^2/S
         0.423*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5)
         \tau <= \tau_{max_w}
         W_{struct} >= W_{web} + W_{cap}
         AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5)
         Mission1.Aircraft.Wing.WingBox.N_{lift} = 3
         Mission1.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8
         \lambda = taper
         W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt})
         0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}}
     
     Engine
         Compressor
           (no constraints)
         
         Combustor
           (no constraints)
         
         Turbine
           (no constraints)
         
         Thrust
           (no constraints)
         
         FanMap
           (no constraints)
         
         LPCMap
           (no constraints)
         
         HPCMap
           (no constraints)
         
         Sizing
           A_{2} >= A_{5} + A_{7}
         
         FlightState
             V[:] = V[:]
             a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
             V[:] = M[:]*a[:]
           
           Altitude
             h[:] = hft[:]
           
           Atmosphere
             (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
             \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
             T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
             \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
         
         EnginePerformance
           CompressorPerformance
               T_{t_0}[:] = T_{atm}[:]/c1[:]^-1
               h_{t_0}[:] = C_{p_{air}*T_{t_0}[:]
               P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:]
               T_{t_{1.8}}[:] = T_{t_0}[:]
               h_{t_{1.8}}[:] = h_{t_0}[:]
               P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5
               T_{T_{2}}[:] = T_{t_{1.8}}[:]
               h_{T_{2}}[:] = h_{t_{1.8}}[:]
               P_{T_{2}}[:] = P_{t_{1.8}}[:]
               P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:]
               T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016
               h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:]
               P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:]
               T_{t_7}[:] = T_{t_{2.1}}[:]
               h_{t_7}[:] = h_{t_{2.1}}[:]
               P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:]
               T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152
               h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1}
               P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:]
               T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491
               h_{t_3}[:] = C_{p_{2}*T_{t_3}[:]
           
           CombustorPerformance
             h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:]
             h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:]
             fp1[:] = f[:] + 1
             M_{4a}[:] = 0.1025
             fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5
             T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]]
             P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891
             u_{4a}[:] = M_{4a}[:]*(1.31*Mission1.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a}
             u_c[:] = r_{uc}*u_{4a}[:]
             P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891
           
           TurbinePerformance
             h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:]
             P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:]
             \pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565
             h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:]
             P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:]
             T_{t_5}[:] = T_{t_{4.9}}[:]
             h_{t_5}[:] = h_{t_{4.9}}[:]
           
           ThrustPerformance
             P_{8}[:] = P_{atm}[:]
             h_{8}[:] = C_{p_{fex}*T_{8}[:]
             u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:]
             (P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:]
             h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:]
             P_{6}[:] = P_{atm}[:]
             (P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:]
             u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:]
             h_6[:] = C_{p_{tex}*T_{6}[:]
             h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:]
             \alpha[:] = m_{fan}[:]/m_{core}[:]
             \alpha_{+1}[:] = \alpha[:] + 1
             \alpha[:] <= \alpha_{max}
             F[:] <= F_{6}[:] + F_{8}[:]
             F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:])
             TSFC[:] = 1/I_{sp}[:]
             F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:]
           
           FanMapPerformance
             m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}}
           
           LPCMapPerformance
             m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D}
           
           HPCMapPerformance
             m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D}
           
           SizingPerformance
             P_{7}[:] >= P_{atm}[:]
             M_7[:] <= 1
             a_{7}[:] = (1.4*Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5
             a_{7}[:]*M_7[:] = u_{7}[:]
             \rho_7[:] = P_{7}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])
             P_{5}[:] >= P_{atm}[:]
             M_5[:] <= 1
             a_{5}[:] = (1.39*Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5
             a_{5}[:]*M_5[:] = u_{5}[:]
             \rho_5[:] = P_{5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])
             h_{2}[:] = C_{p_{1}*T_{2}[:]
             \rho_{2}[:] = P_{2}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:])
             u_{2}[:] = M_2[:]*(C_{p_{1}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:]/781)^0.5
             h_{2.5}[:] = C_{p_{2}*T_{2.5}[:]
             \rho_{2.5}[:] = P_{2.5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:])
             u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/781)^0.5
         m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine}
           d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5
           d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5
           \eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]])
           h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:]
           P_{t_4}[:] = \pi_{b}*P_{t_3}[:]
           M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]]
           M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]])
           P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:]
           \pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013
           \pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10
           \pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10
           \pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10
           m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
           \pi_{f}[:] >= 1
           \pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10
           \pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10
           \pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10
           \pi_{lc}[:] >= 1
           m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
           \pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10
           \pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10
           \pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10
           m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref})
           \pi_{hc}[:] >= 1
         OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:]
           P_{t_8}[:] = P_{t_7}[:]
           T_{t_8}[:] = T_{t_7}[:]
           P_{t_6}[:] = P_{t_5}[:]
           T_{t_6}[:] = T_{t_5}[:]
           F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:]
           I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g)
           N_{f}[:]*G_{f} = N_{1}[:]
           N_{1}[:] <= 1.1
           N_{2}[:] <= 1.1
         fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD}
         fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD}
           P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5
           (T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2
           P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979
           (T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2
           M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:]
           m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:]
           m_{total}[:] = m_{fan}[:] + m_{core}[:]
           P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512
           T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1
           m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2}
           P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857
           T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1
           m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5}
           1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD}
           0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD}
           1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD}
           0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD}
           m_{lc_D} >= 0.7*m_{coreD}/0.649
           m_{lc_D} <= 1.3*m_{coreD}/0.649
           m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23
           m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23
           \bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405
           \bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405
           F[:] = F_{spec}[:]
           T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}}
           OPR[:] <= OPR_{max}
     
     VerticalTail
       VerticalTailNoStruct
         C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}}
         L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}}
         c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt}))
         A_{vt} = b_{vt}^2/S_{vt}
         b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt}
         p_{vt} >= 1 + 2*\lambda_{vt}
         2*q_{vt} >= 1 + p_{vt}
         y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
         z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
         0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt}
         \lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}}
         \Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}}
         \Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt}
         \lambda_{vt} >= 0.25
         V_{vt} >= V_{vt_{min}}
       
       WingBox
         AR_{vt} = (2*b_{vt})^2/(2*S_{vt})
         0.423*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
         \tau_{vt} <= 0.14
         W_{struct} >= 0.5*(W_{web} + W_{cap})
         Mission1.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24
         AR_{vt}*2*L_{vt_{max}}*Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
         Mission1.Aircraft.VerticalTail.WingBox.N_{lift} = 1
         Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*Mission1.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8
         \lambda_{vt} = taper
         W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT})
     
     HorizontalTail
       HorizontalTailNoStruct
         \Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht}
         \Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}}
         p_{ht} >= 1 + 2*\lambda_{ht}
         2*q_{ht} >= 1 + p_{ht}
         y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht}
         0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht}
         \lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}}
         S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2
         0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht})
         e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1
         AR_{ht} = b_{ht}^2/S_{ht}
         \lambda_{ht} >= 0.2
         \lambda_{ht} <= 1
       
       WingBox
         AR_{ht} = b_{ht}^2/S_{ht}
         0.423*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
         \tau_{ht} <= 0.14
         W_{struct} >= W_{web} + W_{cap}
         L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2
         L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht})
         2*AR_{ht}*L_{shear}*Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
         Mission1.Aircraft.HorizontalTail.WingBox.N_{lift} = 1
         Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission1.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8
         L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht}
         L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}}
         W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht})
     
     LandingGear
       l_n + z_{wing} + y_m*\tan(\gamma) >= l_m
       T = 2*y_m
       x_m >= x_n + B
       x_n >= 5
       \tan(\phi) = \tan(\phi_{min})
       (z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1
       \tan(\psi) <= \tan(\psi_{max})
       x_{up} - x_m <= l_m/\tan(\theta_{max})
       y_m >= l_m
       S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG})
       l_{oleo} = 2.5*S_{sa}
       d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5
       l_m >= l_{oleo} + d_{t_m}/2
       F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in])
       W_{wa,m} = 1.2*F_{w_m}^0.609
       F_{w_n} = L_{w_n}*d_{t_n}/1e+03
       W_{wa,n} = 1.2*F_{w_n}^0.609
       L_{w_m} = L_m/(n_{mg}*n_{wps})
       L_{w_n} = L_n/n_{wps}
       d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315
       w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48
       d_{t_n} = 0.8*d_{t_m}
       w_{t_n} = 0.8*w_{t_m}
       W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g
       N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m
       W_{mw} = n_{wps}*W_{wa,m}
       W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g
       \sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}})
       W_{nw} >= n_{wps}*W_{wa,n}
       L_m <= 9.87*E*I_m/(K*l_m)^2
       I_m = PI*r_m^3*t_m
       L_n <= 9.87*E*I_n/(K*l_n)^2
       I_n = PI*r_n^3*t_n
       2*r_m/t_m <= 40
       2*r_m/t_n <= 40
       h_{hold} >= 2*w_{t_m} + 2*r_m
       0.8 >= 2*w_{t_n} + 2*r_n
       W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m}))
       W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n})
       W_{lg} >= C_{lg}*(W_{mg} + W_{ng})
       W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m
       x_m >= x_{CG_{lg}}
     c_{root} = c_0
     Mission1.Aircraft.Wing.WingBox.r_{w/c} = Mission1.Aircraft.Fuselage.r_{w/c}
     x_w = x_{wing}
     Mission1.Aircraft.Fuselage.N_{lift} = Mission1.Aircraft.Wing.WingBox.N_{lift}
     f_{L_{total/wing}}*L_{max} >= Mission1.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}}
     W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc}
     W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
     W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
     W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:]
     W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:]
     W_{total}[:] <= W_{total, max}
     f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}}
     W_{misc} >= W_{lg} + W_{hpesys}
     W_{hpesys} = f_{hpesys}*W_{total, max}
     x_n <= l_{nose}
     x_m >= x_{wing}
     \Delta x_{AC_{wing}} + x_{wing} >= x_m
     x_{hpesys} = 1.1*l_{nose}
     x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys}
     d_{nacelle} >= d_{f} + 2*t_{nacelle}
     E_{land} >= W_{total, max}/(2*g)*w_{ult}^2
     x_{up} = x_{shell2}
     L_n = W_{total, max}*\Delta x_m/B
     L_m = W_{total, max}*\Delta x_n/B
     L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max}
     y_{eng} >= y_m
     3*n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}}
     V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse}
     W_{tail} >= n_{vt}*W_{vt} + W_{ht}
     2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db}
     B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v})
     m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht}
     x_{CG_{ht}} <= l_{fuse}
     V_{ht} = S_{ht}*l_{ht}/(S*mac)
     L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}}
     L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}}
     x_{CG_{vt}} <= l_{fuse}
     V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b)
     n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max}
     n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng}
     D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}}
     I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:]
     I_{z}[:] <= I_{z, max}
     S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2
     l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}}
     f_{S_{nacelle}} = S_{nacelle}*S^-1
     A_{inlet} = 0.4*S_{nacelle}
     A_{fancowl} = 0.2*S_{nacelle}
     A_{exh} = 0.4*S_{nacelle}
     A_{corecowl} = 3PI*d_{LPC}^2
       W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl})
       W_{eadd} = f_{eadd}*W_{engine}
     W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon}
     W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine})
     y_{eng} = 0.5*w_{fuse}
     (L_{max} - Mission1.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission1.Aircraft.Wing.WingBox.M_r*c_{root}
     A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend})
     A_{1h_{MLF}} >= (Mission1.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h})
     I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16)
     I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81
     I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81)
     x_{shell2} + l_{cone} >= x_{eng}
     x_{eng} >= x_{shell2} + 0.75*l_{cone}
     S_{floor} = 0.312*P_{floor}
     M_{floor} = 0.0352*P_{floor}*w_{floor}
     \Delta R_{fuse} = R_{fuse}*0.43/1.75
     b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2
     b_{ht_{out}} = 0.5*b_{ht} - w_{fuse}
     L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}}
     M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}}
     L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}}
     c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach}
     \pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht})
 
 FlightSegment
   FlightState
       V[:] = V[:]
       a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
       V[:] = M[:]*a[:]
     
     Altitude
       h[:] = hft[:]
     
     Atmosphere
       (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
       \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
       T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
       \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
   
   FlightP
     P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:]
     RC[:] = P_{excess}[:]/W_{avg}[:]
     \theta[:]*V[:] = RC[:]
     dhft[:] = tmin[:]*RC[:]
     R_{segment}[:] = thr[:]*V[:]
       WingPerformance
         0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:]
         \Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:]
         \Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2
         (AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2
         C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:]
         \alpha_w[:] <= \alpha_{max,w}[:]
         D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:]
         C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:]
         C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR)
         Re_w[:] = \rho[:]*V[:]*mac/\mu[:]
         C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114
       
       FuselagePerformance
         (no constraints)
       
       VerticalTailPerformance
         D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:]
         Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:]
         C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577
       
       HorizontalTailPerformance
         L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:]
         C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:]
         \alpha_{ht}[:] <= \alpha_{ht,max}
         C_{L_{\alpha,ht_0}}[:] = 6.28
         D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:]
         C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht})
         Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:]
         C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852
       W_{burn}[:] = W_{burn}[:]
       F_{fuel}[:] = F_{fuel}[:]
       \rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:])
       P_{cabin}[:] = 7.5e+04
       T_{cabin}[:] = 297
       V[:] >= V_{stall}[:]
       W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:]
       tmin[:] = thr[:]
       L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:]
       L_{total}[:] = f_{L_{total/wing}}*L_w[:]
       L_{total}[:] >= W_{avg}[:] + L_{ht}[:]
       D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2
       D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:])
       C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S)
       L/D[:] = W_{avg}[:]/D[:]
       W_{Load}[:] <= W_{Load_{max}}[:]
       W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S
       p_{o}[:] >= L_w[:]*c_{root}/S
       \eta_{o}[:] = w_{fuse}/(b/2)
       x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:]
       c_{m_{w}}[:] = 1.9
       x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2)
       x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse}
       x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}}
       x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}}
       C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht}
       AR_{ht} >= 4
       C_{L_{ht}}[:] >= 0.01
       SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac
       SM[:] >= SM_{min}
       SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}}
       x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:]
       R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:]
       C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2
       V_{nacelle}[:] = r_{v_{nacelle}}*V[:]
       V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]]
       r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0)
       C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0
       D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S
       \Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}}
   M_2[:3] = M[:3]
   M_{2.5}[:3] = 0.6
   hold_{2}[:3] = 1.07164
   hold_{2.5}[:3] = 1.06372
   P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:]
   c1[:] = 1 + 0.201*M[:]^2.0
   M_2[3:] = M[3:]
   M_{2.5}[3:] = 0.6
   hold_{2}[3:] = 1.07164
   hold_{2.5}[3:] = 1.06372
Beginning signomial solve.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.02    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 869
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3451              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.48e+004         after factor           : 1.46e+005       
Factor     - dense dim.             : 0                 flops                  : 2.87e+007       
Factor     - GP saved nzs           : 3.32e+004         GP saved flops         : 9.06e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.2e+005 0.00e+000  -1.224940108e+005 2.000000000e+000  1.0e+000 0.06  
1   1.6e+003 2.1e+003 8.4e+004 -9.71e-001 -1.216116943e+005 2.766603376e+000  6.9e-001 0.08  
2   8.2e+002 1.1e+003 4.4e+004 -9.57e-001 -1.191567559e+005 5.074629256e+000  3.6e-001 0.11  
3   2.9e+002 3.9e+002 1.6e+004 -9.16e-001 -1.104285966e+005 2.156321042e+001  1.3e-001 0.13  
4   2.9e+002 3.9e+002 1.6e+004 -7.68e-001 -1.084694817e+005 1.724066982e+003  1.3e-001 0.16  
5   1.1e+002 1.5e+002 6.0e+003 -7.59e-001 -8.491241754e+004 6.645584441e+003  4.9e-002 0.17  
6   3.8e+001 5.0e+001 2.0e+003 -4.14e-001 -4.569721752e+004 1.064008602e+004  1.7e-002 0.20  
7   2.0e+001 2.7e+001 1.1e+003 2.50e-001  -2.851392658e+004 6.956951010e+003  9.0e-003 0.22  
8   9.4e+000 1.2e+001 5.0e+002 5.70e-001  -1.400586088e+004 4.219068590e+003  4.2e-003 0.25  
9   4.7e+000 6.3e+000 2.6e+002 8.27e-001  -7.040645343e+003 2.497942694e+003  2.1e-003 0.27  
10  1.4e+000 1.9e+000 7.8e+001 9.33e-001  -2.011591950e+003 9.403827672e+002  6.4e-004 0.28  
11  6.4e-001 8.5e-001 3.5e+001 9.93e-001  -6.796564304e+002 6.596896968e+002  2.9e-004 0.31  
12  4.8e-001 6.4e-001 2.6e+001 9.96e-001  -4.512245086e+002 5.573058292e+002  2.2e-004 0.33  
13  3.5e-001 7.3e-001 1.9e+001 9.80e-001  -2.681666129e+002 4.735665754e+002  1.6e-004 0.34  
14  1.7e-001 3.6e-001 9.5e+000 9.96e-001  -1.492700781e+000 3.632401846e+002  7.9e-005 0.38  
15  5.7e-002 1.5e-001 3.2e+000 9.94e-001  1.664296823e+002  2.900324402e+002  2.7e-005 0.39  
16  3.3e-002 1.3e-001 1.9e+000 1.00e+000  2.025936912e+002  2.744117059e+002  1.6e-005 0.41  
17  5.1e-003 1.9e-001 3.2e-001 1.00e+000  2.450141520e+002  2.572047198e+002  2.8e-006 0.44  
18  1.5e-003 1.3e-001 9.4e-002 1.00e+000  2.510878635e+002  2.546831567e+002  8.5e-007 0.45  
19  4.8e-004 1.1e-001 3.1e-002 1.00e+000  2.528341318e+002  2.540184841e+002  2.8e-007 0.48  
20  2.1e-004 8.8e-002 1.3e-002 1.00e+000  2.533178434e+002  2.538309261e+002  1.2e-007 0.50  
21  1.9e-004 8.0e-002 1.2e-002 1.00e+000  2.533559246e+002  2.538177109e+002  1.1e-007 0.52  
22  1.7e-004 7.3e-002 1.1e-002 1.00e+000  2.533891273e+002  2.538047106e+002  9.9e-008 0.55  
23  1.5e-004 6.6e-002 9.8e-003 1.00e+000  2.534190446e+002  2.537930533e+002  9.0e-008 0.56  
24  1.4e-004 6.0e-002 8.8e-003 1.00e+000  2.534459451e+002  2.537825390e+002  8.1e-008 0.59  
25  1.2e-004 5.5e-002 7.9e-003 1.00e+000  2.534701386e+002  2.537730615e+002  7.3e-008 0.61  
26  1.1e-004 5.0e-002 7.1e-003 1.00e+000  2.534918966e+002  2.537645177e+002  6.5e-008 0.64  
27  1.0e-004 4.6e-002 6.4e-003 1.00e+000  2.535114665e+002  2.537568176e+002  5.9e-008 0.66  
28  9.0e-005 4.2e-002 5.8e-003 1.00e+000  2.535290693e+002  2.537498787e+002  5.3e-008 0.67  
29  8.1e-005 3.9e-002 5.2e-003 1.00e+000  2.535449033e+002  2.537436266e+002  4.8e-008 0.70  
30  7.3e-005 3.6e-002 4.7e-003 1.00e+000  2.535591471e+002  2.537379938e+002  4.3e-008 0.72  
31  6.6e-005 3.3e-002 4.2e-003 1.00e+000  2.535719607e+002  2.537329193e+002  3.9e-008 0.75  
32  5.9e-005 3.0e-002 3.8e-003 1.00e+000  2.535834881e+002  2.537283480e+002  3.5e-008 0.77  
33  5.3e-005 2.8e-002 3.4e-003 1.00e+000  2.535938586e+002  2.537242304e+002  3.1e-008 0.80  
34  4.8e-005 2.6e-002 3.1e-003 1.00e+000  2.536031886e+002  2.537205215e+002  2.8e-008 0.81  
35  4.3e-005 2.4e-002 2.8e-003 1.00e+000  2.536115826e+002  2.537171809e+002  2.5e-008 0.84  
36  3.9e-005 2.2e-002 2.5e-003 1.00e+000  2.536191347e+002  2.537141721e+002  2.3e-008 0.86  
37  3.5e-005 2.1e-002 2.2e-003 1.00e+000  2.536259295e+002  2.537114623e+002  2.0e-008 0.89  
38  3.1e-005 2.0e-002 2.0e-003 1.00e+000  2.536320430e+002  2.537090219e+002  1.8e-008 0.91  
39  2.8e-005 1.8e-002 1.8e-003 1.00e+000  2.536375436e+002  2.537068241e+002  1.7e-008 0.94  
40  2.5e-005 1.7e-002 1.6e-003 1.00e+000  2.536424928e+002  2.537048450e+002  1.5e-008 0.95  
41  2.3e-005 1.6e-002 1.5e-003 1.00e+000  2.536469461e+002  2.537030627e+002  1.3e-008 0.97  
42  2.1e-005 1.6e-002 1.3e-003 1.00e+000  2.536509531e+002  2.537014579e+002  1.2e-008 1.00  
43  1.9e-005 1.5e-002 1.2e-003 1.00e+000  2.536545587e+002  2.537000129e+002  1.1e-008 1.02  
44  1.7e-005 1.4e-002 1.1e-003 1.00e+000  2.536578031e+002  2.536987118e+002  9.8e-009 1.05  
45  1.5e-005 1.3e-002 9.6e-004 1.00e+000  2.536607226e+002  2.536975404e+002  8.8e-009 1.06  
46  1.3e-005 1.3e-002 8.7e-004 1.00e+000  2.536633497e+002  2.536964857e+002  7.9e-009 1.09  
47  1.2e-005 1.2e-002 7.8e-004 1.00e+000  2.536657138e+002  2.536955361e+002  7.1e-009 1.11  
48  1.1e-005 1.2e-002 7.0e-004 1.00e+000  2.536678412e+002  2.536946813e+002  6.4e-009 1.13  
49  9.8e-006 1.1e-002 6.3e-004 1.00e+000  2.536697556e+002  2.536939118e+002  5.8e-009 1.16  
50  8.9e-006 1.1e-002 5.7e-004 1.00e+000  2.536714784e+002  2.536932190e+002  5.2e-009 1.17  
51  8.0e-006 1.1e-002 5.1e-004 1.00e+000  2.536730288e+002  2.536925954e+002  4.7e-009 1.20  
52  7.2e-006 1.0e-002 4.6e-004 1.00e+000  2.536744241e+002  2.536920340e+002  4.2e-009 1.22  
53  6.5e-006 1.0e-002 4.1e-004 1.00e+000  2.536756797e+002  2.536915286e+002  3.8e-009 1.23  
54  5.8e-006 9.8e-003 3.7e-004 1.00e+000  2.536768097e+002  2.536910737e+002  3.4e-009 1.27  
55  5.2e-006 9.6e-003 3.4e-004 1.00e+000  2.536778266e+002  2.536906643e+002  3.1e-009 1.28  
56  4.7e-006 9.4e-003 3.0e-004 1.00e+000  2.536787417e+002  2.536902957e+002  2.8e-009 1.31  
57  4.2e-006 9.2e-003 2.7e-004 1.00e+000  2.536795653e+002  2.536899639e+002  2.5e-009 1.33  
58  3.8e-006 9.0e-003 2.4e-004 1.00e+000  2.536803064e+002  2.536896652e+002  2.2e-009 1.36  
59  3.4e-006 8.9e-003 2.2e-004 1.00e+000  2.536809734e+002  2.536893963e+002  2.0e-009 1.38  
60  3.1e-006 8.8e-003 2.0e-004 1.00e+000  2.536815737e+002  2.536891543e+002  1.8e-009 1.41  
61  1.2e-006 3.4e-003 7.7e-005 1.00e+000  2.536848864e+002  2.536878176e+002  7.0e-010 1.42  
62  1.1e-006 3.0e-003 6.9e-005 1.00e+000  2.536850957e+002  2.536877339e+002  6.3e-010 1.44  
63  3.8e-007 1.1e-003 2.5e-005 1.00e+000  2.536863015e+002  2.536872470e+002  2.3e-010 1.47  
64  3.5e-007 9.8e-004 2.2e-005 1.00e+000  2.536863689e+002  2.536872198e+002  2.0e-010 1.48  
65  3.1e-007 8.8e-004 2.0e-005 1.00e+000  2.536864295e+002  2.536871953e+002  1.8e-010 1.50  
66  2.8e-007 7.9e-004 1.8e-005 1.00e+000  2.536864840e+002  2.536871733e+002  1.7e-010 1.53  
67  2.5e-007 7.1e-004 1.6e-005 1.00e+000  2.536865331e+002  2.536871534e+002  1.5e-010 1.55  
68  2.3e-007 6.4e-004 1.5e-005 1.00e+000  2.536865772e+002  2.536871356e+002  1.3e-010 1.58  
69  2.0e-007 5.8e-004 1.3e-005 1.00e+000  2.536866170e+002  2.536871195e+002  1.2e-010 1.59  
70  1.8e-007 5.2e-004 1.2e-005 1.00e+000  2.536866528e+002  2.536871050e+002  1.1e-010 1.61  
71  1.7e-007 4.7e-004 1.1e-005 1.00e+000  2.536866850e+002  2.536870920e+002  9.8e-011 1.64  
72  1.5e-007 4.2e-004 9.6e-006 1.00e+000  2.536867140e+002  2.536870803e+002  8.8e-011 1.66  
73  1.3e-007 3.8e-004 8.6e-006 1.00e+000  2.536867400e+002  2.536870697e+002  7.9e-011 1.67  
74  1.2e-007 3.4e-004 7.8e-006 1.00e+000  2.536867635e+002  2.536870602e+002  7.1e-011 1.70  
75  1.1e-007 3.1e-004 7.0e-006 1.00e+000  2.536867846e+002  2.536870517e+002  6.4e-011 1.72  
76  9.8e-008 2.8e-004 6.3e-006 1.00e+000  2.536868036e+002  2.536870440e+002  5.8e-011 1.75  
77  8.8e-008 2.5e-004 5.7e-006 1.00e+000  2.536868207e+002  2.536870371e+002  5.2e-011 1.77  
78  7.9e-008 2.2e-004 5.1e-006 1.00e+000  2.536868361e+002  2.536870308e+002  4.7e-011 1.78  
79  7.1e-008 2.0e-004 4.6e-006 1.00e+000  2.536868500e+002  2.536870252e+002  4.2e-011 1.81  
80  6.4e-008 1.8e-004 4.1e-006 1.00e+000  2.536868625e+002  2.536870202e+002  3.8e-011 1.83  
81  5.8e-008 1.6e-004 3.7e-006 1.00e+000  2.536868737e+002  2.536870156e+002  3.4e-011 1.86  
82  5.2e-008 1.5e-004 3.3e-006 1.00e+000  2.536868838e+002  2.536870115e+002  3.1e-011 1.88  
83  4.7e-008 1.3e-004 3.0e-006 1.00e+000  2.536868929e+002  2.536870078e+002  2.8e-011 1.89  
84  4.2e-008 1.2e-004 2.7e-006 1.00e+000  2.536869010e+002  2.536870045e+002  2.5e-011 1.92  
85  3.8e-008 1.1e-004 2.4e-006 1.00e+000  2.536869084e+002  2.536870015e+002  2.2e-011 1.94  
86  3.4e-008 9.7e-005 2.2e-006 1.00e+000  2.536869150e+002  2.536869988e+002  2.0e-011 1.95  
87  3.1e-008 8.7e-005 2.0e-006 1.00e+000  2.536869210e+002  2.536869964e+002  1.8e-011 1.98  
88  2.8e-008 7.8e-005 1.8e-006 9.99e-001  2.536869264e+002  2.536869943e+002  1.6e-011 2.00  
89  2.5e-008 7.0e-005 1.6e-006 1.00e+000  2.536869312e+002  2.536869923e+002  1.5e-011 2.02  
90  2.2e-008 6.3e-005 1.4e-006 1.00e+000  2.536869355e+002  2.536869905e+002  1.3e-011 2.05  
91  2.0e-008 5.7e-005 1.3e-006 1.00e+000  2.536869394e+002  2.536869889e+002  1.2e-011 2.06  
92  1.8e-008 5.1e-005 1.2e-006 1.00e+000  2.536869430e+002  2.536869875e+002  1.1e-011 2.09  
93  1.6e-008 4.6e-005 1.0e-006 1.00e+000  2.536869461e+002  2.536869862e+002  9.6e-012 2.11  
94  1.5e-008 4.2e-005 9.4e-007 1.00e+000  2.536869490e+002  2.536869851e+002  8.6e-012 2.13  
95  1.3e-008 3.7e-005 8.5e-007 1.00e+000  2.536869516e+002  2.536869840e+002  7.8e-012 2.16  
96  1.2e-008 3.4e-005 7.6e-007 9.99e-001  2.536869539e+002  2.536869831e+002  7.0e-012 2.17  
97  1.1e-008 3.0e-005 6.9e-007 1.00e+000  2.536869559e+002  2.536869822e+002  6.3e-012 2.20  
Interior-point optimizer terminated. Time: 2.20. 

Optimizer terminated. Time: 2.22    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 2.5368695594e+002   nrm: 4e+001   Viol.  con: 2e-007   var: 0e+000 
  Dual.    obj: 2.5368698224e+002   nrm: 8e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.25 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.05    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 870
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3453              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 : 1.48e+004         after factor           : 1.47e+005       
Factor     - dense dim.             : 0                 flops                  : 2.89e+007       
Factor     - GP saved nzs           : 3.32e+004         GP saved flops         : 9.06e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.2e+005 0.00e+000  -1.221561281e+005 2.000000000e+000  1.0e+000 0.11  
1   1.6e+003 2.1e+003 8.5e+004 -9.71e-001 -1.212978652e+005 2.752982256e+000  6.9e-001 0.14  
2   7.8e+002 1.0e+003 4.2e+004 -9.57e-001 -1.185504083e+005 5.334628806e+000  3.4e-001 0.19  
3   2.9e+002 3.9e+002 1.6e+004 -9.11e-001 -1.101594684e+005 2.219951840e+001  1.3e-001 0.20  
4   2.9e+002 3.9e+002 1.6e+004 -7.68e-001 -1.082604777e+005 1.672822298e+003  1.3e-001 0.23  
5   1.2e+002 1.6e+002 6.6e+003 -7.60e-001 -8.744006606e+004 6.083271602e+003  5.4e-002 0.27  
6   3.9e+001 5.2e+001 2.1e+003 -4.56e-001 -4.674489084e+004 1.085261406e+004  1.7e-002 0.28  
7   2.3e+001 3.0e+001 1.2e+003 2.29e-001  -3.111491303e+004 7.216069316e+003  1.0e-002 0.31  
8   9.3e+000 1.2e+001 5.0e+002 5.24e-001  -1.392423929e+004 3.980816117e+003  4.1e-003 0.34  
9   6.0e+000 7.9e+000 3.2e+002 8.27e-001  -9.002854354e+003 2.812640292e+003  2.7e-003 0.36  
10  2.1e+000 2.8e+000 1.1e+002 9.04e-001  -3.054862730e+003 1.183594141e+003  9.3e-004 0.39  
11  1.4e+000 1.9e+000 7.7e+001 9.76e-001  -1.995669605e+003 9.332734266e+002  6.4e-004 0.41  
12  7.4e-001 1.0e+000 4.0e+001 9.81e-001  -9.691540617e+002 5.758460567e+002  3.3e-004 0.44  
13  4.2e-001 7.1e-001 2.3e+001 9.89e-001  -4.601097558e+002 4.178441756e+002  1.9e-004 0.47  
14  1.6e-001 2.8e-001 8.7e+000 9.97e-001  -6.497666230e+001 2.680748454e+002  7.3e-005 0.48  
15  8.8e-002 1.6e-001 4.9e+000 1.00e+000  3.934544604e+001  2.264489933e+002  4.1e-005 0.53  
16  3.1e-002 1.2e-001 1.7e+000 1.00e+000  1.252794418e+002  1.912670963e+002  1.5e-005 0.56  
17  1.1e-002 9.8e-002 6.5e-001 1.01e+000  1.548216650e+002  1.794829027e+002  5.6e-006 0.59  
18  6.0e-003 7.7e-002 3.5e-001 1.01e+000  1.628975305e+002  1.761823713e+002  3.0e-006 0.63  
19  1.1e-003 1.5e-001 6.7e-002 1.01e+000  1.705549197e+002  1.731199396e+002  6.0e-007 0.64  
20  4.2e-004 1.1e-001 2.6e-002 1.01e+000  1.716972368e+002  1.726832676e+002  2.4e-007 0.67  
21  1.8e-004 9.1e-002 1.1e-002 1.00e+000  1.721012347e+002  1.725269235e+002  1.0e-007 0.69  
22  1.0e-004 7.2e-002 6.3e-003 1.00e+000  1.722344270e+002  1.724717684e+002  5.7e-008 0.72  
23  9.0e-005 6.5e-002 5.6e-003 1.00e+000  1.722521544e+002  1.724657980e+002  5.1e-008 0.73  
24  8.1e-005 6.0e-002 5.1e-003 1.00e+000  1.722674355e+002  1.724597078e+002  4.6e-008 0.77  
25  7.3e-005 5.5e-002 4.6e-003 1.00e+000  1.722812819e+002  1.724543221e+002  4.2e-008 0.80  
26  6.6e-005 5.0e-002 4.1e-003 1.00e+000  1.722937136e+002  1.724494457e+002  3.7e-008 0.83  
27  5.9e-005 4.6e-002 3.7e-003 1.00e+000  1.723048900e+002  1.724450453e+002  3.4e-008 0.86  
28  5.3e-005 4.2e-002 3.3e-003 1.00e+000  1.723149329e+002  1.724410697e+002  3.0e-008 0.89  
29  4.8e-005 3.9e-002 3.0e-003 1.00e+000  1.723239572e+002  1.724374779e+002  2.7e-008 0.91  
30  4.3e-005 3.6e-002 2.7e-003 1.00e+000  1.723320657e+002  1.724342323e+002  2.5e-008 0.94  
31  3.9e-005 3.3e-002 2.4e-003 1.00e+000  1.723393515e+002  1.724312996e+002  2.2e-008 0.95  
32  3.5e-005 3.0e-002 2.2e-003 1.00e+000  1.723458983e+002  1.724286503e+002  2.0e-008 0.97  
33  3.1e-005 2.8e-002 2.0e-003 1.00e+000  1.723517817e+002  1.724262574e+002  1.8e-008 1.00  
34  2.8e-005 2.6e-002 1.8e-003 1.00e+000  1.723570697e+002  1.724240969e+002  1.6e-008 1.03  
35  2.5e-005 2.5e-002 1.6e-003 1.00e+000  1.723618230e+002  1.724221468e+002  1.5e-008 1.05  
36  2.3e-005 2.3e-002 1.4e-003 1.00e+000  1.723660963e+002  1.724203871e+002  1.3e-008 1.08  
37  2.1e-005 2.1e-002 1.3e-003 1.00e+000  1.723699383e+002  1.724187996e+002  1.2e-008 1.11  
38  1.9e-005 2.0e-002 1.2e-003 1.00e+000  1.723733929e+002  1.724173678e+002  1.1e-008 1.13  
39  1.7e-005 1.9e-002 1.0e-003 1.00e+000  1.723764994e+002  1.724160766e+002  9.5e-009 1.16  
40  1.5e-005 1.8e-002 9.4e-004 1.00e+000  1.723792931e+002  1.724149123e+002  8.6e-009 1.17  
41  1.4e-005 1.7e-002 8.5e-004 1.00e+000  1.723818055e+002  1.724138628e+002  7.7e-009 1.20  
42  1.2e-005 1.6e-002 7.6e-004 1.00e+000  1.723840652e+002  1.724129167e+002  6.9e-009 1.22  
43  1.1e-005 1.5e-002 6.9e-004 1.00e+000  1.723860977e+002  1.724120639e+002  6.2e-009 1.25  
44  9.9e-006 1.4e-002 6.2e-004 1.00e+000  1.723879258e+002  1.724112954e+002  5.6e-009 1.27  
45  8.9e-006 1.4e-002 5.6e-004 1.00e+000  1.723895702e+002  1.724106028e+002  5.1e-009 1.30  
46  8.0e-006 1.3e-002 5.0e-004 1.00e+000  1.723910494e+002  1.724099788e+002  4.6e-009 1.31  
47  7.2e-006 1.3e-002 4.5e-004 1.00e+000  1.723923801e+002  1.724094166e+002  4.1e-009 1.34  
48  6.5e-006 1.2e-002 4.1e-004 1.00e+000  1.723935772e+002  1.724089100e+002  3.7e-009 1.36  
49  5.8e-006 1.2e-002 3.6e-004 1.00e+000  1.723946541e+002  1.724084537e+002  3.3e-009 1.39  
50  5.2e-006 1.1e-002 3.3e-004 1.00e+000  1.723956230e+002  1.724080427e+002  3.0e-009 1.41  
51  4.7e-006 1.1e-002 3.0e-004 1.00e+000  1.723964947e+002  1.724076724e+002  2.7e-009 1.44  
52  4.2e-006 1.1e-002 2.7e-004 1.00e+000  1.723972790e+002  1.724073389e+002  2.4e-009 1.45  
53  3.8e-006 1.0e-002 2.4e-004 1.00e+000  1.723979846e+002  1.724070386e+002  2.2e-009 1.49  
54  3.4e-006 1.0e-002 2.2e-004 1.00e+000  1.723986195e+002  1.724067681e+002  2.0e-009 1.50  
55  3.1e-006 9.9e-003 1.9e-004 1.00e+000  1.723991907e+002  1.724065245e+002  1.8e-009 1.53  
56  2.8e-006 9.7e-003 1.7e-004 1.00e+000  1.723997047e+002  1.724063051e+002  1.6e-009 1.55  
57  2.5e-006 9.5e-003 1.6e-004 1.00e+000  1.724001672e+002  1.724061076e+002  1.4e-009 1.58  
58  2.3e-006 9.3e-003 1.4e-004 1.00e+000  1.724005833e+002  1.724059297e+002  1.3e-009 1.59  
59  2.0e-006 9.2e-003 1.3e-004 1.00e+000  1.724009577e+002  1.724057696e+002  1.2e-009 1.63  
60  1.8e-006 9.0e-003 1.1e-004 1.00e+000  1.724012947e+002  1.724056253e+002  1.0e-009 1.66  
61  1.6e-006 8.9e-003 1.0e-004 1.00e+000  1.724015979e+002  1.724054955e+002  9.4e-010 1.67  
62  1.5e-006 8.8e-003 9.3e-005 1.00e+000  1.724018707e+002  1.724053786e+002  8.4e-010 1.70  
63  1.3e-006 8.7e-003 8.3e-005 1.00e+000  1.724021162e+002  1.724052733e+002  7.6e-010 1.72  
64  1.2e-006 8.6e-003 7.5e-005 1.00e+000  1.724023371e+002  1.724051785e+002  6.8e-010 1.75  
65  1.1e-006 8.5e-003 6.8e-005 1.00e+000  1.724025359e+002  1.724050931e+002  6.2e-010 1.77  
66  9.7e-007 8.4e-003 6.1e-005 1.00e+000  1.724027148e+002  1.724050163e+002  5.5e-010 1.80  
67  8.7e-007 8.3e-003 5.5e-005 1.00e+000  1.724028757e+002  1.724049471e+002  5.0e-010 1.81  
68  7.9e-007 8.3e-003 4.9e-005 1.00e+000  1.724030206e+002  1.724048848e+002  4.5e-010 1.84  
69  7.1e-007 8.2e-003 4.4e-005 1.00e+000  1.724031509e+002  1.724048288e+002  4.0e-010 1.86  
70  6.4e-007 8.1e-003 4.0e-005 1.00e+000  1.724032682e+002  1.724047783e+002  3.6e-010 1.88  
71  5.7e-007 8.1e-003 3.6e-005 1.00e+000  1.724033737e+002  1.724047328e+002  3.3e-010 1.91  
72  5.2e-007 8.0e-003 3.2e-005 1.00e+000  1.724034687e+002  1.724046919e+002  2.9e-010 1.92  
73  4.6e-007 8.0e-003 2.9e-005 1.00e+000  1.724035542e+002  1.724046551e+002  2.6e-010 1.95  
74  4.2e-007 7.9e-003 2.6e-005 1.00e+000  1.724036311e+002  1.724046219e+002  2.4e-010 1.97  
75  3.8e-007 7.9e-003 2.4e-005 1.00e+000  1.724037003e+002  1.724045920e+002  2.1e-010 1.99  
76  3.4e-007 7.9e-003 2.1e-005 1.00e+000  1.724037626e+002  1.724045652e+002  1.9e-010 2.02  
77  3.0e-007 7.8e-003 1.9e-005 1.00e+000  1.724038186e+002  1.724045410e+002  1.7e-010 2.03  
78  2.7e-007 7.8e-003 1.7e-005 1.00e+000  1.724038691e+002  1.724045192e+002  1.6e-010 2.06  
79  2.5e-007 7.8e-003 1.5e-005 1.00e+000  1.724039145e+002  1.724044996e+002  1.4e-010 2.08  
80  2.2e-007 7.7e-003 1.4e-005 1.00e+000  1.724039553e+002  1.724044819e+002  1.3e-010 2.09  
81  2.0e-007 7.7e-003 1.3e-005 1.00e+000  1.724039921e+002  1.724044660e+002  1.1e-010 2.13  
82  1.8e-007 7.7e-003 1.1e-005 1.00e+000  1.724040251e+002  1.724044517e+002  1.0e-010 2.14  
83  1.6e-007 7.7e-003 1.0e-005 1.00e+000  1.724040549e+002  1.724044388e+002  9.2e-011 2.17  
84  1.5e-007 7.7e-003 9.1e-006 1.00e+000  1.724040817e+002  1.724044271e+002  8.3e-011 2.19  
85  1.3e-007 7.6e-003 8.2e-006 9.99e-001  1.724041058e+002  1.724044167e+002  7.5e-011 2.20  
86  1.2e-007 7.6e-003 7.4e-006 9.97e-001  1.724041275e+002  1.724044073e+002  6.7e-011 2.23  
87  1.1e-007 7.6e-003 6.7e-006 9.99e-001  1.724041470e+002  1.724043988e+002  6.1e-011 2.25  
88  9.6e-008 7.6e-003 6.0e-006 1.00e+000  1.724041646e+002  1.724043913e+002  5.5e-011 2.28  
89  8.6e-008 7.5e-003 5.4e-006 9.97e-001  1.724041804e+002  1.724043844e+002  4.9e-011 2.30  
90  7.8e-008 6.8e-003 4.9e-006 1.00e+000  1.724041947e+002  1.724043782e+002  4.4e-011 2.33  
91  7.0e-008 6.1e-003 4.4e-006 9.97e-001  1.724042075e+002  1.724043725e+002  4.0e-011 2.34  
92  6.3e-008 5.5e-003 3.9e-006 1.02e+000  1.724042198e+002  1.724043672e+002  3.6e-011 2.36  
93  5.7e-008 5.0e-003 3.5e-006 9.99e-001  1.724042301e+002  1.724043627e+002  3.2e-011 2.39  
94  5.1e-008 4.5e-003 3.2e-006 9.97e-001  1.724042393e+002  1.724043587e+002  2.9e-011 2.41  
95  4.6e-008 4.0e-003 2.9e-006 9.84e-001  1.724042476e+002  1.724043551e+002  2.6e-011 2.44  
96  4.1e-008 3.6e-003 2.6e-006 1.02e+000  1.724042558e+002  1.724043515e+002  2.4e-011 2.45  
97  3.7e-008 3.2e-003 2.3e-006 1.02e+000  1.724042631e+002  1.724043483e+002  2.2e-011 2.48  
98  3.4e-008 2.9e-003 2.1e-006 1.01e+000  1.724042692e+002  1.724043456e+002  2.0e-011 2.50  
99  3.1e-008 2.6e-003 1.9e-006 9.80e-001  1.724042745e+002  1.724043433e+002  1.8e-011 2.53  
100 2.8e-008 2.4e-003 1.7e-006 1.05e+000  1.724042803e+002  1.724043410e+002  1.6e-011 2.55  
101 8.0e-008 5.7e-004 4.1e-007 9.09e-001  1.724043115e+002  1.724043253e+002  3.2e-012 2.56  
102 1.6e-007 5.6e-004 2.1e-007 1.00e+000  1.724043180e+002  1.724043253e+002  3.1e-012 2.59  
103 1.6e-007 5.6e-004 2.1e-007 1.00e+000  1.724043180e+002  1.724043253e+002  3.1e-012 2.61  
Interior-point optimizer terminated. Time: 2.61. 

Optimizer terminated. Time: 2.64    
solsta = 8, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : NEAR_OPTIMAL
  Primal.  obj: 1.7240431800e+002   nrm: 4e+001   Viol.  con: 4e-006   var: 0e+000 
  Dual.    obj: 1.7240432526e+002   nrm: 8e+002   Viol.  con: 0e+000   var: 4e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.65 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 870
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3453              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 : 1.48e+004         after factor           : 1.47e+005       
Factor     - dense dim.             : 0                 flops                  : 2.89e+007       
Factor     - GP saved nzs           : 3.32e+004         GP saved flops         : 9.06e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.2e+005 0.00e+000  -1.223637184e+005 2.000000000e+000  1.0e+000 0.11  
1   1.6e+003 2.2e+003 8.8e+004 -9.71e-001 -1.215967808e+005 2.651772494e+000  7.2e-001 0.13  
2   8.4e+002 1.1e+003 4.5e+004 -9.59e-001 -1.191448781e+005 4.832349680e+000  3.7e-001 0.16  
3   2.9e+002 3.9e+002 1.6e+004 -9.18e-001 -1.103945992e+005 2.042686551e+001  1.3e-001 0.19  
4   2.9e+002 3.9e+002 1.6e+004 -7.70e-001 -1.083023424e+005 1.844868228e+003  1.3e-001 0.22  
5   1.2e+002 1.6e+002 6.6e+003 -7.61e-001 -8.791556502e+004 6.054839798e+003  5.4e-002 0.23  
6   4.4e+001 5.8e+001 2.3e+003 -4.61e-001 -5.101708789e+004 1.028633272e+004  1.9e-002 0.27  
7   2.6e+001 3.4e+001 1.4e+003 1.61e-001  -3.519361174e+004 7.240899593e+003  1.1e-002 0.28  
8   1.3e+001 1.7e+001 6.9e+002 4.61e-001  -1.921647038e+004 4.626290561e+003  5.7e-003 0.31  
9   4.5e+000 6.0e+000 2.4e+002 7.41e-001  -6.880765256e+003 2.210470680e+003  2.0e-003 0.33  
10  3.1e+000 4.1e+000 1.7e+002 9.38e-001  -4.631423648e+003 1.676632184e+003  1.4e-003 0.34  
11  1.1e+000 1.4e+000 5.9e+001 9.65e-001  -1.539476274e+003 7.012203882e+002  4.9e-004 0.38  
12  8.8e-001 1.2e+000 4.7e+001 9.86e-001  -1.197505589e+003 6.195578478e+002  4.0e-004 0.39  
13  7.0e-001 1.0e+000 3.8e+001 9.67e-001  -9.471282503e+002 5.295124596e+002  3.2e-004 0.42  
14  3.6e-001 5.2e-001 2.0e+001 9.89e-001  -3.846483045e+002 3.804639195e+002  1.7e-004 0.44  
15  1.9e-001 2.7e-001 1.0e+001 9.96e-001  -1.312879009e+002 2.658374698e+002  8.6e-005 0.47  
16  8.8e-002 1.6e-001 4.9e+000 1.00e+000  1.803215082e+001  2.051404679e+002  4.1e-005 0.48  
17  7.9e-002 1.4e-001 4.4e+000 1.01e+000  4.002680848e+001  2.078285478e+002  3.7e-005 0.52  
18  3.0e-002 8.6e-002 1.7e+000 1.01e+000  1.183710120e+002  1.818137406e+002  1.4e-005 0.55  
19  1.2e-002 1.2e-001 6.7e-001 1.02e+000  1.484292083e+002  1.737272237e+002  5.6e-006 0.58  
20  5.3e-003 3.5e-001 3.0e-001 1.01e+000  1.582996783e+002  1.697487855e+002  2.6e-006 0.61  
21  2.1e-003 1.6e-001 1.2e-001 1.01e+000  1.636377290e+002  1.682805147e+002  1.1e-006 0.64  
22  1.4e-003 1.1e-001 8.2e-002 1.01e+000  1.648786240e+002  1.679500242e+002  7.0e-007 0.66  
23  5.7e-004 8.7e-002 3.4e-002 1.01e+000  1.662107621e+002  1.674617509e+002  2.9e-007 0.69  
24  2.8e-004 7.7e-002 1.7e-002 1.01e+000  1.666545657e+002  1.672853077e+002  1.5e-007 0.72  
25  2.6e-004 7.0e-002 1.5e-002 1.01e+000  1.667019756e+002  1.672695197e+002  1.3e-007 0.73  
26  2.3e-004 6.4e-002 1.4e-002 1.01e+000  1.667420639e+002  1.672526664e+002  1.2e-007 0.77  
27  2.1e-004 5.9e-002 1.2e-002 1.01e+000  1.667784573e+002  1.672378649e+002  1.1e-007 0.78  
28  1.9e-004 5.3e-002 1.1e-002 1.01e+000  1.668110162e+002  1.672243696e+002  9.6e-008 0.81  
29  1.7e-004 4.9e-002 1.0e-002 1.01e+000  1.668402136e+002  1.672121391e+002  8.7e-008 0.83  
30  1.5e-004 4.5e-002 9.0e-003 1.01e+000  1.668663827e+002  1.672010404e+002  7.8e-008 0.86  
31  1.4e-004 4.1e-002 8.1e-003 1.01e+000  1.668898406e+002  1.671909692e+002  7.0e-008 0.88  
32  1.2e-004 3.8e-002 7.3e-003 1.01e+000  1.669108720e+002  1.671818378e+002  6.3e-008 0.91  
33  1.1e-004 3.5e-002 6.6e-003 1.01e+000  1.669297286e+002  1.671735573e+002  5.7e-008 0.92  
34  9.9e-005 3.2e-002 5.9e-003 1.00e+000  1.669466397e+002  1.671660536e+002  5.1e-008 0.95  
35  8.9e-005 3.0e-002 5.3e-003 1.00e+000  1.669618079e+002  1.671592528e+002  4.6e-008 0.97  
36  8.0e-005 2.8e-002 4.8e-003 1.00e+000  1.669754170e+002  1.671530960e+002  4.1e-008 1.00  
37  7.2e-005 2.6e-002 4.3e-003 1.00e+000  1.669876280e+002  1.671475221e+002  3.7e-008 1.02  
38  6.5e-005 2.4e-002 3.9e-003 1.00e+000  1.669985865e+002  1.671424771e+002  3.4e-008 1.05  
39  5.9e-005 2.2e-002 3.5e-003 1.00e+000  1.670084229e+002  1.671379129e+002  3.0e-008 1.06  
40  5.3e-005 2.1e-002 3.1e-003 1.00e+000  1.670172531e+002  1.671337856e+002  2.7e-008 1.08  
41  4.7e-005 2.0e-002 2.8e-003 1.00e+000  1.670251807e+002  1.671300531e+002  2.5e-008 1.11  
42  4.3e-005 1.8e-002 2.5e-003 1.00e+000  1.670322992e+002  1.671266778e+002  2.2e-008 1.13  
43  3.8e-005 1.7e-002 2.3e-003 1.00e+000  1.670386923e+002  1.671236290e+002  2.0e-008 1.16  
44  3.5e-005 1.7e-002 2.1e-003 1.00e+000  1.670444337e+002  1.671208738e+002  1.8e-008 1.17  
45  3.1e-005 1.6e-002 1.9e-003 1.00e+000  1.670495910e+002  1.671183839e+002  1.6e-008 1.20  
46  2.8e-005 1.5e-002 1.7e-003 1.00e+000  1.670542242e+002  1.671161359e+002  1.4e-008 1.22  
47  2.5e-005 1.4e-002 1.5e-003 1.00e+000  1.670583865e+002  1.671141062e+002  1.3e-008 1.25  
48  2.3e-005 1.4e-002 1.4e-003 1.00e+000  1.670621263e+002  1.671122728e+002  1.2e-008 1.27  
49  2.0e-005 1.3e-002 1.2e-003 1.00e+000  1.670654871e+002  1.671106177e+002  1.1e-008 1.30  
50  1.8e-005 1.3e-002 1.1e-003 1.00e+000  1.670685074e+002  1.671091237e+002  9.5e-009 1.31  
51  1.7e-005 1.2e-002 9.9e-004 1.00e+000  1.670712218e+002  1.671077768e+002  8.6e-009 1.34  
52  1.5e-005 1.2e-002 8.9e-004 1.00e+000  1.670736614e+002  1.671065603e+002  7.7e-009 1.36  
53  1.3e-005 1.1e-002 8.0e-004 1.00e+000  1.670758544e+002  1.671054642e+002  6.9e-009 1.39  
54  1.2e-005 1.1e-002 7.2e-004 1.00e+000  1.670778257e+002  1.671044746e+002  6.2e-009 1.41  
55  1.1e-005 1.1e-002 6.5e-004 1.00e+000  1.670795983e+002  1.671035816e+002  5.6e-009 1.44  
56  9.8e-006 1.1e-002 5.8e-004 1.00e+000  1.670811918e+002  1.671027777e+002  5.1e-009 1.45  
57  8.8e-006 1.0e-002 5.3e-004 1.00e+000  1.670826247e+002  1.671020519e+002  4.6e-009 1.47  
58  7.9e-006 1.0e-002 4.7e-004 1.00e+000  1.670839132e+002  1.671013980e+002  4.1e-009 1.50  
59  7.1e-006 1.0e-002 4.3e-004 1.00e+000  1.670850720e+002  1.671008083e+002  3.7e-009 1.52  
60  6.4e-006 9.8e-003 3.8e-004 1.00e+000  1.670861140e+002  1.671002773e+002  3.3e-009 1.55  
61  5.8e-006 9.6e-003 3.4e-004 1.00e+000  1.670870512e+002  1.670997987e+002  3.0e-009 1.56  
62  2.2e-006 3.6e-003 1.3e-004 1.00e+000  1.670922663e+002  1.670970997e+002  1.1e-009 1.59  
63  8.7e-007 1.5e-003 5.3e-005 9.99e-001  1.670941717e+002  1.670961158e+002  4.6e-010 1.61  
64  7.9e-007 1.3e-003 4.7e-005 1.01e+000  1.670943047e+002  1.670960519e+002  4.1e-010 1.63  
65  7.1e-007 1.2e-003 4.3e-005 1.01e+000  1.670944213e+002  1.670959899e+002  3.7e-010 1.66  
66  6.4e-007 1.1e-003 3.8e-005 9.98e-001  1.670945244e+002  1.670959362e+002  3.3e-010 1.67  
67  5.7e-007 9.6e-004 3.4e-005 9.84e-001  1.670946168e+002  1.670958884e+002  3.0e-010 1.70  
68  5.2e-007 8.6e-004 3.1e-005 9.97e-001  1.670947001e+002  1.670958447e+002  2.7e-010 1.72  
69  4.6e-007 7.8e-004 2.8e-005 9.69e-001  1.670947747e+002  1.670958065e+002  2.4e-010 1.75  
70  4.2e-007 7.0e-004 2.5e-005 9.97e-001  1.670948421e+002  1.670957709e+002  2.2e-010 1.77  
71  3.8e-007 6.3e-004 2.3e-005 9.73e-001  1.670949026e+002  1.670957396e+002  2.0e-010 1.80  
72  3.4e-007 5.7e-004 2.0e-005 1.04e+000  1.670949665e+002  1.670957043e+002  1.8e-010 1.81  
73  3.0e-007 5.1e-004 1.8e-005 1.01e+000  1.670950159e+002  1.670956779e+002  1.6e-010 1.84  
74  2.7e-007 4.6e-004 1.6e-005 1.00e+000  1.670950592e+002  1.670956550e+002  1.5e-010 1.86  
75  2.5e-007 4.1e-004 1.5e-005 1.04e+000  1.670951053e+002  1.670956296e+002  1.3e-010 1.88  
76  2.2e-007 3.7e-004 1.3e-005 9.64e-001  1.670951394e+002  1.670956121e+002  1.2e-010 1.91  
77  2.0e-007 3.3e-004 1.2e-005 9.89e-001  1.670951702e+002  1.670955959e+002  1.1e-010 1.92  
78  1.8e-007 3.0e-004 1.1e-005 1.01e+000  1.670951985e+002  1.670955808e+002  9.8e-011 1.95  
79  1.6e-007 2.7e-004 9.7e-006 9.52e-001  1.670952233e+002  1.670955682e+002  8.8e-011 1.97  
80  1.5e-007 2.4e-004 8.8e-006 9.48e-001  1.670952456e+002  1.670955568e+002  8.0e-011 1.99  
81  1.3e-007 2.2e-004 7.9e-006 1.01e+000  1.670952669e+002  1.670955452e+002  7.2e-011 2.02  
82  1.2e-007 2.0e-004 7.1e-006 1.12e+000  1.670952947e+002  1.670955288e+002  6.9e-011 2.03  
83  1.1e-007 1.8e-004 6.4e-006 1.15e+000  1.670953203e+002  1.670955137e+002  6.6e-011 2.06  
84  9.7e-008 1.6e-004 5.8e-006 1.08e+000  1.670953374e+002  1.670955043e+002  6.2e-011 2.08  
85  8.7e-008 1.4e-004 5.2e-006 9.51e-001  1.670953484e+002  1.670954990e+002  5.6e-011 2.09  
86  7.9e-008 1.3e-004 4.7e-006 1.01e+000  1.670953588e+002  1.670954936e+002  5.0e-011 2.13  
87  8.1e-008 1.2e-004 4.2e-006 2.06e+000  1.670953696e+002  1.670954830e+002  4.5e-011 2.14  
88  7.4e-008 1.1e-004 3.8e-006 1.05e+000  1.670953791e+002  1.670954786e+002  4.1e-011 2.17  
89  6.7e-008 9.5e-005 3.4e-006 1.00e+000  1.670953861e+002  1.670954755e+002  3.7e-011 2.19  
90  6.3e-008 8.5e-005 3.1e-006 1.38e+000  1.670953929e+002  1.670954714e+002  3.3e-011 2.22  
91  5.9e-008 7.7e-005 2.8e-006 1.03e+000  1.670953991e+002  1.670954687e+002  3.0e-011 2.23  
92  5.0e-008 6.9e-005 2.5e-006 8.60e-001  1.670954038e+002  1.670954670e+002  2.7e-011 2.27  
93  4.7e-008 6.2e-005 2.2e-006 1.27e+000  1.670954085e+002  1.670954645e+002  2.5e-011 2.28  
94  2.9e-008 4.8e-006 1.7e-007 6.87e-001  1.670954476e+002  1.670954526e+002  4.6e-012 2.31  
Interior-point optimizer terminated. Time: 2.31. 

Optimizer terminated. Time: 2.33    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6709544761e+002   nrm: 2e+001   Viol.  con: 8e-007   var: 0e+000 
  Dual.    obj: 1.6709545263e+002   nrm: 9e+002   Viol.  con: 0e+000   var: 2e-005 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.36 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.02    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 870
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3453              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.48e+004         after factor           : 1.47e+005       
Factor     - dense dim.             : 0                 flops                  : 2.89e+007       
Factor     - GP saved nzs           : 3.32e+004         GP saved flops         : 9.06e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.2e+005 0.00e+000  -1.221995260e+005 2.000000000e+000  1.0e+000 0.06  
1   1.6e+003 2.2e+003 8.8e+004 -9.71e-001 -1.214485098e+005 2.632752263e+000  7.2e-001 0.08  
2   8.7e+002 1.1e+003 4.6e+004 -9.59e-001 -1.191331143e+005 4.655497767e+000  3.8e-001 0.09  
3   2.9e+002 3.8e+002 1.5e+004 -9.20e-001 -1.102221824e+005 2.014414807e+001  1.3e-001 0.13  
4   2.9e+002 3.8e+002 1.5e+004 -7.70e-001 -1.080548328e+005 1.913931252e+003  1.3e-001 0.14  
5   1.2e+002 1.6e+002 6.3e+003 -7.61e-001 -8.679130231e+004 6.275735811e+003  5.3e-002 0.16  
6   4.0e+001 5.3e+001 2.1e+003 -4.46e-001 -4.754060874e+004 1.089180817e+004  1.8e-002 0.19  
7   2.5e+001 3.3e+001 1.3e+003 2.21e-001  -3.385858067e+004 7.489008433e+003  1.1e-002 0.20  
8   1.2e+001 1.6e+001 6.4e+002 4.86e-001  -1.817870398e+004 4.242994690e+003  5.3e-003 0.22  
9   4.0e+000 5.4e+000 2.2e+002 7.62e-001  -6.124808057e+003 2.033340610e+003  1.8e-003 0.23  
10  2.3e+000 3.1e+000 1.2e+002 9.49e-001  -3.337738506e+003 1.370042100e+003  1.0e-003 0.27  
11  1.0e+000 1.3e+000 5.5e+001 9.83e-001  -1.382986637e+003 6.916304353e+002  4.6e-004 0.28  
12  7.6e-001 1.0e+000 4.1e+001 9.81e-001  -1.037935124e+003 5.643375943e+002  3.5e-004 0.30  
13  7.3e-001 9.6e-001 4.0e+001 9.85e-001  -9.748701489e+002 5.508849705e+002  3.3e-004 0.31  
14  2.7e-001 4.0e-001 1.5e+001 9.85e-001  -2.694368731e+002 3.066547144e+002  1.3e-004 0.34  
15  1.7e-001 4.3e-001 9.5e+000 1.01e+000  -1.164029131e+002 2.501967852e+002  8.0e-005 0.36  
16  9.4e-002 2.4e-001 5.2e+000 1.01e+000  5.072440659e+000  2.050337745e+002  4.4e-005 0.39  
17  9.3e-002 2.4e-001 5.1e+000 1.02e+000  7.675436626e+000  2.051340656e+002  4.3e-005 0.41  
18  7.9e-002 2.0e-001 4.4e+000 1.02e+000  3.681134015e+001  2.041150325e+002  3.7e-005 0.44  
19  3.6e-002 1.1e-001 2.0e+000 1.01e+000  1.082091563e+002  1.832572580e+002  1.7e-005 0.45  
20  9.9e-003 1.8e-001 5.6e-001 1.01e+000  1.513921348e+002  1.723807829e+002  4.7e-006 0.47  
21  3.0e-003 1.9e-001 1.7e-001 1.01e+000  1.617922657e+002  1.682950059e+002  1.5e-006 0.50  
22  1.2e-003 1.4e-001 7.3e-002 1.01e+000  1.646594569e+002  1.673895810e+002  6.2e-007 0.52  
23  7.8e-004 1.0e-001 4.6e-002 9.78e-001  1.653887018e+002  1.671255529e+002  4.0e-007 0.55  
24  2.3e-004 1.1e-001 1.4e-002 9.86e-001  1.662687147e+002  1.667933784e+002  1.2e-007 0.56  
25  7.6e-005 1.1e-001 4.8e-003 1.01e+000  1.665139108e+002  1.666910462e+002  4.2e-008 0.58  
26  3.4e-005 9.0e-002 2.2e-003 1.01e+000  1.665818717e+002  1.666619038e+002  1.9e-008 0.61  
27  3.1e-005 8.4e-002 2.0e-003 1.01e+000  1.665881350e+002  1.666606638e+002  1.7e-008 0.63  
28  2.8e-005 7.5e-002 1.8e-003 1.00e+000  1.665931511e+002  1.666584046e+002  1.6e-008 0.66  
29  2.5e-005 6.9e-002 1.6e-003 1.00e+000  1.665976565e+002  1.666563779e+002  1.4e-008 0.67  
30  2.3e-005 6.2e-002 1.4e-003 1.00e+000  1.666017058e+002  1.666545470e+002  1.3e-008 0.69  
31  2.0e-005 5.7e-002 1.3e-003 1.00e+000  1.666053433e+002  1.666528935e+002  1.1e-008 0.72  
32  1.8e-005 5.2e-002 1.2e-003 1.00e+000  1.666086117e+002  1.666514010e+002  1.0e-008 0.73  
33  1.6e-005 4.8e-002 1.0e-003 1.00e+000  1.666115488e+002  1.666500544e+002  9.2e-009 0.75  
34  1.5e-005 4.4e-002 9.4e-004 1.00e+000  1.666141886e+002  1.666488397e+002  8.3e-009 0.78  
35  1.3e-005 4.0e-002 8.4e-004 1.00e+000  1.666165612e+002  1.666477440e+002  7.5e-009 0.80  
36  1.2e-005 3.7e-002 7.6e-004 1.00e+000  1.666186939e+002  1.666467558e+002  6.7e-009 0.81  
37  1.1e-005 3.4e-002 6.8e-004 1.00e+000  1.666206110e+002  1.666458646e+002  6.1e-009 0.84  
38  9.7e-006 3.1e-002 6.1e-004 1.00e+000  1.666223345e+002  1.666450609e+002  5.4e-009 0.86  
39  8.7e-006 2.9e-002 5.5e-004 1.00e+000  1.666238839e+002  1.666443363e+002  4.9e-009 0.88  
40  7.9e-006 2.7e-002 5.0e-004 1.00e+000  1.666252770e+002  1.666436829e+002  4.4e-009 0.91  
41  7.1e-006 2.5e-002 4.5e-004 1.00e+000  1.666265295e+002  1.666430939e+002  4.0e-009 0.92  
42  6.4e-006 2.3e-002 4.0e-004 1.00e+000  1.666276557e+002  1.666425629e+002  3.6e-009 0.95  
43  5.7e-006 2.2e-002 3.6e-004 1.00e+000  1.666286684e+002  1.666420843e+002  3.2e-009 0.97  
44  5.2e-006 2.0e-002 3.3e-004 1.00e+000  1.666295790e+002  1.666416528e+002  2.9e-009 0.98  
45  4.6e-006 1.9e-002 2.9e-004 1.00e+000  1.666303979e+002  1.666412639e+002  2.6e-009 1.02  
46  4.2e-006 1.8e-002 2.6e-004 1.00e+000  1.666311342e+002  1.666409134e+002  2.3e-009 1.03  
47  3.8e-006 1.7e-002 2.4e-004 1.00e+000  1.666317963e+002  1.666405973e+002  2.1e-009 1.06  
48  3.4e-006 1.6e-002 2.1e-004 1.00e+000  1.666323917e+002  1.666403124e+002  1.9e-009 1.08  
49  3.0e-006 1.5e-002 1.9e-004 1.00e+000  1.666329271e+002  1.666400556e+002  1.7e-009 1.11  
50  2.7e-006 1.5e-002 1.7e-004 1.00e+000  1.666334086e+002  1.666398240e+002  1.5e-009 1.13  
51  2.5e-006 1.4e-002 1.6e-004 1.00e+000  1.666338415e+002  1.666396153e+002  1.4e-009 1.16  
52  2.2e-006 1.3e-002 1.4e-004 1.00e+000  1.666342309e+002  1.666394272e+002  1.2e-009 1.17  
53  2.0e-006 1.3e-002 1.3e-004 1.00e+000  1.666345811e+002  1.666392577e+002  1.1e-009 1.20  
54  1.8e-006 1.2e-002 1.1e-004 1.00e+000  1.666348961e+002  1.666391050e+002  1.0e-009 1.22  
55  1.6e-006 1.2e-002 1.0e-004 1.00e+000  1.666351794e+002  1.666389674e+002  9.1e-010 1.25  
56  1.5e-006 1.2e-002 9.2e-005 1.00e+000  1.666354342e+002  1.666388434e+002  8.2e-010 1.28  
57  1.3e-006 1.1e-002 8.3e-005 1.00e+000  1.666356635e+002  1.666387317e+002  7.4e-010 1.30  
58  1.2e-006 1.1e-002 7.5e-005 1.00e+000  1.666358696e+002  1.666386310e+002  6.6e-010 1.33  
59  1.1e-006 1.1e-002 6.7e-005 1.00e+000  1.666360551e+002  1.666385403e+002  6.0e-010 1.36  
60  9.6e-007 1.0e-002 6.1e-005 1.00e+000  1.666362218e+002  1.666384585e+002  5.4e-010 1.39  
61  8.6e-007 1.0e-002 5.4e-005 1.00e+000  1.666363718e+002  1.666383848e+002  4.8e-010 1.42  
62  7.7e-007 9.9e-003 4.9e-005 1.00e+000  1.666365067e+002  1.666383184e+002  4.3e-010 1.44  
63  7.0e-007 9.7e-003 4.4e-005 1.00e+000  1.666366280e+002  1.666382585e+002  3.9e-010 1.47  
64  6.3e-007 9.5e-003 4.0e-005 1.00e+000  1.666367371e+002  1.666382046e+002  3.5e-010 1.48  
65  5.6e-007 9.4e-003 3.6e-005 1.00e+000  1.666368352e+002  1.666381559e+002  3.2e-010 1.52  
66  5.1e-007 9.2e-003 3.2e-005 1.00e+000  1.666369234e+002  1.666381120e+002  2.9e-010 1.53  
67  4.6e-007 9.1e-003 2.9e-005 1.00e+000  1.666370027e+002  1.666380725e+002  2.6e-010 1.56  
68  4.1e-007 9.0e-003 2.6e-005 1.00e+000  1.666370740e+002  1.666380368e+002  2.3e-010 1.58  
69  3.7e-007 8.9e-003 2.3e-005 1.00e+000  1.666371381e+002  1.666380047e+002  2.1e-010 1.61  
70  3.3e-007 8.8e-003 2.1e-005 1.00e+000  1.666371958e+002  1.666379757e+002  1.9e-010 1.63  
71  3.0e-007 8.7e-003 1.9e-005 1.00e+000  1.666372477e+002  1.666379496e+002  1.7e-010 1.66  
72  2.7e-007 8.6e-003 1.7e-005 1.00e+000  1.666372943e+002  1.666379260e+002  1.5e-010 1.67  
73  2.4e-007 8.6e-003 1.5e-005 1.00e+000  1.666373363e+002  1.666379048e+002  1.4e-010 1.70  
74  2.2e-007 8.5e-003 1.4e-005 1.00e+000  1.666373740e+002  1.666378857e+002  1.2e-010 1.72  
75  2.0e-007 8.4e-003 1.2e-005 1.00e+000  1.666374080e+002  1.666378685e+002  1.1e-010 1.75  
76  1.8e-007 8.4e-003 1.1e-005 1.00e+000  1.666374385e+002  1.666378530e+002  1.0e-010 1.77  
77  1.6e-007 8.3e-003 1.0e-005 1.00e+000  1.666374660e+002  1.666378390e+002  9.0e-011 1.80  
78  1.4e-007 8.3e-003 9.1e-006 1.00e+000  1.666374908e+002  1.666378265e+002  8.1e-011 1.81  
79  1.3e-007 8.2e-003 8.2e-006 1.00e+000  1.666375130e+002  1.666378151e+002  7.3e-011 1.84  
80  1.2e-007 8.2e-003 7.4e-006 1.00e+000  1.666375330e+002  1.666378050e+002  6.5e-011 1.86  
81  1.0e-007 8.2e-003 6.6e-006 1.00e+000  1.666375510e+002  1.666377958e+002  5.9e-011 1.89  
82  9.4e-008 8.1e-003 6.0e-006 1.00e+000  1.666375673e+002  1.666377875e+002  5.3e-011 1.91  
83  8.5e-008 8.1e-003 5.4e-006 1.00e+000  1.666375819e+002  1.666377801e+002  4.8e-011 1.94  
84  7.6e-008 8.0e-003 4.8e-006 9.98e-001  1.666375950e+002  1.666377734e+002  4.3e-011 1.95  
85  6.9e-008 8.0e-003 4.3e-006 1.00e+000  1.666376068e+002  1.666377674e+002  3.9e-011 1.98  
86  6.2e-008 8.0e-003 3.9e-006 1.00e+000  1.666376174e+002  1.666377619e+002  3.5e-011 2.00  
87  5.6e-008 8.0e-003 3.5e-006 9.99e-001  1.666376270e+002  1.666377571e+002  3.1e-011 2.03  
88  5.0e-008 7.9e-003 3.2e-006 1.00e+000  1.666376356e+002  1.666377527e+002  2.8e-011 2.05  
89  4.5e-008 7.9e-003 2.9e-006 9.98e-001  1.666376434e+002  1.666377488e+002  2.5e-011 2.08  
90  7.3e-008 7.1e-003 2.6e-006 1.01e+000  1.666376527e+002  1.666377367e+002  2.2e-011 2.09  
91  8.0e-008 6.4e-003 2.3e-006 1.00e+000  1.666376628e+002  1.666377261e+002  1.9e-011 2.13  
92  1.9e-007 5.8e-003 2.1e-006 1.00e+000  1.666376676e+002  1.666377250e+002  1.7e-011 2.14  
93  1.7e-007 5.2e-003 1.9e-006 9.97e-001  1.666376721e+002  1.666377239e+002  1.5e-011 2.17  
94  1.6e-007 4.7e-003 1.7e-006 9.99e-001  1.666376762e+002  1.666377228e+002  1.4e-011 2.19  
95  1.4e-007 4.2e-003 1.5e-006 1.00e+000  1.666376799e+002  1.666377218e+002  1.2e-011 2.20  
96  1.3e-007 3.8e-003 1.4e-006 1.00e+000  1.666376832e+002  1.666377209e+002  1.1e-011 2.23  
97  1.2e-007 3.4e-003 1.2e-006 1.00e+000  1.666376862e+002  1.666377202e+002  9.9e-012 2.25  
98  1.0e-007 3.1e-003 1.1e-006 9.99e-001  1.666376889e+002  1.666377195e+002  8.9e-012 2.28  
99  9.3e-008 2.8e-003 9.9e-007 9.99e-001  1.666376913e+002  1.666377188e+002  8.0e-012 2.31  
100 8.4e-008 2.5e-003 9.0e-007 1.00e+000  1.666376935e+002  1.666377183e+002  7.2e-012 2.33  
101 8.4e-008 2.2e-003 8.1e-007 9.96e-001  1.666376956e+002  1.666377176e+002  6.5e-012 2.38  
102 7.9e-008 2.0e-003 7.2e-007 1.00e+000  1.666376976e+002  1.666377171e+002  5.8e-012 2.39  
103 7.2e-008 1.8e-003 6.5e-007 1.00e+000  1.666376991e+002  1.666377168e+002  5.3e-012 2.42  
104 6.4e-008 1.6e-003 5.8e-007 1.00e+000  1.666377005e+002  1.666377164e+002  4.7e-012 2.44  
105 6.3e-008 1.5e-003 4.7e-007 1.00e+000  1.666377031e+002  1.666377161e+002  4.3e-012 2.47  
106 5.8e-008 1.3e-003 4.3e-007 1.00e+000  1.666377040e+002  1.666377158e+002  3.8e-012 2.48  
107 5.7e-008 1.2e-003 3.7e-007 1.00e+000  1.666377054e+002  1.666377155e+002  3.4e-012 2.52  
108 5.5e-009 1.2e-004 4.1e-008 1.00e+000  1.666377122e+002  1.666377134e+002  3.6e-013 2.53  
Interior-point optimizer terminated. Time: 2.53. 

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

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6663771223e+002   nrm: 2e+001   Viol.  con: 8e-008   var: 0e+000 
  Dual.    obj: 1.6663771336e+002   nrm: 9e+002   Viol.  con: 0e+000   var: 6e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.59 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.05    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 870
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3453              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 : 1.48e+004         after factor           : 1.47e+005       
Factor     - dense dim.             : 0                 flops                  : 2.89e+007       
Factor     - GP saved nzs           : 3.32e+004         GP saved flops         : 9.06e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.2e+005 0.00e+000  -1.222172762e+005 2.000000000e+000  1.0e+000 0.11  
1   1.6e+003 2.2e+003 8.8e+004 -9.71e-001 -1.214723541e+005 2.624860291e+000  7.2e-001 0.14  
2   8.7e+002 1.2e+003 4.6e+004 -9.59e-001 -1.191600648e+005 4.640065791e+000  3.8e-001 0.17  
3   2.9e+002 3.8e+002 1.5e+004 -9.21e-001 -1.101905174e+005 2.007531139e+001  1.3e-001 0.20  
4   2.9e+002 3.8e+002 1.5e+004 -7.70e-001 -1.079534852e+005 1.972409194e+003  1.3e-001 0.23  
5   1.2e+002 1.6e+002 6.3e+003 -7.60e-001 -8.657719809e+004 6.298069819e+003  5.2e-002 0.27  
6   4.2e+001 5.6e+001 2.2e+003 -4.43e-001 -4.925355487e+004 1.070989381e+004  1.9e-002 0.28  
7   2.5e+001 3.3e+001 1.3e+003 1.89e-001  -3.417053963e+004 7.445376119e+003  1.1e-002 0.31  
8   1.3e+001 1.7e+001 7.0e+002 4.80e-001  -1.947379735e+004 4.624174908e+003  5.8e-003 0.33  
9   4.8e+000 6.4e+000 2.6e+002 7.40e-001  -7.348185042e+003 2.244743799e+003  2.1e-003 0.36  
10  2.3e+000 3.0e+000 1.2e+002 9.32e-001  -3.276266972e+003 1.379198718e+003  1.0e-003 0.38  
11  1.4e+000 1.9e+000 7.7e+001 9.82e-001  -2.018898393e+003 9.189992953e+002  6.4e-004 0.41  
12  8.6e-001 1.1e+000 4.6e+001 9.88e-001  -1.150705877e+003 6.195823732e+002  3.9e-004 0.42  
13  7.4e-001 1.0e+000 4.0e+001 9.56e-001  -9.920714059e+002 5.488680050e+002  3.3e-004 0.45  
14  5.7e-001 7.9e-001 3.1e+001 9.89e-001  -7.199092946e+002 4.749626692e+002  2.6e-004 0.47  
15  1.7e-001 2.6e-001 9.4e+000 9.92e-001  -1.186870824e+002 2.437214800e+002  7.9e-005 0.50  
16  9.9e-002 1.6e-001 5.5e+000 1.01e+000  -3.505195583e+000 2.071335851e+002  4.6e-005 0.52  
17  9.8e-002 1.6e-001 5.4e+000 1.02e+000  -1.958210295e+000 2.072290471e+002  4.6e-005 0.55  
18  8.9e-002 1.4e-001 4.9e+000 1.02e+000  1.921030870e+001  2.077670311e+002  4.2e-005 0.56  
19  5.0e-002 8.8e-002 2.8e+000 1.02e+000  8.307361943e+001  1.898185386e+002  2.4e-005 0.59  
20  1.8e-002 8.6e-002 1.0e+000 1.02e+000  1.375912284e+002  1.754534287e+002  8.5e-006 0.63  
21  4.8e-003 2.3e-001 2.8e-001 1.01e+000  1.590499717e+002  1.694335148e+002  2.3e-006 0.64  
22  3.3e-003 2.5e-001 1.9e-001 1.00e+000  1.612917162e+002  1.684642104e+002  1.6e-006 0.67  
23  1.2e-003 1.4e-001 7.0e-002 1.00e+000  1.646656026e+002  1.672873338e+002  5.9e-007 0.69  
24  9.0e-004 1.2e-001 5.3e-002 9.94e-001  1.651194082e+002  1.671012436e+002  4.5e-007 0.72  
25  3.8e-004 8.5e-002 2.3e-002 9.84e-001  1.659363237e+002  1.667827583e+002  1.9e-007 0.73  
26  2.1e-004 7.0e-002 1.3e-002 1.01e+000  1.662008397e+002  1.666736895e+002  1.1e-007 0.77  
27  1.6e-004 6.5e-002 9.5e-003 1.01e+000  1.662864144e+002  1.666424098e+002  8.2e-008 0.78  
28  1.4e-004 5.9e-002 8.6e-003 1.01e+000  1.663125151e+002  1.666327407e+002  7.4e-008 0.81  
29  1.3e-004 5.4e-002 7.7e-003 1.01e+000  1.663345692e+002  1.666227052e+002  6.6e-008 0.83  
30  1.2e-004 4.9e-002 7.0e-003 1.01e+000  1.663546017e+002  1.666138745e+002  6.0e-008 0.86  
31  1.0e-004 4.5e-002 6.3e-003 1.01e+000  1.663725385e+002  1.666058435e+002  5.4e-008 0.88  
32  9.4e-005 4.1e-002 5.6e-003 1.01e+000  1.663886394e+002  1.665985810e+002  4.8e-008 0.91  
33  8.4e-005 3.8e-002 5.1e-003 1.00e+000  1.664030858e+002  1.665920069e+002  4.4e-008 0.92  
34  7.6e-005 3.5e-002 4.6e-003 1.00e+000  1.664160506e+002  1.665860583e+002  3.9e-008 0.94  
35  6.8e-005 3.2e-002 4.1e-003 1.00e+000  1.664276867e+002  1.665806768e+002  3.5e-008 0.97  
36  6.1e-005 2.9e-002 3.7e-003 1.00e+000  1.664381316e+002  1.665758093e+002  3.2e-008 0.98  
37  5.5e-005 2.7e-002 3.3e-003 1.00e+000  1.664475083e+002  1.665714077e+002  2.9e-008 1.02  
38  5.0e-005 2.5e-002 3.0e-003 1.00e+000  1.664559271e+002  1.665674283e+002  2.6e-008 1.03  
39  4.5e-005 2.3e-002 2.7e-003 1.00e+000  1.664634866e+002  1.665638312e+002  2.3e-008 1.06  
40  4.0e-005 2.2e-002 2.4e-003 1.00e+000  1.664702752e+002  1.665605804e+002  2.1e-008 1.08  
41  3.6e-005 2.0e-002 2.2e-003 1.00e+000  1.664763722e+002  1.665576431e+002  1.9e-008 1.11  
42  3.3e-005 1.9e-002 2.0e-003 1.00e+000  1.664818485e+002  1.665549894e+002  1.7e-008 1.13  
43  2.9e-005 1.8e-002 1.8e-003 1.00e+000  1.664867680e+002  1.665525926e+002  1.5e-008 1.16  
44  2.6e-005 1.7e-002 1.6e-003 1.00e+000  1.664911875e+002  1.665504281e+002  1.4e-008 1.17  
45  2.4e-005 1.6e-002 1.4e-003 1.00e+000  1.664951584e+002  1.665484737e+002  1.2e-008 1.19  
46  2.1e-005 1.5e-002 1.3e-003 1.00e+000  1.664987264e+002  1.665467094e+002  1.1e-008 1.22  
47  1.9e-005 1.5e-002 1.2e-003 1.00e+000  1.665019329e+002  1.665451170e+002  1.0e-008 1.24  
48  1.7e-005 1.4e-002 1.0e-003 1.00e+000  1.665048148e+002  1.665436801e+002  9.0e-009 1.27  
49  1.6e-005 1.3e-002 9.4e-004 1.00e+000  1.665074051e+002  1.665423837e+002  8.1e-009 1.28  
50  1.4e-005 1.3e-002 8.5e-004 1.00e+000  1.665097337e+002  1.665412144e+002  7.3e-009 1.30  
51  1.3e-005 1.2e-002 7.6e-004 1.00e+000  1.665118273e+002  1.665401599e+002  6.6e-009 1.33  
52  1.1e-005 1.2e-002 6.9e-004 1.00e+000  1.665137097e+002  1.665392091e+002  5.9e-009 1.34  
53  1.0e-005 1.2e-002 6.2e-004 1.00e+000  1.665154024e+002  1.665383520e+002  5.3e-009 1.38  
54  9.2e-006 1.1e-002 5.6e-004 1.00e+000  1.665169247e+002  1.665375794e+002  4.8e-009 1.39  
55  8.3e-006 1.1e-002 5.0e-004 1.00e+000  1.665182939e+002  1.665368832e+002  4.3e-009 1.41  
56  7.5e-006 1.1e-002 4.5e-004 1.00e+000  1.665195253e+002  1.665362558e+002  3.9e-009 1.44  
57  6.7e-006 1.0e-002 4.0e-004 1.00e+000  1.665206330e+002  1.665356906e+002  3.5e-009 1.45  
58  6.0e-006 1.0e-002 3.6e-004 1.00e+000  1.665216293e+002  1.665351813e+002  3.1e-009 1.49  
59  5.4e-006 1.0e-002 3.3e-004 1.00e+000  1.665225256e+002  1.665347225e+002  2.8e-009 1.50  
60  4.9e-006 9.8e-003 3.0e-004 1.00e+000  1.665233318e+002  1.665343091e+002  2.5e-009 1.53  
61  4.4e-006 9.6e-003 2.7e-004 1.00e+000  1.665240569e+002  1.665339367e+002  2.3e-009 1.55  
62  4.0e-006 9.5e-003 2.4e-004 1.00e+000  1.665247092e+002  1.665336011e+002  2.1e-009 1.56  
63  3.6e-006 9.3e-003 2.2e-004 1.00e+000  1.665252959e+002  1.665332987e+002  1.9e-009 1.59  
64  3.2e-006 9.2e-003 1.9e-004 1.00e+000  1.665258236e+002  1.665330262e+002  1.7e-009 1.61  
65  2.9e-006 9.1e-003 1.7e-004 1.00e+000  1.665262982e+002  1.665327806e+002  1.5e-009 1.64  
66  2.6e-006 9.0e-003 1.6e-004 1.00e+000  1.665267252e+002  1.665325594e+002  1.4e-009 1.66  
67  2.3e-006 8.9e-003 1.4e-004 1.00e+000  1.665271092e+002  1.665323600e+002  1.2e-009 1.67  
68  2.1e-006 8.9e-003 1.3e-004 1.00e+000  1.665274547e+002  1.665321805e+002  1.1e-009 1.70  
69  1.9e-006 8.8e-003 1.1e-004 1.00e+000  1.665277654e+002  1.665320187e+002  9.9e-010 1.72  
70  1.7e-006 8.7e-003 1.0e-004 1.00e+000  1.665280450e+002  1.665318730e+002  8.9e-010 1.75  
71  1.5e-006 8.7e-003 9.3e-005 1.00e+000  1.665282965e+002  1.665317418e+002  8.0e-010 1.77  
72  1.4e-006 8.6e-003 8.3e-005 1.00e+000  1.665285228e+002  1.665316235e+002  7.2e-010 1.78  
73  1.2e-006 8.6e-003 7.5e-005 1.00e+000  1.665287263e+002  1.665315170e+002  6.5e-010 1.81  
74  1.1e-006 8.5e-003 6.8e-005 1.00e+000  1.665289094e+002  1.665314211e+002  5.8e-010 1.83  
75  1.0e-006 8.5e-003 6.1e-005 1.00e+000  1.665290741e+002  1.665313346e+002  5.2e-010 1.86  
76  9.1e-007 8.4e-003 5.5e-005 1.00e+000  1.665292223e+002  1.665312568e+002  4.7e-010 1.88  
77  8.2e-007 8.4e-003 4.9e-005 1.00e+000  1.665293555e+002  1.665311866e+002  4.2e-010 1.89  
78  7.3e-007 8.4e-003 4.4e-005 1.00e+000  1.665294754e+002  1.665311233e+002  3.8e-010 1.92  
79  6.6e-007 8.3e-003 4.0e-005 1.00e+000  1.665295832e+002  1.665310663e+002  3.4e-010 1.94  
80  6.0e-007 8.3e-003 3.6e-005 1.00e+000  1.665296801e+002  1.665310150e+002  3.1e-010 1.97  
81  5.4e-007 8.3e-003 3.2e-005 1.00e+000  1.665297673e+002  1.665309686e+002  2.8e-010 1.99  
82  4.8e-007 8.2e-003 2.9e-005 1.00e+000  1.665298456e+002  1.665309269e+002  2.5e-010 2.02  
83  4.3e-007 8.2e-003 2.6e-005 1.00e+000  1.665299161e+002  1.665308893e+002  2.3e-010 2.03  
84  3.9e-007 8.2e-003 2.4e-005 1.00e+000  1.665299795e+002  1.665308553e+002  2.0e-010 2.05  
85  3.5e-007 8.2e-003 2.1e-005 1.00e+000  1.665300365e+002  1.665308248e+002  1.8e-010 2.08  
86  3.2e-007 8.1e-003 1.9e-005 1.00e+000  1.665300878e+002  1.665307972e+002  1.6e-010 2.09  
87  2.8e-007 8.1e-003 1.7e-005 1.00e+000  1.665301339e+002  1.665307724e+002  1.5e-010 2.13  
88  2.6e-007 8.1e-003 1.5e-005 1.00e+000  1.665301753e+002  1.665307500e+002  1.3e-010 2.14  
89  2.3e-007 8.1e-003 1.4e-005 1.00e+000  1.665302126e+002  1.665307298e+002  1.2e-010 2.17  
90  2.1e-007 8.1e-003 1.3e-005 1.00e+000  1.665302462e+002  1.665307117e+002  1.1e-010 2.19  
91  1.9e-007 8.0e-003 1.1e-005 1.00e+000  1.665302764e+002  1.665306953e+002  9.7e-011 2.22  
92  1.7e-007 8.0e-003 1.0e-005 1.00e+000  1.665303035e+002  1.665306806e+002  8.8e-011 2.23  
93  1.5e-007 8.0e-003 9.1e-006 1.00e+000  1.665303280e+002  1.665306673e+002  7.9e-011 2.27  
94  1.4e-007 8.0e-003 8.2e-006 1.00e+000  1.665303500e+002  1.665306554e+002  7.1e-011 2.28  
95  1.2e-007 8.0e-003 7.4e-006 1.00e+000  1.665303698e+002  1.665306446e+002  6.4e-011 2.31  
96  1.1e-007 8.0e-003 6.7e-006 1.00e+000  1.665303876e+002  1.665306349e+002  5.7e-011 2.33  
97  9.9e-008 8.0e-003 6.0e-006 1.00e+000  1.665304036e+002  1.665306261e+002  5.2e-011 2.36  
98  8.9e-008 7.9e-003 5.4e-006 1.00e+000  1.665304180e+002  1.665306183e+002  4.7e-011 2.38  
99  8.1e-008 7.9e-003 4.9e-006 1.00e+000  1.665304310e+002  1.665306112e+002  4.2e-011 2.41  
100 7.2e-008 7.9e-003 4.4e-006 1.00e+000  1.665304426e+002  1.665306049e+002  3.8e-011 2.42  
101 6.5e-008 7.9e-003 3.9e-006 9.98e-001  1.665304531e+002  1.665305992e+002  3.4e-011 2.45  
102 5.9e-008 7.9e-003 3.5e-006 1.00e+000  1.665304626e+002  1.665305940e+002  3.1e-011 2.47  
103 5.3e-008 7.8e-003 3.2e-006 1.00e+000  1.665304711e+002  1.665305894e+002  2.7e-011 2.50  
104 4.8e-008 7.8e-003 2.9e-006 9.99e-001  1.665304787e+002  1.665305852e+002  2.5e-011 2.52  
105 4.3e-008 7.8e-003 2.6e-006 9.99e-001  1.665304856e+002  1.665305814e+002  2.2e-011 2.53  
106 3.9e-008 7.8e-003 2.3e-006 9.98e-001  1.665304918e+002  1.665305781e+002  2.0e-011 2.56  
107 3.5e-008 7.8e-003 2.1e-006 1.00e+000  1.665304974e+002  1.665305750e+002  1.8e-011 2.58  
108 3.1e-008 7.7e-003 1.9e-006 9.97e-001  1.665305024e+002  1.665305723e+002  1.6e-011 2.61  
109 2.8e-008 7.7e-003 1.7e-006 9.98e-001  1.665305069e+002  1.665305699e+002  1.5e-011 2.63  
110 2.5e-008 7.7e-003 1.5e-006 9.96e-001  1.665305110e+002  1.665305676e+002  1.3e-011 2.66  
111 2.3e-008 7.7e-003 1.4e-006 9.99e-001  1.665305147e+002  1.665305656e+002  1.2e-011 2.67  
112 2.0e-008 7.7e-003 1.2e-006 1.00e+000  1.665305180e+002  1.665305638e+002  1.1e-011 2.70  
113 1.8e-008 6.9e-003 1.1e-006 1.00e+000  1.665305209e+002  1.665305622e+002  9.6e-012 2.72  
114 1.7e-008 6.2e-003 1.0e-006 1.00e+000  1.665305236e+002  1.665305607e+002  8.6e-012 2.75  
115 1.5e-008 5.6e-003 9.0e-007 9.98e-001  1.665305260e+002  1.665305594e+002  7.8e-012 2.77  
116 1.3e-008 5.0e-003 8.1e-007 9.98e-001  1.665305282e+002  1.665305582e+002  7.0e-012 2.80  
117 1.2e-008 4.5e-003 7.3e-007 9.99e-001  1.665305301e+002  1.665305572e+002  6.3e-012 2.81  
118 1.1e-008 4.1e-003 6.6e-007 1.00e+000  1.665305319e+002  1.665305562e+002  5.7e-012 2.84  
119 9.8e-009 3.7e-003 5.9e-007 9.94e-001  1.665305334e+002  1.665305554e+002  5.1e-012 2.86  
120 8.8e-009 3.3e-003 5.3e-007 9.86e-001  1.665305349e+002  1.665305546e+002  4.6e-012 2.88  
121 8.5e-008 1.2e-003 1.9e-007 4.86e-001  1.665305464e+002  1.665305608e+002  2.0e-012 2.91  
122 1.2e-007 1.1e-003 1.7e-007 9.92e-001  1.665305479e+002  1.665305623e+002  1.8e-012 2.92  
123 1.0e-007 9.6e-004 1.6e-007 1.00e+000  1.665305478e+002  1.665305608e+002  1.6e-012 2.95  
124 9.3e-008 8.7e-004 1.4e-007 1.00e+000  1.665305478e+002  1.665305595e+002  1.4e-012 2.97  
125 8.4e-008 7.8e-004 1.3e-007 1.00e+000  1.665305478e+002  1.665305583e+002  1.3e-012 3.00  
126 7.6e-008 7.0e-004 1.1e-007 9.99e-001  1.665305478e+002  1.665305572e+002  1.2e-012 3.02  
127 6.8e-008 6.3e-004 1.0e-007 9.98e-001  1.665305478e+002  1.665305563e+002  1.0e-012 3.05  
128 6.1e-008 5.7e-004 9.2e-008 9.94e-001  1.665305478e+002  1.665305554e+002  9.4e-013 3.06  
Interior-point optimizer terminated. Time: 3.06. 

Optimizer terminated. Time: 3.08    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6653054776e+002   nrm: 2e+001   Viol.  con: 3e-006   var: 0e+000 
  Dual.    obj: 1.6653055541e+002   nrm: 1e+003   Viol.  con: 0e+000   var: 9e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.11 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.05    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 870
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3453              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 : 1.48e+004         after factor           : 1.47e+005       
Factor     - dense dim.             : 0                 flops                  : 2.89e+007       
Factor     - GP saved nzs           : 3.32e+004         GP saved flops         : 9.06e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.2e+005 0.00e+000  -1.222140918e+005 2.000000000e+000  1.0e+000 0.11  
1   1.6e+003 2.2e+003 8.8e+004 -9.71e-001 -1.214694322e+005 2.622524733e+000  7.2e-001 0.14  
2   8.7e+002 1.2e+003 4.7e+004 -9.59e-001 -1.191636199e+005 4.628431031e+000  3.8e-001 0.16  
3   2.9e+002 3.8e+002 1.5e+004 -9.21e-001 -1.101376639e+005 2.011898828e+001  1.3e-001 0.19  
4   2.9e+002 3.8e+002 1.5e+004 -7.69e-001 -1.079182418e+005 1.962140407e+003  1.3e-001 0.22  
5   1.2e+002 1.5e+002 6.2e+003 -7.59e-001 -8.637744746e+004 6.311793233e+003  5.2e-002 0.23  
6   3.3e+001 4.4e+001 1.8e+003 -4.39e-001 -4.095232676e+004 1.163610898e+004  1.5e-002 0.27  
7   2.1e+001 2.7e+001 1.1e+003 3.41e-001  -2.860172757e+004 7.418112995e+003  9.2e-003 0.28  
8   1.0e+001 1.4e+001 5.5e+002 5.82e-001  -1.560633347e+004 4.111275508e+003  4.6e-003 0.31  
9   3.8e+000 5.1e+000 2.1e+002 8.06e-001  -5.848672010e+003 1.904437659e+003  1.7e-003 0.33  
10  2.1e+000 2.8e+000 1.1e+002 9.51e-001  -3.043789412e+003 1.215799273e+003  9.4e-004 0.36  
11  8.8e-001 1.2e+000 4.8e+001 9.86e-001  -1.178824208e+003 6.404720052e+002  4.0e-004 0.38  
12  8.4e-001 1.1e+000 4.6e+001 9.64e-001  -1.144460221e+003 6.102585061e+002  3.8e-004 0.39  
13  5.3e-001 7.0e-001 2.9e+001 9.73e-001  -6.848819951e+002 4.357423100e+002  2.4e-004 0.42  
14  3.5e-001 4.7e-001 1.9e+001 1.00e+000  -3.765174086e+002 3.604658005e+002  1.6e-004 0.44  
15  1.4e-001 2.0e-001 7.6e+000 9.96e-001  -6.326420273e+001 2.308763752e+002  6.5e-005 0.47  
16  8.5e-002 1.3e-001 4.7e+000 1.01e+000  2.245041635e+001  2.023531091e+002  4.0e-005 0.48  
17  8.1e-002 1.2e-001 4.5e+000 1.02e+000  2.818068800e+001  2.011809902e+002  3.8e-005 0.50  
18  5.5e-002 8.5e-002 3.0e+000 1.02e+000  7.590922907e+001  1.918141148e+002  2.6e-005 0.53  
19  1.6e-002 8.7e-002 9.0e-001 1.02e+000  1.408034601e+002  1.746828738e+002  7.6e-006 0.55  
20  4.8e-003 2.0e-001 2.7e-001 1.01e+000  1.590201195e+002  1.692540203e+002  2.3e-006 0.58  
21  3.2e-003 2.2e-001 1.8e-001 1.01e+000  1.614660681e+002  1.682589131e+002  1.5e-006 0.59  
22  1.0e-003 1.3e-001 6.0e-002 1.00e+000  1.648754715e+002  1.671201115e+002  5.1e-007 0.61  
23  3.3e-004 1.1e-001 2.0e-002 1.01e+000  1.659562011e+002  1.666963399e+002  1.7e-007 0.64  
24  1.5e-004 9.4e-002 9.2e-003 1.01e+000  1.662389479e+002  1.665805780e+002  8.0e-008 0.66  
25  1.4e-004 8.5e-002 8.3e-003 1.01e+000  1.662650841e+002  1.665725291e+002  7.2e-008 0.69  
26  1.2e-004 7.7e-002 7.4e-003 1.01e+000  1.662864876e+002  1.665630697e+002  6.5e-008 0.70  
27  1.1e-004 7.0e-002 6.7e-003 1.01e+000  1.663058658e+002  1.665547068e+002  5.8e-008 0.73  
28  9.9e-005 6.4e-002 6.0e-003 1.01e+000  1.663232114e+002  1.665470982e+002  5.3e-008 0.75  
29  8.9e-005 5.9e-002 5.4e-003 1.01e+000  1.663387782e+002  1.665402189e+002  4.7e-008 0.77  
30  8.0e-005 5.3e-002 4.9e-003 1.01e+000  1.663527426e+002  1.665339919e+002  4.3e-008 0.80  
31  7.2e-005 4.9e-002 4.4e-003 1.01e+000  1.663652714e+002  1.665283569e+002  3.8e-008 0.81  
32  6.5e-005 4.5e-002 4.0e-003 1.01e+000  1.663765130e+002  1.665232582e+002  3.5e-008 0.84  
33  5.8e-005 4.1e-002 3.6e-003 1.01e+000  1.663866009e+002  1.665186455e+002  3.1e-008 0.86  
34  5.2e-005 3.8e-002 3.2e-003 1.01e+000  1.663956543e+002  1.665144732e+002  2.8e-008 0.89  
35  4.7e-005 3.5e-002 2.9e-003 1.01e+000  1.664037805e+002  1.665107002e+002  2.5e-008 0.91  
36  4.2e-005 3.2e-002 2.6e-003 1.00e+000  1.664110753e+002  1.665072890e+002  2.3e-008 0.94  
37  3.8e-005 3.0e-002 2.3e-003 1.00e+000  1.664176245e+002  1.665042055e+002  2.0e-008 0.95  
38  3.4e-005 2.8e-002 2.1e-003 1.00e+000  1.664235051e+002  1.665014188e+002  1.8e-008 0.98  
39  3.1e-005 2.6e-002 1.9e-003 1.00e+000  1.664287861e+002  1.664989010e+002  1.7e-008 1.00  
40  2.8e-005 2.4e-002 1.7e-003 1.00e+000  1.664335290e+002  1.664966264e+002  1.5e-008 1.03  
41  2.5e-005 2.2e-002 1.5e-003 1.00e+000  1.664377892e+002  1.664945721e+002  1.3e-008 1.05  
42  2.3e-005 2.1e-002 1.4e-003 1.00e+000  1.664416163e+002  1.664927171e+002  1.2e-008 1.06  
43  2.0e-005 2.0e-002 1.2e-003 1.00e+000  1.664450547e+002  1.664910424e+002  1.1e-008 1.09  
44  1.8e-005 1.8e-002 1.1e-003 1.00e+000  1.664481441e+002  1.664895306e+002  9.8e-009 1.11  
45  1.6e-005 1.7e-002 1.0e-003 1.00e+000  1.664509203e+002  1.664881663e+002  8.8e-009 1.14  
46  1.5e-005 1.6e-002 9.1e-004 1.00e+000  1.664534154e+002  1.664869352e+002  7.9e-009 1.16  
47  1.3e-005 1.6e-002 8.2e-004 1.00e+000  1.664556579e+002  1.664858246e+002  7.1e-009 1.17  
48  1.2e-005 1.5e-002 7.3e-004 1.00e+000  1.664576737e+002  1.664848228e+002  6.4e-009 1.20  
49  1.1e-005 1.4e-002 6.6e-004 1.00e+000  1.664594858e+002  1.664839194e+002  5.8e-009 1.22  
50  9.7e-006 1.3e-002 5.9e-004 1.00e+000  1.664611151e+002  1.664831047e+002  5.2e-009 1.25  
51  8.7e-006 1.3e-002 5.3e-004 1.00e+000  1.664625800e+002  1.664823703e+002  4.7e-009 1.26  
52  7.9e-006 1.2e-002 4.8e-004 1.00e+000  1.664638973e+002  1.664817083e+002  4.2e-009 1.28  
53  7.1e-006 1.2e-002 4.3e-004 1.00e+000  1.664650820e+002  1.664811116e+002  3.8e-009 1.31  
54  6.4e-006 1.2e-002 3.9e-004 1.00e+000  1.664661475e+002  1.664805740e+002  3.4e-009 1.33  
55  5.7e-006 1.1e-002 3.5e-004 1.00e+000  1.664671058e+002  1.664800895e+002  3.1e-009 1.36  
56  5.2e-006 1.1e-002 3.2e-004 1.00e+000  1.664679677e+002  1.664796530e+002  2.8e-009 1.38  
57  4.6e-006 1.1e-002 2.8e-004 1.00e+000  1.664687431e+002  1.664792598e+002  2.5e-009 1.39  
58  4.2e-006 1.0e-002 2.6e-004 1.00e+000  1.664694406e+002  1.664789056e+002  2.2e-009 1.42  
59  3.8e-006 1.0e-002 2.3e-004 1.00e+000  1.664700680e+002  1.664785865e+002  2.0e-009 1.44  
60  3.4e-006 9.9e-003 2.1e-004 1.00e+000  1.664706323e+002  1.664782990e+002  1.8e-009 1.45  
61  3.0e-006 9.7e-003 1.9e-004 1.00e+000  1.664711400e+002  1.664780400e+002  1.6e-009 1.48  
62  2.7e-006 9.5e-003 1.7e-004 1.00e+000  1.664715968e+002  1.664778068e+002  1.5e-009 1.50  
63  2.5e-006 9.4e-003 1.5e-004 1.00e+000  1.664720077e+002  1.664775967e+002  1.3e-009 1.53  
64  2.2e-006 9.2e-003 1.4e-004 1.00e+000  1.664723775e+002  1.664774076e+002  1.2e-009 1.55  
65  2.0e-006 9.1e-003 1.2e-004 1.00e+000  1.664727102e+002  1.664772373e+002  1.1e-009 1.56  
66  1.8e-006 9.0e-003 1.1e-004 1.00e+000  1.664730096e+002  1.664770841e+002  9.6e-010 1.59  
67  1.6e-006 8.9e-003 9.9e-005 1.00e+000  1.664732791e+002  1.664769461e+002  8.7e-010 1.61  
68  1.5e-006 8.8e-003 8.9e-005 1.00e+000  1.664735216e+002  1.664768219e+002  7.8e-010 1.64  
69  1.3e-006 8.7e-003 8.0e-005 1.00e+000  1.664737398e+002  1.664767101e+002  7.0e-010 1.66  
70  1.2e-006 8.6e-003 7.2e-005 1.00e+000  1.664739362e+002  1.664766095e+002  6.3e-010 1.67  
71  1.1e-006 8.5e-003 6.5e-005 1.00e+000  1.664741129e+002  1.664765189e+002  5.7e-010 1.70  
72  9.6e-007 8.4e-003 5.9e-005 1.00e+000  1.664742720e+002  1.664764374e+002  5.1e-010 1.72  
73  8.6e-007 8.4e-003 5.3e-005 1.00e+000  1.664744151e+002  1.664763639e+002  4.6e-010 1.75  
74  7.7e-007 8.3e-003 4.7e-005 1.00e+000  1.664745438e+002  1.664762978e+002  4.2e-010 1.76  
75  7.0e-007 8.3e-003 4.3e-005 1.00e+000  1.664746597e+002  1.664762383e+002  3.7e-010 1.80  
76  6.3e-007 8.2e-003 3.8e-005 1.00e+000  1.664747639e+002  1.664761847e+002  3.4e-010 1.81  
77  5.6e-007 8.2e-003 3.5e-005 1.00e+000  1.664748577e+002  1.664761364e+002  3.0e-010 1.83  
78  5.1e-007 8.1e-003 3.1e-005 1.00e+000  1.664749420e+002  1.664760929e+002  2.7e-010 1.86  
79  4.6e-007 8.1e-003 2.8e-005 1.00e+000  1.664750179e+002  1.664760537e+002  2.5e-010 1.88  
80  4.1e-007 8.1e-003 2.5e-005 1.00e+000  1.664750862e+002  1.664760183e+002  2.2e-010 1.91  
81  3.7e-007 8.0e-003 2.3e-005 1.00e+000  1.664751476e+002  1.664759865e+002  2.0e-010 1.92  
82  3.3e-007 8.0e-003 2.0e-005 1.00e+000  1.664752028e+002  1.664759579e+002  1.8e-010 1.95  
83  3.0e-007 8.0e-003 1.8e-005 1.00e+000  1.664752525e+002  1.664759320e+002  1.6e-010 1.97  
84  2.7e-007 7.9e-003 1.7e-005 1.00e+000  1.664752972e+002  1.664759088e+002  1.4e-010 2.00  
85  2.4e-007 7.9e-003 1.5e-005 1.00e+000  1.664753374e+002  1.664758878e+002  1.3e-010 2.02  
86  2.2e-007 7.9e-003 1.3e-005 1.00e+000  1.664753736e+002  1.664758690e+002  1.2e-010 2.03  
87  2.0e-007 7.9e-003 1.2e-005 1.00e+000  1.664754061e+002  1.664758520e+002  1.1e-010 2.06  
88  1.8e-007 7.9e-003 1.1e-005 1.00e+000  1.664754354e+002  1.664758367e+002  9.5e-011 2.08  
89  1.6e-007 7.8e-003 9.8e-006 1.00e+000  1.664754618e+002  1.664758229e+002  8.5e-011 2.11  
90  1.4e-007 7.8e-003 8.8e-006 1.00e+000  1.664754855e+002  1.664758105e+002  7.7e-011 2.13  
91  1.3e-007 7.8e-003 7.9e-006 1.00e+000  1.664755068e+002  1.664757994e+002  6.9e-011 2.14  
92  1.2e-007 7.8e-003 7.1e-006 1.00e+000  1.664755261e+002  1.664757893e+002  6.2e-011 2.17  
93  1.0e-007 7.8e-003 6.4e-006 1.00e+000  1.664755433e+002  1.664757803e+002  5.6e-011 2.19  
94  9.4e-008 7.8e-003 5.8e-006 1.00e+000  1.664755589e+002  1.664757722e+002  5.0e-011 2.22  
95  8.5e-008 7.7e-003 5.2e-006 1.00e+000  1.664755729e+002  1.664757648e+002  4.5e-011 2.23  
96  7.6e-008 7.7e-003 4.7e-006 1.00e+000  1.664755855e+002  1.664757582e+002  4.1e-011 2.25  
97  6.9e-008 7.7e-003 4.2e-006 9.98e-001  1.664755968e+002  1.664757523e+002  3.7e-011 2.28  
98  6.2e-008 7.7e-003 3.8e-006 9.99e-001  1.664756070e+002  1.664757470e+002  3.3e-011 2.30  
99  5.6e-008 7.7e-003 3.4e-006 1.00e+000  1.664756162e+002  1.664757421e+002  3.0e-011 2.33  
100 5.0e-008 7.7e-003 3.1e-006 1.00e+000  1.664756245e+002  1.664757378e+002  2.7e-011 2.34  
101 4.5e-008 7.7e-003 2.8e-006 1.00e+000  1.664756319e+002  1.664757339e+002  2.4e-011 2.38  
102 4.1e-008 7.7e-003 2.5e-006 9.99e-001  1.664756386e+002  1.664757304e+002  2.2e-011 2.39  
103 3.6e-008 7.6e-003 2.2e-006 9.98e-001  1.664756446e+002  1.664757273e+002  2.0e-011 2.42  
104 3.3e-008 7.6e-003 2.0e-006 9.99e-001  1.664756500e+002  1.664757244e+002  1.8e-011 2.44  
105 3.0e-008 7.6e-003 1.8e-006 1.00e+000  1.664756549e+002  1.664757219e+002  1.6e-011 2.47  
106 2.7e-008 7.6e-003 1.6e-006 9.99e-001  1.664756593e+002  1.664757196e+002  1.4e-011 2.48  
107 2.4e-008 7.6e-003 1.5e-006 9.98e-001  1.664756632e+002  1.664757175e+002  1.3e-011 2.52  
108 2.2e-008 6.8e-003 1.3e-006 1.00e+000  1.664756669e+002  1.664757156e+002  1.2e-011 2.53  
109 1.9e-008 6.1e-003 1.2e-006 9.96e-001  1.664756700e+002  1.664757139e+002  1.0e-011 2.56  
110 1.8e-008 5.5e-003 1.1e-006 1.01e+000  1.664756730e+002  1.664757123e+002  9.4e-012 2.58  
111 1.6e-008 5.0e-003 9.6e-007 9.96e-001  1.664756756e+002  1.664757110e+002  8.5e-012 2.61  
112 1.4e-008 4.5e-003 8.7e-007 1.00e+000  1.664756779e+002  1.664757098e+002  7.6e-012 2.63  
113 1.3e-008 4.0e-003 7.8e-007 1.00e+000  1.664756800e+002  1.664757087e+002  6.9e-012 2.66  
114 1.2e-008 3.6e-003 7.0e-007 1.01e+000  1.664756820e+002  1.664757076e+002  6.2e-012 2.67  
115 1.1e-008 3.3e-003 6.3e-007 1.01e+000  1.664756838e+002  1.664757066e+002  5.6e-012 2.70  
116 9.5e-009 2.9e-003 5.7e-007 1.00e+000  1.664756853e+002  1.664757057e+002  5.0e-012 2.72  
117 2.7e-009 3.0e-004 5.8e-008 9.93e-001  1.664756974e+002  1.664756995e+002  5.3e-013 2.75  
Interior-point optimizer terminated. Time: 2.75. 

Optimizer terminated. Time: 2.77    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6647569744e+002   nrm: 2e+001   Viol.  con: 7e-008   var: 0e+000 
  Dual.    obj: 1.6647569954e+002   nrm: 1e+003   Viol.  con: 0e+000   var: 2e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.8 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.02    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 870
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3453              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 : 1.48e+004         after factor           : 1.47e+005       
Factor     - dense dim.             : 0                 flops                  : 2.89e+007       
Factor     - GP saved nzs           : 3.32e+004         GP saved flops         : 9.06e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.2e+005 0.00e+000  -1.222123631e+005 2.000000000e+000  1.0e+000 0.06  
1   1.7e+003 2.2e+003 8.8e+004 -9.71e-001 -1.214682219e+005 2.621415548e+000  7.2e-001 0.08  
2   8.7e+002 1.2e+003 4.7e+004 -9.59e-001 -1.191647335e+005 4.623440304e+000  3.8e-001 0.11  
3   2.9e+002 3.8e+002 1.5e+004 -9.21e-001 -1.101037963e+005 2.013991935e+001  1.3e-001 0.13  
4   2.9e+002 3.8e+002 1.5e+004 -7.69e-001 -1.078923757e+005 1.958151072e+003  1.3e-001 0.16  
5   1.2e+002 1.5e+002 6.2e+003 -7.59e-001 -8.630971618e+004 6.301572746e+003  5.2e-002 0.17  
6   2.8e+001 3.7e+001 1.5e+003 -4.39e-001 -3.492611673e+004 1.229725946e+004  1.2e-002 0.20  
7   1.8e+001 2.4e+001 9.8e+002 4.55e-001  -2.548393674e+004 7.216508870e+003  8.1e-003 0.22  
8   1.0e+001 1.4e+001 5.5e+002 6.39e-001  -1.544228746e+004 4.340977769e+003  4.6e-003 0.25  
9   4.1e+000 5.4e+000 2.2e+002 8.09e-001  -6.282618875e+003 1.997763249e+003  1.8e-003 0.27  
10  2.1e+000 2.8e+000 1.1e+002 9.45e-001  -3.056142662e+003 1.213484155e+003  9.4e-004 0.30  
11  8.8e-001 1.2e+000 4.8e+001 9.86e-001  -1.181195182e+003 6.551469962e+002  4.0e-004 0.31  
12  8.4e-001 1.1e+000 4.6e+001 9.63e-001  -1.150216358e+003 6.236806040e+002  3.8e-004 0.34  
13  5.4e-001 7.1e-001 2.9e+001 9.72e-001  -6.970086075e+002 4.450833278e+002  2.5e-004 0.36  
14  3.6e-001 4.8e-001 1.9e+001 1.00e+000  -3.879629390e+002 3.654628760e+002  1.6e-004 0.39  
15  1.2e-001 1.9e-001 6.9e+000 9.97e-001  -4.395156411e+001 2.233187142e+002  5.9e-005 0.41  
16  8.0e-002 1.3e-001 4.5e+000 1.02e+000  2.985138016e+001  2.012752456e+002  3.8e-005 0.44  
17  5.6e-002 8.7e-002 3.1e+000 1.02e+000  7.434142832e+001  1.934294465e+002  2.7e-005 0.45  
18  1.4e-002 1.6e-001 7.8e-001 1.02e+000  1.446084738e+002  1.739074334e+002  6.6e-006 0.48  
19  5.3e-003 1.9e-001 3.0e-001 1.00e+000  1.580769952e+002  1.693860509e+002  2.5e-006 0.50  
20  2.1e-003 2.4e-001 1.2e-001 1.01e+000  1.630566891e+002  1.676367200e+002  1.0e-006 0.52  
21  8.4e-004 1.3e-001 5.0e-002 1.00e+000  1.651006976e+002  1.669759992e+002  4.3e-007 0.55  
22  2.8e-004 1.1e-001 1.7e-002 1.01e+000  1.659965523e+002  1.666301312e+002  1.5e-007 0.56  
23  1.2e-004 9.4e-002 7.4e-003 1.01e+000  1.662528679e+002  1.665270457e+002  6.5e-008 0.59  
24  1.1e-004 8.6e-002 6.6e-003 1.01e+000  1.662737316e+002  1.665204415e+002  5.8e-008 0.61  
25  9.7e-005 7.8e-002 6.0e-003 1.01e+000  1.662908796e+002  1.665128336e+002  5.2e-008 0.64  
26  8.7e-005 7.1e-002 5.4e-003 1.01e+000  1.663064187e+002  1.665061209e+002  4.7e-008 0.66  
27  7.9e-005 6.5e-002 4.8e-003 1.01e+000  1.663203315e+002  1.665000172e+002  4.2e-008 0.69  
28  7.1e-005 5.9e-002 4.4e-003 1.01e+000  1.663328210e+002  1.664945006e+002  3.8e-008 0.70  
29  6.4e-005 5.4e-002 3.9e-003 1.01e+000  1.663440283e+002  1.664895093e+002  3.4e-008 0.73  
30  5.7e-005 4.9e-002 3.5e-003 1.01e+000  1.663540869e+002  1.664849947e+002  3.1e-008 0.75  
31  5.2e-005 4.5e-002 3.2e-003 1.01e+000  1.663631152e+002  1.664809117e+002  2.8e-008 0.78  
32  4.6e-005 4.1e-002 2.9e-003 1.00e+000  1.663712198e+002  1.664772198e+002  2.5e-008 0.80  
33  4.2e-005 3.8e-002 2.6e-003 1.00e+000  1.663784959e+002  1.664738821e+002  2.3e-008 0.83  
34  3.8e-005 3.5e-002 2.3e-003 1.00e+000  1.663850289e+002  1.664708653e+002  2.0e-008 0.84  
35  3.4e-005 3.2e-002 2.1e-003 1.00e+000  1.663908954e+002  1.664681389e+002  1.8e-008 0.86  
36  3.0e-005 3.0e-002 1.9e-003 1.00e+000  1.663961638e+002  1.664656755e+002  1.6e-008 0.89  
37  2.7e-005 2.8e-002 1.7e-003 1.00e+000  1.664008955e+002  1.664634499e+002  1.5e-008 0.91  
38  2.5e-005 2.6e-002 1.5e-003 1.00e+000  1.664051455e+002  1.664614395e+002  1.3e-008 0.94  
39  2.2e-005 2.4e-002 1.4e-003 1.00e+000  1.664089632e+002  1.664596237e+002  1.2e-008 0.95  
40  2.0e-005 2.2e-002 1.2e-003 1.00e+000  1.664123927e+002  1.664579838e+002  1.1e-008 0.98  
41  1.8e-005 2.1e-002 1.1e-003 1.00e+000  1.664154738e+002  1.664565031e+002  9.7e-009 1.00  
42  1.6e-005 1.9e-002 1.0e-003 1.00e+000  1.664182420e+002  1.664551661e+002  8.8e-009 1.03  
43  1.5e-005 1.8e-002 9.0e-004 1.00e+000  1.664207292e+002  1.664539592e+002  7.9e-009 1.05  
44  1.3e-005 1.7e-002 8.1e-004 1.00e+000  1.664229643e+002  1.664528698e+002  7.1e-009 1.08  
45  1.2e-005 1.6e-002 7.3e-004 1.00e+000  1.664249727e+002  1.664518866e+002  6.4e-009 1.09  
46  1.1e-005 1.5e-002 6.5e-004 1.00e+000  1.664267778e+002  1.664509993e+002  5.7e-009 1.11  
47  9.6e-006 1.5e-002 5.9e-004 1.00e+000  1.664284001e+002  1.664501987e+002  5.2e-009 1.14  
48  8.6e-006 1.4e-002 5.3e-004 1.00e+000  1.664298583e+002  1.664494765e+002  4.7e-009 1.16  
49  7.7e-006 1.3e-002 4.8e-004 1.00e+000  1.664311691e+002  1.664488249e+002  4.2e-009 1.19  
50  7.0e-006 1.3e-002 4.3e-004 1.00e+000  1.664323474e+002  1.664482373e+002  3.8e-009 1.20  
51  6.3e-006 1.2e-002 3.9e-004 1.00e+000  1.664334067e+002  1.664477073e+002  3.4e-009 1.24  
52  5.6e-006 1.2e-002 3.5e-004 1.00e+000  1.664343591e+002  1.664472294e+002  3.1e-009 1.25  
53  5.1e-006 1.2e-002 3.1e-004 1.00e+000  1.664352154e+002  1.664467985e+002  2.8e-009 1.28  
54  4.6e-006 1.1e-002 2.8e-004 1.00e+000  1.664359853e+002  1.664464099e+002  2.5e-009 1.30  
55  4.1e-006 1.1e-002 2.5e-004 1.00e+000  1.664366775e+002  1.664460596e+002  2.2e-009 1.31  
56  3.7e-006 1.1e-002 2.3e-004 1.00e+000  1.664372999e+002  1.664457438e+002  2.0e-009 1.34  
57  3.3e-006 1.0e-002 2.1e-004 1.00e+000  1.664378596e+002  1.664454590e+002  1.8e-009 1.36  
58  3.0e-006 1.0e-002 1.8e-004 1.00e+000  1.664383629e+002  1.664452022e+002  1.6e-009 1.39  
59  2.7e-006 9.8e-003 1.7e-004 1.00e+000  1.664388154e+002  1.664449708e+002  1.5e-009 1.41  
60  2.4e-006 9.6e-003 1.5e-004 1.00e+000  1.664392225e+002  1.664447623e+002  1.3e-009 1.44  
61  2.2e-006 9.5e-003 1.3e-004 1.00e+000  1.664395886e+002  1.664445745e+002  1.2e-009 1.45  
62  2.0e-006 9.3e-003 1.2e-004 1.00e+000  1.664399179e+002  1.664444052e+002  1.1e-009 1.47  
63  1.8e-006 9.2e-003 1.1e-004 1.00e+000  1.664402142e+002  1.664442527e+002  9.6e-010 1.50  
64  1.6e-006 9.0e-003 9.8e-005 1.00e+000  1.664404807e+002  1.664441154e+002  8.6e-010 1.52  
65  1.4e-006 8.9e-003 8.8e-005 1.00e+000  1.664407205e+002  1.664439917e+002  7.8e-010 1.55  
66  1.3e-006 8.8e-003 8.0e-005 1.00e+000  1.664409362e+002  1.664438803e+002  7.0e-010 1.58  
67  1.2e-006 8.7e-003 7.2e-005 1.00e+000  1.664411303e+002  1.664437800e+002  6.3e-010 1.61  
68  1.0e-006 8.6e-003 6.5e-005 1.00e+000  1.664413049e+002  1.664436896e+002  5.7e-010 1.63  
69  9.4e-007 8.5e-003 5.8e-005 1.00e+000  1.664414620e+002  1.664436082e+002  5.1e-010 1.66  
70  8.5e-007 8.5e-003 5.2e-005 1.00e+000  1.664416033e+002  1.664435349e+002  4.6e-010 1.67  
71  7.6e-007 8.4e-003 4.7e-005 1.00e+000  1.664417304e+002  1.664434689e+002  4.1e-010 1.70  
72  6.9e-007 8.3e-003 4.2e-005 1.00e+000  1.664418447e+002  1.664434094e+002  3.7e-010 1.72  
73  6.2e-007 8.3e-003 3.8e-005 1.00e+000  1.664419476e+002  1.664433558e+002  3.3e-010 1.75  
74  5.6e-007 8.2e-003 3.4e-005 1.00e+000  1.664420402e+002  1.664433076e+002  3.0e-010 1.77  
75  5.0e-007 8.2e-003 3.1e-005 1.00e+000  1.664421234e+002  1.664432641e+002  2.7e-010 1.80  
76  4.5e-007 8.1e-003 2.8e-005 1.00e+000  1.664421983e+002  1.664432249e+002  2.4e-010 1.81  
77  4.1e-007 8.1e-003 2.5e-005 1.00e+000  1.664422657e+002  1.664431896e+002  2.2e-010 1.84  
78  3.7e-007 8.0e-003 2.2e-005 1.00e+000  1.664423263e+002  1.664431578e+002  2.0e-010 1.86  
79  3.3e-007 8.0e-003 2.0e-005 1.00e+000  1.664423808e+002  1.664431292e+002  1.8e-010 1.89  
80  3.0e-007 8.0e-003 1.8e-005 1.00e+000  1.664424299e+002  1.664431035e+002  1.6e-010 1.91  
81  2.7e-007 7.9e-003 1.6e-005 1.00e+000  1.664424740e+002  1.664430803e+002  1.4e-010 1.94  
82  2.4e-007 7.9e-003 1.5e-005 1.00e+000  1.664425138e+002  1.664430594e+002  1.3e-010 1.95  
83  2.2e-007 7.9e-003 1.3e-005 1.00e+000  1.664425495e+002  1.664430406e+002  1.2e-010 1.97  
84  1.9e-007 7.9e-003 1.2e-005 1.00e+000  1.664425817e+002  1.664430237e+002  1.1e-010 2.00  
85  1.7e-007 7.8e-003 1.1e-005 1.00e+000  1.664426107e+002  1.664430084e+002  9.5e-011 2.02  
86  1.6e-007 7.8e-003 9.7e-006 1.00e+000  1.664426367e+002  1.664429947e+002  8.5e-011 2.05  
87  1.4e-007 7.8e-003 8.7e-006 1.00e+000  1.664426602e+002  1.664429824e+002  7.7e-011 2.06  
88  1.3e-007 7.8e-003 7.8e-006 1.00e+000  1.664426813e+002  1.664429713e+002  6.9e-011 2.09  
89  1.1e-007 7.8e-003 7.1e-006 1.00e+000  1.664427003e+002  1.664429613e+002  6.2e-011 2.11  
90  1.0e-007 7.7e-003 6.4e-006 1.00e+000  1.664427174e+002  1.664429523e+002  5.6e-011 2.14  
91  9.3e-008 7.7e-003 5.7e-006 1.00e+000  1.664427328e+002  1.664429442e+002  5.0e-011 2.16  
92  8.3e-008 7.7e-003 5.1e-006 1.00e+000  1.664427467e+002  1.664429370e+002  4.5e-011 2.17  
93  7.5e-008 7.7e-003 4.6e-006 1.00e+000  1.664427591e+002  1.664429304e+002  4.1e-011 2.20  
94  6.8e-008 7.7e-003 4.2e-006 1.00e+000  1.664427704e+002  1.664429245e+002  3.7e-011 2.22  
95  6.1e-008 7.7e-003 3.8e-006 9.99e-001  1.664427805e+002  1.664429192e+002  3.3e-011 2.25  
96  5.5e-008 7.7e-003 3.4e-006 9.99e-001  1.664427896e+002  1.664429144e+002  3.0e-011 2.27  
97  4.9e-008 7.7e-003 3.0e-006 1.00e+000  1.664427978e+002  1.664429101e+002  2.7e-011 2.30  
98  4.4e-008 7.6e-003 2.7e-006 1.00e+000  1.664428051e+002  1.664429063e+002  2.4e-011 2.31  
99  4.0e-008 7.6e-003 2.5e-006 1.00e+000  1.664428118e+002  1.664429028e+002  2.2e-011 2.33  
100 3.6e-008 7.6e-003 2.2e-006 1.00e+000  1.664428177e+002  1.664428996e+002  1.9e-011 2.36  
101 3.2e-008 7.6e-003 2.0e-006 9.98e-001  1.664428231e+002  1.664428968e+002  1.8e-011 2.38  
102 2.9e-008 6.8e-003 1.8e-006 1.00e+000  1.664428279e+002  1.664428942e+002  1.6e-011 2.41  
103 2.6e-008 6.2e-003 1.6e-006 9.99e-001  1.664428323e+002  1.664428920e+002  1.4e-011 2.42  
104 2.4e-008 5.5e-003 1.5e-006 1.00e+000  1.664428362e+002  1.664428899e+002  1.3e-011 2.45  
105 2.1e-008 5.0e-003 1.3e-006 1.00e+000  1.664428397e+002  1.664428881e+002  1.2e-011 2.47  
106 1.9e-008 4.5e-003 1.2e-006 9.99e-001  1.664428429e+002  1.664428864e+002  1.0e-011 2.48  
107 1.7e-008 4.0e-003 1.1e-006 1.00e+000  1.664428457e+002  1.664428849e+002  9.3e-012 2.52  
108 1.6e-008 3.6e-003 9.5e-007 1.00e+000  1.664428483e+002  1.664428835e+002  8.4e-012 2.53  
109 1.4e-008 3.3e-003 8.6e-007 9.98e-001  1.664428506e+002  1.664428823e+002  7.5e-012 2.56  
110 1.3e-008 2.9e-003 7.7e-007 9.93e-001  1.664428527e+002  1.664428812e+002  6.8e-012 2.58  
111 1.1e-008 2.7e-003 7.0e-007 1.01e+000  1.664428546e+002  1.664428802e+002  6.1e-012 2.59  
112 1.0e-008 2.4e-003 6.3e-007 1.00e+000  1.664428563e+002  1.664428794e+002  5.5e-012 2.63  
113 9.1e-009 2.1e-003 5.6e-007 9.88e-001  1.664428578e+002  1.664428786e+002  5.0e-012 2.64  
114 8.3e-009 1.9e-003 5.1e-007 1.03e+000  1.664428594e+002  1.664428777e+002  4.5e-012 2.67  
115 7.5e-009 1.7e-003 4.6e-007 1.01e+000  1.664428606e+002  1.664428771e+002  4.1e-012 2.69  
116 6.8e-009 1.6e-003 4.1e-007 1.01e+000  1.664428617e+002  1.664428765e+002  3.7e-012 2.72  
117 8.2e-009 1.4e-003 3.7e-007 9.96e-001  1.664428627e+002  1.664428760e+002  3.3e-012 2.73  
118 6.3e-009 1.3e-003 3.3e-007 9.81e-001  1.664428635e+002  1.664428757e+002  3.0e-012 2.77  
119 8.5e-009 1.1e-003 3.0e-007 8.86e-001  1.664428642e+002  1.664428757e+002  2.7e-012 2.78  
120 3.0e-008 1.0e-003 2.7e-007 4.72e+000  1.664428648e+002  1.664428762e+002  2.4e-012 2.80  
121 2.4e-008 9.3e-004 2.4e-007 8.93e-001  1.664428654e+002  1.664428765e+002  2.2e-012 2.83  
122 2.1e-008 8.4e-004 2.2e-007 9.87e-001  1.664428660e+002  1.664428763e+002  2.0e-012 2.84  
123 1.9e-008 7.5e-004 2.0e-007 1.00e+000  1.664428665e+002  1.664428758e+002  1.8e-012 2.88  
124 8.0e-008 7.0e-004 1.8e-007 9.59e-001  1.664428669e+002  1.664428743e+002  1.6e-012 2.89  
125 7.3e-008 6.3e-004 1.6e-007 9.87e-001  1.664428673e+002  1.664428740e+002  1.4e-012 2.92  
126 6.5e-008 5.6e-004 1.5e-007 9.77e-001  1.664428677e+002  1.664428738e+002  1.3e-012 2.94  
127 5.9e-008 5.1e-004 1.3e-007 9.92e-001  1.664428681e+002  1.664428735e+002  1.2e-012 2.97  
128 5.3e-008 4.6e-004 1.2e-007 9.56e-001  1.664428684e+002  1.664428733e+002  1.0e-012 2.98  
129 4.8e-008 4.1e-004 1.1e-007 9.93e-001  1.664428687e+002  1.664428731e+002  9.4e-013 3.00  
Interior-point optimizer terminated. Time: 3.02. 

Optimizer terminated. Time: 3.03    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6644286872e+002   nrm: 2e+001   Viol.  con: 1e-006   var: 0e+000 
  Dual.    obj: 1.6644287314e+002   nrm: 1e+003   Viol.  con: 0e+000   var: 3e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.05 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 870
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3453              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 : 1.48e+004         after factor           : 1.47e+005       
Factor     - dense dim.             : 0                 flops                  : 2.89e+007       
Factor     - GP saved nzs           : 3.32e+004         GP saved flops         : 9.06e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.2e+005 0.00e+000  -1.222116609e+005 2.000000000e+000  1.0e+000 0.09  
1   1.7e+003 2.2e+003 8.8e+004 -9.71e-001 -1.214675652e+005 2.621160176e+000  7.2e-001 0.13  
2   8.7e+002 1.2e+003 4.7e+004 -9.59e-001 -1.191638444e+005 4.622536072e+000  3.8e-001 0.14  
3   2.9e+002 3.8e+002 1.5e+004 -9.21e-001 -1.100828575e+005 2.015276023e+001  1.3e-001 0.17  
4   2.8e+002 3.8e+002 1.5e+004 -7.68e-001 -1.078685042e+005 1.962375391e+003  1.3e-001 0.20  
5   1.2e+002 1.5e+002 6.2e+003 -7.59e-001 -8.628852702e+004 6.284974452e+003  5.1e-002 0.22  
6   2.6e+001 3.5e+001 1.4e+003 -4.38e-001 -3.277713115e+004 1.252867417e+004  1.2e-002 0.25  
7   1.7e+001 2.3e+001 9.2e+002 4.96e-001  -2.417021116e+004 7.054859359e+003  7.6e-003 0.27  
8   1.0e+001 1.4e+001 5.5e+002 6.62e-001  -1.523959566e+004 4.371470581e+003  4.5e-003 0.28  
9   4.1e+000 5.4e+000 2.2e+002 8.12e-001  -6.295564733e+003 2.007176307e+003  1.8e-003 0.30  
10  2.1e+000 2.8e+000 1.1e+002 9.44e-001  -3.085063934e+003 1.208148796e+003  9.4e-004 0.33  
11  8.5e-001 1.1e+000 4.6e+001 9.85e-001  -1.138485055e+003 6.392875647e+002  3.9e-004 0.34  
12  8.3e-001 1.1e+000 4.5e+001 9.54e-001  -1.127974063e+003 6.137246114e+002  3.8e-004 0.36  
13  5.3e-001 7.0e-001 2.9e+001 9.70e-001  -6.831007882e+002 4.399018478e+002  2.4e-004 0.39  
14  3.5e-001 4.7e-001 1.9e+001 1.00e+000  -3.741645029e+002 3.597468492e+002  1.6e-004 0.41  
15  1.1e-001 1.8e-001 6.3e+000 9.97e-001  -2.734678863e+001 2.170570107e+002  5.4e-005 0.42  
16  8.5e-002 1.4e-001 4.7e+000 1.02e+000  2.373021044e+001  2.051007702e+002  4.0e-005 0.44  
17  4.6e-002 8.1e-002 2.6e+000 1.02e+000  9.157529602e+001  1.887679090e+002  2.2e-005 0.47  
18  1.5e-002 8.5e-002 8.7e-001 1.02e+000  1.419709537e+002  1.746774650e+002  7.3e-006 0.48  
19  7.6e-003 7.3e-002 4.3e-001 1.01e+000  1.541223306e+002  1.701620930e+002  3.6e-006 0.52  
20  1.7e-003 1.7e-001 1.0e-001 1.01e+000  1.636745322e+002  1.675279443e+002  8.7e-007 0.53  
21  1.1e-003 1.2e-001 6.4e-002 9.78e-001  1.647246484e+002  1.670996376e+002  5.4e-007 0.55  
22  3.6e-004 1.2e-001 2.3e-002 9.87e-001  1.658339199e+002  1.666857627e+002  1.9e-007 0.58  
23  1.5e-004 1.0e-001 9.7e-003 1.00e+000  1.661720119e+002  1.665344483e+002  8.4e-008 0.59  
24  5.9e-005 9.2e-002 3.8e-003 1.01e+000  1.663243007e+002  1.664664877e+002  3.3e-008 0.63  
25  2.9e-005 7.9e-002 1.9e-003 1.01e+000  1.663745492e+002  1.664438954e+002  1.6e-008 0.64  
26  2.6e-005 7.2e-002 1.7e-003 1.01e+000  1.663801383e+002  1.664425947e+002  1.5e-008 0.67  
27  2.3e-005 6.6e-002 1.5e-003 1.01e+000  1.663842917e+002  1.664404814e+002  1.3e-008 0.69  
28  2.1e-005 6.0e-002 1.4e-003 1.01e+000  1.663881204e+002  1.664386817e+002  1.2e-008 0.72  
29  1.9e-005 5.5e-002 1.2e-003 1.01e+000  1.663915467e+002  1.664370430e+002  1.1e-008 0.73  
30  1.7e-005 5.0e-002 1.1e-003 1.00e+000  1.663946272e+002  1.664355668e+002  9.7e-009 0.75  
31  1.5e-005 4.6e-002 9.9e-004 1.00e+000  1.663973944e+002  1.664342343e+002  8.7e-009 0.78  
32  1.4e-005 4.2e-002 8.9e-004 1.00e+000  1.663998808e+002  1.664330321e+002  7.8e-009 0.80  
33  1.2e-005 3.9e-002 8.0e-004 1.00e+000  1.664021151e+002  1.664319476e+002  7.0e-009 0.83  
34  1.1e-005 3.6e-002 7.2e-004 1.00e+000  1.664041229e+002  1.664309692e+002  6.3e-009 0.84  
35  1.0e-005 3.3e-002 6.5e-004 1.00e+000  1.664059275e+002  1.664300868e+002  5.7e-009 0.86  
36  9.1e-006 3.0e-002 5.9e-004 1.00e+000  1.664075494e+002  1.664292910e+002  5.1e-009 0.89  
37  8.2e-006 2.8e-002 5.3e-004 1.00e+000  1.664090074e+002  1.664285734e+002  4.6e-009 0.91  
38  7.4e-006 2.6e-002 4.7e-004 1.00e+000  1.664103181e+002  1.664279263e+002  4.2e-009 0.94  
39  6.6e-006 2.4e-002 4.3e-004 1.00e+000  1.664114964e+002  1.664273430e+002  3.7e-009 0.95  
40  6.0e-006 2.3e-002 3.8e-004 1.00e+000  1.664125559e+002  1.664268171e+002  3.4e-009 0.97  
41  5.4e-006 2.1e-002 3.5e-004 1.00e+000  1.664135085e+002  1.664263432e+002  3.0e-009 1.00  
42  4.8e-006 2.0e-002 3.1e-004 1.00e+000  1.664143651e+002  1.664259160e+002  2.7e-009 1.01  
43  4.3e-006 1.9e-002 2.8e-004 1.00e+000  1.664151354e+002  1.664255310e+002  2.5e-009 1.03  
44  3.9e-006 1.8e-002 2.5e-004 1.00e+000  1.664158282e+002  1.664251840e+002  2.2e-009 1.06  
45  3.5e-006 1.7e-002 2.3e-004 1.00e+000  1.664164512e+002  1.664248713e+002  2.0e-009 1.08  
46  3.2e-006 1.6e-002 2.0e-004 1.00e+000  1.664170114e+002  1.664245895e+002  1.8e-009 1.09  
47  2.8e-006 1.5e-002 1.8e-004 1.00e+000  1.664175153e+002  1.664243356e+002  1.6e-009 1.13  
48  2.6e-006 1.4e-002 1.7e-004 1.00e+000  1.664179685e+002  1.664241068e+002  1.5e-009 1.14  
49  2.3e-006 1.4e-002 1.5e-004 1.00e+000  1.664183762e+002  1.664239006e+002  1.3e-009 1.16  
50  2.1e-006 1.3e-002 1.3e-004 1.00e+000  1.664187430e+002  1.664237150e+002  1.2e-009 1.19  
51  1.9e-006 1.3e-002 1.2e-004 1.00e+000  1.664190730e+002  1.664235478e+002  1.1e-009 1.20  
52  1.7e-006 1.2e-002 1.1e-004 1.00e+000  1.664193698e+002  1.664233972e+002  9.5e-010 1.22  
53  1.5e-006 1.2e-002 9.8e-005 1.00e+000  1.664196370e+002  1.664232616e+002  8.6e-010 1.25  
54  1.4e-006 1.1e-002 8.8e-005 1.00e+000  1.664198773e+002  1.664231395e+002  7.7e-010 1.26  
55  1.2e-006 1.1e-002 7.9e-005 1.00e+000  1.664200935e+002  1.664230296e+002  6.9e-010 1.28  
56  1.1e-006 1.1e-002 7.1e-005 1.00e+000  1.664202881e+002  1.664229305e+002  6.3e-010 1.30  
57  9.9e-007 1.0e-002 6.4e-005 1.00e+000  1.664204631e+002  1.664228414e+002  5.6e-010 1.33  
58  8.9e-007 1.0e-002 5.8e-005 1.00e+000  1.664206206e+002  1.664227611e+002  5.1e-010 1.34  
59  8.0e-007 9.9e-003 5.2e-005 1.00e+000  1.664207623e+002  1.664226887e+002  4.6e-010 1.36  
60  7.2e-007 9.7e-003 4.7e-005 1.00e+000  1.664208898e+002  1.664226236e+002  4.1e-010 1.39  
61  6.5e-007 9.5e-003 4.2e-005 1.00e+000  1.664210045e+002  1.664225649e+002  3.7e-010 1.41  
62  5.9e-007 9.3e-003 3.8e-005 1.00e+000  1.664211077e+002  1.664225121e+002  3.3e-010 1.44  
63  5.3e-007 9.2e-003 3.4e-005 1.00e+000  1.664212005e+002  1.664224645e+002  3.0e-010 1.45  
64  4.8e-007 9.0e-003 3.1e-005 1.00e+000  1.664212840e+002  1.664224216e+002  2.7e-010 1.47  
65  4.3e-007 8.9e-003 2.8e-005 1.00e+000  1.664213591e+002  1.664223830e+002  2.4e-010 1.50  
66  3.9e-007 8.8e-003 2.5e-005 1.00e+000  1.664214267e+002  1.664223482e+002  2.2e-010 1.51  
67  3.5e-007 8.7e-003 2.2e-005 1.00e+000  1.664214875e+002  1.664223168e+002  2.0e-010 1.55  
68  3.1e-007 8.6e-003 2.0e-005 1.00e+000  1.664215422e+002  1.664222886e+002  1.8e-010 1.56  
69  2.8e-007 8.5e-003 1.8e-005 1.00e+000  1.664215914e+002  1.664222632e+002  1.6e-010 1.59  
70  2.5e-007 8.4e-003 1.6e-005 1.00e+000  1.664216357e+002  1.664222403e+002  1.4e-010 1.63  
71  2.3e-007 8.4e-003 1.5e-005 1.00e+000  1.664216755e+002  1.664222197e+002  1.3e-010 1.64  
72  2.0e-007 8.3e-003 1.3e-005 1.00e+000  1.664217114e+002  1.664222011e+002  1.2e-010 1.67  
73  1.8e-007 8.2e-003 1.2e-005 1.00e+000  1.664217436e+002  1.664221844e+002  1.0e-010 1.69  
74  1.7e-007 8.2e-003 1.1e-005 1.00e+000  1.664217726e+002  1.664221694e+002  9.4e-011 1.72  
75  1.5e-007 8.1e-003 9.6e-006 1.00e+000  1.664217988e+002  1.664221558e+002  8.5e-011 1.73  
76  1.3e-007 8.1e-003 8.7e-006 1.00e+000  1.664218223e+002  1.664221437e+002  7.6e-011 1.75  
77  1.2e-007 8.0e-003 7.8e-006 1.00e+000  1.664218434e+002  1.664221327e+002  6.8e-011 1.78  
78  1.1e-007 8.0e-003 7.0e-006 1.00e+000  1.664218625e+002  1.664221228e+002  6.2e-011 1.80  
79  9.8e-008 8.0e-003 6.3e-006 1.00e+000  1.664218796e+002  1.664221139e+002  5.5e-011 1.83  
80  8.8e-008 7.9e-003 5.7e-006 1.00e+000  1.664218951e+002  1.664221059e+002  5.0e-011 1.84  
81  7.9e-008 7.9e-003 5.1e-006 9.99e-001  1.664219089e+002  1.664220987e+002  4.5e-011 1.88  
82  7.1e-008 7.9e-003 4.6e-006 1.00e+000  1.664219214e+002  1.664220922e+002  4.0e-011 1.89  
83  6.4e-008 7.9e-003 4.1e-006 1.00e+000  1.664219327e+002  1.664220864e+002  3.6e-011 1.91  
84  5.8e-008 7.8e-003 3.7e-006 1.00e+000  1.664219428e+002  1.664220811e+002  3.3e-011 1.94  
85  5.2e-008 7.8e-003 3.4e-006 1.00e+000  1.664219519e+002  1.664220764e+002  2.9e-011 1.95  
86  4.7e-008 7.8e-003 3.0e-006 9.99e-001  1.664219601e+002  1.664220721e+002  2.7e-011 1.98  
87  4.5e-008 7.0e-003 2.7e-006 1.00e+000  1.664219675e+002  1.664220682e+002  2.4e-011 2.00  
88  3.9e-008 6.3e-003 2.4e-006 1.00e+000  1.664219741e+002  1.664220648e+002  2.1e-011 2.02  
89  3.5e-008 5.7e-003 2.2e-006 1.00e+000  1.664219801e+002  1.664220617e+002  1.9e-011 2.05  
90  3.2e-008 5.1e-003 2.0e-006 9.98e-001  1.664219854e+002  1.664220589e+002  1.7e-011 2.06  
91  2.9e-008 4.6e-003 1.8e-006 9.99e-001  1.664219903e+002  1.664220564e+002  1.6e-011 2.08  
92  2.6e-008 4.1e-003 1.6e-006 9.97e-001  1.664219946e+002  1.664220542e+002  1.4e-011 2.11  
93  2.3e-008 3.7e-003 1.4e-006 1.00e+000  1.664219986e+002  1.664220521e+002  1.3e-011 2.13  
94  2.1e-008 3.3e-003 1.3e-006 1.00e+000  1.664220021e+002  1.664220503e+002  1.1e-011 2.16  
95  1.9e-008 3.0e-003 1.2e-006 9.98e-001  1.664220053e+002  1.664220486e+002  1.0e-011 2.17  
96  1.7e-008 2.7e-003 1.1e-006 1.00e+000  1.664220081e+002  1.664220471e+002  9.3e-012 2.20  
97  1.5e-008 2.4e-003 9.5e-007 1.00e+000  1.664220107e+002  1.664220458e+002  8.3e-012 2.22  
98  1.4e-008 2.2e-003 8.5e-007 1.00e+000  1.664220130e+002  1.664220446e+002  7.5e-012 2.23  
99  1.2e-008 2.0e-003 7.7e-007 1.01e+000  1.664220152e+002  1.664220435e+002  6.8e-012 2.27  
100 1.1e-008 1.8e-003 6.9e-007 1.00e+000  1.664220170e+002  1.664220425e+002  6.1e-012 2.28  
101 9.9e-009 1.6e-003 6.2e-007 9.98e-001  1.664220187e+002  1.664220416e+002  5.5e-012 2.31  
102 8.9e-009 1.4e-003 5.6e-007 9.97e-001  1.664220202e+002  1.664220408e+002  4.9e-012 2.33  
103 8.1e-009 1.3e-003 5.0e-007 9.99e-001  1.664220216e+002  1.664220401e+002  4.4e-012 2.36  
104 7.3e-009 1.2e-003 4.5e-007 9.95e-001  1.664220228e+002  1.664220395e+002  4.0e-012 2.38  
105 6.5e-009 1.1e-003 4.1e-007 1.00e+000  1.664220239e+002  1.664220389e+002  3.6e-012 2.41  
106 5.9e-009 9.5e-004 3.7e-007 1.00e+000  1.664220249e+002  1.664220384e+002  3.2e-012 2.42  
107 5.3e-009 8.5e-004 3.3e-007 1.00e+000  1.664220258e+002  1.664220380e+002  2.9e-012 2.45  
108 4.8e-009 7.7e-004 3.0e-007 1.00e+000  1.664220266e+002  1.664220375e+002  2.6e-012 2.47  
109 2.8e-008 6.9e-004 2.7e-007 1.04e+000  1.664220274e+002  1.664220370e+002  2.4e-012 2.48  
110 2.5e-008 6.2e-004 2.4e-007 1.00e+000  1.664220281e+002  1.664220368e+002  2.2e-012 2.52  
111 2.1e-008 5.6e-004 2.2e-007 9.99e-001  1.664220286e+002  1.664220365e+002  1.9e-012 2.53  
112 2.6e-005 5.0e-004 2.0e-007 -3.46e+000 1.664220286e+002  1.664220382e+002  1.7e-012 2.56  
113 2.5e-005 4.9e-004 1.9e-007 9.66e-001  1.664220288e+002  1.664220456e+002  1.3e-012 2.58  
114 2.2e-005 4.4e-004 1.7e-007 9.99e-001  1.664220326e+002  1.664220539e+002  1.1e-012 2.61  
115 2.0e-005 3.9e-004 1.5e-007 1.01e+000  1.664220325e+002  1.664220514e+002  9.9e-013 2.63  
Interior-point optimizer terminated. Time: 2.63. 

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

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6642203251e+002   nrm: 2e+001   Viol.  con: 2e-003   var: 0e+000 
  Dual.    obj: 1.6642205142e+002   nrm: 1e+003   Viol.  con: 0e+000   var: 9e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.67 seconds.
Using solver 'mosek'
Solving for 1748 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1749            
  Cones                  : 0               
  Scalar variables       : 6101            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 471
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 870
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3453              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 : 1.48e+004         after factor           : 1.47e+005       
Factor     - dense dim.             : 0                 flops                  : 2.89e+007       
Factor     - GP saved nzs           : 3.32e+004         GP saved flops         : 9.06e+005       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.2e+005 0.00e+000  -1.222107726e+005 2.000000000e+000  1.0e+000 0.09  
1   1.7e+003 2.2e+003 8.8e+004 -9.71e-001 -1.214665807e+005 2.621211724e+000  7.2e-001 0.13  
2   8.7e+002 1.2e+003 4.7e+004 -9.59e-001 -1.191609265e+005 4.623830382e+000  3.8e-001 0.16  
3   2.9e+002 3.8e+002 1.5e+004 -9.21e-001 -1.100676265e+005 2.016523942e+001  1.3e-001 0.17  
4   2.8e+002 3.8e+002 1.5e+004 -7.68e-001 -1.078531695e+005 1.963403751e+003  1.3e-001 0.20  
5   1.2e+002 1.5e+002 6.2e+003 -7.58e-001 -8.623777521e+004 6.284285009e+003  5.1e-002 0.22  
6   2.6e+001 3.5e+001 1.4e+003 -4.38e-001 -3.254096842e+004 1.253725743e+004  1.2e-002 0.25  
7   1.7e+001 2.3e+001 9.1e+002 5.00e-001  -2.398745748e+004 7.020282101e+003  7.6e-003 0.27  
8   1.0e+001 1.3e+001 5.4e+002 6.65e-001  -1.514052973e+004 4.351351154e+003  4.5e-003 0.28  
9   4.1e+000 5.4e+000 2.2e+002 8.13e-001  -6.238379304e+003 1.993343166e+003  1.8e-003 0.31  
10  2.1e+000 2.7e+000 1.1e+002 9.44e-001  -3.061044977e+003 1.203829098e+003  9.3e-004 0.33  
11  8.5e-001 1.1e+000 4.6e+001 9.85e-001  -1.145429950e+003 6.324606894e+002  3.9e-004 0.36  
12  8.3e-001 1.1e+000 4.5e+001 9.52e-001  -1.136620444e+003 6.075583148e+002  3.8e-004 0.38  
13  5.2e-001 7.0e-001 2.9e+001 9.70e-001  -6.808638359e+002 4.358294676e+002  2.4e-004 0.39  
14  3.4e-001 4.6e-001 1.9e+001 1.00e+000  -3.640950668e+002 3.552965833e+002  1.6e-004 0.42  
15  1.1e-001 1.8e-001 6.2e+000 9.96e-001  -2.495409105e+001 2.163906604e+002  5.3e-005 0.44  
16  8.4e-002 1.3e-001 4.7e+000 1.02e+000  2.492793763e+001  2.047993787e+002  4.0e-005 0.45  
17  4.3e-002 7.9e-002 2.4e+000 1.02e+000  9.670034637e+001  1.873779831e+002  2.0e-005 0.48  
18  1.2e-002 1.7e-001 6.5e-001 1.02e+000  1.484301026e+002  1.729535582e+002  5.5e-006 0.50  
19  3.5e-003 2.0e-001 2.0e-001 1.01e+000  1.606421497e+002  1.683354733e+002  1.7e-006 0.53  
20  1.4e-003 1.2e-001 8.3e-002 1.01e+000  1.641623570e+002  1.672579017e+002  7.1e-007 0.55  
21  4.7e-004 1.1e-001 2.8e-002 1.00e+000  1.656592130e+002  1.667113725e+002  2.4e-007 0.58  
22  2.2e-004 8.7e-002 1.4e-002 1.01e+000  1.660533350e+002  1.665578710e+002  1.2e-007 0.59  
23  9.3e-005 8.4e-002 5.8e-003 1.01e+000  1.662596616e+002  1.664732795e+002  5.1e-008 0.61  
24  8.4e-005 7.7e-002 5.2e-003 1.01e+000  1.662767700e+002  1.664690310e+002  4.6e-008 0.64  
25  7.5e-005 7.0e-002 4.7e-003 1.01e+000  1.662899640e+002  1.664629286e+002  4.1e-008 0.66  
26  6.8e-005 6.4e-002 4.2e-003 1.01e+000  1.663020343e+002  1.664576548e+002  3.7e-008 0.69  
27  6.1e-005 5.8e-002 3.8e-003 1.01e+000  1.663128294e+002  1.664528471e+002  3.3e-008 0.70  
28  5.5e-005 5.3e-002 3.4e-003 1.01e+000  1.663225231e+002  1.664485059e+002  3.0e-008 0.73  
29  4.9e-005 4.9e-002 3.1e-003 1.01e+000  1.663312218e+002  1.664445790e+002  2.7e-008 0.75  
30  4.4e-005 4.5e-002 2.8e-003 1.01e+000  1.663390297e+002  1.664410289e+002  2.4e-008 0.77  
31  4.0e-005 4.1e-002 2.5e-003 1.01e+000  1.663460387e+002  1.664378198e+002  2.2e-008 0.80  
32  3.6e-005 3.8e-002 2.2e-003 1.01e+000  1.663523313e+002  1.664349196e+002  2.0e-008 0.81  
33  3.2e-005 3.5e-002 2.0e-003 1.00e+000  1.663579816e+002  1.664322990e+002  1.8e-008 0.84  
34  2.9e-005 3.2e-002 1.8e-003 1.00e+000  1.663630556e+002  1.664299315e+002  1.6e-008 0.86  
35  2.6e-005 3.0e-002 1.6e-003 1.00e+000  1.663676126e+002  1.664277931e+002  1.4e-008 0.89  
36  2.4e-005 2.8e-002 1.5e-003 1.00e+000  1.663717058e+002  1.664258618e+002  1.3e-008 0.92  
37  2.1e-005 2.6e-002 1.3e-003 1.00e+000  1.663753826e+002  1.664241179e+002  1.2e-008 0.94  
38  1.9e-005 2.4e-002 1.2e-003 1.00e+000  1.663786858e+002  1.664225434e+002  1.0e-008 0.97  
39  1.7e-005 2.2e-002 1.1e-003 1.00e+000  1.663816536e+002  1.664211221e+002  9.4e-009 0.98  
40  1.6e-005 2.1e-002 9.6e-004 1.00e+000  1.663843202e+002  1.664198392e+002  8.5e-009 1.01  
41  1.4e-005 2.0e-002 8.7e-004 1.00e+000  1.663867164e+002  1.664186814e+002  7.6e-009 1.03  
42  1.3e-005 1.8e-002 7.8e-004 1.00e+000  1.663888699e+002  1.664176366e+002  6.9e-009 1.06  
43  1.1e-005 1.7e-002 7.0e-004 1.00e+000  1.663908053e+002  1.664166940e+002  6.2e-009 1.08  
44  1.0e-005 1.7e-002 6.3e-004 1.00e+000  1.663925449e+002  1.664158437e+002  5.6e-009 1.11  
45  9.2e-006 1.6e-002 5.7e-004 1.00e+000  1.663941086e+002  1.664150767e+002  5.0e-009 1.14  
46  8.2e-006 1.5e-002 5.1e-004 1.00e+000  1.663955144e+002  1.664143849e+002  4.5e-009 1.16  
47  7.4e-006 1.4e-002 4.6e-004 1.00e+000  1.663967781e+002  1.664137611e+002  4.1e-009 1.19  
48  6.7e-006 1.4e-002 4.1e-004 1.00e+000  1.663979144e+002  1.664131986e+002  3.7e-009 1.20  
49  6.0e-006 1.3e-002 3.7e-004 1.00e+000  1.663989360e+002  1.664126915e+002  3.3e-009 1.23  
50  5.4e-006 1.3e-002 3.4e-004 1.00e+000  1.663998547e+002  1.664122344e+002  3.0e-009 1.25  
51  4.9e-006 1.2e-002 3.0e-004 1.00e+000  1.664006807e+002  1.664118223e+002  2.7e-009 1.26  
52  4.4e-006 1.2e-002 2.7e-004 1.00e+000  1.664014235e+002  1.664114508e+002  2.4e-009 1.30  
53  3.9e-006 1.1e-002 2.4e-004 1.00e+000  1.664020915e+002  1.664111159e+002  2.2e-009 1.31  
54  3.5e-006 1.1e-002 2.2e-004 1.00e+000  1.664026922e+002  1.664108141e+002  1.9e-009 1.34  
55  3.2e-006 1.1e-002 2.0e-004 1.00e+000  1.664032323e+002  1.664105420e+002  1.7e-009 1.36  
56  2.9e-006 1.1e-002 1.8e-004 1.00e+000  1.664037181e+002  1.664102968e+002  1.6e-009 1.39  
57  2.6e-006 1.0e-002 1.6e-004 1.00e+000  1.664041551e+002  1.664100758e+002  1.4e-009 1.41  
58  2.3e-006 1.0e-002 1.4e-004 1.00e+000  1.664045482e+002  1.664098768e+002  1.3e-009 1.42  
59  2.1e-006 9.9e-003 1.3e-004 1.00e+000  1.664049017e+002  1.664096975e+002  1.1e-009 1.45  
60  1.9e-006 9.7e-003 1.2e-004 1.00e+000  1.664052198e+002  1.664095360e+002  1.0e-009 1.47  
61  1.7e-006 9.5e-003 1.1e-004 1.00e+000  1.664055060e+002  1.664093906e+002  9.3e-010 1.50  
62  1.5e-006 9.4e-003 9.5e-005 1.00e+000  1.664057635e+002  1.664092596e+002  8.4e-010 1.51  
63  1.4e-006 9.2e-003 8.5e-005 1.00e+000  1.664059951e+002  1.664091416e+002  7.5e-010 1.53  
64  1.2e-006 9.1e-003 7.7e-005 1.00e+000  1.664062035e+002  1.664090354e+002  6.8e-010 1.56  
65  1.1e-006 9.0e-003 6.9e-005 1.00e+000  1.664063910e+002  1.664089397e+002  6.1e-010 1.58  
66  1.0e-006 8.9e-003 6.2e-005 1.00e+000  1.664065597e+002  1.664088535e+002  5.5e-010 1.61  
67  9.0e-007 8.8e-003 5.6e-005 1.00e+000  1.664067115e+002  1.664087759e+002  4.9e-010 1.63  
68  8.1e-007 8.7e-003 5.0e-005 1.00e+000  1.664068480e+002  1.664087060e+002  4.4e-010 1.64  
69  7.3e-007 8.6e-003 4.5e-005 1.00e+000  1.664069709e+002  1.664086430e+002  4.0e-010 1.67  
70  6.6e-007 8.5e-003 4.1e-005 1.00e+000  1.664070814e+002  1.664085863e+002  3.6e-010 1.69  
71  5.9e-007 8.5e-003 3.7e-005 1.00e+000  1.664071808e+002  1.664085352e+002  3.2e-010 1.72  
72  5.3e-007 8.4e-003 3.3e-005 1.00e+000  1.664072702e+002  1.664084892e+002  2.9e-010 1.73  
73  4.8e-007 8.4e-003 3.0e-005 1.00e+000  1.664073506e+002  1.664084477e+002  2.6e-010 1.76  
74  4.3e-007 8.3e-003 2.7e-005 1.00e+000  1.664074229e+002  1.664084104e+002  2.4e-010 1.78  
75  3.9e-007 8.3e-003 2.4e-005 1.00e+000  1.664074880e+002  1.664083767e+002  2.1e-010 1.81  
76  3.5e-007 8.2e-003 2.2e-005 1.00e+000  1.664075465e+002  1.664083463e+002  1.9e-010 1.83  
77  3.1e-007 8.2e-003 2.0e-005 1.00e+000  1.664075992e+002  1.664083190e+002  1.7e-010 1.84  
78  2.8e-007 8.1e-003 1.8e-005 1.00e+000  1.664076466e+002  1.664082944e+002  1.6e-010 1.88  
79  2.5e-007 8.1e-003 1.6e-005 1.00e+000  1.664076892e+002  1.664082723e+002  1.4e-010 1.89  
80  2.3e-007 8.1e-003 1.4e-005 1.00e+000  1.664077275e+002  1.664082523e+002  1.3e-010 1.92  
81  2.1e-007 8.0e-003 1.3e-005 1.00e+000  1.664077621e+002  1.664082344e+002  1.1e-010 1.94  
82  1.9e-007 8.0e-003 1.2e-005 1.00e+000  1.664077931e+002  1.664082182e+002  1.0e-010 1.97  
83  1.7e-007 8.0e-003 1.0e-005 1.00e+000  1.664078210e+002  1.664082036e+002  9.2e-011 1.98  
84  1.5e-007 7.9e-003 9.3e-006 1.00e+000  1.664078462e+002  1.664081905e+002  8.2e-011 2.02  
85  1.4e-007 7.9e-003 8.4e-006 1.00e+000  1.664078688e+002  1.664081787e+002  7.4e-011 2.03  
86  1.2e-007 7.9e-003 7.6e-006 1.00e+000  1.664078892e+002  1.664081681e+002  6.7e-011 2.06  
87  1.1e-007 7.9e-003 6.8e-006 1.00e+000  1.664079075e+002  1.664081585e+002  6.0e-011 2.08  
88  9.9e-008 7.8e-003 6.1e-006 1.00e+000  1.664079240e+002  1.664081499e+002  5.4e-011 2.09  
89  8.9e-008 7.8e-003 5.5e-006 1.00e+000  1.664079388e+002  1.664081422e+002  4.9e-011 2.13  
90  8.0e-008 7.8e-003 5.0e-006 1.00e+000  1.664079522e+002  1.664081352e+002  4.4e-011 2.14  
91  7.2e-008 7.8e-003 4.5e-006 1.00e+000  1.664079642e+002  1.664081289e+002  3.9e-011 2.17  
92  6.5e-008 7.8e-003 4.0e-006 1.00e+000  1.664079750e+002  1.664081232e+002  3.5e-011 2.19  
93  5.8e-008 7.8e-003 3.6e-006 9.99e-001  1.664079848e+002  1.664081181e+002  3.2e-011 2.22  
94  5.2e-008 7.8e-003 3.3e-006 9.99e-001  1.664079935e+002  1.664081135e+002  2.9e-011 2.23  
95  4.7e-008 7.7e-003 2.9e-006 1.00e+000  1.664080014e+002  1.664081094e+002  2.6e-011 2.25  
96  4.3e-008 7.7e-003 2.6e-006 1.00e+000  1.664080085e+002  1.664081057e+002  2.3e-011 2.28  
97  3.8e-008 7.7e-003 2.4e-006 9.99e-001  1.664080149e+002  1.664081024e+002  2.1e-011 2.30  
98  3.4e-008 7.7e-003 2.1e-006 9.99e-001  1.664080206e+002  1.664080994e+002  1.9e-011 2.33  
99  3.1e-008 7.7e-003 1.9e-006 1.00e+000  1.664080258e+002  1.664080967e+002  1.7e-011 2.34  
100 2.8e-008 7.7e-003 1.7e-006 1.00e+000  1.664080304e+002  1.664080942e+002  1.5e-011 2.36  
101 2.5e-008 7.7e-003 1.6e-006 9.99e-001  1.664080346e+002  1.664080920e+002  1.4e-011 2.39  
102 2.3e-008 7.7e-003 1.4e-006 1.00e+000  1.664080384e+002  1.664080901e+002  1.2e-011 2.41  
103 2.0e-008 7.6e-003 1.3e-006 9.97e-001  1.664080418e+002  1.664080883e+002  1.1e-011 2.44  
104 1.8e-008 6.9e-003 1.1e-006 1.00e+000  1.664080448e+002  1.664080867e+002  1.0e-011 2.45  
105 1.7e-008 6.2e-003 1.0e-006 1.01e+000  1.664080476e+002  1.664080852e+002  9.0e-012 2.47  
106 1.5e-008 5.6e-003 9.2e-007 1.00e+000  1.664080501e+002  1.664080839e+002  8.1e-012 2.50  
107 1.3e-008 5.0e-003 8.3e-007 9.97e-001  1.664080523e+002  1.664080827e+002  7.3e-012 2.52  
108 1.3e-008 4.5e-003 7.5e-007 1.02e+000  1.664080544e+002  1.664080816e+002  6.6e-012 2.53  
109 1.1e-008 4.1e-003 6.7e-007 1.01e+000  1.664080563e+002  1.664080806e+002  6.0e-012 2.56  
110 1.0e-008 3.6e-003 6.0e-007 1.00e+000  1.664080579e+002  1.664080798e+002  5.4e-012 2.58  
111 9.3e-009 3.3e-003 5.4e-007 1.01e+000  1.664080594e+002  1.664080790e+002  4.9e-012 2.61  
112 8.4e-009 3.0e-003 4.9e-007 1.01e+000  1.664080607e+002  1.664080783e+002  4.4e-012 2.63  
113 7.5e-009 2.7e-003 4.4e-007 9.88e-001  1.664080619e+002  1.664080777e+002  4.0e-012 2.66  
114 6.9e-009 2.4e-003 4.0e-007 9.98e-001  1.664080629e+002  1.664080772e+002  3.6e-012 2.67  
115 1.1e-008 2.2e-003 3.6e-007 9.94e-001  1.664080640e+002  1.664080762e+002  3.2e-012 2.70  
116 1.0e-008 1.9e-003 3.2e-007 1.00e+000  1.664080648e+002  1.664080758e+002  2.9e-012 2.72  
117 1.0e-008 1.8e-003 2.9e-007 8.94e-001  1.664080655e+002  1.664080757e+002  2.6e-012 2.73  
118 9.2e-009 1.6e-003 2.6e-007 1.04e+000  1.664080663e+002  1.664080752e+002  2.4e-012 2.77  
119 8.2e-009 1.5e-003 2.3e-007 1.01e+000  1.664080669e+002  1.664080749e+002  2.1e-012 2.78  
120 7.6e-009 1.3e-003 2.1e-007 1.01e+000  1.664080675e+002  1.664080747e+002  1.9e-012 2.81  
121 1.2e-008 1.2e-003 1.9e-007 2.70e+000  1.664080681e+002  1.664080740e+002  1.7e-012 2.83  
122 1.1e-008 1.1e-003 1.7e-007 1.00e+000  1.664080685e+002  1.664080738e+002  1.5e-012 2.84  
123 9.9e-009 9.7e-004 1.5e-007 9.94e-001  1.664080689e+002  1.664080737e+002  1.4e-012 2.88  
124 8.9e-009 8.8e-004 1.4e-007 9.97e-001  1.664080692e+002  1.664080735e+002  1.2e-012 2.89  
125 8.0e-009 7.9e-004 1.2e-007 1.00e+000  1.664080695e+002  1.664080734e+002  1.1e-012 2.92  
126 7.2e-009 7.1e-004 1.1e-007 1.00e+000  1.664080698e+002  1.664080733e+002  1.0e-012 2.94  
127 6.6e-009 6.4e-004 1.0e-007 1.05e+000  1.664080701e+002  1.664080731e+002  9.3e-013 2.95  
Interior-point optimizer terminated. Time: 2.97. 

Optimizer terminated. Time: 2.98    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6640807014e+002   nrm: 2e+001   Viol.  con: 1e-007   var: 0e+000 
  Dual.    obj: 1.6640807311e+002   nrm: 1e+003   Viol.  con: 0e+000   var: 4e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.02 seconds.
Solving took 9 GP solves and 36.1 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: 1.4957411894472056e+110 vs 1.49570207917e+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: sum of nu^T * A did not vanish
WEIGHT DIFFERENCES


Total Fuel Weight Percent Diff: [-92.94683103]


Total Aircraft Weight Percent Diff: [-21.48041435]


Engine Weight Percent Diff: -56.27774589313234


Fuselage Weight Percent Diff: -0.8696958114504642


Payload Weight Percent Diff: [-0.04003556]


VT Weight Percent Diff: -8.60723652224414


HT Weight Percent Diff: -93.23327859649434


Wing Weight Percent Diff: 8.267882867655096




WING DIFFERENCES


Wing Span Percent Diff: -0.0299961250114644


Wing Area Percent Diff: 32.899077030368126




HORIZONTAL TAIL DIFFERENCES


HT Area Percent Diff: 40.487670020285755




VERTICAL TAIL DIFFERENCES




VT Span Percent Diff: -11.022213364298166


VT Area Percent Diff: -60.38672249246082




CRUISE SEGMENT 1 DRAG DIFFERENCES


Overall Cd Percent Diff: [-18.5474118]


L/D Percent Diff: [24.01029603]


Nacelle Cd Percent Diff: [-94.27640648]


HT Cd Percent Diff: [-80.76937891] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-58.00254226] dimensionless


Wing Cd percent Diff: [-14.22928986]
Induced Drag Cd Percent Diff: [1.21854359]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-90.57036499]




FUSELAGE DIFFERENCES




Weight of HB material: -38.35820637691987 


Weight of VB material: 87.82381853902206 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.71260558]

Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 99.188s

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 c:\anaconda2\lib\site-packages (0.24.2)
Requirement already satisfied: numpy>=1.12.0 in c:\anaconda2\lib\site-packages (from pandas) (1.16.4)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in c:\anaconda2\lib\site-packages (from pandas) (2.8.0)
Requirement already satisfied: six>=1.5 in c:\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-4dekmb
  Running command git clone -q https://github.com/convexengineering/gpfit.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-4dekmb'
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Requirement already satisfied: mkl in c:\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 c:\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=aa985ada9a56a34a0a216bdeb4af13134db7570c39a1025efacc583f697e16c2
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-krgol9\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-burrpy
  Running command git clone -q https://github.com/convexengineering/gassolar.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-burrpy'
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.2.2)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek (from gassolar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.24.2)
Requirement already satisfied: gpfit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.8.1 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.9)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.2.3)
Requirement already satisfied: six in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.12.0)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.8.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gassolar==0.0.0.0) (1.0.2)
Requirement already satisfied: mkl in c:\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 c:\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): finished with status 'done'
  Created wheel for gassolar: filename=gassolar-0.0.0.0-cp27-none-any.whl size=4895585 sha256=2cc307215001dd1853096f4fbf4204c110d4adb31b7bf1628e8cdb500c59b407
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-pfnrqq\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 c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\solar
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.2.2)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek (from solar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.24.2)
Requirement already satisfied: gpfit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\gplibrary (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.8.1 in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.9)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.2.3)
Requirement already satisfied: six in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.12.0)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.8.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->solar==0.0.0.0) (1.0.2)
Requirement already satisfied: mkl in c:\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 c:\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=14954 sha256=28999839ab5cf3af6370046ceb52ccf20963fd4fa723e135c2de7774da535111
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-nigi0s\wheels\e3\97\6b\b6c3101ac862c33e80ce983780b03bed9308fedc7582e649c7
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 1.61 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 1632916.9436 but bound is 600000.0000
Warning: Variable Mission.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1259333.2961 but bound is 1000000.0000

N=3
Beginning signomial solve.
Solving took 5 GP solves and 1.56 seconds.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1135 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1036204.4448 but bound is 600000.0000
Warning: Variable Mission1.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1006645.3572 but bound is 1000000.0000

N=5
Beginning signomial solve.
Solving took 5 GP solves and 1.82 seconds.
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1487 but bound is 0.9465
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 989673.4665 but bound is 600000.0000
Warning: Variable Mission2.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1019678.5408 but bound is 1000000.0000

N=7
Beginning signomial solve.
Solving took 5 GP solves and 1.61 seconds.
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 976142.1475 but bound is 600000.0000
Warning: Variable Mission3.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1042059.4123 but bound is 1000000.0000

N=9
Beginning signomial solve.
Solving took 5 GP solves and 2.3 seconds.
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1567 but bound is 0.9465
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1007400.4788 but bound is 600000.0000
Warning: Variable Mission4.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1092545.5152 but bound is 1000000.0000

N=0
Beginning signomial solve.
Solving took 4 GP solves and 1.04 seconds.
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2077 but bound is 600000.0000

N=1
Beginning signomial solve.
Solving took 5 GP solves and 2.36 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 0.8904 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1632919.3776 but bound is 600000.0000
Warning: Variable Mission.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1259329.5070 but bound is 1000000.0000

N=3
Beginning signomial solve.
Solving took 5 GP solves and 2.53 seconds.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1135 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1036209.6021 but bound is 600000.0000
Warning: Variable Mission1.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1006641.3990 but bound is 1000000.0000

N=5
Beginning signomial solve.
Solving took 5 GP solves and 2.51 seconds.
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1487 but bound is 0.9465
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 989673.1341 but bound is 600000.0000
Warning: Variable Mission2.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1019680.6011 but bound is 1000000.0000

N=7
Beginning signomial solve.
Solving took 5 GP solves and 2.49 seconds.
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 976138.7332 but bound is 600000.0000
Warning: Variable Mission3.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1042059.9154 but bound is 1000000.0000

N=9
Beginning signomial solve.
Solving took 5 GP solves and 2.81 seconds.
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1567 but bound is 0.9465
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1007396.6632 but bound is 600000.0000
Warning: Variable Mission4.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1092544.5684 but bound is 1000000.0000

N=0
Beginning signomial solve.
Solving took 4 GP solves and 1.73 seconds.
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119116.3963 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 5.3 seconds.
Allowing negative dual variable(s) as small as -6.409089854045921e-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 671709.7387 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 4.45 seconds.
Allowing negative dual variable(s) as small as -5.059110243720389e-10.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2812 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 729183.6211 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 4.64 seconds.
Allowing negative dual variable(s) as small as -7.327879492396591e-10.
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 802959.6185 but bound is 600000.0000
Using solver 'mosek'
Solving for 7672 variables.
Solving took 2.54 seconds.
Allowing negative dual variable(s) as small as -4.488146621352752e-10.
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 839122.5090 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 5.12 seconds.
Allowing negative dual variable(s) as small as -3.84676352079733e-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 671709.7472 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 4.65 seconds.
Allowing negative dual variable(s) as small as -1.0513827951487807e-09.
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 729183.6354 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 4.89 seconds.
Allowing negative dual variable(s) as small as -4.196616197382457e-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 802959.6052 but bound is 600000.0000
Using solver 'mosek'
Solving for 7672 variables.
Solving took 2.56 seconds.
Allowing negative dual variable(s) as small as -3.7179466705010363e-09.
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 839122.5022 but bound is 600000.0000
Beginning signomial solve.
Solving took 4 GP solves and 0.937 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2076 but bound is 600000.0000
Beginning signomial solve.
Solving took 4 GP solves and 1.09 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2076 but bound is 600000.0000

Running tests...
----------------------------------------------------------------------
c:\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)
..C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\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 290.396s

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 c:\anaconda2\lib\site-packages (0.24.2)
Requirement already satisfied: numpy>=1.12.0 in c:\anaconda2\lib\site-packages (from pandas) (1.16.4)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2019.2)
Requirement already satisfied: python-dateutil>=2.5.0 in c:\anaconda2\lib\site-packages (from pandas) (2.8.0)
Requirement already satisfied: six>=1.5 in c:\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-rhylc_
  Running command git clone -q https://github.com/hoburg/gpfit.git 'c:\users\jenkins\appdata\local\temp\pip-req-build-rhylc_'
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\anaconda2\lib\site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Requirement already satisfied: mkl in c:\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 c:\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=3b7cc3b1470fa49a21d1d891f96299d7f01d60a952e3d3b62850300b1aa0072e
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-kxv7kt\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 c:\users\jenkins\workspace\gpkit_pullrequest_models\buildnode\windows10x64\optimizer\mosek\gplibrary
Requirement already satisfied: numpy>=1.12 in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.9)
Requirement already satisfied: funcsigs; python_version == "2.7" in c:\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=66262 sha256=c310ca8169218fb6fdba7c53c8d4daa6d0bd949845e7fbf8b836ab5f986ca98f
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-wzr64_\wheels\eb\4c\19\5da160becfc0e5fbac9d85b5692dbdf86f88d8bac3bd1ed9ac
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 0.041 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.09 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.027 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.03 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.022 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 0.942 seconds.
Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.073 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.084 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.109 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 2.85 seconds.
Using solver 'mosek'
Solving for 13 variables.
Solving took 0.027 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 0.664 seconds.
Warning: Variable BladeElementProp.BladeElementPerf.cl[:] could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable BladeElementProp.BladeElementPerf.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1619898.2350 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.072 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 1.85 seconds.
Warning: Variable BladeElementProp.BladeElementPerf.cl[:] could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable BladeElementProp.BladeElementPerf.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000
Warning: Variable TailAero.Re could cause inaccurate result because it is above upper bound. Solution is 2220953.3838 but bound is 1000000.0000
Warning: Variable TailAero1.Re could cause inaccurate result because it is above upper bound. Solution is 2499787.9776 but bound is 1000000.0000
Warning: Variable TailAero2.Re could cause inaccurate result because it is above upper bound. Solution is 2223878.3883 but bound is 1000000.0000
Warning: Variable TailAero3.Re could cause inaccurate result because it is above upper bound. Solution is 2223877.9590 but bound is 1000000.0000
Warning: Variable TailAero4.Re could cause inaccurate result because it is above upper bound. Solution is 1853897.1004 but bound is 1000000.0000
Warning: Variable TailAero5.Re could cause inaccurate result because it is above upper bound. Solution is 1853897.1004 but bound is 1000000.0000
Warning: Variable TailAero.Re could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000
Warning: Variable TailAero1.Re could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000
Warning: Variable TailAero2.Re could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable TailAero3.Re could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable TailAero4.Re could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable TailAero5.Re could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable WingAero.Re could cause inaccurate result because it is above upper bound. Solution is 1884891.6332 but bound is 700000.0000
Warning: Variable WingAero1.Re could cause inaccurate result because it is above upper bound. Solution is 1910419.6195 but bound is 700000.0000
Warning: Variable WingAero.Re could cause inaccurate result because it is above upper bound. Solution is 1910412.9866 but bound is 700000.0000
Warning: Variable WingAero1.Re could cause inaccurate result because it is above upper bound. Solution is 1910412.9866 but bound is 700000.0000
SP is not converging! Last GP iteration had a higher cost (3e+03) than the previous one (2.7e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (3e+03) than the previous one (2.7e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (3.4e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (3.4e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
Beginning signomial solve.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.036 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.028 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.025 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.023 seconds.
Solving took 4 GP solves and 0.12 seconds.
Beginning signomial solve.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.114 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.072 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.08 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.094 seconds.
Solving took 4 GP solves and 0.371 seconds.

Running tests...
----------------------------------------------------------------------
..c:\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 16.995s

OK

Generating XML reports...
Cloning into 'eVTOL'...
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adding test for 'models/model_tests.py'

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 6.211s

OK

Generating XML reports...

----------------------------------------------------------------------
Ran 243 tests in 115.500s

OK
pkit@mit.edu or https://github.com/convexengineering/gpkit/issues/new
so we can prevent others from having these errors.

The same goes for any other bugs you encounter with GPkit:
send 'em our way, along with any interesting models, speculative features,
comments, discussions, or clarifications you feel like sharing.

Finally, we hope you find our documentation (https://gpkit.readthedocs.io/)
and engineering-design models (https://github.com/convexengineering/gplibrary/)
to be useful resources for your own applications.

Enjoy!

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

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

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

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

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

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

calling ['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) C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\mosek>exit 0 
INFO: Starting to record.
INFO: Processing JUnit
INFO: [JUnit] - 9 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'C:\Users\jenkins\workspace\gpkit_PullRequest_Models\buildnode\windows10x64\optimizer\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