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  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-55irag\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: gpfit
Successfully installed gpfit-0.1
Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gassolar
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0)
Building wheels for collected packages: gassolar
  Running setup.py bdist_wheel for gassolar: started
  Running setup.py bdist_wheel for gassolar: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-bxq7e5\wheels\08\33\b8\d36cec4e8239569444cd725d0dbfe83a0cfc534951775e5535
Successfully built gassolar
grin 1.2.1 requires argparse>=1.1, which is not installed.
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 0.379 seconds.
Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ 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 1.96 seconds.
Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss 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 0.509 seconds.
Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ 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 1 seconds.
Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss 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 0.936 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1496 but bound is 150000.0000
Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.1345 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 6.18 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0581 but bound is 150000.0000
Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.9086 but bound is 150000.0000
Using solver 'mosek_cli'
Solving for 1250 variables.
Solving took 1.92 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.0147 but bound is 150000.0000
Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.3302 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 4.32 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134552.5355 but bound is 150000.0000
Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.8810 but bound is 150000.0000

Running tests...
----------------------------------------------------------------------
..D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
..
----------------------------------------------------------------------
Ran 4 tests in 59.049s

OK

Generating XML reports...
Cloning into 'jho'...
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0)
grin 1.2.1 requires argparse>=1.1, which is not installed.
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-22rdid
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-eizpdo\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
adding test for 'model/jho.py'
adding test for 'model/print_perf.py'
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.102992681194074e-14.
Allowing negative dual variable(s) as small as -7.504630597510165e-14.
Allowing negative dual variable(s) as small as -1.5090099309000848e-13.
Allowing negative dual variable(s) as small as -1.4924042904262969e-13.
Solving took 4 GP solves and 6.56 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.128276275856436e-14.
Allowing negative dual variable(s) as small as -7.539628643637997e-14.
Allowing negative dual variable(s) as small as -1.5005921852329074e-13.
Allowing negative dual variable(s) as small as -1.489771847551502e-13.
Solving took 4 GP solves and 5.55 seconds.
Allowing negative dual variable(s) as small as -5.182815981941147e-13.
Allowing negative dual variable(s) as small as -1.4302985879011132e-12.
Allowing negative dual variable(s) as small as -4.450120827392823e-13.
Allowing negative dual variable(s) as small as -4.442158446638089e-13.
Allowing negative dual variable(s) as small as -1.2967603336619393e-12.
Allowing negative dual variable(s) as small as -1.0912152258180097e-12.
Allowing negative dual variable(s) as small as -1.0907444652347165e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.4741065189206137e-14.
Allowing negative dual variable(s) as small as -5.6960391505668125e-12.
Allowing negative dual variable(s) as small as -2.0879033542380764e-11.
Allowing negative dual variable(s) as small as -2.088079317958388e-11.
Solving took 4 GP solves and 6.15 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 10.4 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.186389512301659e-13.
Allowing negative dual variable(s) as small as -1.42993776541811e-12.
Allowing negative dual variable(s) as small as -4.443754392235988e-13.
Allowing negative dual variable(s) as small as -4.4523933151463524e-13.
Allowing negative dual variable(s) as small as -1.2969615615851526e-12.
Allowing negative dual variable(s) as small as -1.0912002638280294e-12.
Allowing negative dual variable(s) as small as -1.0913494500469634e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.4538602080197494e-14.
Allowing negative dual variable(s) as small as -5.696055323178633e-12.
Allowing negative dual variable(s) as small as -2.087917922032158e-11.
Allowing negative dual variable(s) as small as -2.0880753961323147e-11.
Solving took 4 GP solves and 9.41 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.32 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417

Running tests...
----------------------------------------------------------------------
....
----------------------------------------------------------------------
Ran 4 tests in 132.144s

OK

Generating XML reports...
Cloning into 'turbofan'...
Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\turbofan
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.8.1)
Building wheels for collected packages: turbofan
  Running setup.py bdist_wheel for turbofan: started
  Running setup.py bdist_wheel for turbofan: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-xg3vx3\wheels\e5\cb\a8\3b11c975e79b3f632de8c1b88ce438a834a6b07b3850d6b107
Successfully built turbofan
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: turbofan
Successfully installed turbofan-0.0.0.0
adding test for 'turbofan/engine_validation.py'
Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528315 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%)

Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485055 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%)


Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 2.615s

OK

Generating XML reports...
Cloning into 'SPaircraft'...
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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-ktezp8
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.8.1)
Building wheels for collected packages: turbofan
  Running setup.py bdist_wheel for turbofan: started
  Running setup.py bdist_wheel for turbofan: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-adzj6e\wheels\49\e6\3a\5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5
Successfully built turbofan
grin 1.2.1 requires argparse>=1.1, which is not installed.
adding test for 'SP_aircraft.py'
Beginning signomial solve.
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1900            
  Cones                  : 0               
  Scalar variables       : 6471            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1015
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1025
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 1025            
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            : 826
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3575              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.11              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.67e+004         after factor           : 1.69e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.290114216e+005 2.000000000e+000  1.0e+000 0.14  
1   1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.268199332e+005 3.700570996e+000  4.8e-001 0.20  
2   3.9e+002 5.0e+002 2.2e+004 -9.36e-001 -1.196731173e+005 1.153832762e+001  1.7e-001 0.23  
3   2.8e+002 3.7e+002 1.6e+004 -8.23e-001 -1.157725499e+005 8.911193657e+001  1.2e-001 0.27  
4   2.8e+002 3.6e+002 1.6e+004 -7.55e-001 -1.127836302e+005 2.530618096e+003  1.2e-001 0.30  
5   6.9e+001 9.0e+001 3.9e+003 -7.46e-001 -7.044561375e+004 1.168298555e+004  3.1e-002 0.33  
6   3.1e+001 4.1e+001 1.8e+003 -1.39e-001 -4.096532654e+004 1.098732371e+004  1.4e-002 0.36  
7   1.6e+001 2.1e+001 9.1e+002 3.72e-001  -2.384884033e+004 6.701248905e+003  7.2e-003 0.39  
8   7.3e+000 9.5e+000 4.1e+002 6.70e-001  -1.130515668e+004 3.761163374e+003  3.3e-003 0.42  
9   3.4e+000 4.4e+000 1.9e+002 8.75e-001  -5.068498667e+003 2.154890886e+003  1.5e-003 0.44  
10  1.7e+000 2.2e+000 9.8e+001 9.56e-001  -2.274239213e+003 1.449630149e+003  7.8e-004 0.47  
11  6.5e-001 8.4e-001 3.7e+001 9.85e-001  -6.386409604e+002 7.708877882e+002  2.9e-004 0.50  
12  5.5e-001 7.6e-001 3.2e+001 9.80e-001  -4.977186201e+002 7.157125316e+002  2.5e-004 0.53  
13  3.9e-001 9.4e-001 2.2e+001 9.74e-001  -2.511527669e+002 6.146396419e+002  1.8e-004 0.58  
14  2.1e-001 6.0e-001 1.2e+001 9.86e-001  2.118551310e+001  4.971611734e+002  9.8e-005 0.61  
15  6.4e-002 2.4e-001 3.8e+000 1.00e+000  2.547904550e+002  4.008091633e+002  3.1e-005 0.67  
16  2.0e-002 1.4e-001 1.2e+000 1.00e+000  3.243515273e+002  3.710547149e+002  9.9e-006 0.75  
17  4.6e-003 1.5e-001 2.8e-001 1.00e+000  3.496092054e+002  3.605442939e+002  2.4e-006 0.80  
18  2.7e-003 1.2e-001 1.7e-001 1.00e+000  3.526527396e+002  3.591730387e+002  1.4e-006 0.84  
19  6.5e-004 1.3e-001 4.1e-002 9.94e-001  3.562031755e+002  3.577903302e+002  3.5e-007 0.89  
20  2.4e-004 9.9e-002 1.5e-002 9.98e-001  3.569203947e+002  3.575142357e+002  1.3e-007 0.94  
21  1.2e-004 7.9e-002 7.5e-003 1.00e+000  3.571413806e+002  3.574309325e+002  6.3e-008 0.98  
22  1.1e-004 7.2e-002 6.8e-003 1.00e+000  3.571621286e+002  3.574227098e+002  5.7e-008 1.01  
23  9.5e-005 6.6e-002 6.1e-003 1.00e+000  3.571807621e+002  3.574152867e+002  5.1e-008 1.06  
24  8.6e-005 6.0e-002 5.5e-003 1.00e+000  3.571975379e+002  3.574086184e+002  4.6e-008 1.09  
25  7.7e-005 5.4e-002 4.9e-003 1.00e+000  3.572126371e+002  3.574026145e+002  4.2e-008 1.14  
26  7.0e-005 4.9e-002 4.4e-003 1.00e+000  3.572262247e+002  3.573972063e+002  3.7e-008 1.17  
27  6.3e-005 4.5e-002 4.0e-003 1.00e+000  3.572384517e+002  3.573923352e+002  3.4e-008 1.20  
28  5.6e-005 4.1e-002 3.6e-003 1.00e+000  3.572494550e+002  3.573879494e+002  3.0e-008 1.25  
29  5.1e-005 3.8e-002 3.2e-003 1.00e+000  3.572593579e+002  3.573840019e+002  2.7e-008 1.28  
30  4.6e-005 3.5e-002 2.9e-003 1.00e+000  3.572682711e+002  3.573804497e+002  2.5e-008 1.31  
31  4.1e-005 3.2e-002 2.6e-003 1.00e+000  3.572762938e+002  3.573772537e+002  2.2e-008 1.36  
32  3.7e-005 2.9e-002 2.4e-003 1.00e+000  3.572835153e+002  3.573743784e+002  2.0e-008 1.39  
33  3.3e-005 2.7e-002 2.1e-003 1.00e+000  3.572900159e+002  3.573717920e+002  1.8e-008 1.44  
34  3.0e-005 2.5e-002 1.9e-003 1.00e+000  3.572958675e+002  3.573694654e+002  1.6e-008 1.47  
35  2.7e-005 2.3e-002 1.7e-003 1.00e+000  3.573011351e+002  3.573673728e+002  1.4e-008 1.51  
36  2.4e-005 2.2e-002 1.5e-003 1.00e+000  3.573058769e+002  3.573654906e+002  1.3e-008 1.56  
37  2.2e-005 2.0e-002 1.4e-003 1.00e+000  3.573101455e+002  3.573637976e+002  1.2e-008 1.59  
38  2.0e-005 1.9e-002 1.3e-003 1.00e+000  3.573139881e+002  3.573622748e+002  1.1e-008 1.64  
39  1.8e-005 1.8e-002 1.1e-003 1.00e+000  3.573174472e+002  3.573609051e+002  9.5e-009 1.67  
40  1.6e-005 1.7e-002 1.0e-003 1.00e+000  3.573205611e+002  3.573596730e+002  8.6e-009 1.70  
41  1.4e-005 1.6e-002 9.1e-004 1.00e+000  3.573233641e+002  3.573585648e+002  7.7e-009 1.75  
42  1.3e-005 1.5e-002 8.2e-004 1.00e+000  3.573258873e+002  3.573575679e+002  6.9e-009 1.78  
43  1.2e-005 1.4e-002 7.4e-004 1.00e+000  3.573281586e+002  3.573566712e+002  6.2e-009 1.81  
44  1.0e-005 1.3e-002 6.7e-004 1.00e+000  3.573302032e+002  3.573558645e+002  5.6e-009 1.86  
45  9.4e-006 1.3e-002 6.0e-004 1.00e+000  3.573320436e+002  3.573551388e+002  5.1e-009 1.89  
46  8.5e-006 1.2e-002 5.4e-004 1.00e+000  3.573337002e+002  3.573544859e+002  4.5e-009 1.94  
47  7.6e-006 1.2e-002 4.9e-004 1.00e+000  3.573351914e+002  3.573538985e+002  4.1e-009 1.97  
48  6.9e-006 1.1e-002 4.4e-004 1.00e+000  3.573365336e+002  3.573533700e+002  3.7e-009 2.01  
49  6.2e-006 1.1e-002 3.9e-004 1.00e+000  3.573377418e+002  3.573528946e+002  3.3e-009 2.04  
50  5.6e-006 1.0e-002 3.5e-004 1.00e+000  3.573388292e+002  3.573524667e+002  3.0e-009 2.08  
51  5.0e-006 1.0e-002 3.2e-004 1.00e+000  3.573398079e+002  3.573520818e+002  2.7e-009 2.12  
52  4.5e-006 9.8e-003 2.9e-004 1.00e+000  3.573406889e+002  3.573517354e+002  2.4e-009 2.15  
53  4.0e-006 9.5e-003 2.6e-004 1.00e+000  3.573414818e+002  3.573514236e+002  2.2e-009 2.20  
54  3.6e-006 9.3e-003 2.3e-004 1.00e+000  3.573421954e+002  3.573511430e+002  2.0e-009 2.31  
55  3.3e-006 9.1e-003 2.1e-004 1.00e+000  3.573428376e+002  3.573508905e+002  1.8e-009 2.36  
56  3.0e-006 8.9e-003 1.9e-004 1.00e+000  3.573434156e+002  3.573506633e+002  1.6e-009 2.40  
57  2.7e-006 8.7e-003 1.7e-004 1.00e+000  3.573439358e+002  3.573504587e+002  1.4e-009 2.46  
58  2.4e-006 8.6e-003 1.5e-004 1.00e+000  3.573444040e+002  3.573502746e+002  1.3e-009 3.14  
59  2.2e-006 8.5e-003 1.4e-004 1.00e+000  3.573448253e+002  3.573501089e+002  1.2e-009 3.18  
60  1.9e-006 8.3e-003 1.2e-004 1.00e+000  3.573452045e+002  3.573499597e+002  1.0e-009 3.21  
61  1.7e-006 8.2e-003 1.1e-004 1.00e+000  3.573455458e+002  3.573498255e+002  9.4e-010 3.26  
62  1.6e-006 8.1e-003 1.0e-004 1.00e+000  3.573458529e+002  3.573497046e+002  8.4e-010 3.37  
63  1.4e-006 8.1e-003 9.0e-005 1.00e+000  3.573461293e+002  3.573495958e+002  7.6e-010 3.85  
64  1.3e-006 8.0e-003 8.1e-005 1.00e+000  3.573463780e+002  3.573494979e+002  6.8e-010 4.15  
65  1.1e-006 7.9e-003 7.3e-005 1.00e+000  3.573466018e+002  3.573494098e+002  6.1e-010 4.65  
66  1.0e-006 7.8e-003 6.6e-005 1.00e+000  3.573468033e+002  3.573493304e+002  5.5e-010 4.70  
67  9.3e-007 7.8e-003 5.9e-005 1.00e+000  3.573469846e+002  3.573492590e+002  5.0e-010 4.74  
68  8.3e-007 7.7e-003 5.3e-005 1.00e+000  3.573471477e+002  3.573491947e+002  4.5e-010 4.77  
69  7.5e-007 7.7e-003 4.8e-005 1.00e+000  3.573472946e+002  3.573491368e+002  4.0e-010 4.80  
70  6.8e-007 7.6e-003 4.3e-005 1.00e+000  3.573474267e+002  3.573490847e+002  3.6e-010 4.84  
71  6.1e-007 7.6e-003 3.9e-005 1.00e+000  3.573475456e+002  3.573490378e+002  3.3e-010 4.87  
72  5.5e-007 7.6e-003 3.5e-005 1.00e+000  3.573476526e+002  3.573489956e+002  2.9e-010 4.91  
73  4.9e-007 7.5e-003 3.1e-005 1.00e+000  3.573477489e+002  3.573489576e+002  2.6e-010 4.95  
74  4.4e-007 7.5e-003 2.8e-005 1.00e+000  3.573478355e+002  3.573489234e+002  2.4e-010 4.98  
75  4.0e-007 7.5e-003 2.5e-005 1.00e+000  3.573479135e+002  3.573488925e+002  2.1e-010 5.01  
76  3.6e-007 7.5e-003 2.3e-005 1.00e+000  3.573479836e+002  3.573488648e+002  1.9e-010 5.04  
77  3.2e-007 7.4e-003 2.1e-005 1.00e+000  3.573480468e+002  3.573488398e+002  1.7e-010 5.09  
78  2.9e-007 7.4e-003 1.9e-005 1.00e+000  3.573481036e+002  3.573488173e+002  1.6e-010 5.12  
79  2.6e-007 7.4e-003 1.7e-005 1.00e+000  3.573481547e+002  3.573487970e+002  1.4e-010 5.13  
80  2.4e-007 7.4e-003 1.5e-005 1.00e+000  3.573482007e+002  3.573487788e+002  1.3e-010 5.16  
81  2.1e-007 7.4e-003 1.3e-005 1.00e+000  3.573482421e+002  3.573487624e+002  1.1e-010 5.20  
82  1.9e-007 7.3e-003 1.2e-005 1.00e+000  3.573482795e+002  3.573487475e+002  1.0e-010 5.23  
83  1.7e-007 7.3e-003 1.1e-005 9.99e-001  3.573483130e+002  3.573487343e+002  9.2e-011 5.29  
84  1.5e-007 7.3e-003 9.8e-006 1.00e+000  3.573483431e+002  3.573487223e+002  8.3e-011 5.30  
85  1.4e-007 7.3e-003 8.9e-006 1.00e+000  3.573483704e+002  3.573487114e+002  7.5e-011 5.34  
86  1.3e-007 7.3e-003 8.0e-006 9.99e-001  3.573483948e+002  3.573487017e+002  6.7e-011 5.38  
87  1.1e-007 7.3e-003 7.2e-006 1.00e+000  3.573484167e+002  3.573486930e+002  6.1e-011 5.40  
88  1.0e-007 7.3e-003 6.5e-006 1.00e+000  3.573484365e+002  3.573486851e+002  5.5e-011 5.41  
89  9.1e-008 7.3e-003 5.8e-006 9.98e-001  3.573484543e+002  3.573486781e+002  4.9e-011 5.52  
90  8.2e-008 7.3e-003 5.2e-006 9.98e-001  3.573484703e+002  3.573486717e+002  4.4e-011 5.69  
91  7.4e-008 7.2e-003 4.7e-006 1.00e+000  3.573484847e+002  3.573486660e+002  4.0e-011 5.80  
92  6.6e-008 7.2e-003 4.2e-006 9.96e-001  3.573484977e+002  3.573486609e+002  3.6e-011 5.96  
93  6.0e-008 7.2e-003 3.8e-006 1.00e+000  3.573485094e+002  3.573486562e+002  3.2e-011 6.35  
94  1.2e-008 1.4e-003 7.4e-007 1.00e+000  3.573485940e+002  3.573486224e+002  6.2e-012 6.58  
95  1.1e-008 1.3e-003 6.7e-007 1.02e+000  3.573485962e+002  3.573486215e+002  5.7e-012 6.62  
96  9.5e-009 1.1e-003 6.0e-007 1.02e+000  3.573485983e+002  3.573486207e+002  5.2e-012 6.66  
97  8.5e-009 1.0e-003 5.4e-007 1.08e+000  3.573486004e+002  3.573486198e+002  4.8e-012 6.68  
98  7.7e-009 9.2e-004 4.9e-007 9.54e-001  3.573486018e+002  3.573486193e+002  4.3e-012 6.71  
99  6.9e-009 8.3e-004 4.4e-007 1.05e+000  3.573486034e+002  3.573486186e+002  4.0e-012 6.74  
100 6.2e-009 7.4e-004 3.9e-007 1.03e+000  3.573486046e+002  3.573486181e+002  3.7e-012 6.77  
101 5.6e-009 6.7e-004 3.5e-007 9.96e-001  3.573486056e+002  3.573486178e+002  3.3e-012 6.80  
102 5.1e-009 6.0e-004 3.2e-007 1.02e+000  3.573486065e+002  3.573486174e+002  3.0e-012 6.85  
103 4.6e-009 5.4e-004 2.9e-007 1.11e+000  3.573486077e+002  3.573486169e+002  2.8e-012 6.88  
104 4.1e-009 4.9e-004 2.6e-007 1.00e+000  3.573486084e+002  3.573486166e+002  2.6e-012 6.91  
105 3.7e-009 4.4e-004 2.3e-007 9.93e-001  3.573486090e+002  3.573486164e+002  2.3e-012 7.21  
106 3.3e-009 4.0e-004 2.1e-007 1.01e+000  3.573486095e+002  3.573486162e+002  2.1e-012 7.35  
107 3.0e-009 3.6e-004 1.9e-007 1.00e+000  3.573486100e+002  3.573486160e+002  1.9e-012 7.47  
108 1.7e-010 2.0e-005 1.0e-008 1.00e+000  3.573486141e+002  3.573486145e+002  1.0e-013 7.88  
Interior-point optimizer terminated. Time: 7.92. 

Optimizer terminated. Time: 8.05    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 3.5734861414e+002   Viol.  con: 2e-009   var: 0e+000 
  Dual.    obj: 3.5734861447e+002   Viol.  con: 0e+000   var: 1e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 8.08 seconds.
result packing took 4.1% of solve time
solution checking took 2.4% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1900            
  Cones                  : 0               
  Scalar variables       : 6471            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1012
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1023
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 1023            
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            : 830
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3579              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 : 1.67e+004         after factor           : 1.72e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.289216044e+005 2.000000000e+000  1.0e+000 0.11  
1   1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.266775833e+005 3.803741995e+000  4.7e-001 0.17  
2   4.4e+002 5.7e+002 2.5e+004 -9.35e-001 -1.207998723e+005 1.084180485e+001  1.9e-001 0.22  
3   2.9e+002 3.7e+002 1.6e+004 -8.43e-001 -1.159533006e+005 6.141739872e+001  1.3e-001 0.25  
4   2.9e+002 3.7e+002 1.6e+004 -7.60e-001 -1.137614547e+005 1.946616189e+003  1.3e-001 0.30  
5   8.6e+001 1.1e+002 4.9e+003 -7.56e-001 -7.873790509e+004 1.029432382e+004  3.8e-002 0.34  
6   2.8e+001 3.7e+001 1.6e+003 -2.75e-001 -3.706476158e+004 1.220641178e+004  1.3e-002 0.61  
7   1.4e+001 1.8e+001 7.7e+002 4.35e-001  -2.030567765e+004 6.163509244e+003  6.0e-003 0.69  
8   7.6e+000 9.8e+000 4.3e+002 7.35e-001  -1.180252319e+004 3.699007682e+003  3.4e-003 0.72  
9   2.9e+000 3.7e+000 1.6e+002 8.69e-001  -4.542573700e+003 1.611196358e+003  1.3e-003 0.75  
10  1.4e+000 1.8e+000 7.9e+001 9.69e-001  -2.009194607e+003 9.676508748e+002  6.2e-004 0.80  
11  9.6e-001 1.2e+000 5.5e+001 9.89e-001  -1.381391070e+003 6.944428100e+002  4.3e-004 0.83  
12  8.4e-001 1.1e+000 4.8e+001 9.74e-001  -1.220057560e+003 6.089997660e+002  3.8e-004 0.87  
13  3.5e-001 4.5e-001 2.0e+001 9.84e-001  -4.954102103e+002 2.767212404e+002  1.6e-004 0.91  
14  1.9e-001 2.6e-001 1.1e+001 1.01e+000  -2.547933824e+002 1.739583138e+002  8.8e-005 0.95  
15  7.8e-002 1.3e-001 4.5e+000 9.99e-001  -8.253601494e+001 9.184408990e+001  3.6e-005 0.98  
16  2.3e-002 1.1e-001 1.4e+000 1.00e+000  -6.423406117e-001 5.294764344e+001  1.1e-005 1.03  
17  1.5e-002 8.3e-002 8.7e-001 1.00e+000  1.306801265e+001  4.649531716e+001  7.1e-006 1.09  
18  2.8e-003 1.4e-001 1.7e-001 1.00e+000  3.161977038e+001  3.829726013e+001  1.4e-006 1.12  
19  1.4e-003 9.8e-002 8.9e-002 1.00e+000  3.387235780e+001  3.730611477e+001  7.5e-007 1.17  
20  4.6e-004 1.0e-001 2.8e-002 1.00e+000  3.549090232e+001  3.658199314e+001  2.4e-007 1.20  
21  2.1e-004 7.9e-002 1.3e-002 1.00e+000  3.589090055e+001  3.640151219e+001  1.1e-007 1.23  
22  1.9e-004 7.1e-002 1.2e-002 1.00e+000  3.592726625e+001  3.638680812e+001  1.0e-007 1.26  
23  1.7e-004 6.5e-002 1.1e-002 1.00e+000  3.595897540e+001  3.637253316e+001  9.1e-008 1.28  
24  1.6e-004 5.9e-002 9.7e-003 1.00e+000  3.598753826e+001  3.635971796e+001  8.1e-008 1.29  
25  1.4e-004 5.4e-002 8.7e-003 1.00e+000  3.601321373e+001  3.634815674e+001  7.3e-008 1.33  
26  1.3e-004 4.9e-002 7.9e-003 1.00e+000  3.603630339e+001  3.633773672e+001  6.6e-008 1.34  
27  1.1e-004 4.5e-002 7.1e-003 1.00e+000  3.605706904e+001  3.632834638e+001  5.9e-008 1.36  
28  1.0e-004 4.1e-002 6.4e-003 1.00e+000  3.607574604e+001  3.631988529e+001  5.3e-008 1.39  
29  9.2e-005 3.8e-002 5.7e-003 1.00e+000  3.609254563e+001  3.631226250e+001  4.8e-008 1.42  
30  8.3e-005 3.5e-002 5.2e-003 1.00e+000  3.610765748e+001  3.630539577e+001  4.3e-008 1.45  
31  7.4e-005 3.2e-002 4.6e-003 1.00e+000  3.612125192e+001  3.629921076e+001  3.9e-008 1.48  
32  6.7e-005 3.0e-002 4.2e-003 1.00e+000  3.613348190e+001  3.629364029e+001  3.5e-008 1.51  
33  6.0e-005 2.7e-002 3.8e-003 1.00e+000  3.614448484e+001  3.628862371e+001  3.2e-008 1.54  
34  5.4e-005 2.5e-002 3.4e-003 1.00e+000  3.615438424e+001  3.628410624e+001  2.8e-008 1.58  
35  4.9e-005 2.3e-002 3.1e-003 1.00e+000  3.616329107e+001  3.628003848e+001  2.6e-008 1.61  
36  4.4e-005 2.2e-002 2.7e-003 1.00e+000  3.617130510e+001  3.627637585e+001  2.3e-008 1.64  
37  3.9e-005 2.0e-002 2.5e-003 1.00e+000  3.617851603e+001  3.627307817e+001  2.1e-008 1.67  
38  3.6e-005 1.9e-002 2.2e-003 1.00e+000  3.618500449e+001  3.627010920e+001  1.9e-008 1.70  
39  3.2e-005 1.8e-002 2.0e-003 1.00e+000  3.619084302e+001  3.626743628e+001  1.7e-008 1.73  
40  2.9e-005 1.7e-002 1.8e-003 1.00e+000  3.619609682e+001  3.626502998e+001  1.5e-008 1.76  
41  2.6e-005 1.6e-002 1.6e-003 1.00e+000  3.620082454e+001  3.626286377e+001  1.4e-008 1.79  
42  2.3e-005 1.5e-002 1.5e-003 1.00e+000  3.620507892e+001  3.626091374e+001  1.2e-008 1.83  
43  2.1e-005 1.4e-002 1.3e-003 1.00e+000  3.620890741e+001  3.625915838e+001  1.1e-008 1.86  
44  1.9e-005 1.3e-002 1.2e-003 1.00e+000  3.621235268e+001  3.625757826e+001  9.9e-009 1.89  
45  1.7e-005 1.3e-002 1.1e-003 1.00e+000  3.621545312e+001  3.625615591e+001  8.9e-009 1.92  
46  1.5e-005 1.2e-002 9.6e-004 1.00e+000  3.621824327e+001  3.625487560e+001  8.0e-009 1.95  
47  1.4e-005 1.2e-002 8.6e-004 1.00e+000  3.622075418e+001  3.625372315e+001  7.2e-009 1.98  
48  1.2e-005 1.1e-002 7.8e-004 1.00e+000  3.622301382e+001  3.625268579e+001  6.5e-009 2.01  
49  1.1e-005 1.1e-002 7.0e-004 1.00e+000  3.622504733e+001  3.625175204e+001  5.9e-009 2.04  
50  1.0e-005 1.1e-002 6.3e-004 1.00e+000  3.622687735e+001  3.625091153e+001  5.3e-009 2.08  
51  9.0e-006 1.0e-002 5.7e-004 1.00e+000  3.622852423e+001  3.625015496e+001  4.7e-009 2.12  
52  8.1e-006 9.9e-003 5.1e-004 1.00e+000  3.623000631e+001  3.624947396e+001  4.3e-009 2.15  
53  7.3e-006 9.6e-003 4.6e-004 1.00e+000  3.623134008e+001  3.624886096e+001  3.8e-009 2.18  
54  6.6e-006 9.4e-003 4.1e-004 1.00e+000  3.623254037e+001  3.624830915e+001  3.5e-009 2.20  
55  5.9e-006 9.2e-003 3.7e-004 1.00e+000  3.623362054e+001  3.624781245e+001  3.1e-009 2.25  
56  5.3e-006 9.0e-003 3.3e-004 1.00e+000  3.623459263e+001  3.624736533e+001  2.8e-009 2.28  
57  4.8e-006 8.8e-003 3.0e-004 1.00e+000  3.623546742e+001  3.624696285e+001  2.5e-009 2.31  
58  4.3e-006 8.6e-003 2.7e-004 1.00e+000  3.623625467e+001  3.624660056e+001  2.3e-009 2.36  
59  3.9e-006 8.5e-003 2.4e-004 1.00e+000  3.623696313e+001  3.624627444e+001  2.0e-009 2.39  
60  3.5e-006 8.4e-003 2.2e-004 1.00e+000  3.623760070e+001  3.624598088e+001  1.8e-009 2.43  
61  3.1e-006 8.3e-003 2.0e-004 1.00e+000  3.623817445e+001  3.624571662e+001  1.7e-009 2.46  
62  2.8e-006 8.1e-003 1.8e-004 1.00e+000  3.623869079e+001  3.624547874e+001  1.5e-009 2.50  
63  2.6e-006 8.1e-003 1.6e-004 1.00e+000  3.623915545e+001  3.624526463e+001  1.3e-009 2.54  
64  2.3e-006 8.0e-003 1.4e-004 1.00e+000  3.623957361e+001  3.624507187e+001  1.2e-009 2.57  
65  2.1e-006 7.9e-003 1.3e-004 1.00e+000  3.623994992e+001  3.624489837e+001  1.1e-009 2.61  
66  1.9e-006 7.8e-003 1.2e-004 1.00e+000  3.624028858e+001  3.624474216e+001  9.8e-010 2.65  
67  1.7e-006 7.7e-003 1.0e-004 1.00e+000  3.624059334e+001  3.624460158e+001  8.8e-010 2.68  
68  1.5e-006 7.7e-003 9.4e-005 1.00e+000  3.624086760e+001  3.624447503e+001  7.9e-010 2.71  
69  1.4e-006 7.6e-003 8.5e-005 1.00e+000  3.624111442e+001  3.624436110e+001  7.1e-010 2.75  
70  1.2e-006 7.6e-003 7.6e-005 1.00e+000  3.624133654e+001  3.624425855e+001  6.4e-010 2.79  
71  1.1e-006 7.5e-003 6.9e-005 1.00e+000  3.624153643e+001  3.624416624e+001  5.8e-010 2.82  
72  9.9e-007 7.5e-003 6.2e-005 1.00e+000  3.624171631e+001  3.624408315e+001  5.2e-010 2.87  
73  8.9e-007 7.5e-003 5.6e-005 1.00e+000  3.624187820e+001  3.624400837e+001  4.7e-010 2.90  
74  8.0e-007 7.4e-003 5.0e-005 1.00e+000  3.624202388e+001  3.624394105e+001  4.2e-010 2.93  
75  7.2e-007 7.4e-003 4.5e-005 1.00e+000  3.624215500e+001  3.624388043e+001  3.8e-010 2.98  
76  6.5e-007 7.4e-003 4.1e-005 1.00e+000  3.624227298e+001  3.624382589e+001  3.4e-010 3.01  
77  5.8e-007 7.3e-003 3.7e-005 1.00e+000  3.624237917e+001  3.624377679e+001  3.1e-010 3.06  
78  5.3e-007 7.3e-003 3.3e-005 1.00e+000  3.624247472e+001  3.624373260e+001  2.8e-010 3.09  
79  4.7e-007 7.3e-003 3.0e-005 1.00e+000  3.624256072e+001  3.624369282e+001  2.5e-010 3.14  
80  4.3e-007 7.3e-003 2.7e-005 1.00e+000  3.624263812e+001  3.624365700e+001  2.2e-010 3.17  
81  3.8e-007 7.2e-003 2.4e-005 1.00e+000  3.624270777e+001  3.624362476e+001  2.0e-010 3.20  
82  3.4e-007 7.2e-003 2.2e-005 1.00e+000  3.624277044e+001  3.624359576e+001  1.8e-010 3.23  
83  3.1e-007 7.2e-003 1.9e-005 1.00e+000  3.624282685e+001  3.624356965e+001  1.6e-010 3.28  
84  2.8e-007 7.2e-003 1.7e-005 1.00e+000  3.624287762e+001  3.624354614e+001  1.5e-010 3.31  
85  2.5e-007 7.2e-003 1.6e-005 1.00e+000  3.624292330e+001  3.624352499e+001  1.3e-010 3.34  
86  2.3e-007 7.2e-003 1.4e-005 9.99e-001  3.624296442e+001  3.624350595e+001  1.2e-010 3.39  
87  2.0e-007 7.1e-003 1.3e-005 1.00e+000  3.624300142e+001  3.624348880e+001  1.1e-010 3.42  
88  1.8e-007 7.1e-003 1.1e-005 1.00e+000  3.624303473e+001  3.624347335e+001  9.6e-011 3.46  
89  1.6e-007 7.1e-003 1.0e-005 1.00e+000  3.624306470e+001  3.624345945e+001  8.7e-011 3.50  
90  1.5e-007 7.1e-003 9.3e-006 1.00e+000  3.624309167e+001  3.624344694e+001  7.8e-011 3.53  
91  1.3e-007 7.1e-003 8.4e-006 1.00e+000  3.624311594e+001  3.624343569e+001  7.0e-011 3.56  
92  1.2e-007 7.1e-003 7.5e-006 9.99e-001  3.624313778e+001  3.624342557e+001  6.3e-011 3.59  
93  1.1e-007 7.1e-003 6.8e-006 1.00e+000  3.624315744e+001  3.624341645e+001  5.7e-011 3.63  
94  9.7e-008 7.1e-003 6.1e-006 1.00e+000  3.624317514e+001  3.624340824e+001  5.1e-011 3.67  
95  8.8e-008 7.1e-003 5.5e-006 1.00e+000  3.624319106e+001  3.624340084e+001  4.6e-011 3.70  
96  7.9e-008 7.1e-003 4.9e-006 9.99e-001  3.624320539e+001  3.624339421e+001  4.1e-011 3.73  
97  7.1e-008 6.4e-003 4.4e-006 1.00e+000  3.624321833e+001  3.624338819e+001  3.7e-011 3.78  
98  6.4e-008 5.7e-003 4.0e-006 9.99e-001  3.624322993e+001  3.624338281e+001  3.4e-011 3.81  
99  5.7e-008 5.1e-003 3.6e-006 1.00e+000  3.624324038e+001  3.624337796e+001  3.0e-011 3.84  
100 5.2e-008 4.6e-003 3.2e-006 1.00e+000  3.624324979e+001  3.624337359e+001  2.7e-011 3.87  
101 4.7e-008 4.2e-003 2.9e-006 1.00e+000  3.624325824e+001  3.624336966e+001  2.4e-011 3.90  
102 4.2e-008 3.8e-003 2.6e-006 1.00e+000  3.624326586e+001  3.624336612e+001  2.2e-011 3.95  
103 3.8e-008 3.4e-003 2.4e-006 1.00e+000  3.624327271e+001  3.624336294e+001  2.0e-011 3.98  
104 3.4e-008 3.0e-003 2.1e-006 1.00e+000  3.624327892e+001  3.624336005e+001  1.8e-011 4.01  
105 3.1e-008 2.7e-003 1.9e-006 9.94e-001  3.624328446e+001  3.624335749e+001  1.6e-011 4.04  
106 2.7e-008 2.5e-003 1.7e-006 1.00e+000  3.624328947e+001  3.624335516e+001  1.4e-011 4.09  
107 2.5e-008 2.2e-003 1.5e-006 1.01e+000  3.624329409e+001  3.624335300e+001  1.3e-011 4.12  
108 2.2e-008 2.0e-003 1.4e-006 9.97e-001  3.624329811e+001  3.624335114e+001  1.2e-011 4.15  
109 2.0e-008 1.8e-003 1.3e-006 1.00e+000  3.624330178e+001  3.624334943e+001  1.1e-011 4.20  
110 1.8e-008 1.6e-003 1.1e-006 1.00e+000  3.624330505e+001  3.624334791e+001  9.5e-012 4.23  
111 1.6e-008 1.5e-003 1.0e-006 9.94e-001  3.624330797e+001  3.624334656e+001  8.6e-012 4.26  
112 1.5e-008 1.3e-003 9.1e-007 1.01e+000  3.624331070e+001  3.624334528e+001  7.8e-012 4.29  
113 1.3e-008 1.2e-003 8.2e-007 1.00e+000  3.624331310e+001  3.624334416e+001  7.0e-012 4.34  
114 1.2e-008 1.1e-003 7.4e-007 1.00e+000  3.624331522e+001  3.624334318e+001  6.3e-012 4.37  
115 1.1e-008 9.5e-004 6.7e-007 1.00e+000  3.624331713e+001  3.624334229e+001  5.7e-012 4.40  
116 9.6e-009 8.6e-004 6.0e-007 1.00e+000  3.624331886e+001  3.624334149e+001  5.1e-012 4.43  
117 8.6e-009 7.7e-004 5.4e-007 1.00e+000  3.624332040e+001  3.624334077e+001  4.6e-012 4.46  
118 7.8e-009 7.0e-004 4.9e-007 1.00e+000  3.624332180e+001  3.624334013e+001  4.1e-012 4.51  
119 7.0e-009 6.3e-004 4.4e-007 1.00e+000  3.624332305e+001  3.624333955e+001  3.7e-012 4.54  
120 6.3e-009 5.6e-004 3.9e-007 9.99e-001  3.624332417e+001  3.624333902e+001  3.3e-012 4.57  
121 5.7e-009 5.1e-004 3.5e-007 9.98e-001  3.624332519e+001  3.624333855e+001  3.0e-012 4.62  
122 5.1e-009 4.6e-004 3.2e-007 1.00e+000  3.624332610e+001  3.624333813e+001  2.7e-012 4.67  
123 4.6e-009 4.1e-004 2.9e-007 9.97e-001  3.624332692e+001  3.624333775e+001  2.4e-012 4.71  
124 4.1e-009 3.7e-004 2.6e-007 9.99e-001  3.624332766e+001  3.624333741e+001  2.2e-012 4.74  
125 3.7e-009 3.3e-004 2.3e-007 9.98e-001  3.624332833e+001  3.624333710e+001  2.0e-012 4.79  
126 3.3e-009 3.0e-004 2.1e-007 1.00e+000  3.624332893e+001  3.624333682e+001  1.8e-012 4.82  
127 3.0e-009 2.7e-004 1.9e-007 1.00e+000  3.624332947e+001  3.624333657e+001  1.6e-012 4.85  
128 2.7e-009 2.4e-004 1.7e-007 1.00e+000  3.624332996e+001  3.624333634e+001  1.4e-012 4.90  
129 2.4e-009 2.2e-004 1.5e-007 1.00e+000  3.624333040e+001  3.624333613e+001  1.3e-012 4.93  
130 2.2e-009 2.0e-004 1.4e-007 9.97e-001  3.624333079e+001  3.624333595e+001  1.2e-012 4.96  
131 2.0e-009 1.8e-004 1.2e-007 9.94e-001  3.624333114e+001  3.624333579e+001  1.1e-012 5.01  
132 1.8e-009 1.6e-004 1.1e-007 1.00e+000  3.624333146e+001  3.624333564e+001  9.5e-013 5.04  
Interior-point optimizer terminated. Time: 5.05. 

Optimizer terminated. Time: 5.07    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 3.6243331463e+001   Viol.  con: 3e-008   var: 0e+000 
  Dual.    obj: 3.6243335642e+001   Viol.  con: 0e+000   var: 1e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 5.12 seconds.
result packing took 5.6% of solve time
solution checking took 1.5% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1900            
  Cones                  : 0               
  Scalar variables       : 6471            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1012
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1023
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 1023            
Lin. dep.  - tries                  : 1                 time                   : 0.02            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 830
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3579              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.08              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.05            
Factor     - nonzeros before factor : 1.67e+004         after factor           : 1.72e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.288863851e+005 2.000000000e+000  1.0e+000 0.14  
1   1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.266339056e+005 3.774599296e+000  4.7e-001 0.19  
2   4.2e+002 5.5e+002 2.4e+004 -9.35e-001 -1.204516316e+005 1.083248639e+001  1.9e-001 0.23  
3   2.8e+002 3.7e+002 1.6e+004 -8.37e-001 -1.157870811e+005 6.665174534e+001  1.3e-001 0.27  
4   2.8e+002 3.7e+002 1.6e+004 -7.58e-001 -1.132101904e+005 2.261946792e+003  1.2e-001 0.31  
5   7.5e+001 9.8e+001 4.3e+003 -7.51e-001 -7.369912359e+004 1.114793955e+004  3.3e-002 0.34  
6   3.0e+001 3.9e+001 1.7e+003 -1.92e-001 -3.984853678e+004 1.107249603e+004  1.3e-002 0.38  
7   1.4e+001 1.8e+001 7.8e+002 3.92e-001  -2.070937160e+004 5.965042613e+003  6.1e-003 0.41  
8   9.0e+000 1.2e+001 5.1e+002 7.29e-001  -1.410200922e+004 4.103524561e+003  4.0e-003 0.42  
9   3.6e+000 4.7e+000 2.1e+002 8.34e-001  -5.837225648e+003 1.819161917e+003  1.6e-003 0.45  
10  2.0e+000 2.6e+000 1.1e+002 9.52e-001  -2.940268099e+003 1.325303596e+003  8.9e-004 0.47  
11  9.0e-001 1.2e+000 5.1e+001 9.84e-001  -1.324698611e+003 6.203743594e+002  4.1e-004 0.50  
12  8.6e-001 1.2e+000 4.9e+001 9.64e-001  -1.286285142e+003 5.821375524e+002  3.9e-004 0.52  
13  3.8e-001 5.3e-001 2.2e+001 9.81e-001  -5.626622793e+002 2.744796467e+002  1.7e-004 0.53  
14  1.5e-001 2.3e-001 8.6e+000 1.00e+000  -2.179542760e+002 1.114770849e+002  6.9e-005 0.55  
15  8.6e-002 1.5e-001 5.0e+000 1.00e+000  -1.179869106e+002 7.375582825e+001  4.0e-005 0.58  
16  2.6e-002 1.2e-001 1.6e+000 1.00e+000  -2.807278717e+001 3.131489331e+001  1.3e-005 0.61  
17  1.1e-002 9.3e-002 6.9e-001 1.00e+000  -5.276658637e+000 2.122045343e+001  5.7e-006 0.64  
18  1.0e-002 8.5e-002 6.3e-001 1.01e+000  -3.410718351e+000 2.059177775e+001  5.2e-006 0.67  
19  6.6e-003 6.5e-002 4.0e-001 1.01e+000  2.894594403e+000  1.822582006e+001  3.3e-006 0.70  
20  4.5e-003 4.7e-002 2.8e-001 1.01e+000  6.709261900e+000  1.712856584e+001  2.3e-006 0.75  
21  1.8e-003 5.9e-002 1.1e-001 1.01e+000  1.119392102e+001  1.545045903e+001  9.4e-007 0.78  
22  1.0e-003 4.8e-002 6.2e-002 1.02e+000  1.264898917e+001  1.495383701e+001  5.1e-007 0.81  
23  4.6e-004 5.4e-002 2.9e-002 1.02e+000  1.351660745e+001  1.458946415e+001  2.4e-007 0.86  
24  2.6e-004 5.0e-002 1.6e-002 1.01e+000  1.385886377e+001  1.445533915e+001  1.4e-007 0.89  
25  1.3e-004 5.2e-002 8.5e-003 1.01e+000  1.406163748e+001  1.437394320e+001  7.1e-008 0.92  
26  9.0e-005 4.6e-002 5.6e-003 1.01e+000  1.413613226e+001  1.434341596e+001  4.7e-008 0.95  
27  8.1e-005 4.2e-002 5.1e-003 1.00e+000  1.415437997e+001  1.434100903e+001  4.3e-008 0.98  
28  7.3e-005 3.9e-002 4.6e-003 1.00e+000  1.416702901e+001  1.433496262e+001  3.8e-008 1.01  
29  6.5e-005 3.6e-002 4.1e-003 1.00e+000  1.417864639e+001  1.432976652e+001  3.4e-008 1.03  
30  5.9e-005 3.3e-002 3.7e-003 1.00e+000  1.418904801e+001  1.432503941e+001  3.1e-008 1.06  
31  5.3e-005 3.0e-002 3.3e-003 1.00e+000  1.419838830e+001  1.432076707e+001  2.8e-008 1.08  
32  4.8e-005 2.8e-002 3.0e-003 1.00e+000  1.420677331e+001  1.431690308e+001  2.5e-008 1.11  
33  4.3e-005 2.6e-002 2.7e-003 1.00e+000  1.421430163e+001  1.431340955e+001  2.3e-008 1.12  
34  3.9e-005 2.4e-002 2.4e-003 1.00e+000  1.422106175e+001  1.431025135e+001  2.0e-008 1.14  
35  3.5e-005 2.2e-002 2.2e-003 1.00e+000  1.422713353e+001  1.430739842e+001  1.8e-008 1.16  
36  3.1e-005 2.1e-002 2.0e-003 1.00e+000  1.423258827e+001  1.430482205e+001  1.7e-008 1.17  
37  2.8e-005 2.0e-002 1.8e-003 1.00e+000  1.423748983e+001  1.430249622e+001  1.5e-008 1.19  
38  2.5e-005 1.8e-002 1.6e-003 1.00e+000  1.424189511e+001  1.430039743e+001  1.3e-008 1.22  
39  2.3e-005 1.7e-002 1.4e-003 1.00e+000  1.424585488e+001  1.429850428e+001  1.2e-008 1.23  
40  2.0e-005 1.6e-002 1.3e-003 1.00e+000  1.424941454e+001  1.429679715e+001  1.1e-008 1.25  
41  1.8e-005 1.5e-002 1.2e-003 1.00e+000  1.425261485e+001  1.429525778e+001  9.8e-009 1.26  
42  1.7e-005 1.5e-002 1.0e-003 1.00e+000  1.425549240e+001  1.429386987e+001  8.8e-009 1.28  
43  1.5e-005 1.4e-002 9.4e-004 1.00e+000  1.425807994e+001  1.429261861e+001  7.9e-009 1.31  
44  1.3e-005 1.3e-002 8.5e-004 1.00e+000  1.426040678e+001  1.429149097e+001  7.1e-009 1.33  
45  1.2e-005 1.3e-002 7.6e-004 1.00e+000  1.426249925e+001  1.429047420e+001  6.4e-009 1.34  
46  1.1e-005 1.2e-002 6.9e-004 1.00e+000  1.426438097e+001  1.428955809e+001  5.8e-009 1.36  
47  9.8e-006 1.2e-002 6.2e-004 1.00e+000  1.426607309e+001  1.428873225e+001  5.2e-009 1.37  
48  8.8e-006 1.1e-002 5.6e-004 1.00e+000  1.426759475e+001  1.428798737e+001  4.7e-009 1.39  
49  7.9e-006 1.1e-002 5.0e-004 1.00e+000  1.426896298e+001  1.428731647e+001  4.2e-009 1.40  
50  7.1e-006 1.1e-002 4.5e-004 1.00e+000  1.427019324e+001  1.428671103e+001  3.8e-009 1.44  
51  6.4e-006 1.0e-002 4.0e-004 1.00e+000  1.427129942e+001  1.428616536e+001  3.4e-009 1.45  
52  5.8e-006 1.0e-002 3.6e-004 1.00e+000  1.427229406e+001  1.428567314e+001  3.1e-009 1.47  
53  5.2e-006 9.7e-003 3.3e-004 1.00e+000  1.427318838e+001  1.428522976e+001  2.8e-009 1.48  
54  4.7e-006 9.5e-003 3.0e-004 1.00e+000  1.427399261e+001  1.428483007e+001  2.5e-009 1.50  
55  4.2e-006 9.3e-003 2.7e-004 1.00e+000  1.427471600e+001  1.428446955e+001  2.2e-009 1.51  
56  3.8e-006 9.1e-003 2.4e-004 1.00e+000  1.427536662e+001  1.428414505e+001  2.0e-009 1.54  
57  3.4e-006 8.9e-003 2.2e-004 1.00e+000  1.427595189e+001  1.428385272e+001  1.8e-009 1.56  
58  3.1e-006 8.8e-003 1.9e-004 1.00e+000  1.427647846e+001  1.428358933e+001  1.6e-009 1.58  
59  2.8e-006 8.7e-003 1.7e-004 9.99e-001  1.427695217e+001  1.428335228e+001  1.5e-009 1.59  
60  2.5e-006 8.5e-003 1.6e-004 1.00e+000  1.427737844e+001  1.428313861e+001  1.3e-009 1.61  
61  2.2e-006 8.4e-003 1.4e-004 1.00e+000  1.427776204e+001  1.428294598e+001  1.2e-009 1.62  
62  2.0e-006 8.3e-003 1.3e-004 1.00e+000  1.427810715e+001  1.428277278e+001  1.1e-009 1.64  
63  1.8e-006 8.2e-003 1.1e-004 1.00e+000  1.427841769e+001  1.428261678e+001  9.6e-010 1.67  
64  1.6e-006 8.1e-003 1.0e-004 1.00e+000  1.427869718e+001  1.428247607e+001  8.6e-010 1.69  
65  1.5e-006 8.1e-003 9.3e-005 1.00e+000  1.427894865e+001  1.428234955e+001  7.8e-010 1.70  
66  1.3e-006 8.0e-003 8.3e-005 1.00e+000  1.427917491e+001  1.428223568e+001  7.0e-010 1.72  
67  1.2e-006 7.9e-003 7.5e-005 9.98e-001  1.427937845e+001  1.428213343e+001  6.3e-010 1.73  
68  1.1e-006 7.9e-003 6.8e-005 1.00e+000  1.427956173e+001  1.428204087e+001  5.7e-010 1.75  
69  9.7e-007 7.8e-003 6.1e-005 9.99e-001  1.427972657e+001  1.428195794e+001  5.1e-010 1.76  
70  8.7e-007 7.8e-003 5.5e-005 9.99e-001  1.427987490e+001  1.428188325e+001  4.6e-010 1.79  
71  7.8e-007 7.7e-003 4.9e-005 1.00e+000  1.428000866e+001  1.428181560e+001  4.1e-010 1.81  
72  7.0e-007 7.7e-003 4.4e-005 9.95e-001  1.428012870e+001  1.428175532e+001  3.7e-010 1.83  
73  6.3e-007 7.7e-003 4.0e-005 9.99e-001  1.428023678e+001  1.428170081e+001  3.4e-010 1.84  
74  5.7e-007 7.6e-003 3.6e-005 9.97e-001  1.428033402e+001  1.428165182e+001  3.0e-010 1.86  
75  5.1e-007 7.6e-003 3.2e-005 9.97e-001  1.428042152e+001  1.428160771e+001  2.7e-010 1.89  
76  4.6e-007 7.5e-003 2.9e-005 9.98e-001  1.428050027e+001  1.428156798e+001  2.4e-010 1.90  
77  4.2e-007 7.5e-003 2.6e-005 1.00e+000  1.428057153e+001  1.428153181e+001  2.2e-010 1.92  
78  3.7e-007 7.5e-003 2.4e-005 9.96e-001  1.428063526e+001  1.428149968e+001  2.0e-010 1.94  
79  3.4e-007 7.5e-003 2.1e-005 9.99e-001  1.428069264e+001  1.428147065e+001  1.8e-010 1.95  
80  3.0e-007 7.5e-003 1.9e-005 9.98e-001  1.428074426e+001  1.428144456e+001  1.6e-010 1.97  
81  2.7e-007 7.4e-003 1.7e-005 9.93e-001  1.428079069e+001  1.428142118e+001  1.4e-010 1.98  
82  2.5e-007 6.7e-003 1.5e-005 1.01e+000  1.428083314e+001  1.428139954e+001  1.3e-010 2.01  
83  2.2e-007 6.0e-003 1.4e-005 1.00e+000  1.428087073e+001  1.428138045e+001  1.2e-010 2.03  
84  2.0e-007 5.4e-003 1.3e-005 9.93e-001  1.428090451e+001  1.428136343e+001  1.1e-010 2.04  
85  1.8e-007 4.9e-003 1.1e-005 1.01e+000  1.428093599e+001  1.428134731e+001  9.5e-011 2.06  
86  1.6e-007 4.4e-003 1.0e-005 1.00e+000  1.428096332e+001  1.428133342e+001  8.6e-011 2.08  
87  1.4e-007 3.9e-003 9.1e-006 9.95e-001  1.428098786e+001  1.428132103e+001  7.7e-011 2.09  
88  1.3e-007 3.6e-003 8.2e-006 1.01e+000  1.428101075e+001  1.428130930e+001  7.0e-011 2.11  
89  1.2e-007 3.2e-003 7.4e-006 1.02e+000  1.428103189e+001  1.428129841e+001  6.3e-011 2.12  
90  1.1e-007 2.9e-003 6.7e-006 1.00e+000  1.428104970e+001  1.428128936e+001  5.7e-011 2.15  
91  9.5e-008 2.6e-003 6.0e-006 1.01e+000  1.428106620e+001  1.428128092e+001  5.1e-011 2.17  
92  8.6e-008 2.3e-003 5.4e-006 1.03e+000  1.428108230e+001  1.428127255e+001  4.7e-011 2.18  
93  7.7e-008 2.1e-003 4.8e-006 9.89e-001  1.428109493e+001  1.428126625e+001  4.2e-011 2.20  
94  6.9e-008 1.9e-003 4.4e-006 9.65e-001  1.428110625e+001  1.428126070e+001  3.8e-011 2.22  
95  6.2e-008 1.7e-003 3.9e-006 9.31e-001  1.428111640e+001  1.428125589e+001  3.4e-011 2.23  
96  5.6e-008 1.5e-003 3.5e-006 9.46e-001  1.428112556e+001  1.428125144e+001  3.1e-011 2.26  
97  5.1e-008 1.4e-003 3.2e-006 9.89e-001  1.428113386e+001  1.428124721e+001  2.8e-011 2.28  
98  4.6e-008 1.2e-003 2.9e-006 9.84e-001  1.428114133e+001  1.428124343e+001  2.5e-011 2.29  
99  4.1e-008 1.1e-003 2.6e-006 9.14e-001  1.428114799e+001  1.428124027e+001  2.2e-011 2.31  
100 3.7e-008 1.0e-003 2.3e-006 1.01e+000  1.428115433e+001  1.428123694e+001  2.0e-011 2.34  
101 3.3e-008 9.0e-004 2.1e-006 9.05e-001  1.428115970e+001  1.428123440e+001  1.8e-011 2.36  
102 3.0e-008 8.1e-004 1.9e-006 9.89e-001  1.428116459e+001  1.428123186e+001  1.6e-011 2.37  
103 2.7e-008 7.3e-004 1.7e-006 1.17e+000  1.428117237e+001  1.428122715e+001  1.6e-011 2.39  
104 2.4e-008 6.6e-004 1.5e-006 9.56e-001  1.428117598e+001  1.428122540e+001  1.4e-011 2.40  
105 2.2e-008 5.9e-004 1.4e-006 9.95e-001  1.428117925e+001  1.428122373e+001  1.3e-011 2.43  
106 2.0e-008 5.3e-004 1.2e-006 9.85e-001  1.428118219e+001  1.428122225e+001  1.2e-011 2.45  
107 1.8e-008 4.8e-004 1.1e-006 1.01e+000  1.428118500e+001  1.428122079e+001  1.1e-011 2.46  
108 1.6e-008 4.3e-004 1.0e-006 1.01e+000  1.428118747e+001  1.428121950e+001  9.6e-012 2.48  
109 1.4e-008 3.9e-004 9.0e-007 1.03e+000  1.428118986e+001  1.428121824e+001  8.8e-012 2.50  
110 1.3e-008 3.5e-004 8.1e-007 9.74e-001  1.428119174e+001  1.428121731e+001  7.9e-012 2.51  
111 1.2e-008 3.1e-004 7.3e-007 1.00e+000  1.428119345e+001  1.428121643e+001  7.1e-012 2.54  
112 1.0e-008 2.8e-004 6.6e-007 1.03e+000  1.428119515e+001  1.428121554e+001  6.5e-012 2.56  
113 9.4e-009 2.5e-004 5.9e-007 9.75e-001  1.428119650e+001  1.428121487e+001  5.8e-012 2.57  
114 8.5e-009 2.3e-004 5.3e-007 1.03e+000  1.428119787e+001  1.428121415e+001  5.3e-012 2.59  
115 7.6e-009 2.1e-004 4.8e-007 9.94e-001  1.428119895e+001  1.428121361e+001  4.8e-012 2.61  
116 6.9e-009 1.9e-004 4.3e-007 9.56e-001  1.428119991e+001  1.428121314e+001  4.3e-012 2.62  
117 6.2e-009 1.7e-004 3.9e-007 1.03e+000  1.428120091e+001  1.428121261e+001  4.0e-012 2.64  
118 5.6e-009 1.5e-004 3.5e-007 9.99e-001  1.428120169e+001  1.428121222e+001  3.6e-012 2.65  
119 5.0e-009 1.4e-004 3.1e-007 1.03e+000  1.428120248e+001  1.428121180e+001  3.2e-012 2.68  
120 4.5e-009 1.2e-004 2.8e-007 1.02e+000  1.428120315e+001  1.428121145e+001  3.0e-012 2.70  
121 4.1e-009 1.1e-004 2.5e-007 1.05e+000  1.428120383e+001  1.428121110e+001  2.7e-012 2.71  
122 3.7e-009 9.9e-005 2.3e-007 9.88e-001  1.428120431e+001  1.428121086e+001  2.5e-012 2.73  
123 3.3e-009 8.9e-005 2.1e-007 9.85e-001  1.428120475e+001  1.428121064e+001  2.2e-012 2.75  
124 2.4e-009 5.5e-006 1.3e-008 8.49e-001  1.428120860e+001  1.428120900e+001  2.7e-013 2.76  
Interior-point optimizer terminated. Time: 2.78. 

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

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.4281208604e+001   Viol.  con: 7e-008   var: 0e+000 
  Dual.    obj: 1.4281208999e+001   Viol.  con: 0e+000   var: 3e-005 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.82 seconds.
result packing took 9.6% of solve time
solution checking took 2.8% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1900            
  Cones                  : 0               
  Scalar variables       : 6471            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1012
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1023
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 1023            
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            : 830
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3579              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.02            
Factor     - nonzeros before factor : 1.67e+004         after factor           : 1.72e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.288411172e+005 2.000000000e+000  1.0e+000 0.06  
1   1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265468781e+005 3.779122206e+000  4.6e-001 0.11  
2   4.0e+002 5.1e+002 2.2e+004 -9.34e-001 -1.197894150e+005 1.137202451e+001  1.7e-001 0.14  
3   2.8e+002 3.6e+002 1.6e+004 -8.28e-001 -1.156608588e+005 8.370973139e+001  1.2e-001 0.19  
4   2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.123538775e+005 2.834296985e+003  1.2e-001 0.22  
5   6.3e+001 8.2e+001 3.6e+003 -7.47e-001 -6.634108828e+004 1.270081629e+004  2.8e-002 0.27  
6   3.9e+001 5.1e+001 2.2e+003 -7.14e-002 -4.857698584e+004 1.113562807e+004  1.7e-002 0.30  
7   2.8e+001 3.7e+001 1.6e+003 2.50e-001  -3.836499077e+004 8.756670074e+003  1.3e-002 0.33  
8   1.6e+001 2.1e+001 9.0e+002 4.36e-001  -2.423973951e+004 5.449778491e+003  7.1e-003 0.38  
9   6.4e+000 8.3e+000 3.6e+002 6.75e-001  -1.031393095e+004 2.807510742e+003  2.9e-003 0.41  
10  3.6e+000 4.6e+000 2.0e+002 8.88e-001  -5.601632236e+003 1.893110588e+003  1.6e-003 0.45  
11  1.3e+000 1.7e+000 7.4e+001 9.54e-001  -1.992795409e+003 7.844611497e+002  5.9e-004 0.48  
12  1.0e+000 1.3e+000 5.7e+001 9.87e-001  -1.518114771e+003 6.370446626e+002  4.5e-004 0.53  
13  8.5e-001 1.5e+000 4.8e+001 9.70e-001  -1.291761244e+003 5.484331361e+002  3.8e-004 0.56  
14  2.9e-001 5.2e-001 1.7e+001 9.89e-001  -4.376765678e+002 1.993767480e+002  1.3e-004 0.59  
15  1.6e-001 3.0e-001 9.3e+000 1.00e+000  -2.387356781e+002 1.166815333e+002  7.5e-005 0.61  
16  7.3e-002 1.6e-001 4.3e+000 1.00e+000  -1.046286684e+002 5.798946009e+001  3.5e-005 0.64  
17  3.6e-002 1.0e-001 2.1e+000 1.01e+000  -4.706792552e+001 3.277908678e+001  1.7e-005 0.66  
18  1.8e-002 7.9e-002 1.1e+000 1.01e+000  -2.055740903e+001 2.053409321e+001  8.8e-006 0.67  
19  1.8e-002 7.6e-002 1.0e+000 1.02e+000  -1.904089648e+001 2.053047942e+001  8.5e-006 0.69  
20  9.3e-003 5.9e-002 5.5e-001 1.02e+000  -4.148209180e+000 1.645185394e+001  4.5e-006 0.72  
21  4.0e-003 5.8e-002 2.4e-001 1.02e+000  4.760118069e+000  1.363841062e+001  2.0e-006 0.73  
22  2.1e-003 5.1e-002 1.3e-001 1.01e+000  7.802478207e+000  1.260166776e+001  1.1e-006 0.75  
23  5.9e-004 8.2e-002 3.9e-002 9.86e-001  1.035412392e+001  1.180687856e+001  3.4e-007 0.77  
24  1.8e-004 8.8e-002 1.3e-002 9.78e-001  1.109336841e+001  1.156814682e+001  1.1e-007 0.78  
25  5.9e-005 8.7e-002 4.2e-003 9.88e-001  1.133359132e+001  1.149440925e+001  3.9e-008 0.81  
26  2.2e-005 8.4e-002 1.6e-003 9.96e-001  1.141357008e+001  1.147302708e+001  1.4e-008 0.84  
27  8.2e-006 8.1e-002 6.0e-004 9.99e-001  1.144291245e+001  1.146569884e+001  5.6e-009 0.86  
28  7.4e-006 7.3e-002 5.4e-004 1.00e+000  1.144484183e+001  1.146535107e+001  5.0e-009 0.89  
29  6.7e-006 6.7e-002 4.8e-004 1.00e+000  1.144643566e+001  1.146489438e+001  4.5e-009 0.91  
30  6.0e-006 6.1e-002 4.4e-004 1.00e+000  1.144786958e+001  1.146448276e+001  4.1e-009 0.92  
31  5.4e-006 5.5e-002 3.9e-004 1.00e+000  1.144915746e+001  1.146410964e+001  3.6e-009 0.95  
32  4.9e-006 5.0e-002 3.5e-004 1.00e+000  1.145031536e+001  1.146377255e+001  3.3e-009 0.97  
33  4.4e-006 4.6e-002 3.2e-004 1.00e+000  1.145135633e+001  1.146346796e+001  3.0e-009 1.01  
34  3.9e-006 4.2e-002 2.9e-004 1.00e+000  1.145229230e+001  1.146319289e+001  2.7e-009 1.06  
35  3.5e-006 3.9e-002 2.6e-004 1.00e+000  1.145313393e+001  1.146294455e+001  2.4e-009 1.11  
36  3.2e-006 3.5e-002 2.3e-004 1.00e+000  1.145389079e+001  1.146272044e+001  2.2e-009 1.14  
37  2.9e-006 3.3e-002 2.1e-004 1.00e+000  1.145457150e+001  1.146251826e+001  1.9e-009 1.17  
38  2.6e-006 3.0e-002 1.9e-004 1.00e+000  1.145518377e+001  1.146233590e+001  1.7e-009 1.22  
39  2.3e-006 2.8e-002 1.7e-004 1.00e+000  1.145573452e+001  1.146217148e+001  1.6e-009 1.25  
40  2.1e-006 2.6e-002 1.5e-004 1.00e+000  1.145622997e+001  1.146202324e+001  1.4e-009 1.28  
41  1.9e-006 2.4e-002 1.4e-004 1.00e+000  1.145667571e+001  1.146188962e+001  1.3e-009 1.33  
42  1.7e-006 2.2e-002 1.2e-004 1.00e+000  1.145707671e+001  1.146176927e+001  1.1e-009 1.36  
43  1.5e-006 2.1e-002 1.1e-004 1.00e+000  1.145743750e+001  1.146166083e+001  1.0e-009 1.40  
44  1.4e-006 1.9e-002 1.0e-004 1.00e+000  1.145776212e+001  1.146156313e+001  9.3e-010 1.44  
45  1.2e-006 1.8e-002 9.0e-005 1.00e+000  1.145805423e+001  1.146147509e+001  8.4e-010 1.47  
46  1.1e-006 1.7e-002 8.1e-005 1.00e+000  1.145831706e+001  1.146139585e+001  7.5e-010 1.50  
47  1.0e-006 1.6e-002 7.3e-005 1.00e+000  1.145855356e+001  1.146132448e+001  6.8e-010 1.54  
48  9.0e-007 1.5e-002 6.5e-005 1.00e+000  1.145876636e+001  1.146126025e+001  6.1e-010 1.58  
49  8.1e-007 1.4e-002 5.9e-005 1.00e+000  1.145895789e+001  1.146120232e+001  5.5e-010 1.62  
50  7.3e-007 1.4e-002 5.3e-005 1.00e+000  1.145913023e+001  1.146115021e+001  4.9e-010 1.65  
51  6.6e-007 1.3e-002 4.8e-005 1.00e+000  1.145928531e+001  1.146110335e+001  4.4e-010 1.69  
52  2.3e-007 4.5e-003 1.7e-005 1.00e+000  1.146019562e+001  1.146082739e+001  1.5e-010 1.73  
53  2.0e-007 4.0e-003 1.5e-005 1.00e+000  1.146024473e+001  1.146081289e+001  1.4e-010 1.76  
54  7.0e-008 1.4e-003 5.1e-006 1.00e+000  1.146053131e+001  1.146072557e+001  4.7e-011 1.79  
55  6.3e-008 1.2e-003 4.6e-006 1.01e+000  1.146054721e+001  1.146072072e+001  4.3e-011 1.83  
56  5.7e-008 1.1e-003 4.1e-006 9.99e-001  1.146056051e+001  1.146071667e+001  3.9e-011 1.86  
57  5.1e-008 1.0e-003 3.7e-006 1.05e+000  1.146057510e+001  1.146071188e+001  3.6e-011 1.89  
58  4.6e-008 9.0e-004 3.3e-006 1.03e+000  1.146058693e+001  1.146070820e+001  3.3e-011 1.92  
59  4.2e-008 8.1e-004 3.0e-006 9.74e-001  1.146059624e+001  1.146070549e+001  2.9e-011 1.94  
60  3.8e-008 7.3e-004 2.7e-006 9.90e-001  1.146060463e+001  1.146070300e+001  2.6e-011 1.97  
61  3.5e-008 6.6e-004 2.4e-006 1.16e+000  1.146061792e+001  1.146069775e+001  2.6e-011 2.00  
62  2.2e-008 4.1e-005 1.5e-007 8.92e-001  1.146067843e+001  1.146068374e+001  3.0e-012 2.03  
63  1.8e-008 3.7e-005 1.4e-007 1.57e+000  1.146067839e+001  1.146068282e+001  2.6e-012 2.06  
64  1.6e-008 3.3e-005 1.2e-007 1.48e+000  1.146067851e+001  1.146068239e+001  2.4e-012 2.11  
65  1.1e-008 2.7e-006 1.0e-008 6.78e-001  1.146068064e+001  1.146068101e+001  4.7e-013 2.14  
Interior-point optimizer terminated. Time: 2.14. 

Optimizer terminated. Time: 2.15    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1460680636e+001   Viol.  con: 2e-007   var: 0e+000 
  Dual.    obj: 1.1460681008e+001   Viol.  con: 0e+000   var: 2e-005 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.19 seconds.
result packing took 18% of solve time
solution checking took 4.2% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1900            
  Cones                  : 0               
  Scalar variables       : 6471            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1010
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1022
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 1022            
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            : 831
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3581              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 : 1.67e+004         after factor           : 1.72e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.288998615e+005 2.000000000e+000  1.0e+000 0.06  
1   1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265875373e+005 3.780619869e+000  4.6e-001 0.11  
2   3.9e+002 5.0e+002 2.2e+004 -9.34e-001 -1.197188591e+005 1.155031711e+001  1.7e-001 0.16  
3   2.8e+002 3.6e+002 1.6e+004 -8.27e-001 -1.157108910e+005 9.417269035e+001  1.2e-001 0.19  
4   2.8e+002 3.6e+002 1.6e+004 -7.57e-001 -1.123914173e+005 2.811278463e+003  1.2e-001 0.23  
5   7.6e+001 9.8e+001 4.2e+003 -7.47e-001 -7.376461344e+004 1.082770768e+004  3.3e-002 0.27  
6   3.7e+001 4.8e+001 2.1e+003 -1.88e-001 -4.660332067e+004 1.110740852e+004  1.6e-002 0.31  
7   2.2e+001 2.8e+001 1.2e+003 2.82e-001  -3.096729728e+004 7.346528455e+003  9.6e-003 0.34  
8   1.0e+001 1.3e+001 5.6e+002 5.65e-001  -1.574573457e+004 3.981871767e+003  4.4e-003 0.37  
9   4.4e+000 5.7e+000 2.5e+002 8.13e-001  -6.958350773e+003 2.167141817e+003  2.0e-003 0.41  
10  2.0e+000 2.6e+000 1.1e+002 9.36e-001  -3.050731869e+003 1.180728956e+003  9.0e-004 0.45  
11  1.5e+000 1.9e+000 8.2e+001 9.82e-001  -2.218826770e+003 8.695229230e+002  6.5e-004 0.48  
12  9.1e-001 1.2e+000 5.1e+001 9.85e-001  -1.370740975e+003 5.641488471e+002  4.1e-004 0.52  
13  7.7e-001 1.2e+000 4.4e+001 9.63e-001  -1.183360837e+003 4.845449788e+002  3.5e-004 0.56  
14  3.1e-001 4.8e-001 1.8e+001 9.89e-001  -4.667202022e+002 2.156594022e+002  1.4e-004 0.59  
15  1.6e-001 2.5e-001 9.0e+000 1.00e+000  -2.293351638e+002 1.130415616e+002  7.2e-005 0.62  
16  4.8e-002 1.5e-001 2.8e+000 1.00e+000  -6.729480076e+001 4.025159135e+001  2.3e-005 0.66  
17  3.8e-002 1.2e-001 2.3e+000 1.00e+000  -5.211469365e+001 3.388224659e+001  1.8e-005 0.69  
18  1.9e-002 8.8e-002 1.2e+000 1.00e+000  -2.289462935e+001 2.097975574e+001  9.4e-006 0.73  
19  1.5e-002 7.0e-002 8.6e-001 1.02e+000  -1.404740653e+001 1.855063162e+001  7.1e-006 0.76  
20  6.1e-003 5.3e-002 3.7e-001 1.03e+000  9.891390682e-001  1.458099741e+001  3.0e-006 0.81  
21  2.3e-003 6.6e-002 1.4e-001 1.02e+000  7.379545654e+000  1.257551185e+001  1.2e-006 0.84  
22  9.1e-004 6.0e-002 5.7e-002 9.85e-001  9.669241348e+000  1.180960807e+001  5.0e-007 0.87  
23  3.1e-004 7.8e-002 2.1e-002 9.66e-001  1.073876307e+001  1.152847168e+001  1.8e-007 0.92  
24  1.4e-004 6.2e-002 9.5e-003 9.55e-001  1.106594200e+001  1.143047811e+001  8.4e-008 0.95  
25  6.1e-005 6.2e-002 4.3e-003 9.85e-001  1.122223752e+001  1.138775087e+001  3.9e-008 0.98  
26  3.2e-005 5.6e-002 2.3e-003 9.91e-001  1.128379459e+001  1.137132940e+001  2.0e-008 1.03  
27  2.9e-005 5.1e-002 2.0e-003 9.91e-001  1.129250626e+001  1.137142449e+001  1.8e-008 1.06  
28  2.6e-005 4.7e-002 1.8e-003 9.94e-001  1.129844696e+001  1.136947302e+001  1.7e-008 1.09  
29  2.3e-005 4.3e-002 1.6e-003 9.93e-001  1.130400382e+001  1.136794304e+001  1.5e-008 1.12  
30  2.1e-005 3.9e-002 1.5e-003 9.94e-001  1.130896361e+001  1.136653202e+001  1.3e-008 1.15  
31  1.9e-005 3.6e-002 1.3e-003 9.94e-001  1.131341296e+001  1.136524252e+001  1.2e-008 1.19  
32  1.7e-005 3.3e-002 1.2e-003 9.95e-001  1.131741167e+001  1.136407279e+001  1.1e-008 1.22  
33  1.5e-005 3.0e-002 1.1e-003 9.95e-001  1.132100502e+001  1.136301254e+001  9.8e-009 1.26  
34  1.4e-005 2.8e-002 9.7e-004 9.95e-001  1.132423421e+001  1.136205173e+001  8.8e-009 1.29  
35  1.2e-005 2.6e-002 8.8e-004 9.96e-001  1.132713687e+001  1.136118176e+001  7.9e-009 1.33  
36  1.1e-005 2.4e-002 7.9e-004 9.96e-001  1.132974657e+001  1.136039465e+001  7.1e-009 1.36  
37  1.0e-005 2.2e-002 7.1e-004 9.96e-001  1.133209330e+001  1.135968295e+001  6.4e-009 1.39  
38  9.0e-006 2.1e-002 6.4e-004 9.97e-001  1.133420380e+001  1.135903975e+001  5.8e-009 1.42  
39  8.1e-006 1.9e-002 5.8e-004 9.97e-001  1.133610202e+001  1.135845873e+001  5.2e-009 1.45  
40  7.3e-006 1.8e-002 5.2e-004 9.97e-001  1.133780941e+001  1.135793399e+001  4.7e-009 1.50  
41  6.6e-006 1.7e-002 4.7e-004 9.98e-001  1.133934519e+001  1.135746022e+001  4.2e-009 1.51  
42  5.9e-006 1.6e-002 4.2e-004 9.98e-001  1.134072664e+001  1.135703251e+001  3.8e-009 1.54  
43  5.3e-006 1.5e-002 3.8e-004 9.98e-001  1.134196925e+001  1.135664648e+001  3.4e-009 1.59  
44  4.8e-006 1.4e-002 3.4e-004 9.98e-001  1.134308699e+001  1.135629806e+001  3.1e-009 1.62  
45  4.3e-006 1.4e-002 3.1e-004 9.98e-001  1.134409239e+001  1.135598365e+001  2.8e-009 1.65  
46  3.9e-006 1.3e-002 2.8e-004 9.99e-001  1.134499678e+001  1.135569995e+001  2.5e-009 1.69  
47  3.5e-006 1.2e-002 2.5e-004 9.99e-001  1.134581032e+001  1.135544405e+001  2.2e-009 1.72  
48  3.2e-006 1.2e-002 2.2e-004 9.99e-001  1.134654218e+001  1.135521323e+001  2.0e-009 1.75  
49  2.8e-006 1.1e-002 2.0e-004 9.99e-001  1.134720060e+001  1.135500513e+001  1.8e-009 1.78  
50  2.6e-006 1.1e-002 1.8e-004 9.99e-001  1.134779301e+001  1.135481755e+001  1.6e-009 1.81  
51  2.3e-006 1.1e-002 1.6e-004 9.99e-001  1.134832606e+001  1.135464849e+001  1.5e-009 1.83  
52  2.1e-006 1.0e-002 1.5e-004 9.99e-001  1.134880572e+001  1.135449621e+001  1.3e-009 1.86  
53  1.9e-006 9.8e-003 1.3e-004 9.99e-001  1.134923736e+001  1.135435906e+001  1.2e-009 1.89  
54  1.7e-006 9.6e-003 1.2e-004 9.99e-001  1.134962581e+001  1.135423556e+001  1.1e-009 1.90  
55  1.5e-006 9.3e-003 1.1e-004 1.00e+000  1.134997541e+001  1.135412435e+001  9.6e-010 1.92  
56  1.4e-006 9.1e-003 9.6e-005 1.00e+000  1.135029005e+001  1.135402422e+001  8.7e-010 1.93  
57  1.2e-006 8.9e-003 8.6e-005 1.00e+000  1.135057323e+001  1.135393411e+001  7.8e-010 1.97  
58  1.1e-006 8.7e-003 7.8e-005 1.00e+000  1.135082811e+001  1.135385300e+001  7.0e-010 1.98  
59  9.9e-007 8.5e-003 7.0e-005 1.00e+000  1.135105751e+001  1.135378000e+001  6.3e-010 2.00  
60  8.9e-007 8.3e-003 6.3e-005 1.00e+000  1.135126399e+001  1.135371431e+001  5.7e-010 2.01  
61  8.0e-007 8.2e-003 5.7e-005 1.00e+000  1.135144983e+001  1.135365519e+001  5.1e-010 2.04  
62  7.2e-007 8.1e-003 5.1e-005 1.00e+000  1.135161712e+001  1.135360195e+001  4.6e-010 2.06  
63  6.5e-007 8.0e-003 4.6e-005 1.00e+000  1.135176769e+001  1.135355406e+001  4.1e-010 2.08  
64  5.8e-007 7.9e-003 4.1e-005 1.00e+000  1.135190321e+001  1.135351096e+001  3.7e-010 2.09  
65  5.3e-007 7.8e-003 3.7e-005 1.00e+000  1.135202519e+001  1.135347217e+001  3.4e-010 2.12  
66  4.7e-007 7.7e-003 3.3e-005 1.00e+000  1.135213498e+001  1.135343727e+001  3.0e-010 2.14  
67  4.3e-007 7.6e-003 3.0e-005 1.00e+000  1.135223379e+001  1.135340587e+001  2.7e-010 2.17  
68  3.8e-007 7.5e-003 2.7e-005 1.00e+000  1.135232272e+001  1.135337762e+001  2.4e-010 2.18  
69  3.4e-007 7.5e-003 2.4e-005 1.00e+000  1.135240277e+001  1.135335218e+001  2.2e-010 2.20  
70  3.1e-007 7.4e-003 2.2e-005 1.00e+000  1.135247482e+001  1.135332929e+001  2.0e-010 2.21  
71  2.8e-007 7.4e-003 2.0e-005 1.00e+000  1.135253966e+001  1.135330869e+001  1.8e-010 2.25  
72  2.5e-007 7.3e-003 1.8e-005 1.00e+000  1.135259802e+001  1.135329015e+001  1.6e-010 2.26  
73  2.3e-007 7.3e-003 1.6e-005 1.00e+000  1.135265054e+001  1.135327346e+001  1.4e-010 2.28  
74  2.0e-007 7.2e-003 1.4e-005 1.00e+000  1.135269782e+001  1.135325843e+001  1.3e-010 2.31  
75  1.8e-007 7.2e-003 1.3e-005 1.00e+000  1.135274037e+001  1.135324489e+001  1.2e-010 2.32  
76  1.6e-007 7.2e-003 1.2e-005 9.99e-001  1.135277866e+001  1.135323274e+001  1.1e-010 2.34  
77  1.5e-007 7.1e-003 1.1e-005 9.99e-001  1.135281311e+001  1.135322181e+001  9.5e-011 2.36  
78  1.3e-007 7.1e-003 9.5e-006 1.00e+000  1.135284413e+001  1.135321195e+001  8.5e-011 2.39  
79  1.2e-007 7.1e-003 8.5e-006 9.99e-001  1.135287203e+001  1.135320309e+001  7.7e-011 2.40  
80  1.1e-007 7.1e-003 7.7e-006 1.00e+000  1.135289715e+001  1.135319511e+001  6.9e-011 2.42  
81  9.7e-008 7.1e-003 6.9e-006 1.00e+000  1.135291976e+001  1.135318792e+001  6.2e-011 2.43  
82  8.8e-008 7.0e-003 6.2e-006 1.00e+000  1.135294010e+001  1.135318145e+001  5.6e-011 2.46  
83  7.9e-008 7.0e-003 5.6e-006 9.99e-001  1.135295841e+001  1.135317564e+001  5.0e-011 2.48  
84  7.1e-008 7.0e-003 5.0e-006 1.00e+000  1.135297489e+001  1.135317039e+001  4.5e-011 2.50  
85  6.4e-008 7.0e-003 4.5e-006 9.96e-001  1.135298971e+001  1.135316570e+001  4.1e-011 2.51  
86  5.8e-008 7.0e-003 4.1e-006 9.99e-001  1.135300305e+001  1.135316146e+001  3.7e-011 2.54  
87  5.2e-008 6.9e-003 3.7e-006 9.99e-001  1.135301507e+001  1.135315763e+001  3.3e-011 2.56  
88  4.7e-008 6.9e-003 3.3e-006 1.00e+000  1.135302588e+001  1.135315418e+001  3.0e-011 2.57  
89  4.2e-008 6.2e-003 3.0e-006 1.00e+000  1.135303571e+001  1.135315103e+001  2.7e-011 2.59  
90  3.8e-008 5.6e-003 2.7e-006 1.00e+000  1.135304446e+001  1.135314824e+001  2.4e-011 2.61  
91  3.4e-008 5.1e-003 2.4e-006 1.00e+000  1.135305233e+001  1.135314573e+001  2.2e-011 2.64  
92  3.1e-008 4.6e-003 2.2e-006 9.99e-001  1.135305941e+001  1.135314348e+001  2.0e-011 2.65  
93  2.8e-008 4.1e-003 1.9e-006 1.01e+000  1.135306594e+001  1.135314138e+001  1.8e-011 2.67  
94  2.5e-008 3.7e-003 1.8e-006 9.99e-001  1.135307166e+001  1.135313956e+001  1.6e-011 2.68  
95  2.2e-008 3.3e-003 1.6e-006 9.98e-001  1.135307681e+001  1.135313792e+001  1.4e-011 2.70  
96  2.0e-008 3.0e-003 1.4e-006 1.01e+000  1.135308162e+001  1.135313637e+001  1.3e-011 2.73  
97  1.8e-008 2.7e-003 1.3e-006 1.01e+000  1.135308596e+001  1.135313497e+001  1.2e-011 2.75  
98  1.6e-008 2.4e-003 1.1e-006 9.97e-001  1.135308968e+001  1.135313379e+001  1.1e-011 2.76  
99  1.5e-008 2.2e-003 1.0e-006 9.84e-001  1.135309302e+001  1.135313275e+001  9.5e-012 2.78  
100 1.3e-008 2.0e-003 9.3e-007 9.97e-001  1.135309603e+001  1.135313179e+001  8.5e-012 2.81  
101 1.2e-008 1.8e-003 8.4e-007 1.01e+000  1.135309880e+001  1.135313090e+001  7.7e-012 2.82  
102 1.1e-008 1.6e-003 7.5e-007 9.96e-001  1.135310124e+001  1.135313013e+001  6.9e-012 2.84  
103 1.4e-009 1.7e-004 7.9e-008 1.01e+000  1.135312081e+001  1.135312382e+001  7.1e-013 2.86  
Interior-point optimizer terminated. Time: 2.86. 

Optimizer terminated. Time: 2.87    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1353120811e+001   Viol.  con: 2e-008   var: 0e+000 
  Dual.    obj: 1.1353123822e+001   Viol.  con: 0e+000   var: 1e-003 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.9 seconds.
result packing took 9.9% of solve time
solution checking took 2.7% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1900            
  Cones                  : 0               
  Scalar variables       : 6471            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1010
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1022
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 1022            
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            : 831
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3581              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.02            
Factor     - nonzeros before factor : 1.68e+004         after factor           : 1.72e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.289005965e+005 2.000000000e+000  1.0e+000 0.05  
1   1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265819984e+005 3.775575058e+000  4.6e-001 0.09  
2   3.8e+002 4.9e+002 2.1e+004 -9.34e-001 -1.194852974e+005 1.178222237e+001  1.7e-001 0.13  
3   2.8e+002 3.6e+002 1.6e+004 -8.24e-001 -1.156698982e+005 1.068051391e+002  1.2e-001 0.16  
4   2.8e+002 3.6e+002 1.5e+004 -7.56e-001 -1.123119776e+005 2.781216452e+003  1.2e-001 0.19  
5   7.6e+001 9.8e+001 4.2e+003 -7.45e-001 -7.369506665e+004 1.086779666e+004  3.3e-002 0.22  
6   3.6e+001 4.7e+001 2.0e+003 -1.88e-001 -4.546773342e+004 1.112170224e+004  1.6e-002 0.27  
7   2.0e+001 2.6e+001 1.1e+003 3.02e-001  -2.909749277e+004 7.248066178e+003  9.0e-003 0.30  
8   9.7e+000 1.3e+001 5.4e+002 5.97e-001  -1.524996869e+004 3.925528531e+003  4.3e-003 0.33  
9   4.3e+000 5.6e+000 2.4e+002 8.22e-001  -6.824959006e+003 2.126891278e+003  1.9e-003 0.36  
10  1.6e+000 2.1e+000 9.0e+001 9.39e-001  -2.382072757e+003 9.940754489e+002  7.2e-004 0.39  
11  1.1e+000 1.5e+000 6.3e+001 9.88e-001  -1.660147169e+003 6.956312160e+002  5.0e-004 0.44  
12  7.8e-001 1.0e+000 4.4e+001 9.83e-001  -1.186272347e+003 4.998439238e+002  3.5e-004 0.47  
13  5.9e-001 7.7e-001 3.3e+001 9.85e-001  -8.730515899e+002 3.883191372e+002  2.6e-004 0.52  
14  2.1e-001 2.9e-001 1.2e+001 9.89e-001  -3.245247406e+002 1.424685631e+002  9.8e-005 0.55  
15  8.9e-002 1.4e-001 5.1e+000 1.01e+000  -1.284380200e+002 6.667989124e+001  4.2e-005 0.59  
16  3.5e-002 9.9e-002 2.1e+000 1.01e+000  -4.749419864e+001 3.075570357e+001  1.7e-005 0.62  
17  2.9e-002 8.4e-002 1.7e+000 9.96e-001  -3.703624685e+001 2.753513760e+001  1.4e-005 0.66  
18  1.8e-002 6.6e-002 1.0e+000 1.01e+000  -1.901892964e+001 2.024512556e+001  8.5e-006 0.69  
19  1.5e-002 5.7e-002 8.8e-001 1.02e+000  -1.416317513e+001 1.901459735e+001  7.2e-006 0.73  
20  5.4e-003 6.6e-002 3.2e-001 1.02e+000  2.106448548e+000  1.405587552e+001  2.6e-006 0.76  
21  1.8e-003 7.8e-002 1.1e-001 1.02e+000  8.170101360e+000  1.230684192e+001  9.7e-007 0.80  
22  1.3e-003 6.0e-002 8.3e-002 9.63e-001  8.936942492e+000  1.202329007e+001  7.2e-007 0.89  
23  4.8e-004 6.6e-002 3.1e-002 9.59e-001  1.040637313e+001  1.160345203e+001  2.8e-007 0.92  
24  1.9e-004 6.2e-002 1.3e-002 9.58e-001  1.093938344e+001  1.142612431e+001  1.1e-007 0.95  
25  1.7e-004 5.7e-002 1.1e-002 9.76e-001  1.097689973e+001  1.141479104e+001  1.0e-007 0.98  
26  1.5e-004 5.2e-002 1.0e-002 9.75e-001  1.101084126e+001  1.140546147e+001  9.2e-008 1.01  
27  1.4e-004 4.7e-002 9.2e-003 9.76e-001  1.104378279e+001  1.139945360e+001  8.3e-008 1.04  
28  1.2e-004 4.3e-002 8.3e-003 9.78e-001  1.107351800e+001  1.139406154e+001  7.5e-008 1.08  
29  1.1e-004 3.9e-002 7.5e-003 9.80e-001  1.110027883e+001  1.138913509e+001  6.7e-008 1.11  
30  9.9e-005 3.6e-002 6.7e-003 9.82e-001  1.112431371e+001  1.138458877e+001  6.1e-008 1.14  
31  8.9e-005 3.3e-002 6.0e-003 9.83e-001  1.114589271e+001  1.138039241e+001  5.5e-008 1.17  
32  8.0e-005 3.1e-002 5.4e-003 9.85e-001  1.116526094e+001  1.137651916e+001  4.9e-008 1.20  
33  7.2e-005 2.8e-002 4.9e-003 9.86e-001  1.118264132e+001  1.137294598e+001  4.4e-008 1.23  
34  6.5e-005 2.6e-002 4.4e-003 9.88e-001  1.119823527e+001  1.136965160e+001  4.0e-008 1.26  
35  5.8e-005 2.4e-002 4.0e-003 9.89e-001  1.121222503e+001  1.136661688e+001  3.6e-008 1.28  
36  5.2e-005 2.3e-002 3.6e-003 9.90e-001  1.122477504e+001  1.136382418e+001  3.2e-008 1.31  
37  4.7e-005 2.1e-002 3.2e-003 9.91e-001  1.123603330e+001  1.136125683e+001  2.9e-008 1.34  
38  4.3e-005 2.0e-002 2.9e-003 9.92e-001  1.124613297e+001  1.135889928e+001  2.6e-008 1.37  
39  3.8e-005 1.8e-002 2.6e-003 9.92e-001  1.125519353e+001  1.135673665e+001  2.4e-008 1.40  
40  3.4e-005 1.7e-002 2.3e-003 9.93e-001  1.126332209e+001  1.135475469e+001  2.1e-008 1.44  
41  3.1e-005 1.6e-002 2.1e-003 9.94e-001  1.127061484e+001  1.135294009e+001  1.9e-008 1.47  
42  2.8e-005 1.5e-002 1.9e-003 9.94e-001  1.127715807e+001  1.135128017e+001  1.7e-008 1.50  
43  2.5e-005 1.5e-002 1.7e-003 9.95e-001  1.128302949e+001  1.134976341e+001  1.5e-008 1.53  
44  2.3e-005 1.4e-002 1.5e-003 9.96e-001  1.128829891e+001  1.134837908e+001  1.4e-008 1.56  
45  2.0e-005 1.3e-002 1.4e-003 9.96e-001  1.129302890e+001  1.134711706e+001  1.3e-008 1.59  
46  1.8e-005 1.3e-002 1.2e-003 9.96e-001  1.129727547e+001  1.134596792e+001  1.1e-008 1.62  
47  1.6e-005 1.2e-002 1.1e-003 9.97e-001  1.130108863e+001  1.134492253e+001  1.0e-008 1.67  
48  1.5e-005 1.2e-002 1.0e-003 9.97e-001  1.130451317e+001  1.134397244e+001  9.1e-009 1.70  
49  1.3e-005 1.1e-002 9.1e-004 9.97e-001  1.130758919e+001  1.134310965e+001  8.2e-009 1.73  
50  1.2e-005 1.1e-002 8.2e-004 9.98e-001  1.131035258e+001  1.134232678e+001  7.4e-009 1.76  
51  1.1e-005 1.0e-002 7.4e-004 9.98e-001  1.131283547e+001  1.134161700e+001  6.7e-009 1.79  
52  9.7e-006 1.0e-002 6.6e-004 9.98e-001  1.131506660e+001  1.134097382e+001  6.0e-009 1.83  
53  8.8e-006 9.7e-003 6.0e-004 9.98e-001  1.131707176e+001  1.134039143e+001  5.4e-009 1.87  
54  7.9e-006 9.5e-003 5.4e-004 9.99e-001  1.131887399e+001  1.133986427e+001  4.9e-009 1.90  
55  7.1e-006 9.2e-003 4.8e-004 9.99e-001  1.132049398e+001  1.133938734e+001  4.4e-009 1.93  
56  6.4e-006 9.0e-003 4.4e-004 9.99e-001  1.132195026e+001  1.133895598e+001  3.9e-009 1.97  
57  5.7e-006 8.8e-003 3.9e-004 9.99e-001  1.132325944e+001  1.133856594e+001  3.5e-009 2.00  
58  5.2e-006 8.7e-003 3.5e-004 9.99e-001  1.132443644e+001  1.133821339e+001  3.2e-009 2.03  
59  4.7e-006 8.5e-003 3.2e-004 9.99e-001  1.132549463e+001  1.133789478e+001  2.9e-009 2.06  
60  4.2e-006 8.4e-003 2.9e-004 9.99e-001  1.132644605e+001  1.133760692e+001  2.6e-009 2.09  
61  3.8e-006 8.2e-003 2.6e-004 9.99e-001  1.132730152e+001  1.133734692e+001  2.3e-009 2.12  
62  3.4e-006 8.1e-003 2.3e-004 9.99e-001  1.132807078e+001  1.133711213e+001  2.1e-009 2.15  
63  3.1e-006 8.0e-003 2.1e-004 9.99e-001  1.132876257e+001  1.133690023e+001  1.9e-009 2.18  
64  2.7e-006 7.9e-003 1.9e-004 1.00e+000  1.132938477e+001  1.133670899e+001  1.7e-009 2.20  
65  2.5e-006 7.8e-003 1.7e-004 1.00e+000  1.132994443e+001  1.133653647e+001  1.5e-009 2.23  
66  2.2e-006 7.8e-003 1.5e-004 1.00e+000  1.133044787e+001  1.133638092e+001  1.4e-009 2.28  
67  2.0e-006 7.7e-003 1.4e-004 1.00e+000  1.133090078e+001  1.133624072e+001  1.2e-009 2.31  
68  1.8e-006 7.6e-003 1.2e-004 1.00e+000  1.133130827e+001  1.133611430e+001  1.1e-009 2.34  
69  1.6e-006 7.6e-003 1.1e-004 1.00e+000  1.133167489e+001  1.133600047e+001  1.0e-009 2.39  
70  1.5e-006 7.5e-003 1.0e-004 1.00e+000  1.133200477e+001  1.133589791e+001  9.0e-010 2.42  
71  1.3e-006 7.4e-003 9.0e-005 1.00e+000  1.133230160e+001  1.133580553e+001  8.1e-010 2.45  
72  1.2e-006 7.4e-003 8.1e-005 1.00e+000  1.133256870e+001  1.133572232e+001  7.3e-010 2.50  
73  1.1e-006 7.4e-003 7.3e-005 1.00e+000  1.133280906e+001  1.133564736e+001  6.6e-010 2.53  
74  9.6e-007 7.3e-003 6.5e-005 1.00e+000  1.133302537e+001  1.133557982e+001  5.9e-010 2.56  
75  8.6e-007 7.3e-003 5.9e-005 1.00e+000  1.133322001e+001  1.133551904e+001  5.3e-010 2.59  
76  7.8e-007 7.2e-003 5.3e-005 1.00e+000  1.133339518e+001  1.133546429e+001  4.8e-010 2.62  
77  7.0e-007 7.2e-003 4.8e-005 1.00e+000  1.133355283e+001  1.133541495e+001  4.3e-010 2.65  
78  6.3e-007 7.2e-003 4.3e-005 1.00e+000  1.133369470e+001  1.133537056e+001  3.9e-010 2.67  
79  5.7e-007 7.2e-003 3.9e-005 1.00e+000  1.133382236e+001  1.133533063e+001  3.5e-010 2.68  
80  5.1e-007 7.1e-003 3.5e-005 1.00e+000  1.133393725e+001  1.133529468e+001  3.1e-010 2.71  
81  4.6e-007 7.1e-003 3.1e-005 1.00e+000  1.133404062e+001  1.133526235e+001  2.8e-010 2.73  
82  4.1e-007 7.1e-003 2.8e-005 1.00e+000  1.133413367e+001  1.133523321e+001  2.5e-010 2.75  
83  3.7e-007 7.1e-003 2.5e-005 9.99e-001  1.133421739e+001  1.133520702e+001  2.3e-010 2.76  
84  3.3e-007 7.1e-003 2.3e-005 9.99e-001  1.133429273e+001  1.133518344e+001  2.1e-010 2.79  
85  3.0e-007 7.0e-003 2.1e-005 1.00e+000  1.133436054e+001  1.133516218e+001  1.9e-010 2.81  
86  2.7e-007 7.0e-003 1.8e-005 1.00e+000  1.133442157e+001  1.133514306e+001  1.7e-010 2.82  
87  2.4e-007 7.0e-003 1.7e-005 1.00e+000  1.133447649e+001  1.133512581e+001  1.5e-010 2.84  
88  2.2e-007 7.0e-003 1.5e-005 9.98e-001  1.133452590e+001  1.133511034e+001  1.4e-010 2.86  
89  2.0e-007 7.0e-003 1.3e-005 1.00e+000  1.133457038e+001  1.133509639e+001  1.2e-010 2.89  
90  1.8e-007 7.0e-003 1.2e-005 1.00e+000  1.133461041e+001  1.133508380e+001  1.1e-010 2.90  
91  1.6e-007 7.0e-003 1.1e-005 1.00e+000  1.133464643e+001  1.133507248e+001  9.9e-011 2.92  
92  1.4e-007 6.9e-003 9.8e-006 9.99e-001  1.133467885e+001  1.133506232e+001  8.9e-011 2.93  
93  1.3e-007 6.9e-003 8.8e-006 1.00e+000  1.133470802e+001  1.133505314e+001  8.0e-011 2.95  
94  1.2e-007 6.9e-003 8.0e-006 9.96e-001  1.133473426e+001  1.133504492e+001  7.2e-011 2.98  
95  1.0e-007 6.9e-003 7.2e-006 9.98e-001  1.133475788e+001  1.133503751e+001  6.5e-011 3.00  
96  9.4e-008 6.2e-003 6.4e-006 1.00e+000  1.133477932e+001  1.133503073e+001  5.8e-011 3.01  
97  8.5e-008 5.6e-003 5.8e-006 1.00e+000  1.133479844e+001  1.133502470e+001  5.3e-011 3.03  
98  7.6e-008 5.0e-003 5.2e-006 1.00e+000  1.133481564e+001  1.133501929e+001  4.7e-011 3.06  
99  6.9e-008 4.5e-003 4.7e-006 1.00e+000  1.133483113e+001  1.133501440e+001  4.3e-011 3.11  
100 6.2e-008 4.1e-003 4.2e-006 9.99e-001  1.133484506e+001  1.133501002e+001  3.8e-011 3.15  
101 5.6e-008 3.7e-003 3.8e-006 1.00e+000  1.133485768e+001  1.133500602e+001  3.4e-011 3.18  
102 5.0e-008 3.3e-003 3.4e-006 9.96e-001  1.133486895e+001  1.133500249e+001  3.1e-011 3.21  
103 4.5e-008 3.0e-003 3.1e-006 9.99e-001  1.133487910e+001  1.133499929e+001  2.8e-011 3.25  
104 4.1e-008 2.7e-003 2.8e-006 9.92e-001  1.133488822e+001  1.133499644e+001  2.5e-011 3.28  
105 3.7e-008 2.4e-003 2.5e-006 1.01e+000  1.133489671e+001  1.133499372e+001  2.3e-011 3.31  
106 3.3e-008 2.2e-003 2.2e-006 1.00e+000  1.133490408e+001  1.133499140e+001  2.0e-011 3.32  
107 3.0e-008 2.0e-003 2.0e-006 1.00e+000  1.133491074e+001  1.133498929e+001  1.8e-011 3.35  
108 2.7e-008 1.8e-003 1.8e-006 1.00e+000  1.133491674e+001  1.133498739e+001  1.7e-011 3.37  
109 2.4e-008 1.6e-003 1.6e-006 1.00e+000  1.133492219e+001  1.133498565e+001  1.5e-011 3.40  
110 2.2e-008 1.4e-003 1.5e-006 9.96e-001  1.133492701e+001  1.133498414e+001  1.3e-011 3.43  
111 4.7e-009 2.7e-004 2.8e-007 9.78e-001  1.133496225e+001  1.133497329e+001  2.7e-012 3.46  
112 2.9e-010 1.6e-005 1.6e-008 1.01e+000  1.133496990e+001  1.133497055e+001  1.5e-013 3.50  
Interior-point optimizer terminated. Time: 3.50. 

Optimizer terminated. Time: 3.51    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1334969905e+001   Viol.  con: 4e-009   var: 0e+000 
  Dual.    obj: 1.1334970545e+001   Viol.  con: 0e+000   var: 1e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.55 seconds.
result packing took 65% of solve time
solution checking took 2.2% of solve time
Solving took 6 GP solves and 34.6 seconds.
Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2418945.73259 force_pound * meter but the right hand side evaluated to 2375461.23883 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.3786375 force_pound but the right hand side evaluated to 32399.9999981 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116797 meter but the right hand side evaluated to 2.0816064894 meter (Allowable error: 0.1%, Actual error: 6%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1243582.26432 joule / kilogram but the right hand side evaluated to 1.56115607979 megajoule / kilogram (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 664761.650755 joule / kilogram but the right hand side evaluated to 0.667340459869 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.17%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.3998913664 meter but the right hand side evaluated to 16.3228902944 meter (Allowable error: 0.1%, Actual error: 13%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.903626913372433 but the right hand side evaluated to 4.788858793067725 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.01981056340295 but the right hand side evaluated to 4.788858784431628 (Allowable error: 0.1%, Actual error: 52%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.144910636826193 but the right hand side evaluated to 4.788858795173274 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.3622338933 meter but the right hand side evaluated to 18.1377229255 meter (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3622338933 meter but the right hand side evaluated to 18.2420595954 meter (Allowable error: 0.1%, Actual error: 0.65%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.2960340541782607 but the right hand side evaluated to 0.18973855620052116 (Allowable error: 0.1%, Actual error: 2.2%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23302083125394546 but the right hand side evaluated to 0.17434674726353194 (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.563249725889682 but the right hand side evaluated to 4.7306398392698465 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.583098822651346 but the right hand side evaluated to 4.757852693343093 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission


Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 47.113s

OK

Generating XML reports...
Cloning into 'solar'...
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0)
grin 1.2.1 requires argparse>=1.1, which is not installed.
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-wr34eb
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-9rqte4\wheels\d5\94\ac\b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
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-lt2hk7
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0)
Building wheels for collected packages: gassolar
  Running setup.py bdist_wheel for gassolar: started
  Running setup.py bdist_wheel for gassolar: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-7jn2zy\wheels\fe\11\0a\2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
grin 1.2.1 requires argparse>=1.1, which is not installed.
Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\solar
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in d:\jenkins\workspace\gplibrary_pr_models\mosek (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2017.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.11.0)
Building wheels for collected packages: solar
  Running setup.py bdist_wheel for solar: started
  Running setup.py bdist_wheel for solar: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-pkfwoi\wheels\9f\ae\a9\52e286ff9ea1428d6dd1e8c6df0d12b22c44363d9dcc1dd331
Successfully built solar
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: solar
Successfully installed solar-0.0.0.0
adding test for 'solar/solar.py'
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
adding test for 'solar/npod_trade.py'
Beginning signomial solve.
Solving took 10 GP solves and 6.69 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1372946.1519 but bound is 600000.0000
Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 79493.7395 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.1182607574 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781592 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%)

Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 1.63010986524 meter ** 2 / second ** 2 but the right hand side evaluated to 1.6301057481 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%)

Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985264156 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983814541 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)

Beginning signomial solve.
Solving took 10 GP solves and 6.73 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1372945.2779 but bound is 600000.0000
Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 79493.7395 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.11826075493 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781346 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%)

Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 1.63010986523 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010574808 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%)

Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985264139 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983814524 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)

Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.16 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2985 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 720429.8177 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.08 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2521 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 791679.4824 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.77 seconds.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1920 but bound is 0.9465
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 883741.3351 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 1.62 seconds.
Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.1637 but bound is 0.9465
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 933393.0310 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.36 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2985 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 720429.8204 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.25 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2521 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 791679.4808 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.74 seconds.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1920 but bound is 0.9465
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 883741.3340 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 1.45 seconds.
Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.1637 but bound is 0.9465
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 933393.0312 but bound is 600000.0000
Beginning signomial solve.
Solving took 10 GP solves and 6.59 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1372945.2718 but bound is 600000.0000
Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 79493.7395 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.11826075491 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781344 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%)

Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 1.63010986523 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010574808 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%)

Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985264137 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983814522 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)

Beginning signomial solve.
Solving took 10 GP solves and 6.59 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1372945.2753 but bound is 600000.0000
Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 79493.7395 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.11826075493 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781345 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%)

Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 1.63010986523 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010574808 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%)

Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985264138 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983814523 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)

Using solver 'mosek'
Solving for 702 variables.
Solving took 0.311 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2555 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 773120.5118 but bound is 600000.0000
Beginning signomial solve.
Solving took 9 GP solves and 7.2 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.0784 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1002038.7300 but bound is 600000.0000
Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,),  could cause inaccurate result because it is below lower bound. Solution is 76735.5639 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(1... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.39813215992 meter ** 2 / second ** 2 but the right hand side evaluated to 1.39812954852 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00019%)

Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.803919027516 meter ** 2 / second ** 2 but the right hand side evaluated to 0.803918046081 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%)

Using solver 'mosek_cli'
Solving for 702 variables.
Solving took 0.566 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2555 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 773120.3442 but bound is 600000.0000
Beginning signomial solve.
Solving took 9 GP solves and 7.63 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.0784 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1002041.5231 but bound is 600000.0000
Warning: Constraint [dQ_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,) [N... >= B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,)*G_M...] is not tight because the left hand side evaluated to 0.0359295931977 meter * newton but the right hand side evaluated to 0.0359295529168 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%)

Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,),  could cause inaccurate result because it is below lower bound. Solution is 76735.5213 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(1... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.39813162962 meter ** 2 / second ** 2 but the right hand side evaluated to 1.39812837496 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00023%)


Running tests...
----------------------------------------------------------------------
..D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
  tau = np.exp(-0.175/costhsun)
....EE
======================================================================
ERROR [12.281s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn
    mod.test()
  File "solar.py", line 654, in test
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
  File "solar.py", line 633, in setup
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
  File "solar.py", line 536, in setup
AttributeError: 'SparLoading' object has no attribute 'Sout'

======================================================================
ERROR [13.249s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn
    mod.test()
  File "solar.py", line 654, in test
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
  File "solar.py", line 633, in setup
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
  File "solar.py", line 536, in setup
AttributeError: 'SparLoading' object has no attribute 'Sout'

----------------------------------------------------------------------
Ran 8 tests in 481.182s

FAILED (errors=2)

Generating XML reports...
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0)
grin 1.2.1 requires argparse>=1.1, which is not installed.
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-ef7g4b
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-xmqwrf\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gplibrary
Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1)
Building wheels for collected packages: gpkitmodels
  Running setup.py bdist_wheel for gpkitmodels: started
  Running setup.py bdist_wheel for gpkitmodels: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-3hvq3c\wheels\4a\da\60\bea5372bf288606a399bdc749979f532f5aff24f4c362a9887
Successfully built gpkitmodels
grin 1.2.1 requires argparse>=1.1, which is not installed.
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'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.031 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.12 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.024 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.027 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.036 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 2.92 seconds.
Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006556021 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%)

Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544371514 meter * revolutions_per_minute but the right hand side evaluated to 103.04140943 meter / second (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585925022 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573144962 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.003%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.31464503395 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629895187 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0048%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.168936438401 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931603966 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0639642380861 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631379984 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0017%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226356535429 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354005877 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)

Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.101 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.108 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.137 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 4.94 seconds.
Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006568341 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%)

Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544539109 meter * revolutions_per_minute but the right hand side evaluated to 103.041408191 meter / second (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [dQ_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [N*m]... >= B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement_...] is not tight because the left hand side evaluated to 74.5041627751 meter * newton but the right hand side evaluated to 74.5040725471 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%)

Warning: Constraint [-B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement... >= dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [lbf]...] is not tight because the left hand side evaluated to 134.449579759 kilogram * meter / second ** 2 but the right hand side evaluated to 30.2255018449 force_pound (Allowable error: 0.0001%, Actual error: 0.00011%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585903433 meter ** 2 / second ** 2 but the right hand side evaluated to 0.42057303321 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0031%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.314644998908 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629685653 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0049%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.16893640237 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931506563 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.063964051843 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639630073546 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0016%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226356673111 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226353930664 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0012%)

Using solver 'mosek'
Solving for 13 variables.
Solving took 0.037 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 2.02 seconds.
Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619897.4209 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.084 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 3.29 seconds.
Warning: Constraint [omega_BladeElementProp/BladeElementPerf_(0,)*r_BladeElementProp/BladeElementPerf_(0,) [m*rpm]... >= Wt_BladeElementProp/BladeElementPerf_(0,) + vt_BladeElementProp/BladeElementPerf_(0,) [m/s]...] is not tight because the left hand side evaluated to 147.268875342 meter * revolutions_per_minute but the right hand side evaluated to 15.4219435408 meter / second (Allowable error: 0.0001%, Actual error: 0.00011%)

Warning: Constraint [dQ_BladeElementProp/BladeElementPerf_(3,) [N*m]... >= B_BladeElementProp/BladeElementPerf_(3,)*G_BladeElementProp/BladeElementPerf_(3,)*Wa_BladeElementPro...] is not tight because the left hand side evaluated to 42.7884411703 meter * newton but the right hand side evaluated to 42.7884887635 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%)

Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3481 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9721 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3856 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9562 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.2729 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.1579 but bound is 700000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000

Running tests...
----------------------------------------------------------------------
..........
----------------------------------------------------------------------
Ran 10 tests in 21.839s

OK

Generating XML reports...
Cloning into 'eVTOL'...
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adding test for 'aircraft_models.py'

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 2.536s

OK

Generating XML reports...
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.']
  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 ['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

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

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

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


(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>exit 0 
Build step 'Console output (build log) parsing' changed build result to FAILURE
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'D:\jenkins\workspace\gplibrary_PR_Models\mosek' for the testing framework 'JUnit'.
[xUnit] [INFO] - Check 'Failed Tests' threshold.
[xUnit] [INFO] - Check 'Skipped Tests' threshold.
[xUnit] [INFO] - Setting the build status to FAILURE
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: FAILURE