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Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2018.4)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.7.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-oIdtNH/wheels/62/18/d3/616f96cc7315a5d96e00418a41713828819a211a1260f4c2f6
Successfully built gassolar
Installing collected packages: gassolar
Successfully installed gassolar-0.0.0.0

Running tests...
----------------------------------------------------------------------
../Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
..
----------------------------------------------------------------------
Ran 4 tests in 26.171s

OK

Generating XML reports...
adding test for 'gassolar/gas/gas.py'
adding test for 'gassolar/solar/solar.py'
Using solver 'mosek'
Solving for 592 variables.
Solving took 0.172 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 0.636 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 0.0548 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 0.754 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 0.227 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1495 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 1.78 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 0.484 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 2.8 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
Cloning into 'jho'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0)
Collecting git+https://github.com/hoburg/gpfit.git
  Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-H8QSVL
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-ycyeGJ/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit

Running tests...
----------------------------------------------------------------------
....
----------------------------------------------------------------------
Ran 4 tests in 40.158s

OK

Generating XML reports...
adding test for 'model/jho.py'
adding test for 'model/print_perf.py'
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.219739571127313e-14.
Allowing negative dual variable(s) as small as -7.455277714618624e-14.
Allowing negative dual variable(s) as small as -1.5124143257216893e-13.
Allowing negative dual variable(s) as small as -1.5034197844987496e-13.
Solving took 4 GP solves and 1.49 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.976791548316761e-14.
Allowing negative dual variable(s) as small as -7.349589686844737e-14.
Allowing negative dual variable(s) as small as -1.4906565565242502e-13.
Allowing negative dual variable(s) as small as -1.4885445306922485e-13.
Solving took 4 GP solves and 2.66 seconds.
Allowing negative dual variable(s) as small as -5.188054846838597e-13.
Allowing negative dual variable(s) as small as -1.4305084894417064e-12.
Allowing negative dual variable(s) as small as -4.443008461141318e-13.
Allowing negative dual variable(s) as small as -4.433640954371043e-13.
Allowing negative dual variable(s) as small as -1.2970375641574439e-12.
Allowing negative dual variable(s) as small as -1.090706301318245e-12.
Allowing negative dual variable(s) as small as -1.0900240128910998e-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 -2.4208442189884924e-14.
Allowing negative dual variable(s) as small as -5.696078658777511e-12.
Allowing negative dual variable(s) as small as -2.087891440169102e-11.
Allowing negative dual variable(s) as small as -2.088077509249231e-11.
Solving took 4 GP solves and 1.85 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.79 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.176553630192871e-13.
Allowing negative dual variable(s) as small as -1.4304200185444316e-12.
Allowing negative dual variable(s) as small as -4.4475187421788576e-13.
Allowing negative dual variable(s) as small as -4.4558107203940267e-13.
Allowing negative dual variable(s) as small as -1.296803376488187e-12.
Allowing negative dual variable(s) as small as -1.0926626357182778e-12.
Allowing negative dual variable(s) as small as -1.0907542230542688e-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 -2.497929712314879e-14.
Allowing negative dual variable(s) as small as -5.696092591887158e-12.
Allowing negative dual variable(s) as small as -2.0879010539454076e-11.
Allowing negative dual variable(s) as small as -2.0881047093512277e-11.
Solving took 4 GP solves and 2.07 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.48 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Cloning into 'turbofan'...
Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/turbofan
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-7Wez2a/wheels/5a/d9/61/61e35684062bfcf52c1d9781b80aeffbe3c3604f4de326b4d2
Successfully built turbofan
Installing collected packages: turbofan
Successfully installed turbofan-0.0.0.0

Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 1.181s

OK

Generating XML reports...
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%)

Cloning into 'SPaircraft'...
Collecting git+https://github.com/hoburg/turbofan.git
  Cloning https://github.com/hoburg/turbofan.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-f2PHSx
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-WpkkNx/wheels/49/e6/3a/5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5
Successfully built turbofan

Running tests...
----------------------------------------------------------------------
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               : MACOSX/64-X86   
  Cores                  : 4               

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                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 4               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 826
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3575              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.01            
Factor     - nonzeros before factor : 1.67e+04          after factor           : 1.69e+05        
Factor     - dense dim.             : 0                 flops                  : 0.00e+00        
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+00        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.3e+05  0.00e+00   -1.290114216e+05  2.000000000e+00   1.0e+00  0.05  
1   1.1e+03  1.4e+03  6.2e+04  -9.71e-01  -1.268480541e+05  3.677917588e+00   4.8e-01  0.13  
2   3.8e+02  4.9e+02  2.1e+04  -9.36e-01  -1.195240616e+05  1.166054397e+01   1.7e-01  0.46  
3   2.8e+02  3.7e+02  1.6e+04  -8.21e-01  -1.157847903e+05  9.419380750e+01   1.2e-01  0.86  
4   2.8e+02  3.6e+02  1.6e+04  -7.55e-01  -1.126192885e+05  2.644815609e+03   1.2e-01  1.02  
5   6.4e+01  8.3e+01  3.6e+03  -7.45e-01  -6.715490567e+04  1.234316434e+04   2.8e-02  1.30  
6   2.9e+01  3.8e+01  1.7e+03  -8.76e-02  -3.900247076e+04  1.063813187e+04   1.3e-02  1.82  
7   1.5e+01  1.9e+01  8.3e+02  4.08e-01   -2.201101408e+04  6.179481181e+03   6.5e-03  2.36  
8   6.2e+00  8.1e+00  3.5e+02  7.01e-01   -9.556932382e+03  3.306290049e+03   2.8e-03  2.90  
9   2.9e+00  3.7e+00  1.6e+02  9.00e-01   -4.198892234e+03  1.894112680e+03   1.3e-03  3.36  
10  9.4e-01  1.2e+00  5.4e+01  9.67e-01   -1.111371535e+03  9.394246146e+02   4.3e-04  3.74  
11  6.8e-01  9.5e-01  3.9e+01  9.87e-01   -6.962698209e+02  7.955224154e+02   3.1e-04  4.22  
12  5.3e-01  7.4e-01  3.0e+01  9.84e-01   -4.682721695e+02  7.028962849e+02   2.4e-04  4.56  
13  2.2e-01  3.3e-01  1.3e+01  9.84e-01   1.279679145e+01   5.050163626e+02   1.0e-04  4.59  
14  9.3e-02  2.2e-01  5.5e+00  9.97e-01   2.102997069e+02   4.213184014e+02   4.4e-05  4.79  
15  2.3e-02  1.4e-01  1.4e+00  9.94e-01   3.195642046e+02   3.727189962e+02   1.1e-05  5.34  
16  5.9e-03  1.4e-01  3.7e-01  1.00e+00   3.472576359e+02   3.614178634e+02   3.1e-06  5.68  
17  2.4e-03  1.2e-01  1.5e-01  1.00e+00   3.531037493e+02   3.589508980e+02   1.3e-06  6.05  
18  3.9e-04  1.7e-01  2.5e-02  1.00e+00   3.566421741e+02   3.576042395e+02   2.1e-07  6.14  
19  1.5e-04  1.1e-01  9.8e-03  9.89e-01   3.570738940e+02   3.574516584e+02   8.4e-08  6.37  
20  4.1e-05  1.1e-01  2.7e-03  9.99e-01   3.572730425e+02   3.573766516e+02   2.3e-08  6.61  
21  1.8e-05  9.0e-02  1.2e-03  9.93e-01   3.573159415e+02   3.573607606e+02   9.9e-09  6.87  
22  6.2e-06  8.4e-02  4.1e-04  9.97e-01   3.573370872e+02   3.573529071e+02   3.5e-09  7.09  
23  2.8e-06  7.1e-02  1.9e-04  1.00e+00   3.573433682e+02   3.573505739e+02   1.6e-09  7.51  
24  2.5e-06  6.5e-02  1.7e-04  1.00e+00   3.573439018e+02   3.573503859e+02   1.4e-09  7.64  
25  2.3e-06  5.9e-02  1.5e-04  1.00e+00   3.573443725e+02   3.573502080e+02   1.3e-09  7.85  
26  2.1e-06  5.4e-02  1.4e-04  1.00e+00   3.573447970e+02   3.573500489e+02   1.2e-09  7.98  
27  1.9e-06  4.9e-02  1.2e-04  1.00e+00   3.573451790e+02   3.573499057e+02   1.0e-09  8.16  
28  1.7e-06  4.5e-02  1.1e-04  1.00e+00   3.573455228e+02   3.573497767e+02   9.4e-10  8.21  
29  1.5e-06  4.1e-02  9.9e-05  1.00e+00   3.573458322e+02   3.573496607e+02   8.5e-10  8.25  
30  1.4e-06  3.8e-02  8.9e-05  1.00e+00   3.573461107e+02   3.573495563e+02   7.6e-10  8.76  
31  1.2e-06  3.5e-02  8.0e-05  1.00e+00   3.573463613e+02   3.573494623e+02   6.9e-10  9.02  
32  1.1e-06  3.2e-02  7.2e-05  1.00e+00   3.573465868e+02   3.573493776e+02   6.2e-10  9.04  
33  9.9e-07  2.9e-02  6.5e-05  1.00e+00   3.573467897e+02   3.573493015e+02   5.6e-10  9.09  
34  8.9e-07  2.7e-02  5.9e-05  1.00e+00   3.573469724e+02   3.573492330e+02   5.0e-10  9.12  
35  8.0e-07  2.5e-02  5.3e-05  1.00e+00   3.573471367e+02   3.573491712e+02   4.5e-10  9.14  
36  7.2e-07  2.3e-02  4.7e-05  1.00e+00   3.573472847e+02   3.573491157e+02   4.0e-10  9.32  
37  6.5e-07  2.2e-02  4.3e-05  1.00e+00   3.573474178e+02   3.573490657e+02   3.6e-10  9.39  
38  5.8e-07  2.0e-02  3.8e-05  1.00e+00   3.573475376e+02   3.573490207e+02   3.3e-10  9.76  
39  5.2e-07  1.9e-02  3.5e-05  1.00e+00   3.573476453e+02   3.573489802e+02   2.9e-10  10.03 
40  4.7e-07  1.8e-02  3.1e-05  1.00e+00   3.573477423e+02   3.573489437e+02   2.7e-10  10.60 
41  4.3e-07  1.7e-02  2.8e-05  1.00e+00   3.573478296e+02   3.573489109e+02   2.4e-10  10.76 
42  3.8e-07  1.6e-02  2.5e-05  1.00e+00   3.573479082e+02   3.573488813e+02   2.2e-10  10.77 
43  3.4e-07  1.5e-02  2.3e-05  1.00e+00   3.573479789e+02   3.573488546e+02   1.9e-10  10.79 
44  3.1e-07  1.4e-02  2.0e-05  1.00e+00   3.573480425e+02   3.573488307e+02   1.7e-10  10.80 
45  2.8e-07  1.3e-02  1.8e-05  1.00e+00   3.573480997e+02   3.573488091e+02   1.6e-10  10.81 
46  2.5e-07  1.3e-02  1.7e-05  9.99e-01   3.573481512e+02   3.573487897e+02   1.4e-10  10.82 
47  2.3e-07  1.2e-02  1.5e-05  1.00e+00   3.573481976e+02   3.573487722e+02   1.3e-10  10.84 
48  2.0e-07  1.2e-02  1.3e-05  1.00e+00   3.573482393e+02   3.573487564e+02   1.1e-10  10.85 
49  1.8e-07  1.1e-02  1.2e-05  1.00e+00   3.573482768e+02   3.573487422e+02   1.0e-10  10.86 
50  1.6e-07  1.1e-02  1.1e-05  1.00e+00   3.573483106e+02   3.573487294e+02   9.3e-11  10.87 
51  1.5e-07  1.0e-02  9.8e-06  1.00e+00   3.573483411e+02   3.573487179e+02   8.3e-11  10.88 
52  1.3e-07  1.0e-02  8.8e-06  9.99e-01   3.573483684e+02   3.573487076e+02   7.5e-11  10.89 
53  1.2e-07  9.9e-03  7.9e-06  1.00e+00   3.573483930e+02   3.573486983e+02   6.8e-11  10.90 
54  1.1e-07  9.6e-03  7.1e-06  1.00e+00   3.573484152e+02   3.573486898e+02   6.1e-11  10.92 
55  9.7e-08  9.3e-03  6.4e-06  1.00e+00   3.573484352e+02   3.573486823e+02   5.5e-11  10.93 
56  8.8e-08  9.2e-03  5.8e-06  1.00e+00   3.573484533e+02   3.573486754e+02   4.9e-11  10.94 
57  7.9e-08  9.0e-03  5.2e-06  1.00e+00   3.573484695e+02   3.573486692e+02   4.4e-11  10.96 
58  7.1e-08  8.8e-03  4.7e-06  1.00e+00   3.573484841e+02   3.573486637e+02   4.0e-11  10.97 
59  6.4e-08  8.6e-03  4.2e-06  1.00e+00   3.573484971e+02   3.573486588e+02   3.6e-11  10.99 
60  5.7e-08  8.5e-03  3.8e-06  9.99e-01   3.573485089e+02   3.573486543e+02   3.2e-11  11.00 
61  5.2e-08  8.3e-03  3.4e-06  9.97e-01   3.573485194e+02   3.573486504e+02   2.9e-11  11.01 
62  4.7e-08  8.3e-03  3.1e-06  1.00e+00   3.573485291e+02   3.573486467e+02   2.6e-11  11.02 
63  4.2e-08  8.2e-03  2.8e-06  1.00e+00   3.573485377e+02   3.573486434e+02   2.4e-11  11.03 
64  3.8e-08  8.0e-03  2.5e-06  9.94e-01   3.573485453e+02   3.573486405e+02   2.1e-11  11.04 
65  3.4e-08  8.0e-03  2.2e-06  1.00e+00   3.573485522e+02   3.573486379e+02   1.9e-11  11.06 
66  3.1e-08  7.9e-03  2.0e-06  1.00e+00   3.573485585e+02   3.573486356e+02   1.7e-11  11.07 
67  2.7e-08  7.8e-03  1.8e-06  9.91e-01   3.573485640e+02   3.573486335e+02   1.6e-11  11.08 
68  2.5e-08  7.7e-03  1.6e-06  9.92e-01   3.573485691e+02   3.573486316e+02   1.4e-11  11.09 
69  2.2e-08  7.6e-03  1.5e-06  9.96e-01   3.573485736e+02   3.573486299e+02   1.3e-11  11.11 
70  2.0e-08  7.6e-03  1.3e-06  1.00e+00   3.573485777e+02   3.573486283e+02   1.1e-11  11.12 
71  1.8e-08  7.5e-03  1.2e-06  9.88e-01   3.573485814e+02   3.573486269e+02   1.0e-11  11.13 
72  1.6e-08  7.5e-03  1.1e-06  9.92e-01   3.573485847e+02   3.573486257e+02   9.2e-12  11.14 
73  1.5e-08  6.8e-03  9.6e-07  1.02e+00   3.573485879e+02   3.573486244e+02   8.3e-12  11.15 
74  1.3e-08  6.1e-03  8.7e-07  9.97e-01   3.573485906e+02   3.573486234e+02   7.5e-12  11.16 
75  1.2e-08  5.5e-03  7.8e-07  1.01e+00   3.573485931e+02   3.573486225e+02   6.8e-12  11.18 
76  1.1e-08  4.9e-03  7.0e-07  1.01e+00   3.573485952e+02   3.573486216e+02   6.1e-12  11.19 
77  9.6e-09  4.4e-03  6.3e-07  1.02e+00   3.573485973e+02   3.573486208e+02   5.6e-12  11.20 
78  8.6e-09  4.0e-03  5.7e-07  9.72e-01   3.573485990e+02   3.573486202e+02   5.0e-12  11.22 
79  7.8e-09  3.6e-03  5.1e-07  9.75e-01   3.573486005e+02   3.573486197e+02   4.5e-12  11.23 
80  1.1e-09  2.0e-04  2.8e-08  9.99e-01   3.573486136e+02   3.573486147e+02   2.5e-13  11.24 
Interior-point optimizer terminated. Time: 11.24. 

Optimizer terminated. Time: 11.25   
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 3.5734861362e+02    Viol.  con: 3e-08    var: 0e+00  
  Dual.    obj: 3.5734861467e+02    Viol.  con: 0e+00    var: 1e-03  
* End solution on dual form. *
Transforming to primal solution.
Solving took 11.3 seconds.
result packing took 2.1% of solve time
solution checking took 0.52% 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               : MACOSX/64-X86   
  Cores                  : 4               

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: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 4               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 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+04          after factor           : 1.72e+05        
Factor     - dense dim.             : 0                 flops                  : 0.00e+00        
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+00        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.3e+05  0.00e+00   -1.289216043e+05  2.000000000e+00   1.0e+00  0.04  
1   1.1e+03  1.4e+03  6.1e+04  -9.71e-01  -1.267234623e+05  3.765824507e+00   4.8e-01  0.06  
2   4.4e+02  5.7e+02  2.5e+04  -9.36e-01  -1.207891901e+05  1.079220696e+01   1.9e-01  0.07  
3   2.9e+02  3.7e+02  1.6e+04  -8.43e-01  -1.159643308e+05  6.124840936e+01   1.3e-01  0.09  
4   2.9e+02  3.7e+02  1.6e+04  -7.61e-01  -1.137878989e+05  1.933393813e+03   1.3e-01  0.11  
5   8.6e+01  1.1e+02  4.9e+03  -7.56e-01  -7.882906344e+04  1.027174326e+04   3.8e-02  0.12  
6   2.9e+01  3.7e+01  1.6e+03  -2.77e-01  -3.734750357e+04  1.217880912e+04   1.3e-02  0.13  
7   1.4e+01  1.8e+01  7.6e+02  4.30e-01   -2.027313450e+04  6.145213700e+03   6.0e-03  0.15  
8   7.6e+00  9.8e+00  4.3e+02  7.36e-01   -1.178613513e+04  3.700599094e+03   3.3e-03  0.16  
9   2.9e+00  3.7e+00  1.6e+02  8.69e-01   -4.521200079e+03  1.607709322e+03   1.3e-03  0.18  
10  1.4e+00  1.8e+00  7.8e+01  9.69e-01   -1.993005199e+03  9.612507524e+02   6.1e-04  0.19  
11  9.6e-01  1.2e+00  5.4e+01  9.89e-01   -1.376515242e+03  6.927086403e+02   4.3e-04  0.21  
12  8.3e-01  1.1e+00  4.7e+01  9.73e-01   -1.213273098e+03  6.063516389e+02   3.7e-04  0.23  
13  3.4e-01  4.4e-01  2.0e+01  9.84e-01   -4.820537960e+02  2.711212780e+02   1.5e-04  0.24  
14  1.8e-01  2.4e-01  1.0e+01  1.01e+00   -2.287523383e+02  1.619766578e+02   8.1e-05  0.26  
15  6.3e-02  1.3e-01  3.7e+00  9.99e-01   -6.068913376e+01  8.123117011e+01   3.0e-05  0.27  
16  2.7e-02  8.9e-02  1.6e+00  1.00e+00   -5.697627179e+00  5.547999097e+01   1.3e-05  0.29  
17  1.4e-02  7.6e-02  8.5e-01  1.00e+00   1.353070472e+01   4.630832532e+01   6.9e-06  0.31  
18  3.0e-03  1.3e-01  1.9e-01  1.00e+00   3.130592595e+01   3.844541768e+01   1.5e-06  0.32  
19  1.8e-03  9.3e-02  1.1e-01  1.00e+00   3.336545518e+01   3.754073097e+01   9.0e-07  0.34  
20  4.6e-04  1.1e-01  2.9e-02  1.00e+00   3.548910363e+01   3.658515831e+01   2.4e-07  0.36  
21  2.3e-04  8.4e-02  1.5e-02  1.00e+00   3.585850823e+01   3.641775549e+01   1.2e-07  0.37  
22  2.1e-04  7.6e-02  1.3e-02  1.00e+00   3.589840085e+01   3.640172469e+01   1.1e-07  0.39  
23  1.3e-04  6.2e-02  7.8e-03  1.00e+00   3.603816392e+01   3.633745879e+01   6.5e-08  0.40  
24  1.1e-04  5.6e-02  7.0e-03  1.00e+00   3.605907788e+01   3.632844007e+01   5.9e-08  0.42  
25  1.0e-04  5.1e-02  6.3e-03  1.00e+00   3.607756192e+01   3.631997468e+01   5.3e-08  0.44  
26  9.2e-05  4.7e-02  5.7e-03  1.00e+00   3.609418403e+01   3.631234560e+01   4.8e-08  0.46  
27  8.2e-05  4.3e-02  5.1e-03  1.00e+00   3.610913195e+01   3.630546906e+01   4.3e-08  0.48  
28  7.4e-05  3.9e-02  4.6e-03  1.00e+00   3.612257865e+01   3.629927529e+01   3.9e-08  0.50  
29  6.7e-05  3.6e-02  4.2e-03  1.00e+00   3.613467559e+01   3.629369705e+01   3.5e-08  0.51  
30  6.0e-05  3.3e-02  3.7e-03  1.00e+00   3.614555885e+01   3.628867368e+01   3.1e-08  0.53  
31  5.4e-05  3.1e-02  3.4e-03  1.00e+00   3.615535056e+01   3.628415028e+01   2.8e-08  0.55  
32  4.9e-05  2.8e-02  3.0e-03  1.00e+00   3.616416052e+01   3.628007732e+01   2.5e-08  0.57  
33  4.4e-05  2.6e-02  2.7e-03  1.00e+00   3.617208739e+01   3.627641014e+01   2.3e-08  0.58  
34  3.9e-05  2.4e-02  2.5e-03  1.00e+00   3.617921989e+01   3.627310846e+01   2.0e-08  0.60  
35  3.5e-05  2.3e-02  2.2e-03  1.00e+00   3.618563780e+01   3.627013596e+01   1.8e-08  0.62  
36  3.2e-05  2.1e-02  2.0e-03  1.00e+00   3.619141284e+01   3.626745993e+01   1.7e-08  0.64  
37  2.9e-05  2.0e-02  1.8e-03  1.00e+00   3.619660951e+01   3.626505090e+01   1.5e-08  0.66  
38  2.6e-05  1.8e-02  1.6e-03  1.00e+00   3.620128582e+01   3.626288229e+01   1.3e-08  0.68  
39  2.3e-05  1.7e-02  1.4e-03  1.00e+00   3.620549394e+01   3.626093014e+01   1.2e-08  0.70  
40  2.1e-05  1.6e-02  1.3e-03  1.00e+00   3.620928080e+01   3.625917290e+01   1.1e-08  0.72  
41  1.9e-05  1.5e-02  1.2e-03  1.00e+00   3.621268862e+01   3.625759109e+01   9.8e-09  0.73  
42  1.7e-05  1.5e-02  1.1e-03  1.00e+00   3.621575535e+01   3.625616726e+01   8.8e-09  0.75  
43  1.5e-05  1.4e-02  9.5e-04  1.00e+00   3.621851516e+01   3.625488563e+01   7.9e-09  0.77  
44  1.4e-05  1.3e-02  8.6e-04  1.00e+00   3.622099878e+01   3.625373200e+01   7.1e-09  0.79  
45  1.2e-05  1.3e-02  7.7e-04  1.00e+00   3.622323385e+01   3.625269360e+01   6.4e-09  0.81  
46  1.1e-05  1.2e-02  6.9e-04  1.00e+00   3.622524525e+01   3.625175891e+01   5.8e-09  0.82  
47  1.0e-05  1.2e-02  6.2e-04  1.00e+00   3.622705537e+01   3.625091758e+01   5.2e-09  0.85  
48  9.0e-06  1.1e-02  5.6e-04  1.00e+00   3.622868435e+01   3.625016027e+01   4.7e-09  0.86  
49  8.1e-06  1.1e-02  5.1e-04  1.00e+00   3.623015031e+01   3.624947859e+01   4.2e-09  0.88  
50  7.3e-06  1.0e-02  4.5e-04  1.00e+00   3.623146957e+01   3.624886498e+01   3.8e-09  0.90  
51  6.6e-06  1.0e-02  4.1e-04  1.00e+00   3.623265681e+01   3.624831265e+01   3.4e-09  0.92  
52  5.9e-06  9.8e-03  3.7e-04  1.00e+00   3.623372524e+01   3.624781548e+01   3.1e-09  0.94  
53  5.3e-06  9.5e-03  3.3e-04  1.00e+00   3.623468674e+01   3.624736796e+01   2.8e-09  0.96  
54  4.8e-06  9.3e-03  3.0e-04  1.00e+00   3.623555202e+01   3.624696511e+01   2.5e-09  0.97  
55  4.3e-06  9.1e-03  2.7e-04  1.00e+00   3.623633070e+01   3.624660248e+01   2.2e-09  0.99  
56  3.9e-06  8.9e-03  2.4e-04  1.00e+00   3.623703146e+01   3.624627606e+01   2.0e-09  1.00  
57  3.5e-06  8.7e-03  2.2e-04  1.00e+00   3.623766209e+01   3.624598223e+01   1.8e-09  1.02  
58  3.1e-06  8.6e-03  2.0e-04  1.00e+00   3.623822960e+01   3.624571773e+01   1.6e-09  1.05  
59  2.8e-06  8.4e-03  1.8e-04  1.00e+00   3.623874032e+01   3.624547964e+01   1.5e-09  1.07  
60  2.5e-06  8.3e-03  1.6e-04  1.00e+00   3.623919993e+01   3.624526531e+01   1.3e-09  1.08  
61  2.3e-06  8.2e-03  1.4e-04  1.00e+00   3.623961354e+01   3.624507237e+01   1.2e-09  1.10  
62  2.1e-06  8.1e-03  1.3e-04  1.00e+00   3.623998576e+01   3.624489872e+01   1.1e-09  1.12  
63  1.9e-06  8.0e-03  1.2e-04  1.00e+00   3.624032072e+01   3.624474239e+01   9.7e-10  1.14  
64  1.7e-06  7.9e-03  1.0e-04  1.00e+00   3.624062217e+01   3.624460167e+01   8.7e-10  1.15  
65  1.5e-06  7.8e-03  9.4e-05  1.00e+00   3.624089345e+01   3.624447500e+01   7.8e-10  1.16  
66  1.4e-06  7.8e-03  8.4e-05  1.00e+00   3.624113758e+01   3.624436098e+01   7.0e-10  1.18  
67  1.2e-06  7.7e-03  7.6e-05  1.00e+00   3.624135728e+01   3.624425836e+01   6.3e-10  1.20  
68  1.1e-06  7.6e-03  6.8e-05  1.00e+00   3.624155499e+01   3.624416596e+01   5.7e-10  1.21  
69  9.9e-07  7.6e-03  6.1e-05  1.00e+00   3.624173292e+01   3.624408281e+01   5.1e-10  1.23  
70  8.9e-07  7.5e-03  5.5e-05  1.00e+00   3.624189305e+01   3.624400796e+01   4.6e-10  1.25  
71  8.0e-07  7.5e-03  5.0e-05  1.00e+00   3.624203715e+01   3.624394058e+01   4.2e-10  1.26  
72  7.2e-07  7.5e-03  4.5e-05  1.00e+00   3.624216683e+01   3.624387993e+01   3.7e-10  1.28  
73  6.5e-07  7.4e-03  4.0e-05  1.00e+00   3.624228354e+01   3.624382532e+01   3.4e-10  1.30  
74  5.8e-07  7.4e-03  3.6e-05  1.00e+00   3.624238856e+01   3.624377619e+01   3.0e-10  1.31  
75  5.2e-07  7.4e-03  3.3e-05  1.00e+00   3.624248308e+01   3.624373195e+01   2.7e-10  1.33  
76  4.7e-07  7.3e-03  2.9e-05  1.00e+00   3.624256814e+01   3.624369213e+01   2.5e-10  1.34  
77  4.2e-07  7.3e-03  2.6e-05  1.00e+00   3.624264470e+01   3.624365628e+01   2.2e-10  1.36  
78  3.8e-07  7.3e-03  2.4e-05  1.00e+00   3.624271359e+01   3.624362401e+01   2.0e-10  1.38  
79  3.4e-07  7.3e-03  2.1e-05  1.00e+00   3.624277559e+01   3.624359496e+01   1.8e-10  1.40  
80  3.1e-07  7.2e-03  1.9e-05  1.00e+00   3.624283139e+01   3.624356883e+01   1.6e-10  1.41  
81  2.8e-07  7.2e-03  1.7e-05  1.00e+00   3.624288160e+01   3.624354529e+01   1.4e-10  1.43  
82  2.5e-07  7.2e-03  1.6e-05  1.00e+00   3.624292679e+01   3.624352411e+01   1.3e-10  1.51  
83  2.3e-07  7.2e-03  1.4e-05  1.00e+00   3.624296747e+01   3.624350504e+01   1.2e-10  1.58  
84  2.0e-07  7.2e-03  1.3e-05  9.99e-01   3.624300406e+01   3.624348790e+01   1.1e-10  1.60  
85  1.8e-07  7.2e-03  1.1e-05  1.00e+00   3.624303700e+01   3.624347246e+01   9.5e-11  1.61  
86  1.6e-07  7.1e-03  1.0e-05  9.99e-01   3.624306664e+01   3.624345857e+01   8.6e-11  1.63  
87  1.5e-07  7.1e-03  9.2e-06  1.00e+00   3.624309331e+01   3.624344606e+01   7.7e-11  1.64  
88  1.3e-07  7.1e-03  8.3e-06  1.00e+00   3.624311733e+01   3.624343478e+01   6.9e-11  1.65  
89  1.2e-07  7.1e-03  7.5e-06  1.00e+00   3.624313893e+01   3.624342464e+01   6.2e-11  1.67  
90  1.1e-07  7.1e-03  6.7e-06  1.00e+00   3.624315838e+01   3.624341552e+01   5.6e-11  1.68  
91  9.7e-08  7.1e-03  6.0e-06  1.00e+00   3.624317588e+01   3.624340731e+01   5.1e-11  1.69  
92  8.7e-08  7.1e-03  5.4e-06  1.00e+00   3.624319163e+01   3.624339991e+01   4.6e-11  1.70  
93  7.9e-08  6.4e-03  4.9e-06  1.00e+00   3.624320587e+01   3.624339320e+01   4.1e-11  1.71  
94  7.1e-08  5.7e-03  4.4e-06  1.00e+00   3.624321862e+01   3.624338722e+01   3.7e-11  1.73  
95  6.4e-08  5.2e-03  4.0e-06  1.00e+00   3.624323010e+01   3.624338183e+01   3.3e-11  1.74  
96  5.7e-08  4.6e-03  3.6e-06  1.00e+00   3.624324043e+01   3.624337698e+01   3.0e-11  1.75  
97  5.2e-08  4.2e-03  3.2e-06  9.97e-01   3.624324972e+01   3.624337263e+01   2.7e-11  1.76  
98  4.6e-08  3.8e-03  2.9e-06  9.98e-01   3.624325808e+01   3.624336871e+01   2.4e-11  1.77  
99  4.2e-08  3.4e-03  2.6e-06  9.99e-01   3.624326560e+01   3.624336518e+01   2.2e-11  1.79  
100 3.8e-08  3.0e-03  2.3e-06  1.00e+00   3.624327238e+01   3.624336200e+01   2.0e-11  1.80  
101 3.4e-08  2.7e-03  2.1e-06  1.01e+00   3.624327859e+01   3.624335906e+01   1.8e-11  1.81  
102 3.1e-08  2.5e-03  1.9e-06  9.93e-01   3.624328406e+01   3.624335651e+01   1.6e-11  1.83  
103 2.7e-08  2.2e-03  1.7e-06  9.99e-01   3.624328899e+01   3.624335419e+01   1.4e-11  1.84  
104 2.5e-08  2.0e-03  1.5e-06  1.00e+00   3.624329350e+01   3.624335206e+01   1.3e-11  1.85  
105 2.2e-08  1.8e-03  1.4e-06  1.00e+00   3.624329752e+01   3.624335017e+01   1.2e-11  1.86  
106 2.0e-08  1.6e-03  1.2e-06  1.00e+00   3.624330113e+01   3.624334846e+01   1.0e-11  1.87  
107 1.8e-08  1.5e-03  1.1e-06  9.98e-01   3.624330435e+01   3.624334695e+01   9.4e-12  1.88  
108 1.6e-08  1.3e-03  1.0e-06  9.95e-01   3.624330725e+01   3.624334560e+01   8.5e-12  1.90  
109 1.5e-08  1.2e-03  9.1e-07  1.00e+00   3.624330990e+01   3.624334435e+01   7.7e-12  1.91  
110 1.3e-08  1.1e-03  8.2e-07  1.01e+00   3.624331229e+01   3.624334321e+01   6.9e-12  1.92  
111 1.2e-08  9.6e-04  7.4e-07  9.99e-01   3.624331440e+01   3.624334223e+01   6.2e-12  1.94  
112 1.1e-08  8.6e-04  6.6e-07  1.00e+00   3.624331629e+01   3.624334134e+01   5.6e-12  1.95  
113 9.6e-09  7.7e-04  6.0e-07  1.00e+00   3.624331799e+01   3.624334054e+01   5.0e-12  1.97  
114 8.6e-09  7.0e-04  5.4e-07  9.99e-01   3.624331953e+01   3.624333982e+01   4.5e-12  1.98  
115 7.8e-09  6.3e-04  4.8e-07  1.00e+00   3.624332091e+01   3.624333916e+01   4.1e-12  2.00  
116 7.0e-09  5.6e-04  4.3e-07  1.00e+00   3.624332215e+01   3.624333858e+01   3.7e-12  2.01  
117 6.3e-09  5.1e-04  3.9e-07  9.99e-01   3.624332327e+01   3.624333805e+01   3.3e-12  2.03  
118 5.7e-09  4.6e-04  3.5e-07  1.00e+00   3.624332428e+01   3.624333758e+01   3.0e-12  2.04  
119 5.1e-09  4.1e-04  3.2e-07  1.00e+00   3.624332519e+01   3.624333715e+01   2.7e-12  2.06  
120 4.6e-09  3.7e-04  2.8e-07  1.00e+00   3.624332600e+01   3.624333677e+01   2.4e-12  2.07  
121 4.1e-09  3.3e-04  2.6e-07  1.00e+00   3.624332674e+01   3.624333642e+01   2.2e-12  2.09  
122 3.7e-09  3.0e-04  2.3e-07  9.98e-01   3.624332740e+01   3.624333611e+01   2.0e-12  2.10  
123 3.3e-09  2.7e-04  2.1e-07  1.00e+00   3.624332799e+01   3.624333583e+01   1.8e-12  2.12  
124 3.0e-09  2.4e-04  1.9e-07  9.98e-01   3.624332852e+01   3.624333558e+01   1.6e-12  2.13  
125 2.7e-09  2.2e-04  1.7e-07  9.98e-01   3.624332900e+01   3.624333536e+01   1.4e-12  2.14  
126 2.4e-09  2.0e-04  1.5e-07  1.00e+00   3.624332944e+01   3.624333515e+01   1.3e-12  2.16  
127 2.2e-09  1.8e-04  1.4e-07  9.98e-01   3.624332983e+01   3.624333497e+01   1.2e-12  2.17  
128 2.0e-09  1.6e-04  1.2e-07  1.00e+00   3.624333018e+01   3.624333481e+01   1.0e-12  2.18  
129 1.8e-09  1.4e-04  1.1e-07  1.00e+00   3.624333049e+01   3.624333466e+01   9.4e-13  2.20  
Interior-point optimizer terminated. Time: 2.20. 

Optimizer terminated. Time: 2.21    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 3.6243330493e+01    Viol.  con: 3e-08    var: 0e+00  
  Dual.    obj: 3.6243334658e+01    Viol.  con: 0e+00    var: 1e-03  
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.23 seconds.
result packing took 10% of solve time
solution checking took 3.4% 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               : MACOSX/64-X86   
  Cores                  : 4               

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: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 4               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 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 : 1.68e+04          after factor           : 1.72e+05        
Factor     - dense dim.             : 0                 flops                  : 0.00e+00        
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+00        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.3e+05  0.00e+00   -1.288884984e+05  2.000000000e+00   1.0e+00  0.04  
1   1.1e+03  1.4e+03  6.1e+04  -9.71e-01  -1.266820511e+05  3.737215726e+00   4.7e-01  0.05  
2   4.2e+02  5.4e+02  2.4e+04  -9.36e-01  -1.204157429e+05  1.081474446e+01   1.8e-01  0.06  
3   2.8e+02  3.7e+02  1.6e+04  -8.37e-01  -1.158007450e+05  6.704673268e+01   1.3e-01  0.08  
4   2.8e+02  3.7e+02  1.6e+04  -7.58e-01  -1.132325325e+05  2.253045227e+03   1.3e-01  0.09  
5   7.6e+01  9.8e+01  4.3e+03  -7.52e-01  -7.382533601e+04  1.111355887e+04   3.4e-02  0.11  
6   3.1e+01  4.0e+01  1.8e+03  -1.94e-01  -4.049644069e+04  1.108917960e+04   1.4e-02  0.12  
7   1.4e+01  1.8e+01  7.8e+02  3.80e-01   -2.080727929e+04  5.941320023e+03   6.1e-03  0.14  
8   9.1e+00  1.2e+01  5.2e+02  7.28e-01   -1.424653656e+04  4.128716153e+03   4.1e-03  0.15  
9   3.6e+00  4.7e+00  2.1e+02  8.32e-01   -5.839340219e+03  1.817801172e+03   1.6e-03  0.16  
10  2.0e+00  2.6e+00  1.1e+02  9.53e-01   -2.954017022e+03  1.332822173e+03   9.0e-04  0.17  
11  9.0e-01  1.2e+00  5.1e+01  9.84e-01   -1.322610957e+03  6.197743148e+02   4.1e-04  0.19  
12  8.6e-01  1.2e+00  4.9e+01  9.64e-01   -1.285088758e+03  5.818497466e+02   3.9e-04  0.20  
13  3.8e-01  5.3e-01  2.2e+01  9.81e-01   -5.636834299e+02  2.752505457e+02   1.7e-04  0.21  
14  1.5e-01  2.3e-01  8.6e+00  1.00e+00   -2.175252852e+02  1.113181123e+02   6.9e-05  0.23  
15  8.6e-02  1.5e-01  5.0e+00  1.00e+00   -1.179457363e+02  7.374921030e+01   4.0e-05  0.24  
16  2.6e-02  1.2e-01  1.6e+00  1.00e+00   -2.814249572e+01  3.134816686e+01   1.3e-05  0.25  
17  1.1e-02  9.3e-02  6.9e-01  1.00e+00   -5.281172182e+00  2.122383987e+01   5.7e-06  0.27  
18  1.0e-02  8.5e-02  6.3e-01  1.01e+00   -3.407113433e+00  2.059327051e+01   5.2e-06  0.29  
19  6.6e-03  6.5e-02  4.0e-01  1.01e+00   2.894343015e+00   1.822729808e+01   3.3e-06  0.30  
20  4.5e-03  4.7e-02  2.8e-01  1.01e+00   6.716937820e+00   1.712679469e+01   2.3e-06  0.31  
21  1.8e-03  5.9e-02  1.1e-01  1.01e+00   1.120108485e+01   1.544829229e+01   9.4e-07  0.32  
22  1.0e-03  4.8e-02  6.2e-02  1.02e+00   1.265242209e+01   1.495250842e+01   5.1e-07  0.33  
23  4.6e-04  5.4e-02  2.9e-02  1.02e+00   1.351745514e+01   1.458911808e+01   2.4e-07  0.35  
24  2.6e-04  5.1e-02  1.6e-02  1.01e+00   1.386209162e+01   1.445405127e+01   1.3e-07  0.36  
25  1.3e-04  5.2e-02  8.4e-03  1.01e+00   1.406310935e+01   1.437335775e+01   7.1e-08  0.38  
26  8.9e-05  4.6e-02  5.6e-03  1.01e+00   1.413708002e+01   1.434303555e+01   4.7e-08  0.40  
27  8.0e-05  4.2e-02  5.0e-03  1.00e+00   1.415520978e+01   1.434064260e+01   4.2e-08  0.42  
28  7.2e-05  3.9e-02  4.5e-03  1.00e+00   1.416777692e+01   1.433463427e+01   3.8e-08  0.43  
29  6.5e-05  3.6e-02  4.1e-03  1.00e+00   1.417931743e+01   1.432946876e+01   3.4e-08  0.44  
30  5.8e-05  3.3e-02  3.7e-03  1.00e+00   1.418965056e+01   1.432477025e+01   3.1e-08  0.46  
31  5.3e-05  3.0e-02  3.3e-03  1.00e+00   1.419892928e+01   1.432052345e+01   2.8e-08  0.48  
32  4.7e-05  2.8e-02  3.0e-03  1.00e+00   1.420725910e+01   1.431668306e+01   2.5e-08  0.49  
33  4.3e-05  2.6e-02  2.7e-03  1.00e+00   1.421473784e+01   1.431321069e+01   2.3e-08  0.51  
34  3.8e-05  2.4e-02  2.4e-03  1.00e+00   1.422145355e+01   1.431007207e+01   2.0e-08  0.52  
35  3.4e-05  2.2e-02  2.2e-03  1.00e+00   1.422748549e+01   1.430723641e+01   1.8e-08  0.53  
36  3.1e-05  2.1e-02  2.0e-03  1.00e+00   1.423290462e+01   1.430467558e+01   1.6e-08  0.55  
37  2.8e-05  2.0e-02  1.8e-03  1.00e+00   1.423777426e+01   1.430236434e+01   1.5e-08  0.56  
38  2.5e-05  1.8e-02  1.6e-03  1.00e+00   1.424215080e+01   1.430027879e+01   1.3e-08  0.57  
39  2.3e-05  1.7e-02  1.4e-03  1.00e+00   1.424608474e+01   1.429839761e+01   1.2e-08  0.59  
40  2.0e-05  1.6e-02  1.3e-03  1.00e+00   1.424962124e+01   1.429670081e+01   1.1e-08  0.60  
41  1.8e-05  1.6e-02  1.2e-03  1.00e+00   1.425280084e+01   1.429517098e+01   9.7e-09  0.62  
42  1.6e-05  1.5e-02  1.0e-03  1.00e+00   1.425565978e+01   1.429379127e+01   8.7e-09  0.64  
43  1.5e-05  1.4e-02  9.4e-04  1.00e+00   1.425823065e+01   1.429254754e+01   7.9e-09  0.65  
44  1.3e-05  1.3e-02  8.4e-04  1.00e+00   1.426054248e+01   1.429142685e+01   7.1e-09  0.66  
45  1.2e-05  1.3e-02  7.6e-04  1.00e+00   1.426262137e+01   1.429041684e+01   6.4e-09  0.68  
46  1.1e-05  1.2e-02  6.8e-04  1.00e+00   1.426449088e+01   1.428950615e+01   5.7e-09  0.69  
47  9.7e-06  1.2e-02  6.1e-04  1.00e+00   1.426617204e+01   1.428868573e+01   5.2e-09  0.71  
48  8.8e-06  1.1e-02  5.5e-04  1.00e+00   1.426768377e+01   1.428794578e+01   4.6e-09  0.72  
49  7.9e-06  1.1e-02  5.0e-04  1.00e+00   1.426904315e+01   1.428727862e+01   4.2e-09  0.74  
50  7.1e-06  1.1e-02  4.5e-04  1.00e+00   1.427026545e+01   1.428667714e+01   3.8e-09  0.75  
51  6.4e-06  1.0e-02  4.0e-04  1.00e+00   1.427136445e+01   1.428613480e+01   3.4e-09  0.76  
52  5.8e-06  1.0e-02  3.6e-04  1.00e+00   1.427235265e+01   1.428564563e+01   3.0e-09  0.78  
53  5.2e-06  9.8e-03  3.3e-04  1.00e+00   1.427324132e+01   1.428520431e+01   2.7e-09  0.79  
54  4.7e-06  9.5e-03  2.9e-04  1.00e+00   1.427404034e+01   1.428480738e+01   2.5e-09  0.81  
55  4.2e-06  9.3e-03  2.6e-04  9.99e-01   1.427475889e+01   1.428444980e+01   2.2e-09  0.82  
56  3.8e-06  9.1e-03  2.4e-04  9.99e-01   1.427540523e+01   1.428412754e+01   2.0e-09  0.84  
57  3.4e-06  9.0e-03  2.1e-04  1.00e+00   1.427598678e+01   1.428383680e+01   1.8e-09  0.85  
58  3.1e-06  8.8e-03  1.9e-04  1.00e+00   1.427650997e+01   1.428357501e+01   1.6e-09  0.87  
59  2.8e-06  8.7e-03  1.7e-04  9.99e-01   1.427698063e+01   1.428333944e+01   1.5e-09  0.88  
60  2.5e-06  8.5e-03  1.6e-04  1.00e+00   1.427740416e+01   1.428312709e+01   1.3e-09  0.89  
61  2.2e-06  8.4e-03  1.4e-04  1.00e+00   1.427778527e+01   1.428293578e+01   1.2e-09  0.90  
62  2.0e-06  8.3e-03  1.3e-04  9.99e-01   1.427812811e+01   1.428276386e+01   1.1e-09  0.92  
63  1.8e-06  8.2e-03  1.1e-04  9.99e-01   1.427843660e+01   1.428260902e+01   9.6e-10  0.93  
64  1.6e-06  8.1e-03  1.0e-04  9.99e-01   1.427871421e+01   1.428246953e+01   8.6e-10  0.94  
65  1.5e-06  8.1e-03  9.2e-05  9.98e-01   1.427896397e+01   1.428234411e+01   7.7e-10  0.96  
66  1.3e-06  8.0e-03  8.3e-05  9.99e-01   1.427918874e+01   1.428223112e+01   7.0e-10  0.97  
67  1.2e-06  7.9e-03  7.5e-05  9.97e-01   1.427939096e+01   1.428212954e+01   6.3e-10  0.99  
68  1.1e-06  7.9e-03  6.7e-05  1.00e+00   1.427957314e+01   1.428203742e+01   5.6e-10  1.00  
69  9.6e-07  7.8e-03  6.0e-05  9.98e-01   1.427973692e+01   1.428195501e+01   5.1e-10  1.02  
70  8.6e-07  7.8e-03  5.4e-05  1.00e+00   1.427988433e+01   1.428188062e+01   4.6e-10  1.03  
71  7.8e-07  7.7e-03  4.9e-05  1.00e+00   1.428001701e+01   1.428181358e+01   4.1e-10  1.05  
72  7.0e-07  7.7e-03  4.4e-05  1.00e+00   1.428013649e+01   1.428175310e+01   3.7e-10  1.06  
73  6.3e-07  7.7e-03  4.0e-05  1.00e+00   1.428024393e+01   1.428169875e+01   3.3e-10  1.07  
74  5.7e-07  7.7e-03  3.6e-05  1.00e+00   1.428034143e+01   1.428164931e+01   3.0e-10  1.09  
75  5.1e-07  6.9e-03  3.2e-05  1.01e+00   1.428043103e+01   1.428160368e+01   2.7e-10  1.10  
76  4.6e-07  6.2e-03  2.9e-05  1.00e+00   1.428050898e+01   1.428156426e+01   2.4e-10  1.12  
77  4.1e-07  5.6e-03  2.6e-05  9.91e-01   1.428057902e+01   1.428152922e+01   2.2e-10  1.13  
78  3.7e-07  5.0e-03  2.3e-05  1.01e+00   1.428064435e+01   1.428149589e+01   2.0e-10  1.15  
79  3.3e-07  4.5e-03  2.1e-05  1.01e+00   1.428070232e+01   1.428146641e+01   1.8e-10  1.17  
80  3.0e-07  4.1e-03  1.9e-05  9.88e-01   1.428075302e+01   1.428144110e+01   1.6e-10  1.18  
81  2.7e-07  3.7e-03  1.7e-05  9.93e-01   1.428079867e+01   1.428141815e+01   1.5e-10  1.19  
82  2.4e-07  3.3e-03  1.5e-05  9.94e-01   1.428083976e+01   1.428139747e+01   1.3e-10  1.21  
83  2.2e-07  3.0e-03  1.4e-05  1.01e+00   1.428087874e+01   1.428137747e+01   1.2e-10  1.23  
84  2.0e-07  2.7e-03  1.2e-05  9.99e-01   1.428091185e+01   1.428136074e+01   1.1e-10  1.24  
85  1.8e-07  2.4e-03  1.1e-05  1.00e+00   1.428094174e+01   1.428134557e+01   9.6e-11  1.26  
86  1.6e-07  2.2e-03  1.0e-05  9.88e-01   1.428096851e+01   1.428133218e+01   8.6e-11  1.27  
87  1.4e-07  1.9e-03  9.1e-06  9.76e-01   1.428099255e+01   1.428132026e+01   7.8e-11  1.28  
88  1.3e-07  1.8e-03  8.2e-06  1.01e+00   1.428101522e+01   1.428130861e+01   7.0e-11  1.30  
89  1.2e-07  1.6e-03  7.3e-06  9.99e-01   1.428103468e+01   1.428129874e+01   6.3e-11  1.31  
90  1.1e-07  1.4e-03  6.6e-06  9.71e-01   1.428105211e+01   1.428129012e+01   5.7e-11  1.32  
91  9.5e-08  1.3e-03  6.0e-06  9.80e-01   1.428106783e+01   1.428128225e+01   5.1e-11  1.33  
92  8.5e-08  1.1e-03  5.4e-06  1.07e+00   1.428108671e+01   1.428127196e+01   4.8e-11  1.35  
93  7.7e-08  1.0e-03  4.8e-06  9.96e-01   1.428109901e+01   1.428126577e+01   4.3e-11  1.36  
94  6.9e-08  9.3e-04  4.3e-06  9.81e-01   1.428111005e+01   1.428126027e+01   3.9e-11  1.37  
95  6.2e-08  8.4e-04  3.9e-06  9.74e-01   1.428111998e+01   1.428125536e+01   3.5e-11  1.38  
96  5.6e-08  7.5e-04  3.5e-06  1.03e+00   1.428113023e+01   1.428124999e+01   3.2e-11  1.39  
97  5.1e-08  6.8e-04  3.2e-06  1.14e+00   1.428114322e+01   1.428124258e+01   3.1e-11  1.40  
98  4.6e-08  6.1e-04  2.8e-06  9.51e-01   1.428114982e+01   1.428123947e+01   2.8e-11  1.41  
99  4.1e-08  5.5e-04  2.6e-06  9.85e-01   1.428115579e+01   1.428123654e+01   2.5e-11  1.42  
100 3.7e-08  4.9e-04  2.3e-06  1.01e+00   1.428116144e+01   1.428123369e+01   2.2e-11  1.43  
101 3.3e-08  4.4e-04  2.1e-06  9.83e-01   1.428116626e+01   1.428123133e+01   2.0e-11  1.44  
102 3.0e-08  4.0e-04  1.9e-06  1.29e+00   1.428117078e+01   1.428122851e+01   1.8e-11  1.46  
103 2.7e-08  3.6e-04  1.7e-06  1.09e+00   1.428117627e+01   1.428122563e+01   1.7e-11  1.47  
104 2.5e-08  3.2e-04  1.5e-06  9.89e-01   1.428117961e+01   1.428122406e+01   1.5e-11  1.48  
105 2.2e-08  2.9e-04  1.4e-06  9.81e-01   1.428118261e+01   1.428122265e+01   1.4e-11  1.49  
106 2.0e-08  2.6e-04  1.2e-06  9.80e-01   1.428118530e+01   1.428122138e+01   1.2e-11  1.50  
107 1.8e-08  2.4e-04  1.1e-06  1.01e+00   1.428118784e+01   1.428122014e+01   1.1e-11  1.51  
108 1.6e-08  2.1e-04  9.9e-07  1.03e+00   1.428119027e+01   1.428121894e+01   1.0e-11  1.52  
109 1.5e-08  1.9e-04  8.9e-07  9.74e-01   1.428119220e+01   1.428121804e+01   9.2e-12  1.53  
110 1.3e-08  1.7e-04  8.0e-07  9.92e-01   1.428119394e+01   1.428121721e+01   8.3e-12  1.55  
111 1.2e-08  1.6e-04  7.2e-07  1.04e+00   1.428119576e+01   1.428121630e+01   7.6e-12  1.56  
112 1.1e-08  1.4e-04  6.5e-07  1.02e+00   1.428119724e+01   1.428121558e+01   6.9e-12  1.57  
113 9.5e-09  1.3e-04  5.9e-07  9.74e-01   1.428119848e+01   1.428121501e+01   6.2e-12  1.59  
114 8.6e-09  1.1e-04  5.3e-07  9.91e-01   1.428119959e+01   1.428121448e+01   5.6e-12  1.60  
115 7.8e-09  1.0e-04  4.7e-07  1.05e+00   1.428120083e+01   1.428121385e+01   5.2e-12  1.61  
116 7.0e-09  9.2e-05  4.3e-07  9.97e-01   1.428120171e+01   1.428121344e+01   4.6e-12  1.63  
117 6.3e-09  8.2e-05  3.8e-07  1.05e+00   1.428120268e+01   1.428121294e+01   4.3e-12  1.64  
118 5.9e-09  7.4e-05  3.5e-07  1.14e+00   1.428120381e+01   1.428121233e+01   4.1e-12  1.66  
119 5.3e-09  6.7e-05  3.1e-07  9.78e-01   1.428120439e+01   1.428121207e+01   3.7e-12  1.67  
120 4.8e-09  6.0e-05  2.8e-07  9.90e-01   1.428120492e+01   1.428121183e+01   3.3e-12  1.69  
121 4.4e-09  5.4e-05  2.5e-07  1.11e+00   1.428120563e+01   1.428121147e+01   3.2e-12  1.70  
122 4.0e-09  4.9e-05  2.3e-07  9.23e-01   1.428120603e+01   1.428121130e+01   2.9e-12  1.71  
123 3.6e-09  4.4e-05  2.0e-07  1.18e+00   1.428120640e+01   1.428121110e+01   2.6e-12  1.73  
124 3.2e-09  3.9e-05  1.8e-07  9.19e-01   1.428120672e+01   1.428121097e+01   2.3e-12  1.74  
125 3.0e-09  3.5e-05  1.7e-07  1.39e+00   1.428120703e+01   1.428121079e+01   2.1e-12  1.75  
126 3.0e-09  3.5e-05  1.7e-07  1.15e+00   1.428120703e+01   1.428121079e+01   2.1e-12  1.76  
127 2.8e-09  3.2e-05  1.5e-07  1.09e+00   1.428120740e+01   1.428121061e+01   2.0e-12  1.77  
128 2.5e-09  2.9e-05  1.3e-07  1.04e+00   1.428120766e+01   1.428121050e+01   1.8e-12  1.78  
Interior-point optimizer terminated. Time: 1.78. 

Optimizer terminated. Time: 1.79    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.4281207661e+01    Viol.  con: 2e-08    var: 0e+00  
  Dual.    obj: 1.4281210495e+01    Viol.  con: 0e+00    var: 1e-04  
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.81 seconds.
result packing took 9.4% 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               : MACOSX/64-X86   
  Cores                  : 4               

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: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 4               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 831
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3581              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.02              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.01            
Factor     - nonzeros before factor : 1.68e+04          after factor           : 1.72e+05        
Factor     - dense dim.             : 0                 flops                  : 0.00e+00        
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+00        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.3e+05  0.00e+00   -1.289122963e+05  2.000000000e+00   1.0e+00  0.03  
1   1.1e+03  1.4e+03  6.0e+04  -9.71e-01  -1.266641855e+05  3.741476762e+00   4.7e-01  0.04  
2   4.0e+02  5.1e+02  2.2e+04  -9.35e-01  -1.198199307e+05  1.134152236e+01   1.7e-01  0.05  
3   2.8e+02  3.6e+02  1.6e+04  -8.28e-01  -1.157343514e+05  8.423404354e+01   1.2e-01  0.07  
4   2.8e+02  3.6e+02  1.6e+04  -7.56e-01  -1.124205614e+05  2.836434211e+03   1.2e-01  0.08  
5   6.3e+01  8.2e+01  3.6e+03  -7.47e-01  -6.653639604e+04  1.265850643e+04   2.8e-02  0.10  
6   3.9e+01  5.1e+01  2.2e+03  -7.39e-02  -4.844534873e+04  1.112911726e+04   1.7e-02  0.11  
7   2.8e+01  3.6e+01  1.6e+03  2.53e-01   -3.796102008e+04  8.631275866e+03   1.2e-02  0.12  
8   1.5e+01  2.0e+01  8.6e+02  4.43e-01   -2.324603353e+04  5.309498801e+03   6.8e-03  0.13  
9   5.9e+00  7.6e+00  3.3e+02  6.91e-01   -9.449281539e+03  2.651165846e+03   2.6e-03  0.14  
10  3.3e+00  4.2e+00  1.8e+02  9.01e-01   -5.020447390e+03  1.803995326e+03   1.5e-03  0.15  
11  1.1e+00  1.4e+00  6.3e+01  9.61e-01   -1.685591796e+03  6.933209085e+02   5.0e-04  0.16  
12  9.1e-01  1.3e+00  5.2e+01  9.86e-01   -1.368780046e+03  5.972104188e+02   4.1e-04  0.17  
13  6.9e-01  1.2e+00  3.9e+01  9.72e-01   -1.052846903e+03  4.579754379e+02   3.1e-04  0.18  
14  3.7e-01  6.3e-01  2.1e+01  9.98e-01   -5.484248499e+02  2.640773145e+02   1.7e-04  0.19  
15  1.2e-01  2.2e-01  6.7e+00  9.94e-01   -1.704694296e+02  8.550126015e+01   5.4e-05  0.20  
16  8.2e-02  1.7e-01  4.8e+00  1.01e+00   -1.180299081e+02  6.425286973e+01   3.9e-05  0.21  
17  3.3e-02  1.1e-01  1.9e+00  1.01e+00   -4.285663239e+01  3.068998130e+01   1.6e-05  0.22  
18  1.8e-02  8.2e-02  1.1e+00  1.01e+00   -2.020795108e+01  2.029575279e+01   8.7e-06  0.23  
19  1.7e-02  7.9e-02  1.0e+00  1.02e+00   -1.893334809e+01  2.022143785e+01   8.5e-06  0.25  
20  1.0e-02  6.0e-02  6.2e-01  1.02e+00   -5.882682737e+00  1.716798531e+01   5.0e-06  0.26  
21  4.4e-03  6.0e-02  2.6e-01  1.02e+00   4.086876962e+00   1.378683844e+01   2.1e-06  0.27  
22  2.2e-03  5.7e-02  1.3e-01  1.01e+00   7.629385167e+00   1.261761962e+01   1.1e-06  0.28  
23  6.0e-04  8.3e-02  3.9e-02  9.80e-01   1.031730189e+01   1.179835972e+01   3.4e-07  0.29  
24  1.7e-04  8.8e-02  1.2e-02  9.64e-01   1.108842463e+01   1.155999006e+01   1.1e-07  0.30  
25  5.7e-05  8.4e-02  4.2e-03  9.80e-01   1.132953629e+01   1.149071900e+01   3.9e-08  0.32  
26  2.1e-05  8.3e-02  1.5e-03  9.93e-01   1.141258295e+01   1.147148141e+01   1.4e-08  0.33  
27  7.6e-06  8.1e-02  5.7e-04  9.98e-01   1.144298018e+01   1.146497788e+01   5.4e-09  0.35  
28  6.8e-06  7.3e-02  5.1e-04  1.00e+00   1.144490443e+01   1.146470418e+01   4.8e-09  0.36  
29  6.2e-06  6.7e-02  4.6e-04  1.00e+00   1.144649120e+01   1.146431184e+01   4.3e-09  0.37  
30  5.5e-06  6.1e-02  4.1e-04  1.00e+00   1.144791949e+01   1.146395875e+01   3.9e-09  0.38  
31  5.0e-06  5.5e-02  3.7e-04  1.00e+00   1.144920234e+01   1.146363823e+01   3.5e-09  0.39  
32  4.5e-06  5.0e-02  3.4e-04  1.00e+00   1.145035575e+01   1.146334851e+01   3.2e-09  0.40  
33  4.0e-06  4.6e-02  3.0e-04  1.00e+00   1.145139271e+01   1.146308654e+01   2.9e-09  0.41  
34  3.6e-06  4.2e-02  2.7e-04  1.00e+00   1.145232508e+01   1.146284980e+01   2.6e-09  0.42  
35  3.3e-06  3.9e-02  2.4e-04  1.00e+00   1.145316348e+01   1.146263599e+01   2.3e-09  0.43  
36  2.9e-06  3.5e-02  2.2e-04  1.00e+00   1.145391746e+01   1.146244294e+01   2.1e-09  0.44  
37  2.7e-06  3.3e-02  2.0e-04  1.00e+00   1.145459559e+01   1.146226865e+01   1.9e-09  0.46  
38  2.4e-06  3.0e-02  1.8e-04  1.00e+00   1.145520554e+01   1.146211141e+01   1.7e-09  0.47  
39  2.1e-06  2.8e-02  1.6e-04  1.00e+00   1.145575422e+01   1.146196958e+01   1.5e-09  0.48  
40  1.9e-06  2.6e-02  1.4e-04  1.00e+00   1.145624779e+01   1.146184172e+01   1.4e-09  0.49  
41  1.7e-06  2.4e-02  1.3e-04  1.00e+00   1.145669183e+01   1.146172646e+01   1.2e-09  0.50  
42  1.6e-06  2.2e-02  1.2e-04  1.00e+00   1.145709134e+01   1.146162255e+01   1.1e-09  0.51  
43  1.4e-06  2.1e-02  1.1e-04  1.00e+00   1.145745078e+01   1.146152892e+01   1.0e-09  0.53  
44  1.3e-06  1.9e-02  9.5e-05  1.00e+00   1.145777417e+01   1.146144460e+01   9.0e-10  0.67  
45  1.1e-06  1.8e-02  8.5e-05  1.00e+00   1.145806516e+01   1.146136863e+01   8.1e-10  0.90  
46  1.0e-06  1.7e-02  7.7e-05  1.00e+00   1.145832701e+01   1.146130018e+01   7.3e-10  0.97  
47  9.2e-07  1.6e-02  6.9e-05  1.00e+00   1.145856263e+01   1.146123851e+01   6.5e-10  1.03  
48  8.3e-07  1.5e-02  6.2e-05  1.00e+00   1.145877466e+01   1.146118298e+01   5.9e-10  1.04  
49  7.5e-07  1.4e-02  5.6e-05  1.00e+00   1.145896544e+01   1.146113301e+01   5.3e-10  1.23  
50  6.7e-07  1.3e-02  5.0e-05  1.00e+00   1.145913714e+01   1.146108798e+01   4.8e-10  1.55  
51  6.1e-07  1.3e-02  4.5e-05  1.00e+00   1.145929166e+01   1.146104742e+01   4.3e-10  1.63  
52  5.5e-07  1.2e-02  4.1e-05  1.00e+00   1.145943073e+01   1.146101085e+01   3.9e-10  1.81  
53  4.9e-07  1.2e-02  3.7e-05  1.00e+00   1.145955587e+01   1.146097798e+01   3.5e-10  2.49  
54  1.7e-07  4.0e-03  1.3e-05  1.00e+00   1.146029176e+01   1.146078409e+01   1.2e-10  3.02  
55  1.5e-07  3.6e-03  1.1e-05  1.00e+00   1.146033124e+01   1.146077400e+01   1.1e-10  3.52  
56  5.2e-08  1.2e-03  3.9e-06  1.00e+00   1.146056194e+01   1.146071306e+01   3.7e-11  4.02  
57  4.7e-08  1.1e-03  3.5e-06  9.97e-01   1.146057395e+01   1.146070998e+01   3.3e-11  4.53  
58  4.2e-08  1.0e-03  3.2e-06  1.03e+00   1.146058621e+01   1.146070654e+01   3.0e-11  4.96  
59  1.6e-08  1.9e-04  6.1e-07  9.41e-01   1.146066419e+01   1.146068820e+01   6.6e-12  5.44  
60  2.3e-08  1.7e-04  5.5e-07  9.75e-01   1.146066593e+01   1.146068754e+01   5.9e-12  5.98  
61  3.1e-09  2.1e-05  6.8e-08  1.03e+00   1.146067938e+01   1.146068194e+01   6.3e-13  6.65  
Interior-point optimizer terminated. Time: 6.65. 

Optimizer terminated. Time: 6.66    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1460679380e+01    Viol.  con: 6e-08    var: 0e+00  
  Dual.    obj: 1.1460681936e+01    Viol.  con: 0e+00    var: 2e-04  
* End solution on dual form. *
Transforming to primal solution.
Solving took 6.68 seconds.
result packing took 3% of solve time
solution checking took 0.78% 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               : MACOSX/64-X86   
  Cores                  : 4               

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: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 4               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 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 : 1.67e+04          after factor           : 1.72e+05        
Factor     - dense dim.             : 0                 flops                  : 0.00e+00        
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+00        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.3e+05  0.00e+00   -1.288998622e+05  2.000000000e+00   1.0e+00  0.04  
1   1.1e+03  1.4e+03  6.0e+04  -9.71e-01  -1.266356631e+05  3.742467675e+00   4.7e-01  0.27  
2   3.9e+02  5.0e+02  2.2e+04  -9.35e-01  -1.196284527e+05  1.157206574e+01   1.7e-01  0.46  
3   2.8e+02  3.6e+02  1.6e+04  -8.26e-01  -1.157140903e+05  9.724186391e+01   1.2e-01  0.68  
4   2.8e+02  3.6e+02  1.6e+04  -7.57e-01  -1.123511185e+05  2.829386311e+03   1.2e-01  0.83  
5   7.6e+01  9.8e+01  4.2e+03  -7.46e-01  -7.380965031e+04  1.079461445e+04   3.4e-02  0.95  
6   3.7e+01  4.8e+01  2.1e+03  -1.89e-01  -4.675734287e+04  1.109128586e+04   1.7e-02  1.02  
7   2.2e+01  2.8e+01  1.2e+03  2.80e-01   -3.081534419e+04  7.269345016e+03   9.5e-03  1.04  
8   9.8e+00  1.3e+01  5.5e+02  5.68e-01   -1.544071585e+04  3.913317654e+03   4.4e-03  1.05  
9   4.3e+00  5.6e+00  2.4e+02  8.18e-01   -6.768005243e+03  2.130343604e+03   1.9e-03  1.06  
10  2.0e+00  2.6e+00  1.1e+02  9.38e-01   -2.992669543e+03  1.174791871e+03   8.8e-04  1.07  
11  1.4e+00  1.8e+00  8.0e+01  9.83e-01   -2.138665289e+03  8.478739236e+02   6.3e-04  1.08  
12  9.0e-01  1.2e+00  5.1e+01  9.85e-01   -1.363628613e+03  5.635915091e+02   4.1e-04  1.09  
13  7.5e-01  1.1e+00  4.3e+01  9.64e-01   -1.152052992e+03  4.738402527e+02   3.4e-04  1.11  
14  2.9e-01  4.3e-01  1.6e+01  9.89e-01   -4.269653693e+02  1.973282739e+02   1.3e-04  1.12  
15  1.5e-01  2.3e-01  8.6e+00  1.00e+00   -2.191074201e+02  1.087043265e+02   6.9e-05  1.13  
16  4.4e-02  1.5e-01  2.6e+00  1.00e+00   -6.101179011e+01  3.727654829e+01   2.1e-05  1.15  
17  3.6e-02  1.3e-01  2.1e+00  1.00e+00   -4.920937030e+01  3.255867757e+01   1.8e-05  1.16  
18  2.0e-02  9.0e-02  1.2e+00  1.00e+00   -2.393088460e+01  2.130475943e+01   9.7e-06  1.18  
19  1.5e-02  7.0e-02  8.7e-01  1.02e+00   -1.436469667e+01  1.845759479e+01   7.1e-06  1.19  
20  8.1e-03  4.7e-02  4.8e-01  1.03e+00   -2.357640143e+00  1.563339742e+01   4.0e-06  1.20  
21  2.3e-03  8.8e-02  1.4e-01  1.02e+00   7.463787831e+00   1.257879557e+01   1.2e-06  1.22  
22  1.2e-03  5.9e-02  7.6e-02  9.89e-01   9.105869602e+00   1.193675386e+01   6.5e-07  1.23  
23  4.1e-04  7.4e-02  2.7e-02  9.72e-01   1.056493038e+01   1.158083218e+01   2.4e-07  1.25  
24  1.6e-04  6.8e-02  1.1e-02  9.77e-01   1.102208126e+01   1.144786899e+01   1.0e-07  1.26  
25  7.0e-05  6.7e-02  4.8e-03  9.91e-01   1.120979970e+01   1.139317382e+01   4.3e-08  1.27  
26  3.3e-05  6.3e-02  2.3e-03  9.96e-01   1.128509538e+01   1.137213324e+01   2.1e-08  1.28  
27  1.5e-05  6.3e-02  1.1e-03  9.99e-01   1.132163636e+01   1.136210149e+01   9.6e-09  1.30  
28  7.4e-06  6.0e-02  5.2e-04  1.00e+00   1.133790565e+01   1.135773320e+01   4.7e-09  1.31  
29  6.7e-06  5.4e-02  4.7e-04  1.00e+00   1.133973074e+01   1.135757724e+01   4.3e-09  1.32  
30  6.0e-06  5.0e-02  4.2e-04  1.00e+00   1.134107293e+01   1.135713509e+01   3.8e-09  1.34  
31  5.4e-06  4.5e-02  3.8e-04  1.00e+00   1.134228326e+01   1.135673956e+01   3.4e-09  1.35  
32  4.9e-06  4.2e-02  3.4e-04  1.00e+00   1.134337073e+01   1.135638167e+01   3.1e-09  1.37  
33  4.4e-06  3.8e-02  3.1e-04  1.00e+00   1.134434877e+01   1.135605884e+01   2.8e-09  1.38  
34  3.9e-06  3.5e-02  2.8e-04  1.00e+00   1.134522827e+01   1.135576752e+01   2.5e-09  1.39  
35  3.5e-06  3.2e-02  2.5e-04  1.00e+00   1.134601926e+01   1.135550473e+01   2.3e-09  1.40  
36  3.2e-06  3.0e-02  2.2e-04  1.00e+00   1.134673071e+01   1.135526775e+01   2.0e-09  1.41  
37  2.9e-06  2.7e-02  2.0e-04  1.00e+00   1.134737067e+01   1.135505410e+01   1.8e-09  1.42  
38  2.6e-06  2.5e-02  1.8e-04  1.00e+00   1.134794637e+01   1.135486157e+01   1.6e-09  1.44  
39  2.3e-06  2.4e-02  1.6e-04  1.00e+00   1.134846432e+01   1.135468807e+01   1.5e-09  1.45  
40  2.1e-06  2.2e-02  1.5e-04  1.00e+00   1.134893035e+01   1.135453178e+01   1.3e-09  1.47  
41  1.9e-06  2.0e-02  1.3e-04  1.00e+00   1.134934968e+01   1.135439104e+01   1.2e-09  1.48  
42  1.7e-06  1.9e-02  1.2e-04  1.00e+00   1.134972702e+01   1.135426430e+01   1.1e-09  1.49  
43  1.5e-06  1.8e-02  1.1e-04  1.00e+00   1.135006659e+01   1.135415019e+01   9.7e-10  1.50  
44  1.4e-06  1.7e-02  9.6e-05  1.00e+00   1.135037219e+01   1.135404743e+01   8.8e-10  1.51  
45  1.2e-06  1.6e-02  8.7e-05  1.00e+00   1.135064721e+01   1.135395497e+01   7.9e-10  1.52  
46  1.1e-06  1.5e-02  7.8e-05  1.00e+00   1.135089473e+01   1.135387173e+01   7.1e-10  1.53  
47  1.0e-06  1.4e-02  7.0e-05  1.00e+00   1.135111751e+01   1.135379681e+01   6.4e-10  1.55  
48  9.0e-07  1.3e-02  6.3e-05  1.00e+00   1.135131800e+01   1.135372940e+01   5.8e-10  1.56  
49  8.1e-07  1.3e-02  5.7e-05  1.00e+00   1.135149847e+01   1.135366872e+01   5.2e-10  1.58  
50  7.3e-07  1.2e-02  5.1e-05  1.00e+00   1.135166089e+01   1.135361411e+01   4.7e-10  1.59  
51  6.6e-07  1.2e-02  4.6e-05  1.00e+00   1.135180708e+01   1.135356498e+01   4.2e-10  1.60  
52  5.9e-07  1.1e-02  4.2e-05  1.00e+00   1.135193865e+01   1.135352076e+01   3.8e-10  1.61  
53  5.3e-07  1.1e-02  3.7e-05  1.00e+00   1.135205707e+01   1.135348098e+01   3.4e-10  1.62  
54  4.8e-07  1.0e-02  3.4e-05  1.00e+00   1.135216366e+01   1.135344516e+01   3.1e-10  1.63  
55  4.3e-07  1.0e-02  3.0e-05  1.00e+00   1.135225959e+01   1.135341293e+01   2.8e-10  1.65  
56  3.9e-07  9.8e-03  2.7e-05  1.00e+00   1.135234593e+01   1.135338392e+01   2.5e-10  1.66  
57  3.5e-07  9.5e-03  2.5e-05  1.00e+00   1.135242364e+01   1.135335783e+01   2.2e-10  1.67  
58  3.1e-07  9.3e-03  2.2e-05  1.00e+00   1.135249357e+01   1.135333433e+01   2.0e-10  1.68  
59  2.8e-07  9.0e-03  2.0e-05  1.00e+00   1.135255652e+01   1.135331319e+01   1.8e-10  1.69  
60  2.5e-07  8.8e-03  1.8e-05  1.00e+00   1.135261317e+01   1.135329418e+01   1.6e-10  1.70  
61  2.3e-07  8.7e-03  1.6e-05  1.00e+00   1.135266415e+01   1.135327706e+01   1.5e-10  1.72  
62  2.1e-07  8.5e-03  1.4e-05  9.99e-01   1.135271003e+01   1.135326167e+01   1.3e-10  1.73  
63  1.9e-07  8.3e-03  1.3e-05  1.00e+00   1.135275133e+01   1.135324778e+01   1.2e-10  1.75  
64  1.7e-07  8.2e-03  1.2e-05  1.00e+00   1.135278849e+01   1.135323530e+01   1.1e-10  1.76  
65  1.5e-07  8.1e-03  1.1e-05  9.99e-01   1.135282194e+01   1.135322408e+01   9.6e-11  1.78  
66  1.4e-07  8.0e-03  9.5e-06  1.00e+00   1.135285204e+01   1.135321397e+01   8.6e-11  1.79  
67  1.2e-07  7.9e-03  8.6e-06  1.00e+00   1.135287913e+01   1.135320487e+01   7.8e-11  1.80  
68  1.1e-07  7.8e-03  7.7e-06  9.98e-01   1.135290351e+01   1.135319670e+01   7.0e-11  1.82  
69  9.8e-08  7.7e-03  6.9e-06  9.98e-01   1.135292544e+01   1.135318934e+01   6.3e-11  1.83  
70  8.9e-08  7.6e-03  6.2e-06  9.98e-01   1.135294518e+01   1.135318272e+01   5.7e-11  1.85  
71  8.0e-08  7.6e-03  5.6e-06  1.00e+00   1.135296296e+01   1.135317674e+01   5.1e-11  1.86  
72  7.2e-08  7.5e-03  5.0e-06  1.00e+00   1.135297895e+01   1.135317135e+01   4.6e-11  1.87  
73  6.5e-08  7.5e-03  4.5e-06  1.00e+00   1.135299339e+01   1.135316648e+01   4.1e-11  1.88  
74  5.8e-08  7.4e-03  4.1e-06  9.98e-01   1.135300634e+01   1.135316213e+01   3.7e-11  1.89  
75  5.2e-08  7.4e-03  3.7e-06  1.00e+00   1.135301806e+01   1.135315818e+01   3.3e-11  1.90  
76  4.7e-08  6.7e-03  3.3e-06  1.01e+00   1.135302875e+01   1.135315455e+01   3.0e-11  1.92  
77  4.2e-08  6.0e-03  3.0e-06  9.99e-01   1.135303816e+01   1.135315139e+01   2.7e-11  1.93  
78  3.8e-08  5.4e-03  2.7e-06  1.00e+00   1.135304664e+01   1.135314853e+01   2.4e-11  1.95  
79  3.4e-08  4.8e-03  2.4e-06  1.00e+00   1.135305438e+01   1.135314591e+01   2.2e-11  1.96  
80  3.1e-08  4.4e-03  2.2e-06  1.00e+00   1.135306124e+01   1.135314360e+01   2.0e-11  1.97  
81  2.8e-08  3.9e-03  2.0e-06  1.01e+00   1.135306756e+01   1.135314145e+01   1.8e-11  1.99  
82  2.5e-08  3.5e-03  1.8e-06  1.02e+00   1.135307348e+01   1.135313942e+01   1.6e-11  2.00  
83  2.3e-08  3.2e-03  1.6e-06  1.01e+00   1.135307852e+01   1.135313772e+01   1.5e-11  2.01  
84  2.0e-08  2.9e-03  1.4e-06  1.00e+00   1.135308295e+01   1.135313623e+01   1.3e-11  2.02  
85  1.8e-08  2.6e-03  1.3e-06  9.95e-01   1.135308694e+01   1.135313490e+01   1.2e-11  2.03  
86  1.6e-08  2.3e-03  1.2e-06  9.92e-01   1.135309053e+01   1.135313371e+01   1.1e-11  2.04  
87  1.5e-08  2.1e-03  1.0e-06  9.97e-01   1.135309376e+01   1.135313263e+01   9.6e-12  2.06  
88  1.3e-08  1.9e-03  9.4e-07  9.95e-01   1.135309666e+01   1.135313166e+01   8.7e-12  2.07  
89  1.2e-08  1.7e-03  8.4e-07  9.90e-01   1.135309928e+01   1.135313079e+01   7.8e-12  2.08  
90  1.1e-08  1.5e-03  7.6e-07  1.00e+00   1.135310167e+01   1.135312998e+01   7.0e-12  2.09  
91  1.5e-09  1.6e-04  7.8e-08  1.00e+00   1.135312067e+01   1.135312357e+01   7.2e-13  2.11  
Interior-point optimizer terminated. Time: 2.11. 

Optimizer terminated. Time: 2.12    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1353120668e+01    Viol.  con: 2e-08    var: 0e+00  
  Dual.    obj: 1.1353123566e+01    Viol.  con: 0e+00    var: 1e-03  
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.13 seconds.
result packing took 9% of solve time
solution checking took 3.1% 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               : MACOSX/64-X86   
  Cores                  : 4               

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: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 4               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 830
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3579              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.02              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.02            
Factor     - nonzeros before factor : 1.67e+04          after factor           : 1.72e+05        
Factor     - dense dim.             : 0                 flops                  : 0.00e+00        
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+00        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.3e+05  0.00e+00   -1.288293936e+05  2.000000000e+00   1.0e+00  0.04  
1   1.1e+03  1.4e+03  6.0e+04  -9.71e-01  -1.265602742e+05  3.737386422e+00   4.7e-01  0.05  
2   3.8e+02  4.9e+02  2.1e+04  -9.35e-01  -1.193807297e+05  1.174272358e+01   1.7e-01  0.06  
3   2.8e+02  3.6e+02  1.6e+04  -8.23e-01  -1.156142604e+05  1.083125195e+02   1.2e-01  0.07  
4   2.8e+02  3.6e+02  1.5e+04  -7.56e-01  -1.122191743e+05  2.799924484e+03   1.2e-01  0.09  
5   7.6e+01  9.8e+01  4.2e+03  -7.45e-01  -7.374086532e+04  1.082386998e+04   3.4e-02  0.10  
6   3.6e+01  4.7e+01  2.0e+03  -1.89e-01  -4.564195121e+04  1.110466456e+04   1.6e-02  0.12  
7   2.0e+01  2.6e+01  1.1e+03  2.99e-01   -2.889299607e+04  7.167366862e+03   8.9e-03  0.13  
8   9.6e+00  1.2e+01  5.4e+02  6.01e-01   -1.507112367e+04  3.884705098e+03   4.3e-03  0.14  
9   4.4e+00  5.6e+00  2.4e+02  8.25e-01   -6.840633439e+03  2.132789045e+03   1.9e-03  0.16  
10  1.6e+00  2.1e+00  8.8e+01  9.39e-01   -2.330092031e+03  9.750495938e+02   7.0e-04  0.17  
11  1.1e+00  1.5e+00  6.4e+01  9.89e-01   -1.687039050e+03  7.037715592e+02   5.1e-04  0.19  
12  7.5e-01  9.9e-01  4.3e+01  9.84e-01   -1.140368806e+03  4.823395493e+02   3.4e-04  0.20  
13  6.0e-01  7.8e-01  3.4e+01  9.85e-01   -8.873098891e+02  3.932685934e+02   2.7e-04  0.22  
14  2.2e-01  2.9e-01  1.2e+01  9.88e-01   -3.281486920e+02  1.436250352e+02   1.0e-04  0.23  
15  9.0e-02  1.4e-01  5.2e+00  1.01e+00   -1.298113156e+02  6.747979686e+01   4.2e-05  0.24  
16  3.6e-02  9.9e-02  2.1e+00  1.00e+00   -4.860141645e+01  3.127973220e+01   1.7e-05  0.26  
17  2.9e-02  8.4e-02  1.7e+00  9.96e-01   -3.783016542e+01  2.775894185e+01   1.4e-05  0.27  
18  1.8e-02  6.6e-02  1.
----------------------------------------------------------------------
Ran 1 test in 36.036s

OK

Generating XML reports...
.1e+00  1.01e+00   -1.989153911e+01  2.054764919e+01   8.8e-06  0.28  
19  1.6e-02  5.9e-02  9.4e-01  1.02e+00   -1.599043755e+01  1.956741576e+01   7.7e-06  0.29  
20  5.8e-03  6.7e-02  3.4e-01  1.02e+00   1.488949433e+00   1.421994688e+01   2.8e-06  0.30  
21  2.0e-03  7.7e-02  1.2e-01  1.02e+00   7.927152545e+00   1.240190266e+01   1.0e-06  0.31  
22  1.4e-03  5.8e-02  8.7e-02  9.67e-01   8.833017509e+00   1.205662675e+01   7.5e-07  0.32  
23  4.9e-04  6.7e-02  3.2e-02  9.59e-01   1.037973175e+01   1.160986332e+01   2.9e-07  0.34  
24  2.0e-04  6.0e-02  1.3e-02  9.57e-01   1.091534648e+01   1.143360658e+01   1.2e-07  0.35  
25  1.8e-04  5.5e-02  1.2e-02  9.75e-01   1.095406697e+01   1.142030338e+01   1.1e-07  0.37  
26  1.6e-04  5.0e-02  1.1e-02  9.73e-01   1.098987277e+01   1.141004524e+01   9.8e-08  0.38  
27  1.5e-04  4.6e-02  9.8e-03  9.75e-01   1.102487759e+01   1.140360657e+01   8.8e-08  0.39  
28  1.3e-04  4.2e-02  8.8e-03  9.77e-01   1.105651918e+01   1.139787049e+01   7.9e-08  0.41  
29  1.2e-04  3.8e-02  7.9e-03  9.79e-01   1.108501156e+01   1.139264218e+01   7.1e-08  0.42  
30  1.1e-04  3.5e-02  7.2e-03  9.81e-01   1.111060678e+01   1.138781839e+01   6.4e-08  0.44  
31  9.5e-05  3.2e-02  6.4e-03  9.82e-01   1.113359020e+01   1.138336582e+01   5.8e-08  0.45  
32  8.6e-05  3.0e-02  5.8e-03  9.84e-01   1.115422155e+01   1.137925565e+01   5.2e-08  0.46  
33  7.7e-05  2.7e-02  5.2e-03  9.85e-01   1.117273714e+01   1.137546296e+01   4.7e-08  0.47  
34  6.9e-05  2.5e-02  4.7e-03  9.87e-01   1.118935080e+01   1.137196523e+01   4.2e-08  0.48  
35  6.3e-05  2.4e-02  4.2e-03  9.88e-01   1.120425581e+01   1.136874171e+01   3.8e-08  0.49  
36  5.6e-05  2.2e-02  3.8e-03  9.89e-01   1.121762700e+01   1.136577387e+01   3.4e-08  0.50  
37  5.1e-05  2.0e-02  3.4e-03  9.90e-01   1.122962178e+01   1.136304410e+01   3.1e-08  0.51  
38  4.6e-05  1.9e-02  3.1e-03  9.91e-01   1.124038194e+01   1.136053618e+01   2.8e-08  0.53  
39  4.1e-05  1.8e-02  2.8e-03  9.92e-01   1.125003472e+01   1.135823442e+01   2.5e-08  0.54  
40  3.7e-05  1.7e-02  2.5e-03  9.93e-01   1.125869434e+01   1.135612402e+01   2.3e-08  0.56  
41  3.3e-05  1.6e-02  2.2e-03  9.93e-01   1.126646331e+01   1.135419102e+01   2.0e-08  0.57  
42  3.0e-05  1.5e-02  2.0e-03  9.94e-01   1.127343343e+01   1.135242187e+01   1.8e-08  0.59  
43  2.7e-05  1.4e-02  1.8e-03  9.95e-01   1.127968749e+01   1.135080448e+01   1.6e-08  0.60  
44  2.4e-05  1.4e-02  1.6e-03  9.95e-01   1.128529972e+01   1.134932747e+01   1.5e-08  0.61  
45  2.2e-05  1.3e-02  1.5e-03  9.96e-01   1.129033683e+01   1.134798012e+01   1.3e-08  0.63  
46  2.0e-05  1.2e-02  1.3e-03  9.96e-01   1.129485863e+01   1.134675259e+01   1.2e-08  0.64  
47  1.8e-05  1.2e-02  1.2e-03  9.97e-01   1.129891852e+01   1.134563533e+01   1.1e-08  0.65  
48  1.6e-05  1.1e-02  1.1e-03  9.97e-01   1.130256429e+01   1.134461945e+01   9.7e-09  0.67  
49  1.4e-05  1.1e-02  9.7e-04  9.97e-01   1.130583869e+01   1.134369649e+01   8.7e-09  0.68  
50  1.3e-05  1.1e-02  8.7e-04  9.97e-01   1.130878004e+01   1.134285873e+01   7.9e-09  0.69  
51  1.2e-05  1.0e-02  7.8e-04  9.98e-01   1.131142257e+01   1.134209884e+01   7.1e-09  0.71  
52  1.0e-05  9.9e-03  7.1e-04  9.98e-01   1.131379699e+01   1.134141000e+01   6.4e-09  0.72  
53  9.4e-06  9.6e-03  6.4e-04  9.98e-01   1.131593078e+01   1.134078608e+01   5.7e-09  0.74  
54  8.4e-06  9.4e-03  5.7e-04  9.98e-01   1.131784851e+01   1.134022114e+01   5.2e-09  0.75  
55  7.6e-06  9.2e-03  5.2e-04  9.99e-01   1.131957223e+01   1.133970999e+01   4.6e-09  0.76  
56  6.8e-06  9.0e-03  4.6e-04  9.99e-01   1.132112168e+01   1.133924765e+01   4.2e-09  0.77  
57  6.2e-06  8.8e-03  4.2e-04  9.99e-01   1.132251456e+01   1.133882952e+01   3.8e-09  0.79  
58  5.5e-06  8.6e-03  3.8e-04  9.99e-01   1.132376678e+01   1.133845150e+01   3.4e-09  0.80  
59  5.0e-06  8.5e-03  3.4e-04  9.99e-01   1.132489256e+01   1.133810989e+01   3.0e-09  0.81  
60  4.5e-06  8.3e-03  3.0e-04  9.99e-01   1.132590473e+01   1.133780117e+01   2.7e-09  0.82  
61  4.0e-06  8.2e-03  2.7e-04  9.99e-01   1.132681477e+01   1.133752236e+01   2.5e-09  0.84  
62  3.6e-06  8.1e-03  2.5e-04  9.99e-01   1.132763307e+01   1.133727047e+01   2.2e-09  0.85  
63  3.3e-06  8.0e-03  2.2e-04  1.00e+00   1.132836895e+01   1.133704302e+01   2.0e-09  0.87  
64  2.9e-06  7.9e-03  2.0e-04  9.99e-01   1.132903073e+01   1.133683784e+01   1.8e-09  0.88  
65  2.7e-06  7.8e-03  1.8e-04  9.99e-01   1.132962595e+01   1.133665270e+01   1.6e-09  0.89  
66  2.4e-06  7.7e-03  1.6e-04  1.00e+00   1.133016137e+01   1.133648568e+01   1.5e-09  0.90  
67  2.1e-06  7.7e-03  1.5e-04  1.00e+00   1.133064304e+01   1.133633509e+01   1.3e-09  0.92  
68  1.9e-06  7.6e-03  1.3e-04  1.00e+00   1.133107636e+01   1.133619939e+01   1.2e-09  0.93  
69  1.7e-06  7.5e-03  1.2e-04  1.00e+00   1.133146624e+01   1.133607706e+01   1.1e-09  0.94  
70  1.6e-06  7.5e-03  1.1e-04  1.00e+00   1.133181702e+01   1.133596689e+01   9.6e-10  0.96  
71  1.4e-06  7.4e-03  9.5e-05  1.00e+00   1.133213267e+01   1.133586758e+01   8.6e-10  0.97  
72  1.3e-06  7.4e-03  8.6e-05  1.00e+00   1.133241669e+01   1.133577816e+01   7.8e-10  0.99  
73  1.1e-06  7.3e-03  7.7e-05  1.00e+00   1.133267226e+01   1.133569764e+01   7.0e-10  1.00  
74  1.0e-06  7.3e-03  7.0e-05  1.00e+00   1.133290224e+01   1.133562516e+01   6.3e-10  1.02  
75  9.2e-07  7.3e-03  6.3e-05  1.00e+00   1.133310919e+01   1.133555990e+01   5.7e-10  1.03  
76  8.3e-07  7.2e-03  5.6e-05  1.00e+00   1.133329542e+01   1.133550112e+01   5.1e-10  1.05  
77  7.5e-07  7.2e-03  5.1e-05  1.00e+00   1.133346303e+01   1.133544819e+01   4.6e-10  1.06  
78  6.7e-07  7.2e-03  4.6e-05  9.99e-01   1.133361384e+01   1.133540059e+01   4.1e-10  1.07  
79  6.1e-07  7.2e-03  4.1e-05  1.00e+00   1.133374957e+01   1.133535766e+01   3.7e-10  1.09  
80  5.5e-07  7.1e-03  3.7e-05  1.00e+00   1.133387173e+01   1.133531903e+01   3.3e-10  1.10  
81  4.9e-07  7.1e-03  3.3e-05  1.00e+00   1.133398167e+01   1.133528421e+01   3.0e-10  1.12  
82  4.4e-07  7.1e-03  3.0e-05  1.00e+00   1.133408060e+01   1.133525288e+01   2.7e-10  1.13  
83  4.0e-07  7.1e-03  2.7e-05  1.00e+00   1.133416964e+01   1.133522466e+01   2.4e-10  1.14  
84  3.6e-07  7.0e-03  2.4e-05  1.00e+00   1.133424976e+01   1.133519930e+01   2.2e-10  1.15  
85  3.2e-07  7.0e-03  2.2e-05  1.00e+00   1.133432187e+01   1.133517641e+01   2.0e-10  1.16  
86  2.9e-07  7.0e-03  2.0e-05  1.00e+00   1.133438676e+01   1.133515584e+01   1.8e-10  1.17  
87  2.6e-07  7.0e-03  1.8e-05  1.00e+00   1.133444516e+01   1.133513732e+01   1.6e-10  1.19  
88  2.3e-07  7.0e-03  1.6e-05  9.98e-01   1.133449770e+01   1.133512070e+01   1.4e-10  1.20  
89  2.1e-07  7.0e-03  1.4e-05  1.00e+00   1.133454499e+01   1.133510569e+01   1.3e-10  1.22  
90  1.9e-07  7.0e-03  1.3e-05  1.00e+00   1.133458755e+01   1.133509218e+01   1.2e-10  1.23  
91  1.7e-07  6.9e-03  1.2e-05  9.98e-01   1.133462584e+01   1.133508006e+01   1.0e-10  1.25  
92  1.5e-07  6.9e-03  1.0e-05  1.00e+00   1.133466031e+01   1.133506910e+01   9.4e-11  1.26  
93  1.4e-07  6.2e-03  9.4e-06  1.00e+00   1.133469145e+01   1.133505917e+01   8.5e-11  1.28  
94  1.2e-07  5.6e-03  8.5e-06  1.00e+00   1.133471948e+01   1.133505023e+01   7.6e-11  1.29  
95  1.1e-07  5.1e-03  7.6e-06  1.00e+00   1.133474458e+01   1.133504225e+01   6.9e-11  1.31  
96  1.0e-07  4.6e-03  6.9e-06  9.99e-01   1.133476716e+01   1.133503508e+01   6.2e-11  1.32  
97  9.1e-08  4.1e-03  6.2e-06  1.01e+00   1.133478800e+01   1.133502839e+01   5.6e-11  1.33  
98  8.2e-08  3.7e-03  5.6e-06  1.00e+00   1.133480624e+01   1.133502260e+01   5.0e-11  1.34  
99  7.4e-08  3.3e-03  5.0e-06  1.00e+00   1.133482284e+01   1.133501730e+01   4.5e-11  1.36  
100 6.6e-08  3.0e-03  4.5e-06  9.92e-01   1.133483758e+01   1.133501266e+01   4.1e-11  1.37  
101 6.0e-08  2.7e-03  4.0e-06  1.00e+00   1.133485100e+01   1.133500837e+01   3.7e-11  1.38  
102 5.4e-08  2.4e-03  3.6e-06  1.01e+00   1.133486353e+01   1.133500431e+01   3.3e-11  1.39  
103 4.8e-08  2.2e-03  3.3e-06  1.01e+00   1.133487449e+01   1.133500080e+01   3.0e-11  1.41  
104 4.4e-08  2.0e-03  3.0e-06  9.92e-01   1.133488407e+01   1.133499779e+01   2.7e-11  1.42  
105 3.9e-08  1.8e-03  2.7e-06  1.00e+00   1.133489282e+01   1.133499499e+01   2.4e-11  1.43  
106 3.5e-08  1.6e-03  2.4e-06  1.01e+00   1.133490075e+01   1.133499245e+01   2.2e-11  1.44  
107 3.2e-08  1.4e-03  2.2e-06  1.03e+00   1.133490852e+01   1.133498990e+01   2.0e-11  1.46  
108 2.9e-08  1.3e-03  1.9e-06  9.99e-01   1.133491470e+01   1.133498795e+01   1.8e-11  1.47  
109 2.6e-08  1.2e-03  1.7e-06  9.96e-01   1.133492026e+01   1.133498620e+01   1.6e-11  1.48  
110 2.3e-08  1.0e-03  1.6e-06  1.01e+00   1.133492548e+01   1.133498452e+01   1.5e-11  1.50  
111 4.6e-09  2.0e-04  3.0e-07  9.87e-01   1.133496185e+01   1.133497318e+01   2.9e-12  1.51  
112 3.6e-10  1.1e-05  1.7e-08  9.99e-01   1.133496984e+01   1.133497047e+01   1.6e-13  1.53  
Interior-point optimizer terminated. Time: 1.53. 

Optimizer terminated. Time: 1.54    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1334969841e+01    Viol.  con: 5e-09    var: 0e+00  
  Dual.    obj: 1.1334970467e+01    Viol.  con: 0e+00    var: 8e-05  
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.55 seconds.
result packing took 14% of solve time
solution checking took 3.4% of solve time
Solving took 6 GP solves and 30.6 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 2418945.80592 force_pound * meter but the right hand side evaluated to 2375461.08698 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 32774.3852942 force_pound but the right hand side evaluated to 32399.999998 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 2.21510116796 meter but the right hand side evaluated to 2.08160421131 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 1243581.56278 joule / kilogram but the right hand side evaluated to 1.56114554119 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 664761.16197 joule / kilogram but the right hand side evaluated to 0.667339833905 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 18.3998918073 meter but the right hand side evaluated to 16.3228929556 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 10.903626367393652 but the right hand side evaluated to 4.788858789234022 (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 10.019807080710393 but the right hand side evaluated to 4.788858780375711 (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 8.144911164730637 but the right hand side evaluated to 4.788858791383541 (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 18.3622360691 meter but the right hand side evaluated to 18.1377248385 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 18.3622360691 meter but the right hand side evaluated to 18.2420610992 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 0.2960343953111906 but the right hand side evaluated to 0.18973867009634293 (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 0.2330206484835573 but the right hand side evaluated to 0.17434658828377772 (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 7.563249143929341 but the right hand side evaluated to 4.730639770186216 (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 7.583097166948614 but the right hand side evaluated to 4.757852514285048 (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

Cloning into 'solar'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0)
Collecting git+https://github.com/convexengineering/gpfit.git
  Cloning https://github.com/convexengineering/gpfit.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-1WmhCX
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-hZzYfo/wheels/d5/94/ac/b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
Collecting git+https://github.com/convexengineering/gassolar.git
  Cloning https://github.com/convexengineering/gassolar.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-hr608x
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2018.4)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.7.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-jz7Hre/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/solar
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in /Users/jenkins/workspace/gplibrary_PR_Models/mosek (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2018.4)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2.7.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-Xt8ZYd/wheels/1f/1c/61/aec93436439dcd4a965e159a026d3a7ed265e591b64e6d6bfc
Successfully built solar
Installing collected packages: solar
Successfully installed solar-0.0.0.0

Running tests...
----------------------------------------------------------------------
../Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
  tau = np.exp(-0.175/costhsun)
....EE
======================================================================
ERROR [6.305s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "/Users/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 "/Users/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 "/Users/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 "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 83, in __init__
    CostedConstraintSet.__init__(self, cost, constraints, substitutions)
  File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/costed.py", line 21, in __init__
    ConstraintSet.__init__(self, constraints, subs)
  File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 58, in __init__
    list.__setitem__(self, i, ConstraintSet(constraint))
  File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 67, in __init__
    raise_elementhasnumpybools(constraint)
  File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 357, in raise_elementhasnumpybools
    % (cause, constraint))
ValueError: An ArrayConstraint was created with elements of numpy.bool_
Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]

======================================================================
ERROR [7.505s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "/Users/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 "/Users/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 "/Users/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 "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 83, in __init__
    CostedConstraintSet.__init__(self, cost, constraints, substitutions)
  File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/costed.py", line 21, in __init__
    ConstraintSet.__init__(self, constraints, subs)
  File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 58, in __init__
    list.__setitem__(self, i, ConstraintSet(constraint))
  File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 67, in __init__
    raise_elementhasnumpybools(constraint)
  File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 357, in raise_elementhasnumpybools
    % (cause, constraint))
ValueError: An ArrayConstraint was created with elements of numpy.bool_
Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]

----------------------------------------------------------------------
Ran 8 tests in 232.949s

FAILED (errors=2)

Generating XML reports...
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 3.45 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 1372945.2542 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 2.11826075487 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781339 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 3.32 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 1372945.2687 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 2.1182607549 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781343 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 1.63010986522 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010574807 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 0.911985264136 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983814521 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)

Using solver 'mosek'
Solving for 12129 variables.
Solving took 1.99 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 720429.8178 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.17 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 791679.4793 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.35 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 883741.3414 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 0.684 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 2.12 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 720429.8155 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.1 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 791679.4705 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.08 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 883741.3294 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 0.71 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 933393.0311 but bound is 600000.0000
Beginning signomial solve.
Solving took 10 GP solves and 3.43 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 1372945.2522 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 2.11826075486 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781339 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 2.68 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 1372945.2729 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 2.11826075492 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 1.63010986522 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%)

Using solver 'mosek'
Solving for 702 variables.
Solving took 0.0921 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 3.1 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 1002038.7317 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%)

Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Using solver 'mosek_cli'
Solving for 702 variables.
Solving took 0.279 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 4.12 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%)

Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0)
Collecting git+https://github.com/hoburg/gpfit.git
  Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-rxWMY7
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-Hp78xo/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gplibrary
Requirement already satisfied: numpy>=1.12 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/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: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-ZO6TR5/wheels/89/83/63/5c5e519ca7ad1fa93cf087f53642d88b5b0eb066ca83d4bb19
Successfully built gpkitmodels
Installing collected packages: gpkitmodels
  Found existing installation: gpkitmodels 0.0.0.0
    Uninstalling gpkitmodels-0.0.0.0:
      Successfully uninstalled gpkitmodels-0.0.0.0
Successfully installed gpkitmodels-0.0.0.0

Running tests...
----------------------------------------------------------------------
..........
----------------------------------------------------------------------
Ran 10 tests in 16.733s

OK

Generating XML reports...
adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py'
adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py'
adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py'
adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py'
adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.013 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.227 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.0107 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0101 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.012 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 1.47 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 985.544371525 meter * revolutions_per_minute but the right hand side evaluated to 103.041409431 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 0.420585924989 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573144929 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 0.314645033962 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629895199 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 0.168936438407 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931603972 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 0.0639631379985 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 0.0226356535431 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354005879 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)

Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.232 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.283 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.226 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 4.9 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 0.420585895021 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 0.0114 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 0.945 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 1619897.4157 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.237 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 3.33 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
Cloning into 'eVTOL'...

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 1.360s

OK

Generating XML reports...
adding test for 'aircraft_models.py'
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/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 ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
  attempt 1

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

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
  attempt 1

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

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
  attempt 1

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

calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/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 ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/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 ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
  attempt 1

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

[Execution node] check if [macys_VM] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
Build step 'Console output (build log) parsing' changed build result to FAILURE
[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 '/Users/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