Skipping 28 KB..
Full LogRequirement already satisfied: pint in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1)
Installing collected packages: gpfit
Running setup.py install for gpfit: started
Running setup.py install for gpfit: finished with status 'done'
Successfully installed gpfit-0.1
Running tests...
----------------------------------------------------------------------
...adding test for 'model/jho.py'
adding test for 'model/print_perf.py'
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.48438464781e-13.
Allowing negative dual variable(s) as small as -3.36647810323e-13.
Allowing negative dual variable(s) as small as -5.21676452037e-13.
Allowing negative dual variable(s) as small as -5.4175544259e-13.
Solving took 4 GP solves and 2.86 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.48687831281e-13.
Allowing negative dual variable(s) as small as -3.37023811636e-13.
Allowing negative dual variable(s) as small as -5.45741837138e-13.
Allowing negative dual variable(s) as small as -5.36242057703e-13.
Solving took 4 GP solves and 2.64 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000
Allowing negative dual variable(s) as small as -8.57188452164e-13.
Allowing negative dual variable(s) as small as -7.72677928584e-13.
Allowing negative dual variable(s) as small as -7.38573265047e-13.
Allowing negative dual variable(s) as small as -7.40963713997e-13.
Allowing negative dual variable(s) as small as -7.41205707921e-13.
Allowing negative dual variable(s) as small as -1.5210369856e-12.
Allowing negative dual variable(s) as small as -1.04771649256e-12.
Allowing negative dual variable(s) as small as -1.06172915511e-12.
Allowing negative dual variable(s) as small as -1.06049956143e-12.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
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 = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -1.48838558665e-12.
Allowing negative dual variable(s) as small as -1.14066742163e-13.
Allowing negative dual variable(s) as small as -6.93737602087e-15.
Allowing negative dual variable(s) as small as -1.62405570762e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.50673062453e-14.
Allowing negative dual variable(s) as small as -1.0810979109e-12.
Solving took 4 GP solves and 2.55 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Solving took 4 GP solves and 1.74 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.56776455338e-13.
Allowing negative dual variable(s) as small as -7.72753389056e-13.
Allowing negative dual variable(s) as small as -7.38518621257e-13.
Allowing negative dual variable(s) as small as -7.41347955246e-13.
Allowing negative dual variable(s) as small as -7.41762554157e-13.
Allowing negative dual variable(s) as small as -1.52109770092e-12.
Allowing negative dual variable(s) as small as -1.04905320542e-12.
Allowing negative dual variable(s) as small as -1.061081778e-12.
Allowing negative dual variable(s) as small as -1.06327631162e-12.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
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 = 21.769
speed at top of climb [m/s] = 26.550
design .
----------------------------------------------------------------------
Ran 4 tests in 54.866s
OK
Generating XML reports...
loiter speed [m/s] = 25.056
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -1.48049996741e-12.
Allowing negative dual variable(s) as small as -1.13952250413e-13.
Allowing negative dual variable(s) as small as -6.2141047516e-15.
Allowing negative dual variable(s) as small as -1.60776340158e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.49241646652e-14.
Allowing negative dual variable(s) as small as -1.08101979286e-12.
Solving took 4 GP solves and 2.26 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Solving took 4 GP solves and 1.91 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Cloning into 'turbofan'...
Cannot uninstall requirement turbofan, not installed
Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/turbofan
Installing collected packages: turbofan
Running setup.py develop for turbofan
Successfully installed turbofan
From https://github.com/convexengineering/gpkit-models
* branch master -> FETCH_HEAD
HEAD is now at 11cee6a... ipynb2module is a tool for importing jupyter notebooks as modules (#116)
Cannot uninstall requirement gpkit-models, not installed
Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit-models
Installing collected packages: gpkitmodels
Found existing installation: gpkitmodels 0.0.0.0
Uninstalling gpkitmodels-0.0.0.0:
Successfully uninstalled gpkitmodels-0.0.0.0
Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels
Running tests...
----------------------------------------------------------------------
adding test for 'turbofan/engine_validation.py'
adding test for 'turbofan/engine_flight_profile_fleet.py'
T_{t_{4.1_{max}}}_FleetMission/Aircraft/Engine has no upper bound
Beginning signomial solve.
Using solver 'mosek'
Solving for 2480 variables.
Warning: The variable with index '1860' has only negative coefficients akj.
The problem is possibly ill-posed.
Number of Hessian non-zeros: 1090
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Linux/64-X86
Cores : 20
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2481
Cones : 0
Scalar variables : 5898
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 : 987
Eliminator terminated.
Eliminator started.
Total number of eliminations : 990
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 990
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.02
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 329
Optimizer - Cones : 0
Optimizer - Scalar variables : 1038 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.07 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 6388 after factor : 1.11e+04
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 1.2e+03 1.8e+04 2.1e+04 0.00e+00 -2.068680080e+04 1.023181539e-12 1.0e+00 0.10
1 9.0e+02 1.3e+04 1.5e+04 -1.09e-01 -1.772348494e+04 2.815948399e+00 7.3e-01 0.10
2 3.6e+02 5.2e+03 6.0e+03 4.01e-02 -1.101707996e+04 1.002502274e+01 3.0e-01 0.11
3 1.9e+02 2.7e+03 3.1e+03 6.47e-01 -5.771848537e+03 1.375651253e+01 1.7e-01 0.11
4 5.8e+01 8.4e+02 9.8e+02 1.20e+00 -1.605083557e+03 1.625562900e+01 5.7e-02 0.12
5 3.1e+01 4.5e+02 5.2e+02 1.69e+00 -6.744957596e+02 1.621109351e+01 3.1e-02 0.12
6 1.0e+01 1.4e+02 1.7e+02 1.50e+00 -1.671041152e+02 1.570774188e+01 1.0e-02 0.13
7 4.4e+00 6.5e+01 7.4e+01 1.15e+00 -6.553353096e+01 1.497839963e+01 4.8e-03 0.13
8 2.1e+00 3.2e+01 3.6e+01 8.76e-01 -3.007490357e+01 1.440760135e+01 2.4e-03 0.13
9 9.9e-01 1.8e+01 1.7e+01 5.55e-01 -1.319615757e+01 1.384697541e+01 1.2e-03 0.14
10 3.3e-01 6.3e+00 5.6e+00 5.48e-01 1.823505446e+00 1.321184723e+01 4.6e-04 0.14
11 1.5e-01 3.2e+00 2.6e+00 6.35e-01 7.019670079e+00 1.295306976e+01 2.2e-04 0.14
12 9.8e-02 2.5e+00 1.7e+00 7.48e-01 8.809147105e+00 1.282119834e+01 1.4e-04 0.15
13 2.3e-02 1.5e+00 4.1e-01 8.18e-01 1.155758190e+01 1.259122520e+01 4.1e-05 0.15
14 7.4e-03 1.5e+00 1.3e-01 9.41e-01 1.219964259e+01 1.254374830e+01 1.5e-05 0.16
15 2.0e-03 1.5e+00 3.7e-02 9.82e-01 1.242499856e+01 1.252083344e+01 4.4e-06 0.16
16 6.0e-04 1.3e+00 1.1e-02 9.88e-01 1.248690054e+01 1.251546983e+01 1.3e-06 0.16
17 2.4e-04 1.0e+00 4.4e-03 9.73e-01 1.250287189e+01 1.251430060e+01 5.4e-07 0.17
18 2.1e-04 9.6e-01 3.9e-03 9.97e-01 1.250392961e+01 1.251421138e+01 4.8e-07 0.17
19 1.9e-04 8.7e-01 3.5e-03 9.64e-01 1.250487597e+01 1.251414608e+01 4.3e-07 0.18
20 1.7e-04 7.9e-01 3.2e-03 9.53e-01 1.250573845e+01 1.251408313e+01 3.9e-07 0.18
21 1.6e-04 7.2e-01 2.9e-03 9.77e-01 1.250650025e+01 1.251403234e+01 3.5e-07 0.18
22 1.4e-04 6.6e-01 2.6e-03 9.93e-01 1.250722003e+01 1.251397784e+01 3.2e-07 0.18
23 1.3e-04 6.0e-01 2.3e-03 1.01e+00 1.250788831e+01 1.251392919e+01 2.9e-07 0.19
24 1.1e-04 5.6e-01 2.1e-03 1.01e+00 1.250848792e+01 1.251388456e+01 2.6e-07 0.19
25 1.0e-04 5.1e-01 1.9e-03 9.86e-01 1.250900262e+01 1.251384654e+01 2.3e-07 0.19
26 9.2e-05 4.7e-01 1.7e-03 9.33e-01 1.250945688e+01 1.251381457e+01 2.1e-07 0.20
27 8.3e-05 4.3e-01 1.5e-03 1.02e+00 1.250989671e+01 1.251378450e+01 1.9e-07 0.20
28 7.4e-05 4.0e-01 1.4e-03 9.03e-01 1.251025679e+01 1.251375991e+01 1.7e-07 0.20
29 6.7e-05 3.8e-01 1.2e-03 1.08e+00 1.251071500e+01 1.251372793e+01 1.6e-07 0.21
30 6.0e-05 3.6e-01 1.1e-03 1.05e+00 1.251105277e+01 1.251370690e+01 1.5e-07 0.21
31 5.4e-05 3.5e-01 1.0e-03 1.10e+00 1.251142509e+01 1.251367888e+01 1.4e-07 0.21
32 4.9e-05 3.3e-01 9.0e-04 9.51e-01 1.251165685e+01 1.251365988e+01 1.2e-07 0.22
33 4.4e-05 3.1e-01 8.1e-04 7.94e-01 1.251184649e+01 1.251364760e+01 1.1e-07 0.22
34 3.9e-05 3.0e-01 7.3e-04 1.39e+00 1.251203774e+01 1.251363260e+01 1.0e-07 0.23
35 3.5e-05 2.7e-01 6.6e-04 1.08e+00 1.251225782e+01 1.251361731e+01 9.4e-08 0.23
36 3.2e-05 2.5e-01 5.9e-04 7.69e-01 1.251239514e+01 1.251360767e+01 8.4e-08 0.23
37 2.9e-05 2.4e-01 5.3e-04 9.15e-01 1.251249695e+01 1.251360460e+01 7.6e-08 0.23
38 2.6e-05 2.3e-01 4.8e-04 1.21e+00 1.251261263e+01 1.251359640e+01 6.8e-08 0.24
39 2.3e-05 2.2e-01 4.3e-04 8.42e-01 1.251269976e+01 1.251359265e+01 6.2e-08 0.24
40 2.1e-05 2.0e-01 3.9e-04 9.92e-01 1.251277757e+01 1.251358970e+01 5.5e-08 0.25
41 1.9e-05 1.9e-01 3.5e-04 7.91e-01 1.251285094e+01 1.251358594e+01 5.0e-08 0.25
42 1.7e-05 1.7e-01 3.1e-04 1.15e+00 1.251295862e+01 1.251358119e+01 4.8e-08 0.25
43 6.4e-06 6.3e-02 1.2e-04 4.33e-01 1.251332175e+01 1.251356347e+01 1.9e-08 0.26
44 5.8e-06 5.7e-02 1.0e-04 -3.62e-01 1.251333666e+01 1.251356376e+01 1.7e-08 0.26
45 5.3e-06 5.1e-02 9.4e-05 1.17e+00 1.251337448e+01 1.251356046e+01 1.7e-08 0.27
46 1.5e-06 1.1e-02 2.1e-05 4.96e-01 1.251350849e+01 1.251354902e+01 3.5e-09 0.27
47 1.3e-06 1.0e-02 1.5e-05 1.00e+00 1.251351901e+01 1.251354880e+01 3.1e-09 0.27
48 2.2e-06 7.7e-03 1.2e-05 6.00e-01 1.251352968e+01 1.251354675e+01 1.8e-09 0.28
49 7.7e-07 8.3e-04 1.2e-06 3.02e-01 1.251354473e+01 1.251354671e+01 3.0e-10 0.28
50 3.8e-06 1.8e-04 2.7e-07 1.11e+00 1.251354620e+01 1.251354657e+01 4.4e-11 0.28
Interior-point optimizer terminated. Time: 0.29.
Optimizer terminated. Time: 0.31
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.2513546199e+01 Viol. con: 5e-06 var: 0e+00
Dual. obj: 1.2513546574e+01 Viol. con: 0e+00 var: 5e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.336 seconds.
result packing took 48% of solve time
solution checking took 20% of solve time
Using solver 'mosek'
Solving for 2480 variables.
Warning: The variable with index '1860' has only negative coefficients akj.
The problem is possibly ill-posed.
Number of Hessian non-zeros: 1090
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Linux/64-X86
Cores : 20
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2481
Cones : 0
Scalar variables : 5898
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 : 1029
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1046
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1046
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.03
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 283
Optimizer - Cones : 0
Optimizer - Scalar variables : 992 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 : 6516 after factor : 1.06e+04
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 3.8e+03 7.6e+03 0.00e+00 -7.644378007e+03 1.023181539e-12 1.0e+00 0.05
1 7.5e+02 1.2e+03 2.5e+03 9.80e-02 -3.407479634e+03 9.786322642e+00 3.5e-01 0.05
2 3.9e+02 6.4e+02 1.3e+03 1.32e+00 -1.482253519e+03 1.282296477e+01 1.9e-01 0.06
3 2.8e+02 4.6e+02 9.5e+02 1.54e+00 -9.489273590e+02 1.334846972e+01 1.4e-01 0.06
4 8.5e+01 1.4e+02 2.9e+02 1.50e+00 -2.206854375e+02 1.377114285e+01 4.5e-02 0.06
5 2.7e+01 4.7e+01 9.4e+01 1.38e+00 -5.391135377e+01 1.255157258e+01 1.5e-02 0.07
6 7.2e+00 1.8e+01 2.5e+01 1.15e+00 -5.357648476e+00 1.118504506e+01 4.6e-03 0.07
7 1.9e+00 1.3e+01 6.8e+00 1.04e+00 6.211185702e+00 1.065374608e+01 1.4e-03 0.07
8 1.8e+00 1.2e+01 6.3e+00 8.06e-01 6.408078736e+00 1.064029136e+01 1.3e-03 0.08
9 8.0e-01 1.2e+01 2.8e+00 7.51e-01 8.166288108e+00 1.051014155e+01 6.0e-04 0.08
10 6.7e-01 9.7e+00 2.3e+00 3.05e-01 8.319320138e+00 1.048321242e+01 5.1e-04 0.08
11 2.1e-01 3.5e+00 7.8e-01 3.97e-01 9.318878173e+00 1.033893707e+01 2.0e-04 0.09
12 5.1e-02 3.6e+00 1.9e-01 7.03e-01 9.955769900e+00 1.024572827e+01 5.8e-05 0.09
13 1.6e-02 3.3e+00 6.2e-02 9.10e-01 1.012192736e+01 1.021849667e+01 2.0e-05 0.09
14 6.8e-03 2.6e+00 2.7e-02 9.70e-01 1.016844964e+01 1.021016410e+01 8.6e-06 0.10
15 3.1e-03 2.2e+00 1.2e-02 9.87e-01 1.018781568e+01 1.020660642e+01 3.9e-06 0.10
16 1.4e-03 2.0e+00 5.4e-03 9.94e-01 1.019655562e+01 1.020501175e+01 1.7e-06 0.10
17 5.1e-04 7.6e-01 2.0e-03 9.98e-01 1.020101422e+01 1.020419675e+01 6.6e-07 0.11
18 4.6e-04 6.9e-01 1.8e-03 9.99e-01 1.020130748e+01 1.020417908e+01 5.9e-07 0.11
19 4.2e-04 6.3e-01 1.6e-03 9.99e-01 1.020154363e+01 1.020412891e+01 5.3e-07 0.11
20 1.6e-04 2.5e-01 6.4e-04 9.99e-01 1.020285734e+01 1.020387196e+01 2.1e-07 0.12
21 1.5e-04 2.4e-01 5.8e-04 9.99e-01 1.020294093e+01 1.020385412e+01 1.9e-07 0.12
22 5.6e-05 9.0e-02 2.2e-04 9.99e-01 1.020341703e+01 1.020376372e+01 7.2e-08 0.12
23 5.0e-05 8.1e-02 2.0e-04 1.00e+00 1.020344562e+01 1.020375764e+01 6.4e-08 0.13
24 4.5e-05 7.3e-02 1.8e-04 1.00e+00 1.020347188e+01 1.020375271e+01 5.8e-08 0.13
25 4.1e-05 6.5e-02 1.6e-04 1.00e+00 1.020349552e+01 1.020374827e+01 5.2e-08 0.13
26 3.7e-05 5.9e-02 1.4e-04 1.00e+00 1.020351681e+01 1.020374428e+01 4.7e-08 0.13
27 3.3e-05 5.3e-02 1.3e-04 1.00e+00 1.020353597e+01 1.020374070e+01 4.2e-08 0.14
28 3.0e-05 4.8e-02 1.2e-04 1.00e+00 1.020355322e+01 1.020373748e+01 3.8e-08 0.14
29 2.7e-05 4.3e-02 1.1e-04 1.00e+00 1.020356875e+01 1.020373459e+01 3.4e-08 0.14
30 2.4e-05 3.9e-02 9.5e-05 1.00e+00 1.020358273e+01 1.020373199e+01 3.1e-08 0.14
31 2.2e-05 3.5e-02 8.5e-05 1.00e+00 1.020359532e+01 1.020372965e+01 2.8e-08 0.15
32 1.9e-05 3.1e-02 7.7e-05 1.00e+00 1.020360665e+01 1.020372755e+01 2.5e-08 0.15
33 3.9e-06 6.2e-03 1.5e-05 1.00e+00 1.020368849e+01 1.020371250e+01 5.0e-09 0.15
34 2.2e-07 3.5e-04 8.6e-07 1.00e+00 1.020370762e+01 1.020370897e+01 2.8e-10 0.16
35 1.4e-09 2.3e-06 6.0e-09 9.97e-01 1.020370875e+01 1.020370876e+01 2.4e-12 0.16
Interior-point optimizer terminated. Time: 0.16.
Optimizer terminated. Time: 0.19
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0203708750e+01 Viol. con: 2e-09 var: 0e+00
Dual. obj: 1.0203708760e+01 Viol. con: 0e+00 var: 7e-07
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.217 seconds.
result packing took 51% of solve time
solution checking took 21% of solve time
Using solver 'mosek'
Solving for 2480 variables.
Warning: The variable with index '1860' has only negative coefficients akj.
The problem is possibly ill-posed.
Number of Hessian non-zeros: 1090
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Linux/64-X86
Cores : 20
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2481
Cones : 0
Scalar variables : 5898
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 : 1026
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1041
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1041
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 : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 286
Optimizer - Cones : 0
Optimizer - Scalar variables : 995 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.01 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 6535 after factor : 1.08e+04
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 2.7e+03 3.8e+03 5.3e+03 0.00e+00 -5.250824815e+03 1.023181539e-12 1.0e+00 0.03
1 8.6e+02 1.2e+03 1.7e+03 6.90e-03 -2.364177425e+03 9.864732565e+00 3.4e-01 0.03
2 3.9e+02 5.3e+02 7.7e+02 1.39e+00 -8.737396701e+02 1.336734353e+01 1.6e-01 0.04
3 3.6e+02 4.9e+02 7.0e+02 1.66e+00 -7.541381937e+02 1.344006533e+01 1.5e-01 0.04
4 1.5e+02 2.1e+02 3.1e+02 1.62e+00 -2.491413788e+02 1.390019128e+01 6.8e-02 0.04
5 4.0e+01 5.7e+01 8.0e+01 1.47e+00 -4.387236879e+01 1.303970155e+01 1.9e-02 0.04
6 1.0e+01 1.9e+01 2.1e+01 1.13e+00 -2.532000744e+00 1.139381582e+01 5.4e-03 0.05
7 5.3e+00 1.0e+01 1.1e+01 9.94e-01 3.610852388e+00 1.099016923e+01 2.9e-03 0.05
8 2.1e+00 1.1e+01 4.4e+00 9.83e-01 7.608082312e+00 1.068251922e+01 1.3e-03 0.05
9 1.9e+00 9.8e+00 4.0e+00 6.81e-01 7.721680870e+00 1.066293893e+01 1.1e-03 0.05
10 1.8e+00 9.1e+00 3.8e+00 6.28e-01 7.517085457e+00 1.065829136e+01 1.1e-03 0.06
11 5.6e-01 7.7e+00 1.2e+00 6.30e-01 9.159151967e+00 1.044591249e+01 3.8e-04 0.06
12 4.2e-01 7.7e+00 9.0e-01 4.74e-01 9.324301741e+00 1.040423620e+01 2.9e-04 0.06
13 9.2e-02 3.4e+00 2.1e-01 5.40e-01 9.935055002e+00 1.025973229e+01 8.5e-05 0.07
14 2.6e-02 3.0e+00 6.2e-02 8.67e-01 1.011305926e+01 1.021259564e+01 2.7e-05 0.07
15 8.4e-03 2.9e+00 2.1e-02 9.67e-01 1.016487364e+01 1.019839659e+01 9.2e-06 0.07
16 3.0e-03 2.7e+00 7.6e-03 9.91e-01 1.018148455e+01 1.019384059e+01 3.4e-06 0.07
17 1.3e-03 2.2e+00 3.2e-03 9.97e-01 1.018700480e+01 1.019224403e+01 1.5e-06 0.08
18 5.9e-04 1.9e+00 1.5e-03 9.98e-01 1.018921165e+01 1.019161182e+01 6.7e-07 0.08
19 2.7e-04 1.8e+00 6.7e-04 9.98e-01 1.019022844e+01 1.019132550e+01 3.1e-07 0.08
20 1.2e-04 1.7e+00 3.0e-04 9.93e-01 1.019070147e+01 1.019119435e+01 1.4e-07 0.09
21 1.1e-04 1.6e+00 2.7e-04 8.67e-01 1.019070821e+01 1.019123212e+01 1.2e-07 0.09
22 1.0e-04 1.6e+00 2.6e-04 9.28e-01 1.019074948e+01 1.019120316e+01 1.2e-07 0.09
23 7.7e-05 1.2e+00 1.9e-04 7.64e-01 1.019083550e+01 1.019121701e+01 8.9e-08 0.09
24 3.8e-05 5.7e-01 9.6e-05 9.93e-01 1.019099458e+01 1.019118193e+01 4.4e-08 0.10
25 3.4e-05 5.5e-01 8.6e-05 9.94e-01 1.019100635e+01 1.019117506e+01 3.9e-08 0.10
26 3.1e-05 5.1e-01 7.7e-05 9.91e-01 1.019102065e+01 1.019117238e+01 3.5e-08 0.10
27 2.8e-05 4.7e-01 7.0e-05 9.89e-01 1.019103362e+01 1.019117017e+01 3.2e-08 0.10
28 2.5e-05 4.4e-01 6.3e-05 9.89e-01 1.019104535e+01 1.019116832e+01 2.9e-08 0.10
29 2.2e-05 4.1e-01 5.6e-05 9.91e-01 1.019105595e+01 1.019116671e+01 2.6e-08 0.11
30 2.0e-05 3.8e-01 5.1e-05 9.93e-01 1.019106551e+01 1.019116526e+01 2.3e-08 0.11
31 1.8e-05 3.6e-01 4.6e-05 9.95e-01 1.019107411e+01 1.019116393e+01 2.1e-08 0.11
32 1.6e-05 3.3e-01 4.1e-05 9.96e-01 1.019108186e+01 1.019116272e+01 1.9e-08 0.11
33 1.5e-05 3.1e-01 3.7e-05 9.97e-01 1.019108883e+01 1.019116162e+01 1.7e-08 0.12
34 1.3e-05 3.0e-01 3.3e-05 9.98e-01 1.019109510e+01 1.019116063e+01 1.5e-08 0.12
35 1.2e-05 2.8e-01 3.0e-05 9.98e-01 1.019110075e+01 1.019115973e+01 1.4e-08 0.12
36 1.1e-05 2.7e-01 2.7e-05 9.99e-01 1.019110584e+01 1.019115892e+01 1.2e-08 0.12
37 9.7e-06 2.5e-01 2.4e-05 9.99e-01 1.019111041e+01 1.019115820e+01 1.1e-08 0.13
38 8.7e-06 2.4e-01 2.2e-05 9.99e-01 1.019111454e+01 1.019115754e+01 1.0e-08 0.13
39 7.8e-06 2.3e-01 2.0e-05 9.99e-01 1.019111825e+01 1.019115696e+01 9.0e-09 0.13
40 7.0e-06 2.2e-01 1.8e-05 9.99e-01 1.019112159e+01 1.019115643e+01 8.1e-09 0.13
41 6.3e-06 2.2e-01 1.6e-05 1.00e+00 1.019112460e+01 1.019115596e+01 7.3e-09 0.14
42 5.7e-06 2.1e-01 1.4e-05 9.99e-01 1.019112731e+01 1.019115553e+01 6.6e-09 0.14
43 5.1e-06 2.0e-01 1.3e-05 1.00e+00 1.019112975e+01 1.019115515e+01 5.9e-09 0.14
44 4.6e-06 2.0e-01 1.2e-05 9.99e-01 1.019113194e+01 1.019115480e+01 5.3e-09 0.14
45 4.2e-06 1.9e-01 1.0e-05 9.99e-01 1.019113392e+01 1.019115449e+01 4.8e-09 0.15
46 3.7e-06 1.9e-01 9.4e-06 9.99e-01 1.019113570e+01 1.019115422e+01 4.3e-09 0.15
47 3.4e-06 1.8e-01 8.5e-06 9.99e-01 1.019113730e+01 1.019115397e+01 3.9e-09 0.15
48 3.0e-06 1.8e-01 7.6e-06 9.99e-01 1.019113874e+01 1.019115374e+01 3.5e-09 0.15
49 2.7e-06 1.7e-01 6.9e-06 1.00e+00 1.019114004e+01 1.019115354e+01 3.1e-09 0.15
50 2.5e-06 1.7e-01 6.2e-06 1.00e+00 1.019114121e+01 1.019115336e+01 2.8e-09 0.16
51 2.2e-06 1.7e-01 5.6e-06 1.00e+00 1.019114226e+01 1.019115320e+01 2.5e-09 0.16
52 2.0e-06 1.6e-01 5.0e-06 1.00e+00 1.019114321e+01 1.019115305e+01 2.3e-09 0.16
53 1.8e-06 1.6e-01 4.5e-06 1.00e+00 1.019114406e+01 1.019115292e+01 2.1e-09 0.16
54 1.6e-06 1.6e-01 4.1e-06 9.99e-01 1.019114483e+01 1.019115280e+01 1.9e-09 0.17
55 1.4e-06 1.6e-01 3.6e-06 1.00e+00 1.019114552e+01 1.019115269e+01 1.7e-09 0.17
56 1.3e-06 1.6e-01 3.3e-06 1.00e+00 1.019114614e+01 1.019115260e+01 1.5e-09 0.17
57 1.2e-06 1.6e-01 3.0e-06 1.00e+00 1.019114670e+01 1.019115251e+01 1.4e-09 0.17
58 1.1e-06 1.5e-01 2.7e-06 1.00e+00 1.019114720e+01 1.019115243e+01 1.2e-09 0.18
59 9.5e-07 1.5e-01 2.4e-06 1.00e+00 1.019114766e+01 1.019115236e+01 1.1e-09 0.18
60 8.6e-07 1.5e-01 2.2e-06 1.00e+00 1.019114806e+01 1.019115230e+01 9.9e-10 0.18
61 7.7e-07 1.5e-01 1.9e-06 9.99e-01 1.019114843e+01 1.019115224e+01 8.9e-10 0.18
62 6.9e-07 1.5e-01 1.7e-06 9.99e-01 1.019114876e+01 1.019115219e+01 8.0e-10 0.18
63 6.2e-07 1.5e-01 1.6e-06 1.00e+00 1.019114906e+01 1.019115215e+01 7.2e-10 0.19
64 5.6e-07 1.5e-01 1.4e-06 1.00e+00 1.019114933e+01 1.019115211e+01 6.5e-10 0.19
65 5.1e-07 1.5e-01 1.3e-06 9.99e-01 1.019114957e+01 1.019115207e+01 5.8e-10 0.19
66 4.5e-07 1.5e-01 1.1e-06 1.00e+00 1.019114979e+01 1.019115204e+01 5.2e-10 0.19
67 4.1e-07 1.5e-01 1.0e-06 9.95e-01 1.019114998e+01 1.019115201e+01 4.7e-10 0.20
68 3.7e-07 1.3e-01 9.3e-07 1.00e+00 1.019115016e+01 1.019115198e+01 4.2e-10 0.20
69 3.3e-07 1.2e-01 8.3e-07 9.97e-01 1.019115032e+01 1.019115196e+01 3.8e-10 0.20
70 3.0e-07 1.1e-01 7.5e-07 9.93e-01 1.019115046e+01 1.019115193e+01 3.4e-10 0.20
71 2.7e-07 9.6e-02 6.8e-07 9.91e-01 1.019115059e+01 1.019115191e+01 3.1e-10 0.21
72 2.4e-07 8.6e-02 6.1e-07 9.85e-01 1.019115070e+01 1.019115190e+01 2.8e-10 0.21
73 2.2e-07 7.8e-02 5.5e-07 9.99e-01 1.019115080e+01 1.019115188e+01 2.5e-10 0.21
74 2.0e-07 7.0e-02 4.9e-07 9.93e-01 1.019115090e+01 1.019115187e+01 2.3e-10 0.21
75 1.8e-07 6.3e-02 4.4e-07 1.00e+00 1.019115098e+01 1.019115185e+01 2.0e-10 0.21
76 1.6e-07 5.7e-02 4.0e-07 9.96e-01 1.019115106e+01 1.019115184e+01 1.8e-10 0.22
77 1.4e-07 5.1e-02 3.6e-07 1.00e+00 1.019115113e+01 1.019115183e+01 1.6e-10 0.22
78 1.3e-07 4.6e-02 3.2e-07 1.01e+00 1.019115119e+01 1.019115182e+01 1.5e-10 0.22
79 1.2e-07 4.1e-02 2.9e-07 9.75e-01 1.019115124e+01 1.019115181e+01 1.3e-10 0.22
80 1.0e-07 3.7e-02 2.6e-07 1.03e+00 1.019115130e+01 1.019115181e+01 1.2e-10 0.23
81 9.4e-08 3.3e-02 2.4e-07 1.01e+00 1.019115135e+01 1.019115180e+01 1.1e-10 0.23
82 5.6e-09 1.9e-03 1.4e-08 9.59e-01 1.019115172e+01 1.019115175e+01 8.4e-12 0.23
83 5.0e-09 1.7e-03 1.2e-08 1.08e+00 1.019115172e+01 1.019115175e+01 7.9e-12 0.23
84 6.1e-10 1.0e-04 7.2e-10 9.57e-01 1.019115174e+01 1.019115174e+01 5.8e-13 0.24
Interior-point optimizer terminated. Time: 0.24.
Optimizer terminated. Time: 0.26
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0191151738e+01 Viol. con: 8e-10 var: 0e+00
Dual. obj: 1.0191151740e+01 Viol. con: 0e+00 var: 4e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.28 seconds.
result packing took 38% of solve time
solution checking took 21% of solve time
Using solver 'mosek'
Solving for 2480 variables.
Warning: The variable with index '1860' has only negative coefficients akj.
The problem is possibly ill-posed.
Number of Hessian non-zeros: 1090
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Linux/64-X86
Cores : 20
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2481
Cones : 0
Scalar variables : 5898
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 : 1026
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1043
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1043
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.02
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 286
Optimizer - Cones : 0
Optimizer - Scalar variables : 995 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 : 6557 after factor : 1.08e+04
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 2.5e+03 3.8e+03 7.7e+03 0.00e+00 -7.710634185e+03 1.023181539e-12 1.0e+00 0.05
1 7.9e+02 1.2e+03 2.4e+03 -1.02e-03 -3.455815933e+03 9.887470590e+00 3.4e-01 0.05
2 5.9e+02 8.8e+02 1.8e+03 1.40e+00 -2.233566960e+03 1.170308749e+01 2.5e-01 0.06
3 3.6e+02 5.3e+02 1.1e+03 1.45e+00 -1.157841611e+03 1.326816702e+01 1.6e-01 0.06
4 1.2e+02 1.8e+02 3.8e+02 1.58e+00 -2.954548013e+02 1.395262273e+01 5.6e-02 0.07
5 3.9e+01 6.0e+01 1.2e+02 1.45e+00 -7.301293680e+01 1.289185532e+01 1.9e-02 0.07
6 9.7e+00 2.0e+01 3.0e+01 1.14e+00 -8.861529136e+00 1.133462341e+01 5.4e-03 0.07
7 2.4e+00 1.5e+01 7.6e+00 1.01e+00 5.597932820e+00 1.067653305e+01 1.5e-03 0.07
8 2.2e+00 1.4e+01 7.0e+00 7.89e-01 5.808252279e+00 1.066015711e+01 1.4e-03 0.08
9 1.0e+00 9.8e+00 3.3e+00 7.43e-01 7.722060618e+00 1.051633312e+01 7.2e-04 0.08
10 8.0e-01 9.9e+00 2.6e+00 4.53e-01 8.056008602e+00 1.047012368e+01 5.6e-04 0.09
11 3.9e-01 6.6e+00 1.3e+00 4.91e-01 8.908553707e+00 1.036283692e+01 2.9e-04 0.09
12 2.8e-01 4.8e+00 9.2e-01 5.43e-01 9.174059693e+00 1.032567811e+01 2.1e-04 0.09
13 4.9e-02 4.0e+00 1.7e-01 6.16e-01 9.948200615e+00 1.021226761e+01 5.3e-05 0.09
14 1.5e-02 3.7e+00 5.3e-02 9.08e-01 1.010040330e+01 1.018375016e+01 1.7e-05 0.10
15 5.9e-03 3.4e+00 2.1e-02 9.80e-01 1.014208315e+01 1.017613381e+01 7.2e-06 0.10
16 1.4e-03 3.2e+00 5.0e-03 9.91e-01 1.016356050e+01 1.017158507e+01 1.7e-06 0.10
17 3.5e-04 3.2e+00 1.3e-03 9.97e-01 1.016855827e+01 1.017058435e+01 4.4e-07 0.11
18 8.7e-05 3.1e+00 3.2e-04 9.99e-01 1.016983601e+01 1.017034908e+01 1.1e-07 0.11
19 2.2e-05 2.9e+00 8.2e-05 9.99e-01 1.017015666e+01 1.017028719e+01 2.9e-08 0.11
20 2.0e-05 2.6e+00 7.4e-05 9.98e-01 1.017016683e+01 1.017028461e+01 2.6e-08 0.12
21 1.8e-05 2.4e+00 6.6e-05 9.98e-01 1.017017673e+01 1.017028276e+01 2.3e-08 0.12
22 1.6e-05 2.2e+00 6.0e-05 9.99e-01 1.017018567e+01 1.017028111e+01 2.1e-08 0.12
23 1.4e-05 2.0e+00 5.4e-05 9.99e-01 1.017019372e+01 1.017027962e+01 1.9e-08 0.12
24 1.3e-05 1.8e+00 4.8e-05 9.99e-01 1.017020097e+01 1.017027828e+01 1.7e-08 0.13
25 1.2e-05 1.6e+00 4.3e-05 1.00e+00 1.017020749e+01 1.017027708e+01 1.5e-08 0.13
26 1.1e-05 1.5e+00 3.9e-05 1.00e+00 1.017021337e+01 1.017027599e+01 1.4e-08 0.13
27 9.5e-06 1.4e+00 3.5e-05 1.00e+00 1.017021865e+01 1.017027502e+01 1.2e-08 0.14
28 8.5e-06 1.2e+00 3.2e-05 1.00e+00 1.017022341e+01 1.017027414e+01 1.1e-08 0.14
29 7.7e-06 1.1e+00 2.9e-05 1.00e+00 1.017022769e+01 1.017027334e+01 1.0e-08 0.14
30 6.9e-06 1.0e+00 2.6e-05 1.00e+00 1.017023154e+01 1.017027263e+01 9.1e-09 0.14
31 6.2e-06 9.5e-01 2.3e-05 1.00e+00 1.017023501e+01 1.017027199e+01 8.2e-09 0.15
32 5.6e-06 8.7e-01 2.1e-05 1.00e+00 1.017023813e+01 1.017027141e+01 7.4e-09 0.15
33 5.0e-06 8.0e-01 1.9e-05 1.00e+00 1.017024094e+01 1.017027090e+01 6.6e-09 0.15
34 4.5e-06 7.4e-01 1.7e-05 1.00e+00 1.017024347e+01 1.017027043e+01 6.0e-09 0.15
35 4.1e-06 6.8e-01 1.5e-05 1.00e+00 1.017024574e+01 1.017027001e+01 5.4e-09 0.16
36 3.7e-06 6.3e-01 1.4e-05 1.00e+00 1.017024779e+01 1.017026963e+01 4.8e-09 0.16
37 3.3e-06 5.9e-01 1.2e-05 1.00e+00 1.017024964e+01 1.017026929e+01 4.4e-09 0.16
38 3.0e-06 5.5e-01 1.1e-05 1.00e+00 1.017025129e+01 1.017026898e+01 3.9e-09 0.16
39 2.7e-06 5.1e-01 9.9e-06 1.00e+00 1.017025279e+01 1.017026871e+01 3.5e-09 0.17
40 2.4e-06 4.8e-01 8.9e-06 1.00e+00 1.017025413e+01 1.017026846e+01 3.2e-09 0.17
41 2.2e-06 4.5e-01 8.1e-06 9.99e-01 1.017025534e+01 1.017026824e+01 2.9e-09 0.17
42 2.0e-06 4.2e-01 7.2e-06 1.00e+00 1.017025643e+01 1.017026803e+01 2.6e-09 0.18
43 1.8e-06 4.0e-01 6.5e-06 1.00e+00 1.017025741e+01 1.017026785e+01 2.3e-09 0.18
44 1.6e-06 3.7e-01 5.9e-06 1.00e+00 1.017025829e+01 1.017026769e+01 2.1e-09 0.18
45 1.4e-06 3.5e-01 5.3e-06 1.00e+00 1.017025908e+01 1.017026754e+01 1.9e-09 0.18
46 1.3e-06 3.4e-01 4.8e-06 1.00e+00 1.017025980e+01 1.017026741e+01 1.7e-09 0.19
47 1.2e-06 3.2e-01 4.3e-06 1.00e+00 1.017026044e+01 1.017026729e+01 1.5e-09 0.19
48 1.0e-06 3.1e-01 3.9e-06 9.99e-01 1.017026102e+01 1.017026718e+01 1.4e-09 0.19
49 9.3e-07 2.9e-01 3.5e-06 1.00e+00 1.017026154e+01 1.017026709e+01 1.2e-09 0.19
50 8.4e-07 2.8e-01 3.1e-06 1.00e+00 1.017026201e+01 1.017026700e+01 1.1e-09 0.20
51 7.6e-07 2.7e-01 2.8e-06 1.00e+00 1.017026243e+01 1.017026692e+01 1.0e-09 0.20
52 6.8e-07 2.6e-01 2.5e-06 9.99e-01 1.017026281e+01 1.017026685e+01 9.0e-10 0.20
53 6.1e-07 2.5e-01 2.3e-06 1.00e+00 1.017026315e+01 1.017026679e+01 8.1e-10 0.20
54 5.5e-07 2.5e-01 2.0e-06 1.00e+00 1.017026346e+01 1.017026673e+01 7.3e-10 0.21
55 5.0e-07 2.4e-01 1.8e-06 1.00e+00 1.017026373e+01 1.017026668e+01 6.5e-10 0.21
56 4.5e-07 2.3e-01 1.7e-06 1.00e+00 1.017026398e+01 1.017026663e+01 5.9e-10 0.21
57 4.0e-07 2.3e-01 1.5e-06 1.00e+00 1.017026420e+01 1.017026659e+01 5.3e-10 0.21
58 3.6e-07 2.2e-01 1.3e-06 9.99e-01 1.017026441e+01 1.017026656e+01 4.8e-10 0.22
59 3.3e-07 2.2e-01 1.2e-06 1.00e+00 1.017026459e+01 1.017026652e+01 4.3e-10 0.22
60 2.9e-07 2.2e-01 1.1e-06 1.01e+00 1.017026475e+01 1.017026649e+01 3.9e-10 0.22
61 2.6e-07 2.2e-01 9.8e-07 1.01e+00 1.017026491e+01 1.017026646e+01 3.5e-10 0.22
62 2.4e-07 2.1e-01 8.8e-07 9.91e-01 1.017026504e+01 1.017026644e+01 3.1e-10 0.23
63 2.1e-07 2.1e-01 7.9e-07 1.01e+00 1.017026516e+01 1.017026641e+01 2.8e-10 0.23
64 1.9e-07 2.1e-01 7.1e-07 1.00e+00 1.017026527e+01 1.017026640e+01 2.6e-10 0.23
65 1.7e-07 2.0e-01 6.4e-07 9.93e-01 1.017026536e+01 1.017026638e+01 2.3e-10 0.23
66 3.5e-08 4.1e-02 1.3e-07 9.86e-01 1.017026605e+01 1.017026625e+01 4.7e-11 0.24
67 2.6e-09 2.6e-03 8.1e-09 9.33e-01 1.017026621e+01 1.017026622e+01 4.1e-12 0.24
68 2.9e-10 2.3e-04 7.3e-10 1.04e+00 1.017026622e+01 1.017026622e+01 2.5e-13 0.24
Interior-point optimizer terminated. Time: 0.24.
Optimizer terminated. Time: 0.27
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0170266218e+01 Viol. con: 3e-10 var: 0e+00
Dual. obj: 1.0170266219e+01 Viol. con: 0e+00 var: 6e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.297 seconds.
result packing took 54% of solve time
solution checking took 16% of solve time
Using solver 'mosek'
Solving for 2480 variables.
Warning: The variable with index '1860' has only negative coefficients akj.
The problem is possibly ill-posed.
Number of Hessian non-zeros: 1090
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Linux/64-X86
Cores : 20
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2481
Cones : 0
Scalar variables : 5898
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 : 1026
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1041
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1041
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.02
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 286
Optimizer - Cones : 0
Optimizer - Scalar variables : 995 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.01 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 6557 after factor : 1.08e+04
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 2.6e+03 3.8e+03 7.7e+03 0.00e+00 -7.721659721e+03 1.023181539e-12 1.0e+00 0.03
1 7.9e+02 1.2e+03 2.4e+03 -2.26e-03 -3.459676503e+03 9.890412879e+00 3.4e-01 0.03
2 5.9e+02 8.8e+02 1.8e+03 1.40e+00 -2.229481930e+03 1.171399327e+01 2.5e-01 0.04
3 3.8e+02 5.6e+02 1.2e+03 1.45e+00 -1.236908905e+03 1.314739581e+01 1.6e-01 0.04
4 1.3e+02 2.0e+02 4.0e+02 1.56e+00 -3.249939769e+02 1.397273366e+01 6.0e-02 0.04
5 4.2e+01 6.3e+01 1.3e+02 1.47e+00 -7.775438341e+01 1.298045877e+01 2.0e-02 0.05
6 1.1e+01 2.0e+01 3.4e+01 1.15e+00 -1.121604200e+01 1.141512116e+01 6.0e-03 0.05
7 2.4e+00 1.5e+01 7.6e+00 1.02e+00 5.607856265e+00 1.067191867e+01 1.5e-03 0.05
8 2.2e+00 1.4e+01 7.1e+00 7.87e-01 5.805630203e+00 1.065684993e+01 1.4e-03 0.05
9 1.1e+00 9.6e+00 3.5e+00 7.42e-01 7.632597743e+00 1.052164175e+01 7.5e-04 0.06
10 1.0e+00 9.2e+00 3.3e+00 4.62e-01 7.565677811e+00 1.051356260e+01 7.2e-04 0.06
11 3.9e-01 6.8e+00 1.3e+00 5.15e-01 8.911385988e+00 1.036015865e+01 3.0e-04 0.06
12 2.8e-01 4.9e+00 9.1e-01 5.59e-01 9.187032050e+00 1.032242960e+01 2.2e-04 0.07
13 4.6e-02 4.2e+00 1.6e-01 6.42e-01 9.960825343e+00 1.020958464e+01 5.2e-05 0.07
14 1.4e-02 3.9e+00 5.2e-02 9.15e-01 1.010227806e+01 1.018331199e+01 1.8e-05 0.07
15 5.5e-03 3.6e+00 2.0e-02 9.80e-01 1.014380132e+01 1.017568024e+01 7.0e-06 0.07
16 1.2e-03 3.4e+00 4.4e-03 9.91e-01 1.016437082e+01 1.017127237e+01 1.6e-06 0.08
17 2.7e-04 3.4e+00 1.0e-03 9.97e-01 1.016879807e+01 1.017037997e+01 3.6e-07 0.08
18 6.2e-05 3.2e+00 2.3e-04 9.99e-01 1.016982392e+01 1.017018980e+01 8.5e-08 0.08
19 1.5e-05 3.0e+00 5.7e-05 9.99e-01 1.017005490e+01 1.017014539e+01 2.1e-08 0.09
20 1.4e-05 2.7e+00 5.2e-05 9.99e-01 1.017006192e+01 1.017014358e+01 1.9e-08 0.09
21 1.2e-05 2.5e+00 4.6e-05 9.99e-01 1.017006879e+01 1.017014231e+01 1.7e-08 0.09
22 1.1e-05 2.2e+00 4.2e-05 9.99e-01 1.017007499e+01 1.017014116e+01 1.5e-08 0.09
23 1.0e-05 2.0e+00 3.8e-05 9.99e-01 1.017008057e+01 1.017014012e+01 1.4e-08 0.10
24 9.0e-06 1.8e+00 3.4e-05 1.00e+00 1.017008559e+01 1.017013919e+01 1.3e-08 0.10
25 8.1e-06 1.7e+00 3.0e-05 1.00e+00 1.017009011e+01 1.017013835e+01 1.1e-08 0.10
26 7.3e-06 1.5e+00 2.7e-05 1.00e+00 1.017009418e+01 1.017013759e+01 1.0e-08 0.10
27 6.5e-06 1.4e+00 2.5e-05 1.00e+00 1.017009784e+01 1.017013691e+01 9.1e-09 0.11
28 5.9e-06 1.3e+00 2.2e-05 1.00e+00 1.017010113e+01 1.017013630e+01 8.2e-09 0.11
29 5.3e-06 1.2e+00 2.0e-05 1.00e+00 1.017010410e+01 1.017013575e+01 7.4e-09 0.11
30 4.8e-06 1.1e+00 1.8e-05 1.00e+00 1.017010677e+01 1.017013525e+01 6.6e-09 0.11
31 4.3e-06 9.7e-01 1.6e-05 1.00e+00 1.017010917e+01 1.017013481e+01 6.0e-09 0.12
32 3.9e-06 8.9e-01 1.5e-05 1.00e+00 1.017011133e+01 1.017013441e+01 5.4e-09 0.12
33 3.5e-06 8.2e-01 1.3e-05 1.00e+00 1.017011328e+01 1.017013404e+01 4.8e-09 0.12
34 3.1e-06 7.6e-01 1.2e-05 1.00e+00 1.017011503e+01 1.017013372e+01 4.4e-09 0.12
35 2.8e-06 7.0e-01 1.1e-05 1.00e+00 1.017011660e+01 1.017013343e+01 3.9e-09 0.13
36 2.5e-06 6.5e-01 9.5e-06 1.00e+00 1.017011802e+01 1.017013316e+01 3.5e-09 0.13
37 2.3e-06 6.0e-01 8.6e-06 1.00e+00 1.017011930e+01 1.017013292e+01 3.2e-09 0.13
38 2.1e-06 5.6e-01 7.7e-06 1.00e+00 1.017012045e+01 1.017013271e+01 2.9e-09 0.13
39 1.8e-06 5.2e-01 7.0e-06 1.00e+00 1.017012148e+01 1.017013252e+01 2.6e-09 0.14
40 1.7e-06 4.9e-01 6.3e-06 1.00e+00 1.017012241e+01 1.017013235e+01 2.3e-09 0.14
41 1.5e-06 4.6e-01 5.6e-06 1.00e+00 1.017012325e+01 1.017013219e+01 2.1e-09 0.14
42 1.3e-06 4.3e-01 5.1e-06 9.98e-01 1.017012400e+01 1.017013205e+01 1.9e-09 0.14
43 1.2e-06 4.0e-01 4.6e-06 9.99e-01 1.017012468e+01 1.017013192e+01 1.7e-09 0.15
44 1.1e-06 3.8e-01 4.1e-06 9.98e-01 1.017012529e+01 1.017013181e+01 1.5e-09 0.15
45 9.8e-07 3.6e-01 3.7e-06 9.99e-01 1.017012584e+01 1.017013171e+01 1.4e-09 0.15
46 8.8e-07 3.4e-01 3.3e-06 1.00e+00 1.017012633e+01 1.017013161e+01 1.2e-09 0.15
47 8.0e-07 3.3e-01 3.0e-06 1.00e+00 1.017012678e+01 1.017013153e+01 1.1e-09 0.16
48 7.2e-07 3.1e-01 2.7e-06 9.98e-01 1.017012718e+01 1.017013146e+01 1.0e-09 0.16
49 6.4e-07 3.0e-01 2.4e-06 1.00e+00 1.017012754e+01 1.017013139e+01 9.0e-10 0.16
50 5.8e-07 2.9e-01 2.2e-06 1.00e+00 1.017012787e+01 1.017013133e+01 8.1e-10 0.16
51 5.2e-07 2.8e-01 2.0e-06 1.00e+00 1.017012816e+01 1.017013127e+01 7.3e-10 0.17
52 4.7e-07 2.7e-01 1.8e-06 9.98e-01 1.017012842e+01 1.017013122e+01 6.6e-10 0.17
53 4.2e-07 2.6e-01 1.6e-06 1.00e+00 1.017012866e+01 1.017013118e+01 5.9e-10 0.17
54 3.8e-07 2.5e-01 1.4e-06 1.00e+00 1.017012887e+01 1.017013114e+01 5.3e-10 0.18
55 3.4e-07 2.5e-01 1.3e-06 1.00e+00 1.017012906e+01 1.017013110e+01 4.8e-10 0.18
56 3.1e-07 2.4e-01 1.2e-06 1.00e+00 1.017012924e+01 1.017013107e+01 4.3e-10 0.18
57 2.8e-07 2.3e-01 1.0e-06 9.99e-01 1.017012939e+01 1.017013104e+01 3.9e-10 0.18
58 2.5e-07 2.3e-01 9.4e-07 1.01e+00 1.017012954e+01 1.017013102e+01 3.5e-10 0.19
59 2.2e-07 2.3e-01 8.5e-07 1.00e+00 1.017012966e+01 1.017013099e+01 3.2e-10 0.19
60 2.0e-07 2.2e-01 7.6e-07 1.00e+00 1.017012977e+01 1.017013097e+01 2.8e-10 0.19
61 1.8e-07 2.0e-01 6.9e-07 1.02e+00 1.017012988e+01 1.017013095e+01 2.6e-10 0.19
62 1.6e-07 2.0e-01 6.2e-07 9.89e-01 1.017012997e+01 1.017013093e+01 2.3e-10 0.20
63 1.5e-07 1.8e-01 5.6e-07 1.01e+00 1.017013006e+01 1.017013092e+01 2.1e-10 0.20
64 1.3e-07 1.6e-01 5.0e-07 1.01e+00 1.017013013e+01 1.017013090e+01 1.9e-10 0.20
65 1.2e-07 1.4e-01 4.5e-07 1.01e+00 1.017013020e+01 1.017013089e+01 1.7e-10 0.20
66 1.1e-07 1.3e-01 4.0e-07 9.87e-01 1.017013026e+01 1.017013088e+01 1.5e-10 0.21
67 9.7e-08 1.2e-01 3.6e-07 1.02e+00 1.017013032e+01 1.017013087e+01 1.4e-10 0.21
68 8.7e-08 1.0e-01 3.3e-07 9.89e-01 1.017013036e+01 1.017013086e+01 1.3e-10 0.21
69 7.8e-08 9.4e-02 3.0e-07 9.94e-01 1.017013040e+01 1.017013085e+01 1.1e-10 0.21
70 7.1e-08 8.5e-02 2.7e-07 1.03e+00 1.017013045e+01 1.017013084e+01 1.0e-10 0.22
71 6.3e-08 7.6e-02 2.4e-07 1.05e+00 1.017013049e+01 1.017013084e+01 9.5e-11 0.22
72 5.7e-08 6.8e-02 2.2e-07 1.06e+00 1.017013053e+01 1.017013083e+01 8.9e-11 0.22
73 3.6e-09 3.9e-03 1.2e-08 9.69e-01 1.017013077e+01 1.017013079e+01 6.3e-12 0.22
74 2.7e-10 2.3e-04 7.5e-10 9.11e-01 1.017013078e+01 1.017013078e+01 5.7e-13 0.23
Interior-point optimizer terminated. Time: 0.23.
Optimizer terminated. Time: 0.25
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0170130781e+01 Viol. con: 2e-10 var: 0e+00
Dual. obj: 1.0170130782e+01 Viol. con: 0e+00 var: 6e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.272 seconds.
result packing took 39% of solve time
solution checking took 16% of solve time
Solving took 5 GP solves and 3.97 seconds.
Warning: Constraint [W_{total}_FleetMission_(0,) [N]... >= W_{dry}_FleetMission_(0,) + W_{f_{total}}_FleetMission_(0,) [N]...] is not tight because the left hand side evaluated to 366641.677652 newton but the right hand side evaluated to 366630.065872 newton (Allowable error: 0.0001%, Actual error: 0.0032%)
Warning: Constraint [W_{total}_FleetMission_(1,) [N]... >= W_{dry}_FleetMission_(1,) + W_{f_{total}}_FleetMission_(1,) [N]...] is not tight because the left hand side evaluated to 377162.191602 newton but the right hand side evaluated to 377115.440896 newton (Allowable error: 0.0001%, Actual error: 0.012%)
Warning: Constraint [W_{total}_FleetMission_(2,) [N]... >= W_{dry}_FleetMission_(2,) + W_{f_{total}}_FleetMission_(2,) [N]...] is not tight because the left hand side evaluated to 388105.090001 newton but the right hand side evaluated to 387998.859576 newton (Allowable error: 0.0001%, Actual error: 0.027%)
Warning: Constraint [W_{total}_FleetMission_(3,) [N]... >= W_{dry}_FleetMission_(3,) + W_{f_{total}}_FleetMission_(3,) [N]...] is not tight because the left hand side evaluated to 399470.244148 newton but the right hand side evaluated to 399279.092859 newton (Allowable error: 0.0001%, Actual error: 0.048%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 361212.19376 newton but the right hand side evaluated to 361206.369135 newton (Allowable error: 0.0001%, Actual error: 0.0016%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 1) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 1) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 371522.140357 newton but the right hand side evaluated to 371498.543848 newton (Allowable error: 0.0001%, Actual error: 0.0064%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 2) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 2) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 382190.305941 newton but the right hand side evaluated to 382135.967579 newton (Allowable error: 0.0001%, Actual error: 0.014%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 3) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 3) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 393255.642727 newton but the right hand side evaluated to 393156.477541 newton (Allowable error: 0.0001%, Actual error: 0.025%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 356181.886364 newton but the right hand side evaluated to 356176.099248 newton (Allowable error: 0.0001%, Actual error: 0.0016%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 1) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 1) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 361243.203314 newton but the right hand side evaluated to 361220.049153 newton (Allowable error: 0.0001%, Actual error: 0.0064%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 2) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 2) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side ev.aluated to 366354.224789 newton but the right hand side evaluated to 366302.332829 newton (Allowable error: 0.0001%, Actual error: 0.014%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 3) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 3) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 371535.454606 newton but the right hand side evaluated to 371443.468602 newton (Allowable error: 0.0001%, Actual error: 0.025%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) [N]...] is not tight because the left hand side evaluated to 18366.9601708 newton but the right hand side evaluated to 18366.717364 newton (Allowable error: 0.0001%, Actual error: 0.0013%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 1) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 1) [N]...] is not tight because the left hand side evaluated to 18344.4540562 newton but the right hand side evaluated to 18344.2047199 newton (Allowable error: 0.0001%, Actual error: 0.0014%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 2) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 2) [N]...] is not tight because the left hand side evaluated to 18344.4539974 newton but the right hand side evaluated to 18344.2046312 newton (Allowable error: 0.0001%, Actual error: 0.0014%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 3) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 3) [N]...] is not tight because the left hand side evaluated to 18344.4540219 newton but the right hand side evaluated to 18344.2046543 newton (Allowable error: 0.0001%, Actual error: 0.0014%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) [N]...] is not tight because the left hand side evaluated to 18924.2850918 newton but the right hand side evaluated to 18924.2646045 newton (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 2) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 2) [N]...] is not tight because the left hand side evaluated to 8445.89963406 newton but the right hand side evaluated to 8445.84800191 newton (Allowable error: 0.0001%, Actual error: 0.00061%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 3) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 3) [N]...] is not tight because the left hand side evaluated to 8626.29336459 newton but the right hand side evaluated to 8626.24784668 newton (Allowable error: 0.0001%, Actual error: 0.00053%)
T_{t_{4.1_{max}}}_FleetMission/Aircraft/Engine has no upper bound
Beginning signomial solve.
Using solver 'mosek'
Solving for 2480 variables.
Warning: The variable with index '1860' has only negative coefficients akj.
The problem is possibly ill-posed.
Number of Hessian non-zeros: 1090
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Linux/64-X86
Cores : 20
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2481
Cones : 0
Scalar variables : 5898
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 : 987
Eliminator terminated.
Eliminator started.
Total number of eliminations : 990
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 990
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 : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 329
Optimizer - Cones : 0
Optimizer - Scalar variables : 1038 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.01 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 6388 after factor : 1.11e+04
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 1.2e+03 1.8e+04 2.1e+04 0.00e+00 -2.068680080e+04 1.023181539e-12 1.0e+00 0.03
1 9.0e+02 1.3e+04 1.5e+04 -1.09e-01 -1.772348494e+04 2.815948399e+00 7.3e-01 0.03
2 3.6e+02 5.2e+03 6.0e+03 4.01e-02 -1.101707998e+04 1.002502268e+01 3.0e-01 0.03
3 1.9e+02 2.7e+03 3.1e+03 6.47e-01 -5.771848562e+03 1.375651249e+01 1.7e-01 0.04
4 5.8e+01 8.4e+02 9.8e+02 1.20e+00 -1.605083548e+03 1.625562896e+01 5.7e-02 0.04
5 3.1e+01 4.5e+02 5.2e+02 1.69e+00 -6.744957436e+02 1.621109356e+01 3.1e-02 0.04
6 1.0e+01 1.4e+02 1.7e+02 1.50e+00 -1.671041217e+02 1.570774204e+01 1.0e-02 0.05
7 4.4e+00 6.5e+01 7.4e+01 1.15e+00 -6.553349527e+01 1.497839910e+01 4.8e-03 0.05
8 2.1e+00 3.2e+01 3.6e+01 8.76e-01 -3.007494893e+01 1.440760238e+01 2.4e-03 0.05
9 9.9e-01 1.8e+01 1.7e+01 5.55e-01 -1.319622815e+01 1.384697765e+01 1.2e-03 0.06
10 3.3e-01 6.3e+00 5.6e+00 5.48e-01 1.823497698e+00 1.321184673e+01 4.6e-04 0.06
11 1.5e-01 3.2e+00 2.6e+00 6.35e-01 7.019627949e+00 1.295307377e+01 2.2e-04 0.06
12 9.8e-02 2.5e+00 1.7e+00 7.48e-01 8.809147686e+00 1.282120181e+01 1.4e-04 0.07
13 2.3e-02 1.5e+00 4.1e-01 8.18e-01 1.155748783e+01 1.259122796e+01 4.1e-05 0.07
14 7.4e-03 1.5e+00 1.3e-01 9.41e-01 1.219956625e+01 1.254374950e+01 1.5e-05 0.07
15 2.0e-03 1.5e+00 3.7e-02 9.82e-01 1.242497573e+01 1.252084982e+01 4.4e-06 0.08
16 6.0e-04 1.3e+00 1.1e-02 9.93e-01 1.248670132e+01 1.251547964e+01 1.3e-06 0.08
17 2.4e-04 1.1e+00 4.4e-03 9.71e-01 1.250278539e+01 1.251429835e+01 5.4e-07 0.08
18 2.1e-04 9.6e-01 4.0e-03 9.59e-01 1.250379104e+01 1.251422237e+01 4.9e-07 0.09
19 1.9e-04 8.7e-01 3.6e-03 9.81e-01 1.250475352e+01 1.251415878e+01 4.4e-07 0.09
20 1.7e-04 7.9e-01 3.2e-03 9.69e-01 1.250561460e+01 1.251409802e+01 3.9e-07 0.09
21 1.6e-04 7.2e-01 2.9e-03 1.01e+00 1.250641758e+01 1.251404110e+01 3.5e-07 0.10
22 1.4e-04 6.7e-01 2.6e-03 1.08e+00 1.250736650e+01 1.251397265e+01 3.3e-07 0.10
23 1.3e-04 6.1e-01 2.4e-03 1.01e+00 1.250799785e+01 1.251392571e+01 3.0e-07 0.10
24 1.1e-04 5.6e-01 2.1e-03 9.64e-01 1.250855129e+01 1.251388527e+01 2.7e-07 0.11
25 1.0e-04 5.2e-01 1.9e-03 1.04e+00 1.250913907e+01 1.251384275e+01 2.5e-07 0.11
26 9.3e-05 4.8e-01 1.7e-03 9.76e-01 1.250958483e+01 1.251380976e+01 2.2e-07 0.11
27 8.3e-05 4.4e-01 1.5e-03 1.01e+00 1.250999595e+01 1.251378202e+01 2.0e-07 0.11
28 7.5e-05 4.1e-01 1.4e-03 1.00e+00 1.251035191e+01 1.251375748e+01 1.8e-07 0.12
29 6.7e-05 3.7e-01 1.2e-03 8.60e-01 1.251064635e+01 1.251374078e+01 1.6e-07 0.12
30 6.1e-05 3.5e-01 1.1e-03 1.01e+00 1.251095465e+01 1.251371958e+01 1.5e-07 0.12
31 5.5e-05 3.3e-01 1.0e-03 1.09e+00 1.251131074e+01 1.251369602e+01 1.4e-07 0.13
32 4.9e-05 3.3e-01 9.1e-04 1.12e+00 1.251166213e+01 1.251367007e+01 1.3e-07 0.13
33 4.4e-05 3.0e-01 8.2e-04 8.83e-01 1.251182252e+01 1.251366340e+01 1.2e-07 0.13
34 4.0e-05 2.9e-01 7.4e-04 1.07e+00 1.251204634e+01 1.251364788e+01 1.1e-07 0.14
35 3.6e-05 2.7e-01 6.6e-04 8.56e-01 1.251218288e+01 1.251364040e+01 9.9e-08 0.14
36 3.2e-05 2.6e-01 6.0e-04 7.71e-01 1.251232399e+01 1.251362946e+01 8.9e-08 0.14
37 2.9e-05 2.5e-01 5.4e-04 9.91e-01 1.251246554e+01 1.251361663e+01 8.0e-08 0.15
38 2.6e-05 2.4e-01 4.8e-04 9.37e-01 1.251257459e+01 1.251360925e+01 7.2e-08 0.15
39 2.3e-05 2.2e-01 4.4e-04 6.36e-01 1.251265913e+01 1.251360561e+01 6.5e-08 0.15
40 2.1e-05 2.1e-01 3.9e-04 1.05e+00 1.251275889e+01 1.251360073e+01 6.0e-08 0.16
41 1.9e-05 2.0e-01 3.5e-04 8.52e-01 1.251283158e+01 1.251359662e+01 5.4e-08 0.16
42 1.7e-05 1.8e-01 3.2e-04 9.60e-01 1.251289621e+01 1.251359352e+01 4.9e-08 0.16
43 1.5e-05 1.8e-01 2.9e-04 1.55e+00 1.251296794e+01 1.251358699e+01 4.4e-08 0.17
44 1.4e-05 1.6e-01 2.6e-04 2.83e+00 1.251310989e+01 1.251356086e+01 3.6e-08 0.17
45 1.3e-05 1.6e-01 2.3e-04 1.76e+00 1.251315438e+01 1.251355941e+01 3.2e-08 0.17
46 1.1e-05 1.5e-01 2.1e-04 1.16e+00 1.251321371e+01 1.251355861e+01 3.2e-08 0.18
47 1.0e-05 1.3e-01 1.9e-04 8.37e-01 1.251324924e+01 1.251355692e+01 2.8e-08 0.18
48 9.2e-06 1.2e-01 1.7e-04 2.33e+00 1.251328935e+01 1.251355422e+01 2.5e-08 0.18
49 8.3e-06 1.1e-01 1.5e-04 2.28e+00 1.251331791e+01 1.251355304e+01 2.3e-08 0.19
50 4.7e-06 5.9e-02 8.5e-05 3.28e-01 1.251343314e+01 1.251354687e+01 1.1e-08 0.19
51 4.2e-06 5.3e-02 7.7e-05 1.00e+00 1.251344333e+01 1.251354688e+01 9.6e-09 0.19
52 3.8e-06 4.8e-02 7.1e-05 1.00e+00 1.251345178e+01 1.251354686e+01 8.7e-09 0.20
53 3.4e-06 4.6e-02 6.4e-05 1.88e+00 1.251345934e+01 1.251354698e+01 7.8e-09 0.20
54 9.9e-07 3.7e-03 5.1e-06 -4.42e-02 1.251353915e+01 1.251354827e+01 1.8e-09 0.20
55 5.6e-06 3.9e-04 3.1e-05 1.00e+00 1.251349203e+01 1.251354675e+01 1.9e-10 0.21
56 2.4e-06 3.2e-06 4.5e-06 1.00e+00 1.251353849e+01 1.251354657e+01 1.6e-12 0.21
Interior-point optimizer terminated. Time: 0.21.
Optimizer terminated. Time: 0.23
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.2513538486e+01 Viol. con: 2e-06 var: 0e+00
Dual. obj: 1.2513546571e+01 Viol. con: 0e+00 var: 1e-06
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.246 seconds.
result packing took 2.1e+02% of solve time
solution checking took 13% of solve time
Using solver 'mosek'
Solving for 2480 variables.
Warning: The variable with index '1860' has only negative coefficients akj.
The problem is possibly ill-posed.
Number of Hessian non-zeros: 1090
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Linux/64-X86
Cores : 20
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2481
Cones : 0
Scalar variables : 5898
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 : 1029
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1042
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1042
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 : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 283
Optimizer - Cones : 0
Optimizer - Scalar variables : 992 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.01 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 6474 after factor : 1.07e+04
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 2.8e+03 3.7e+03 3.0e+03 0.00e+00 -3.007135100e+03 1.023181539e-12 1.0e+00 0.03
1 9.0e+02 1.2e+03 1.0e+03 1.08e-01 -1.341963821e+03 9.797917674e+00 3.5e-01 0.03
2 2.9e+02 3.8e+02 3.3e+02 1.32e+00 -3.590144644e+02 1.400159696e+01 1.2e-01 0.03
3 9.2e+01 1.2e+02 1.1e+02 1.76e+00 -7.670787429e+01 1.406682636e+01 4.1e-02 0.04
4 2.6e+01 3.7e+01 3.1e+01 1.37e+00 -1.050795785e+01 1.256362606e+01 1.3e-02 0.04
5 6.8e+00 1.3e+01 8.5e+00 1.11e+00 5.163474625e+00 1.114702896e+01 3.8e-03 0.04
6 2.2e+00 1.0e+01 2.8e+00 1.03e+00 8.704318315e+00 1.068267203e+01 1.3e-03 0.05
7 2.0e+00 9.4e+00 2.6e+00 8.25e-01 8.800439145e+00 1.066518122e+01 1.2e-03 0.05
8 9.4e-01 8.3e+00 1.2e+00 7.72e-01 9.473361603e+00 1.052722204e+01 6.0e-04 0.05
9 6.8e-01 7.9e+00 8.8e-01 3.66e-01 9.557043801e+00 1.047595794e+01 4.5e-04 0.06
10 2.9e-01 4.0e+00 3.9e-01 4.99e-01 9.849777350e+00 1.035919528e+01 2.1e-04 0.06
11 6.0e-02 3.7e+00 9.0e-02 6.71e-01 1.010954387e+01 1.024813589e+01 5.6e-05 0.06
12 2.0e-02 3.4e+00 3.1e-02 9.08e-01 1.017081788e+01 1.022013277e+01 2.0e-05 0.07
13 5.7e-03 3.2e+00 9.3e-03 9.67e-01 1.019375750e+01 1.020861467e+01 6.1e-06 0.07
14 1.7e-03 3.1e+00 2.8e-03 9.91e-01 1.020061827e+01 1.020520487e+01 1.9e-06 0.07
15 5.3e-04 2.9e+00 8.8e-04 9.98e-01 1.020274612e+01 1.020416108e+01 5.8e-07 0.08
16 2.1e-04 2.7e+00 3.4e-04 9.99e-01 1.020333993e+01 1.020389094e+01 2.3e-07 0.08
17 1.9e-04 2.5e+00 3.1e-04 1.00e+00 1.020337344e+01 1.020387029e+01 2.0e-07 0.08
18 1.7e-04 2.2e+00 2.8e-04 1.00e+00 1.020340617e+01 1.020385342e+01 1.8e-07 0.09
19 1.5e-04 2.0e+00 2.5e-04 1.00e+00 1.020343614e+01 1.020383868e+01 1.7e-07 0.09
20 1.4e-04 1.9e+00 2.2e-04 1.00e+00 1.020346317e+01 1.020382545e+01 1.5e-07 0.09
21 1.2e-04 1.7e+00 2.0e-04 1.00e+00 1.020348754e+01 1.020381360e+01 1.3e-07 0.10
22 1.1e-04 1.5e+00 1.8e-04 1.00e+00 1.020350950e+01 1.020380296e+01 1.2e-07 0.10
23 9.9e-05 1.4e+00 1.6e-04 1.00e+00 1.020352930e+01 1.020379341e+01 1.1e-07 0.10
24 8.9e-05 1.3e+00 1.5e-04 1.00e+00 1.020354714e+01 1.020378485e+01 9.8e-08 0.11
25 8.0e-05 1.2e+00 1.3e-04 1.00e+00 1.020356322e+01 1.020377715e+01 8.8e-08 0.11
26 7.2e-05 1.1e+00 1.2e-04 1.00e+00 1.020357770e+01 1.020377025e+01 7.9e-08 0.11
27 6.5e-05 9.8e-01 1.1e-04 1.00e+00 1.020359075e+01 1.020376404e+01 7.1e-08 0.12
28 5.8e-05 9.0e-01 9.6e-05 1.00e+00 1.020360251e+01 1.020375847e+01 6.4e-08 0.12
29 5.3e-05 8.2e-01 8.7e-05 1.00e+00 1.020361310e+01 1.020375347e+01 5.8e-08 0.12
30 4.7e-05 7.6e-01 7.8e-05 1.00e+00 1.020362264e+01 1.020374897e+01 5.2e-08 0.12
31 4.3e-05 7.0e-01 7.0e-05 1.00e+00 1.020363123e+01 1.020374493e+01 4.7e-08 0.13
32 3.8e-05 6.5e-01 6.3e-05 1.00e+00 1.020363897e+01 1.020374130e+01 4.2e-08 0.13
33 3.5e-05 6.0e-01 5.7e-05 1.00e+00 1.020364594e+01 1.020373804e+01 3.8e-08 0.13
34 3.1e-05 5.6e-01 5.1e-05 1.00e+00 1.020365222e+01 1.020373511e+01 3.4e-08 0.14
35 2.8e-05 5.2e-01 4.6e-05 1.00e+00 1.020365788e+01 1.020373248e+01 3.1e-08 0.14
36 2.5e-05 4.9e-01 4.1e-05 1.00e+00 1.020366297e+01 1.020373011e+01 2.8e-08 0.14
37 2.3e-05 4.6e-01 3.7e-05 1.00e+00 1.020366756e+01 1.020372798e+01 2.5e-08 0.15
38 2.0e-05 4.3e-01 3.4e-05 1.00e+00 1.020367169e+01 1.020372607e+01 2.2e-08 0.15
39 1.8e-05 4.0e-01 3.0e-05 1.00e+00 1.020367540e+01 1.020372435e+01 2.0e-08 0.15
40 1.7e-05 3.8e-01 2.7e-05 1.00e+00 1.020367875e+01 1.020372281e+01 1.8e-08 0.16
41 1.5e-05 3.6e-01 2.5e-05 1.00e+00 1.020368177e+01 1.020372142e+01 1.6e-08 0.16
42 1.3e-05 3.4e-01 2.2e-05 1.00e+00 1.020368448e+01 1.020372017e+01 1.5e-08 0.16
43 1.2e-05 3.3e-01 2.0e-05 1.00e+00 1.020368693e+01 1.020371904e+01 1.3e-08 0.16
44 1.3e-06 3.5e-02 2.1e-06 1.00e+00 1.020370662e+01 1.020371005e+01 1.4e-09 0.17
45 7.1e-08 1.9e-03 1.2e-07 1.00e+00 1.020370884e+01 1.020370903e+01 8.0e-11 0.17
46 6.3e-10 1.7e-05 1.2e-09 1.01e+00 1.020370897e+01 1.020370897e+01 5.1e-13 0.17
Interior-point optimizer terminated. Time: 0.18.
Optimizer terminated. Time: 0.19
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0203708971e+01 Viol. con: 8e-10 var: 0e+00
Dual. obj: 1.0203708973e+01 Viol. con: 0e+00 var: 5e-06
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.21 seconds.
result packing took 81% of solve time
solution checking took 34% of solve time
Using solver 'mosek'
Solving for 2480 variables.
Warning: The variable with index '1860' has only negative coefficients akj.
The problem is possibly ill-posed.
Number of Hessian non-zeros: 1090
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Linux/64-X86
Cores : 20
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2481
Cones : 0
Scalar variables : 5898
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 : 1026
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1043
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1043
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 : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 286
Optimizer - Cones : 0
Optimizer - Scalar variables : 995 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.01 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 6557 after factor : 1.08e+04
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 2.5e+03 3.8e+03 7.6e+03 0.00e+00 -7.646714999e+03 1.023181539e-12 1.0e+00 0.03
1 7.9e+02 1.2e+03 2.4e+03 4.43e-03 -3.439952706e+03 9.865562135e+00 3.4e-01 0.03
2 5.5e+02 8.3e+02 1.7e+03 1.39e+00 -2.072269266e+03 1.199516136e+01 2.4e-01 0.03
3 2.4e+02 3.6e+02 7.4e+02 1.50e+00 -7.271047382e+02 1.390011863e+01 1.1e-01 0.03
4 7.2e+01 1.1e+02 2.2e+02 1.65e+00 -1.536469103e+02 1.372034911e+01 3.4e-02 0.04
5 1.9e+01 3.1e+01 5.8e+01 1.27e+00 -2.763506312e+01 1.211217867e+01 9.8e-03 0.04
6 4.5e+00 1.2e+01 1.4e+01 1.05e+00 1.436159313e+00 1.092817001e+01 2.7e-03 0.04
7 2.1e+00 1.1e+01 6.5e+00 9.71e-01 6.193041079e+00 1.068618414e+01 1.3e-03 0.04
8 1.9e+00 9.6e+00 5.9e+00 7.00e-01 6.369614845e+00 1.066665806e+01 1.2e-03 0.05
9 7.5e-01 7.8e+00 2.4e+00 6.46e-01 8.110264072e+00 1.049629842e+01 5.4e-04 0.05
10 6.1e-01 6.3e+00 1.9e+00 5.13e-01 8.387124980e+00 1.045979773e+01 4.3e-04 0.05
11 1.9e-01 3.0e+00 6.4e-01 5.08e-01 9.417594042e+00 1.031757347e+01 1.6e-04 0.05
12 8.2e-02 3.1e+00 2.7e-01 7.46e-01 9.843804471e+00 1.025740580e+01 7.4e-05 0.06
13 7.4e-02 2.8e+00 2.5e-01 8.54e-01 9.883249897e+00 1.025562260e+01 6.6e-05 0.06
14 6.6e-02 2.6e+00 2.2e-01 8.50e-01 9.912632523e+00 1.025014278e+01 6.0e-05 0.06
15 6.0e-02 2.3e+00 2.0e-01 8.61e-01 9.939030181e+00 1.024491298e+01 5.4e-05 0.06
16 5.4e-02 2.1e+00 1.8e-01 8.72e-01 9.963012883e+00 1.024007380e+01 4.8e-05 0.07
17 4.8e-02 1.9e+00 1.6e-01 8.83e-01 9.984803449e+00 1.023562315e+01 4.4e-05 0.07
18 4.4e-02 1.8e+00 1.5e-01 8.93e-01 1.000459165e+01 1.023153944e+01 3.9e-05 0.07
19 3.9e-02 1.6e+00 1.3e-01 9.03e-01 1.002254787e+01 1.022779897e+01 3.5e-05 0.07
20 3.5e-02 1.5e+00 1.2e-01 9.12e-01 1.003883012e+01 1.022437813e+01 3.2e-05 0.08
21 3.2e-02 1.3e+00 1.1e-01 9.20e-01 1.005358473e+01 1.022125406e+01 2.9e-05 0.08
22 2.9e-02 1.2e+00 9.6e-02 9.27e-01 1.006694697e+01 1.021840477e+01 2.6e-05 0.08
23 2.6e-02 1.1e+00 8.6e-02 9.34e-01 1.007904157e+01 1.021580929e+01 2.3e-05 0.08
24 2.3e-02 1.0e+00 7.8e-02 9.40e-01 1.008998325e+01 1.021344765e+01 2.1e-05 0.09
25 2.1e-02 9.6e-01 7.0e-02 9.45e-01 1.009987733e+01 1.021130099e+01 1.9e-05 0.09
26 1.9e-02 8.8e-01 6.3e-02 9.51e-01 1.010882030e+01 1.020935154e+01 1.7e-05 0.09
27 1.7e-02 8.1e-01 5.7e-02 9.55e-01 1.011690044e+01 1.020758270e+01 1.5e-05 0.09
28 1.5e-02 7.5e-01 5.1e-02 9.60e-01 1.012419842e+01 1.020597899e+01 1.4e-05 0.10
29 1.4e-02 7.0e-01 4.6e-02 9.64e-01 1.013078784e+01 1.020452606e+01 1.2e-05 0.10
30 1.2e-02 6.5e-01 4.1e-02 9.67e-01 1.013673579e+01 1.020321063e+01 1.1e-05 0.10
31 1.1e-02 6.0e-01 3.7e-02 9.70e-01 1.014210334e+01 1.020202048e+01 1.0e-05 0.10
32 1.0e-02 5.6e-01 3.3e-02 9.73e-01 1.014694601e+01 1.020094436e+01 9.1e-06 0.10
33 9.0e-03 5.2e-01 3.0e-02 9.76e-01 1.015131428e+01 1.019997191e+01 8.2e-06 0.11
34 8.1e-03 4.9e-01 2.7e-02 9.79e-01 1.015525390e+01 1.019909367e+01 7.3e-06 0.11
35 7.3e-03 4.6e-01 2.4e-02 9.81e-01 1.015880640e+01 1.019830094e+01 6.6e-06 0.11
36 6.5e-03 4.3e-01 2.2e-02 9.83e-01 1.016200938e+01 1.019758577e+01 5.9e-06 0.11
37 5.9e-03 4.1e-01 2.0e-02 9.85e-01 1.016489687e+01 1.019694087e+01 5.4e-06 0.12
38 5.3e-03 3.8e-01 1.8e-02 9.86e-01 1.016749968e+01 1.019635962e+01 4.8e-06 0.12
39 4.8e-03 3.6e-01 1.6e-02 9.88e-01 1.016984564e+01 1.019583595e+01 4.3e-06 0.12
40 4.3e-03 3.5e-01 1.4e-02 9.89e-01 1.017195993e+01 1.019536434e+01 3.9e-06 0.12
41 3.9e-03 3.3e-01 1.3e-02 9.90e-01 1.017386526e+01 1.019493976e+01 3.5e-06 0.13
42 3.5e-03 3.1e-01 1.2e-02 9.91e-01 1.017558217e+01 1.019455764e+01 3.2e-06 0.13
43 3.1e-03 3.0e-01 1.1e-02 9.92e-01 1.017712917e+01 1.019421381e+01 2.8e-06 0.13
44 2.8e-03 2.9e-01 9.5e-03 9.93e-01 1.017852297e+01 1.019390451e+01 2.6e-06 0.13
45 2.5e-03 2.8e-01 8.5e-03 9.94e-01 1.017977867e+01 1.019362629e+01 2.3e-06 0.13
46 2.3e-03 2.7e-01 7.7e-03 9.95e-01 1.018090985e+01 1.019337608e+01 2.1e-06 0.14
47 2.1e-03 2.6e-01 6.9e-03 9.95e-01 1.018192881e+01 1.019315107e+01 1.9e-06 0.14
48 1.8e-03 2.5e-01 6.2e-03 9.96e-01 1.018284660e+01 1.019294872e+01 1.7e-06 0.14
49 1.7e-03 2.4e-01 5.6e-03 9.96e-01 1.018367323e+01 1.019276678e+01 1.5e-06 0.14
50 1.5e-03 2.4e-01 5.0e-03 9.97e-01 1.018441770e+01 1.019260318e+01 1.4e-06 0.15
51 1.3e-03 2.3e-01 4.5e-03 9.97e-01 1.018508816e+01 1.019245608e+01 1.2e-06 0.15
52 1.2e-03 2.3e-01 4.1e-03 9.98e-01 1.018569193e+01 1.019232382e+01 1.1e-06 0.15
53 1.1e-03 2.2e-01 3.7e-03 9.98e-01 1.018623562e+01 1.019220491e+01 9.9e-07 0.15
54 9.8e-04 2.2e-01 3.3e-03 9.98e-01 1.018672520e+01 1.019209802e+01 8.9e-07 0.16
55 8.8e-04 2.1e-01 3.0e-03 9.98e-01 1.018716605e+01 1.019200193e+01 8.1e-07 0.16
56 7.9e-04 2.1e-01 2.7e-03 9.99e-01 1.018756301e+01 1.019191556e+01 7.2e-07 0.16
57 7.2e-04 2.1e-01 2.4e-03 9.99e-01 1.018792045e+01 1.019183793e+01 6.5e-07 0.16
58 6.4e-04 2.0e-01 2.2e-03 9.99e-01 1.018824231e+01 1.019176817e+01 5.9e-07 0.16
59 5.8e-04 2.0e-01 1.9e-03 9.99e-01 1.018853212e+01 1.019170549e+01 5.3e-07 0.17
60 5.2e-04 2.0e-01 1.8e-03 1.00e+00 1.018879308e+01 1.019164918e+01 4.8e-07 0.17
61 4.7e-04 2.0e-01 1.6e-03 1.00e+00 1.018902806e+01 1.019159860e+01 4.3e-07 0.17
62 4.2e-04 1.9e-01 1.4e-03 1.00e+00 1.018923964e+01 1.019155316e+01 3.9e-07 0.17
63 3.8e-04 1.9e-01 1.3e-03 1.00e+00 1.018943016e+01 1.019151234e+01 3.5e-07 0.18
64 3.4e-04 1.9e-01 1.2e-03 1.00e+00 1.018960172e+01 1.019147569e+01 3.1e-07 0.18
65 3.1e-04 1.9e-01 1.0e-03 1.00e+00 1.018975618e+01 1.019144276e+01 2.8e-07 0.18
66 2.8e-04 1.9e-01 9.3e-04 1.00e+00 1.018989527e+01 1.019141318e+01 2.5e-07 0.18
67 2.5e-04 1.9e-01 8.4e-04 1.00e+00 1.019002049e+01 1.019138661e+01 2.3e-07 0.19
68 2.2e-04 1.8e-01 7.6e-04 1.00e+00 1.019013324e+01 1.019136274e+01 2.0e-07 0.19
69 2.0e-04 1.8e-01 6.8e-04 1.00e+00 1.019023476e+01 1.019134129e+01 1.8e-07 0.19
70 1.8e-04 1.8e-01 6.1e-04 1.00e+00 1.019032616e+01 1.019132203e+01 1.7e-07 0.19
71 1.6e-04 1.8e-01 5.5e-04 1.00e+00 1.019040845e+01 1.019130472e+01 1.5e-07 0.19
72 1.5e-04 1.8e-01 5.0e-04 1.00e+00 1.019048254e+01 1.019128918e+01 1.3e-07 0.20
73 1.3e-04 1.8e-01 4.5e-04 1.00e+00 1.019054925e+01 1.019127522e+01 1.2e-07 0.20
74 1.2e-04 1.8e-01 4.0e-04 1.00e+00 1.019060931e+01 1.019126267e+01 1.1e-07 0.20
75 1.1e-04 1.8e-01 3.6e-04 1.00e+00 1.019066339e+01 1.019125140e+01 9.8e-08 0.20
76 9.7e-05 1.8e-01 3.3e-04 1.00e+00 1.019071208e+01 1.019124128e+01 8.8e-08 0.21
77 8.7e-05 1.8e-01 2.9e-04 1.00e+00 1.019075592e+01 1.019123220e+01 7.9e-08 0.21
78 7.8e-05 1.8e-01 2.6e-04 1.00e+00 1.019079539e+01 1.019122403e+01 7.1e-08 0.21
79 7.0e-05 1.8e-01 2.4e-04 1.00e+00 1.019083093e+01 1.019121670e+01 6.4e-08 0.22
80 6.3e-05 1.8e-01 2.1e-04 1.00e+00 1.019086293e+01 1.019121012e+01 5.8e-08 0.22
81 5.7e-05 1.8e-01 1.9e-04 1.00e+00 1.019089174e+01 1.019120421e+01 5.2e-08 0.22
82 5.1e-05 1.8e-01 1.7e-04 1.00e+00 1.019091768e+01 1.019119890e+01 4.7e-08 0.22
83 4.6e-05 1.8e-01 1.6e-04 1.00e+00 1.019094104e+01 1.019119413e+01 4.2e-08 0.23
84 4.2e-05 1.8e-01 1.4e-04 1.00e+00 1.019096207e+01 1.019118985e+01 3.8e-08 0.23
85 3.7e-05 1.8e-01 1.3e-04 1.00e+00 1.019098100e+01 1.019118600e+01 3.4e-08 0.23
86 3.4e-05 1.8e-01 1.1e-04 1.00e+00 1.019099805e+01 1.019118255e+01 3.1e-08 0.23
87 3.0e-05 1.7e-01 1.0e-04 1.00e+00 1.019101339e+01 1.019117944e+01 2.8e-08 0.23
88 2.7e-05 1.7e-01 9.2e-05 1.00e+00 1.019102721e+01 1.019117665e+01 2.5e-08 0.24
89 2.5e-05 1.7e-01 8.3e-05 1.00e+00 1.019103965e+01 1.019117415e+01 2.2e-08 0.24
90 2.2e-05 1.7e-01 7.4e-05 1.00e+00 1.019105085e+01 1.019117189e+01 2.0e-08 0.24
91 2.0e-05 1.7e-01 6.7e-05 1.00e+00 1.019106092e+01 1.019116987e+01 1.8e-08 0.24
92 1.8e-05 1.7e-01 6.0e-05 1.00e+00 1.019107000e+01 1.019116804e+01 1.6e-08 0.25
93 1.6e-05 1.7e-01 5.4e-05 1.00e+00 1.019107817e+01 1.019116641e+01 1.5e-08 0.25
94 1.4e-05 1.7e-01 4.9e-05 1.00e+00 1.019108552e+01 1.019116493e+01 1.3e-08 0.25
95 1.3e-05 1.7e-01 4.4e-05 1.00e+00 1.019109214e+01 1.019116361e+01 1.2e-08 0.25
96 1.2e-05 1.7e-01 4.0e-05 1.00e+00 1.019109809e+01 1.019116242e+01 1.1e-08 0.26
97 1.1e-05 1.7e-01 3.6e-05 1.00e+00 1.019110346e+01 1.019116135e+01 9.7e-09 0.26
98 9.5e-06 1.7e-01 3.2e-05 1.00e+00 1.019110828e+01 1.019116039e+01 8.7e-09 0.26
99 8.6e-06 1.7e-01 2.9e-05 1.00e+00 1.019111263e+01 1.019115952e+01 7.8e-09 0.26
100 7.7e-06 1.7e-01 2.6e-05 1.00e+00 1.019111654e+01 1.019115874e+01 7.0e-09 0.26
101 6.9e-06 1.7e-01 2.3e-05 1.00e+00 1.019112006e+01 1.019115804e+01 6.3e-09 0.27
102 6.2e-06 1.7e-01 2.1e-05 1.00e+00 1.019112323e+01 1.019115741e+01 5.7e-09 0.27
103 5.6e-06 1.7e-01 1.9e-05 1.00e+00 1.019112608e+01 1.019115685e+01 5.1e-09 0.27
104 5.1e-06 1.7e-01 1.7e-05 1.00e+00 1.019112865e+01 1.019115634e+01 4.6e-09 0.27
105 4.5e-06 1.7e-01 1.5e-05 1.00e+00 1.019113096e+01 1.019115588e+01 4.2e-09 0.28
106 4.1e-06 1.7e-01 1.4e-05 1.00e+00 1.019113304e+01 1.019115546e+01 3.7e-09 0.28
107 3.7e-06 1.7e-01 1.2e-05 1.00e+00 1.019113491e+01 1.019115509e+01 3.4e-09 0.28
108 3.3e-06 1.7e-01 1.1e-05 1.00e+00 1.019113659e+01 1.019115476e+01 3.0e-09 0.28
109 3.0e-06 1.7e-01 1.0e-05 1.00e+00 1.019113811e+01 1.019115446e+01 2.7e-09 0.28
110 2.7e-06 1.7e-01 9.0e-06 1.00e+00 1.019113948e+01 1.019115419e+01 2.5e-09 0.29
111 2.4e-06 1.7e-01 8.1e-06 1.00e+00 1.019114070e+01 1.019115395e+01 2.2e-09 0.29
112 2.2e-06 1.7e-01 7.3e-06 9.99e-01 1.019114181e+01 1.019115373e+01 2.0e-09 0.29
113 2.0e-06 1.7e-01 6.6e-06 1.00e+00 1.019114280e+01 1.019115353e+01 1.8e-09 0.29
114 1.8e-06 1.7e-01 5.9e-06 9.99e-01 1.019114370e+01 1.019115336e+01 1.6e-09 0.30
115 1.6e-06 1.7e-01 5.3e-06 1.00e+00 1.019114451e+01 1.019115320e+01 1.4e-09 0.30
116 1.4e-06 1.7e-01 4.8e-06 1.00e+00 1.019114523e+01 1.019115305e+01 1.3e-09 0.30
117 1.3e-06 1.7e-01 4.3e-06 1.00e+00 1.019114589e+01 1.019115292e+01 1.2e-09 0.30
118 1.2e-06 1.5e-01 3.9e-06 1.00e+00 1.019114647e+01 1.019115281e+01 1.1e-09 0.31
119 1.0e-06 1.4e-01 3.5e-06 1.00e+00 1.019114700e+01 1.019115270e+01 9.5e-10 0.31
120 9.4e-07 1.3e-01 3.2e-06 1.00e+00 1.019114748e+01 1.019115261e+01 8.6e-10 0.31
121 8.4e-07 1.1e-01 2.8e-06 1.00e+00 1.019114791e+01 1.019115252e+01 7.7e-10 0.31
122 7.6e-07 1.0e-01 2.6e-06 1.00e+00 1.019114830e+01 1.019115245e+01 6.9e-10 0.31
123 6.8e-07 9.1e-02 2.3e-06 1.00e+00 1.019114865e+01 1.019115238e+01 6.2e-10 0.32
124 6.1e-07 8.2e-02 2.1e-06 1.00e+00 1.019114896e+01 1.019115232e+01 5.6e-10 0.32
125 5.5e-07 7.4e-02 1.9e-06 1.00e+00 1.019114924e+01 1.019115226e+01 5.1e-10 0.32
126 5.0e-07 6.7e-02 1.7e-06 1.00e+00 1.019114949e+01 1.019115221e+01 4.6e-10 0.32
127 4.5e-07 6.0e-02 1.5e-06 9.99e-01 1.019114972e+01 1.019115217e+01 4.1e-10 0.33
128 4.0e-07 5.4e-02 1.4e-06 9.97e-01 1.019114992e+01 1.019115213e+01 3.7e-10 0.33
129 3.6e-07 4.9e-02 1.2e-06 9.98e-01 1.019115011e+01 1.019115209e+01 3.3e-10 0.33
130 3.3e-07 4.4e-02 1.1e-06 1.00e+00 1.019115027e+01 1.019115206e+01 3.0e-10 0.33
131 2.9e-07 3.9e-02 9.9e-07 9.94e-01 1.019115042e+01 1.019115203e+01 2.7e-10 0.33
132 2.6e-07 3.5e-02 8.9e-07 1.00e+00 1.019115056e+01 1.019115200e+01 2.4e-10 0.34
133 2.4e-07 3.2e-02 8.0e-07 1.00e+00 1.019115068e+01 1.019115198e+01 2.2e-10 0.34
134 2.1e-07 2.9e-02 7.2e-07 1.00e+00 1.019115079e+01 1.019115196e+01 2.0e-10 0.34
135 1.9e-07 2.6e-02 6.5e-07 1.01e+00 1.019115089e+01 1.019115194e+01 1.8e-10 0.34
136 1.7e-07 2.3e-02 5.8e-07 9.87e-01 1.019115098e+01 1.019115192e+01 1.6e-10 0.35
137 1.6e-07 2.1e-02 5.3e-07 1.00e+00 1.019115106e+01 1.019115191e+01 1.4e-10 0.35
138 1.4e-07 1.9e-02 4.7e-07 9.84e-01 1.019115113e+01 1.019115189e+01 1.3e-10 0.35
139 1.3e-07 1.7e-02 4.3e-07 9.97e-01 1.019115119e+01 1.019115188e+01 1.2e-10 0.35
140 7.3e-09 9.6e-04 2.4e-08 9.87e-01 1.019115173e+01 1.019115177e+01 7.5e-12 0.36
141 2.9e-09 2.0e-04 5.1e-09 1.19e+00 1.019115176e+01 1.019115177e+01 1.0e-12 0.36
142 2.6e-09 1.8e-04 4.6e-09 1.02e+00 1.019115176e+01 1.019115177e+01 9.5e-13 0.36
Interior-point optimizer terminated. Time: 0.36.
Optimizer terminated. Time: 0.38
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0191151761e+01 Viol. con: 3e-09 var: 0e+00
Dual. obj: 1.0191151767e+01 Viol. con: 0e+00 var: 5e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.398 seconds.
result packing took 41% of solve time
solution checking took 11% of solve time
Using solver 'mosek'
Solving for 2480 variables.
Warning: The variable with index '1860' has only negative coefficients akj.
The problem is possibly ill-posed.
Number of Hessian non-zeros: 1090
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Linux/64-X86
Cores : 20
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2481
Cones : 0
Scalar variables : 5898
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 : 1026
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1043
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1043
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 : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 286
Optimizer - Cones : 0
Optimizer - Scalar variables : 995 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.01 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 6557 after factor : 1.08e+04
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 2.5e+03 3.8e+03 7.7e+03 0.00e+00 -7.710634220e+03 1.023181539e-12 1.0e+00 0.03
1 7.9e+02 1.2e+03 2.4e+03 -1.02e-03 -3.455815945e+03 9.887470596e+00 3.4e-01 0.03
2 5.9e+02 8.8e+02 1.8e+03 1.40e+00 -2.233542381e+03 1.170313454e+01 2.5e-01 0.03
3 3.6e+02 5.3e+02 1.1e+03 1.45e+00 -1.157854744e+03 1.326814366e+01 1.6e-01 0.03
4 1.2e+02 1.8e+02 3.8e+02 1.58e+00 -2.954607854e+02 1.395262476e+01 5.6e-02 0.04
5 3.9e+01 6.0e+01 1.2e+02 1.45e+00 -7.301391020e+01 1.289187307e+01 1.9e-02 0.04
6 9.7e+00 2.0e+01 3.0e+01 1.14e+00 -8.862040243e+00 1.133464079e+01 5.4e-03 0.04
7 2.4e+00 1.5e+01 7.6e+00 1.01e+00 5.597954972e+00 1.067653110e+01 1.5e-03 0.04
8 2.2e+00 1.4e+01 7.0e+00 7.89e-01 5.808270981e+00 1.066015534e+01 1.4e-03 0.05
9 1.0e+00 9.8e+00 3.3e+00 7.43e-01 7.722054414e+00 1.051633281e+01 7.2e-04 0.05
10 8.0e-01 9.9e+00 2.6e+00 4.53e-01 8.056006368e+00 1.047012328e+01 5.6e-04 0.05
11 3.9e-01 6.6e+00 1.3e+00 4.91e-01 8.908550857e+00 1.036283695e+01 2.9e-04 0.06
12 2.8e-01 4.8e+00 9.2e-01 5.43e-01 9.174056521e+00 1.032567829e+01 2.1e-04 0.06
13 4.9e-02 4.0e+00 1.7e-01 6.16e-01 9.948200175e+00 1.021226765e+01 5.3e-05 0.06
14 1.5e-02 3.7e+00 5.3e-02 9.08e-01 1.010040305e+01 1.018375020e+01 1.7e-05 0.06
15 5.9e-03 3.4e+00 2.1e-02 9.80e-01 1.014208304e+01 1.017613383e+01 7.2e-06 0.07
16 1.4e-03 3.2e+00 5.0e-03 9.91e-01 1.016356048e+01 1.017158507e+01 1.7e-06 0.07
17 3.5e-04 3.2e+00 1.3e-03 9.97e-01 1.016855827e+01 1.017058435e+01 4.4e-07 0.07
18 8.7e-05 3.1e+00 3.2e-04 9.99e-01 1.016983601e+01 1.017034908e+01 1.1e-07 0.07
19 2.2e-05 2.9e+00 8.2e-05 9.99e-01 1.017015665e+01 1.017028719e+01 2.9e-08 0.08
20 2.0e-05 2.6e+00 7.4e-05 9.98e-01 1.017016683e+01 1.017028461e+01 2.6e-08 0.08
21 1.8e-05 2.4e+00 6.6e-05 9.98e-01 1.017017673e+01 1.017028276e+01 2.3e-08 0.08
22 1.6e-05 2.2e+00 6.0e-05 9.99e-01 1.017018567e+01 1.017028111e+01 2.1e-08 0.09
23 1.4e-05 2.0e+00 5.4e-05 9.99e-01 1.017019372e+01 1.017027962e+01 1.9e-08 0.09
24 1.3e-05 1.8e+00 4.8e-05 9.99e-01 1.017020097e+01 1.017027828e+01 1.7e-08 0.09
25 1.2e-05 1.6e+00 4.3e-05 1.00e+00 1.017020749e+01 1.017027708e+01 1.5e-08 0.09
26 1.1e-05 1.5e+00 3.9e-05 1.00e+00 1.017021336e+01 1.017027599e+01 1.4e-08 0.10
27 9.5e-06 1.4e+00 3.5e-05 1.00e+00 1.017021865e+01 1.017027501e+01 1.2e-08 0.10
28 8.5e-06 1.2e+00 3.2e-05 1.00e+00 1.017022341e+01 1.017027414e+01 1.1e-08 0.10
29 7.7e-06 1.1e+00 2.9e-05 1.00e+00 1.017022769e+01 1.017027334e+01 1.0e-08 0.10
30 6.9e-06 1.0e+00 2.6e-05 1.00e+00 1.017023154e+01 1.017027263e+01 9.1e-09 0.11
31 6.2e-06 9.5e-01 2.3e-05 1.00e+00 1.017023501e+01 1.017027199e+01 8.2e-09 0.11
32 5.6e-06 8.7e-01 2.1e-05 1.00e+00 1.017023813e+01 1.017027141e+01 7.4e-09 0.11
33 5.0e-06 8.0e-01 1.9e-05 1.00e+00 1.017024094e+01 1.017027090e+01 6.6e-09 0.11
34 4.5e-06 7.4e-01 1.7e-05 1.00e+00 1.017024347e+01 1.017027043e+01 6.0e-09 0.12
35 4.1e-06 6.8e-01 1.5e-05 1.00e+00 1.017024574e+01 1.017027001e+01 5.4e-09 0.12
36 3.7e-06 6.3e-01 1.4e-05 1.00e+00 1.017024779e+01 1.017026963e+01 4.8e-09 0.12
37 3.3e-06 5.9e-01 1.2e-05 1.00e+00 1.017024964e+01 1.017026929e+01 4.4e-09 0.12
38 3.0e-06 5.5e-01 1.1e-05 1.00e+00 1.017025129e+01 1.017026898e+01 3.9e-09 0.13
39 2.7e-06 5.1e-01 9.9e-06 1.00e+00 1.017025279e+01 1.017026871e+01 3.5e-09 0.13
40 2.4e-06 4.8e-01 8.9e-06 1.00e+00 1.017025413e+01 1.017026846e+01 3.2e-09 0.13
41 2.2e-06 4.5e-01 8.1e-06 1.00e+00 1.017025534e+01 1.017026823e+01 2.9e-09 0.13
42 2.0e-06 4.2e-01 7.2e-06 9.99e-01 1.017025643e+01 1.017026803e+01 2.6e-09 0.14
43 1.8e-06 4.0e-01 6.5e-06 1.00e+00 1.017025741e+01 1.017026785e+01 2.3e-09 0.14
44 1.6e-06 3.7e-01 5.9e-06 1.00e+00 1.017025829e+01 1.017026769e+01 2.1e-09 0.14
45 1.4e-06 3.5e-01 5.3e-06 9.99e-01 1.017025908e+01 1.017026754e+01 1.9e-09 0.14
46 1.3e-06 3.4e-01 4.8e-06 9.98e-01 1.017025980e+01 1.017026741e+01 1.7e-09 0.15
47 1.2e-06 3.2e-01 4.3e-06 1.00e+00 1.017026044e+01 1.017026729e+01 1.5e-09 0.15
48 1.0e-06 3.1e-01 3.9e-06 1.00e+00 1.017026102e+01 1.017026718e+01 1.4e-09 0.15
49 9.3e-07 2.9e-01 3.5e-06 9.98e-01 1.017026154e+01 1.017026709e+01 1.2e-09 0.15
50 8.4e-07 2.8e-01 3.1e-06 1.00e+00 1.017026201e+01 1.017026700e+01 1.1e-09 0.16
51 7.6e-07 2.7e-01 2.8e-06 1.00e+00 1.017026243e+01 1.017026692e+01 1.0e-09 0.16
52 6.8e-07 2.6e-01 2.5e-06 9.99e-01 1.017026281e+01 1.017026685e+01 9.0e-10 0.16
53 6.1e-07 2.5e-01 2.3e-06 9.96e-01 1.017026315e+01 1.017026679e+01 8.1e-10 0.16
54 5.5e-07 2.5e-01 2.0e-06 9.95e-01 1.017026345e+01 1.017026673e+01 7.3e-10 0.17
55 5.0e-07 2.4e-01 1.8e-06 1.01e+00 1.017026373e+01 1.017026668e+01 6.5e-10 0.17
56 4.5e-07 2.3e-01 1.7e-06 1.00e+00 1.017026398e+01 1.017026663e+01 5.9e-10 0.17
57 4.0e-07 2.3e-01 1.5e-06 9.97e-01 1.017026421e+01 1.017026659e+01 5.3e-10 0.17
58 3.6e-07 2.2e-01 1.3e-06 1.00e+00 1.017026441e+01 1.017026655e+01 4.8e-10 0.17
59 3.3e-07 2.2e-01 1.2e-06 9.93e-01 1.017026459e+01 1.017026652e+01 4.3e-10 0.18
60 2.9e-07 2.2e-01 1.1e-06 9.96e-01 1.017026475e+01 1.017026649e+01 3.9e-10 0.18
61 2.6e-07 2.1e-01 9.8e-07 9.95e-01 1.017026490e+01 1.017026646e+01 3.5e-10 0.18
62 2.4e-07 2.1e-01 8.8e-07 9.86e-01 1.017026503e+01 1.017026644e+01 3.1e-10 0.18
63 2.1e-07 2.0e-01 7.9e-07 9.90e-01 1.017026515e+01 1.017026642e+01 2.8e-10 0.19
64 1.9e-07 2.0e-01 7.1e-07 1.00e+00 1.017026525e+01 1.017026640e+01 2.5e-10 0.19
65 1.7e-07 2.0e-01 6.4e-07 1.00e+00 1.017026535e+01 1.017026638e+01 2.3e-10 0.19
66 3.7e-08 4.3e-02 1.4e-07 1.02e+00 1.017026603e+01 1.017026625e+01 4.8e-11 0.19
67 4.3e-09 5.0e-03 1.6e-08 9.82e-01 1.017026620e+01 1.017026622e+01 5.8e-12 0.20
68 4.2e-10 4.6e-04 1.5e-09 8.71e-01 1.017026622e+01 1.017026622e+01 4.8e-13 0.20
Interior-point optimizer terminated. Time: 0.20.
Optimizer terminated. Time: 0.22
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0170266216e+01 Viol. con: 4e-10 var: 0e+00
Dual. obj: 1.0170266218e+01 Viol. con: 0e+00 var: 1e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.237 seconds.
result packing took 72% of solve time
solution checking took 22% of solve time
Using solver 'mosek'
Solving for 2480 variables.
Warning: The variable with index '1860' has only negative coefficients akj.
The problem is possibly ill-posed.
Number of Hessian non-zeros: 1090
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Linux/64-X86
Cores : 20
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2481
Cones : 0
Scalar variables : 5898
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 : 1026
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1041
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1041
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 : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 286
Optimizer - Cones : 0
Optimizer - Scalar variables : 995 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.01 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 6557 after factor : 1.08e+04
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 2.6e+03 3.8e+03 7.7e+03 0.00e+00 -7.721659731e+03 1.023181539e-12 1.0e+00 0.03
1 7.9e+02 1.2e+03 2.4e+03 -2.26e-03 -3.459676508e+03 9.890412880e+00 3.4e-01 0.03
2 5.9e+02 8.8e+02 1.8e+03 1.40e+00 -2.229481946e+03 1.171399325e+01 2.5e-01 0.03
3 3.8e+02 5.6e+02 1.2e+03 1.45e+00 -1.236908325e+03 1.314739668e+01 1.6e-01 0.03
4 1.3e+02 2.0e+02 4.0e+02 1.56e+00 -3.249937274e+02 1.397273356e+01 6.0e-02 0.04
5 4.2e+01 6.3e+01 1.3e+02 1.47e+00 -7.775435177e+01 1.298045810e+01 2.0e-02 0.04
6 1.1e+01 2.0e+01 3.4e+01 1.15e+00 -1.121602622e+01 1.141512060e+01 6.0e-03 0.04
7 2.4e+00 1.5e+01 7.6e+00 1.02e+00 5.607856891e+00 1.067191866e+01 1.5e-03 0.04
8 2.2e+00 1.4e+01 7.1e+00 7.87e-01 5.805630778e+00 1.065684992e+01 1.4e-03 0.05
9 1.1e+00 9.6e+00 3.5e+00 7.42e-01 7.632598545e+00 1.052164168e+01 7.5e-04 0.05
10 1.0e+00 9.2e+00 3.3e+00 4.62e-01 7.565678775e+00 1.051356252e+01 7.2e-04 0.05
11 3.9e-01 6.8e+00 1.3e+00 5.15e-01 8.911386501e+00 1.036015859e+01 3.0e-04 0.06
12 2.8e-01 4.9e+00 9.1e-01 5.59e-01 9.187032974e+00 1.032242948e+01 2.2e-04 0.06
13 4.6e-02 4.2e+00 1.6e-01 6.42e-01 9.960825529e+00 1.020958460e+01 5.2e-05 0.06
14 1.4e-02 3.9e+00 5.2e-02 9.15e-01 1.010227821e+01 1.018331196e+01 1.8e-05 0.06
15 5.5e-03 3.6e+00 2.0e-02 9.80e-01 1.014380142e+01 1.017568022e+01 7.0e-06 0.07
16 1.2e-03 3.4e+00 4.4e-03 9.91e-01 1.016437084e+01 1.017127236e+01 1.6e-06 0.07
17 2.7e-04 3.4e+00 1.0e-03 9.97e-01 1.016879808e+01 1.017037997e+01 3.6e-07 0.07
18 6.2e-05 3.2e+00 2.3e-04 9.99e-01 1.016982391e+01 1.017018980e+01 8.5e-08 0.07
19 1.5e-05 3.0e+00 5.7e-05 9.99e-01 1.017005490e+01 1.017014539e+01 2.1e-08 0.08
20 1.4e-05 2.7e+00 5.2e-05 9.99e-01 1.017006192e+01 1.017014358e+01 1.9e-08 0.08
21 1.2e-05 2.5e+00 4.6e-05 9.99e-01 1.017006879e+01 1.017014231e+01 1.7e-08 0.08
22 1.1e-05 2.2e+00 4.2e-05 9.99e-01 1.017007499e+01 1.017014116e+01 1.5e-08 0.08
23 1.0e-05 2.0e+00 3.8e-05 1.00e+00 1.017008057e+01 1.017014012e+01 1.4e-08 0.09
24 9.0e-06 1.8e+00 3.4e-05 1.00e+00 1.017008559e+01 1.017013919e+01 1.3e-08 0.09
25 8.1e-06 1.7e+00 3.0e-05 1.00e+00 1.017009011e+01 1.017013835e+01 1.1e-08 0.09
26 7.3e-06 1.5e+00 2.7e-05 1.00e+00 1.017009418e+01 1.017013759e+01 1.0e-08 0.09
27 6.5e-06 1.4e+00 2.5e-05 1.00e+00 1.017009784e+01 1.017013691e+01 9.1e-09 0.10
28 5.9e-06 1.3e+00 2.2e-05 1.00e+00 1.017010113e+01 1.017013630e+01 8.2e-09 0.10
29 5.3e-06 1.2e+00 2.0e-05 1.00e+00 1.017010410e+01 1.017013575e+01 7.4e-09 0.10
30 4.8e-06 1.1e+00 1.8e-05 1.00e+00 1.017010677e+01 1.017013525e+01 6.6e-09 0.10
31 4.3e-06 9.7e-01 1.6e-05 1.00e+00 1.017010917e+01 1.017013481e+01 6.0e-09 0.11
32 3.9e-06 8.9e-01 1.5e-05 1.00e+00 1.017011133e+01 1.017013441e+01 5.4e-09 0.11
33 3.5e-06 8.2e-01 1.3e-05 1.00e+00 1.017011328e+01 1.017013404e+01 4.8e-09 0.11
34 3.1e-06 7.6e-01 1.2e-05 1.00e+00 1.017011503e+01 1.017013372e+01 4.4e-09 0.11
35 2.8e-06 7.0e-01 1.1e-05 1.00e+00 1.017011660e+01 1.017013343e+01 3.9e-09 0.12
36 2.5e-06 6.5e-01 9.5e-06 1.00e+00 1.017011802e+01 1.017013316e+01 3.5e-09 0.12
37 2.3e-06 6.0e-01 8.6e-06 1.00e+00 1.017011930e+01 1.017013292e+01 3.2e-09 0.12
38 2.1e-06 5.6e-01 7.7e-06 1.00e+00 1.017012045e+01 1.017013271e+01 2.9e-09 0.12
39 1.8e-06 5.2e-01 7.0e-06 1.00e+00 1.017012148e+01 1.017013252e+01 2.6e-09 0.13
40 1.7e-06 4.9e-01 6.3e-06 1.00e+00 1.017012241e+01 1.017013234e+01 2.3e-09 0.13
41 1.5e-06 4.6e-01 5.6e-06 1.00e+00 1.017012325e+01 1.017013219e+01 2.1e-09 0.13
42 1.3e-06 4.3e-01 5.1e-06 1.00e+00 1.017012400e+01 1.017013205e+01 1.9e-09 0.13
43 1.2e-06 4.0e-01 4.6e-06 1.00e+00 1.017012468e+01 1.017013192e+01 1.7e-09 0.14
44 1.1e-06 3.8e-01 4.1e-06 1.00e+00 1.017012529e+01 1.017013181e+01 1.5e-09 0.14
45 9.8e-07 3.6e-01 3.7e-06 1.00e+00 1.017012584e+01 1.017013171e+01 1.4e-09 0.14
46 8.8e-07 3.4e-01 3.3e-06 1.00e+00 1.017012634e+01 1.017013161e+01 1.2e-09 0.14
47 8.0e-07 3.3e-01 3.0e-06 9.99e-01 1.017012678e+01 1.017013153e+01 1.1e-09 0.15
48 7.2e-07 3.1e-01 2.7e-06 1.00e+00 1.017012718e+01 1.017013146e+01 1.0e-09 0.15
49 6.4e-07 3.0e-01 2.4e-06 1.00e+00 1.017012754e+01 1.017013139e+01 9.0e-10 0.15
50 5.8e-07 2.9e-01 2.2e-06 1.01e+00 1.017012787e+01 1.017013133e+01 8.1e-10 0.15
51 5.2e-07 2.8e-01 2.0e-06 1.00e+00 1.017012816e+01 1.017013127e+01 7.3e-10 0.16
52 4.7e-07 2.7e-01 1.8e-06 1.01e+00 1.017012843e+01 1.017013122e+01 6.6e-10 0.16
53 4.2e-07 2.6e-01 1.6e-06 1.00e+00 1.017012866e+01 1.017013118e+01 5.9e-10 0.16
54 3.8e-07 2.5e-01 1.4e-06 9.99e-01 1.017012887e+01 1.017013114e+01 5.3e-10 0.16
55 3.4e-07 2.4e-01 1.3e-06 9.94e-01 1.017012906e+01 1.017013110e+01 4.8e-10 0.17
56 3.1e-07 2.4e-01 1.2e-06 9.97e-01 1.017012924e+01 1.017013107e+01 4.3e-10 0.17
57 2.8e-07 2.3e-01 1.0e-06 1.00e+00 1.017012939e+01 1.017013104e+01 3.9e-10 0.17
58 2.5e-07 2.3e-01 9.4e-07 9.91e-01 1.017012953e+01 1.017013102e+01 3.5e-10 0.17
59 2.2e-07 2.2e-01 8.5e-07 9.94e-01 1.017012965e+01 1.017013099e+01 3.1e-10 0.18
60 2.0e-07 2.2e-01 7.6e-07 1.00e+00 1.017012977e+01 1.017013097e+01 2.8e-10 0.18
61 1.8e-07 2.1e-01 6.9e-07 9.82e-01 1.017012987e+01 1.017013095e+01 2.5e-10 0.18
62 1.6e-07 1.9e-01 6.2e-07 1.02e+00 1.017012997e+01 1.017013093e+01 2.3e-10 0.18
63 1.5e-07 1.9e-01 5.6e-07 1.00e+00 1.017013005e+01 1.017013092e+01 2.1e-10 0.19
64 1.3e-07 1.7e-01 5.0e-07 1.01e+00 1.017013012e+01 1.017013091e+01 1.9e-10 0.19
65 1.2e-07 1.5e-01 4.5e-07 1.00e+00 1.017013019e+01 1.017013089e+01 1.7e-10 0.19
66 1.1e-07 1.4e-01 4.0e-07 9.99e-01 1.017013025e+01 1.017013088e+01 1.5e-10 0.19
67 9.7e-08 1.3e-01 3.6e-07 9.89e-01 1.017013030e+01 1.017013087e+01 1.4e-10 0.20
68 8.7e-08 1.1e-01 3.3e-07 9.85e-01 1.017013035e+01 1.017013086e+01 1.2e-10 0.20
69 7.8e-08 1.0e-01 3.0e-07 1.04e+00 1.017013040e+01 1.017013085e+01 1.1e-10 0.20
70 7.0e-08 9.1e-02 2.7e-07 1.01e+00 1.017013044e+01 1.017013085e+01 1.0e-10 0.20
71 6.3e-08 8.2e-02 2.4e-07 9.81e-01 1.017013047e+01 1.017013084e+01 9.2e-11 0.20
72 5.7e-08 7.4e-02 2.2e-07 1.03e+00 1.017013051e+01 1.017013083e+01 8.4e-11 0.21
73 5.1e-08 6.7e-02 1.9e-07 9.98e-01 1.017013054e+01 1.017013083e+01 7.5e-11 0.21
74 3.2e-09 3.7e-03 1.1e-08 9.78e-01 1.017013077e+01 1.017013079e+01 4.8e-12 0.21
75 2.7e-10 2.5e-04 7.5e-10 9.58e-01 1.017013078e+01 1.017013078e+01 3.9e-13 0.21
Interior-point optimizer terminated. Time: 0.22.
Optimizer terminated. Time: 0.23
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0170130781e+01 Viol. con: 2e-10 var: 0e+00
Dual. obj: 1.0170130782e+01 Viol. con: 0e+00 var: 7e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.252 seconds.
result packing took 70% of solve time
solution checking took 32% of solve time
Solving took 5 GP solves and 4.08 seconds.
Warning: Constraint [W_{total}_FleetMission_(0,) [N]... >= W_{dry}_FleetMission_(0,) + W_{f_{total}}_FleetMission_(0,) [N]...] is not tight because the left hand side evaluated to 366641.67789 newton but the right hand side evaluated to 366630.066125 newton (Allowable error: 0.0001%, Actual error: 0.0032%)
Warning: Constraint [W_{total}_FleetMission_(1,) [N]... >= W_{dry}_FleetMission_(1,) + W_{f_{total}}_FleetMission_(1,) [N]...] is not tight because the left hand side evaluated to 377162.191853 newton but the right hand side evaluated to 377115.44116 newton (Allowable error: 0.0001%, Actual error: 0.012%)
Warning: Constraint [W_{total}_FleetMission_(2,) [N]... >= W_{dry}_FleetMission_(2,) + W_{f_{total}}_FleetMission_(2,) [N]...] is not tight because the left hand side evaluated to 388105.090227 newton but the right hand side evaluated to 387998.859838 newton (Allowable error: 0.0001%, Actual error: 0.027%)
Warning: Constraint [W_{total}_FleetMission_(3,) [N]... >= W_{dry}_FleetMission_(3,) + W_{f_{total}}_FleetMission_(3,) [N]...] is not tight because the left hand side evaluated to 399470.24438 newton but the right hand side evaluated to 399279.093125 newton (Allowable error: 0.0001%, Actual error: 0.048%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 361212.193996 newton but the right hand side evaluated to 361206.369374 newton (Allowable error: 0.0001%, Actual error: 0.0016%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 1) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 1) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 371522.140637 newton but the right hand side evaluated to 371498.54413 newton (Allowable error: 0.0001%, Actual error: 0.0064%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 2) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 2) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 382190.30622 newton but the right hand side evaluated to 382135.967862 newton (Allowable error: 0.0001%, Actual error: 0.014%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 3) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(0, 3) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 393255.643013 newton but the right hand side evaluated to 393156.477829 newton (Allowable error: 0.0001%, Actual error: 0.025%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 356181.886604 newton but the right hand side evaluated to 356176.09949 newton (Allowable error: 0.0001%, Actual error: 0.0016%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 1) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 1) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 361243.203585 newton but the right hand side evaluated to 361220.049425 newton (Allowable error: 0.0001%, Actual error: 0.0064%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 2) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 2) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 366354.225061 newton but the right hand side evaluated to 366302.333104 newton (Allowable error: 0.0001%, Actual error: 0.014%)
Warning: Constraint [W_{start}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 3) [N]... >= W_{burn}_FleetMission/CruiseSegment/CruiseP/AircraftP.1_(1, 3) + W_{end}_FleetMission/CruiseSegment/...] is not tight because the left hand side evaluated to 371535.454885 newton but the right hand side evaluated to 371443.468883 newton (Allowable error: 0.0001%, Actual error: 0.025%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) [N]...] is not tight because the left hand side evaluated to 18366.9602629 newton but the right hand side evaluated to 18366.7174583 newton (Allowable error: 0.0001%, Actual error: 0.0013%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 1) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 1) [N]...] is not tight because the left hand side evaluated to 18344.4541318 newton but the right hand side evaluated to 18344.2047991 newton (Allowable error: 0.0001%, Actual error: 0.0014%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 2) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 2) [N]...] is not tight because the left hand side evaluated to 18344.4540797 newton but the right hand side evaluated to 18344.2047169 newton (Allowable error: 0.0001%, Actual error: 0.0014%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 3) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 3) [N]...] is not tight because the left hand side evaluated to 18344.45410..27 newton but the right hand side evaluated to 18344.2047385 newton (Allowable error: 0.0001%, Actual error: 0.0014%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) [N]...] is not tight because the left hand side evaluated to 18924.2850642 newton but the right hand side evaluated to 18924.2645771 newton (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 2) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 2) [N]...] is not tight because the left hand side evaluated to 8445.89963188 newton but the right hand side evaluated to 8445.84799981 newton (Allowable error: 0.0001%, Actual error: 0.00061%)
Warning: Constraint [F_{6}_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 3) + F_{8}_FleetMission/A... >= F_FleetMission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(2, 3) [N]...] is not tight because the left hand side evaluated to 8626.29336319 newton but the right hand side evaluated to 8626.24784534 newton (Allowable error: 0.0001%, Actual error: 0.00053%)
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%)
Warning: Constraint [2*h_{t_8}_Engine/EnginePerformance/ThrustPerformance_(0,) [J/kg]... >= 2*h_{8}_Engine/EnginePerformance/ThrustPerformance_(0,) + u_{8}_Engine/EnginePerformance/ThrustPerfo...] is not tight because the left hand side evaluated to 589044.599547 joule / kilogram but the right hand side evaluated to 589043.979375 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Constraint [2*h_{t_8}_Engine/EnginePerformance/ThrustPerformance_(1,) [J/kg]... >= 2*h_{8}_Engine/EnginePerformance/ThrustPerformance_(1,) + u_{8}_Engine/EnginePerformance/ThrustPerfo...] is not tight because the left hand side evaluated to 591115.778885 joule / kilogram but the right hand side evaluated to 591111.945235 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00065%)
Warning: Constraint [2*h_{t_6}_Engine/EnginePerformance/ThrustPerformance_(0,) [J/kg]... >= 2*h_6_Engine/EnginePerformance/ThrustPerformance_(0,) + u_{6}_Engine/EnginePerformance/ThrustPerform...] is not tight because the left hand side evaluated to 956319.346357 joule / kilogram but the right hand side evaluated to 956318.172744 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%)
Warning: Constraint [2*h_{t_6}_Engine/EnginePerformance/ThrustPerformance_(1,) [J/kg]... >= 2*h_6_Engine/EnginePerformance/ThrustPerformance_(1,) + u_{6}_Engine/EnginePerformance/ThrustPerform...] is not tight because the left hand side evaluated to 1001778.20172 joule / kilogram but the right hand side evaluated to 1001774.61731 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00036%)
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 24184.7513167 newton but the right hand side evaluated to 24184.0837624 newton (Allowable error: 0.0001%, Actual error: 0.0028%)
Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerf.
----------------------------------------------------------------------
Ran 4 tests in 22.195s
OK
Generating XML reports...
ormance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.855488 newton but the right hand side evaluated to 26232.3851273 newton (Allowable error: 0.0001%, Actual error: 0.0018%)
Cloning into 'gassolar'...
Cannot uninstall requirement gassolar, not installed
Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gassolar
Installing collected packages: gassolar
Running setup.py develop for gassolar
Successfully installed gassolar
From https://github.com/convexengineering/gpkit-models
* branch master -> FETCH_HEAD
HEAD is now at 11cee6a... ipynb2module is a tool for importing jupyter notebooks as modules (#116)
Cannot uninstall requirement gpkit-models, not installed
Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit-models
Installing collected packages: gpkitmodels
Found existing installation: gpkitmodels 0.0.0.0
Uninstalling gpkitmodels-0.0.0.0:
Successfully uninstalled gpkitmodels-0.0.0.0
Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels
Requirement already satisfied: pandas in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas)
Requirement already satisfied: python-dateutil in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas)
Requirement already satisfied: numpy>=1.7.0 in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas)
Requirement already satisfied: six>=1.5 in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas)
Collecting git+https://github.com/hoburg/gpfit.git
Cloning https://github.com/hoburg/gpfit.git to /tmp/pip-Wz9Om3-build
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1)
Requirement already satisfied: scipy in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1)
Requirement already satisfied: gpkit in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit (from gpfit==0.1)
Requirement already satisfied: pint in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1)
Running tests...
----------------------------------------------------------------------
...adding test for 'gassolar/gas/gas.py'
adding test for 'gassolar/gas/gas_simple/gassimple.py'
adding test for 'gassolar/solar/solar.py'
Using solver 'mosek'
Solving for 554 variables.
Solving took 0.23 seconds.
Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955
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
Using solver 'mosek'
Solving for 554 variables.
Solving took 0.222 seconds.
Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955
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
Using solver 'mosek'
Solving for 554 variables.
Solving took 0.202 seconds.
Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955
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
Using solver 'mosek_cli'
Solving for 554 variables.
Solving took 0.271 seconds.
Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955
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
Warning: Constraint [z_{bre}_Mission/Climb/FlightSegment/BreguetEndurance_(2,)... >= 4.02*BSFC_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(2,)*P_{total}_Mission/Climb/FlightSeg...] is not tight because the left hand side evaluated to 0.000749180961118 but the right hand side evaluated to 0.000749181778306 (Allowable error: 0.0001%, Actual error: 0.00011%)
Using solver 'mosek'
Solving for 79 variables.
Solving took 0.0471 seconds.
Using solver 'mosek_cli'
Solving for 79 variables.
Solving took 0.24 seconds.
Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(0,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(0,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.214978340025 but the right hand side evaluated to 0.214990343824 (Allowable error: 0.0001%, Actual error: 0.0056%)
Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(1,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(1,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.201770573866 but the right hand side evaluated to 0.201762873578 (Allowable error: 0.0001%, Actual error: 0.0038%)
Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(2,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(2,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.197669665026 but the right hand side evaluated to 0.197658958675 (Allowable error: 0.0001%, Actual error: 0.0054%)
Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(3,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(3,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.201770775637 but the right hand side evaluated to 0.201762873578 (Allowable error: 0.0001%, Actual error: 0.0039%)
Warning: Constraint [z_{bre}_Mission./jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gassolar/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
tau = np.exp(-0.175/costhsun)
..
----------------------------------------------------------------------
Ran 6 tests in 21.938s
OK
Generating XML reports...
/Loiter/FlightSegment/BreguetEndurance_(4,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(4,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.214978769982 but the right hand side evaluated to 0.214979594576 (Allowable error: 0.0001%, Actual error: 0.00038%)
Using solver 'mosek'
Solving for 1057 variables.
Solving took 0.344 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 135385.4203 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 135386.6378 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Beginning signomial solve.
Solving took 5 GP solves and 2.3 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 137254.6796 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 137255.9458 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Using solver 'mosek_cli'
Solving for 1057 variables.
Solving took 0.5 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 135385.2910 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 135386.6449 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Beginning signomial solve.
Solving took 5 GP solves and 3.78 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 137254.2055 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 137255.5780 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Cloning into 'SPaircraft'...
From https://github.com/convexengineering/gpkit-models
* branch master -> FETCH_HEAD
HEAD is now at 11cee6a... ipynb2module is a tool for importing jupyter notebooks as modules (#116)
Cannot uninstall requirement gpkit-models, not installed
Obtaining file:///jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit-models
Installing collected packages: gpkitmodels
Found existing installation: gpkitmodels 0.0.0.0
Uninstalling gpkitmodels-0.0.0.0:
Successfully uninstalled gpkitmodels-0.0.0.0
Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels
Collecting git+https://github.com/hoburg/turbofan.git
Cloning https://github.com/hoburg/turbofan.git to /tmp/pip-hqak6f-build
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/turbofan
Requirement already satisfied: numpy in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0)
Requirement already satisfied: scipy in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0)
Requirement already satisfied: pint in /jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0)
Running tests...
----------------------------------------------------------------------
adding test for 'SP_aircraft.py'
Beginning signomial solve.
Solving took 7 GP solves and 8.72 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 2427079.1154 force_pound * meter but the right hand side evaluated to 2397884.6535 force_pound * meter (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 2.21510116776 meter but the right hand side evaluated to 1.96471421268 meter (Allowable error: 0.1%, Actual error: 11%)
Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) [N]...] is not tight because the left hand side evaluated to 17472.580014 newton but the right hand side evaluated to 17443.247308 newton (Allowable error: 0.1%, Actual error: 0.17%)
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 1242117.37127 joule / kilogram but the right hand side evaluated to 1.48135516658 megajoule / kilogram (Allowable error: 0.1%, Actual error: 9.5%)
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 642471.583267 joule / kilogram but the right hand side evaluated to 0.643956081756 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.1%)
Warning: Constraint [W_{lg}_Mission/Aircraft/LandingGear*x_{CG_{lg}}_Mission/Aircraft/LandingGear [N*m]... >= W_{mg}_Mission/Aircraft/LandingGear*x_m_Mission/Aircraft/LandingGear + W_{ng}_Mission/Aircraft/Landi...] is not tight because the left hand side evaluated to 271789.676024 meter * newton but the right hand side evaluated to 263034.781643 meter * newton (Allowable error: 1.0%, Actual error: 3.3%)
Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.5759770413 meter but the right hand side evaluated to 16.6120344693 meter (Allowable error: 0.1%, Actual error: 12%)
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 10.9551731413 but the right hand side evaluated to 4.85819162885 (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 10.0069366754 but the right hand side evaluated to 4.8582018519 (Allowable error: 0.1%, Actual error: 51%)
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 8.21524805935 but the right hand side evaluated to 4.85820188787 (Allowable error: 0.1%, Actual error: 41%)
Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/C.ruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.6219893681 meter but the right hand side evaluated to 18.3758563273 meter (Allowable error: 0.1%, Actual error: 1.3%)
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 18.6219893681 meter but the right hand side evaluated to 18.4513094982 meter (Allowable error: 0.1%, Actual error: 0.92%)
Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.67771707402 but the right hand side evaluated to 4.79404513416 (Allowable error: 0.1%, Actual error: 2.4%)
Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.73113716496 but the right hand side evaluated to 4.81372998041 (Allowable error: 0.1%, Actual error: 1.7%)
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 7.60828434873 but the right hand side evaluated to 4.79404513416 (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 7.57970300197 but the right hand side evaluated to 4.81372998041 (Allowable error: 0.1%, Actual error: 36%)
Solves with these variables bounded:
value near lower bound: [MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, CruiseAlt_Mission, ClimbDistance_Mission]
value near upper bound: [TotalTime_Mission, A_{tri}_Mission/Aircraft/Wing/WingNoStruct]
Checking for relaxed constants...
WEIGHT DIFFERENCES
Total Fuel Weight Percent Diff: [-6.97455386]
Total Aircraft Weight Percent Diff: [-4.9504418]
Engine Weight Percent Diff: -8.23499669297
Fuselage Weight Percent Diff: -10.9542138449
Payload Weight Percent Diff: [-0.0400356]
VT Weight Percent Diff: -24.5190737152
HT Weight Percent Diff: -85.1525537388
Wing Weight Percent Diff: 0.426058031923
WING DIFFERENCES
Wing Span Percent Diff: 0.921607350726
Wing Area Percent Diff: -6.86185711352
HORIZONTAL TAIL DIFFERENCES
HT Area Percent Diff: -54.6185284229
VERTICAL TAIL DIFFERENCES
VT Span Percent Diff: -16.3232334483
VT Area Percent Diff: -29.9970383249
CRUISE SEGMENT 1 DRAG DIFFERENCES
Overall Cd Percent Diff: [-0.13085299]
Nacelle Cd Percent Diff: [ 23.80939441]
HT Cd Percent Diff: [-63.50970081] dimensionless
Fuselage Cd Percent Diff: [ 45.32349081]
VT Cd Percent Diff: [ 60.36853973] dimensionless
Induced Drag Cd Percent Diff: [ 1.06380269]
Wing Profile Cd Percent Diff: [-15.69392772]
CRUISE SEGMENT 1 TSFC DIFFERENCES
Initial Cruise TSFC Percent Diff: [ 2.99108438]
FUSELAGE DIFFERENCES
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
0.790004758366
Beginning signomial solve.
Solving took 7 GP solves and 11.1 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 2427083.77006 force_pound * meter but the right hand side evaluated to 2397878.14391 force_pound * meter (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 2.21510098519 meter but the right hand side evaluated to 1.96471795369 meter (Allowable error: 0.1%, Actual error: 11%)
Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) [N]...] is not tight because the left hand side evaluated to 17472.4964891 newton but the right hand side evaluated to 17443.2145325 newton (Allowable error: 0.1%, Actual error: 0.17%)
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 1242108.05255 joule / kilogram but the right hand side evaluated to 1.48151077346 megajoule / kilogram (Allowable error: 0.1%, Actual error: 9.5%)
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 642492.36616 joule / kilogram but the right hand side evaluated to 0.643976116336 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.1%)
Warning: Constraint [W_{lg}_Mission/Aircraft/LandingGear*x_{CG_{lg}}_Mission/Aircraft/LandingGear [N*m]... >= W_{mg}_Mission/Aircraft/LandingGear*x_m_Mission/Aircraft/LandingGear + W_{ng}_Mission/Aircraft/Landi...] is not tight because the left hand side evaluated to 271789.7314 meter * newton but the right hand side evaluated to 263034.971207 meter * newton (Allowable error: 1.0%, Actual error: 3.3%)
Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.575992106 meter but the right hand side evaluated to 16.6120444244 meter (Allowable error: 0.1%, Actual error: 12%)
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 10.9552248455 but the right hand side evaluated to 4.8581805724 (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 10.0071246236 but the right hand side evaluated to 4.85819028877 (Allowable error: 0.1%, Actual error: 51%)
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 8.21526155098 but the right hand side evaluated to 4.85819028877 (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 18.6220024229 meter but the right hand side evaluated to 18.3758628166 meter (Allowable error: 0.1%, Actual error: 1.3%)
Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1.
----------------------------------------------------------------------
Ran 2 tests in 28.412s
OK
Generating XML reports...
_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.6220024229 meter but the right hand side evaluated to 18.4513216119 meter (Allowable error: 0.1%, Actual error: 0.92%)
Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.67770643186 but the right hand side evaluated to 4.79403290607 (Allowable error: 0.1%, Actual error: 2.4%)
Warning: Constraint [SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) + mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{... <= 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 4.7311273671 but the right hand side evaluated to 4.81371916251 (Allowable error: 0.1%, Actual error: 1.7%)
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 7.60820099543 but the right hand side evaluated to 4.79403290607 (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 7.5796955958 but the right hand side evaluated to 4.81371916251 (Allowable error: 0.1%, Actual error: 36%)
Solves with these variables bounded:
value near lower bound: [MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct, CruiseAlt_Mission, ClimbDistance_Mission]
value near upper bound: [TotalTime_Mission, A_{tri}_Mission/Aircraft/Wing/WingNoStruct]
Checking for relaxed constants...
WEIGHT DIFFERENCES
Total Fuel Weight Percent Diff: [-6.97422995]
Total Aircraft Weight Percent Diff: [-4.95044675]
Engine Weight Percent Diff: -8.23468392487
Fuselage Weight Percent Diff: -10.954618425
Payload Weight Percent Diff: [-0.04052335]
VT Weight Percent Diff: -24.5186291271
HT Weight Percent Diff: -85.1525984735
Wing Weight Percent Diff: 0.425462741526
WING DIFFERENCES
Wing Span Percent Diff: 0.921619801497
Wing Area Percent Diff: -6.86153415504
HORIZONTAL TAIL DIFFERENCES
HT Area Percent Diff: -54.6182474474
VERTICAL TAIL DIFFERENCES
VT Span Percent Diff: -16.3230602377
VT Area Percent Diff: -29.9967358734
CRUISE SEGMENT 1 DRAG DIFFERENCES
Overall Cd Percent Diff: [-0.12878397]
Nacelle Cd Percent Diff: [ 23.80939215]
HT Cd Percent Diff: [-63.50960413] dimensionless
Fuselage Cd Percent Diff: [ 45.32347143]
VT Cd Percent Diff: [ 60.36820461] dimensionless
Induced Drag Cd Percent Diff: [ 1.06883829]
Wing Profile Cd Percent Diff: [-15.69240054]
CRUISE SEGMENT 1 TSFC DIFFERENCES
Initial Cruise TSFC Percent Diff: [ 2.99028604]
FUSELAGE DIFFERENCES
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
0.790005398454
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gpkit-models.git']
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/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 ['git', 'fetch', '--depth', '1', 'origin', 'master']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'turbofan']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'gpkit-models branch': 'master'})
calling ['git', 'fetch', '--depth', '1', 'origin', 'master']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gassolar']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})
calling ['git', 'fetch', '--depth', '1', 'origin', 'master']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})
calling ['git', 'fetch', '--depth', '1', 'origin', 'master']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models']
attempt 1
calling ['python', '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
attempt 1
[Execution node] check if [reynolds] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 5 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/jenkins/workspace/gpkit_commons_PR_Models/buildnode/reynolds/optimizer/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 SUCCESS
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: SUCCESS
![[Jenkins]](/csi/static/a404d988/images/svgs/logo.svg){kind=logo}
