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Full LogOptimizer - solved problem : the primal
Optimizer - Constraints : 1764
Optimizer - Cones : 0
Optimizer - Scalar variables : 4242 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.04 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.03
Factor - nonzeros before factor : 2.24e+04 after factor : 4.24e+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 5.3e+03 3.3e+02 1.6e+03 0.00e+00 -1.551864740e+03 1.023181539e-12 1.0e+00 0.06
1 3.5e+03 2.2e+02 1.0e+03 -5.02e-01 -1.066320887e+03 4.024938066e+01 6.7e-01 0.06
2 1.6e+03 9.8e+01 4.7e+02 8.06e-01 -3.017003262e+02 5.474665192e+01 3.0e-01 0.06
3 1.0e+03 6.7e+01 3.1e+02 4.97e+00 -6.733365514e+01 2.531189966e+01 2.0e-01 0.06
4 6.1e+02 5.1e+01 1.9e+02 2.47e+00 -2.079133945e+01 1.883790715e+01 1.2e-01 0.07
5 4.4e+02 4.9e+01 1.3e+02 1.55e+00 -9.836509932e+00 1.758095023e+01 8.7e-02 0.07
6 2.3e+02 5.2e+01 7.1e+01 1.38e+00 2.162434162e+00 1.590897981e+01 4.7e-02 0.08
7 1.6e+02 5.3e+01 4.9e+01 1.19e+00 5.926741625e+00 1.504983774e+01 3.2e-02 0.08
8 9.6e+01 3.4e+01 3.0e+01 1.14e+00 8.903115801e+00 1.430840692e+01 2.0e-02 0.08
9 7.1e+01 2.6e+01 2.2e+01 1.07e+00 1.004524058e+01 1.401339157e+01 1.5e-02 0.09
10 3.6e+01 3.6e+01 1.1e+01 1.02e+00 1.154641035e+01 1.360391867e+01 7.8e-03 0.09
11 3.5e+01 3.5e+01 1.1e+01 7.63e-01 1.150798118e+01 1.358457268e+01 7.7e-03 0.09
12 2.4e+01 2.5e+01 7.6e+00 7.43e-01 1.177554979e+01 1.340022004e+01 5.3e-03 0.09
13 1.4e+01 1.9e+01 4.6e+00 6.44e-01 1.208183992e+01 1.320869508e+01 3.2e-03 0.10
14 1.1e+01 2.1e+01 3.6e+00 4.30e-01 1.212670497e+01 1.312259708e+01 2.6e-03 0.10
15 6.4e+00 1.8e+01 2.1e+00 4.86e-01 1.229146754e+01 1.296725628e+01 1.5e-03 0.10
16 5.9e+00 1.6e+01 2.0e+00 3.31e-01 1.228587339e+01 1.294711942e+01 1.4e-03 0.11
17 4.4e+00 1.3e+01 1.5e+00 3.18e-01 1.227912743e+01 1.286630770e+01 1.1e-03 0.11
18 2.3e+00 8.6e+00 7.9e-01 3.02e-01 1.227682869e+01 1.267983434e+01 5.8e-04 0.11
19 1.3e+00 8.6e+00 4.7e-01 4.30e-01 1.230060196e+01 1.256670366e+01 3.5e-04 0.11
20 4.8e-01 8.3e+00 2.0e-01 5.64e-01 1.228028943e+01 1.240831865e+01 1.4e-04 0.12
21 3.1e-01 7.0e+00 1.3e-01 7.96e-01 1.228655841e+01 1.237297370e+01 9.4e-05 0.12
22 2.2e-01 6.5e+00 9.3e-02 8.30e-01 1.228812273e+01 1.235338263e+01 6.8e-05 0.12
23 6.5e-02 6.2e+00 3.3e-02 8.82e-01 1.228853024e+01 1.231272518e+01 2.4e-05 0.13
24 2.9e-02 5.8e+00 1.5e-02 9.47e-01 1.229220770e+01 1.230369905e+01 1.1e-05 0.13
25 9.9e-03 5.3e+00 5.5e-03 9.71e-01 1.229529292e+01 1.229940952e+01 3.9e-06 0.13
26 4.2e-03 5.1e+00 2.3e-03 9.88e-01 1.229638262e+01 1.229815639e+01 1.7e-06 0.13
27 1.4e-03 5.0e+00 8.0e-04 9.95e-01 1.229701442e+01 1.229762434e+01 5.8e-07 0.14
28 6.6e-04 4.2e+00 3.8e-04 9.98e-01 1.229719390e+01 1.229747902e+01 2.7e-07 0.14
29 5.9e-04 4.1e+00 3.4e-04 9.99e-01 1.229720126e+01 1.229745792e+01 2.4e-07 0.14
30 5.3e-04 3.7e+00 3.0e-04 9.99e-01 1.229721690e+01 1.229744792e+01 2.2e-07 0.15
31 4.8e-04 3.4e+00 2.7e-04 9.99e-01 1.229723099e+01 1.229743893e+01 2.0e-07 0.15
32 4.3e-04 3.1e+00 2.5e-04 9.99e-01 1.229724366e+01 1.229743081e+01 1.8e-07 0.15
33 3.9e-04 2.8e+00 2.2e-04 9.99e-01 1.229725505e+01 1.229742349e+01 1.6e-07 0.16
34 3.5e-04 2.5e+00 2.0e-04 9.99e-01 1.229726528e+01 1.229741689e+01 1.4e-07 0.16
35 3.2e-04 2.3e+00 1.8e-04 1.00e+00 1.229727448e+01 1.229741094e+01 1.3e-07 0.16
36 2.8e-04 2.1e+00 1.6e-04 1.00e+00 1.229728275e+01 1.229740557e+01 1.2e-07 0.16
37 2.6e-04 2.0e+00 1.5e-04 1.00e+00 1.229729019e+01 1.229740072e+01 1.0e-07 0.17
38 2.3e-04 1.8e+00 1.3e-04 1.00e+00 1.229729687e+01 1.229739636e+01 9.4e-08 0.17
39 2.1e-04 1.7e+00 1.2e-04 1.00e+00 1.229730288e+01 1.229739242e+01 8.4e-08 0.17
40 1.9e-04 1.5e+00 1.1e-04 1.00e+00 1.229730828e+01 1.229738887e+01 7.6e-08 0.18
41 1.7e-04 1.4e+00 9.6e-05 1.00e+00 1.229731314e+01 1.229738567e+01 6.8e-08 0.18
42 1.5e-04 1.3e+00 8.6e-05 1.00e+00 1.229731751e+01 1.229738279e+01 6.2e-08 0.18
43 1.4e-04 1.2e+00 7.7e-05 1.00e+00 1.229732144e+01 1.229738019e+01 5.5e-08 0.18
44 1.2e-04 1.1e+00 7.0e-05 1.00e+00 1.229732497e+01 1.229737785e+01 5.0e-08 0.19
45 3.6e-05 3.4e-01 2.1e-05 1.00e+00 1.229734727e+01 1.229736297e+01 1.5e-08 0.19
46 3.3e-05 3.3e-01 1.9e-05 1.00e+00 1.229734825e+01 1.229736238e+01 1.3e-08 0.19
47 9.2e-06 9.4e-02 5.3e-06 1.00e+00 1.229735435e+01 1.229735836e+01 3.8e-09 0.20
48 8.3e-06 8.5e-02 4.7e-06 1.00e+00 1.229735459e+01 1.229735820e+01 3.4e-09 0.20
49 3.0e-06 3.1e-02 1.7e-06 1.00e+00 1.229735598e+01 1.229735729e+01 1.2e-09 0.21
50 2.7e-06 2.8e-02 1.6e-06 1.00e+00 1.229735605e+01 1.229735724e+01 1.1e-09 0.21
51 2.4e-06 2.5e-02 1.4e-06 1.00e+00 1.229735613e+01 1.229735719e+01 1.0e-09 0.21
52 2.2e-06 2.2e-02 1.3e-06 1.00e+00 1.229735619e+01 1.229735715e+01 9.0e-10 0.22
53 2.0e-06 2.0e-02 1.1e-06 1.00e+00 1.229735625e+01 1.229735711e+01 8.1e-10 0.22
54 1.8e-06 1.8e-02 1.0e-06 1.00e+00 1.229735630e+01 1.229735708e+01 7.3e-10 0.22
55 1.6e-06 1.6e-02 9.2e-07 1.00e+00 1.229735635e+01 1.229735705e+01 6.6e-10 0.22
56 1.4e-06 1.5e-02 8.3e-07 1.00e+00 1.229735639e+01 1.229735702e+01 5.9e-10 0.23
57 1.3e-06 1.3e-02 7.4e-07 1.00e+00 1.229735643e+01 1.229735699e+01 5.3e-10 0.23
58 1.2e-06 1.2e-02 6.7e-07 1.00e+00 1.229735646e+01 1.229735697e+01 4.8e-10 0.23
59 1.1e-06 1.1e-02 6.0e-07 1.00e+00 1.229735649e+01 1.229735695e+01 4.3e-10 0.24
60 9.5e-07 9.7e-03 5.4e-07 1.00e+00 1.229735652e+01 1.229735693e+01 3.9e-10 0.24
61 8.5e-07 8.7e-03 4.9e-07 1.00e+00 1.229735655e+01 1.229735692e+01 3.5e-10 0.24
62 7.7e-07 7.8e-03 4.4e-07 1.00e+00 1.229735657e+01 1.229735690e+01 3.1e-10 0.24
63 6.9e-07 7.1e-03 4.0e-07 1.00e+00 1.229735659e+01 1.229735689e+01 2.8e-10 0.25
64 6.2e-07 6.4e-03 3.6e-07 1.00e+00 1.229735661e+01 1.229735688e+01 2.5e-10 0.25
65 5.6e-07 5.7e-03 3.2e-07 1.00e+00 1.229735662e+01 1.229735687e+01 2.3e-10 0.25
66 5.7e-08 5.8e-04 3.3e-08 1.00e+00 1.229735675e+01 1.229735678e+01 2.3e-11 0.26
67 3.2e-09 3.3e-05 1.8e-09 1.00e+00 1.229735677e+01 1.229735677e+01 1.3e-12 0.26
68 2.9e-11 3.1e-07 1.8e-11 9.98e-01 1.229735677e+01 1.229735677e+01 7.9e-15 0.26
Interior-point optimizer terminated. Time: 0.26.
Optimizer terminated. Time: 0.27
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.2297356769e+01 Viol. con: 2e-11 var: 0e+00
Dual. obj: 1.2297356769e+01 Viol. con: 0e+00 var: 5e-08
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.304 seconds.
result packing took 45% of solve time
solution checking took 53% 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 : MACOSX/64-X86
Cores : 8
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 : 1062
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1071
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1071
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Interior-point optimizer terminated. Time: 0.01.
Optimizer terminated. Time: 0.02
solsta = 6, prosta = 5
Interior-point solution summary
Problem status : DUAL_INFEASIBLE
Solution status : DUAL_INFEASIBLE_CER
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.0465 seconds.
T_{t_{4.1_{max}}}_FleetMission/Aircraft/Engine has no upper bound
Using solver 'mosek'
Solving for 2481 variables.
Warning: The variable with index '1861' 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 : MACOSX/64-X86
Cores : 8
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2482
Cones : 0
Scalar variables : 5899
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 : 503
Eliminator terminated.
Eliminator started.
Total number of eliminations : 580
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 580
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 : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 1768
Optimizer - Cones : 0
Optimizer - Scalar variables : 4250 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.05 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.04
Factor - nonzeros before factor : 2.25e+04 after factor : 4.34e+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 5.4e+03 3.2e+02 1.3e+03 0.00e+00 -1.262616920e+03 1.023181539e-12 1.0e+00 0.07
1 3.0e+03 1.8e+02 7.2e+02 -5.31e-01 -7.599781805e+02 5.319668037e+01 5.7e-01 0.07
2 1.5e+03 8.8e+01 3.7e+02 1.27e+00 -2.026577350e+02 5.073268277e+01 2.9e-01 0.07
3 9.8e+02 6.1e+01 2.4e+02 4.38e+00 -4.440288996e+01 2.455687734e+01 1.9e-01 0.08
4 6.1e+02 4.9e+01 1.5e+02 2.31e+00 -1.468557521e+01 1.846289791e+01 1.2e-01 0.08
5 4.9e+02 4.9e+01 1.2e+02 1.29e+00 -1.046029443e+01 1.720861143e+01 9.5e-02 0.08
6 3.5e+02 5.1e+01 8.8e+01 1.03e+00 -5.926926449e+00 1.563693922e+01 6.9e-02 0.08
7 3.1e+02 4.5e+01 7.7e+01 9.90e-01 -4.406742426e+00 1.548841102e+01 6.1e-02 0.09
8 2.5e+02 3.6e+01 6.1e+01 1.03e+00 -1.277495930e+00 1.457668263e+01 4.8e-02 0.09
9 1.5e+02 2.7e+01 3.8e+01 1.09e+00 3.398416125e+00 1.273707029e+01 3.0e-02 0.09
10 5.8e+01 3.6e+01 1.5e+01 1.12e+00 7.377357182e+00 1.073509700e+01 1.2e-02 0.09
11 2.3e+01 2.9e+01 6.0e+00 1.08e+00 8.839633620e+00 1.014652969e+01 5.1e-03 0.10
12 8.0e+00 3.5e+01 2.2e+00 9.94e-01 9.418062237e+00 9.901274216e+00 2.0e-03 0.10
13 5.5e+00 2.4e+01 1.5e+00 9.11e-01 9.519121406e+00 9.859109316e+00 1.3e-03 0.10
14 5.2e+00 2.4e+01 1.4e+00 8.36e-01 9.515583756e+00 9.848934828e+00 1.3e-03 0.11
15 4.9e+00 2.4e+01 1.3e+00 7.87e-01 9.503876950e+00 9.835861127e+00 1.2e-03 0.11
16 4.4e+00 2.1e+01 1.2e+00 7.59e-01 9.505927279e+00 9.823365236e+00 1.1e-03 0.11
17 3.9e+00 1.9e+01 1.1e+00 7.07e-01 9.516089830e+00 9.814683706e+00 9.9e-04 0.12
18 3.5e+00 1.7e+01 9.9e-01 6.65e-01 9.528081323e+00 9.806851710e+00 8.9e-04 0.12
19 3.2e+00 1.6e+01 8.9e-01 6.30e-01 9.541129692e+00 9.799567433e+00 8.0e-04 0.12
20 2.9e+00 1.4e+01 8.0e-01 6.03e-01 9.554321856e+00 9.792823641e+00 7.2e-04 0.13
21 2.6e+00 1.3e+01 7.2e-01 5.79e-01 9.566760218e+00 9.786507088e+00 6.5e-04 0.13
22 2.3e+00 1.2e+01 6.5e-01 5.58e-01 9.578273557e+00 9.780572471e+00 5.8e-04 0.14
23 2.1e+00 1.1e+01 5.8e-01 5.39e-01 9.588832475e+00 9.774971180e+00 5.3e-04 0.14
24 1.9e+00 1.0e+01 5.3e-01 5.23e-01 9.598443393e+00 9.769657775e+00 4.7e-04 0.14
25 1.7e+00 9.2e+00 4.7e-01 5.09e-01 9.607125094e+00 9.764586389e+00 4.3e-04 0.15
26 1.5e+00 8.6e+00 4.3e-01 4.99e-01 9.614910316e+00 9.759714418e+00 3.9e-04 0.15
27 1.4e+00 8.1e+00 3.8e-01 4.92e-01 9.621845976e+00 9.755005986e+00 3.5e-04 0.15
28 1.2e+00 7.7e+00 3.5e-01 4.89e-01 9.627992755e+00 9.750435894e+00 3.1e-04 0.15
29 1.1e+00 7.3e+00 3.1e-01 4.91e-01 9.633420883e+00 9.745991725e+00 2.8e-04 0.16
30 1.0e+00 7.0e+00 2.8e-01 4.96e-01 9.638203513e+00 9.741672701e+00 2.5e-04 0.16
31 9.0e-01 6.8e+00 2.5e-01 5.06e-01 9.642411127e+00 9.737485661e+00 2.3e-04 0.16
32 8.1e-01 6.5e+00 2.3e-01 5.20e-01 9.646109916e+00 9.733440901e+00 2.1e-04 0.17
33 7.3e-01 6.2e+00 2.1e-01 5.37e-01 9.649362683e+00 9.729549850e+00 1.9e-04 0.17
34 6.6e-01 6.0e+00 1.8e-01 5.56e-01 9.652229564e+00 9.725824217e+00 1.7e-04 0.17
35 5.9e-01 5.7e+00 1.7e-01 5.77e-01 9.654767491e+00 9.722275434e+00 1.5e-04 0.17
36 5.3e-01 5.4e+00 1.5e-01 6.00e-01 9.657028627e+00 9.718913785e+00 1.4e-04 0.18
37 4.8e-01 5.2e+00 1.4e-01 6.24e-01 9.659058685e+00 9.715747357e+00 1.2e-04 0.18
38 4.3e-01 4.9e+00 1.2e-01 6.48e-01 9.660895552e+00 9.712780988e+00 1.1e-04 0.18
39 3.9e-01 4.6e+00 1.1e-01 6.72e-01 9.662568711e+00 9.710015539e+00 1.0e-04 0.19
40 3.5e-01 4.3e+00 9.9e-02 6.96e-01 9.664099765e+00 9.707447761e+00 9.0e-05 0.19
41 3.1e-01 4.0e+00 8.9e-02 7.19e-01 9.665504050e+00 9.705070930e+00 8.1e-05 0.19
42 2.8e-01 3.7e+00 8.0e-02 7.42e-01 9.666792820e+00 9.702876012e+00 7.3e-05 0.19
43 2.5e-01 3.5e+00 7.2e-02 7.63e-01 9.667975231e+00 9.700852917e+00 6.6e-05 0.20
44 2.3e-01 3.2e+00 6.5e-02 7.84e-01 9.669059706e+00 9.698991491e+00 5.9e-05 0.20
45 2.1e-01 3.0e+00 5.9e-02 8.04e-01 9.670054611e+00 9.697282123e+00 5.3e-05 0.20
46 1.9e-01 2.8e+00 5.3e-02 8.23e-01 9.670968364e+00 9.695715963e+00 4.8e-05 0.21
47 1.7e-01 2.6e+00 4.8e-02 8.40e-01 9.671809166e+00 9.694284818e+00 4.3e-05 0.21
48 1.5e-01 2.4e+00 4.3e-02 8.56e-01 9.672584558e+00 9.692980853e+00 3.9e-05 0.21
49 1.4e-01 2.3e+00 3.9e-02 8.71e-01 9.673301028e+00 9.691796247e+00 3.5e-05 0.21
50 1.2e-01 2.1e+00 3.5e-02 8.84e-01 9.673963824e+00 9.690722961e+00 3.2e-05 0.22
51 1.1e-01 2.0e+00 3.1e-02 8.96e-01 9.674577024e+00 9.689752691e+00 2.8e-05 0.22
52 9.9e-02 1.9e+00 2.8e-02 9.07e-01 9.675143792e+00 9.688876998e+00 2.6e-05 0.22
53 8.9e-02 1.8e+00 2.5e-02 9.17e-01 9.675666720e+00 9.688087530e+00 2.3e-05 0.22
54 8.0e-02 1.6e+00 2.3e-02 9.25e-01 9.676148122e+00 9.687376254e+00 2.1e-05 0.23
55 7.2e-02 1.5e+00 2.1e-02 9.32e-01 9.676590237e+00 9.686735632e+00 1.9e-05 0.23
56 6.5e-02 1.5e+00 1.9e-02 9.39e-01 9.676995327e+00 9.686158720e+00 1.7e-05 0.23
57 5.8e-02 1.4e+00 1.7e-02 9.45e-01 9.677365702e+00 9.685639197e+00 1.5e-05 0.24
58 5.2e-02 1.3e+00 1.5e-02 9.51e-01 9.677703691e+00 9.685171347e+00 1.4e-05 0.24
59 4.7e-02 1.2e+00 1.4e-02 9.55e-01 9.678011615e+00 9.684750022e+00 1.2e-05 0.24
60 4.2e-02 1.2e+00 1.2e-02 9.60e-01 9.678291747e+00 9.684370592e+00 1.1e-05 0.24
61 3.8e-02 1.1e+00 1.1e-02 9.63e-01 9.678546291e+00 9.684028905e+00 1.0e-05 0.25
62 3.4e-02 1.1e+00 9.9e-03 9.67e-01 9.678777366e+00 9.683721235e+00 9.0e-06 0.25
63 3.1e-02 1.0e+00 8.9e-03 9.70e-01 9.678986977e+00 9.683444239e+00 8.1e-06 0.25
64 2.8e-02 9.9e-01 8.0e-03 9.73e-01 9.679176996e+00 9.683194898e+00 7.3e-06 0.26
65 2.5e-02 9.5e-01 7.2e-03 9.75e-01 9.679349153e+00 9.682970477e+00 6.5e-06 0.26
66 2.3e-02 9.2e-01 6.5e-03 9.78e-01 9.679505033e+00 9.682768496e+00 5.9e-06 0.27
67 2.0e-02 8.9e-01 5.8e-03 9.80e-01 9.679646093e+00 9.682586711e+00 5.3e-06 0.27
68 1.8e-02 8.6e-01 5.3e-03 9.82e-01 9.679773669e+00 9.682423098e+00 4.8e-06 0.27
69 1.6e-02 8.3e-01 4.7e-03 9.83e-01 9.679888987e+00 9.682275831e+00 4.3e-06 0.28
70 1.5e-02 8.1e-01 4.3e-03 9.85e-01 9.679993174e+00 9.682143268e+00 3.9e-06 0.28
71 1.3e-02 7.9e-01 3.8e-03 9.86e-01 9.680087259e+00 9.682023931e+00 3.5e-06 0.28
72 1.2e-02 7.7e-01 3.5e-03 9.88e-01 9.680172184e+00 9.681916492e+00 3.1e-06 0.28
73 1.1e-02 7.5e-01 3.1e-03 9.89e-01 9.680248809e+00 9.681819755e+00 2.8e-06 0.29
74 9.7e-03 7.4e-01 2.8e-03 9.90e-01 9.680317917e+00 9.681732645e+00 2.5e-06 0.29
75 8.7e-03 7.2e-01 2.5e-03 9.91e-01 9.680380221e+00 9.681654196e+00 2.3e-06 0.29
76 7.9e-03 7.1e-01 2.3e-03 9.92e-01 9.680436370e+00 9.681583539e+00 2.1e-06 0.30
77 7.1e-03 7.0e-01 2.0e-03 9.92e-01 9.680486954e+00 9.681519891e+00 1.9e-06 0.30
78 6.4e-03 6.8e-01 1.8e-03 9.93e-01 9.680532510e+00 9.681462550e+00 1.7e-06 0.30
79 5.7e-03 6.7e-01 1.7e-03 9.94e-01 9.680573524e+00 9.681410888e+00 1.5e-06 0.30
80 5.2e-03 6.7e-01 1.5e-03 9.94e-01 9.680610443e+00 9.681364339e+00 1.3e-06 0.31
81 4.6e-03 6.6e-01 1.3e-03 9.95e-01 9.680643669e+00 9.681322396e+00 1.2e-06 0.31
82 4.2e-03 6.5e-01 1.2e-03 9.95e-01 9.680673571e+00 9.681284607e+00 1.1e-06 0.31
83 3.8e-03 6.4e-01 1.1e-03 9.96e-01 9.680700480e+00 9.681250562e+00 9.8e-07 0.32
84 3.4e-03 6.4e-01 9.8e-04 9.96e-01 9.680724698e+00 9.681219894e+00 8.9e-07 0.32
85 3.1e-03 6.3e-01 8.8e-04 9.96e-01 9.680746494e+00 9.681192271e+00 8.0e-07 0.32
86 2.7e-03 6.2e-01 7.9e-04 9.97e-01 9.680766111e+00 9.681167394e+00 7.2e-07 0.32
87 2.5e-03 6.2e-01 7.1e-04 9.97e-01 9.680783768e+00 9.681144991e+00 6.5e-07 0.33
88 2.2e-03 6.2e-01 6.4e-04 9.97e-01 9.680799660e+00 9.681124817e+00 5.8e-07 0.33
89 2.0e-03 6.1e-01 5.8e-04 9.98e-01 9.680813964e+00 9.681106651e+00 5.2e-07 0.33
90 1.8e-03 6.1e-01 5.2e-04 9.98e-01 9.680826837e+00 9.681090293e+00 4.7e-07 0.34
91 1.6e-03 6.0e-01 4.7e-04 9.98e-01 9.680838422e+00 9.681075564e+00 4.2e-07 0.34
92 6.6e-04 2.4e-01 1.9e-04 9.98e-01 9.680900066e+00 9.680996463e+00 1.7e-07 0.34
93 5.9e-04 2.2e-01 1.7e-04 9.99e-01 9.680904444e+00 9.680991203e+00 1.5e-07 0.35
94 5.3e-04 2.0e-01 1.5e-04 9.99e-01 9.680908242e+00 9.680986330e+00 1.4e-07 0.35
95 4.8e-04 1.8e-01 1.4e-04 9.99e-01 9.680911655e+00 9.680981938e+00 1.3e-07 0.35
96 4.3e-04 1.6e-01 1.2e-04 9.99e-01 9.680914724e+00 9.680977981e+00 1.1e-07 0.35
97 3.9e-04 1.4e-01 1.1e-04 9.99e-01 9.680917482e+00 9.680974417e+00 1.0e-07 0.36
98 3.5e-04 1.3e-01 1.0e-04 9.99e-01 9.680919962e+00 9.680971205e+00 9.1e-08 0.36
99 3.1e-04 1.2e-01 9.1e-05 1.00e+00 9.680922192e+00 9.680968312e+00 8.2e-08 0.36
100 2.8e-04 1.1e-01 8.2e-05 1.00e+00 9.680924196e+00 9.680965706e+00 7.4e-08 0.36
101 2.5e-04 9.5e-02 7.3e-05 1.00e+00 9.680925997e+00 9.680963357e+00 6.7e-08 0.37
102 2.3e-04 8.5e-02 6.6e-05 1.00e+00 9.680927616e+00 9.680961241e+00 6.0e-08 0.37
103 2.1e-04 7.7e-02 6.0e-05 1.00e+00 9.680929072e+00 9.680959335e+00 5.4e-08 0.37
104 1.9e-04 6.9e-02 5.4e-05 1.00e+00 9.680930380e+00 9.680957617e+00 4.9e-08 0.38
105 1.7e-04 6.2e-02 4.8e-05 1.00e+00 9.680931555e+00 9.680956069e+00 4.4e-08 0.38
106 1.5e-04 5.6e-02 4.3e-05 1.00e+00 9.680932611e+00 9.680954675e+00 3.9e-08 0.38
107 1.4e-04 5.0e-02 3.9e-05 1.00e+00 9.680933561e+00 9.680953418e+00 3.5e-08 0.38
108 1.2e-04 4.5e-02 3.5e-05 1.00e+00 9.680934414e+00 9.680952286e+00 3.2e-08 0.39
109 1.1e-04 4.1e-02 3.2e-05 1.00e+00 9.680935181e+00 9.680951266e+00 2.9e-08 0.39
110 9.9e-05 3.7e-02 2.8e-05 1.00e+00 9.680935870e+00 9.680950347e+00 2.6e-08 0.40
111 8.9e-05 3.3e-02 2.6e-05 1.00e+00 9.680936489e+00 9.680949519e+00 2.3e-08 0.40
112 8.0e-05 3.0e-02 2.3e-05 1.00e+00 9.680937046e+00 9.680948772e+00 2.1e-08 0.41
113 7.2e-05 2.7e-02 2.1e-05 1.00e+00 9.680937546e+00 9.680948100e+00 1.9e-08 0.41
114 6.5e-05 2.4e-02 1.9e-05 1.00e+00 9.680937996e+00 9.680947494e+00 1.7e-08 0.41
115 5.8e-05 2.2e-02 1.7e-05 1.00e+00 9.680938400e+00 9.680946949e+00 1.5e-08 0.41
116 1.5e-05 5.5e-03 4.3e-06 1.00e+00 9.680941086e+00 9.680943259e+00 3.9e-09 0.42
117 3.1e-06 1.2e-03 9.1e-07 1.00e+00 9.680941802e+00 9.680942263e+00 8.2e-10 0.42
118 1.8e-07 6.8e-05 5.3e-08 1.00e+00 9.680941983e+00 9.680942010e+00 4.8e-11 0.42
119 1.0e-09 3.9e-07 3.2e-10 9.97e-01 9.680941994e+00 9.680941995e+00 3.4e-13 0.43
Interior-point optimizer terminated. Time: 0.43.
Optimizer terminated. Time: 0.44
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 9.6809419945e+00 Viol. con: 5e-10 var: 0e+00
Dual. obj: 9.6809419946e+00 Viol. con: 0e+00 var: 4e-08
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.469 seconds.
result packing took 29% 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 : MACOSX/64-X86
Cores : 8
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 : 1059
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1067
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1067
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Interior-point optimizer terminated. Time: 0.01.
Optimizer terminated. Time: 0.02
solsta = 6, prosta = 5
Interior-point solution summary
Problem status : DUAL_INFEASIBLE
Solution status : DUAL_INFEASIBLE_CER
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.0464 seconds.
T_{t_{4.1_{max}}}_FleetMission/Aircraft/Engine has no upper bound
Using solver 'mosek'
Solving for 2481 variables.
Warning: The variable with index '1861' 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 : MACOSX/64-X86
Cores : 8
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2482
Cones : 0
Scalar variables : 5899
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 : 503
Eliminator terminated.
Eliminator started.
Total number of eliminations : 580
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 580
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 : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 1768
Optimizer - Cones : 0
Optimizer - Scalar variables : 4250 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.06 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.04
Factor - nonzeros before factor : 2.25e+04 after factor : 4.34e+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 5.6e+03 3.1e+02 9.8e+02 0.00e+00 -9.745812179e+02 1.023181539e-12 1.0e+00 0.08
1 3.2e+03 1.8e+02 5.7e+02 -3.53e-01 -5.528342284e+02 4.830487029e+01 5.8e-01 0.08
2 1.6e+03 8.6e+01 2.8e+02 1.45e+00 -1.274426648e+02 4.615147027e+01 2.8e-01 0.08
3 9.9e+02 6.4e+01 1.9e+02 4.75e+00 -2.343557696e+01 2.218003479e+01 1.9e-01 0.09
4 5.7e+02 5.4e+01 1.1e+02 2.00e+00 -4.459450386e+00 1.749192673e+01 1.1e-01 0.09
5 5.0e+02 5.3e+01 9.6e+01 8.33e-01 -3.805995610e+00 1.716055356e+01 9.5e-02 0.09
6 3.7e+02 7.9e+01 7.3e+01 5.39e-01 -4.401913078e+00 1.683462526e+01 7.2e-02 0.09
7 2.2e+02 6.2e+01 4.4e+01 2.45e-01 -3.830724548e+00 1.486585775e+01 4.4e-02 0.10
8 1.4e+02 4.1e+01 2.9e+01 5.72e-01 -7.498325770e-01 1.184340615e+01 2.9e-02 0.10
9 1.0e+02 3.3e+01 2.0e+01 8.58e-01 2.252967241e+00 1.035362642e+01 2.0e-02 0.10
10 3.3e+01 1.9e+01 6.9e+00 7.89e-01 3.321165002e+00 6.027251604e+00 7.0e-03 0.10
11 2.0e+01 1.9e+01 4.3e+00 1.07e+00 4.032171425e+00 5.714865790e+00 4.4e-03 0.11
12 4.4e+00 2.7e+01 1.0e+00 1.08e+00 4.577333220e+00 4.969664418e+00 1.1e-03 0.11
13 2.0e+00 2.0e+01 4.7e-01 9.99e-01 4.693656077e+00 4.872681036e+00 4.8e-04 0.11
14 1.9e+00 2.0e+01 4.5e-01 9.42e-01 4.685966994e+00 4.861470057e+00 4.7e-04 0.11
15 1.3e+00 1.4e+01 3.1e-01 9.37e-01 4.715961965e+00 4.838000466e+00 3.2e-04 0.12
16 7.7e-01 1.1e+01 1.9e-01 9.29e-01 4.742993001e+00 4.818885809e+00 1.9e-04 0.12
17 5.5e-01 8.3e+00 1.4e-01 8.96e-01 4.753612773e+00 4.810194918e+00 1.4e-04 0.12
18 2.4e-01 8.1e+00 6.2e-02 9.07e-01 4.771983047e+00 4.798718523e+00 6.4e-05 0.13
19 1.2e-01 7.5e+00 3.1e-02 9.33e-01 4.780718796e+00 4.794229066e+00 3.1e-05 0.13
20 7.6e-02 7.5e+00 2.0e-02 9.15e-01 4.783235686e+00 4.792401997e+00 2.0e-05 0.13
21 5.8e-02 6.6e+00 1.5e-02 9.11e-01 4.784500999e+00 4.791592308e+00 1.6e-05 0.14
22 3.7e-02 5.8e+00 9.8e-03 9.19e-01 4.785959025e+00 4.790666432e+00 1.0e-05 0.14
23 2.6e-02 5.5e+00 6.9e-03 9.29e-01 4.786787738e+00 4.790140128e+00 7.0e-06 0.14
24 1.7e-02 4.7e+00 4.5e-03 9.23e-01 4.787429441e+00 4.789668722e+00 4.6e-06 0.14
25 1.1e-02 4.4e+00 3.0e-03 9.50e-01 4.787874569e+00 4.789388555e+00 3.1e-06 0.15
26 4.0e-03 1.5e+00 1.1e-03 9.71e-01 4.788464028e+00 4.789003316e+00 1.1e-06 0.15
27 2.2e-03 8.5e-01 6.0e-04 9.87e-01 4.788598802e+00 4.788898376e+00 6.1e-07 0.15
28 7.6e-04 2.9e-01 2.1e-04 9.94e-01 4.788709522e+00 4.788813160e+00 2.1e-07 0.15
29 2.9e-04 1.1e-01 7.9e-05 9.99e-01 4.788745440e+00 4.788785168e+00 8.0e-08 0.16
30 1.4e-04 5.4e-02 3.8e-05 1.00e+00 4.788756927e+00 4.788776081e+00 3.8e-08 0.16
31 3.4e-05 1.3e-02 9.3e-06 1.00e+00 4.788765055e+00 4.788769747e+00 9.4e-09 0.17
32 3.7e-06 1.4e-03 1.0e-06 1.00e+00 4.788767379e+00 4.788767897e+00 1.0e-09 0.17
33 8.1e-08 3.1e-05 2.3e-08 1.00e+00 4.788767660e+00 4.788767672e+00 2.3e-11 0.17
34 6.6e-10 2.5e-07 2.1e-10 1.00e+00 4.788767666e+00 4.788767667e+00 1.6e-13 0.18
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: 4.7887676664e+00 Viol. con: 3e-10 var: 0e+00
Dual. obj: 4.7887676665e+00 Viol. con: 0e+00 var: 3e-08
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.218 seconds.
result packing took 61% of solve time
solution checking took 62% 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 : MACOSX/64-X86
Cores : 8
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 : 1017
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1039
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1039
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Interior-point optimizer terminated. Time: 0.01.
Optimizer terminated. Time: 0.02
solsta = 6, prosta = 5
Interior-point solution summary
Problem status : DUAL_INFEASIBLE
Solution status : DUAL_INFEASIBLE_CER
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.0448 seconds.
T_{t_{4.1_{max}}}_FleetMission/Aircraft/Engine has no upper bound
Using solver 'mosek'
Solving for 2481 variables.
Warning: The variable with index '1861' 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 : MACOSX/64-X86
Cores : 8
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 2482
Cones : 0
Scalar variables : 5899
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 : 503
Eliminator terminated.
Eliminator started.
Total number of eliminations : 580
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 580
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 : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 1768
Optimizer - Cones : 0
Optimizer - Scalar variables : 4250 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.06 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.04
Factor - nonzeros before factor : 2.25e+04 after factor : 4.34e+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 5.6e+03 3.1e+02 7.4e+02 0.00e+00 -7.404333840e+02 1.023181539e-12 1.0e+00 0.07
1 3.3e+03 1.9e+02 4.5e+02 -1.97e-01 -3.933128746e+02 4.429754496e+01 6.0e-01 0.07
2 1.5e+03 8.2e+01 2.1e+02 1.70e+00 -6.626926032e+01 4.151949627e+01 2.7e-01 0.07
3 1.0e+03 6.1e+01 1.5e+02 4.74e+00 -1.497962120e+01 2.327484518e+01 1.9e-01 0.08
4 6.9e+02 4.5e+01 1.0e+02 2.21e+00 -2.379341880e+00 1.864741079e+01 1.3e-01 0.08
5 5.3e+02 4.4e+01 7.9e+01 1.23e+00 -4.949735246e-01 1.795246933e+01 1.0e-01 0.08
6 4.1e+02 4.3e+01 6.0e+01 6.67e-01 -7.179830019e-01 1.741822996e+01 7.7e-02 0.09
7 2.0e+02 9.9e+01 2.9e+01 1.26e-01 -4.463329333e+00 1.639837197e+01 3.7e-02 0.09
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151 1.7e-32 0.0e+00 5.7e-34 -5.09e-02 9.722200623e+00 -1.973374420e+06 6.7e-60 0.49
152 1.8e-32 0.0e+00 5.7e-34 -5.08e-02 9.643202475e+00 -1.972219870e+06 6.7e-60 0.49
153 1.7e-32 0.0e+00 8.2e-34 -5.14e-02 1.002222755e+01 -1.967787856e+06 6.6e-60 0.50
154 1.8e-32 0.0e+00 8.3e-34 -5.12e-02 9.594399887e+00 -1.962246353e+06 6.5e-60 0.50
155 1.8e-32 0.0e+00 8.4e-34 -5.56e-02 9.731479784e+00 -1.961303432e+06 6.5e-60 0.50
156 1.9e-32 0.0e+00 8.6e-34 -5.55e-02 9.743530099e+00 -1.958944678e+06 6.5e-60 0.50
157 1.9e-32 0.0e+00 9.2e-34 -5.63e-02 9.671301441e+00 -1.957556542e+06 6.5e-60 0.51
158 1.9e-32 0.0e+00 9.3e-34 -5.66e-02 9.351581602e+00 -1.953998429e+06 6.5e-60 0.51
159 1.9e-32 0.0e+00 9.5e-34 -5.96e-02 9.384648868e+00 -1.952390875e+06 6.5e-60 0.52
160 1.9e-32 0.0e+00 1.0e-33 -6.00e-02 9.341233819e+00 -1.951152185e+06 6.5e-60 0.52
161 2.0e-32 0.0e+00 1.0e-33 -5.98e-02 9.039204919e+00 -1.948003016e+06 6.4e-60 0.52
162 2.0e-32 0.0e+00 1.1e-33 -6.23e-02 9.099072430e+00 -1.946096981e+06 6.4e-60 0.52
163 2.0e-32 0.0e+00 1.1e-33 -6.24e-02 9.063959137e+00 -1.944945767e+06 6.4e-60 0.53
164 2.0e-32 0.0e+00 1.2e-33 -6.19e-02 8.898131402e+00 -1.942132695e+06 6.4e-60 0.53
165 2.0e-32 0.0e+00 1.2e-33 -6.27e-02 9.056538797e+00 -1.940577307e+06 6.4e-60 0.53
166 2.1e-32 0.0e+00 1.3e-33 -6.21e-02 8.973765255e+00 -1.930343372e+06 6.4e-60 0.53
167 2.2e-32 0.0e+00 1.2e-33 -6.39e-02 7.813036936e+00 -1.920662671e+06 6.0e-60 0.54
168 2.3e-32 0.0e+00 1.2e-33 -7.56e-02 7.588140421e+00 -1.913115096e+06 6.0e-60 0.54
169 2.4e-32 0.0e+00 1.2e-33 -7.84e-02 7.370571774e+00 -1.906616546Ee+06 5.8e-60 0.54
170 2.3e-32 0.0e+00 1.1e-33 -8.19e-02 7.173435948e+00 -1.903123933e+06 5.4e-60 0.55
171 2.3e-32 0.0e+00 1.1e-33 -8.28e-02 7.438951637e+00 -1.901786531e+06 5.4e-60 0.55
172 2.3e-32 0.0e+00 1.1e-33 -8.14e-02 7.564797119e+00 -1.900440547e+06 5.3e-60 0.55
173 2.3e-32 0.0e+00 1.1e-33 -8.10e-02 7.559399003e+00 -1.900087361e+06 5.3e-60 0.55
174 2.3e-32 0.0e+00 1.4e-33 -8.10e-02 7.578523333e+00 -1.898863994e+06 5.3e-60 0.56
175 2.3e-32 0.0e+00 1.6e-33 -8.09e-02 7.713618613e+00 -1.896786359e+06 5.3e-60 0.56
176 2.3e-32 0.0e+00 1.8e-33 -7.97e-02 7.549960069e+00 -1.893068345e+06 5.3e-60 0.56
177 2.3e-32 0.0e+00 1.8e-33 -8.05e-02 7.579468831e+00 -1.891533812e+06 5.3e-60 0.56
178 2.3e-32 0.0e+00 1.8e-33 -8.11e-02 7.679809787e+00 -1.890506928e+06 5.3e-60 0.57
179 2.3e-32 0.0e+00 1.6e-33 -8.19e-02 7.700653586e+00 -1.878301267e+06 4.7e-60 0.57
180 2.2e-32 0.0e+00 1.6e-33 -8.53e-02 7.985775442e+00 -1.877512450e+06 4.6e-60 0.57
181 2.2e-32 0.0e+00 1.6e-33 -8.25e-02 7.747734981e+00 -1.874925422e+06 4.6e-60 0.57
182 2.2e-32 0.0e+00 1.6e-33 -8.24e-02 7.803379725e+00 -1.872757610e+06 4.6e-60 0.58
183 2.2e-32 0.0e+00 1.8e-33 -8.19e-02 8.018019121e+00 -1.863661324e+06 4.5e-60 0.58
184 2.2e-32 0.0e+00 1.8e-33 -8.32e-02 8.110520065e+00 -1.862140802e+06 4.5e-60 0.58
185 2.4e-32 0.0e+00 1.8e-33 -8.41e-02 9.023598004e+00 -1.806179884e+06 4.3e-60 0.58
186 2.3e-32 0.0e+00 1.9e-33 -8.79e-02 1.031852227e+01 -1.800794266e+06 4.2e-60 0.59
187 2.2e-32 0.0e+00 1.9e-33 -8.50e-02 1.224693237e+01 -1.800762035e+06 4.2e-60 0.59
188 2.3e-32 0.0e+00 1.9e-33 -7.33e-02 1.079869185e+01 -1.796410621e+06 4.2e-60 0.59
189 2.4e-32 0.0e+00 1.9e-33 -8.19e-02 1.034263164e+01 -1.794550003e+06 4.2e-60 0.60
190 2.4e-32 0.0e+00 2.0e-33 -8.48e-02 9.636935768e+00 -1.791137489e+06 4.2e-60 0.60
191 2.4e-32 0.0e+00 2.0e-33 -8.66e-02 9.622974321e+00 -1.791082115e+06 4.2e-60 0.60
192 2.3e-32 0.0e+00 2.0e-33 -8.65e-02 9.120024325e+00 -1.787232782e+06 4.2e-60 0.60
193 2.3e-32 0.0e+00 2.0e-33 -8.46e-02 8.850307208e+00 -1.784264797e+06 4.2e-60 0.61
194 2.3e-32 0.0e+00 2.0e-33 -8.30e-02 8.483556703e+00 -1.781667548e+06 4.2e-60 0.61
195 2.3e-32 0.0e+00 2.0e-33 -8.14e-02 7.103097019e+00 -1.779908735e+06 4.2e-60 0.61
196 2.2e-32 0.0e+00 2.1e-33 -8.32e-02 5.756495645e+00 -1.777236919e+06 4.2e-60 0.61
197 2.2e-32 0.0e+00 2.1e-33 -7.91e-02 5.171853831e+00 -1.774208340e+06 4.2e-60 0.62
198 2.2e-32 0.0e+00 2.1e-33 -7.95e-02 5.114239919e+00 -1.771642822e+06 4.2e-60 0.62
199 2.2e-32 0.0e+00 2.1e-33 -8.20e-02 4.005518426e+00 -1.766342926e+06 4.2e-60 0.62
200 2.0e-32 0.0e+00 2.1e-33 -8.11e-02 2.835514538e+00 -1.761817767e+06 4.2e-60 0.62
Interior-point optimizer terminated. Time: 0.63.
Optimizer terminated. Time: 0.64
Return code from optimize - 10000
Interior-point solution summary
Problem status : UNKNOWN
Solution status : UNKNOWN
Primal. obj: 2.8355145384e+00 Viol. con: 1e+01 var: 0e+00
Dual. obj: -1.7618177672e+06 Viol. con: 0e+00 var: 9e-06
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.668 seconds.
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 : MACOSX/64-X86
Cores : 8
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 : 8
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 : 0.02 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 -1.772328772e+04 2.816143901e+00 7.3e-01 0.03
2 3.6e+02 5.2e+03 6.0e+03 4.01e-02 -1.101718534e+04 1.002493481e+01 3.0e-01 0.03
3 1.9e+02 2.7e+03 3.1e+03 6.47e-01 -5.771883934e+03 1.375649329e+01 1.7e-01 0.03
4 5.8e+01 8.4e+02 9.8e+02 1.20e+00 -1.604999939e+03 1.625567845e+01 5.7e-02 0.03
5 3.1e+01 4.5e+02 5.2e+02 1.69e+00 -6.745231597e+02 1.621109942e+01 3.1e-02 0.03
6 1.0e+01 1.4e+02 1.7e+02 1.50e+00 -1.671132178e+02 1.570777426e+01 1.0e-02 0.04
7 4.4e+00 6.5e+01 7.4e+01 1.15e+00 -6.553629269e+01 1.497843182e+01 4.8e-03 0.04
8 2.1e+00 3.2e+01 3.6e+01 8.76e-01 -3.007572408e+01 1.440762799e+01 2.4e-03 0.04
9 9.9e-01 1.8e+01 1.7e+01 5.55e-01 -1.319812582e+01 1.384703465e+01 1.2e-03 0.04
10 3.3e-01 6.3e+00 5.6e+00 5.48e-01 1.823370487e+00 1.321186295e+01 4.6e-04 0.04
11 1.5e-01 3.2e+00 2.6e+00 6.35e-01 7.019845442e+00 1.295307085e+01 2.2e-04 0.04
12 9.8e-02 2.5e+00 1.7e+00 7.48e-01 8.809265040e+00 1.282119448e+01 1.4e-04 0.04
13 2.3e-02 1.5e+00 4.1e-01 8.18e-01 1.155756886e+01 1.259122704e+01 4.1e-05 0.04
14 7.4e-03 1.5e+00 1.3e-01 9.41e-01 1.219960883e+01 1.254375020e+01 1.5e-05 0.05
15 2.0e-03 1.5e+00 3.7e-02 9.82e-01 1.242500224e+01 1.252082718e+01 4.4e-06 0.05
16 6.0e-04 1.3e+00 1.1e-02 9.90e-01 1.248681380e+01 1.251547330e+01 1.3e-06 0.05
17 2.4e-04 1.0e+00 4.4e-03 9.91e-01 1.250280389e+01 1.251431402e+01 5.4e-07 0.05
18 2.1e-04 9.5e-01 4.0e-03 9.82e-01 1.250383155e+01 1.251422947e+01 4.9e-07 0.05
19 1.9e-04 8.6e-01 3.6e-03 9.42e-01 1.250478258e+01 1.251416353e+01 4.4e-07 0.05
20 1.7e-04 7.8e-01 3.2e-03 9.46e-01 1.250564377e+01 1.251410233e+01 3.9e-07 0.06
21 1.6e-04 7.2e-01 2.9e-03 1.07e+00 1.250667235e+01 1.251402866e+01 3.7e-07 0.06
22 1.4e-04 6.6e-01 2.6e-03 9.86e-01 1.250733488e+01 1.251398144e+01 3.3e-07 0.06
23 1.3e-04 6.0e-01 2.3e-03 9.65e-01 1.250795813e+01 1.251393465e+01 3.0e-07 0.06
24 1.1e-04 5.5e-01 2.1e-03 1.02e+00 1.250855592e+01 1.251389376e+01 2.7e-07 0.20
25 1.0e-04 5.1e-01 1.9e-03 1.04e+00 1.250913479e+01 1.251385173e+01 2.5e-07 0.36
26 9.2e-05 4.7e-01 1.7e-03 1.02e+00 1.250959942e+01 1.251381840e+01 2.2e-07 0.51
27 8.3e-05 4.3e-01 1.5e-03 9.64e-01 1.250999380e+01 1.251378965e+01 2.0e-07 0.67
28 7.5e-05 4.0e-01 1.4e-03 8.64e-01 1.251033549e+01 1.251376704e+01 1.8e-07 0.73
29 6.7e-05 3.7e-01 1.2e-03 9.39e-01 1.251064723e+01 1.251374763e+01 1.6e-07 0.73
30 6.1e-05 3.4e-01 1.1e-03 9.34e-01 1.251094033e+01 1.251372624e+01 1.5e-07 0.73
31 5.4e-05 3.2e-01 1.0e-03 1.01e+00 1.251121488e+01 1.251370604e+01 1.3e-07 0.73
32 4.9e-05 2.9e-01 9.1e-04 7.61e-01 1.251143521e+01 1.251369168e+01 1.2e-07 0.74
33 4.4e-05 2.9e-01 8.2e-04 1.05e+00 1.251171365e+01 1.251366881e+01 1.1e-07 0.74
34 4.0e-05 2.6e-01 7.3e-04 1.17e+00 1.251202759e+01 1.251364903e+01 1.1e-07 0.74
35 3.6e-05 2.5e-01 6.6e-04 1.06e+00 1.251220722e+01 1.251363779e+01 9.9e-08 0.74
36 3.2e-05 2.5e-01 6.0e-04 1.02e+00 1.251237051e+01 1.251362294e+01 9.0e-08 0.75
37 2.9e-05 2.4e-01 5.4e-04 1.30e+00 1.251250098e+01 1.251361172e+01 8.1e-08 0.75
38 2.6e-05 2.4e-01 4.8e-04 1.35e+00 1.251261859e+01 1.251360205e+01 7.3e-08 0.75
39 2.3e-05 2.3e-01 4.3e-04 1.30e+00 1.251271393e+01 1.251359589e+01 6.5e-08 0.76
40 2.1e-05 2.0e-01 3.9e-04 1.04e+00 1.251282651e+01 1.251358625e+01 5.9e-08 0.76
41 1.9e-05 1.8e-01 3.5e-04 6.75e-01 1.251287829e+01 1.251358638e+01 5.4e-08 0.76
42 1.7e-05 1.8e-01 3.2e-04 8.93e-01 1.251294542e+01 1.251358247e+01 4.8e-08 0.76
43 1.5e-05 1.7e-01 2.8e-04 1.04e+00 1.251300997e+01 1.251357953e+01 4.4e-08 0.79
44 1.4e-05 1.7e-01 2.6e-04 1.31e+00 1.251306773e+01 1.251357520e+01 4.0e-08 0.79
45 1.2e-05 1.5e-01 2.3e-04 1.11e+00 1.251313734e+01 1.251357120e+01 3.8e-08 0.79
46 2.1e-06 2.2e-02 3.4e-05 3.96e-01 1.251348522e+01 1.251356043e+01 9.5e-09 0.79
47 1.9e-06 2.0e-02 3.0e-05 1.95e+00 1.251348882e+01 1.251356103e+01 8.6e-09 0.80
48 2.8e-06 1.5e-03 2.3e-06 7.92e-01 1.251356279e+01 1.251357599e+01 2.3e-09 0.80
49 1.8e-05 1.5e-03 2.2e-06 9.15e-01 1.251356308e+01 1.251357591e+01 2.2e-09 0.80
50 5.3e-06 4.3e-04 6.5e-07 9.99e-01 1.251355145e+01 1.251355527e+01 6.5e-10 0.80
51 4.8e-06 3.9e-04 5.8e-07 1.41e+00 1.251355113e+01 1.251355463e+01 5.8e-10 0.80
52 4.3e-06 3.5e-04 5.2e-07 4.76e-01 1.251355052e+01 1.251355364e+01 5.2e-10 0.81
53 3.8e-06 3.2e-04 4.7e-07 7.09e-01 1.251355134e+01 1.251355447e+01 4.7e-10 0.81
54 3.5e-06 2.8e-04 4.5e-07 1.00e+00 1.251355074e+01 1.251355369e+01 4.2e-10 0.81
55 3.1e-06 2.6e-04 4.0e-07 1.27e+00 1.251355042e+01 1.251355310e+01 3.8e-10 0.81
56 2.8e-06 2.3e-04 3.6e-07 5.40e+00 1.251354929e+01 1.251355152e+01 3.4e-10 0.81
57 4.1e-07 2.4e-05 3.8e-08 9.57e-01 1.251354692e+01 1.251354717e+01 3.9e-11 0.81
Interior-point optimizer terminated. Time: 0.82.
Optimizer terminated. Time: 0.83
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.2513546924e+01 Viol. con: 2e-06 var: 0e+00
Dual. obj: 1.2513547165e+01 Viol. con: 0e+00 var: 3e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.856 seconds.
result packing took 32% of solve time
solution checking took 10% 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 : MACOSX/64-X86
Cores : 8
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 : 1044
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1044
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 : 8
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 : 6496 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 2.5e+03 3.8e+03 5.1e+03 0.00e+00 -5.076391716e+03 1.023181539e-12 1.0e+00 0.03
1 8.2e+02 1.2e+03 1.7e+03 1.03e-01 -2.262606312e+03 9.793259309e+00 3.5e-01 0.09
2 3.1e+02 4.6e+02 6.4e+02 1.32e+00 -7.031177110e+02 1.364099335e+01 1.4e-01 0.12
3 1.9e+02 2.9e+02 4.0e+02 1.69e+00 -3.608126332e+02 1.379009519e+01 9.0e-02 0.15
4 4.9e+01 7.6e+01 1.0e+02 1.51e+00 -6.493574175e+01 1.334036736e+01 2.4e-02 0.21
5 1.2e+01 2.1e+01 2.7e+01 1.21e+00 -6.998698640e+00 1.169175514e+01 7.1e-03 0.21
6 3.0e+00 8.9e+00 6.6e+00 1.07e+00 6.331233451e+00 1.077607668e+01 1.9e-03 0.21
7 1.5e+00 8.7e+00 3.4e+00 9.48e-01 8.201034541e+00 1.061891704e+01 1.0e-03 0.21
8 8.8e-01 8.5e+00 2.0e+00 6.43e-01 8.689761083e+00 1.052144796e+01 6.2e-04 0.21
9 5.9e-01 6.2e+00 1.3e+00 5.19e-01 9.027360023e+00 1.046194807e+01 4.3e-04 0.21
10 1.3e-01 4.0e+00 3.0e-01 5.66e-01 9.865226607e+00 1.029329488e+01 1.2e-04 0.22
11 4.3e-02 3.9e+00 1.1e-01 8.05e-01 1.007786780e+01 1.024038951e+01 4.5e-05 0.22
12 1.3e-02 3.3e+00 3.2e-02 9.18e-01 1.016511293e+01 1.021509304e+01 1.4e-05 0.22
13 3.3e-03 3.1e+00 8.7e-03 9.76e-01 1.019307657e+01 1.020672791e+01 3.9e-06 0.22
14 1.1e-03 3.0e+00 3.0e-03 9.94e-01 1.020008182e+01 1.020476509e+01 1.4e-06 0.22
15 3.5e-04 3.0e+00 9.1e-04 9.98e-01 1.020259316e+01 1.020402634e+01 4.2e-07 0.22
16 1.3e-04 2.6e+00 3.5e-04 9.99e-01 1.020328441e+01 1.020383211e+01 1.6e-07 0.22
17 1.2e-04 2.4e+00 3.1e-04 1.00e+00 1.020332474e+01 1.020381851e+01 1.4e-07 0.23
18 1.1e-04 2.2e+00 2.8e-04 1.00e+00 1.020336268e+01 1.020380715e+01 1.3e-07 0.23
19 9.6e-05 2.0e+00 2.5e-04 1.00e+00 1.020339713e+01 1.020379716e+01 1.2e-07 0.23
20 8.6e-05 1.8e+00 2.3e-04 1.00e+00 1.020342816e+01 1.020378820e+01 1.0e-07 0.23
21 7.8e-05 1.6e+00 2.0e-04 1.00e+00 1.020345612e+01 1.020378016e+01 9.4e-08 0.23
22 7.0e-05 1.5e+00 1.8e-04 1.00e+00 1.020348131e+01 1.020377294e+01 8.5e-08 0.23
23 6.3e-05 1.3e+00 1.7e-04 1.00e+00 1.020350399e+01 1.020376646e+01 7.6e-08 0.23
24 5.7e-05 1.2e+00 1.5e-04 1.00e+00 1.020352441e+01 1.020376064e+01 6.9e-08 0.24
25 5.1e-05 1.1e+00 1.3e-04 1.00e+00 1.020354280e+01 1.020375541e+01 6.2e-08 0.24
26 4.6e-05 1.0e+00 1.2e-04 1.00e+00 1.020355937e+01 1.020375072e+01 5.6e-08 0.24
27 4.1e-05 9.4e-01 1.1e-04 1.00e+00 1.020357428e+01 1.020374650e+01 5.0e-08 0.24
28 3.7e-05 8.7e-01 9.8e-05 1.00e+00 1.020358771e+01 1.020374271e+01 4.5e-08 0.24
29 3.3e-05 8.0e-01 8.8e-05 1.00e+00 1.020359981e+01 1.020373930e+01 4.1e-08 0.24
30 3.0e-05 7.3e-01 7.9e-05 1.00e+00 1.020361069e+01 1.020373624e+01 3.7e-08 0.24
31 2.7e-05 6.8e-01 7.1e-05 1.00e+00 1.020362050e+01 1.020373349e+01 3.3e-08 0.25
32 2.4e-05 6.3e-01 6.4e-05 1.00e+00 1.020362932e+01 1.020373102e+01 3.0e-08 0.25
33 2.2e-05 5.8e-01 5.8e-05 1.00e+00 1.020363727e+01 1.020372880e+01 2.7e-08 0.25
34 2.0e-05 5.4e-01 5.2e-05 1.00e+00 1.020364443e+01 1.020372680e+01 2.4e-08 0.26
35 1.8e-05 5.1e-01 4.7e-05 1.00e+00 1.020365087e+01 1.020372501e+01 2.2e-08 0.26
36 1.6e-05 4.7e-01 4.2e-05 1.00e+00 1.020365667e+01 1.020372339e+01 1.9e-08 0.26
37 1.4e-05 4.5e-01 3.8e-05 1.00e+00 1.020366189e+01 1.020372194e+01 1.7e-08 0.26
38 1.3e-05 4.2e-01 3.4e-05 1.00e+00 1.020366659e+01 1.020372064e+01 1.6e-08 0.26
39 1.2e-05 4.0e-01 3.1e-05 1.00e+00 1.020367082e+01 1.020371946e+01 1.4e-08 0.26
40 1.1e-05 3.7e-01 2.8e-05 1.00e+00 1.020367463e+01 1.020371841e+01 1.3e-08 0.26
41 9.5e-06 3.5e-01 2.5e-05 1.00e+00 1.020367806e+01 1.020371746e+01 1.1e-08 0.26
42 1.0e-06 3.7e-02 2.6e-06 1.00e+00 1.020370568e+01 1.020370985e+01 1.2e-09 0.27
43 6.8e-08 2.5e-03 1.8e-07 9.99e-01 1.020370872e+01 1.020370901e+01 8.4e-11 0.27
44 1.2e-08 4.5e-04 3.2e-08 1.00e+00 1.020370891e+01 1.020370896e+01 1.5e-11 0.27
45 2.9e-09 1.1e-04 7.7e-09 1.04e+00 1.020370894e+01 1.020370895e+01 3.5e-12 0.27
46 1.8e-10 6.9e-06 4.9e-10 1.02e+00 1.020370895e+01 1.020370895e+01 2.0e-13 0.27
Interior-point optimizer terminated. Time: 0.27.
Optimizer terminated. Time: 0.29
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0203708947e+01 Viol. con: 2e-10 var: 0e+00
Dual. obj: 1.0203708947e+01 Viol. con: 0e+00 var: 2e-06
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.312 seconds.
result packing took 70% of solve time
solution checking took 38% 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 : MACOSX/64-X86
Cores : 8
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 : 1024
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 : 8
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 -7.646714257e+03 1.023181539e-12 1.0e+00 0.03
1 7.9e+02 1.2e+03 2.4e+03 4.43e-03 -3.439951897e+03 9.865562676e+00 3.4e-01 0.03
2 5.5e+02 8.3e+02 1.7e+03 1.39e+00 -2.072275034e+03 1.199515115e+01 2.4e-01 0.03
3 2.4e+02 3.6e+02 7.4e+02 1.50e+00 -7.270989008e+02 1.390012936e+01 1.1e-01 0.03
4 7.2e+01 1.1e+02 2.2e+02 1.65e+00 -1.536450788e+02 1.372034501e+01 3.4e-02 0.03
5 1.9e+01 3.1e+01 5.8e+01 1.27e+00 -2.763392199e+01 1.211215709e+01 9.8e-03 0.03
6 4.5e+00 1.2e+01 1.4e+01 1.05e+00 1.436322391e+00 1.092816410e+01 2.7e-03 0.03
7 2.1e+00 1.1e+01 6.5e+00 9.71e-01 6.193059377e+00 1.068618351e+01 1.3e-03 0.03
8 1.9e+00 9.6e+00 5.9e+00 7.00e-01 6.369635690e+00 1.066665711e+01 1.2e-03 0.04
9 7.5e-01 7.8e+00 2.4e+00 6.46e-01 8.110270538e+00 1.049629732e+01 5.4e-04 0.04
10 6.1e-01 6.3e+00 1.9e+00 5.13e-01 8.387130703e+00 1.045979674e+01 4.3e-04 0.04
11 1.9e-01 3.0e+00 6.4e-01 5.08e-01 9.417598516e+00 1.031757266e+01 1.6e-04 0.04
12 8.2e-02 3.1e+00 2.7e-01 7.46e-01 9.843808482e+00 1.025740484e+01 7.4e-05 0.04
13 7.4e-02 2.8e+00 2.5e-01 8.54e-01 9.883253514e+00 1.025562170e+01 6.6e-05 0.04
14 6.6e-02 2.6e+00 2.2e-01 8.50e-01 9.912635802e+00 1.025014193e+01 6.0e-05 0.05
15 6.0e-02 2.3e+00 2.0e-01 8.61e-01 9.939033152e+00 1.024491217e+01 5.4e-05 0.05
16 5.4e-02 2.1e+00 1.8e-01 8.72e-01 9.963015571e+00 1.024007304e+01 4.8e-05 0.05
17 4.8e-02 1.9e+00 1.6e-01 8.83e-01 9.984805877e+00 1.023562243e+01 4.4e-05 0.05
18 4.4e-02 1.8e+00 1.5e-01 8.93e-01 1.000459384e+01 1.023153876e+01 3.9e-05 0.05
19 3.9e-02 1.6e+00 1.3e-01 9.03e-01 1.002254984e+01 1.022779833e+01 3.5e-05 0.05
20 3.5e-02 1.5e+00 1.2e-01 9.12e-01 1.003883189e+01 1.022437753e+01 3.2e-05 0.05
21 3.2e-02 1.3e+00 1.1e-01 9.20e-01 1.005358632e+01 1.022125349e+01 2.9e-05 0.05
22 2.9e-02 1.2e+00 9.6e-02 9.27e-01 1.006694839e+01 1.021840424e+01 2.6e-05 0.06
23 2.6e-02 1.1e+00 8.6e-02 9.34e-01 1.007904283e+01 1.021580878e+01 2.3e-05 0.06
24 2.3e-02 1.0e+00 7.8e-02 9.40e-01 1.008998438e+01 1.021344717e+01 2.1e-05 0.06
25 2.1e-02 9.6e-01 7.0e-02 9.45e-01 1.009987833e+01 1.021130053e+01 1.9e-05 0.06
26 1.9e-02 8.8e-01 6.3e-02 9.51e-01 1.010882118e+01 1.020935111e+01 1.7e-05 0.06
27 1.7e-02 8.1e-01 5.7e-02 9.55e-01 1.011690122e+01 1.020758229e+01 1.5e-05 0.06
28 1.5e-02 7.5e-01 5.1e-02 9.60e-01 1.012419910e+01 1.020597860e+01 1.4e-05 0.06
29 1.4e-02 7.0e-01 4.6e-02 9.64e-01 1.013078844e+01 1.020452568e+01 1.2e-05 0.07
30 1.2e-02 6.5e-01 4.1e-02 9.67e-01 1.013673631e+01 1.020321027e+01 1.1e-05 0.07
31 1.1e-02 6.0e-01 3.7e-02 9.70e-01 1.014210378e+01 1.020202014e+01 1.0e-05 0.07
32 1.0e-02 5.6e-01 3.3e-02 9.73e-01 1.014694640e+01 1.020094402e+01 9.1e-06 0.07
33 9.0e-03 5.2e-01 3.0e-02 9.76e-01 1.015131460e+01 1.019997159e+01 8.2e-06 0.08
34 8.1e-03 4.9e-01 2.7e-02 9.79e-01 1.015525417e+01 1.019909336e+01 7.3e-06 0.08
35 7.3e-03 4.6e-01 2.4e-02 9.81e-01 1.015880663e+01 1.019830064e+01 6.6e-06 0.08
36 6.5e-03 4.3e-01 2.2e-02 9.83e-01 1.016200956e+01 1.019758547e+01 5.9e-06 0.08
37 5.9e-03 4.1e-01 2.0e-02 9.85e-01 1.016489702e+01 1.019694059e+01 5.4e-06 0.08
38 5.3e-03 3.8e-01 1.8e-02 9.86e-01 1.016749979e+01 1.019635934e+01 4.8e-06 0.08
39 4.8e-03 3.6e-01 1.6e-02 9.88e-01 1.016984572e+01 1.019583568e+01 4.3e-06 0.08
40 4.3e-03 3.5e-01 1.4e-02 9.89e-01 1.017195998e+01 1.019536408e+01 3.9e-06 0.08
41 3.9e-03 3.3e-01 1.3e-02 9.90e-01 1.017386528e+01 1.019493950e+01 3.5e-06 0.09
42 3.5e-03 3.1e-01 1.2e-02 9.91e-01 1.017558217e+01 1.019455738e+01 3.2e-06 0.09
43 3.1e-03 3.0e-01 1.1e-02 9.92e-01 1.017712915e+01 1.019421356e+01 2.8e-06 0.09
44 2.8e-03 2.9e-01 9.5e-03 9.93e-01 1.017852293e+01 1.019390426e+01 2.6e-06 0.09
45 2.5e-03 2.8e-01 8.5e-03 9.94e-01 1.017977861e+01 1.019362605e+01 2.3e-06 0.09
46 2.3e-03 2.7e-01 7.7e-03 9.95e-01 1.018090978e+01 1.019337584e+01 2.1e-06 0.09
47 2.1e-03 2.6e-01 6.9e-03 9.95e-01 1.018192872e+01 1.019315083e+01 1.9e-06 0.09
48 1.8e-03 2.5e-01 6.2e-03 9.96e-01 1.018284650e+01 1.019294849e+01 1.7e-06 0.10
49 1.7e-03 2.4e-01 5.6e-03 9.96e-01 1.018367312e+01 1.019276654e+01 1.5e-06 0.10
50 1.5e-03 2.4e-01 5.0e-03 9.97e-01 1.018441758e+01 1.019260295e+01 1.4e-06 0.10
51 1.3e-03 2.3e-01 4.5e-03 9.97e-01 1.018508803e+01 1.019245585e+01 1.2e-06 0.10
52 1.2e-03 2.3e-01 4.1e-03 9.98e-01 1.018569179e+01 1.019232359e+01 1.1e-06 0.10
53 1.1e-03 2.2e-01 3.7e-03 9.98e-01 1.018623547e+01 1.019220469e+01 9.9e-07 0.10
54 9.8e-04 2.2e-01 3.3e-03 9.98e-01 1.018672505e+01 1.019209779e+01 8.9e-07 0.10
55 8.8e-04 2.1e-01 3.0e-03 9.98e-01 1.018716590e+01 1.019200170e+01 8.1e-07 0.11
56 7.9e-04 2.1e-01 2.7e-03 9.99e-01 1.018756285e+01 1.019191533e+01 7.2e-07 0.11
57 7.2e-04 2.1e-01 2.4e-03 9.99e-01 1.018792029e+01 1.019183771e+01 6.5e-07 0.11
58 6.4e-04 2.0e-01 2.2e-03 9.99e-01 1.018824214e+01 1.019176795e+01 5.9e-07 0.11
59 5.8e-04 2.0e-01 1.9e-03 9.99e-01 1.018853194e+01 1.019170528e+01 5.3e-07 0.11
60 5.2e-04 2.0e-01 1.8e-03 1.00e+00 1.018879290e+01 1.019164896e+01 4.8e-07 0.11
61 4.7e-04 2.0e-01 1.6e-03 1.00e+00 1.018902787e+01 1.019159838e+01 4.3e-07 0.11
62 4.2e-04 1.9e-01 1.4e-03 1.00e+00 1.018923946e+01 1.019155294e+01 3.9e-07 0.11
63 3.8e-04 1.9e-01 1.3e-03 1.00e+00 1.018942998e+01 1.019151213e+01 3.5e-07 0.12
64 3.4e-04 1.9e-01 1.2e-03 1.00e+00 1.018960153e+01 1.019147547e+01 3.1e-07 0.12
65 3.1e-04 1.9e-01 1.0e-03 1.00e+00 1.018975599e+01 1.019144254e+01 2.8e-07 0.12
66 2.8e-04 1.9e-01 9.3e-04 1.00e+00 1.018989507e+01 1.019141296e+01 2.5e-07 0.12
67 2.5e-04 1.9e-01 8.4e-04 1.00e+00 1.019002030e+01 1.019138639e+01 2.3e-07 0.12
68 2.2e-04 1.8e-01 7.6e-04 1.00e+00 1.019013305e+01 1.019136252e+01 2.0e-07 0.12
69 2.0e-04 1.8e-01 6.8e-04 1.00e+00 1.019023456e+01 1.019134108e+01 1.8e-07 0.12
70 1.8e-04 1.8e-01 6.1e-04 1.00e+00 1.019032596e+01 1.019132182e+01 1.7e-07 0.13
71 1.6e-04 1.8e-01 5.5e-04 1.00e+00 1.019040825e+01 1.019130451e+01 1.5e-07 0.13
72 1.5e-04 1.8e-01 5.0e-04 1.00e+00 1.019048234e+01 1.019128897e+01 1.3e-07 0.13
73 1.3e-04 1.8e-01 4.5e-04 1.00e+00 1.019054905e+01 1.019127500e+01 1.2e-07 0.13
74 1.2e-04 1.8e-01 4.0e-04 1.00e+00 1.019060911e+01 1.019126246e+01 1.1e-07 0.13
75 1.1e-04 1.8e-01 3.6e-04 1.00e+00 1.019066318e+01 1.019125119e+01 9.8e-08 0.13
76 9.7e-05 1.8e-01 3.3e-04 1.00e+00 1.019071187e+01 1.019124107e+01 8.8e-08 0.13
77 8.7e-05 1.8e-01 2.9e-04 1.00e+00 1.019075571e+01 1.019123198e+01 7.9e-08 0.13
78 7.8e-05 1.8e-01 2.6e-04 1.00e+00 1.019079518e+01 1.019122382e+01 7.1e-08 0.14
79 7.0e-05 1.8e-01 2.4e-04 1.00e+00 1.019083072e+01 1.019121649e+01 6.4e-08 0.14
80 6.3e-05 1.8e-01 2.1e-04 1.00e+00 1.019086272e+01 1.019120991e+01 5.8e-08 0.14
81 5.7e-05 1.8e-01 1.9e-04 1.00e+00 1.019089153e+01 1.019120400e+01 5.2e-08 0.14
82 5.1e-05 1.8e-01 1.7e-04 1.00e+00 1.019091747e+01 1.019119869e+01 4.7e-08 0.14
83 4.6e-05 1.8e-01 1.6e-04 1.00e+00 1.019094083e+01 1.019119392e+01 4.2e-08 0.14
84 4.2e-05 1.8e-01 1.4e-04 1.00e+00 1.019096186e+01 1.019118964e+01 3.8e-08 0.14
85 3.7e-05 1.8e-01 1.3e-04 1.00e+00 1.019098079e+01 1.019118579e+01 3.4e-08 0.15
86 3.4e-05 1.8e-01 1.1e-04 1.00e+00 1.019099784e+01 1.019118234e+01 3.1e-08 0.15
87 3.0e-05 1.7e-01 1.0e-04 1.00e+00 1.019101318e+01 1.019117923e+01 2.8e-08 0.15
88 2.7e-05 1.7e-01 9.2e-05 1.00e+00 1.019102700e+01 1.019117644e+01 2.5e-08 0.15
89 2.5e-05 1.7e-01 8.3e-05 1.00e+00 1.019103944e+01 1.019117393e+01 2.2e-08 0.15
90 2.2e-05 1.7e-01 7.4e-05 1.00e+00 1.019105063e+01 1.019117168e+01 2.0e-08 0.15
91 2.0e-05 1.7e-01 6.7e-05 1.00e+00 1.019106071e+01 1.019116965e+01 1.8e-08 0.15
92 1.8e-05 1.7e-01 6.0e-05 1.00e+00 1.019106979e+01 1.019116783e+01 1.6e-08 0.15
93 1.6e-05 1.7e-01 5.4e-05 1.00e+00 1.019107795e+01 1.019116619e+01 1.5e-08 0.16
94 1.4e-05 1.7e-01 4.9e-05 1.00e+00 1.019108531e+01 1.019116472e+01 1.3e-08 0.16
95 1.3e-05 1.7e-01 4.4e-05 1.00e+00 1.019109192e+01 1.019116340e+01 1.2e-08 0.16
96 1.2e-05 1.7e-01 4.0e-05 1.00e+00 1.019109788e+01 1.019116221e+01 1.1e-08 0.16
97 1.1e-05 1.7e-01 3.6e-05 1.00e+00 1.019110324e+01 1.019116114e+01 9.7e-09 0.16
98 9.5e-06 1.7e-01 3.2e-05 1.00e+00 1.019110807e+01 1.019116017e+01 8.7e-09 0.16
99 8.6e-06 1.7e-01 2.9e-05 1.00e+00 1.019111242e+01 1.019115931e+01 7.8e-09 0.16
100 7.7e-06 1.7e-01 2.6e-05 1.00e+00 1.019111633e+01 1.019115853e+01 7.0e-09 0.17
101 6.9e-06 1.7e-01 2.3e-05 1.00e+00 1.019111985e+01 1.019115783e+01 6.3e-09 0.17
102 6.2e-06 1.7e-01 2.1e-05 1.00e+00 1.019112302e+01 1.019115720e+01 5.7e-09 0.17
103 5.6e-06 1.7e-01 1.9e-05 1.00e+00 1.019112587e+01 1.019115663e+01 5.1e-09 0.17
104 5.1e-06 1.7e-01 1.7e-05 1.00e+00 1.019112843e+01 1.019115612e+01 4.6e-09 0.17
105 4.5e-06 1.7e-01 1.5e-05 1.00e+00 1.019113075e+01 1.019115567e+01 4.2e-09 0.17
106 4.1e-06 1.7e-01 1.4e-05 1.00e+00 1.019113283e+01 1.019115525e+01 3.7e-09 0.17
107 3.7e-06 1.7e-01 1.2e-05 1.00e+00 1.019113470e+01 1.019115488e+01 3.4e-09 0.17
108 3.3e-06 1.7e-01 1.1e-05 1.00e+00 1.019113638e+01 1.019115455e+01 3.0e-09 0.18
109 3.0e-06 1.7e-01 1.0e-05 1.00e+00 1.019113790e+01 1.019115425e+01 2.7e-09 0.18
110 2.7e-06 1.7e-01 9.0e-06 1.00e+00 1.019113926e+01 1.019115398e+01 2.5e-09 0.18
111 2.4e-06 1.7e-01 8.1e-06 1.00e+00 1.019114049e+01 1.019115374e+01 2.2e-09 0.18
112 2.2e-06 1.7e-01 7.3e-06 1.00e+00 1.019114160e+01 1.019115352e+01 2.0e-09 0.18
113 2.0e-06 1.7e-01 6.6e-06 1.00e+00 1.019114259e+01 1.019115332e+01 1.8e-09 0.18
114 1.8e-06 1.7e-01 5.9e-06 1.00e+00 1.019114349e+01 1.019115314e+01 1.6e-09 0.18
115 1.6e-06 1.7e-01 5.3e-06 9.99e-01 1.019114430e+01 1.019115298e+01 1.4e-09 0.19
116 1.4e-06 1.5e-01 4.8e-06 1.00e+00 1.019114502e+01 1.019115284e+01 1.3e-09 0.19
117 1.3e-06 1.4e-01 4.3e-06 1.00e+00 1.019114567e+01 1.019115271e+01 1.2e-09 0.19
118 1.2e-06 1.3e-01 3.9e-06 1.00e+00 1.019114626e+01 1.019115260e+01 1.1e-09 0.19
119 1.0e-06 1.1e-01 3.5e-06 1.00e+00 1.019114679e+01 1.019115249e+01 9.5e-10 0.19
120 9.4e-07 1.0e-01 3.2e-06 1.00e+00 1.019114727e+01 1.019115240e+01 8.6e-10 0.19
121 8.4e-07 9.1e-02 2.8e-06 1.00e+00 1.019114770e+01 1.019115231e+01 7.7e-10 0.19
122 7.6e-07 8.2e-02 2.6e-06 9.99e-01 1.019114808e+01 1.019115224e+01 6.9e-10 0.19
123 6.8e-07 7.4e-02 2.3e-06 1.00e+00 1.019114843e+01 1.019115217e+01 6.2e-10 0.20
124 6.1e-07 6.7e-02 2.1e-06 9.99e-01 1.019114874e+01 1.019115211e+01 5.6e-10 0.20
125 5.5e-07 6.0e-02 1.9e-06 1.00e+00 1.019114902e+01 1.019115205e+01 5.1e-10 0.20
126 5.0e-07 5.4e-02 1.7e-06 9.99e-01 1.019114928e+01 1.019115200e+01 4.5e-10 0.21
127 4.5e-07 4.9e-02 1.5e-06 1.00e+00 1.019114951e+01 1.019115196e+01 4.1e-10 0.21
128 4.0e-07 4.4e-02 1.4e-06 9.99e-01 1.019114971e+01 1.019115192e+01 3.7e-10 0.21
129 3.6e-07 3.9e-02 1.2e-06 1.00e+00 1.019114989e+01 1.019115188e+01 3.3e-10 0.21
130 3.3e-07 3.5e-02 1.1e-06 9.97e-01 1.019115006e+01 1.019115185e+01 3.0e-10 0.21
131 2.9e-07 3.2e-02 9.9e-07 1.01e+00 1.019115022e+01 1.019115182e+01 2.7e-10 0.21
132 2.6e-07 2.9e-02 8.9e-07 9.99e-01 1.019115035e+01 1.019115179e+01 2.4e-10 0.21
133 2.4e-07 2.6e-02 8.0e-07 9.94e-01 1.019115047e+01 1.019115177e+01 2.2e-10 0.22
134 2.1e-07 2.3e-02 7.2e-07 1.01e+00 1.019115058e+01 1.019115174e+01 2.0e-10 0.22
135 1.9e-07 2.1e-02 6.5e-07 1.01e+00 1.019115068e+01 1.019115173e+01 1.8e-10 0.22
136 1.7e-07 1.9e-02 5.8e-07 1.01e+00 1.019115077e+01 1.019115171e+01 1.6e-10 0.22
137 1.6e-07 1.7e-02 5.3e-07 1.02e+00 1.019115086e+01 1.019115169e+01 1.5e-10 0.22
138 1.4e-07 1.5e-02 4.7e-07 1.00e+00 1.019115093e+01 1.019115168e+01 1.3e-10 0.22
139 1.3e-07 1.4e-02 4.3e-07 1.01e+00 1.019115099e+01 1.019115166e+01 1.2e-10 0.22
140 1.1e-07 1.2e-02 3.8e-07 9.95e-01 1.019115105e+01 1.019115165e+01 1.1e-10 0.22
141 1.2e-08 1.3e-03 4.0e-08 1.01e+00 1.019115150e+01 1.019115156e+01 1.1e-11 0.23
142 1.2e-09 8.7e-05 2.7e-09 9.97e-01 1.019115155e+01 1.019115155e+01 6.4e-13 0.23
Interior-point optimizer terminated. Time: 0.23.
Optimizer terminated. Time: 0.24
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0191151551e+01 Viol. con: 8e-10 var: 0e+00
Dual. obj: 1.0191151555e+01 Viol. con: 0e+00 var: 3e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.266 seconds.
result packing took 84% of solve time
solution checking took 40% 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 : MACOSX/64-X86
Cores : 8
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 : 8
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 3.7e+03 5.3e+03 0.00e+00 -5.296202970e+03 1.023181539e-12 1.0e+00 0.02
1 8.5e+02 1.2e+03 1.7e+03 1.11e-03 -2.376466181e+03 9.885579213e+00 3.4e-01 0.03
2 5.9e+02 8.0e+02 1.1e+03 1.39e+00 -1.418132784e+03 1.206000357e+01 2.3e-01 0.03
3 2.2e+02 3.0e+02 4.4e+02 1.52e+00 -4.109368604e+02 1.409918939e+01 9.3e-02 0.03
4 6.6e+01 9.0e+01 1.3e+02 1.67e+00 -8.392014750e+01 1.359201268e+01 2.9e-02 0.03
5 1.6e+01 2.6e+01 3.3e+01 1.21e+00 -1.083002805e+01 1.187823018e+01 8.2e-03 0.03
6 5.3e+00 1.6e+01 1.1e+01 1.04e+00 3.446159767e+00 1.095662092e+01 2.9e-03 0.03
7 2.2e+00 1.3e+01 4.5e+00 9.90e-01 7.495529052e+00 1.065233851e+01 1.3e-03 0.03
8 2.0e+00 1.2e+01 4.1e+00 7.11e-01 7.616656456e+00 1.063384041e+01 1.2e-03 0.04
9 7.6e-01 9.1e+00 1.6e+00 6.62e-01 8.866434694e+00 1.045993759e+01 5.1e-04 0.04
10 5.3e-01 8.9e+00 1.1e+00 5.22e-01 9.162400649e+00 1.040172449e+01 3.6e-04 0.04
11 1.8e-01 3.8e+00 4.0e-01 5.32e-01 9.723476849e+00 1.028165314e+01 1.4e-04 0.04
12 6.7e-02 3.7e+00 1.5e-01 7.74e-01 9.991204486e+00 1.022241216e+01 5.8e-05 0.04
13 1.4e-02 3.4e+00 3.5e-02 8.82e-01 1.012712155e+01 1.018244658e+01 1.5e-05 0.04
14 5.6e-03 3.0e+00 1.4e-02 9.81e-01 1.015355564e+01 1.017529304e+01 5.9e-06 0.04
15 1.8e-03 2.6e+00 4.4e-03 9.93e-01 1.016475377e+01 1.017187054e+01 1.9e-06 0.05
16 6.2e-04 2.4e+00 1.5e-03 9.98e-01 1.016836749e+01 1.017080172e+01 6.7e-07 0.05
17 2.8e-04 2.0e+00 6.9e-04 1.00e+00 1.016940713e+01 1.017050969e+01 3.0e-07 0.05
18 1.1e-04 1.9e+00 2.8e-04 1.00e+00 1.016991428e+01 1.017036555e+01 1.2e-07 0.05
19 1.0e-04 1.8e+00 2.5e-04 1.00e+00 1.016994965e+01 1.017035651e+01 1.1e-07 0.05
20 9.3e-05 1.7e+00 2.3e-04 1.00e+00 1.016998099e+01 1.017034724e+01 1.0e-07 0.05
21 8.3e-05 1.5e+00 2.1e-04 1.00e+00 1.017000944e+01 1.017033906e+01 9.1e-08 0.05
22 7.5e-05 1.4e+00 1.8e-04 1.00e+00 1.017003504e+01 1.017033169e+01 8.2e-08 0.06
23 6.7e-05 1.3e+00 1.7e-04 1.00e+00 1.017005810e+01 1.017032508e+01 7.3e-08 0.06
24 6.1e-05 1.2e+00 1.5e-04 1.00e+00 1.017007886e+01 1.017031915e+01 6.6e-08 0.06
25 5.5e-05 1.1e+00 1.3e-04 1.00e+00 1.017009756e+01 1.017031381e+01 5.9e-08 0.06
26 4.9e-05 9.7e-01 1.2e-04 1.00e+00 1.017011439e+01 1.017030902e+01 5.4e-08 0.06
27 4.4e-05 8.9e-01 1.1e-04 1.00e+00 1.017012955e+01 1.017030471e+01 4.8e-08 0.06
28 4.0e-05 8.2e-01 9.8e-05 1.00e+00 1.017014319e+01 1.017030084e+01 4.3e-08 0.06
29 3.6e-05 7.6e-01 8.8e-05 1.00e+00 1.017015548e+01 1.017029736e+01 3.9e-08 0.07
30 3.2e-05 7.0e-01 8.0e-05 1.00e+00 1.017016654e+01 1.017029423e+01 3.5e-08 0.07
31 2.9e-05 6.5e-01 7.2e-05 1.00e+00 1.017017649e+01 1.017029141e+01 3.2e-08 0.07
32 2.6e-05 6.0e-01 6.4e-05 1.00e+00 1.017018546e+01 1.017028888e+01 2.8e-08 0.07
33 2.4e-05 5.6e-01 5.8e-05 1.00e+00 1.017019353e+01 1.017028661e+01 2.6e-08 0.07
34 2.1e-05 5.2e-01 5.2e-05 1.00e+00 1.017020079e+01 1.017028457e+01 2.3e-08 0.07
35 1.9e-05 4.9e-01 4.7e-05 1.00e+00 1.017020733e+01 1.017028273e+01 2.1e-08 0.08
36 1.7e-05 4.5e-01 4.2e-05 1.00e+00 1.017021321e+01 1.017028107e+01 1.9e-08 0.08
37 1.5e-05 4.3e-01 3.8e-05 1.00e+00 1.017021851e+01 1.017027958e+01 1.7e-08 0.08
38 1.4e-05 4.0e-01 3.4e-05 1.00e+00 1.017022328e+01 1.017027825e+01 1.5e-08 0.08
39 1.3e-05 3.8e-01 3.1e-05 1.00e+00 1.017022757e+01 1.017027704e+01 1.4e-08 0.08
40 1.1e-05 3.6e-01 2.8e-05 1.00e+00 1.017023144e+01 1.017027596e+01 1.2e-08 0.08
41 1.0e-05 3.4e-01 2.5e-05 1.00e+00 1.017023491e+01 1.017027498e+01 1.1e-08 0.09
42 9.1e-06 3.2e-01 2.2e-05 1.00e+00 1.017023804e+01 1.017027411e+01 9.9e-09 0.09
43 8.2e-06 3.1e-01 2.0e-05 1.00e+00 1.017024086e+01 1.017027332e+01 8.9e-09 0.09
44 7.4e-06 3.0e-01 1.8e-05 1.00e+00 1.017024340e+01 1.017027261e+01 8.0e-09 0.09
45 6.6e-06 2.9e-01 1.6e-05 1.00e+00 1.017024568e+01 1.017027197e+01 7.2e-09 0.09
46 6.0e-06 2.7e-01 1.5e-05 1.00e+00 1.017024773e+01 1.017027139e+01 6.5e-09 0.09
47 5.4e-06 2.7e-01 1.3e-05 1.00e+00 1.017024958e+01 1.017027088e+01 5.9e-09 0.09
48 4.8e-06 2.6e-01 1.2e-05 1.00e+00 1.017025124e+01 1.017027041e+01 5.3e-09 0.10
49 4.4e-06 2.5e-01 1.1e-05 1.00e+00 1.017025274e+01 1.017026999e+01 4.7e-09 0.10
50 3.9e-06 2.4e-01 9.7e-06 1.00e+00 1.017025409e+01 1.017026961e+01 4.3e-09 0.10
51 3.5e-06 2.4e-01 8.7e-06 1.00e+00 1.017025530e+01 1.017026927e+01 3.8e-09 0.10
52 3.2e-06 2.3e-01 7.8e-06 1.00e+00 1.017025639e+01 1.017026897e+01 3.5e-09 0.10
53 2.9e-06 2.2e-01 7.1e-06 1.00e+00 1.017025738e+01 1.017026869e+01 3.1e-09 0.10
54 2.6e-06 2.2e-01 6.3e-06 1.00e+00 1.017025826e+01 1.017026845e+01 2.8e-09 0.10
55 2.3e-06 2.2e-01 5.7e-06 1.00e+00 1.017025906e+01 1.017026822e+01 2.5e-09 0.10
56 2.1e-06 2.1e-01 5.1e-06 1.00e+00 1.017025977e+01 1.017026802e+01 2.3e-09 0.11
57 1.9e-06 2.1e-01 4.6e-06 1.00e+00 1.017026042e+01 1.017026784e+01 2.0e-09 0.11
58 1.7e-06 2.1e-01 4.2e-06 9.99e-01 1.017026100e+01 1.017026768e+01 1.8e-09 0.11
59 1.5e-06 2.0e-01 3.7e-06 9.99e-01 1.017026152e+01 1.017026753e+01 1.7e-09 0.11
60 1.4e-06 2.0e-01 3.4e-06 1.00e+00 1.017026199e+01 1.017026740e+01 1.5e-09 0.11
61 1.2e-06 2.0e-01 3.0e-06 1.00e+00 1.017026241e+01 1.017026728e+01 1.3e-09 0.11
62 1.1e-06 2.0e-01 2.7e-06 1.00e+00 1.017026279e+01 1.017026717e+01 1.2e-09 0.11
63 1.0e-06 2.0e-01 2.5e-06 1.00e+00 1.017026313e+01 1.017026708e+01 1.1e-09 0.12
64 9.0e-07 1.9e-01 2.2e-06 1.00e+00 1.017026344e+01 1.017026699e+01 9.8e-10 0.12
65 8.1e-07 1.9e-01 2.0e-06 1.00e+00 1.017026372e+01 1.017026691e+01 8.8e-10 0.12
66 7.3e-07 1.9e-01 1.8e-06 9.99e-01 1.017026397e+01 1.017026684e+01 7.9e-10 0.12
67 6.5e-07 1.9e-01 1.6e-06 1.00e+00 1.017026419e+01 1.017026678e+01 7.1e-10 0.12
68 5.9e-07 1.9e-01 1.5e-06 1.01e+00 1.017026440e+01 1.017026672e+01 6.4e-10 0.12
69 5.3e-07 1.9e-01 1.3e-06 9.99e-01 1.017026458e+01 1.017026667e+01 5.8e-10 0.12
70 4.8e-07 1.9e-01 1.2e-06 1.00e+00 1.017026474e+01 1.017026662e+01 5.2e-10 0.12
71 4.3e-07 1.9e-01 1.1e-06 1.00e+00 1.017026489e+01 1.017026658e+01 4.7e-10 0.13
72 3.9e-07 1.9e-01 9.5e-07 9.99e-01 1.017026502e+01 1.017026655e+01 4.2e-10 0.13
73 3.5e-07 1.9e-01 8.6e-07 9.99e-01 1.017026514e+01 1.017026651e+01 3.8e-10 0.13
74 3.1e-07 1.9e-01 7.7e-07 9.95e-01 1.017026525e+01 1.017026648e+01 3.4e-10 0.13
75 2.8e-07 1.8e-01 6.9e-07 1.00e+00 1.017026534e+01 1.017026645e+01 3.1e-10 0.13
76 2.5e-07 1.8e-01 6.2e-07 9.92e-01 1.017026543e+01 1.017026643e+01 2.8e-10 0.13
77 2.3e-07 1.8e-01 5.6e-07 9.92e-01 1.017026551e+01 1.017026641e+01 2.5e-10 0.13
78 4.6e-08 3.7e-02 1.1e-07 9.98e-01 1.017026607e+01 1.017026625e+01 5.1e-11 0.14
79 6.7e-09 5.4e-03 1.7e-08 1.03e+00 1.017026619e+01 1.017026622e+01 7.0e-12 0.14
80 1.2e-10 5.0e-05 1.6e-10 1.00e+00 1.017026621e+01 1.017026621e+01 2.3e-13 0.14
Interior-point optimizer terminated. Time: 0.14.
Optimizer terminated. Time: 0.15
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0170266210e+01 Viol. con: 1e-10 var: 0e+00
Dual. obj: 1.0170266211e+01 Viol. con: 0e+00 var: 1e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.177 seconds.
result packing took 1.2e+02% of solve time
solution checking took 67% 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 : MACOSX/64-X86
Cores : 8
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 : 8
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 -7.721659233e+03 1.023181539e-12 1.0e+00 0.03
1 7.9e+02 1.2e+03 2.4e+03 -2.26e-03 -3.459676144e+03 9.890413027e+00 3.4e-01 0.03
2 5.9e+02 8.8e+02 1.8e+03 1.40e+00 -2.229481288e+03 1.171399358e+01 2.5e-01 0.03
3 3.8e+02 5.6e+02 1.2e+03 1.45e+00 -1.236886488e+03 1.314742870e+01 1.6e-01 0.03
4 1.3e+02 2.0e+02 4.0e+02 1.56e+00 -3.249841986e+02 1.397272967e+01 6.0e-02 0.04
5 4.2e+01 6.3e+01 1.3e+02 1.47e+00 -7.775316089e+01 1.298043259e+01 2.0e-02 0.04
6 1.1e+01 2.0e+01 3.4e+01 1.15e+00 -1.121543534e+01 1.141509949e+01 6.0e-03 0.04
7 2.4e+00 1.5e+01 7.6e+00 1.02e+00 5.607877454e+00 1.067191814e+01 1.5e-03 0.04
8 2.2e+00 1.4e+01 7.1e+00 7.87e-01 5.805650575e+00 1.065684919e+01 1.4e-03 0.04
9 1.1e+00 9.6e+00 3.5e+00 7.42e-01 7.632628186e+00 1.052163904e+01 7.5e-04 0.04
10 1.0e+00 9.2e+00 3.3e+00 4.62e-01 7.565713562e+00 1.051355978e+01 7.2e-04 0.04
11 3.9e-01 6.8e+00 1.3e+00 5.15e-01 8.911404622e+00 1.036015638e+01 3.0e-04 0.05
12 2.8e-01 4.9e+00 9.1e-01 5.59e-01 9.187063731e+00 1.032242546e+01 2.2e-04 0.05
13 4.6e-02 4.2e+00 1.6e-01 6.42e-01 9.960832194e+00 1.020958334e+01 5.2e-05 0.05
14 1.4e-02 3.9e+00 5.2e-02 9.15e-01 1.010228303e+01 1.018331103e+01 1.8e-05 0.05
15 5.5e-03 3.6e+00 2.0e-02 9.80e-01 1.014380454e+01 1.017567957e+01 7.0e-06 0.05
16 1.2e-03 3.4e+00 4.4e-03 9.91e-01 1.016437137e+01 1.017127226e+01 1.6e-06 0.05
17 2.7e-04 3.4e+00 1.0e-03 9.97e-01 1.016879823e+01 1.017037993e+01 3.6e-07 0.05
18 6.2e-05 3.2e+00 2.3e-04 9.99e-01 1.016982395e+01 1.017018979e+01 8.5e-08 0.05
19 1.5e-05 3.0e+00 5.7e-05 9.99e-01 1.017005491e+01 1.017014538e+01 2.1e-08 0.06
20 1.4e-05 2.7e+00 5.1e-05 9.99e-01 1.017006193e+01 1.017014358e+01 1.9e-08 0.06
21 1.2e-05 2.5e+00 4.6e-05 9.99e-01 1.017006880e+01 1.017014230e+01 1.7e-08 0.06
22 1.1e-05 2.2e+00 4.2e-05 9.99e-01 1.017007499e+01 1.017014115e+01 1.5e-08 0.06
23 1.0e-05 2.0e+00 3.8e-05 9.99e-01 1.017008057e+01 1.017014012e+01 1.4e-08 0.06
24 9.0e-06 1.8e+00 3.4e-05 1.00e+00 1.017008559e+01 1.017013918e+01 1.3e-08 0.06
25 8.1e-06 1.7e+00 3.0e-05 1.00e+00 1.017009011e+01 1.017013834e+01 1.1e-08 0.06
26 7.3e-06 1.5e+00 2.7e-05 1.00e+00 1.017009418e+01 1.017013759e+01 1.0e-08 0.07
27 6.5e-06 1.4e+00 2.5e-05 1.00e+00 1.017009784e+01 1.017013691e+01 9.1e-09 0.07
28 5.9e-06 1.3e+00 2.2e-05 1.00e+00 1.017010113e+01 1.017013630e+01 8.2e-09 0.07
29 5.3e-06 1.2e+00 2.0e-05 1.00e+00 1.017010410e+01 1.017013575e+01 7.4e-09 0.07
30 4.8e-06 1.1e+00 1.8e-05 1.00e+00 1.017010677e+01 1.017013525e+01 6.6e-09 0.07
31 4.3e-06 9.7e-01 1.6e-05 1.00e+00 1.017010917e+01 1.017013480e+01 6.0e-09 0.07
32 3.9e-06 8.9e-01 1.5e-05 1.00e+00 1.017011133e+01 1.017013440e+01 5.4e-09 0.07
33 3.5e-06 8.2e-01 1.3e-05 1.00e+00 1.017011328e+01 1.017013404e+01 4.8e-09 0.08
34 3.1e-06 7.6e-01 1.2e-05 1.00e+00 1.017011503e+01 1.017013371e+01 4.4e-09 0.08
35 2.8e-06 7.0e-01 1.1e-05 1.00e+00 1.017011660e+01 1.017013342e+01 3.9e-09 0.08
36 2.5e-06 6.5e-01 9.5e-06 1.00e+00 1.017011802e+01 1.017013316e+01 3.5e-09 0.08
37 2.3e-06 6.0e-01 8.6e-06 1.00e+00 1.017011930e+01 1.017013292e+01 3.2e-09 0.08
38 2.1e-06 5.6e-01 7.7e-06 1.00e+00 1.017012045e+01 1.017013271e+01 2.9e-09 0.08
39 1.8e-06 5.2e-01 7.0e-06 1.00e+00 1.017012148e+01 1.017013251e+01 2.6e-09 0.08
40 1.7e-06 4.9e-01 6.3e-06 9.99e-01 1.017012241e+01 1.017013234e+01 2.3e-09 0.08
41 1.5e-06 4.6e-01 5.6e-06 1.00e+00 1.017012325e+01 1.017013218e+01 2.1e-09 0.09
42 1.3e-06 4.3e-01 5.1e-06 1.00e+00 1.017012400e+01 1.017013204e+01 1.9e-09 0.09
43 1.2e-06 4.0e-01 4.6e-06 1.00e+00 1.017012468e+01 1.017013192e+01 1.7e-09 0.09
44 1.1e-06 3.8e-01 4.1e-06 9.99e-01 1.017012529e+01 1.017013180e+01 1.5e-09 0.09
45 9.8e-07 3.6e-01 3.7e-06 9.99e-01 1.017012584e+01 1.017013170e+01 1.4e-09 0.09
46 8.8e-07 3.4e-01 3.3e-06 1.00e+00 1.017012633e+01 1.017013161e+01 1.2e-09 0.09
47 8.0e-07 3.3e-01 3.0e-06 1.00e+00 1.017012678e+01 1.017013153e+01 1.1e-09 0.09
48 7.2e-07 3.1e-01 2.7e-06 9.99e-01 1.017012718e+01 1.017013145e+01 1.0e-09 0.10
49 6.4e-07 3.0e-01 2.4e-06 1.00e+00 1.017012754e+01 1.017013138e+01 9.0e-10 0.10
50 5.8e-07 2.9e-01 2.2e-06 9.97e-01 1.017012786e+01 1.017013132e+01 8.1e-10 0.10
51 5.2e-07 2.8e-01 2.0e-06 9.99e-01 1.017012815e+01 1.017013127e+01 7.3e-10 0.10
52 4.7e-07 2.7e-01 1.8e-06 9.97e-01 1.017012842e+01 1.017013122e+01 6.5e-10 0.10
53 4.2e-07 2.6e-01 1.6e-06 9.94e-01 1.017012865e+01 1.017013118e+01 5.9e-10 0.10
54 3.8e-07 2.5e-01 1.4e-06 9.97e-01 1.017012886e+01 1.017013114e+01 5.3e-10 0.10
55 3.4e-07 2.4e-01 1.3e-06 9.97e-01 1.017012906e+01 1.017013110e+01 4.8e-10 0.10
56 3.1e-07 2.4e-01 1.2e-06 1.00e+00 1.017012923e+01 1.017013107e+01 4.3e-10 0.11
57 2.8e-07 2.3e-01 1.0e-06 1.01e+00 1.017012939e+01 1.017013104e+01 3.9e-10 0.11
58 2.5e-07 2.3e-01 9.4e-07 9.95e-01 1.017012953e+01 1.017013101e+01 3.5e-10 0.11
59 2.2e-07 2.1e-01 8.5e-07 1.02e+00 1.017012966e+01 1.017013099e+01 3.2e-10 0.11
60 2.0e-07 2.0e-01 7.6e-07 9.91e-01 1.017012978e+01 1.017013097e+01 2.9e-10 0.11
61 1.8e-07 2.0e-01 6.9e-07 9.89e-01 1.017012988e+01 1.017013095e+01 2.6e-10 0.11
62 1.6e-07 2.0e-01 6.2e-07 1.00e+00 1.017012997e+01 1.017013093e+01 2.3e-10 0.11
63 1.5e-07 2.0e-01 5.6e-07 1.01e+00 1.017013005e+01 1.017013092e+01 2.1e-10 0.12
64 1.3e-07 2.0e-01 5.0e-07 9.83e-01 1.017013012e+01 1.017013090e+01 1.9e-10 0.12
65 1.2e-07 1.9e-01 4.5e-07 1.00e+00 1.017013019e+01 1.017013089e+01 1.7e-10 0.12
66 1.1e-07 1.9e-01 4.0e-07 9.96e-01 1.017013025e+01 1.017013088e+01 1.5e-10 0.12
67 9.7e-08 1.9e-01 3.6e-07 9.97e-01 1.017013030e+01 1.017013087e+01 1.4e-10 0.12
68 8.7e-08 1.9e-01 3.3e-07 9.77e-01 1.017013035e+01 1.017013086e+01 1.2e-10 0.12
69 7.8e-08 1.9e-01 2.9e-07 9.41e-01 1.017013039e+01 1.017013085e+01 1.1e-10 0.12
70 7.1e-08 1.7e-01 2.7e-07 9.90e-01 1.017013043e+01 1.017013085e+01 1.0e-10 0.13
71 6.3e-08 1.5e-01 2.4e-07 9.93e-01 1.017013046e+01 1.017013084e+01 9.0e-11 0.13
72 5.7e-08 1.4e-01 2.2e-07 9.94e-01 1.017013049e+01 1.017013083e+01 8.1e-11 0.13
73 5.1e-08 1.2e-01 1.9e-07 1.07e+00 1.017013053e+01 1.017013083e+01 7.5e-11 0.13
74 3.8e-09 7.2e-03 1.2e-08 9.42e-01 1.017013077e+01 1.017013078e+01 6.3e-12 0.13
75 3.4e-10 4.2e-04 6.8e-10 1.11e+00 1.017013078e+01 1.017013078e+01 5.2e-13 0.13
Interior-point optimizer terminated. Time: 0.14.
Optimizer terminated. Time: 0.15
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.0170130778e+01 Viol. con: 4e-10 var: 0e+00
Dual. obj: 1.0170130779e+01 Viol. con: 0e+00 var: 1e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.171 seconds.
result packing took 1.3e+02% of solve time
solution checking took 76% of solve time
Solving took 5 GP solves and 5.36 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 366641.653774 newton but the right hand side evaluated to 366630.041997 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 377162.167118 newton but the right hand side evaluated to 377115.416417 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 388105.06549 newton but the right hand side evaluated to 387998.835074 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 399470.22004 newton but the right hand side evaluated to 399279.068755 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 361212.168912 newton but the right hand side evaluated to 361206.344287 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 371522.114848 newton but the right hand side evaluated to 371498.518341 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 382190.280308 newton but the right hand side evaluated to 382135.941946 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 393255.617372 newton but the right hand side evaluated to 393156.452178 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 356181.861873 newton but the right hand side evaluated to 356176.074758 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 361243.178454 newton but the right hand side evaluated to 361220.024295 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 366354.199571 newton but the right hand side evaluated to 366302.307616 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 371535.42905 newton but the right hand side evaluated to 371443.443054 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 18366.9575652 newton but the right hand side evaluated to 18366.7147874 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 18344.4514692 newton but the right hand side evaluated to 18344.2021623 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 18344.4514119 newton but the right hand side evaluated to 18344.2020751 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 18344.4514361 newton but the right hand side evaluated to 18344.2020978 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 18924.2820483 newton but the right hand side evaluated to 18924.2615639 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 8445.89961495 newton but the right hand side evaluated to 8445.84799795 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 8626.29336176 newton but the right hand side evaluated to 8626.24785676 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 59111.
======================================================================
ERROR [25.776s]: test_turbofan_engine_flight_profile_fleet_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 41, in test_fn
mod.test()
File "engine_flight_profile_fleet.py", line 285, in test
File "/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/prog_factories.py", line 83, in solvefn
result = solvefn(solver, verbosity, *args, **kwargs)
File "/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/sgp.py", line 133, in localsolve
result = primal_feas.solve(solver, verbosity=verbosity-1)
File "/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/gpkit/gpkit/constraints/gp.py", line 203, in solve
(solvername, solver_status))
RuntimeWarning: final status of solver 'mosek' was 'UNKNOWN', not 'optimal'.
The solver's result is stored in model.program.solver_out. A result dict can be generated via program._compile_result(program.solver_out).
----------------------------------------------------------------------
Ran 4 tests in 49.646s
FAILED (errors=1)
Generating XML reports...
1.945235 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/ThrustPerformance_(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:///Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/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:///Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/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 /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas)
Requirement already satisfied: numpy>=1.7.0 in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/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 /private/var/folders/wp/20zl4b2n0qxcrp90f31275f80000gp/T/pip-iU2nkJ-build
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/gpkit (from gpfit==0.1)
Requirement already satisfied: pint in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1)
Running tests...
----------------------------------------------------------------------
..../Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/gassolar/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
tau = np.exp(-0.175/costhsun)
..
----------------------------------------------------------------------
Ran 6 tests in 25.754s
OK
Generating XML reports...
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 0.0853 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 0.0886 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 0.0833 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 0.258 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 0.0178 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 0.21497919994 but the right hand side evaluated to 0.214980884457 (Allowable error: 0.0001%, Actual error: 0.00078%)
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 0.20177138095 but the right hand side evaluated to 0.201764084159 (Allowable error: 0.0001%, Actual error: 0.0036%)
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 0.197670258036 but the right hand side evaluated to 0.197660144633 (Allowable error: 0.0001%, Actual error: 0.0051%)
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 0.20177138095 but the right hand side evaluated to 0.201764084159 (Allowable error: 0.0001%, Actual error: 0.0036%)
Warning: Constraint [z_{bre}_Mission/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 0.21497919994 but the right hand side evaluated to 0.214980884457 (Allowable error: 0.0001%, Actual error: 0.00078%)
Using solver 'mosek'
Solving for 1057 variables.
Solving took 0.241 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 2.75 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 0.509 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 3.46 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:///Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/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 /private/var/folders/wp/20zl4b2n0qxcrp90f31275f80000gp/T/pip-yHHCJ0-build
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/turbofan
Requirement already satisfied: numpy in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0)
Requirement already satisfied: pint in /Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0)
Running tests...
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..
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Ran 2 tests in 29.809s
OK
Generating XML reports...
adding test for 'SP_aircraft.py'
Beginning signomial solve.
Solving took 7 GP solves and 8.55 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 2427084.37531 force_pound * meter but the right hand side evaluated to 2397885.35436 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 2.21510116754 meter but the right hand side evaluated to 1.96470589177 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 17472.5831876 newton but the right hand side evaluated to 17443.2503159 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 1242117.41656 joule / kilogram but the right hand side evaluated to 1.48135610305 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 642471.518554 joule / kilogram but the right hand side evaluated to 0.643956034056 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 271789.693635 meter * newton but the right hand side evaluated to 263034.882371 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 18.5759810921 meter but the right hand side evaluated to 16.6120471716 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 10.9551769612 but the right hand side evaluated to 4.85819419264 (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 10.0069394344 but the right hand side evaluated to 4.85820441626 (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 8.21525128207 but the right hand side evaluated to 4.8582044658 (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 18.6220000517 meter but the right hand side evaluated to 18.375865536 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 18.6220000517 meter but the right hand side evaluated to 18.4513282081 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 4.67771839457 but the right hand side evaluated to 4.79404736871 (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 4.73114542605 but the right hand side evaluated to 4.81373469303 (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 7.60828555855 but the right hand side evaluated to 4.79404736871 (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 7.57971241087 but the right hand side evaluated to 4.81373469303 (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: [-6.97454039]
Total Aircraft Weight Percent Diff: [-4.95043277]
Engine Weight Percent Diff: -8.23499908463
Fuselage Weight Percent Diff: -10.9542163512
Payload Weight Percent Diff: [-0.04003559]
VT Weight Percent Diff: -24.5189849703
HT Weight Percent Diff: -85.1525283134
Wing Weight Percent Diff: 0.426082500529
WING DIFFERENCES
Wing Span Percent Diff: 0.92160727563
Wing Area Percent Diff: -6.86185514576
HORIZONTAL TAIL DIFFERENCES
HT Area Percent Diff: -54.6184953533
VERTICAL TAIL DIFFERENCES
VT Span Percent Diff: -16.3232047497
VT Area Percent Diff: -29.9969903068
CRUISE SEGMENT 1 DRAG DIFFERENCES
Overall Cd Percent Diff: [-0.13085241]
Nacelle Cd Percent Diff: [ 23.80938796]
HT Cd Percent Diff: [-63.50967008] dimensionless
Fuselage Cd Percent Diff: [ 45.32349081]
VT Cd Percent Diff: [ 60.36865963] dimensionless
Induced Drag Cd Percent Diff: [ 1.06378822]
Wing Profile Cd Percent Diff: [-15.69393436]
CRUISE SEGMENT 1 TSFC DIFFERENCES
Initial Cruise TSFC Percent Diff: [ 2.99108381]
FUSELAGE DIFFERENCES
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
0.790004745033
Beginning signomial solve.
Solving took 7 GP solves and 9.55 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 2427088.62423 force_pound * meter but the right hand side evaluated to 2397878.87058 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 2.21510301043 meter but the right hand side evaluated to 1.96470773718 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 17472.4999511 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 1242107.70897 joule / kilogram but the right hand side evaluated to 1.48150484743 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 642492.385771 joule / kilogram but the right hand side evaluated to 0.643976760313 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 271790.00319 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 16.6120610364 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 10.9552358245 but the right hand side evaluated to 4.85818543058 (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 10.0071246438 but the right hand side evaluated to 4.85819514696 (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 8.21526261644 but the right hand side evaluated to 4.85819514696 (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 18.6220164808 meter but the right hand side evaluated to 18.3758811924 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 18.6220164808 meter but the right hand side evaluated to 18.4513400632 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 4.67770662453 but the right hand side evaluated to 4.79403770011 (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 4.73113573489 but the right hand side evaluated to 4.81372397623 (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 7.60820193238 but the right hand side evaluated to 4.79403770011 (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 7.57970439014 but the right hand side evaluated to 4.81372397623 (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: -24.5185536457
HT Weight Percent Diff: -85.152583626
Wing Weight Percent Diff: 0.425462741526
WING DIFFERENCES
Wing Span Percent Diff: 0.921619801497
Wing Area Percent Diff: -6.86162729346
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: [-0.12888384]
Nacelle Cd Percent Diff: [ 23.80939215]
HT Cd Percent Diff: [-63.50956764] dimensionless
Fuselage Cd Percent Diff: [ 45.32347143]
VT Cd Percent Diff: [ 60.36836498] dimensionless
Induced Drag Cd Percent Diff: [ 1.06873722]
Wing Profile Cd Percent Diff: [-15.69240054]
CRUISE SEGMENT 1 TSFC DIFFERENCES
Initial Cruise TSFC Percent Diff: [ 2.99030664]
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', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/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', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gpkit-models']
attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
attempt 1
[Execution node] check if [macys] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
Build step 'Console output (build log) parsing' changed build result to FAILURE
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 5 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/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 FAILURE
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: FAILURE
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