Skipping 121 KB..
Full Log73 4.1e-07 7.8e-03 2.7e-05 1.00e+00 1.724035593e+02 1.724046230e+02 2.4e-10 1.69
74 3.7e-07 7.8e-03 2.5e-05 1.00e+00 1.724036357e+02 1.724045930e+02 2.2e-10 1.70
75 3.3e-07 7.7e-03 2.2e-05 1.00e+00 1.724037045e+02 1.724045661e+02 1.9e-10 1.71
76 3.0e-07 7.7e-03 2.0e-05 1.00e+00 1.724037664e+02 1.724045418e+02 1.8e-10 1.73
77 2.7e-07 7.7e-03 1.8e-05 1.00e+00 1.724038221e+02 1.724045200e+02 1.6e-10 1.74
78 2.4e-07 7.6e-03 1.6e-05 1.00e+00 1.724038722e+02 1.724045003e+02 1.4e-10 1.75
79 2.2e-07 7.6e-03 1.5e-05 9.99e-01 1.724039173e+02 1.724044826e+02 1.3e-10 1.77
80 2.0e-07 7.6e-03 1.3e-05 9.99e-01 1.724039579e+02 1.724044667e+02 1.2e-10 1.78
81 1.8e-07 7.5e-03 1.2e-05 9.99e-01 1.724039944e+02 1.724044523e+02 1.0e-10 1.79
82 1.6e-07 7.5e-03 1.1e-05 1.00e+00 1.724040273e+02 1.724044394e+02 9.3e-11 1.80
83 1.4e-07 7.5e-03 9.6e-06 9.99e-01 1.724040568e+02 1.724044277e+02 8.4e-11 1.82
84 1.3e-07 7.5e-03 8.6e-06 1.00e+00 1.724040834e+02 1.724044173e+02 7.5e-11 1.83
85 1.2e-07 7.4e-03 7.8e-06 9.99e-01 1.724041074e+02 1.724044079e+02 6.8e-11 1.84
86 1.0e-07 7.4e-03 7.0e-06 1.00e+00 1.724041289e+02 1.724043993e+02 6.1e-11 1.86
87 9.4e-08 7.4e-03 6.3e-06 9.99e-01 1.724041483e+02 1.724043917e+02 5.5e-11 1.87
88 8.4e-08 7.4e-03 5.7e-06 9.96e-01 1.724041658e+02 1.724043849e+02 5.0e-11 1.88
89 7.6e-08 7.4e-03 5.1e-06 9.98e-01 1.724041815e+02 1.724043787e+02 4.5e-11 1.89
90 6.8e-08 7.3e-03 4.6e-06 9.97e-01 1.724041956e+02 1.724043731e+02 4.0e-11 1.90
91 6.1e-08 7.3e-03 4.1e-06 9.98e-01 1.724042083e+02 1.724043681e+02 3.6e-11 1.91
92 5.5e-08 7.3e-03 3.7e-06 1.00e+00 1.724042198e+02 1.724043636e+02 3.2e-11 1.92
93 5.0e-08 7.3e-03 3.3e-06 1.00e+00 1.724042301e+02 1.724043595e+02 2.9e-11 1.93
94 4.5e-08 7.3e-03 3.0e-06 1.00e+00 1.724042394e+02 1.724043558e+02 2.6e-11 1.97
95 4.0e-08 7.3e-03 2.7e-06 1.00e+00 1.724042477e+02 1.724043525e+02 2.4e-11 1.98
96 3.6e-08 7.3e-03 2.4e-06 9.93e-01 1.724042552e+02 1.724043496e+02 2.1e-11 2.02
97 3.3e-08 6.5e-03 2.2e-06 1.00e+00 1.724042620e+02 1.724043469e+02 1.9e-11 2.03
98 2.9e-08 5.9e-03 2.0e-06 1.00e+00 1.724042681e+02 1.724043445e+02 1.7e-11 2.05
99 2.6e-08 5.3e-03 1.8e-06 9.91e-01 1.724042735e+02 1.724043423e+02 1.6e-11 2.06
100 2.4e-08 4.8e-03 1.6e-06 1.01e+00 1.724042788e+02 1.724043402e+02 1.4e-11 2.08
101 2.1e-08 4.3e-03 1.4e-06 9.99e-01 1.724042832e+02 1.724043385e+02 1.3e-11 2.10
102 1.9e-08 3.9e-03 1.3e-06 1.01e+00 1.724042873e+02 1.724043368e+02 1.1e-11 2.11
103 1.7e-08 3.5e-03 1.2e-06 1.01e+00 1.724042910e+02 1.724043353e+02 1.0e-11 2.12
104 1.6e-08 3.1e-03 1.0e-06 1.00e+00 1.724042942e+02 1.724043341e+02 9.3e-12 2.13
105 4.4e-09 7.7e-04 2.6e-07 9.98e-01 1.724043157e+02 1.724043256e+02 2.3e-12 2.15
106 3.9e-09 7.0e-04 2.3e-07 1.03e+00 1.724043165e+02 1.724043253e+02 2.1e-12 2.16
107 1.3e-09 1.7e-04 5.8e-08 1.07e+00 1.724043212e+02 1.724043232e+02 4.9e-13 2.17
Interior-point optimizer terminated. Time: 2.17.
Optimizer terminated. Time: 2.18
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.7240432117e+02 Viol. con: 2e-08 var: 0e+00
Dual. obj: 1.7240432323e+02 Viol. con: 0e+00 var: 1e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.2 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.289209279e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.267404395e+05 3.637047323e+00 4.8e-01 0.05
2 4.4e+02 5.7e+02 2.4e+04 -9.36e-01 -1.207993260e+05 1.004622010e+01 1.9e-01 0.06
3 2.9e+02 3.8e+02 1.6e+04 -8.43e-01 -1.160618628e+05 5.990662233e+01 1.3e-01 0.07
4 2.9e+02 3.8e+02 1.6e+04 -7.62e-01 -1.136045221e+05 2.136092785e+03 1.3e-01 0.10
5 8.1e+01 1.0e+02 4.5e+03 -7.56e-01 -7.752618955e+04 9.316590632e+03 3.5e-02 0.11
6 4.0e+01 5.2e+01 2.2e+03 -2.34e-01 -5.076741252e+04 1.003179833e+04 1.8e-02 0.12
7 3.0e+01 3.9e+01 1.7e+03 2.19e-01 -4.171035381e+04 8.294890628e+03 1.3e-02 0.15
8 1.9e+01 2.4e+01 1.0e+03 3.81e-01 -2.865141899e+04 5.387064689e+03 8.1e-03 0.17
9 7.9e+00 1.0e+01 4.4e+02 6.03e-01 -1.310597210e+04 3.143049736e+03 3.5e-03 0.18
10 4.0e+00 5.2e+00 2.2e+02 8.46e-01 -6.378101576e+03 2.128677120e+03 1.8e-03 0.21
11 2.2e+00 2.9e+00 1.3e+02 9.42e-01 -3.514555688e+03 1.314876543e+03 9.9e-04 0.27
12 9.1e-01 1.2e+00 5.1e+01 9.75e-01 -1.333953141e+03 6.456467148e+02 4.0e-04 0.28
13 8.2e-01 1.1e+00 4.6e+01 9.70e-01 -1.223648492e+03 5.999353713e+02 3.7e-04 0.29
14 5.9e-01 7.8e-01 3.3e+01 9.74e-01 -8.149794417e+02 4.893554429e+02 2.6e-04 0.30
15 2.2e-01 7.6e-01 1.2e+01 9.90e-01 -1.999795996e+02 2.844530000e+02 9.8e-05 0.32
16 1.1e-01 3.8e-01 6.1e+00 1.00e+00 -2.241201048e+01 2.161154382e+02 4.9e-05 0.33
17 7.7e-02 2.8e-01 4.5e+00 1.01e+00 2.681073930e+01 2.015603399e+02 3.6e-05 0.34
18 5.1e-02 2.0e-01 3.0e+00 1.02e+00 7.892007143e+01 1.950358756e+02 2.4e-05 0.35
19 1.4e-02 1.1e-01 8.5e-01 1.00e+00 1.414700276e+02 1.745815002e+02 6.9e-06 0.35
20 4.0e-03 2.2e-01 2.4e-01 1.02e+00 1.602704576e+02 1.696481183e+02 1.9e-06 0.36
21 2.7e-03 2.1e-01 1.6e-01 1.01e+00 1.624284108e+02 1.687369719e+02 1.3e-06 0.37
22 1.9e-03 1.5e-01 1.2e-01 1.00e+00 1.637170023e+02 1.683012331e+02 9.5e-07 0.38
23 7.5e-04 9.5e-02 4.7e-02 1.01e+00 1.658030249e+02 1.676006389e+02 3.8e-07 0.39
24 3.6e-04 7.9e-02 2.3e-02 1.01e+00 1.664694569e+02 1.673480746e+02 1.9e-07 0.40
25 3.3e-04 7.2e-02 2.1e-02 1.01e+00 1.665375736e+02 1.673287231e+02 1.7e-07 0.41
26 3.0e-04 6.6e-02 1.9e-02 1.01e+00 1.665946655e+02 1.673064407e+02 1.5e-07 0.42
27 2.7e-04 6.0e-02 1.7e-02 1.01e+00 1.666462522e+02 1.672866431e+02 1.4e-07 0.43
28 2.4e-04 5.5e-02 1.5e-02 1.01e+00 1.666924449e+02 1.672686263e+02 1.2e-07 0.45
29 2.2e-04 5.0e-02 1.4e-02 1.01e+00 1.667338925e+02 1.672523163e+02 1.1e-07 0.46
30 1.9e-04 4.6e-02 1.2e-02 1.01e+00 1.667710545e+02 1.672375218e+02 9.9e-08 0.47
31 1.7e-04 4.2e-02 1.1e-02 1.01e+00 1.668043755e+02 1.672241027e+02 8.9e-08 0.48
32 1.6e-04 3.8e-02 9.9e-03 1.01e+00 1.668342505e+02 1.672119290e+02 8.0e-08 0.50
33 1.4e-04 3.5e-02 8.9e-03 1.01e+00 1.668610362e+02 1.672008851e+02 7.2e-08 0.51
34 1.3e-04 3.3e-02 8.0e-03 1.01e+00 1.668850531e+02 1.671908670e+02 6.5e-08 0.52
35 1.1e-04 3.0e-02 7.2e-03 1.01e+00 1.669065896e+02 1.671817816e+02 5.8e-08 0.53
36 1.0e-04 2.8e-02 6.5e-03 1.00e+00 1.669259047e+02 1.671735449e+02 5.3e-08 0.54
37 9.3e-05 2.6e-02 5.8e-03 1.00e+00 1.669432306e+02 1.671660806e+02 4.7e-08 0.55
38 8.3e-05 2.4e-02 5.3e-03 1.00e+00 1.669587748e+02 1.671593190e+02 4.3e-08 0.56
39 7.5e-05 2.2e-02 4.7e-03 1.00e+00 1.669727231e+02 1.671531963e+02 3.8e-08 0.63
40 6.8e-05 2.1e-02 4.3e-03 1.00e+00 1.669852412e+02 1.671476540e+02 3.5e-08 0.69
41 6.1e-05 2.0e-02 3.8e-03 1.00e+00 1.669964774e+02 1.671426385e+02 3.1e-08 0.75
42 5.5e-05 1.8e-02 3.4e-03 1.00e+00 1.670065645e+02 1.671381014e+02 2.8e-08 0.80
43 4.9e-05 1.7e-02 3.1e-03 1.00e+00 1.670156210e+02 1.671339979e+02 2.5e-08 0.85
44 4.4e-05 1.6e-02 2.8e-03 1.00e+00 1.670237533e+02 1.671302877e+02 2.3e-08 0.88
45 4.0e-05 1.6e-02 2.5e-03 1.00e+00 1.670310565e+02 1.671269338e+02 2.0e-08 1.01
46 3.6e-05 1.5e-02 2.3e-03 1.00e+00 1.670376160e+02 1.671239028e+02 1.8e-08 1.24
47 3.2e-05 1.4e-02 2.0e-03 1.00e+00 1.670435081e+02 1.671211642e+02 1.7e-08 1.69
48 2.9e-05 1.4e-02 1.8e-03 1.00e+00 1.670488012e+02 1.671186902e+02 1.5e-08 2.05
49 2.6e-05 1.3e-02 1.7e-03 1.00e+00 1.670535568e+02 1.671164557e+02 1.3e-08 2.19
50 2.4e-05 1.3e-02 1.5e-03 1.00e+00 1.670578298e+02 1.671144381e+02 1.2e-08 2.36
51 2.1e-05 1.2e-02 1.3e-03 1.00e+00 1.670616696e+02 1.671126165e+02 1.1e-08 2.43
52 1.9e-05 1.2e-02 1.2e-03 1.00e+00 1.670651203e+02 1.671109722e+02 9.8e-09 2.73
53 1.7e-05 1.1e-02 1.1e-03 1.00e+00 1.670682217e+02 1.671094882e+02 8.8e-09 3.00
54 1.5e-05 1.1e-02 9.7e-04 1.00e+00 1.670710093e+02 1.671081491e+02 7.9e-09 3.42
55 1.4e-05 1.1e-02 8.8e-04 1.00e+00 1.670735151e+02 1.671069409e+02 7.1e-09 3.78
56 1.3e-05 1.0e-02 7.9e-04 1.00e+00 1.670757678e+02 1.671058510e+02 6.4e-09 3.93
57 1.1e-05 1.0e-02 7.1e-04 1.00e+00 1.670777930e+02 1.671048679e+02 5.8e-09 4.34
58 1.0e-05 1.0e-02 6.4e-04 1.00e+00 1.670796139e+02 1.671039814e+02 5.2e-09 4.72
59 9.1e-06 9.8e-03 5.8e-04 1.00e+00 1.670812512e+02 1.671031821e+02 4.7e-09 5.11
60 8.2e-06 9.6e-03 5.2e-04 1.00e+00 1.670827235e+02 1.671024614e+02 4.2e-09 5.64
61 7.4e-06 9.5e-03 4.7e-04 1.00e+00 1.670840476e+02 1.671018117e+02 3.8e-09 6.35
62 6.6e-06 9.3e-03 4.2e-04 1.00e+00 1.670852383e+02 1.671012261e+02 3.4e-09 6.67
63 6.0e-06 9.2e-03 3.8e-04 1.00e+00 1.670863093e+02 1.671006984e+02 3.1e-09 6.90
64 5.4e-06 9.1e-03 3.4e-04 1.00e+00 1.670872725e+02 1.671002229e+02 2.8e-09 7.16
65 2.0e-06 3.4e-03 1.3e-04 1.00e+00 1.670926183e+02 1.670975534e+02 1.1e-09 7.43
66 6.9e-07 1.2e-03 4.4e-05 1.00e+00 1.670947944e+02 1.670964651e+02 3.6e-10 7.69
67 6.2e-07 1.0e-03 3.9e-05 1.00e+00 1.670949088e+02 1.670964123e+02 3.2e-10 8.04
68 5.6e-07 9.4e-04 3.6e-05 1.00e+00 1.670950084e+02 1.670963615e+02 2.9e-10 8.33
69 5.0e-07 8.5e-04 3.2e-05 9.99e-01 1.670950982e+02 1.670963160e+02 2.6e-10 8.52
70 4.5e-07 7.6e-04 2.9e-05 1.00e+00 1.670951789e+02 1.670962750e+02 2.3e-10 8.98
71 4.1e-07 6.9e-04 2.6e-05 1.00e+00 1.670952516e+02 1.670962379e+02 2.1e-10 9.29
72 3.7e-07 6.2e-04 2.3e-05 1.00e+00 1.670953169e+02 1.670962046e+02 1.9e-10 9.54
73 3.3e-07 5.6e-04 2.1e-05 1.00e+00 1.670953757e+02 1.670961746e+02 1.7e-10 9.81
74 3.0e-07 5.0e-04 1.9e-05 1.00e+00 1.670954286e+02 1.670961476e+02 1.5e-10 10.28
75 2.7e-07 4.5e-04 1.7e-05 1.00e+00 1.670954762e+02 1.670961233e+02 1.4e-10 10.83
76 2.4e-07 4.1e-04 1.5e-05 1.00e+00 1.670955190e+02 1.670961013e+02 1.2e-10 11.39
77 2.2e-07 3.7e-04 1.4e-05 1.00e+00 1.670955575e+02 1.670960815e+02 1.1e-10 11.84
78 2.0e-07 3.3e-04 1.2e-05 1.00e+00 1.670955921e+02 1.670960638e+02 1.0e-10 12.12
79 1.8e-07 3.0e-04 1.1e-05 9.98e-01 1.670956233e+02 1.670960478e+02 9.1e-11 12.40
80 1.6e-07 2.7e-04 1.0e-05 1.00e+00 1.670956515e+02 1.670960333e+02 8.2e-11 12.67
81 1.4e-07 2.4e-04 9.0e-06 1.00e+00 1.670956767e+02 1.670960203e+02 7.3e-11 12.96
82 1.3e-07 2.2e-04 8.1e-06 1.00e+00 1.670956994e+02 1.670960087e+02 6.6e-11 13.03
83 1.2e-07 1.9e-04 7.3e-06 9.96e-01 1.670957199e+02 1.670959982e+02 5.9e-11 13.39
84 1.0e-07 1.7e-04 6.6e-06 1.00e+00 1.670957382e+02 1.670959887e+02 5.4e-11 13.62
85 9.3e-08 1.6e-04 5.9e-06 1.00e+00 1.670957548e+02 1.670959802e+02 4.8e-11 13.79
86 8.4e-08 1.4e-04 5.3e-06 1.01e+00 1.670957699e+02 1.670959724e+02 4.3e-11 13.94
87 7.6e-08 1.3e-04 4.8e-06 9.97e-01 1.670957833e+02 1.670959656e+02 3.9e-11 14.07
88 6.8e-08 1.1e-04 4.3e-06 1.00e+00 1.670957953e+02 1.670959594e+02 3.5e-11 14.22
89 6.1e-08 1.0e-04 3.9e-06 9.94e-01 1.670958061e+02 1.670959538e+02 3.2e-11 14.32
90 5.5e-08 9.3e-05 3.5e-06 9.94e-01 1.670958159e+02 1.670959489e+02 2.8e-11 14.45
91 5.0e-08 8.4e-05 3.2e-06 1.00e+00 1.670958247e+02 1.670959443e+02 2.6e-11 14.58
92 4.5e-08 7.5e-05 2.8e-06 1.00e+00 1.670958326e+02 1.670959402e+02 2.3e-11 14.68
93 4.0e-08 6.8e-05 2.6e-06 1.01e+00 1.670958399e+02 1.670959364e+02 2.1e-11 14.81
94 3.6e-08 6.1e-05 2.3e-06 9.83e-01 1.670958463e+02 1.670959332e+02 1.9e-11 14.99
95 3.3e-08 5.5e-05 2.1e-06 1.01e+00 1.670958522e+02 1.670959301e+02 1.7e-11 15.09
96 2.9e-08 4.9e-05 1.9e-06 1.02e+00 1.670958578e+02 1.670959272e+02 1.5e-11 15.15
97 2.6e-08 4.4e-05 1.7e-06 9.96e-01 1.670958623e+02 1.670959249e+02 1.4e-11 15.27
98 2.4e-08 4.0e-05 1.5e-06 9.76e-01 1.670958664e+02 1.670959228e+02 1.2e-11 15.40
99 2.1e-08 3.6e-05 1.4e-06 1.01e+00 1.670958703e+02 1.670959208e+02 1.1e-11 15.49
100 1.9e-08 3.2e-05 1.2e-06 9.94e-01 1.670958736e+02 1.670959191e+02 1.0e-11 15.80
101 1.7e-08 2.9e-05 1.1e-06 1.02e+00 1.670958768e+02 1.670959174e+02 9.2e-12 16.02
Interior-point optimizer terminated. Time: 16.03.
Optimizer terminated. Time: 16.04
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6709587681e+02 Viol. con: 3e-07 var: 0e+00
Dual. obj: 1.6709591743e+02 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 16.1 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.03 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.286499298e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.264834069e+05 3.586695488e+00 4.8e-01 0.18
2 4.3e+02 5.6e+02 2.4e+04 -9.36e-01 -1.204818408e+05 1.001252852e+01 1.9e-01 0.44
3 2.9e+02 3.7e+02 1.6e+04 -8.42e-01 -1.157492292e+05 6.085649918e+01 1.3e-01 0.87
4 2.9e+02 3.7e+02 1.6e+04 -7.62e-01 -1.131499805e+05 2.257752192e+03 1.3e-01 1.49
5 7.4e+01 9.6e+01 4.1e+03 -7.55e-01 -7.449025152e+04 9.842634114e+03 3.3e-02 1.64
6 3.6e+01 4.7e+01 2.0e+03 -1.90e-01 -4.726343942e+04 1.026281828e+04 1.6e-02 1.87
7 2.2e+01 2.9e+01 1.3e+03 2.77e-01 -3.297733606e+04 7.148459883e+03 9.9e-03 2.21
8 1.4e+01 1.7e+01 7.5e+02 5.32e-01 -2.145913430e+04 4.808156211e+03 6.0e-03 2.59
9 5.3e+00 6.9e+00 3.0e+02 7.21e-01 -8.768077140e+03 2.417294393e+03 2.4e-03 2.86
10 2.4e+00 3.1e+00 1.3e+02 9.13e-01 -3.743298654e+03 1.405439341e+03 1.1e-03 3.11
11 1.7e+00 2.3e+00 9.8e+01 9.75e-01 -2.706783635e+03 1.075294761e+03 7.8e-04 3.43
12 8.2e-01 1.1e+00 4.6e+01 9.83e-01 -1.189758577e+03 5.993132962e+02 3.7e-04 3.77
13 7.5e-01 1.1e+00 4.2e+01 9.48e-01 -1.109365023e+03 5.596606911e+02 3.4e-04 4.09
14 6.3e-01 8.8e-01 3.5e+01 9.86e-01 -8.799127583e+02 5.072307533e+02 2.8e-04 4.58
15 1.8e-01 2.8e-01 1.0e+01 9.89e-01 -1.584747447e+02 2.542000438e+02 8.4e-05 5.04
16 1.0e-01 1.7e-01 5.9e+00 1.01e+00 -1.976707451e+01 2.098853099e+02 4.7e-05 5.33
17 1.0e-01 1.7e-01 5.8e+00 1.02e+00 -1.809004746e+01 2.102290929e+02 4.7e-05 5.60
18 8.6e-02 1.5e-01 5.0e+00 1.02e+00 1.591141088e+01 2.106371433e+02 4.0e-05 5.85
19 4.3e-02 9.6e-02 2.5e+00 1.01e+00 9.060665396e+01 1.877232512e+02 2.0e-05 6.02
20 1.2e-02 1.9e-01 6.8e-01 1.01e+00 1.471514505e+02 1.733932142e+02 5.5e-06 6.23
21 4.3e-03 3.5e-01 2.6e-01 1.01e+00 1.590258134e+02 1.689635190e+02 2.1e-06 6.26
22 1.2e-03 1.7e-01 7.5e-02 1.01e+00 1.645644512e+02 1.674295875e+02 6.1e-07 6.29
23 6.7e-04 1.2e-01 4.2e-02 9.81e-01 1.654779071e+02 1.670872399e+02 3.5e-07 6.80
24 2.0e-04 1.1e-01 1.3e-02 9.95e-01 1.662934708e+02 1.667797855e+02 1.1e-07 7.11
25 6.2e-05 1.1e-01 4.1e-03 1.01e+00 1.665280619e+02 1.666838915e+02 3.5e-08 7.38
26 2.0e-05 1.1e-01 1.4e-03 1.01e+00 1.666013411e+02 1.666531233e+02 1.2e-08 7.75
27 6.5e-06 1.1e-01 4.4e-04 1.00e+00 1.666261907e+02 1.666427298e+02 3.8e-09 7.98
28 2.2e-06 1.0e-01 1.5e-04 1.00e+00 1.666337612e+02 1.666395177e+02 1.3e-09 8.25
29 7.7e-07 9.7e-02 5.3e-05 1.00e+00 1.666363786e+02 1.666383683e+02 4.5e-10 8.41
30 3.4e-07 8.2e-02 2.3e-05 1.00e+00 1.666371513e+02 1.666380164e+02 2.0e-10 8.57
31 7.3e-08 1.8e-02 5.0e-06 1.00e+00 1.666376162e+02 1.666378047e+02 4.3e-11 8.59
32 6.6e-08 1.6e-02 4.5e-06 1.00e+00 1.666376302e+02 1.666377998e+02 3.9e-11 8.60
33 5.9e-08 1.6e-02 4.1e-06 1.01e+00 1.666376419e+02 1.666377943e+02 3.5e-11 8.66
34 5.3e-08 1.5e-02 3.7e-06 9.99e-01 1.666376523e+02 1.666377895e+02 3.1e-11 8.89
35 4.8e-08 1.4e-02 3.3e-06 1.01e+00 1.666376618e+02 1.666377850e+02 2.8e-11 9.13
36 4.3e-08 1.3e-02 3.0e-06 9.96e-01 1.666376702e+02 1.666377811e+02 2.6e-11 9.29
37 3.9e-08 1.3e-02 2.7e-06 9.99e-01 1.666376778e+02 1.666377776e+02 2.3e-11 9.43
38 3.5e-08 1.2e-02 2.4e-06 1.01e+00 1.666376847e+02 1.666377743e+02 2.1e-11 9.61
39 3.1e-08 1.2e-02 2.2e-06 1.00e+00 1.666376909e+02 1.666377715e+02 1.9e-11 9.75
40 2.8e-08 1.1e-02 1.9e-06 9.86e-01 1.666376963e+02 1.666377689e+02 1.7e-11 9.92
41 2.5e-08 1.1e-02 1.8e-06 1.01e+00 1.666377015e+02 1.666377665e+02 1.5e-11 9.99
42 2.3e-08 1.1e-02 1.6e-06 9.82e-01 1.666377059e+02 1.666377645e+02 1.4e-11 10.01
43 2.1e-08 1.0e-02 1.4e-06 1.01e+00 1.666377101e+02 1.666377625e+02 1.2e-11 10.06
44 1.9e-08 1.0e-02 1.3e-06 1.03e+00 1.666377141e+02 1.666377606e+02 1.1e-11 10.07
45 1.7e-08 1.0e-02 1.1e-06 9.68e-01 1.666377172e+02 1.666377592e+02 1.0e-11 10.08
46 1.5e-08 9.8e-03 1.0e-06 9.86e-01 1.666377201e+02 1.666377579e+02 9.1e-12 10.10
47 1.4e-08 9.6e-03 9.3e-07 9.92e-01 1.666377227e+02 1.666377567e+02 8.2e-12 10.11
48 1.2e-08 9.5e-03 8.4e-07 1.01e+00 1.666377251e+02 1.666377555e+02 7.4e-12 10.12
49 1.1e-08 9.2e-03 7.5e-07 9.72e-01 1.666377271e+02 1.666377546e+02 6.7e-12 10.13
50 9.9e-09 8.3e-03 6.8e-07 1.04e+00 1.666377294e+02 1.666377535e+02 6.1e-12 10.15
51 8.9e-09 8.1e-03 6.1e-07 9.70e-01 1.666377310e+02 1.666377528e+02 5.5e-12 10.18
52 8.0e-09 8.1e-03 5.5e-07 9.73e-01 1.666377325e+02 1.666377521e+02 5.0e-12 10.20
53 7.2e-09 7.8e-03 4.9e-07 9.01e-01 1.666377338e+02 1.666377515e+02 4.5e-12 10.21
54 4.7e-09 4.7e-04 3.0e-08 8.68e-01 1.666377455e+02 1.666377467e+02 5.1e-13 10.23
Interior-point optimizer terminated. Time: 10.23.
Optimizer terminated. Time: 10.24
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6663774551e+02 Viol. con: 2e-07 var: 0e+00
Dual. obj: 1.6663774666e+02 Viol. con: 0e+00 var: 4e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 10.3 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.03 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.286106771e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.264423007e+05 3.580365222e+00 4.8e-01 0.06
2 4.3e+02 5.5e+02 2.4e+04 -9.36e-01 -1.203332335e+05 1.010636288e+01 1.9e-01 0.08
3 2.9e+02 3.7e+02 1.6e+04 -8.40e-01 -1.156664730e+05 6.247792604e+01 1.3e-01 0.10
4 2.9e+02 3.7e+02 1.6e+04 -7.61e-01 -1.130152826e+05 2.295884618e+03 1.3e-01 0.11
5 7.3e+01 9.4e+01 4.1e+03 -7.54e-01 -7.379597028e+04 9.860992526e+03 3.2e-02 0.14
6 3.6e+01 4.6e+01 2.0e+03 -1.80e-01 -4.641910319e+04 1.009611434e+04 1.6e-02 0.15
7 2.1e+01 2.7e+01 1.2e+03 2.91e-01 -3.097469823e+04 6.886219939e+03 9.2e-03 0.18
8 1.2e+01 1.6e+01 6.8e+02 5.65e-01 -1.945488591e+04 4.491373678e+03 5.4e-03 0.19
9 4.7e+00 6.1e+00 2.6e+02 7.53e-01 -7.765154187e+03 2.180676492e+03 2.1e-03 0.20
10 2.3e+00 3.0e+00 1.3e+02 9.26e-01 -3.530372780e+03 1.395530077e+03 1.0e-03 0.22
11 1.5e+00 1.9e+00 8.5e+01 9.77e-01 -2.301318826e+03 9.721205230e+02 6.7e-04 0.25
12 8.5e-01 1.1e+00 4.8e+01 9.85e-01 -1.230530091e+03 6.224921019e+02 3.8e-04 0.26
13 7.5e-01 1.0e+00 4.2e+01 9.54e-01 -1.093831153e+03 5.630529286e+02 3.4e-04 0.28
14 3.7e-01 5.0e-01 2.1e+01 9.85e-01 -4.359009575e+02 3.737949774e+02 1.6e-04 0.29
15 1.8e-01 2.5e-01 1.0e+01 9.98e-01 -1.439999276e+02 2.585348621e+02 8.2e-05 0.31
16 8.9e-02 1.6e-01 5.1e+00 1.01e+00 4.980078878e+00 2.043015061e+02 4.1e-05 0.32
17 8.6e-02 1.5e-01 4.9e+00 1.01e+00 1.398829009e+01 2.065699109e+02 4.0e-05 0.33
18 6.1e-02 1.1e-01 3.5e+00 1.01e+00 5.949224722e+01 1.948373534e+02 2.8e-05 0.35
19 3.0e-02 7.3e-02 1.7e+00 1.01e+00 1.152797946e+02 1.809927777e+02 1.4e-05 0.37
20 8.5e-03 1.8e-01 4.9e-01 1.01e+00 1.525612320e+02 1.716192008e+02 4.0e-06 0.38
21 2.5e-03 1.8e-01 1.5e-01 1.00e+00 1.622330892e+02 1.679611454e+02 1.2e-06 0.40
22 1.5e-03 1.2e-01 9.0e-02 1.00e+00 1.639702593e+02 1.674409743e+02 7.3e-07 0.51
23 5.1e-04 1.0e-01 3.2e-02 1.01e+00 1.656550168e+02 1.668671106e+02 2.6e-07 0.52
24 2.0e-04 9.6e-02 1.2e-02 1.01e+00 1.661959789e+02 1.666660332e+02 1.0e-07 0.54
25 1.8e-04 8.7e-02 1.1e-02 1.01e+00 1.662326077e+02 1.666555351e+02 9.2e-08 0.55
26 1.6e-04 7.9e-02 1.0e-02 1.01e+00 1.662628626e+02 1.666433552e+02 8.3e-08 0.57
27 1.4e-04 7.2e-02 9.0e-03 1.01e+00 1.662902734e+02 1.666326040e+02 7.5e-08 0.58
28 1.3e-04 6.6e-02 8.1e-03 1.01e+00 1.663148172e+02 1.666228211e+02 6.7e-08 0.61
29 1.2e-04 6.0e-02 7.3e-03 1.01e+00 1.663368438e+02 1.666139702e+02 6.0e-08 0.63
30 1.0e-04 5.5e-02 6.5e-03 1.01e+00 1.663566055e+02 1.666059557e+02 5.4e-08 0.64
31 9.4e-05 5.0e-02 5.9e-03 1.01e+00 1.663743370e+02 1.665987003e+02 4.9e-08 0.65
32 8.5e-05 4.6e-02 5.3e-03 1.01e+00 1.663902477e+02 1.665921324e+02 4.4e-08 0.66
33 7.6e-05 4.2e-02 4.8e-03 1.01e+00 1.664045257e+02 1.665861875e+02 4.0e-08 0.68
34 6.9e-05 3.8e-02 4.3e-03 1.01e+00 1.664173397e+02 1.665808074e+02 3.6e-08 0.69
35 6.2e-05 3.5e-02 3.9e-03 1.01e+00 1.664288411e+02 1.665759394e+02 3.2e-08 0.72
36 5.5e-05 3.3e-02 3.5e-03 1.00e+00 1.664391654e+02 1.665715357e+02 2.9e-08 0.73
37 5.0e-05 3.0e-02 3.1e-03 1.00e+00 1.664484343e+02 1.665675529e+02 2.6e-08 0.75
38 4.5e-05 2.8e-02 2.8e-03 1.00e+00 1.664567564e+02 1.665639514e+02 2.3e-08 0.76
39 4.0e-05 2.6e-02 2.5e-03 1.00e+00 1.664642293e+02 1.665606955e+02 2.1e-08 0.77
40 3.6e-05 2.4e-02 2.3e-03 1.00e+00 1.664709403e+02 1.665577525e+02 1.9e-08 0.78
41 3.3e-05 2.2e-02 2.1e-03 1.00e+00 1.664769679e+02 1.665550929e+02 1.7e-08 0.82
42 2.9e-05 2.1e-02 1.9e-03 1.00e+00 1.664823821e+02 1.665526899e+02 1.5e-08 0.84
43 2.7e-05 2.0e-02 1.7e-03 1.00e+00 1.664872457e+02 1.665505192e+02 1.4e-08 0.85
44 2.4e-05 1.8e-02 1.5e-03 1.00e+00 1.664916154e+02 1.665485586e+02 1.2e-08 0.87
45 2.1e-05 1.7e-02 1.3e-03 1.00e+00 1.664955415e+02 1.665467882e+02 1.1e-08 0.88
46 1.9e-05 1.6e-02 1.2e-03 1.00e+00 1.664990696e+02 1.665451899e+02 1.0e-08 0.89
47 1.7e-05 1.6e-02 1.1e-03 1.00e+00 1.665022403e+02 1.665437472e+02 9.1e-09 0.91
48 1.6e-05 1.5e-02 9.8e-04 1.00e+00 1.665050900e+02 1.665424452e+02 8.2e-09 0.92
49 1.4e-05 1.4e-02 8.9e-04 1.00e+00 1.665076517e+02 1.665412706e+02 7.4e-09 0.96
50 1.3e-05 1.3e-02 8.0e-04 1.00e+00 1.665099546e+02 1.665402111e+02 6.6e-09 1.00
51 1.1e-05 1.3e-02 7.2e-04 1.00e+00 1.665120251e+02 1.665392556e+02 6.0e-09 1.05
52 1.0e-05 1.2e-02 6.5e-04 1.00e+00 1.665138869e+02 1.665383940e+02 5.4e-09 1.08
53 9.3e-06 1.2e-02 5.8e-04 1.00e+00 1.665155611e+02 1.665376174e+02 4.8e-09 1.14
54 8.3e-06 1.2e-02 5.2e-04 1.00e+00 1.665170668e+02 1.665369173e+02 4.4e-09 1.20
55 7.5e-06 1.1e-02 4.7e-04 1.00e+00 1.665184211e+02 1.665362864e+02 3.9e-09 1.24
56 6.7e-06 1.1e-02 4.2e-04 1.00e+00 1.665196391e+02 1.665357179e+02 3.5e-09 1.25
57 6.1e-06 1.1e-02 3.8e-04 1.00e+00 1.665207348e+02 1.665352057e+02 3.2e-09 1.27
58 5.5e-06 1.0e-02 3.4e-04 1.00e+00 1.665217203e+02 1.665347442e+02 2.9e-09 1.34
59 4.9e-06 1.0e-02 3.1e-04 1.00e+00 1.665226069e+02 1.665343284e+02 2.6e-09 1.36
60 4.4e-06 9.9e-03 2.8e-04 1.00e+00 1.665234043e+02 1.665339537e+02 2.3e-09 1.42
61 4.0e-06 9.7e-03 2.5e-04 1.00e+00 1.665241217e+02 1.665336162e+02 2.1e-09 1.49
62 3.6e-06 9.5e-03 2.3e-04 1.00e+00 1.665247669e+02 1.665333120e+02 1.9e-09 1.51
63 3.2e-06 9.4e-03 2.0e-04 1.00e+00 1.665253472e+02 1.665330379e+02 1.7e-09 1.53
64 2.9e-06 9.2e-03 1.8e-04 1.00e+00 1.665258692e+02 1.665327909e+02 1.5e-09 1.56
65 2.6e-06 9.1e-03 1.6e-04 1.00e+00 1.665263387e+02 1.665325683e+02 1.4e-09 1.60
66 2.4e-06 9.0e-03 1.5e-04 1.00e+00 1.665267610e+02 1.665323677e+02 1.2e-09 1.64
67 2.1e-06 8.9e-03 1.3e-04 1.00e+00 1.665271409e+02 1.665321869e+02 1.1e-09 1.68
68 1.9e-06 8.8e-03 1.2e-04 1.00e+00 1.665274827e+02 1.665320241e+02 1.0e-09 1.75
69 1.7e-06 8.7e-03 1.1e-04 1.00e+00 1.665277901e+02 1.665318775e+02 9.0e-10 1.77
70 1.5e-06 8.6e-03 9.7e-05 1.00e+00 1.665280667e+02 1.665317454e+02 8.1e-10 1.85
71 1.4e-06 8.6e-03 8.7e-05 1.00e+00 1.665283155e+02 1.665316264e+02 7.3e-10 1.88
72 1.3e-06 8.5e-03 7.9e-05 1.00e+00 1.665285394e+02 1.665315192e+02 6.5e-10 1.88
73 1.1e-06 8.5e-03 7.1e-05 1.00e+00 1.665287408e+02 1.665314226e+02 5.9e-10 1.90
74 1.0e-06 8.4e-03 6.4e-05 1.00e+00 1.665289219e+02 1.665313356e+02 5.3e-10 1.91
75 9.1e-07 8.4e-03 5.7e-05 1.00e+00 1.665290848e+02 1.665312572e+02 4.8e-10 1.93
76 8.2e-07 8.3e-03 5.2e-05 1.00e+00 1.665292314e+02 1.665311865e+02 4.3e-10 1.97
77 7.4e-07 8.3e-03 4.6e-05 1.00e+00 1.665293632e+02 1.665311228e+02 3.9e-10 2.00
78 6.6e-07 8.2e-03 4.2e-05 1.00e+00 1.665294818e+02 1.665310655e+02 3.5e-10 2.06
79 6.0e-07 8.2e-03 3.8e-05 1.00e+00 1.665295884e+02 1.665310137e+02 3.1e-10 2.11
80 5.4e-07 8.2e-03 3.4e-05 1.00e+00 1.665296843e+02 1.665309671e+02 2.8e-10 2.12
81 4.8e-07 8.1e-03 3.0e-05 1.00e+00 1.665297706e+02 1.665309250e+02 2.5e-10 2.16
82 4.4e-07 8.1e-03 2.7e-05 9.98e-01 1.665298481e+02 1.665308872e+02 2.3e-10 2.20
83 3.9e-07 8.1e-03 2.5e-05 9.99e-01 1.665299178e+02 1.665308531e+02 2.1e-10 2.23
84 3.5e-07 8.0e-03 2.2e-05 9.98e-01 1.665299805e+02 1.665308223e+02 1.8e-10 2.26
85 3.2e-07 8.0e-03 2.0e-05 1.00e+00 1.665300369e+02 1.665307945e+02 1.7e-10 2.28
86 2.9e-07 8.0e-03 1.8e-05 1.00e+00 1.665300877e+02 1.665307695e+02 1.5e-10 2.35
87 2.6e-07 8.0e-03 1.6e-05 9.99e-01 1.665301333e+02 1.665307469e+02 1.3e-10 2.38
88 2.3e-07 7.9e-03 1.5e-05 9.96e-01 1.665301743e+02 1.665307267e+02 1.2e-10 2.40
89 2.1e-07 7.9e-03 1.3e-05 1.00e+00 1.665302113e+02 1.665307084e+02 1.1e-10 2.41
90 1.9e-07 7.9e-03 1.2e-05 9.95e-01 1.665302445e+02 1.665306920e+02 9.8e-11 2.46
91 1.7e-07 7.9e-03 1.1e-05 1.00e+00 1.665302743e+02 1.665306771e+02 8.8e-11 2.49
92 1.5e-07 7.1e-03 9.6e-06 1.01e+00 1.665303014e+02 1.665306635e+02 8.0e-11 2.55
93 1.4e-07 6.4e-03 8.6e-06 9.97e-01 1.665303256e+02 1.665306515e+02 7.2e-11 2.57
94 1.2e-07 5.7e-03 7.7e-06 9.98e-01 1.665303473e+02 1.665306407e+02 6.5e-11 2.63
95 1.1e-07 5.2e-03 7.0e-06 1.00e+00 1.665303669e+02 1.665306309e+02 5.8e-11 2.67
96 1.0e-07 4.7e-03 6.3e-06 1.00e+00 1.665303845e+02 1.665306221e+02 5.2e-11 2.72
97 9.0e-08 4.2e-03 5.6e-06 1.01e+00 1.665304008e+02 1.665306139e+02 4.7e-11 2.74
98 8.1e-08 3.8e-03 5.1e-06 1.01e+00 1.665304154e+02 1.665306066e+02 4.3e-11 2.78
99 7.3e-08 3.4e-03 4.6e-06 9.99e-01 1.665304282e+02 1.665306002e+02 3.8e-11 2.83
100 6.5e-08 3.1e-03 4.1e-06 9.92e-01 1.665304396e+02 1.665305946e+02 3.4e-11 2.92
101 5.9e-08 2.7e-03 3.7e-06 9.90e-01 1.665304500e+02 1.665305894e+02 3.1e-11 2.95
102 5.3e-08 2.5e-03 3.3e-06 1.01e+00 1.665304595e+02 1.665305847e+02 2.8e-11 2.97
103 4.8e-08 2.2e-03 3.0e-06 1.00e+00 1.665304678e+02 1.665305805e+02 2.5e-11 2.98
104 4.3e-08 2.0e-03 2.7e-06 9.89e-01 1.665304753e+02 1.665305768e+02 2.3e-11 3.00
105 3.9e-08 1.8e-03 2.4e-06 9.84e-01 1.665304821e+02 1.665305734e+02 2.0e-11 3.03
106 3.5e-08 1.6e-03 2.2e-06 9.89e-01 1.665304881e+02 1.665305704e+02 1.8e-11 3.07
107 3.1e-08 1.5e-03 2.0e-06 9.88e-01 1.665304936e+02 1.665305677e+02 1.7e-11 3.10
108 2.8e-08 1.3e-03 1.8e-06 1.01e+00 1.665304988e+02 1.665305650e+02 1.5e-11 3.11
109 2.5e-08 1.2e-03 1.6e-06 9.83e-01 1.665305032e+02 1.665305629e+02 1.3e-11 3.12
110 2.3e-08 1.1e-03 1.4e-06 1.01e+00 1.665305073e+02 1.665305608e+02 1.2e-11 3.14
111 2.1e-08 9.6e-04 1.3e-06 9.75e-01 1.665305108e+02 1.665305591e+02 1.1e-11 3.15
112 1.8e-08 8.6e-04 1.2e-06 1.00e+00 1.665305141e+02 1.665305574e+02 9.9e-12 3.16
113 1.7e-08 7.8e-04 1.0e-06 9.97e-01 1.665305170e+02 1.665305560e+02 8.9e-12 3.18
114 1.5e-08 7.0e-04 9.4e-07 1.10e+00 1.665305207e+02 1.665305539e+02 8.4e-12 3.19
115 1.3e-08 6.3e-04 8.5e-07 1.04e+00 1.665305233e+02 1.665305526e+02 7.7e-12 3.24
116 1.2e-08 5.7e-04 7.6e-07 1.07e+00 1.665305259e+02 1.665305512e+02 7.2e-12 3.29
117 1.1e-08 5.1e-04 6.9e-07 9.76e-01 1.665305276e+02 1.665305504e+02 6.4e-12 3.32
118 9.9e-09 4.6e-04 6.2e-07 9.72e-01 1.665305291e+02 1.665305497e+02 5.8e-12 3.38
119 8.9e-09 4.1e-04 5.6e-07 1.01e+00 1.665305305e+02 1.665305490e+02 5.2e-12 3.44
120 8.0e-09 3.7e-04 5.0e-07 9.23e-01 1.665305318e+02 1.665305484e+02 4.7e-12 3.48
121 7.2e-09 3.3e-04 4.5e-07 9.98e-01 1.665305329e+02 1.665305479e+02 4.2e-12 3.49
122 6.5e-09 3.0e-04 4.1e-07 1.05e+00 1.665305341e+02 1.665305472e+02 3.9e-12 3.55
123 6.0e-09 2.7e-04 3.6e-07 1.11e+00 1.665305354e+02 1.665305465e+02 3.7e-12 3.62
124 5.4e-09 2.4e-04 3.3e-07 9.17e-01 1.665305362e+02 1.665305462e+02 3.3e-12 3.67
125 4.9e-09 2.2e-04 3.0e-07 1.05e+00 1.665305370e+02 1.665305458e+02 3.1e-12 3.71
126 4.6e-09 2.0e-04 2.7e-07 9.62e-01 1.665305376e+02 1.665305455e+02 2.8e-12 3.76
127 4.7e-09 1.8e-04 2.4e-07 1.18e+00 1.665305385e+02 1.665305450e+02 2.7e-12 3.84
128 4.7e-09 1.6e-04 2.2e-07 1.20e+00 1.665305394e+02 1.665305445e+02 2.7e-12 3.89
129 4.3e-09 1.4e-04 1.9e-07 1.04e+00 1.665305398e+02 1.665305443e+02 2.5e-12 3.91
130 2.4e-09 8.2e-06 1.1e-08 1.00e+00 1.665305427e+02 1.665305430e+02 1.4e-13 3.92
Interior-point optimizer terminated. Time: 3.92.
Optimizer terminated. Time: 3.93
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6653054272e+02 Viol. con: 4e-08 var: 0e+00
Dual. obj: 1.6653054298e+02 Viol. con: 0e+00 var: 3e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.96 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.03 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.286069766e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.264280190e+05 3.575761773e+00 4.8e-01 0.06
2 4.3e+02 5.5e+02 2.4e+04 -9.36e-01 -1.202642600e+05 1.018055901e+01 1.9e-01 0.07
3 2.9e+02 3.7e+02 1.6e+04 -8.40e-01 -1.155864699e+05 6.348057000e+01 1.2e-01 0.09
4 2.8e+02 3.7e+02 1.6e+04 -7.60e-01 -1.129604570e+05 2.275516183e+03 1.2e-01 0.16
5 7.5e+01 9.6e+01 4.2e+03 -7.53e-01 -7.467569926e+04 9.661818848e+03 3.3e-02 0.17
6 3.3e+01 4.2e+01 1.8e+03 -1.93e-01 -4.344555550e+04 1.030574895e+04 1.4e-02 0.19
7 1.9e+01 2.5e+01 1.1e+03 3.43e-01 -2.866888252e+04 6.921959471e+03 8.5e-03 0.20
8 1.1e+01 1.5e+01 6.3e+02 6.05e-01 -1.820597939e+04 4.395204082e+03 5.0e-03 0.21
9 4.5e+00 5.8e+00 2.5e+02 7.73e-01 -7.371166904e+03 2.103309766e+03 2.0e-03 0.23
10 2.1e+00 2.7e+00 1.2e+02 9.30e-01 -3.214990468e+03 1.325823099e+03 9.3e-04 0.25
11 1.3e+00 1.7e+00 7.5e+01 9.81e-01 -2.014767646e+03 8.899276566e+02 6.0e-04 0.26
12 8.1e-01 1.0e+00 4.5e+01 9.84e-01 -1.165870649e+03 6.060224068e+02 3.6e-04 0.28
13 6.4e-01 8.5e-01 3.6e+01 9.55e-01 -9.120507046e+02 5.060745857e+02 2.9e-04 0.29
14 3.6e-01 4.9e-01 2.0e+01 9.93e-01 -4.191575491e+02 3.802511459e+02 1.6e-04 0.30
15 1.8e-01 2.4e-01 1.0e+01 9.93e-01 -1.346795984e+02 2.582567727e+02 8.0e-05 0.31
16 7.9e-02 1.4e-01 4.6e+00 1.01e+00 2.126792483e+01 1.996179868e+02 3.7e-05 0.33
17 6.8e-02 1.2e-01 3.9e+00 1.02e+00 4.474499175e+01 1.978720383e+02 3.2e-05 0.34
18 2.8e-02 7.4e-02 1.6e+00 1.02e+00 1.178045934e+02 1.806433001e+02 1.3e-05 0.35
19 8.1e-03 2.0e-01 4.7e-01 1.01e+00 1.531909913e+02 1.714402073e+02 3.8e-06 0.54
20 2.9e-03 2.3e-01 1.7e-01 1.00e+00 1.613911991e+02 1.680582047e+02 1.4e-06 0.83
21 1.7e-03 1.4e-01 1.0e-01 1.01e+00 1.635874230e+02 1.674597121e+02 8.2e-07 0.99
22 5.0e-04 1.2e-01 3.1e-02 1.01e+00 1.656228560e+02 1.668056681e+02 2.5e-07 1.23
23 1.9e-04 1.0e-01 1.2e-02 1.01e+00 1.661602583e+02 1.666050994e+02 9.7e-08 1.46
24 8.5e-05 8.7e-02 5.4e-03 1.01e+00 1.663313715e+02 1.665357285e+02 4.5e-08 1.54
25 3.9e-05 7.9e-02 2.5e-03 1.01e+00 1.664099188e+02 1.665032835e+02 2.1e-08 1.63
26 3.5e-05 7.2e-02 2.2e-03 1.01e+00 1.664180564e+02 1.665021090e+02 1.9e-08 1.67
27 3.1e-05 6.6e-02 2.0e-03 1.01e+00 1.664237676e+02 1.664993862e+02 1.7e-08 1.74
28 2.8e-05 6.0e-02 1.8e-03 1.01e+00 1.664290361e+02 1.664970782e+02 1.5e-08 1.75
29 2.5e-05 5.5e-02 1.6e-03 1.01e+00 1.664337498e+02 1.664949751e+02 1.4e-08 1.76
30 2.3e-05 5.0e-02 1.5e-03 1.01e+00 1.664379869e+02 1.664930794e+02 1.2e-08 1.78
31 2.1e-05 4.6e-02 1.3e-03 1.00e+00 1.664417927e+02 1.664913676e+02 1.1e-08 1.80
32 1.8e-05 4.2e-02 1.2e-03 1.00e+00 1.664452121e+02 1.664898226e+02 1.0e-08 1.89
33 1.7e-05 3.9e-02 1.1e-03 1.00e+00 1.664482844e+02 1.664884284e+02 9.0e-09 2.23
34 1.5e-05 3.6e-02 9.6e-04 1.00e+00 1.664510454e+02 1.664871705e+02 8.1e-09 2.49
35 1.3e-05 3.3e-02 8.6e-04 1.00e+00 1.664535268e+02 1.664860357e+02 7.3e-09 2.59
36 1.2e-05 3.0e-02 7.8e-04 1.00e+00 1.664557571e+02 1.664850122e+02 6.5e-09 2.72
37 1.1e-05 2.8e-02 7.0e-04 1.00e+00 1.664577620e+02 1.664840892e+02 5.9e-09 3.23
38 9.8e-06 2.6e-02 6.3e-04 1.00e+00 1.664595644e+02 1.664832570e+02 5.3e-09 3.53
39 8.8e-06 2.4e-02 5.7e-04 1.00e+00 1.664611850e+02 1.664825068e+02 4.8e-09 3.72
40 8.0e-06 2.3e-02 5.1e-04 1.00e+00 1.664626422e+02 1.664818306e+02 4.3e-09 4.07
41 7.2e-06 2.1e-02 4.6e-04 1.00e+00 1.664639526e+02 1.664812212e+02 3.9e-09 4.37
42 6.4e-06 2.0e-02 4.1e-04 1.00e+00 1.664651312e+02 1.664806721e+02 3.5e-09 4.60
43 5.8e-06 1.9e-02 3.7e-04 1.00e+00 1.664661912e+02 1.664801774e+02 3.1e-09 4.90
44 5.2e-06 1.7e-02 3.3e-04 1.00e+00 1.664671446e+02 1.664797317e+02 2.8e-09 5.48
45 4.7e-06 1.6e-02 3.0e-04 1.00e+00 1.664680022e+02 1.664793303e+02 2.5e-09 5.81
46 4.2e-06 1.6e-02 2.7e-04 1.00e+00 1.664687737e+02 1.664789687e+02 2.3e-09 6.15
47 3.8e-06 1.5e-02 2.4e-04 1.00e+00 1.664694676e+02 1.664786429e+02 2.1e-09 6.48
48 3.4e-06 1.4e-02 2.2e-04 1.00e+00 1.664700919e+02 1.664783495e+02 1.8e-09 6.83
49 3.1e-06 1.3e-02 2.0e-04 1.00e+00 1.664706535e+02 1.664780852e+02 1.7e-09 7.22
50 2.8e-06 1.3e-02 1.8e-04 1.00e+00 1.664711587e+02 1.664778472e+02 1.5e-09 7.63
51 2.5e-06 1.2e-02 1.6e-04 1.00e+00 1.664716133e+02 1.664776328e+02 1.3e-09 7.96
52 2.2e-06 1.2e-02 1.4e-04 1.00e+00 1.664720223e+02 1.664774398e+02 1.2e-09 8.19
53 2.0e-06 1.1e-02 1.3e-04 1.00e+00 1.664723903e+02 1.664772661e+02 1.1e-09 8.39
54 1.8e-06 1.1e-02 1.2e-04 1.00e+00 1.664727215e+02 1.664771097e+02 9.8e-10 8.53
55 1.6e-06 1.1e-02 1.0e-04 1.00e+00 1.664730196e+02 1.664769689e+02 8.8e-10 8.61
56 1.5e-06 1.0e-02 9.4e-05 1.00e+00 1.664732878e+02 1.664768422e+02 8.0e-10 8.69
57 1.3e-06 1.0e-02 8.5e-05 1.00e+00 1.664735292e+02 1.664767281e+02 7.2e-10 8.93
58 1.2e-06 9.9e-03 7.6e-05 1.00e+00 1.664737464e+02 1.664766254e+02 6.5e-10 9.22
59 1.1e-06 9.6e-03 6.9e-05 1.00e+00 1.664739419e+02 1.664765330e+02 5.8e-10 9.59
60 9.7e-07 9.4e-03 6.2e-05 1.00e+00 1.664741178e+02 1.664764498e+02 5.2e-10 10.09
61 8.7e-07 9.2e-03 5.6e-05 1.00e+00 1.664742761e+02 1.664763749e+02 4.7e-10 10.43
62 7.8e-07 9.1e-03 5.0e-05 1.00e+00 1.664744185e+02 1.664763074e+02 4.2e-10 10.78
63 7.1e-07 8.9e-03 4.5e-05 1.00e+00 1.664745467e+02 1.664762467e+02 3.8e-10 11.04
64 6.3e-07 8.8e-03 4.1e-05 1.00e+00 1.664746620e+02 1.664761920e+02 3.4e-10 11.33
65 5.7e-07 8.7e-03 3.7e-05 1.00e+00 1.664747658e+02 1.664761427e+02 3.1e-10 11.70
66 5.1e-07 8.6e-03 3.3e-05 1.00e+00 1.664748591e+02 1.664760984e+02 2.8e-10 12.21
67 4.6e-07 8.5e-03 3.0e-05 1.00e+00 1.664749431e+02 1.664760584e+02 2.5e-10 12.55
68 4.2e-07 8.4e-03 2.7e-05 1.00e+00 1.664750186e+02 1.664760224e+02 2.2e-10 12.91
69 3.7e-07 8.3e-03 2.4e-05 1.00e+00 1.664750865e+02 1.664759899e+02 2.0e-10 13.16
70 3.4e-07 8.2e-03 2.2e-05 1.00e+00 1.664751477e+02 1.664759606e+02 1.8e-10 13.39
71 3.0e-07 8.2e-03 1.9e-05 9.99e-01 1.664752026e+02 1.664759344e+02 1.6e-10 13.72
72 2.7e-07 8.1e-03 1.7e-05 1.00e+00 1.664752521e+02 1.664759106e+02 1.5e-10 14.02
73 2.5e-07 8.1e-03 1.6e-05 1.00e+00 1.664752966e+02 1.664758893e+02 1.3e-10 14.56
74 2.2e-07 8.0e-03 1.4e-05 9.98e-01 1.664753366e+02 1.664758701e+02 1.2e-10 14.99
75 2.0e-07 8.0e-03 1.3e-05 1.00e+00 1.664753726e+02 1.664758528e+02 1.1e-10 15.34
76 1.8e-07 7.9e-03 1.1e-05 1.00e+00 1.664754052e+02 1.664758370e+02 9.7e-11 15.59
77 1.6e-07 7.9e-03 1.0e-05 1.00e+00 1.664754343e+02 1.664758230e+02 8.7e-11 15.80
78 1.5e-07 7.8e-03 9.3e-06 9.97e-01 1.664754605e+02 1.664758104e+02 7.8e-11 15.98
79 1.3e-07 7.8e-03 8.4e-06 1.00e+00 1.664754842e+02 1.664757990e+02 7.1e-11 16.07
80 1.2e-07 7.8e-03 7.5e-06 9.99e-01 1.664755054e+02 1.664757888e+02 6.4e-11 16.39
81 1.1e-07 7.8e-03 6.8e-06 1.00e+00 1.664755246e+02 1.664757795e+02 5.7e-11 16.94
82 9.5e-08 7.7e-03 6.1e-06 9.95e-01 1.664755418e+02 1.664757713e+02 5.2e-11 17.27
83 8.6e-08 7.7e-03 5.5e-06 1.00e+00 1.664755573e+02 1.664757638e+02 4.6e-11 17.67
84 7.7e-08 7.7e-03 4.9e-06 1.00e+00 1.664755712e+02 1.664757570e+02 4.2e-11 18.12
85 6.9e-08 7.7e-03 4.4e-06 9.95e-01 1.664755837e+02 1.664757510e+02 3.8e-11 18.52
86 6.2e-08 7.6e-03 4.0e-06 9.98e-01 1.664755950e+02 1.664757456e+02 3.4e-11 18.82
87 5.6e-08 7.6e-03 3.6e-06 1.00e+00 1.664756052e+02 1.664757406e+02 3.0e-11 19.22
88 5.1e-08 7.6e-03 3.2e-06 1.00e+00 1.664756143e+02 1.664757362e+02 2.7e-11 19.51
89 4.6e-08 7.6e-03 2.9e-06 1.00e+00 1.664756225e+02 1.664757322e+02 2.5e-11 19.97
90 4.1e-08 6.8e-03 2.6e-06 1.00e+00 1.664756300e+02 1.664757286e+02 2.2e-11 20.30
91 3.7e-08 6.1e-03 2.4e-06 9.94e-01 1.664756367e+02 1.664757254e+02 2.0e-11 20.73
92 3.3e-08 5.5e-03 2.1e-06 1.00e+00 1.664756426e+02 1.664757225e+02 1.8e-11 21.37
93 3.0e-08 5.0e-03 1.9e-06 9.95e-01 1.664756480e+02 1.664757199e+02 1.6e-11 21.73
94 2.7e-08 4.5e-03 1.7e-06 1.00e+00 1.664756529e+02 1.664757176e+02 1.5e-11 22.05
95 2.4e-08 4.0e-03 1.6e-06 1.01e+00 1.664756575e+02 1.664757153e+02 1.3e-11 22.41
96 2.2e-08 3.6e-03 1.4e-06 1.00e+00 1.664756614e+02 1.664757134e+02 1.2e-11 22.94
97 2.0e-08 3.3e-03 1.3e-06 1.02e+00 1.664756651e+02 1.664757116e+02 1.1e-11 23.59
98 1.8e-08 2.9e-03 1.1e-06 9.96e-01 1.664756683e+02 1.664757101e+02 9.7e-12 24.02
99 1.6e-08 2.6e-03 1.0e-06 1.02e+00 1.664756713e+02 1.664757086e+02 8.8e-12 24.47
100 1.4e-08 2.4e-03 9.2e-07 1.03e+00 1.664756742e+02 1.664757072e+02 8.0e-12 24.90
101 1.3e-08 2.1e-03 8.2e-07 9.72e-01 1.664756764e+02 1.664757061e+02 7.2e-12 25.37
102 1.2e-08 1.9e-03 7.4e-07 1.06e+00 1.664756789e+02 1.664757049e+02 6.7e-12 25.94
103 1.0e-08 1.7e-03 6.7e-07 1.01e+00 1.664756808e+02 1.664757040e+02 6.1e-12 26.38
104 9.4e-09 1.6e-03 6.0e-07 9.87e-01 1.664756823e+02 1.664757032e+02 5.5e-12 26.81
105 2.2e-09 1.6e-04 6.2e-08 9.90e-01 1.664756950e+02 1.664756972e+02 5.8e-13 27.13
Interior-point optimizer terminated. Time: 27.14.
Optimizer terminated. Time: 27.15
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6647569505e+02 Viol. con: 4e-08 var: 0e+00
Dual. obj: 1.6647569720e+02 Viol. con: 0e+00 var: 1e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 27.2 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.02
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3439 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.03 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.285358117e+05 2.000000000e+00 1.0e+00 0.05
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.263542085e+05 3.574445468e+00 4.8e-01 0.06
2 4.3e+02 5.5e+02 2.4e+04 -9.36e-01 -1.201588472e+05 1.021567231e+01 1.9e-01 0.07
3 2.9e+02 3.7e+02 1.6e+04 -8.39e-01 -1.154718917e+05 6.399968046e+01 1.2e-01 0.09
4 2.8e+02 3.7e+02 1.6e+04 -7.59e-01 -1.128613765e+05 2.263785696e+03 1.2e-01 0.10
5 7.5e+01 9.7e+01 4.2e+03 -7.52e-01 -7.480743550e+04 9.600131301e+03 3.3e-02 0.12
6 3.0e+01 3.9e+01 1.7e+03 -1.96e-01 -4.068261743e+04 1.026881490e+04 1.3e-02 0.13
7 1.8e+01 2.3e+01 1.0e+03 3.91e-01 -2.712655858e+04 6.680853695e+03 7.9e-03 0.14
8 9.7e+00 1.2e+01 5.4e+02 6.31e-01 -1.569361656e+04 3.889214983e+03 4.3e-03 0.15
9 3.9e+00 5.0e+00 2.2e+02 8.12e-01 -6.429968337e+03 1.893873530e+03 1.7e-03 0.17
10 2.1e+00 2.7e+00 1.2e+02 9.41e-01 -3.286676875e+03 1.204165331e+03 9.2e-04 0.18
11 1.0e+00 1.3e+00 5.9e+01 9.80e-01 -1.544941282e+03 7.355115621e+02 4.7e-04 0.23
12 8.1e-01 1.0e+00 4.5e+01 9.78e-01 -1.184101277e+03 6.013207806e+02 3.6e-04 0.24
13 4.8e-01 6.2e-01 2.7e+01 9.74e-01 -6.380956895e+02 4.207594054e+02 2.1e-04 0.51
14 2.6e-01 3.6e-01 1.5e+01 1.00e+00 -2.718762467e+02 3.084915877e+02 1.2e-04 0.67
15 9.7e-02 1.5e-01 5.5e+00 1.00e+00 -1.010192524e+01 2.072399472e+02 4.5e-05 0.69
16 8.6e-02 1.3e-01 4.9e+00 1.02e+00 1.582480471e+01 2.085964057e+02 4.0e-05 0.71
17 5.3e-02 8.8e-02 3.1e+00 1.02e+00 7.252853999e+01 1.918878922e+02 2.5e-05 0.72
18 2.3e-02 6.9e-02 1.3e+00 1.02e+00 1.266655683e+02 1.778066257e+02 1.1e-05 0.73
19 6.2e-03 2.3e-01 3.7e-01 1.01e+00 1.562529231e+02 1.702799638e+02 2.9e-06 0.75
20 3.1e-03 3.1e-01 1.8e-01 1.00e+00 1.610359052e+02 1.681101297e+02 1.5e-06 0.76
21 1.6e-03 1.7e-01 9.8e-02 1.01e+00 1.636142750e+02 1.673814360e+02 8.0e-07 0.77
22 4.9e-04 1.4e-01 3.0e-02 1.01e+00 1.656242398e+02 1.667725437e+02 2.5e-07 0.78
23 3.1e-04 1.1e-01 1.9e-02 9.98e-01 1.659258400e+02 1.666521482e+02 1.6e-07 0.80
24 1.9e-04 7.7e-02 1.2e-02 9.85e-01 1.661267131e+02 1.665737826e+02 9.7e-08 0.81
25 1.7e-04 6.6e-02 1.0e-02 9.99e-01 1.661696325e+02 1.665612833e+02 8.5e-08 0.82
26 1.5e-04 6.0e-02 9.3e-03 1.01e+00 1.661982519e+02 1.665504953e+02 7.7e-08 0.83
27 1.3e-04 5.5e-02 8.4e-03 1.01e+00 1.662230712e+02 1.665399625e+02 6.9e-08 0.85
28 1.2e-04 5.0e-02 7.5e-03 1.01e+00 1.662455484e+02 1.665306826e+02 6.2e-08 0.86
29 1.1e-04 4.6e-02 6.8e-03 1.01e+00 1.662656857e+02 1.665222505e+02 5.6e-08 0.87
30 9.8e-05 4.2e-02 6.1e-03 1.01e+00 1.662837605e+02 1.665146234e+02 5.1e-08 0.89
31 8.8e-05 3.8e-02 5.5e-03 1.01e+00 1.662999797e+02 1.665077195e+02 4.5e-08 0.90
32 7.9e-05 3.5e-02 4.9e-03 1.01e+00 1.663145356e+02 1.665014716e+02 4.1e-08 0.91
33 7.1e-05 3.3e-02 4.4e-03 1.00e+00 1.663275992e+02 1.664958177e+02 3.7e-08 0.93
34 6.4e-05 3.0e-02 4.0e-03 1.00e+00 1.663393246e+02 1.664907020e+02 3.3e-08 0.94
35 5.8e-05 2.8e-02 3.6e-03 1.00e+00 1.663498497e+02 1.664860740e+02 3.0e-08 0.96
36 5.2e-05 2.6e-02 3.2e-03 1.00e+00 1.663592984e+02 1.664818880e+02 2.7e-08 0.97
37 4.7e-05 2.4e-02 2.9e-03 1.00e+00 1.663677816e+02 1.664781026e+02 2.4e-08 0.98
38 4.2e-05 2.2e-02 2.6e-03 1.00e+00 1.663753989e+02 1.664746801e+02 2.2e-08 1.00
39 3.8e-05 2.1e-02 2.4e-03 1.00e+00 1.663822394e+02 1.664715863e+02 2.0e-08 1.01
40 3.4e-05 1.9e-02 2.1e-03 1.00e+00 1.663883828e+02 1.664687903e+02 1.8e-08 1.02
41 3.1e-05 1.8e-02 1.9e-03 1.00e+00 1.663939007e+02 1.664662637e+02 1.6e-08 1.04
42 2.8e-05 1.7e-02 1.7e-03 1.00e+00 1.663988572e+02 1.664639809e+02 1.4e-08 1.05
43 2.5e-05 1.6e-02 1.6e-03 1.00e+00 1.664033097e+02 1.664619188e+02 1.3e-08 1.06
44 2.2e-05 1.5e-02 1.4e-03 1.00e+00 1.664073098e+02 1.664600563e+02 1.2e-08 1.07
45 2.0e-05 1.5e-02 1.3e-03 1.00e+00 1.664109036e+02 1.664583741e+02 1.0e-08 1.09
46 1.8e-05 1.4e-02 1.1e-03 1.00e+00 1.664141327e+02 1.664568551e+02 9.4e-09 1.10
47 1.6e-05 1.3e-02 1.0e-03 1.00e+00 1.664170342e+02 1.664554836e+02 8.4e-09 1.11
48 1.5e-05 1.3e-02 9.2e-04 1.00e+00 1.664196415e+02 1.664542454e+02 7.6e-09 1.13
49 1.3e-05 1.2e-02 8.2e-04 1.00e+00 1.664219846e+02 1.664531277e+02 6.8e-09 1.14
50 1.2e-05 1.2e-02 7.4e-04 1.00e+00 1.664240905e+02 1.664521190e+02 6.2e-09 1.15
51 1.1e-05 1.1e-02 6.7e-04 1.00e+00 1.664259832e+02 1.664512087e+02 5.5e-09 1.16
52 9.6e-06 1.1e-02 6.0e-04 1.00e+00 1.664276845e+02 1.664503874e+02 5.0e-09 1.18
53 8.6e-06 1.1e-02 5.4e-04 1.00e+00 1.664292138e+02 1.664496464e+02 4.5e-09 1.19
54 7.8e-06 1.0e-02 4.9e-04 1.00e+00 1.664305887e+02 1.664489780e+02 4.0e-09 1.21
55 7.0e-06 1.0e-02 4.4e-04 1.00e+00 1.664318247e+02 1.664483751e+02 3.6e-09 1.22
56 6.3e-06 9.9e-03 3.9e-04 1.00e+00 1.664329360e+02 1.664478314e+02 3.3e-09 1.24
57 5.7e-06 9.7e-03 3.5e-04 1.00e+00 1.664339352e+02 1.664473412e+02 2.9e-09 1.25
58 5.1e-06 9.6e-03 3.2e-04 1.00e+00 1.664348337e+02 1.664468991e+02 2.7e-09 1.26
59 4.6e-06 9.4e-03 2.9e-04 1.00e+00 1.664356416e+02 1.664465005e+02 2.4e-09 1.28
60 4.1e-06 9.2e-03 2.6e-04 1.00e+00 1.664363681e+02 1.664461412e+02 2.1e-09 1.29
61 3.7e-06 9.1e-03 2.3e-04 1.00e+00 1.664370213e+02 1.664458172e+02 1.9e-09 1.30
62 3.3e-06 9.0e-03 2.1e-04 1.00e+00 1.664376088e+02 1.664455251e+02 1.7e-09 1.32
63 3.0e-06 8.9e-03 1.9e-04 1.00e+00 1.664381370e+02 1.664452618e+02 1.6e-09 1.33
64 2.7e-06 8.7e-03 1.7e-04 1.00e+00 1.664386121e+02 1.664450245e+02 1.4e-09 1.35
65 2.4e-06 8.7e-03 1.5e-04 1.00e+00 1.664390394e+02 1.664448106e+02 1.3e-09 1.36
66 2.2e-06 8.6e-03 1.4e-04 1.00e+00 1.664394237e+02 1.664446179e+02 1.1e-09 1.37
67 2.0e-06 8.5e-03 1.2e-04 1.00e+00 1.664397695e+02 1.664444443e+02 1.0e-09 1.39
68 1.8e-06 8.4e-03 1.1e-04 1.00e+00 1.664400806e+02 1.664442879e+02 9.3e-10 1.40
69 1.6e-06 8.3e-03 1.0e-04 1.00e+00 1.664403604e+02 1.664441471e+02 8.3e-10 1.42
70 1.4e-06 8.3e-03 9.0e-05 1.00e+00 1.664406121e+02 1.664440202e+02 7.5e-10 1.43
71 1.3e-06 8.2e-03 8.1e-05 1.00e+00 1.664408386e+02 1.664439059e+02 6.7e-10 1.44
72 1.2e-06 8.2e-03 7.3e-05 1.00e+00 1.664410424e+02 1.664438030e+02 6.1e-10 1.46
73 1.1e-06 8.1e-03 6.6e-05 1.00e+00 1.664412257e+02 1.664437103e+02 5.5e-10 1.47
74 9.5e-07 8.1e-03 5.9e-05 1.00e+00 1.664413906e+02 1.664436268e+02 4.9e-10 1.48
75 8.5e-07 8.0e-03 5.3e-05 1.00e+00 1.664415390e+02 1.664435515e+02 4.4e-10 1.50
76 7.7e-07 8.0e-03 4.8e-05 1.00e+00 1.664416725e+02 1.664434838e+02 4.0e-10 1.51
77 6.9e-07 7.9e-03 4.3e-05 1.00e+00 1.664417926e+02 1.664434227e+02 3.6e-10 1.52
78 6.2e-07 7.9e-03 3.9e-05 1.00e+00 1.664419007e+02 1.664433677e+02 3.2e-10 1.54
79 5.6e-07 7.9e-03 3.5e-05 1.00e+00 1.664419978e+02 1.664433182e+02 2.9e-10 1.55
80 5.0e-07 7.8e-03 3.1e-05 1.00e+00 1.664420853e+02 1.664432736e+02 2.6e-10 1.56
81 4.5e-07 7.8e-03 2.8e-05 1.00e+00 1.664421639e+02 1.664432333e+02 2.4e-10 1.57
82 4.1e-07 7.8e-03 2.5e-05 1.00e+00 1.664422347e+02 1.664431972e+02 2.1e-10 1.76
83 3.7e-07 7.8e-03 2.3e-05 1.00e+00 1.664422983e+02 1.664431646e+02 1.9e-10 1.88
84 3.3e-07 7.7e-03 2.1e-05 1.00e+00 1.664423556e+02 1.664431352e+02 1.7e-10 1.97
85 3.0e-07 7.7e-03 1.9e-05 9.99e-01 1.664424071e+02 1.664431088e+02 1.5e-10 2.05
86 2.7e-07 7.7e-03 1.7e-05 1.00e+00 1.664424535e+02 1.664430850e+02 1.4e-10 2.06
87 2.4e-07 7.7e-03 1.5e-05 1.00e+00 1.664424952e+02 1.664430636e+02 1.3e-10 2.07
88 2.2e-07 7.7e-03 1.4e-05 1.00e+00 1.664425328e+02 1.664430443e+02 1.1e-10 2.09
89 1.9e-07 7.6e-03 1.2e-05 1.00e+00 1.664425666e+02 1.664430269e+02 1.0e-10 2.10
90 1.8e-07 7.6e-03 1.1e-05 1.00e+00 1.664425970e+02 1.664430113e+02 9.1e-11 2.11
91 1.6e-07 7.6e-03 9.9e-06 1.00e+00 1.664426244e+02 1.664429972e+02 8.2e-11 2.13
92 1.4e-07 7.6e-03 8.9e-06 1.00e+00 1.664426490e+02 1.664429846e+02 7.4e-11 2.14
93 1.3e-07 7.6e-03 8.0e-06 1.00e+00 1.664426712e+02 1.664429732e+02 6.6e-11 2.15
94 1.2e-07 7.6e-03 7.2e-06 9.97e-01 1.664426912e+02 1.664429630e+02 6.0e-11 2.17
95 1.0e-07 6.8e-03 6.5e-06 1.00e+00 1.664427092e+02 1.664429537e+02 5.4e-11 2.18
96 9.3e-08 6.1e-03 5.8e-06 9.98e-01 1.664427253e+02 1.664429454e+02 4.8e-11 2.19
97 8.4e-08 5.5e-03 5.2e-06 9.97e-01 1.664427399e+02 1.664429380e+02 4.4e-11 2.20
98 7.5e-08 5.0e-03 4.7e-06 9.91e-01 1.664427529e+02 1.664429313e+02 3.9e-11 2.22
99 6.8e-08 4.5e-03 4.3e-06 1.00e+00 1.664427647e+02 1.664429253e+02 3.5e-11 2.23
100 6.1e-08 4.0e-03 3.8e-06 1.00e+00 1.664427754e+02 1.664429198e+02 3.2e-11 2.25
101 5.5e-08 3.6e-03 3.4e-06 1.00e+00 1.664427850e+02 1.664429149e+02 2.9e-11 2.26
102 5.0e-08 3.3e-03 3.1e-06 1.00e+00 1.664427935e+02 1.664429104e+02 2.6e-11 2.27
103 4.5e-08 2.9e-03 2.8e-06 9.99e-01 1.664428013e+02 1.664429065e+02 2.3e-11 2.28
104 4.0e-08 2.6e-03 2.5e-06 9.87e-01 1.664428082e+02 1.664429030e+02 2.1e-11 2.30
105 3.6e-08 2.4e-03 2.3e-06 1.01e+00 1.664428147e+02 1.664428996e+02 1.9e-11 2.31
106 3.2e-08 2.1e-03 2.0e-06 9.95e-01 1.664428203e+02 1.664428967e+02 1.7e-11 2.32
107 2.9e-08 1.9e-03 1.8e-06 9.96e-01 1.664428254e+02 1.664428942e+02 1.5e-11 2.34
108 2.6e-08 1.7e-03 1.6e-06 1.00e+00 1.664428299e+02 1.664428918e+02 1.4e-11 2.35
109 2.4e-08 1.6e-03 1.5e-06 1.01e+00 1.664428341e+02 1.664428897e+02 1.2e-11 2.36
110 2.1e-08 1.4e-03 1.3e-06 1.00e+00 1.664428378e+02 1.664428878e+02 1.1e-11 2.37
111 1.9e-08 1.3e-03 1.2e-06 9.43e-01 1.664428411e+02 1.664428861e+02 1.0e-11 2.38
112 1.7e-08 1.1e-03 1.1e-06 1.04e+00 1.664428446e+02 1.664428842e+02 9.2e-12 2.40
113 1.6e-08 1.0e-03 9.7e-07 1.08e+00 1.664428481e+02 1.664428823e+02 8.6e-12 2.41
114 1.4e-08 9.2e-04 8.8e-07 1.02e+00 1.664428505e+02 1.664428811e+02 7.8e-12 2.42
115 1.3e-08 8.3e-04 7.9e-07 1.08e+00 1.664428533e+02 1.664428796e+02 7.3e-12 2.43
116 1.2e-08 7.5e-04 7.1e-07 8.82e-01 1.664428550e+02 1.664428787e+02 6.5e-12 2.45
117 1.1e-08 6.7e-04 6.4e-07 8.80e-01 1.664428566e+02 1.664428780e+02 5.9e-12 2.46
118 9.4e-09 6.0e-04 5.7e-07 9.29e-01 1.664428580e+02 1.664428774e+02 5.3e-12 2.47
119 8.5e-09 5.4e-04 5.2e-07 9.19e-01 1.664428593e+02 1.664428767e+02 4.8e-12 2.49
120 8.1e-09 4.9e-04 4.7e-07 1.04e+00 1.664428606e+02 1.664428760e+02 4.4e-12 2.50
121 7.5e-09 4.4e-04 4.2e-07 1.02e+00 1.664428617e+02 1.664428755e+02 4.0e-12 2.51
122 1.0e-08 4.0e-04 3.8e-07 1.20e+00 1.664428635e+02 1.664428743e+02 3.9e-12 2.52
123 1.0e-08 3.6e-04 3.4e-07 7.44e-01 1.664428643e+02 1.664428739e+02 3.5e-12 2.53
124 1.5e-08 3.2e-04 3.1e-07 1.19e+00 1.664428654e+02 1.664428731e+02 3.5e-12 2.55
125 1.7e-08 2.9e-04 2.8e-07 4.86e-01 1.664428661e+02 1.664428726e+02 3.1e-12 2.56
126 1.6e-08 2.6e-04 2.5e-07 1.29e+00 1.664428666e+02 1.664428724e+02 2.8e-12 2.57
127 1.3e-08 2.4e-04 2.3e-07 3.99e-01 1.664428670e+02 1.664428724e+02 2.5e-12 2.58
128 1.7e-08 2.1e-04 2.6e-07 1.00e+00 1.664428659e+02 1.664428722e+02 2.3e-12 2.59
129 1.8e-08 1.9e-04 2.4e-07 3.30e+00 1.664428658e+02 1.664428727e+02 2.0e-12 2.61
130 1.6e-08 1.7e-04 2.1e-07 7.03e-01 1.664428662e+02 1.664428726e+02 1.8e-12 2.62
131 1.4e-08 1.6e-04 1.9e-07 1.56e+00 1.664428666e+02 1.664428724e+02 1.6e-12 2.63
132 1.2e-08 1.4e-04 1.7e-07 1.67e+00 1.664428671e+02 1.664428722e+02 1.5e-12 2.65
133 1.3e-08 1.3e-04 1.9e-07 1.00e+00 1.664428666e+02 1.664428720e+02 1.3e-12 2.66
134 1.2e-08 1.1e-04 1.7e-07 7.76e-01 1.664428671e+02 1.664428719e+02 1.2e-12 2.68
135 1.1e-08 1.0e-04 1.5e-07 5.25e-01 1.664428674e+02 1.664428718e+02 1.1e-12 2.69
136 1.2e-08 9.2e-05 1.4e-07 9.92e-01 1.664428678e+02 1.664428717e+02 9.6e-13 2.70
Interior-point optimizer terminated. Time: 2.70.
Optimizer terminated. Time: 2.71
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6644286777e+02 Viol. con: 3e-07 var: 0e+00
Dual. obj: 1.6644287173e+02 Viol. con: 0e+00 var: 5e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.74 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3439 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.03 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.285340957e+05 2.000000000e+00 1.0e+00 0.05
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.263517283e+05 3.573621329e+00 4.8e-01 0.06
2 4.3e+02 5.5e+02 2.4e+04 -9.36e-01 -1.201360090e+05 1.023272656e+01 1.8e-01 0.08
3 2.9e+02 3.7e+02 1.6e+04 -8.39e-01 -1.154380586e+05 6.426640353e+01 1.2e-01 0.09
4 2.8e+02 3.6e+02 1.6e+04 -7.59e-01 -1.128348628e+05 2.258318868e+03 1.2e-01 0.11
5 7.5e+01 9.6e+01 4.1e+03 -7.52e-01 -7.471880335e+04 9.598257258e+03 3.3e-02 0.12
6 3.0e+01 3.9e+01 1.7e+03 -1.95e-01 -4.050837111e+04 1.020869836e+04 1.3e-02 0.13
7 1.8e+01 2.3e+01 1.0e+03 3.94e-01 -2.711076981e+04 6.648787000e+03 7.9e-03 0.15
8 9.5e+00 1.2e+01 5.3e+02 6.30e-01 -1.542139758e+04 3.834874078e+03 4.2e-03 0.16
9 3.6e+00 4.7e+00 2.0e+02 8.16e-01 -5.933715770e+03 1.798172324e+03 1.6e-03 0.17
10 2.0e+00 2.6e+00 1.1e+02 9.47e-01 -3.130705089e+03 1.194463503e+03 8.9e-04 0.19
11 8.4e-01 1.1e+00 4.7e+01 9.81e-01 -1.229432961e+03 6.158762901e+02 3.8e-04 0.20
12 8.2e-01 1.1e+00 4.6e+01 9.50e-01 -1.213196380e+03 5.912535389e+02 3.7e-04 0.22
13 5.1e-01 6.6e-01 2.9e+01 9.72e-01 -7.067517247e+02 4.266802042e+02 2.3e-04 0.23
14 3.1e-01 4.2e-01 1.8e+01 1.00e+00 -3.527408526e+02 3.411005417e+02 1.4e-04 0.24
15 1.1e-01 1.7e-01 6.1e+00 9.98e-01 -2.763122075e+01 2.143698841e+02 5.0e-05 0.26
16 8.2e-02 1.3e-01 4.7e+00 1.02e+00 2.135848180e+01 2.045405480e+02 3.8e-05 0.27
17 4.1e-02 8.3e-02 2.4e+00 1.02e+00 9.501475880e+01 1.868885776e+02 1.9e-05 0.29
18 1.4e-02 8.3e-02 8.2e-01 1.02e+00 1.425019024e+02 1.741744387e+02 6.6e-06 0.30
19 6.2e-03 7.2e-02 3.6e-01 1.01e+00 1.557125030e+02 1.695765297e+02 2.9e-06 0.31
20 1.5e-03 1.6e-01 9.2e-02 1.01e+00 1.638758801e+02 1.673863259e+02 7.4e-07 0.33
21 8.0e-04 1.1e-01 4.9e-02 9.78e-01 1.650620557e+02 1.669373602e+02 4.0e-07 0.34
22 2.4e-04 1.1e-01 1.6e-02 9.90e-01 1.660031289e+02 1.665978524e+02 1.3e-07 0.35
23 1.1e-04 8.9e-02 7.5e-03 1.01e+00 1.662212758e+02 1.665057616e+02 6.3e-08 0.37
24 4.7e-05 8.5e-02 3.1e-03 1.01e+00 1.663394239e+02 1.664571338e+02 2.6e-08 0.38
25 2.2e-05 7.7e-02 1.5e-03 1.01e+00 1.663835790e+02 1.664385513e+02 1.2e-08 0.40
26 2.0e-05 7.1e-02 1.3e-03 1.00e+00 1.663881973e+02 1.664377015e+02 1.1e-08 0.41
27 1.8e-05 6.4e-02 1.2e-03 1.01e+00 1.663915598e+02 1.664361006e+02 1.0e-08 0.43
28 1.6e-05 5.9e-02 1.1e-03 1.00e+00 1.663946472e+02 1.664347271e+02 9.0e-09 0.44
29 1.4e-05 5.4e-02 9.6e-04 1.00e+00 1.663974102e+02 1.664334758e+02 8.1e-09 0.45
30 1.3e-05 4.9e-02 8.6e-04 1.00e+00 1.663998948e+02 1.664323489e+02 7.3e-09 0.47
31 1.2e-05 4.5e-02 7.7e-04 1.00e+00 1.664021273e+02 1.664313320e+02 6.5e-09 0.48
32 1.0e-05 4.1e-02 7.0e-04 1.00e+00 1.664041338e+02 1.664304146e+02 5.9e-09 0.49
33 9.4e-06 3.8e-02 6.3e-04 1.00e+00 1.664059371e+02 1.664295872e+02 5.3e-09 0.50
34 8.5e-06 3.5e-02 5.6e-04 1.00e+00 1.664075581e+02 1.664288411e+02 4.8e-09 0.52
35 7.7e-06 3.2e-02 5.1e-04 1.00e+00 1.664090153e+02 1.664281682e+02 4.3e-09 0.53
36 6.9e-06 3.0e-02 4.6e-04 1.00e+00 1.664103253e+02 1.664275615e+02 3.9e-09 0.54
37 6.2e-06 2.8e-02 4.1e-04 1.00e+00 1.664115031e+02 1.664270145e+02 3.5e-09 0.56
38 5.6e-06 2.6e-02 3.7e-04 1.00e+00 1.664125621e+02 1.664265215e+02 3.1e-09 0.57
39 5.0e-06 2.4e-02 3.3e-04 1.00e+00 1.664135144e+02 1.664260771e+02 2.8e-09 0.58
40 4.5e-06 2.2e-02 3.0e-04 1.00e+00 1.664143706e+02 1.664256765e+02 2.5e-09 0.60
41 4.1e-06 2.1e-02 2.7e-04 1.00e+00 1.664151406e+02 1.664253155e+02 2.3e-09 0.61
42 3.7e-06 2.0e-02 2.4e-04 1.00e+00 1.664158330e+02 1.664249900e+02 2.1e-09 0.62
43 3.3e-06 1.8e-02 2.2e-04 1.00e+00 1.664164557e+02 1.664246967e+02 1.8e-09 0.64
44 3.0e-06 1.7e-02 2.0e-04 1.00e+00 1.664170157e+02 1.664244324e+02 1.7e-09 0.66
45 2.7e-06 1.6e-02 1.8e-04 1.00e+00 1.664175193e+02 1.664241941e+02 1.5e-09 0.68
46 2.4e-06 1.5e-02 1.6e-04 1.00e+00 1.664179722e+02 1.664239795e+02 1.3e-09 0.69
47 2.2e-06 1.5e-02 1.4e-04 1.00e+00 1.664183797e+02 1.664237861e+02 1.2e-09 0.71
48 1.9e-06 1.4e-02 1.3e-04 1.00e+00 1.664187463e+02 1.664236119e+02 1.1e-09 0.72
49 1.8e-06 1.3e-02 1.2e-04 1.00e+00 1.664190761e+02 1.664234550e+02 9.8e-10 0.73
50 1.6e-06 1.3e-02 1.0e-04 1.00e+00 1.664193728e+02 1.664233138e+02 8.8e-10 0.75
51 1.4e-06 1.2e-02 9.4e-05 1.00e+00 1.664196397e+02 1.664231866e+02 8.0e-10 0.76
52 1.3e-06 1.2e-02 8.5e-05 1.00e+00 1.664198799e+02 1.664230721e+02 7.2e-10 0.78
53 1.1e-06 1.1e-02 7.6e-05 1.00e+00 1.664200959e+02 1.664229689e+02 6.4e-10 0.79
54 1.0e-06 1.1e-02 6.9e-05 1.00e+00 1.664202903e+02 1.664228759e+02 5.8e-10 0.80
55 9.3e-07 1.1e-02 6.2e-05 1.00e+00 1.664204652e+02 1.664227923e+02 5.2e-10 0.86
56 8.4e-07 1.0e-02 5.6e-05 1.00e+00 1.664206226e+02 1.664227169e+02 4.7e-10 0.87
57 7.5e-07 1.0e-02 5.0e-05 1.00e+00 1.664207642e+02 1.664226490e+02 4.2e-10 0.89
58 6.8e-07 9.9e-03 4.5e-05 1.00e+00 1.664208915e+02 1.664225879e+02 3.8e-10 0.90
59 6.1e-07 9.7e-03 4.1e-05 1.00e+00 1.664210061e+02 1.664225328e+02 3.4e-10 0.91
60 5.5e-07 9.5e-03 3.6e-05 1.00e+00 1.664211092e+02 1.664224831e+02 3.1e-10 0.93
61 4.9e-07 9.3e-03 3.3e-05 1.00e+00 1.664212019e+02 1.664224384e+02 2.8e-10 0.94
62 4.4e-07 9.1e-03 3.0e-05 1.00e+00 1.664212853e+02 1.664223981e+02 2.5e-10 0.95
63 4.0e-07 9.0e-03 2.7e-05 9.99e-01 1.664213603e+02 1.664223619e+02 2.2e-10 0.98
64 3.6e-07 8.8e-03 2.4e-05 9.99e-01 1.664214278e+02 1.664223292e+02 2.0e-10 1.03
65 3.2e-07 8.7e-03 2.2e-05 1.00e+00 1.664214885e+02 1.664222998e+02 1.8e-10 1.05
66 2.9e-07 8.6e-03 1.9e-05 9.99e-01 1.664215431e+02 1.664222733e+02 1.6e-10 1.06
67 2.6e-07 8.5e-03 1.7e-05 9.99e-01 1.664215922e+02 1.664222495e+02 1.5e-10 1.08
68 2.4e-07 8.4e-03 1.6e-05 1.00e+00 1.664216365e+02 1.664222280e+02 1.3e-10 1.09
69 2.1e-07 8.3e-03 1.4e-05 9.99e-01 1.664216763e+02 1.664222086e+02 1.2e-10 1.12
70 1.9e-07 8.3e-03 1.3e-05 1.00e+00 1.664217121e+02 1.664221912e+02 1.1e-10 1.14
71 1.7e-07 8.2e-03 1.1e-05 1.00e+00 1.664217443e+02 1.664221755e+02 9.7e-11 1.16
72 1.6e-07 8.1e-03 1.0e-05 9.99e-01 1.664217733e+02 1.664221614e+02 8.7e-11 1.17
73 1.4e-07 8.1e-03 9.3e-06 1.00e+00 1.664217995e+02 1.664221485e+02 7.8e-11 1.18
74 1.3e-07 8.0e-03 8.3e-06 1.00e+00 1.664218230e+02 1.664221371e+02 7.1e-11 1.22
75 1.1e-07 8.0e-03 7.5e-06 9.98e-01 1.664218441e+02 1.664221268e+02 6.4e-11 1.24
76 1.0e-07 8.0e-03 6.8e-06 1.01e+00 1.664218634e+02 1.664221174e+02 5.7e-11 1.26
77 9.2e-08 7.9e-03 6.1e-06 9.93e-01 1.664218804e+02 1.664221091e+02 5.2e-11 1.28
78 8.2e-08 7.9e-03 5.5e-06 9.92e-01 1.664218958e+02 1.664221017e+02 4.6e-11 1.30
79 7.4e-08 7.1e-03 4.9e-06 1.01e+00 1.664219100e+02 1.664220947e+02 4.2e-11 1.31
80 6.7e-08 6.4e-03 4.4e-06 1.00e+00 1.664219225e+02 1.664220886e+02 3.8e-11 1.35
81 6.0e-08 5.7e-03 4.0e-06 9.95e-01 1.664219336e+02 1.664220831e+02 3.4e-11 1.37
82 5.4e-08 5.2e-03 3.6e-06 9.95e-01 1.664219437e+02 1.664220783e+02 3.1e-11 1.39
83 4.9e-08 4.6e-03 3.2e-06 9.97e-01 1.664219527e+02 1.664220739e+02 2.7e-11 1.40
84 4.4e-08 4.2e-03 2.9e-06 1.00e+00 1.664219609e+02 1.664220699e+02 2.5e-11 1.42
85 3.9e-08 3.8e-03 2.6e-06 1.02e+00 1.664219688e+02 1.664220659e+02 2.2e-11 1.43
86 3.6e-08 3.4e-03 2.4e-06 9.94e-01 1.664219753e+02 1.664220628e+02 2.0e-11 1.44
87 3.2e-08 3.0e-03 2.1e-06 1.02e+00 1.664219817e+02 1.664220596e+02 1.8e-11 1.46
88 2.9e-08 2.7e-03 1.9e-06 9.86e-01 1.664219869e+02 1.664220571e+02 1.7e-11 1.48
89 2.6e-08 2.5e-03 1.7e-06 1.00e+00 1.664219917e+02 1.664220547e+02 1.5e-11 1.49
90 2.3e-08 2.2e-03 1.5e-06 1.02e+00 1.664219962e+02 1.664220525e+02 1.3e-11 1.50
91 2.1e-08 2.0e-03 1.4e-06 1.03e+00 1.664220005e+02 1.664220504e+02 1.2e-11 1.52
92 1.9e-08 1.8e-03 1.3e-06 1.01e+00 1.664220040e+02 1.664220486e+02 1.1e-11 1.55
93 1.7e-08 1.6e-03 1.1e-06 1.00e+00 1.664220071e+02 1.664220471e+02 1.0e-11 1.58
94 1.5e-08 1.5e-03 1.0e-06 9.96e-01 1.664220098e+02 1.664220458e+02 9.0e-12 1.60
95 1.4e-08 1.3e-03 9.1e-07 9.92e-01 1.664220122e+02 1.664220447e+02 8.1e-12 1.61
96 1.2e-08 1.2e-03 8.2e-07 9.80e-01 1.664220144e+02 1.664220436e+02 7.3e-12 1.63
97 1.1e-08 1.1e-03 7.4e-07 9.55e-01 1.664220163e+02 1.664220427e+02 6.6e-12 1.64
98 1.0e-08 9.6e-04 6.7e-07 9.59e-01 1.664220181e+02 1.664220419e+02 5.9e-12 1.69
99 9.2e-09 8.6e-04 6.0e-07 9.55e-01 1.664220197e+02 1.664220412e+02 5.3e-12 1.70
100 8.3e-09 7.7e-04 5.4e-07 1.06e+00 1.664220215e+02 1.664220402e+02 4.9e-12 1.75
101 7.5e-09 7.0e-04 4.9e-07 9.30e-01 1.664220227e+02 1.664220396e+02 4.5e-12 1.77
102 6.7e-09 6.3e-04 4.4e-07 9.15e-01 1.664220239e+02 1.664220391e+02 4.0e-12 1.78
103 6.1e-09 5.6e-04 3.9e-07 1.10e+00 1.664220253e+02 1.664220383e+02 3.8e-12 1.80
104 5.5e-09 5.1e-04 3.5e-07 1.16e+00 1.664220269e+02 1.664220375e+02 3.7e-12 1.81
105 2.8e-09 3.3e-05 2.3e-08 8.31e-01 1.664220339e+02 1.664220347e+02 4.9e-13 1.83
Interior-point optimizer terminated. Time: 1.83.
Optimizer terminated. Time: 1.84
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6642203391e+02 Viol. con: 6e-08 var: 0e+00
Dual. obj: 1.6642203466e+02 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.86 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 926
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3439 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.03 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.64e+04 after factor : 1.46e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.285332508e+05 2.000000000e+00 1.0e+00 0.05
1 1.1e+03 1.4e+03 6.1e+04 -9.71e-01 -1.263506603e+05 3.573405890e+00 4.8e-01 0.08
2 4.3e+02 5.5e+02 2.4e+04 -9.36e-01 -1.201229629e+05 1.024109129e+01 1.8e-01 0.16
3 2.9e+02 3.7e+02 1.6e+04 -8.38e-01 -1.154146796e+05 6.438967965e+01 1.2e-01 0.17
4 2.8e+02 3.6e+02 1.6e+04 -7.58e-01 -1.128141998e+05 2.256492616e+03 1.2e-01 0.18
5 7.5e+01 9.6e+01 4.1e+03 -7.51e-01 -7.452159547e+04 9.623289244e+03 3.3e-02 0.23
6 3.0e+01 3.8e+01 1.7e+03 -1.92e-01 -4.039642979e+04 1.017306930e+04 1.3e-02 0.27
7 1.8e+01 2.3e+01 1.0e+03 3.96e-01 -2.710383498e+04 6.644076882e+03 7.9e-03 0.28
8 9.5e+00 1.2e+01 5.2e+02 6.30e-01 -1.529784967e+04 3.811651876e+03 4.1e-03 0.30
9 3.3e+00 4.2e+00 1.8e+02 8.18e-01 -5.370881759e+03 1.685460993e+03 1.5e-03 0.31
10 1.6e+00 2.1e+00 9.1e+01 9.54e-01 -2.488163715e+03 1.068021330e+03 7.3e-04 0.33
11 9.3e-01 1.2e+00 5.2e+01 9.86e-01 -1.337520843e+03 6.866519894e+02 4.1e-04 0.34
12 8.5e-01 1.1e+00 4.8e+01 9.60e-01 -1.253928796e+03 6.354852531e+02 3.8e-04 0.36
13 4.7e-01 6.1e-01 2.7e+01 9.77e-01 -6.373643163e+02 4.197161706e+02 2.1e-04 0.38
14 2.5e-01 3.3e-01 1.4e+01 1.00e+00 -2.541512711e+02 3.021241906e+02 1.1e-04 0.39
15 9.3e-02 1.5e-01 5.3e+00 1.00e+00 -3.966326849e+00 2.060664469e+02 4.3e-05 0.40
16 8.6e-02 1.3e-01 4.9e+00 1.02e+00 1.475304501e+01 2.084814275e+02 4.0e-05 0.41
17 6.0e-02 9.6e-02 3.4e+00 1.02e+00 6.117888995e+01 1.950767378e+02 2.8e-05 0.43
18 3.3e-02 7.2e-02 1.9e+00 1.02e+00 1.091859306e+02 1.824025378e+02 1.5e-05 0.44
19 9.2e-03 1.8e-01 5.3e-01 1.02e+00 1.513704968e+02 1.718413722e+02 4.3e-06 0.45
20 3.6e-03 2.1e-01 2.1e-01 1.01e+00 1.602182009e+02 1.683900226e+02 1.7e-06 0.46
21 1.3e-03 1.3e-01 7.6e-02 1.01e+00 1.642699975e+02 1.671903191e+02 6.2e-07 0.48
22 8.6e-04 1.0e-01 5.2e-02 9.84e-01 1.649681567e+02 1.669444025e+02 4.3e-07 0.56
23 2.6e-04 1.1e-01 1.6e-02 9.86e-01 1.659690902e+02 1.665864865e+02 1.3e-07 0.57
24 9.4e-05 1.0e-01 6.1e-03 1.01e+00 1.662459023e+02 1.664756911e+02 5.1e-08 0.59
25 3.7e-05 9.5e-02 2.4e-03 1.01e+00 1.663440798e+02 1.664350964e+02 2.0e-08 0.60
26 1.7e-05 8.1e-02 1.1e-03 1.00e+00 1.663785042e+02 1.664206580e+02 9.5e-09 0.61
27 1.5e-05 7.4e-02 1.0e-03 1.00e+00 1.663820223e+02 1.664199767e+02 8.5e-09 0.71
28 1.4e-05 6.7e-02 9.0e-04 1.01e+00 1.663846091e+02 1.664187607e+02 7.7e-09 0.72
29 1.2e-05 6.1e-02 8.1e-04 1.00e+00 1.663869810e+02 1.664177120e+02 6.9e-09 0.74
30 1.1e-05 5.6e-02 7.3e-04 1.00e+00 1.663891056e+02 1.664167591e+02 6.2e-09 0.78
31 1.0e-05 5.1e-02 6.6e-04 1.00e+00 1.663910162e+02 1.664159007e+02 5.6e-09 0.86
32 9.1e-06 4.7e-02 5.9e-04 1.00e+00 1.663927335e+02 1.664151266e+02 5.0e-09 0.97
33 8.1e-06 4.3e-02 5.3e-04 1.00e+00 1.663942773e+02 1.664144287e+02 4.5e-09 1.07
34 7.3e-06 3.9e-02 4.8e-04 1.00e+00 1.663956653e+02 1.664137995e+02 4.1e-09 1.08
35 6.6e-06 3.6e-02 4.3e-04 1.00e+00 1.663969132e+02 1.664132324e+02 3.7e-09 1.17
36 5.9e-06 3.3e-02 3.9e-04 1.00e+00 1.663980353e+02 1.664127212e+02 3.3e-09 1.19
37 5.3e-06 3.1e-02 3.5e-04 1.00e+00 1.663990443e+02 1.664122606e+02 3.0e-09 1.20
38 4.8e-06 2.9e-02 3.2e-04 1.00e+00 1.663999516e+02 1.664118455e+02 2.7e-09 1.21
39 4.3e-06 2.6e-02 2.8e-04 1.00e+00 1.664007676e+02 1.664114714e+02 2.4e-09 1.24
40 3.9e-06 2.5e-02 2.6e-04 1.00e+00 1.664015014e+02 1.664111343e+02 2.2e-09 1.26
41 3.5e-06 2.3e-02 2.3e-04 1.00e+00 1.664021613e+02 1.664108304e+02 2.0e-09 1.27
42 3.2e-06 2.1e-02 2.1e-04 1.00e+00 1.664027548e+02 1.664105566e+02 1.8e-09 1.29
43 2.8e-06 2.0e-02 1.9e-04 1.00e+00 1.664032885e+02 1.664103100e+02 1.6e-09 1.75
44 2.6e-06 1.9e-02 1.7e-04 1.00e+00 1.664037686e+02 1.664100877e+02 1.4e-09 1.89
45 2.3e-06 1.8e-02 1.5e-04 1.00e+00 1.664042005e+02 1.664098874e+02 1.3e-09 1.91
46 2.1e-06 1.7e-02 1.4e-04 1.00e+00 1.664045890e+02 1.664097071e+02 1.2e-09 1.93
47 1.9e-06 1.6e-02 1.2e-04 1.00e+00 1.664049385e+02 1.664095447e+02 1.0e-09 1.97
48 1.7e-06 1.5e-02 1.1e-04 1.00e+00 1.664052529e+02 1.664093984e+02 9.4e-10 1.98
49 1.5e-06 1.4e-02 9.9e-05 1.00e+00 1.664055358e+02 1.664092668e+02 8.4e-10 2.02
50 1.4e-06 1.4e-02 8.9e-05 1.00e+00 1.664057904e+02 1.664091482e+02 7.6e-10 2.04
51 1.2e-06 1.3e-02 8.0e-05 1.00e+00 1.664060194e+02 1.664090414e+02 6.8e-10 2.08
52 1.1e-06 1.2e-02 7.2e-05 1.00e+00 1.664062254e+02 1.664089452e+02 6.1e-10 2.14
53 9.9e-07 1.2e-02 6.5e-05 1.00e+00 1.664064108e+02 1.664088586e+02 5.5e-10 2.23
54 8.9e-07 1.2e-02 5.9e-05 1.00e+00 1.664065776e+02 1.664087805e+02 5.0e-10 2.28
55 8.0e-07 1.1e-02 5.3e-05 1.00e+00 1.664067277e+02 1.664087103e+02 4.5e-10 2.30
56 7.2e-07 1.1e-02 4.7e-05 1.00e+00 1.664068627e+02 1.664086471e+02 4.0e-10 2.31
57 6.5e-07 1.0e-02 4.3e-05 1.00e+00 1.664069841e+02 1.664085901e+02 3.6e-10 2.37
58 5.8e-07 1.0e-02 3.8e-05 1.00e+00 1.664070934e+02 1.664085387e+02 3.3e-10 2.38
59 5.3e-07 9.9e-03 3.5e-05 1.00e+00 1.664071917e+02 1.664084925e+02 2.9e-10 2.79
60 4.7e-07 9.7e-03 3.1e-05 1.00e+00 1.664072801e+02 1.664084508e+02 2.6e-10 2.81
61 4.3e-07 9.5e-03 2.8e-05 1.00e+00 1.664073596e+02 1.664084132e+02 2.4e-10 2.89
62 3.8e-07 9.3e-03 2.5e-05 1.00e+00 1.664074312e+02 1.664083794e+02 2.1e-10 2.90
63 3.5e-07 9.1e-03 2.3e-05 9.99e-01 1.664074955e+02 1.664083489e+02 1.9e-10 2.92
64 3.1e-07 9.0e-03 2.0e-05 1.00e+00 1.664075534e+02 1.664083215e+02 1.7e-10 3.01
65 2.8e-07 8.8e-03 1.8e-05 9.98e-01 1.664076055e+02 1.664082968e+02 1.6e-10 3.03
66 2.5e-07 8.7e-03 1.7e-05 1.00e+00 1.664076523e+02 1.664082745e+02 1.4e-10 3.04
67 2.3e-07 8.6e-03 1.5e-05 1.00e+00 1.664076945e+02 1.664082544e+02 1.3e-10 3.20
68 2.0e-07 8.5e-03 1.3e-05 1.00e+00 1.664077324e+02 1.664082364e+02 1.1e-10 3.25
69 1.8e-07 8.4e-03 1.2e-05 1.00e+00 1.664077666e+02 1.664082201e+02 1.0e-10 3.43
70 1.7e-07 8.3e-03 1.1e-05 1.01e+00 1.664077977e+02 1.664082052e+02 9.2e-11 3.50
71 1.5e-07 8.3e-03 9.8e-06 1.00e+00 1.664078255e+02 1.664081919e+02 8.3e-11 3.53
72 1.3e-07 8.2e-03 8.8e-06 1.01e+00 1.664078506e+02 1.664081798e+02 7.5e-11 3.72
73 1.2e-07 8.2e-03 7.9e-06 1.00e+00 1.664078729e+02 1.664081692e+02 6.7e-11 3.92
74 1.1e-07 8.1e-03 7.1e-06 9.98e-01 1.664078930e+02 1.664081597e+02 6.1e-11 4.24
75 9.8e-08 8.0e-03 6.4e-06 9.94e-01 1.664079110e+02 1.664081511e+02 5.5e-11 4.56
76 8.8e-08 8.0e-03 5.8e-06 9.99e-01 1.664079273e+02 1.664081434e+02 4.9e-11 4.73
77 7.9e-08 8.0e-03 5.2e-06 1.00e+00 1.664079420e+02 1.664081363e+02 4.4e-11 4.75
78 7.1e-08 7.9e-03 4.7e-06 1.00e+00 1.664079552e+02 1.664081300e+02 4.0e-11 4.76
79 6.4e-08 7.9e-03 4.2e-06 9.93e-01 1.664079670e+02 1.664081244e+02 3.6e-11 4.77
80 5.8e-08 7.9e-03 3.8e-06 1.00e+00 1.664079778e+02 1.664081193e+02 3.2e-11 4.78
81 5.2e-08 7.1e-03 3.4e-06 1.01e+00 1.664079875e+02 1.664081146e+02 2.9e-11 4.80
82 4.7e-08 6.4e-03 3.1e-06 1.00e+00 1.664079961e+02 1.664081105e+02 2.6e-11 4.81
83 4.2e-08 5.7e-03 2.8e-06 1.01e+00 1.664080043e+02 1.664081065e+02 2.4e-11 4.82
84 3.8e-08 5.2e-03 2.5e-06 1.01e+00 1.664080114e+02 1.664081031e+02 2.1e-11 4.83
85 3.4e-08 4.6e-03 2.2e-06 9.95e-01 1.664080176e+02 1.664081002e+02 1.9e-11 4.85
86 3.1e-08 4.2e-03 2.0e-06 1.01e+00 1.664080233e+02 1.664080974e+02 1.7e-11 4.86
87 2.8e-08 3.8e-03 1.8e-06 9.96e-01 1.664080283e+02 1.664080951e+02 1.6e-11 4.87
88 2.5e-08 3.4e-03 1.6e-06 9.84e-01 1.664080328e+02 1.664080929e+02 1.4e-11 4.89
89 2.2e-08 3.0e-03 1.5e-06 9.92e-01 1.664080369e+02 1.664080910e+02 1.3e-11 4.90
90 2.0e-08 2.7e-03 1.3e-06 9.81e-01 1.664080405e+02 1.664080893e+02 1.1e-11 4.91
91 1.8e-08 2.5e-03 1.2e-06 1.04e+00 1.664080444e+02 1.664080874e+02 1.0e-11 5.01
92 1.6e-08 2.2e-03 1.1e-06 9.20e-01 1.664080473e+02 1.664080861e+02 9.4e-12 5.02
93 1.5e-08 2.0e-03 9.6e-07 9.87e-01 1.664080499e+02 1.664080848e+02 8.5e-12 5.15
94 1.3e-08 1.8e-03 8.7e-07 9.59e-01 1.664080522e+02 1.664080838e+02 7.6e-12 5.22
95 1.2e-08 1.6e-03 7.8e-07 9.71e-01 1.664080543e+02 1.664080828e+02 6.9e-12 5.23
96 1.1e-08 1.5e-03 7.0e-07 9.83e-01 1.664080562e+02 1.664080818e+02 6.2e-12 5.24
97 9.7e-09 1.3e-03 6.3e-07 9.95e-01 1.664080580e+02 1.664080810e+02 5.6e-12 5.25
98 8.7e-09 1.2e-03 5.7e-07 1.08e+00 1.664080601e+02 1.664080799e+02 5.2e-12 5.26
99 7.8e-09 1.1e-03 5.1e-07 9.77e-01 1.664080614e+02 1.664080793e+02 4.7e-12 5.28
100 7.1e-09 9.5e-04 4.6e-07 8.48e-01 1.664080626e+02 1.664080788e+02 4.2e-12 5.29
101 6.4e-09 8.6e-04 4.1e-07 9.79e-01 1.664080637e+02 1.664080782e+02 3.8e-12 5.30
102 5.8e-09 7.7e-04 3.7e-07 1.21e+00 1.664080656e+02 1.664080771e+02 3.8e-12 5.31
103 5.3e-09 7.0e-04 3.4e-07 8.63e-01 1.664080664e+02 1.664080768e+02 3.4e-12 5.33
104 4.8e-09 6.3e-04 3.0e-07 1.03e+00 1.664080672e+02 1.664080764e+02 3.1e-12 5.34
105 4.5e-09 5.6e-04 2.7e-07 1.14e+00 1.664080682e+02 1.664080759e+02 3.0e-12 5.35
106 6.2e-09 6.7e-05 3.3e-08 7.54e-01 1.664080731e+02 1.664080742e+02 6.1e-13 5.54
Interior-point optimizer terminated. Time: 5.54.
Optimizer terminated. Time: 5.55
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6640807313e+02 Viol. con: 9e-08 var: 0e+00
Dual. obj: 1.6640807415e+02 Viol. con: 0e+00 var: 4e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 5.57 seconds.
Solving took 9 GP solves and 86.7 seconds.
Solves with these variables bounded:
value near lower bound: Mission.CruiseAlt
value near upper bound: Mission.Aircraft.HorizontalTail.WingBox.M_{r_{out}}, Mission.Aircraft.Engine.Thrust.\alpha_{max}, Mission.Aircraft.Wing.WingNoStruct.A_{tri}, Mission.TotalTime, Mission.Aircraft.LandingGear.d_{nacelle}, Mission.T_{t_{4.1_{max-Cruise}}}
Checking for relaxed constants...
Solution check warning: Primal solution computed cost did not match solver-returned cost: 1.495740870058179e+110 vs 1.49570172575e+110
GP iteration 0 has relaxed constants
Cost
----
1.496e+110
Free Variables
--------------
| Mission.Aircraft.Engine.Turbine.Relax
C_{p_{t2}} : 2.251 Cp Value for Combustion Products in LP Turbine
| Mission.Aircraft.Fuselage.Relax
l_{nose} : 1.042 Nose length
n_{pass} : [ 2.86 ] Number of passengers
| Mission.Aircraft.Relax
f_{L_{total/wing}} : 1.656 Total lift as a percentage of wing lift
| Mission.Aircraft.Wing.WingNoStruct.Relax
\tan(\Lambda) : 1.133 Tangent of quarter-chord sweep angle
| Mission.FlightState.Atmosphere.Relax
L_{atm} : [ 1.77 1 1 1 1 ] Temperature lapse rate
T_{sl} : [ 1 1 1.25 1 1 ] Temperature at sea level
| Mission.Relax
R_{req} : 2.362 Required Cruise Range
GP iteration 1 has relaxed constants
Cost
----
7.486e+74
Free Variables
--------------
| Mission.Aircraft.Engine.Combustor.Relax
hold_{4a} : 1.093 1+(gamma-1)/2 * M_4a**2
| Mission.Aircraft.Fuselage.Relax
n_{pass} : [ 1.03 ] Number of passengers
| Mission.Aircraft.LandingGear.Relax
h_{hold} : 1.006 Hold height
Solution check warning: Primal solution computed cost did not match solver-returned cost: 3.70539773406721e+72 vs 3.70524769429e+72
WEIGHT DIFFERENCES
Total Fuel Weight Percent Diff: [-92.94682341]
Total Aircraft Weight Percent Diff: [-21.48056538]
Engine Weight Percent Diff: -56.27822091678476
Fuselage Weight Percent Diff: -0.869725296853007
Payload Weight Percent Diff: [-0.04003557]
VT Weight Percent Diff: -8.6077263920923
HT Weight Percent Diff: -93.23325716227288
Wing Weight Percent Diff: 8.267439218976007
WING DIFFERENCES
Wing Span Percent Diff: -0.029994856793720385
Wing Area Percent Diff: 32.90010333250834
HORIZONTAL TAIL DIFFERENCES
HT Area Percent Diff: 40.48930585994106
VERTICAL TAIL DIFFERENCES
VT Span Percent Diff: -11.022337366369138
VT Area Percent Diff: -60.38683290529611
CRUISE SEGMENT 1 DRAG DIFFERENCES
Overall Cd Percent Diff: [-18.54730647]
L/D Percent Diff: [24.0102099]
Nacelle Cd Percent Diff: [-94.27641573]
HT Cd Percent Diff: [-80.76936701] dimensionless
Fuselage Cd Percent Diff: [108.78752887]
VT Cd Percent Diff: [-58.00304197] dimensionless
Wing Cd percent Diff: [-14.2292792]
Induced Drag Cd Percent Diff: [1.2194058]
CRUISE SEGMENT 1 TSFC DIFFERENCES
Initial Cruise TSFC Percent Diff: [-90.57035978]
FUSELAGE DIFFERENCES
Weight of HB material: -38.36021065314171
Weight of VB material: 87.82227997816754
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.71260519]
Mission1
========
Cost
----
W_{f_{total}}[:].sum()
Constraints
-----------
W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin}
PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:])
x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:])
x_{CG}[3] <= \Delta x_n + x_n
\Delta x_m + x_{CG}[3] >= x_m
\tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m
C_{D_{fuse}}[:] = 0.018081
M_{fuseD} = 0.72
W_{start}[0] = W_{total}[:]
W_{start}[:] >= W_{end}[:] + W_{burn}[:]
W_{start}[1:] = W_{end}[:4]
W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1]
W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2]
W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1]
hft[2] >= CruiseAlt
hft[1:5] = hft[:4] + dhft[1:5]
hft[0] = dhft[0]
dhft[1:3] = dhft[:2]
RC[0] >= 2.5e+03
RC[:3] >= RC_{min}[:3]
\theta[2] >= 0.015
hft[2] >= MinCruiseAlt
n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:]
R_{segment}[3:4] = R_{segment}[4:5]
M[3:5] >= M_{min}
0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req}
Fsafetyfac*F[0] = T_e
W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:]
V_2[:] = M_2[:]*a[:]
\alpha_{max,w}[:3] = 0.18
\alpha_{max,w}[3:] = 0.1
0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime
0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime
ClimbTime <= MaxClimbTime
T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}}
F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
F_{fuel}[:] <= 1.0000001
OPR[:] <= OPR_{max}
Aircraft
Fuselage
W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on}
W_{pass}[:] >= n_{pass}[:]*W_{avg. pass}
W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo}
W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}}
W_{payload}[:] <= W_{payload_{max}}
n_{pass}[:] <= n_{seat}
n_{rows} = n_{seat}/SPR
l_{shell} = n_{rows}*p_s
\theta_{db} = w_{db}/R_{fuse}
R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db}
A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db}
(PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse}
A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin}
w_{floor} = w_{fuse}
R_{fuse} + w_{db} >= w_{fuse}
h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse}
t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell}
S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2
S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2
l_{fuse} = l_{nose} + l_{shell} + l_{cone}
l_{cone} = R_{fuse}/\lambda_{cone}
x_{shell1} = l_{nose}
x_{shell2} >= l_{nose} + l_{shell}
t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin}
t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin}
\sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell})
\sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin}
l_{floor} >= l_{shell} + 2*R_{fuse}
P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat})
A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor}
V_{floor} = 2*w_{floor}*A_{floor}
W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor}
\tau_{cone} = \sigma_{skin}
W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame})
x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone}
-2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}}
(PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}}
x_{hbend_{Land}} >= x_{wing}
x_{hbend_{Land}} <= l_{fuse}
x_{hbend_{MLF}} >= x_{wing}
x_{hbend_{MLF}} <= l_{fuse}
A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}})
A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}})
A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
A_{2h_{MLF}} >= Mission1.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2)
A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}}
A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}}
A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}}
A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}}
A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}}
A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}}
A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}}
A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}}
V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}}
W_{hbend} >= g*\rho_{bend}*V_{hbend}
x_{vbend} >= x_{wing}
x_{vbend} <= l_{fuse}
B_{0v} = B_{1v}*(x_{tail} - x_{vbend})
B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2)
B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}}
0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}}
V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}}
W_{vbend} >= \rho_{bend}*g*V_{vbend}
x_f = x_{wing} + 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
x_b = x_{wing} - 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
\sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h}
\sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v}
V_{cyl} = A_{skin}*l_{shell}
V_{nose} = S_{nose}*t_{skin}
V_{bulk} = S_{bulk}*t_{skin}
V_{db} = A_{db}*l_{shell}
V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse})
W_{apu} = W_{payload_{max}}*f_{apu}
W_{db} = \rho_{skin}*g*V_{db}
W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk})
W_{window} >= W'_{window}*l_{shell}
W_{padd} = W_{payload_{max}}*f_{padd}
W_{seat} >= W'_{seat}*n_{seat}
W_{seat} >= f_{seat}*W_{payload_{max}}
W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk})
W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db}
W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone})
Wing
WingNoStruct
A_{rect} = c_{tip}*b
0.5*(1 - \lambda)*c_{root}*b <= A_{tri}
p >= 1 + 2*\lambda
2*q >= 1 + p
y_{mac} = b/3*q/p
mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q
\lambda = c_{tip}/c_{root}
S = b*(c_{root} + c_{tip})/2
0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w)
e*(1 + f(\lambda_w)*AR) <= 1
\lambda >= 0.15
V_{fuel, max} <= 0.303*mac^2*b*\tau
W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g
b <= b_{max}
WingBox
AR = b^2/S
0.423*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5)
\tau <= \tau_{max_w}
W_{struct} >= W_{web} + W_{cap}
AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5)
Mission1.Aircraft.Wing.WingBox.N_{lift} = 3
Mission1.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8
\lambda = taper
W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt})
0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}}
Engine
Compressor
(no constraints)
Combustor
(no constraints)
Turbine
(no constraints)
Thrust
(no constraints)
FanMap
(no constraints)
LPCMap
(no constraints)
HPCMap
(no constraints)
Sizing
A_{2} >= A_{5} + A_{7}
FlightState
V[:] = V[:]
a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
V[:] = M[:]*a[:]
Altitude
h[:] = hft[:]
Atmosphere
(P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
\rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
\mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
EnginePerformance
CompressorPerformance
T_{t_0}[:] = T_{atm}[:]/c1[:]^-1
h_{t_0}[:] = C_{p_{air}*T_{t_0}[:]
P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:]
T_{t_{1.8}}[:] = T_{t_0}[:]
h_{t_{1.8}}[:] = h_{t_0}[:]
P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5
T_{T_{2}}[:] = T_{t_{1.8}}[:]
h_{T_{2}}[:] = h_{t_{1.8}}[:]
P_{T_{2}}[:] = P_{t_{1.8}}[:]
P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:]
T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016
h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:]
P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:]
T_{t_7}[:] = T_{t_{2.1}}[:]
h_{t_7}[:] = h_{t_{2.1}}[:]
P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:]
T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152
h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1}
P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:]
T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491
h_{t_3}[:] = C_{p_{2}*T_{t_3}[:]
CombustorPerformance
h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:]
h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:]
fp1[:] = f[:] + 1
M_{4a}[:] = 0.1025
fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5
T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]]
P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891
u_{4a}[:] = M_{4a}[:]*(1.31*Mission1.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a}
u_c[:] = r_{uc}*u_{4a}[:]
P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891
TurbinePerformance
h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:]
P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:]
\pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565
h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:]
P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:]
T_{t_5}[:] = T_{t_{4.9}}[:]
h_{t_5}[:] = h_{t_{4.9}}[:]
ThrustPerformance
P_{8}[:] = P_{atm}[:]
h_{8}[:] = C_{p_{fex}*T_{8}[:]
u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:]
(P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:]
h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:]
P_{6}[:] = P_{atm}[:]
(P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:]
u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:]
h_6[:] = C_{p_{tex}*T_{6}[:]
h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:]
\alpha[:] = m_{fan}[:]/m_{core}[:]
\alpha_{+1}[:] = \alpha[:] + 1
\alpha[:] <= \alpha_{max}
F[:] <= F_{6}[:] + F_{8}[:]
F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:])
TSFC[:] = 1/I_{sp}[:]
F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:]
FanMapPerformance
m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}}
LPCMapPerformance
m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D}
HPCMapPerformance
m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D}
SizingPerformance
P_{7}[:] >= P_{atm}[:]
M_7[:] <= 1
a_{7}[:] = (1.4*Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5
a_{7}[:]*M_7[:] = u_{7}[:]
\rho_7[:] = P_{7}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])
P_{5}[:] >= P_{atm}[:]
M_5[:] <= 1
a_{5}[:] = (1.39*Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5
a_{5}[:]*M_5[:] = u_{5}[:]
\rho_5[:] = P_{5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])
h_{2}[:] = C_{p_{1}*T_{2}[:]
\rho_{2}[:] = P_{2}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:])
u_{2}[:] = M_2[:]*(C_{p_{1}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:]/781)^0.5
h_{2.5}[:] = C_{p_{2}*T_{2.5}[:]
\rho_{2.5}[:] = P_{2.5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:])
u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/781)^0.5
m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine}
d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5
d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5
\eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]])
h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:]
P_{t_4}[:] = \pi_{b}*P_{t_3}[:]
M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]]
M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]])
P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:]
\pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013
\pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10
\pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10
\pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10
m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
\pi_{f}[:] >= 1
\pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10
\pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10
\pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10
\pi_{lc}[:] >= 1
m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
\pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10
\pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10
\pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10
m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref})
\pi_{hc}[:] >= 1
OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:]
P_{t_8}[:] = P_{t_7}[:]
T_{t_8}[:] = T_{t_7}[:]
P_{t_6}[:] = P_{t_5}[:]
T_{t_6}[:] = T_{t_5}[:]
F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:]
I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g)
N_{f}[:]*G_{f} = N_{1}[:]
N_{1}[:] <= 1.1
N_{2}[:] <= 1.1
fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD}
fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD}
P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5
(T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2
P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979
(T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2
M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:]
m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:]
m_{total}[:] = m_{fan}[:] + m_{core}[:]
P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512
T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1
m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2}
P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857
T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1
m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5}
1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD}
0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD}
1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD}
0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD}
m_{lc_D} >= 0.7*m_{coreD}/0.649
m_{lc_D} <= 1.3*m_{coreD}/0.649
m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23
m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23
\bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405
\bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405
F[:] = F_{spec}[:]
T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}}
OPR[:] <= OPR_{max}
VerticalTail
VerticalTailNoStruct
C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}}
L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}}
c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt}))
A_{vt} = b_{vt}^2/S_{vt}
b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt}
p_{vt} >= 1 + 2*\lambda_{vt}
2*q_{vt} >= 1 + p_{vt}
y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt}
\lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}}
\Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}}
\Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt}
\lambda_{vt} >= 0.25
V_{vt} >= V_{vt_{min}}
WingBox
AR_{vt} = (2*b_{vt})^2/(2*S_{vt})
0.423*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
\tau_{vt} <= 0.14
W_{struct} >= 0.5*(W_{web} + W_{cap})
Mission1.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24
AR_{vt}*2*L_{vt_{max}}*Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
Mission1.Aircraft.VerticalTail.WingBox.N_{lift} = 1
Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*Mission1.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8
\lambda_{vt} = taper
W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT})
HorizontalTail
HorizontalTailNoStruct
\Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht}
\Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}}
p_{ht} >= 1 + 2*\lambda_{ht}
2*q_{ht} >= 1 + p_{ht}
y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht}
0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht}
\lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}}
S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2
0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht})
e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1
AR_{ht} = b_{ht}^2/S_{ht}
\lambda_{ht} >= 0.2
\lambda_{ht} <= 1
WingBox
AR_{ht} = b_{ht}^2/S_{ht}
0.423*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap}
\nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56
W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
\tau_{ht} <= 0.14
W_{struct} >= W_{web} + W_{cap}
L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2
L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht})
2*AR_{ht}*L_{shear}*Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12
W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
Mission1.Aircraft.HorizontalTail.WingBox.N_{lift} = 1
Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission1.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8
L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht}
L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}}
W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht})
LandingGear
l_n + z_{wing} + y_m*\tan(\gamma) >= l_m
T = 2*y_m
x_m >= x_n + B
x_n >= 5
\tan(\phi) = \tan(\phi_{min})
(z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1
\tan(\psi) <= \tan(\psi_{max})
x_{up} - x_m <= l_m/\tan(\theta_{max})
y_m >= l_m
S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG})
l_{oleo} = 2.5*S_{sa}
d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5
l_m >= l_{oleo} + d_{t_m}/2
F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in])
W_{wa,m} = 1.2*F_{w_m}^0.609
F_{w_n} = L_{w_n}*d_{t_n}/1e+03
W_{wa,n} = 1.2*F_{w_n}^0.609
L_{w_m} = L_m/(n_{mg}*n_{wps})
L_{w_n} = L_n/n_{wps}
d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315
w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48
d_{t_n} = 0.8*d_{t_m}
w_{t_n} = 0.8*w_{t_m}
W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g
N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m
W_{mw} = n_{wps}*W_{wa,m}
W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g
\sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}})
W_{nw} >= n_{wps}*W_{wa,n}
L_m <= 9.87*E*I_m/(K*l_m)^2
I_m = PI*r_m^3*t_m
L_n <= 9.87*E*I_n/(K*l_n)^2
I_n = PI*r_n^3*t_n
2*r_m/t_m <= 40
2*r_m/t_n <= 40
h_{hold} >= 2*w_{t_m} + 2*r_m
0.8 >= 2*w_{t_n} + 2*r_n
W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m}))
W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n})
W_{lg} >= C_{lg}*(W_{mg} + W_{ng})
W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m
x_m >= x_{CG_{lg}}
c_{root} = c_0
Mission1.Aircraft.Wing.WingBox.r_{w/c} = Mission1.Aircraft.Fuselage.r_{w/c}
x_w = x_{wing}
Mission1.Aircraft.Fuselage.N_{lift} = Mission1.Aircraft.Wing.WingBox.N_{lift}
f_{L_{total/wing}}*L_{max} >= Mission1.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}}
W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc}
W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:]
W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:]
W_{total}[:] <= W_{total, max}
f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}}
W_{misc} >= W_{lg} + W_{hpesys}
W_{hpesys} = f_{hpesys}*W_{total, max}
x_n <= l_{nose}
x_m >= x_{wing}
\Delta x_{AC_{wing}} + x_{wing} >= x_m
x_{hpesys} = 1.1*l_{nose}
x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys}
d_{nacelle} >= d_{f} + 2*t_{nacelle}
E_{land} >= W_{total, max}/(2*g)*w_{ult}^2
x_{up} = x_{shell2}
L_n = W_{total, max}*\Delta x_m/B
L_m = W_{total, max}*\Delta x_n/B
L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max}
y_{eng} >= y_m
3*n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}}
V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse}
W_{tail} >= n_{vt}*W_{vt} + W_{ht}
2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db}
B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v})
m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht}
x_{CG_{ht}} <= l_{fuse}
V_{ht} = S_{ht}*l_{ht}/(S*mac)
L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}}
L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}}
x_{CG_{vt}} <= l_{fuse}
V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b)
n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max}
n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng}
D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}}
I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:]
I_{z}[:] <= I_{z, max}
S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2
l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}}
f_{S_{nacelle}} = S_{nacelle}*S^-1
A_{inlet} = 0.4*S_{nacelle}
A_{fancowl} = 0.2*S_{nacelle}
A_{exh} = 0.4*S_{nacelle}
A_{corecowl} = 3PI*d_{LPC}^2
W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl})
W_{eadd} = f_{eadd}*W_{engine}
W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon}
W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine})
y_{eng} = 0.5*w_{fuse}
(L_{max} - Mission1.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission1.Aircraft.Wing.WingBox.M_r*c_{root}
A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend})
A_{1h_{MLF}} >= (Mission1.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h})
I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16)
I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81
I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81)
x_{shell2} + l_{cone} >= x_{eng}
x_{eng} >= x_{shell2} + 0.75*l_{cone}
S_{floor} = 0.312*P_{floor}
M_{floor} = 0.0352*P_{floor}*w_{floor}
\Delta R_{fuse} = R_{fuse}*0.43/1.75
b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2
b_{ht_{out}} = 0.5*b_{ht} - w_{fuse}
L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}}
M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}}
L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}}
c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach}
\pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht})
FlightSegment
FlightState
V[:] = V[:]
a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
V[:] = M[:]*a[:]
Altitude
h[:] = hft[:]
Atmosphere
(P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
\rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
\mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
FlightP
P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:]
RC[:] = P_{excess}[:]/W_{avg}[:]
\theta[:]*V[:] = RC[:]
dhft[:] = tmin[:]*RC[:]
R_{segment}[:] = thr[:]*V[:]
WingPerformance
0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:]
\Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:]
\Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2
(AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2
C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:]
\alpha_w[:] <= \alpha_{max,w}[:]
D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:]
C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:]
C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR)
Re_w[:] = \rho[:]*V[:]*mac/\mu[:]
C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114
FuselagePerformance
(no constraints)
VerticalTailPerformance
D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:]
Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:]
C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577
HorizontalTailPerformance
L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:]
C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:]
\alpha_{ht}[:] <= \alpha_{ht,max}
C_{L_{\alpha,ht_0}}[:] = 6.28
D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:]
C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht})
Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:]
C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852
W_{burn}[:] = W_{burn}[:]
F_{fuel}[:] = F_{fuel}[:]
\rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:])
P_{cabin}[:] = 7.5e+04
T_{cabin}[:] = 297
V[:] >= V_{stall}[:]
W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:]
tmin[:] = thr[:]
L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:]
L_{total}[:] = f_{L_{total/wing}}*L_w[:]
L_{total}[:] >= W_{avg}[:] + L_{ht}[:]
D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2
D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:])
C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S)
L/D[:] = W_{avg}[:]/D[:]
W_{Load}[:] <= W_{Load_{max}}[:]
W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S
p_{o}[:] >= L_w[:]*c_{root}/S
\eta_{o}[:] = w_{fuse}/(b/2)
x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:]
c_{m_{w}}[:] = 1.9
x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2)
x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse}
x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}}
x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}}
C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht}
AR_{ht} >= 4
C_{L_{ht}}[:] >= 0.01
SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac
SM[:] >= SM_{min}
SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}}
x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:]
R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:]
C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2
V_{nacelle}[:] = r_{v_{nacelle}}*V[:]
V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]]
r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0)
C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0
D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S
\Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}}
M_2[:3] = M[:3]
M_{2.5}[:3] = 0.6
hold_{2}[:3] = 1.07164
hold_{2.5}[:3] = 1.06372
P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:]
c1[:] = 1 + 0.201*M[:]^2.0
M_2[3:] = M[3:]
M_{2.5}[3:] = 0.6
hold_{2}[3:] = 1.07164
hold_{2.5}[3:] = 1.06372
Beginning signomial solve.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 936
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 936
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 769
Optimizer - Cones : 0
Optimizer - Scalar variables : 3438 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.03 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.64e+04 after factor : 1.45e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 2.9e+03 1.3e+05 0.00e+00 -1.280976207e+05 2.000000000e+00 1.0e+00 0.05
1 1.1e+03 1.4e+03 6.3e+04 -9.71e-01 -1.260360597e+05 3.611424052e+00 4.9e-01 0.53
2 4.1e+02 5.3e+02 2.3e+04 -9.38e-01 -1.195206719e+05 1.063331153e+01 1.8e-01 0.62
3 2.9e+02 3.7e+02 1.6e+04 -8.34e-01 -1.151942168e+05 6.795829655e+01 1.3e-01 0.66
4 2.8e+02 3.7e+02 1.6e+04 -7.59e-01 -1.127212826e+05 2.109723808e+03 1.3e-01 1.38
5 8.8e+01 1.1e+02 5.0e+03 -7.53e-01 -8.071413615e+04 8.411072422e+03 3.9e-02 1.56
6 3.7e+01 4.8e+01 2.1e+03 -2.93e-01 -4.787028059e+04 1.016025756e+04 1.6e-02 1.76
7 2.1e+01 2.8e+01 1.2e+03 2.52e-01 -3.173778936e+04 7.155034269e+03 9.5e-03 1.78
8 9.4e+00 1.2e+01 5.3e+02 5.36e-01 -1.511150083e+04 4.167123567e+03 4.2e-03 1.79
9 5.5e+00 7.1e+00 3.1e+02 8.14e-01 -8.836155418e+03 2.832992813e+03 2.5e-03 1.80
10 1.3e+00 1.7e+00 7.6e+01 9.07e-01 -2.021517100e+03 9.278094940e+02 6.1e-04 1.82
11 7.0e-01 9.1e-01 4.0e+01 9.94e-01 -8.292899266e+02 7.204982019e+02 3.2e-04 1.83
12 4.7e-01 6.1e-01 2.7e+01 9.97e-01 -4.810408396e+02 5.632816117e+02 2.1e-04 1.84
13 3.5e-01 7.3e-01 2.0e+01 9.79e-01 -3.119899248e+02 4.857188935e+02 1.6e-04 1.86
14 1.7e-01 3.5e-01 9.8e+00 9.96e-01 -1.727746611e+01 3.656933383e+02 7.9e-05 1.87
15 5.5e-02 1.5e-01 3.2e+00 9.94e-01 1.624902967e+02 2.901499707e+02 2.7e-05 2.50
16 3.2e-02 1.3e-01 1.9e+00 1.00e+00 1.999027139e+02 2.746125040e+02 1.6e-05 2.73
17 5.1e-03 1.8e-01 3.2e-01 1.00e+00 2.445305033e+02 2.572371524e+02 2.8e-06 2.87
18 1.5e-03 1.3e-01 9.6e-02 1.00e+00 2.509424510e+02 2.546897023e+02 8.3e-07 3.61
19 4.8e-04 1.1e-01 3.2e-02 1.00e+00 2.527845502e+02 2.540210950e+02 2.8e-07 4.27
20 2.1e-04 8.6e-02 1.4e-02 1.00e+00 2.532880856e+02 2.538352203e+02 1.2e-07 4.74
21 1.9e-04 7.8e-02 1.3e-02 1.00e+00 2.533292209e+02 2.538216573e+02 1.1e-07 4.99
22 1.7e-04 7.1e-02 1.1e-02 1.00e+00 2.533650962e+02 2.538082643e+02 1.0e-07 5.11
23 1.5e-04 6.4e-02 1.0e-02 1.00e+00 2.533974267e+02 2.537962616e+02 9.0e-08 5.15
24 1.4e-04 5.9e-02 9.2e-03 1.00e+00 2.534264980e+02 2.537854354e+02 8.1e-08 5.25
25 1.2e-04 5.4e-02 8.3e-03 1.00e+00 2.534526435e+02 2.537756756e+02 7.3e-08 5.49
26 1.1e-04 4.9e-02 7.5e-03 1.00e+00 2.534761571e+02 2.537668763e+02 6.5e-08 5.82
27 1.0e-04 4.5e-02 6.7e-03 1.00e+00 2.534973060e+02 2.537589453e+02 5.9e-08 6.14
28 9.0e-05 4.1e-02 6.1e-03 1.00e+00 2.535163290e+02 2.537517977e+02 5.3e-08 6.95
29 8.1e-05 3.8e-02 5.4e-03 1.00e+00 2.535334405e+02 2.537453571e+02 4.8e-08 7.38
30 7.3e-05 3.5e-02 4.9e-03 1.00e+00 2.535488335e+02 2.537395540e+02 4.3e-08 7.44
31 6.6e-05 3.2e-02 4.4e-03 1.00e+00 2.535626808e+02 2.537343259e+02 3.9e-08 7.48
32 5.9e-05 3.0e-02 4.0e-03 1.00e+00 2.535751383e+02 2.537296160e+02 3.5e-08 7.53
33 5.3e-05 2.7e-02 3.6e-03 1.00e+00 2.535863455e+02 2.537253733e+02 3.1e-08 8.65
34 4.8e-05 2.5e-02 3.2e-03 1.00e+00 2.535964283e+02 2.537215515e+02 2.8e-08 9.04
35 4.3e-05 2.4e-02 2.9e-03 1.00e+00 2.536054996e+02 2.537181092e+02 2.5e-08 9.40
36 3.9e-05 2.2e-02 2.6e-03 1.00e+00 2.536136611e+02 2.537150086e+02 2.3e-08 9.57
37 3.5e-05 2.0e-02 2.3e-03 1.00e+00 2.536210042e+02 2.537122161e+02 2.1e-08 9.66
38 3.2e-05 1.9e-02 2.1e-03 1.00e+00 2.536276109e+02 2.537097011e+02 1.9e-08 9.69
39 2.8e-05 1.8e-02 1.9e-03 1.00e+00 2.536335554e+02 2.537074360e+02 1.7e-08 9.72
40 2.6e-05 1.7e-02 1.7e-03 1.00e+00 2.536389040e+02 2.537053963e+02 1.5e-08 9.74
41 2.3e-05 1.6e-02 1.5e-03 1.00e+00 2.536437166e+02 2.537035594e+02 1.3e-08 9.80
42 2.1e-05 1.5e-02 1.4e-03 1.00e+00 2.536480470e+02 2.537019053e+02 1.2e-08 9.82
43 1.9e-05 1.4e-02 1.2e-03 1.00e+00 2.536519435e+02 2.537004159e+02 1.1e-08 10.21
44 1.7e-05 1.4e-02 1.1e-03 1.00e+00 2.536554497e+02 2.536990747e+02 9.8e-09 11.09
45 1.5e-05 1.3e-02 1.0e-03 1.00e+00 2.536586047e+02 2.536978672e+02 8.9e-09 11.45
46 1.4e-05 1.3e-02 9.1e-04 1.00e+00 2.536614438e+02 2.536967800e+02 8.0e-09 11.92
47 1.2e-05 1.2e-02 8.2e-04 1.00e+00 2.536639986e+02 2.536958012e+02 7.2e-09 11.97
48 1.1e-05 1.2e-02 7.4e-04 1.00e+00 2.536662977e+02 2.536949200e+02 6.5e-09 12.01
49 9.9e-06 1.1e-02 6.6e-04 1.00e+00 2.536683666e+02 2.536941267e+02 5.8e-09 12.06
50 8.9e-06 1.1e-02 6.0e-04 1.00e+00 2.536702284e+02 2.536934125e+02 5.2e-09 12.56
51 8.0e-06 1.0e-02 5.4e-04 1.00e+00 2.536719038e+02 2.536927696e+02 4.7e-09 13.09
52 7.2e-06 1.0e-02 4.8e-04 1.00e+00 2.536734116e+02 2.536921909e+02 4.2e-09 14.19
53 6.5e-06 9.9e-03 4.3e-04 1.00e+00 2.536747686e+02 2.536916699e+02 3.8e-09 14.24
54 5.8e-06 9.6e-03 3.9e-04 1.00e+00 2.536759897e+02 2.536912009e+02 3.4e-09 14.32
55 5.3e-06 9.4e-03 3.5e-04 1.00e+00 2.536770886e+02 2.536907788e+02 3.1e-09 15.20
56 4.7e-06 9.2e-03 3.2e-04 1.00e+00 2.536780776e+02 2.536903988e+02 2.8e-09 15.60
57 4.3e-06 9.0e-03 2.9e-04 1.00e+00 2.536789676e+02 2.536900567e+02 2.5e-09 16.50
58 3.8e-06 8.9e-03 2.6e-04 1.00e+00 2.536797686e+02 2.536897487e+02 2.3e-09 17.95
59 3.4e-06 8.7e-03 2.3e-04 1.00e+00 2.536804894e+02 2.536894716e+02 2.0e-09 18.71
60 3.1e-06 8.6e-03 2.1e-04 1.00e+00 2.536811381e+02 2.536892221e+02 1.8e-09 19.67
61 1.2e-06 3.3e-03 8.1e-05 1.00e+00 2.536846983e+02 2.536878513e+02 7.1e-10 20.21
62 1.1e-06 3.0e-03 7.3e-05 1.00e+00 2.536849266e+02 2.536877643e+02 6.4e-10 21.00
63 3.9e-07 1.1e-03 2.6e-05 1.00e+00 2.536862390e+02 2.536872587e+02 2.3e-10 21.04
64 3.5e-07 9.7e-04 2.4e-05 1.00e+00 2.536863127e+02 2.536872303e+02 2.1e-10 21.12
65 3.2e-07 8.8e-04 2.1e-05 9.99e-01 2.536863789e+02 2.536872048e+02 1.9e-10 21.96
66 2.8e-07 7.9e-04 1.9e-05 1.00e+00 2.536864385e+02 2.536871818e+02 1.7e-10 22.97
67 2.6e-07 7.1e-04 1.7e-05 1.00e+00 2.536864921e+02 2.536871611e+02 1.5e-10 23.24
68 2.3e-07 6.4e-04 1.5e-05 1.00e+00 2.536865404e+02 2.536871425e+02 1.4e-10 23.29
69 2.1e-07 5.7e-04 1.4e-05 9.99e-01 2.536865838e+02 2.536871257e+02 1.2e-10 23.32
70 1.9e-07 5.2e-04 1.3e-05 9.99e-01 2.536866229e+02 2.536871106e+02 1.1e-10 24.57
71 1.7e-07 4.7e-04 1.1e-05 1.00e+00 2.536866581e+02 2.536870970e+02 9.9e-11 25.46
72 1.5e-07 4.2e-04 1.0e-05 1.00e+00 2.536866898e+02 2.536870848e+02 8.9e-11 25.50
73 1.4e-07 3.8e-04 9.1e-06 1.00e+00 2.536867183e+02 2.536870738e+02 8.0e-11 25.52
74 1.2e-07 3.4e-04 8.2e-06 1.00e+00 2.536867440e+02 2.536870638e+02 7.2e-11 25.62
75 1.1e-07 3.1e-04 7.4e-06 1.00e+00 2.536867671e+02 2.536870549e+02 6.5e-11 25.65
76 9.9e-08 2.7e-04 6.7e-06 1.00e+00 2.536867879e+02 2.536870469e+02 5.8e-11 26.17
77 8.9e-08 2.5e-04 6.0e-06 9.99e-01 2.536868066e+02 2.536870396e+02 5.3e-11 27.62
78 8.0e-08 2.2e-04 5.4e-06 1.00e+00 2.536868234e+02 2.536870331e+02 4.7e-11 27.74
79 7.2e-08 2.0e-04 4.9e-06 1.00e+00 2.536868385e+02 2.536870273e+02 4.3e-11 27.80
80 6.5e-08 1.8e-04 4.4e-06 1.00e+00 2.536868521e+02 2.536870220e+02 3.8e-11 27.87
81 5.9e-08 1.6e-04 3.9e-06 9.99e-01 2.536868644e+02 2.536870173e+02 3.5e-11 28.10
82 5.3e-08 1.5e-04 3.5e-06 1.00e+00 2.536868755e+02 2.536870130e+02 3.1e-11 29.45
83 4.8e-08 1.3e-04 3.2e-06 1.00e+00 2.536868855e+02 2.536870091e+02 2.8e-11 29.86
84 4.3e-08 1.2e-04 2.9e-06 9.98e-01 2.536868944e+02 2.536870057e+02 2.5e-11 30.10
85 3.8e-08 1.1e-04 2.6e-06 1.00e+00 2.536869025e+02 2.536870026e+02 2.3e-11 30.56
86 3.5e-08 9.6e-05 2.3e-06 9.96e-01 2.536869097e+02 2.536869998e+02 2.0e-11 31.80
87 3.1e-08 8.6e-05 2.1e-06 9.98e-01 2.536869162e+02 2.536869973e+02 1.8e-11 32.38
88 2.8e-08 7.8e-05 1.9e-06 9.93e-01 2.536869220e+02 2.536869950e+02 1.7e-11 33.86
89 2.5e-08 7.0e-05 1.7e-06 9.96e-01 2.536869273e+02 2.536869930e+02 1.5e-11 34.52
90 2.3e-08 6.3e-05 1.5e-06 9.98e-01 2.536869320e+02 2.536869912e+02 1.3e-11 34.64
91 2.0e-08 5.7e-05 1.4e-06 9.92e-01 2.536869363e+02 2.536869895e+02 1.2e-11 36.01
92 1.8e-08 5.1e-05 1.2e-06 1.01e+00 2.536869402e+02 2.536869880e+02 1.1e-11 36.84
93 1.7e-08 4.6e-05 1.1e-06 9.93e-01 2.536869437e+02 2.536869867e+02 9.8e-12 36.88
94 1.5e-08 4.1e-05 1.0e-06 9.99e-01 2.536869468e+02 2.536869855e+02 8.8e-12 36.95
95 1.3e-08 3.7e-05 9.0e-07 9.97e-01 2.536869495e+02 2.536869844e+02 7.9e-12 38.03
96 1.2e-08 3.3e-05 8.1e-07 9.93e-01 2.536869521e+02 2.536869834e+02 7.1e-12 39.09
97 1.1e-08 3.0e-05 7.3e-07 9.95e-01 2.536869543e+02 2.536869826e+02 6.4e-12 39.14
98 9.8e-09 2.7e-05 6.6e-07 1.01e+00 2.536869565e+02 2.536869817e+02 5.8e-12 39.16
Interior-point optimizer terminated. Time: 39.22.
Optimizer terminated. Time: 39.23
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 2.5368695647e+02 Viol. con: 2e-07 var: 0e+00
Dual. obj: 2.5368698170e+02 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 39.3 seconds.
Using solver 'mosek'
Solving for 1748 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1749
Cones : 0
Scalar variables : 6101
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 925
Eliminator terminated.
Eliminator started.
Total number of eliminations : 935
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 935
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.02
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 770
Optimizer - Cones : 0
Optimizer - Scalar variables : 3440 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 : 1.64e+04 after factor : 1.45e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.281787446e+05 2.000000000e+00 1.0e+00 0.06
1 1.1e+03 1.4e+03 6.0e+04 -9.71e-01 -1.259414228e+05 3.780941016e+00 4.7e-01 0.76
2 4.6e+02 5.9e+02 2.6e+04 -9.35e-01 -1.205918795e+05 9.868922463e+00 2.0e-01 0.78
3 2.9e+02 3.7e+02 1.6e+04 -8.50e-01 -1.154239527e+05 5.250197663e+01 1.3e-01 0.84
4 2.9e+02 3.7e+02 1.6e+04 -7.62e-01 -1.133019475e+05 1.862130071e+03 1.3e-01 0.88
5 8.3e+01 1.1e+02 4.6e+03 -7.57e-01 -7.812142135e+04 9.031239867e+03 3.6e-02 0.93
6 3.6e+01 4.6e+01 2.0e+03 -2.53e-01 -4.675648511e+04 1.010078026e+04 1.6e-02 1.38
7 1.9e+01 2.4e+01 1.0e+03 2.76e-01 -2.801894100e+04 6.402312541e+03 8.2e-03 1.54
8 9.2e+00 1.2e+01 5.1e+02 6.02e-01 -1.471216448e+04 4.005088022e+03 4.0e-03 2.06
9 5.7e+00 7.3e+00 3.2e+02 8.20e-01 -9.206577478e+03 2.776623636e+03 2.5e-03 2.28
10 1.9e+00 2.4e+00 1.1e+02 9.02e-01 -2.967188192e+03 1.150548899e+03 8.4e-04 2.56
11 1.6e+00 2.0e+00 8.8e+01 9.75e-01 -2.411824742e+03 1.013250409e+03 7.0e-04 2.91
12 1.0e+00 1.4e+00 5.6e+01 9.78e-01 -1.467425485e+03 7.220754945e+02 4.4e-04 3.12
13 4.6e-01 6.8e-01 2.6e+01 9.83e-01 -5.896881228e+02 4.319680952e+02 2.1e-04 4.53
14 2.5e-01 3.8e-01 1.4e+01 1.00e+00 -2.320840438e+02 3.288887895e+02 1.1e-04 5.26
15 1.0e-01 1.6e-01 5.7e+00 1.00e+00 1.044653981e+01 2.360029459e+02 4.6e-05 5.31
16 4.7e-02 1.0e-01 2.7e+00 1.00e+00 9.574907475e+01 2.020284071e+02 2.2e-05 5.44
17 1.0e-02 1.4e-01 6.2e-01 1.01e+00 1.548431163e+02 1.790677307e+02 5.2e-06 6.20
18 6.3e-03 1.0e-01 3.9e-01 1.01e+00 1.614292033e+02 1.765011127e+02 3.2e-06 6.70
19 1.6e-03 1.2e-01 1.0e-01 1.01e+00 1.695627756e+02 1.734405842e+02 8.5e-07 7.49
20 3.4e-04 1.4e-01 2.2e-02 1.01e+00 1.717721237e+02 1.726293361e+02 1.9e-07 7.54
21 1.4e-04 1.0e-01 9.5e-03 9.94e-01 1.721372136e+02 1.725037900e+02 8.3e-08 7.57
22 8.9e-05 8.2e-02 6.0e-03 1.00e+00 1.722347054e+02 1.724653290e+02 5.2e-08 7.63
23 8.0e-05 7.6e-02 5.4e-03 1.00e+00 1.722527902e+02 1.724604212e+02 4.7e-08 8.37
24 7.2e-05 6.9e-02 4.8e-03 1.00e+00 1.722680411e+02 1.724549097e+02 4.2e-08 9.41
25 6.5e-05 6.3e-02 4.3e-03 1.00e+00 1.722818157e+02 1.724499966e+02 3.8e-08 9.83
26 5.9e-05 5.7e-02 3.9e-03 1.00e+00 1.722941841e+02 1.724455455e+02 3.4e-08 9.93
27 5.3e-05 5.2e-02 3.5e-03 1.00e+00 1.723053032e+02 1.724415268e+02 3.1e-08 11.17
28 4.7e-05 4.8e-02 3.2e-03 1.00e+00 1.723152953e+02 1.724378950e+02 2.8e-08 11.93
29 4.3e-05 4.4e-02 2.8e-03 1.00e+00 1.723242746e+02 1.724346129e+02 2.5e-08 12.09
30 3.8e-05 4.0e-02 2.6e-03 1.00e+00 1.723323436e+02 1.724316468e+02 2.2e-08 12.13
31 3.5e-05 3.7e-02 2.3e-03 1.00e+00 1.723395949e+02 1.724289667e+02 2.0e-08 12.19
32 3.1e-05 3.4e-02 2Build was aborted
Cloning into 'solar'...
/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/jenkins3442355128258613857.sh: line 101: 44523 Terminated: 15 python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True)"
INFO: Starting to record.
INFO: Processing JUnit
INFO: [JUnit] - 5 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/Users/jenkins/workspace/gplibrary_Push_Models/mosek' for the testing framework 'JUnit'.
INFO: Check 'Failed Tests' threshold.
INFO: Check 'Skipped Tests' threshold.
INFO: Setting the build status to ABORTED
INFO: Stopping recording.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: ABORTED
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