Skipping 175 KB..
Full Log52 1.1e-05 1.1e-02 6.5e-04 1.00e+00 1.664270516e+02 1.664511413e+02 5.6e-09 0.64
53 9.5e-06 1.1e-02 5.8e-04 1.00e+00 1.664286458e+02 1.664503266e+02 5.1e-09 0.65
54 8.5e-06 1.1e-02 5.3e-04 1.00e+00 1.664300788e+02 1.664495916e+02 4.6e-09 0.66
55 7.7e-06 1.0e-02 4.7e-04 1.00e+00 1.664313669e+02 1.664489285e+02 4.1e-09 0.67
56 6.9e-06 1.0e-02 4.3e-04 1.00e+00 1.664325250e+02 1.664483305e+02 3.7e-09 0.69
57 6.2e-06 9.9e-03 3.8e-04 1.00e+00 1.664335662e+02 1.664477912e+02 3.3e-09 0.70
58 5.6e-06 9.7e-03 3.4e-04 1.00e+00 1.664345023e+02 1.664473049e+02 3.0e-09 0.71
59 5.0e-06 9.5e-03 3.1e-04 1.00e+00 1.664353439e+02 1.664468664e+02 2.7e-09 0.72
60 4.5e-06 9.4e-03 2.8e-04 1.00e+00 1.664361007e+02 1.664464710e+02 2.4e-09 0.73
61 4.1e-06 9.2e-03 2.5e-04 1.00e+00 1.664367812e+02 1.664461145e+02 2.2e-09 0.74
62 3.7e-06 9.1e-03 2.3e-04 1.00e+00 1.664373931e+02 1.664457931e+02 2.0e-09 0.76
63 3.3e-06 9.0e-03 2.0e-04 1.00e+00 1.664379433e+02 1.664455033e+02 1.8e-09 0.77
64 3.0e-06 8.9e-03 1.8e-04 1.00e+00 1.664384380e+02 1.664452421e+02 1.6e-09 0.78
65 2.7e-06 8.8e-03 1.7e-04 1.00e+00 1.664388829e+02 1.664450067e+02 1.4e-09 0.79
66 2.4e-06 8.7e-03 1.5e-04 1.00e+00 1.664392831e+02 1.664447945e+02 1.3e-09 0.80
67 2.2e-06 8.6e-03 1.3e-04 1.00e+00 1.664396430e+02 1.664446034e+02 1.2e-09 0.80
68 2.0e-06 8.6e-03 1.2e-04 1.00e+00 1.664399668e+02 1.664444312e+02 1.0e-09 0.81
69 1.8e-06 8.5e-03 1.1e-04 1.00e+00 1.664402581e+02 1.664442761e+02 9.4e-10 0.83
70 1.6e-06 8.4e-03 9.7e-05 1.00e+00 1.664405202e+02 1.664441363e+02 8.5e-10 0.84
71 1.4e-06 8.4e-03 8.8e-05 1.00e+00 1.664407559e+02 1.664440105e+02 7.6e-10 0.85
72 1.3e-06 8.3e-03 7.9e-05 1.00e+00 1.664409680e+02 1.664438972e+02 6.9e-10 0.86
73 1.2e-06 8.3e-03 7.1e-05 1.00e+00 1.664411588e+02 1.664437951e+02 6.2e-10 0.87
74 1.0e-06 8.2e-03 6.4e-05 1.00e+00 1.664413305e+02 1.664437031e+02 5.6e-10 0.88
75 9.3e-07 8.2e-03 5.8e-05 1.00e+00 1.664414849e+02 1.664436203e+02 5.0e-10 0.89
76 8.4e-07 8.1e-03 5.2e-05 1.00e+00 1.664416238e+02 1.664435457e+02 4.5e-10 0.90
77 7.6e-07 8.1e-03 4.7e-05 1.00e+00 1.664417488e+02 1.664434785e+02 4.0e-10 0.90
78 6.8e-07 8.1e-03 4.2e-05 1.00e+00 1.664418612e+02 1.664434180e+02 3.6e-10 0.91
79 6.1e-07 8.0e-03 3.8e-05 1.00e+00 1.664419624e+02 1.664433635e+02 3.3e-10 0.93
80 5.5e-07 8.0e-03 3.4e-05 1.00e+00 1.664420534e+02 1.664433144e+02 3.0e-10 0.94
81 5.0e-07 8.0e-03 3.1e-05 1.00e+00 1.664421352e+02 1.664432702e+02 2.7e-10 0.95
82 4.5e-07 7.9e-03 2.8e-05 1.00e+00 1.664422089e+02 1.664432303e+02 2.4e-10 0.96
83 4.0e-07 7.9e-03 2.5e-05 1.00e+00 1.664422751e+02 1.664431944e+02 2.2e-10 0.97
84 3.6e-07 7.9e-03 2.2e-05 1.00e+00 1.664423347e+02 1.664431621e+02 1.9e-10 0.98
85 3.3e-07 7.9e-03 2.0e-05 1.00e+00 1.664423883e+02 1.664431330e+02 1.7e-10 0.99
86 2.9e-07 7.8e-03 1.8e-05 1.00e+00 1.664424366e+02 1.664431067e+02 1.6e-10 1.00
87 2.6e-07 7.8e-03 1.6e-05 1.00e+00 1.664424800e+02 1.664430831e+02 1.4e-10 1.01
88 2.4e-07 7.8e-03 1.5e-05 1.00e+00 1.664425190e+02 1.664430619e+02 1.3e-10 1.02
89 2.1e-07 7.8e-03 1.3e-05 1.00e+00 1.664425542e+02 1.664430428e+02 1.1e-10 1.03
90 1.9e-07 7.8e-03 1.2e-05 1.00e+00 1.664425858e+02 1.664430256e+02 1.0e-10 1.04
91 1.7e-07 7.8e-03 1.1e-05 1.00e+00 1.664426143e+02 1.664430101e+02 9.3e-11 1.05
92 1.6e-07 7.7e-03 9.6e-06 1.00e+00 1.664426399e+02 1.664429961e+02 8.3e-11 1.06
93 1.4e-07 7.7e-03 8.6e-06 1.00e+00 1.664426630e+02 1.664429836e+02 7.5e-11 1.07
94 1.3e-07 7.7e-03 7.8e-06 1.00e+00 1.664426838e+02 1.664429723e+02 6.8e-11 1.08
95 1.1e-07 7.7e-03 7.0e-06 1.00e+00 1.664427025e+02 1.664429622e+02 6.1e-11 1.09
96 1.0e-07 7.7e-03 6.3e-06 1.00e+00 1.664427193e+02 1.664429530e+02 5.5e-11 1.10
97 9.2e-08 7.7e-03 5.7e-06 1.00e+00 1.664427344e+02 1.664429448e+02 4.9e-11 1.11
98 8.3e-08 7.7e-03 5.1e-06 9.99e-01 1.664427480e+02 1.664429374e+02 4.4e-11 1.12
99 7.5e-08 7.6e-03 4.6e-06 1.00e+00 1.664427603e+02 1.664429307e+02 4.0e-11 1.13
100 6.7e-08 7.6e-03 4.1e-06 1.00e+00 1.664427713e+02 1.664429247e+02 3.6e-11 1.14
101 6.0e-08 7.6e-03 3.7e-06 1.00e+00 1.664427813e+02 1.664429193e+02 3.2e-11 1.15
102 5.4e-08 7.6e-03 3.3e-06 9.98e-01 1.664427902e+02 1.664429145e+02 2.9e-11 1.16
103 4.9e-08 7.6e-03 3.0e-06 1.00e+00 1.664427983e+02 1.664429101e+02 2.6e-11 1.17
104 4.4e-08 7.6e-03 2.7e-06 1.00e+00 1.664428055e+02 1.664429062e+02 2.4e-11 1.18
105 4.0e-08 7.6e-03 2.4e-06 1.00e+00 1.664428120e+02 1.664429026e+02 2.1e-11 1.19
106 3.6e-08 7.6e-03 2.2e-06 1.00e+00 1.664428179e+02 1.664428994e+02 1.9e-11 1.20
107 3.2e-08 7.6e-03 2.0e-06 9.97e-01 1.664428232e+02 1.664428966e+02 1.7e-11 1.21
108 2.9e-08 7.6e-03 1.8e-06 9.99e-01 1.664428279e+02 1.664428940e+02 1.5e-11 1.22
109 2.6e-08 7.5e-03 1.6e-06 9.96e-01 1.664428322e+02 1.664428917e+02 1.4e-11 1.23
110 2.3e-08 7.5e-03 1.4e-06 9.98e-01 1.664428360e+02 1.664428896e+02 1.3e-11 1.24
111 2.1e-08 6.8e-03 1.3e-06 1.00e+00 1.664428395e+02 1.664428877e+02 1.1e-11 1.24
112 1.9e-08 6.1e-03 1.2e-06 9.97e-01 1.664428426e+02 1.664428860e+02 1.0e-11 1.26
113 1.7e-08 5.5e-03 1.1e-06 1.00e+00 1.664428454e+02 1.664428845e+02 9.1e-12 1.27
114 1.6e-08 4.9e-03 9.5e-07 1.00e+00 1.664428480e+02 1.664428831e+02 8.2e-12 1.28
115 1.4e-08 4.4e-03 8.5e-07 1.01e+00 1.664428503e+02 1.664428818e+02 7.4e-12 1.29
116 1.3e-08 4.0e-03 7.7e-07 1.00e+00 1.664428524e+02 1.664428807e+02 6.7e-12 1.30
117 1.2e-08 4.0e-03 6.9e-07 9.96e-01 1.664428541e+02 1.664428800e+02 6.0e-12 1.31
118 1.0e-08 3.6e-03 6.2e-07 9.92e-01 1.664428558e+02 1.664428791e+02 5.4e-12 1.32
119 9.2e-09 3.2e-03 5.6e-07 1.02e+00 1.664428574e+02 1.664428781e+02 4.9e-12 1.33
120 8.3e-09 2.9e-03 5.0e-07 9.88e-01 1.664428587e+02 1.664428774e+02 4.4e-12 1.34
121 7.5e-09 2.6e-03 4.5e-07 1.02e+00 1.664428601e+02 1.664428766e+02 4.0e-12 1.35
122 6.8e-09 2.3e-03 4.1e-07 9.75e-01 1.664428611e+02 1.664428760e+02 3.6e-12 1.36
123 6.1e-09 2.1e-03 3.7e-07 1.02e+00 1.664428621e+02 1.664428755e+02 3.3e-12 1.37
124 5.5e-09 1.9e-03 3.3e-07 9.96e-01 1.664428630e+02 1.664428750e+02 3.0e-12 1.39
125 5.0e-09 1.7e-03 3.0e-07 1.00e+00 1.664428638e+02 1.664428746e+02 2.7e-12 1.40
126 4.5e-09 1.5e-03 2.7e-07 9.84e-01 1.664428645e+02 1.664428742e+02 2.4e-12 1.41
127 4.6e-08 1.5e-03 2.6e-07 9.86e-01 1.664428643e+02 1.664428750e+02 2.3e-12 1.43
128 3.6e-08 1.4e-03 2.4e-07 1.06e+00 1.664428651e+02 1.664428743e+02 2.1e-12 1.44
129 3.2e-08 1.2e-03 2.1e-07 9.94e-01 1.664428657e+02 1.664428740e+02 1.9e-12 1.45
130 2.9e-08 1.1e-03 1.9e-07 1.03e+00 1.664428663e+02 1.664428736e+02 1.8e-12 1.45
131 2.6e-08 9.9e-04 1.7e-07 9.43e-01 1.664428667e+02 1.664428733e+02 1.6e-12 1.47
132 2.3e-08 8.9e-04 1.5e-07 1.01e+00 1.664428671e+02 1.664428731e+02 1.4e-12 1.48
133 2.1e-08 8.0e-04 1.4e-07 1.02e+00 1.664428675e+02 1.664428728e+02 1.3e-12 1.49
134 1.9e-08 7.2e-04 1.3e-07 1.01e+00 1.664428678e+02 1.664428726e+02 1.2e-12 1.50
135 1.7e-08 6.5e-04 1.1e-07 9.86e-01 1.664428681e+02 1.664428724e+02 1.1e-12 1.52
136 1.5e-08 5.8e-04 1.0e-07 9.94e-01 1.664428684e+02 1.664428722e+02 9.6e-13 1.53
Optimizer terminated. Time: 1.53
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6644286838e+02 nrm: 2e+01 Viol. con: 4e-07 var: 0e+00
Dual. obj: 1.6644287224e+02 nrm: 1e+03 Viol. con: 0e+00 var: 4e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.56 seconds.
Using solver 'mosek'
Solving for 1768 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (312) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
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. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1769
Cones : 0
Scalar variables : 6131
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 482
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
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.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1769
Cones : 0
Scalar variables : 6131
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 873
Optimizer - Cones : 0
Optimizer - Scalar variables : 3462 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 : 1.49e+04 after factor : 1.57e+05
Factor - dense dim. : 0 flops : 3.26e+07
Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223796803e+05 2.000000000e+00 1.0e+00 0.05
1 1.7e+03 2.2e+03 8.9e+04 -9.71e-01 -1.216476084e+05 2.618554922e+00 7.3e-01 0.06
2 8.8e+02 1.1e+03 4.7e+04 -9.59e-01 -1.193666125e+05 4.610537506e+00 3.8e-01 0.08
3 2.9e+02 3.7e+02 1.5e+04 -9.22e-01 -1.102966097e+05 2.005786766e+01 1.3e-01 0.09
4 2.9e+02 3.7e+02 1.5e+04 -7.69e-01 -1.080118792e+05 2.024242288e+03 1.3e-01 0.10
5 1.2e+02 1.5e+02 6.3e+03 -7.60e-01 -8.686643901e+04 6.264842071e+03 5.2e-02 0.11
6 2.7e+01 3.5e+01 1.5e+03 -4.47e-01 -3.361423875e+04 1.275613178e+04 1.2e-02 0.13
7 1.7e+01 2.2e+01 9.2e+02 4.78e-01 -2.409624449e+04 7.121560004e+03 7.6e-03 0.14
8 1.0e+01 1.3e+01 5.3e+02 6.63e-01 -1.491091001e+04 4.313499207e+03 4.4e-03 0.15
9 3.8e+00 5.0e+00 2.1e+02 8.17e-01 -5.882084267e+03 1.917880415e+03 1.7e-03 0.16
10 2.0e+00 2.6e+00 1.1e+02 9.49e-01 -2.856912142e+03 1.168394898e+03 8.8e-04 0.17
11 8.4e-01 1.1e+00 4.6e+01 9.87e-01 -1.134284740e+03 6.217436659e+02 3.8e-04 0.18
12 8.2e-01 1.1e+00 4.5e+01 9.52e-01 -1.122688405e+03 5.985078074e+02 3.7e-04 0.19
13 5.2e-01 6.8e-01 2.8e+01 9.70e-01 -6.636991795e+02 4.331771302e+02 2.4e-04 0.20
14 3.0e-01 4.1e-01 1.7e+01 1.00e+00 -3.097111699e+02 3.352546183e+02 1.4e-04 0.22
15 1.1e-01 1.7e-01 5.9e+00 1.00e+00 -1.482958391e+01 2.136502396e+02 5.0e-05 0.23
16 8.4e-02 1.3e-01 4.7e+00 1.02e+00 2.760730165e+01 2.071351104e+02 4.0e-05 0.24
17 4.8e-02 9.4e-02 2.7e+00 1.02e+00 8.723176146e+01 1.898083063e+02 2.3e-05 0.26
18 1.6e-02 9.0e-02 8.7e-01 1.02e+00 1.418963690e+02 1.747571509e+02 7.4e-06 0.27
19 7.2e-03 7.0e-02 4.1e-01 1.01e+00 1.546961115e+02 1.700499165e+02 3.5e-06 0.28
20 1.7e-03 1.6e-01 1.0e-01 1.01e+00 1.636916571e+02 1.675254609e+02 8.6e-07 0.29
21 1.0e-03 1.1e-01 6.3e-02 9.76e-01 1.647504813e+02 1.670947428e+02 5.3e-07 0.30
22 3.5e-04 1.2e-01 2.2e-02 9.86e-01 1.658617377e+02 1.666773466e+02 1.9e-07 0.32
23 1.6e-04 9.6e-02 1.0e-02 1.00e+00 1.661549018e+02 1.665439119e+02 9.0e-08 0.33
24 6.2e-05 9.2e-02 4.0e-03 1.01e+00 1.663208740e+02 1.664687668e+02 3.5e-08 0.34
25 3.0e-05 7.9e-02 1.9e-03 1.01e+00 1.663730748e+02 1.664449304e+02 1.7e-08 0.35
26 2.7e-05 7.3e-02 1.7e-03 1.01e+00 1.663788267e+02 1.664435430e+02 1.5e-08 0.37
27 2.4e-05 6.6e-02 1.6e-03 1.01e+00 1.663831112e+02 1.664413337e+02 1.4e-08 0.38
28 2.2e-05 6.0e-02 1.4e-03 1.01e+00 1.663870609e+02 1.664394512e+02 1.2e-08 0.39
29 2.0e-05 5.5e-02 1.3e-03 1.01e+00 1.663905952e+02 1.664377370e+02 1.1e-08 0.40
30 1.8e-05 5.0e-02 1.1e-03 1.00e+00 1.663937727e+02 1.664361929e+02 1.0e-08 0.41
31 1.6e-05 4.6e-02 1.0e-03 1.00e+00 1.663966270e+02 1.664347990e+02 9.0e-09 0.42
32 1.4e-05 4.2e-02 9.2e-04 1.00e+00 1.663991915e+02 1.664335414e+02 8.1e-09 0.44
33 1.3e-05 3.9e-02 8.3e-04 1.00e+00 1.664014960e+02 1.664324068e+02 7.3e-09 0.45
34 1.2e-05 3.6e-02 7.5e-04 1.00e+00 1.664035668e+02 1.664313834e+02 6.6e-09 0.46
35 1.0e-05 3.3e-02 6.7e-04 1.00e+00 1.664054279e+02 1.664304602e+02 5.9e-09 0.47
36 9.4e-06 3.1e-02 6.1e-04 1.00e+00 1.664071006e+02 1.664296277e+02 5.3e-09 0.48
37 8.5e-06 2.8e-02 5.5e-04 1.00e+00 1.664086041e+02 1.664288769e+02 4.8e-09 0.49
38 7.6e-06 2.6e-02 4.9e-04 1.00e+00 1.664099557e+02 1.664281999e+02 4.3e-09 0.51
39 6.9e-06 2.4e-02 4.4e-04 1.00e+00 1.664111708e+02 1.664275896e+02 3.9e-09 0.52
40 6.2e-06 2.3e-02 4.0e-04 1.00e+00 1.664122633e+02 1.664270395e+02 3.5e-09 0.53
41 5.6e-06 2.1e-02 3.6e-04 1.00e+00 1.664132456e+02 1.664265435e+02 3.1e-09 0.54
42 5.0e-06 2.0e-02 3.2e-04 1.00e+00 1.664141289e+02 1.664260966e+02 2.8e-09 0.56
43 4.5e-06 1.9e-02 2.9e-04 1.00e+00 1.664149231e+02 1.664256937e+02 2.5e-09 0.57
44 4.1e-06 1.8e-02 2.6e-04 1.00e+00 1.664156374e+02 1.664253307e+02 2.3e-09 0.58
45 3.7e-06 1.7e-02 2.4e-04 1.00e+00 1.664162797e+02 1.664250035e+02 2.1e-09 0.59
46 3.3e-06 1.6e-02 2.1e-04 1.00e+00 1.664168573e+02 1.664247086e+02 1.9e-09 0.60
47 3.0e-06 1.5e-02 1.9e-04 1.00e+00 1.664173768e+02 1.664244429e+02 1.7e-09 0.61
48 2.7e-06 1.4e-02 1.7e-04 1.00e+00 1.664178440e+02 1.664242034e+02 1.5e-09 0.63
49 2.4e-06 1.4e-02 1.5e-04 1.00e+00 1.664182643e+02 1.664239877e+02 1.4e-09 0.64
50 2.2e-06 1.3e-02 1.4e-04 1.00e+00 1.664186423e+02 1.664237934e+02 1.2e-09 0.65
51 1.9e-06 1.3e-02 1.2e-04 1.00e+00 1.664189825e+02 1.664236185e+02 1.1e-09 0.67
52 1.7e-06 1.2e-02 1.1e-04 1.00e+00 1.664192885e+02 1.664234609e+02 9.8e-10 0.68
53 1.6e-06 1.2e-02 1.0e-04 1.00e+00 1.664195638e+02 1.664233190e+02 8.9e-10 0.69
54 1.4e-06 1.1e-02 9.1e-05 1.00e+00 1.664198115e+02 1.664231912e+02 8.0e-10 0.70
55 1.3e-06 1.1e-02 8.2e-05 1.00e+00 1.664200344e+02 1.664230761e+02 7.2e-10 0.71
56 1.1e-06 1.1e-02 7.4e-05 1.00e+00 1.664202349e+02 1.664229724e+02 6.5e-10 0.73
57 1.0e-06 1.0e-02 6.6e-05 1.00e+00 1.664204153e+02 1.664228791e+02 5.8e-10 0.74
58 9.3e-07 1.0e-02 6.0e-05 1.00e+00 1.664205776e+02 1.664227951e+02 5.2e-10 0.75
59 8.4e-07 9.9e-03 5.4e-05 1.00e+00 1.664207236e+02 1.664227194e+02 4.7e-10 0.77
60 7.5e-07 9.7e-03 4.8e-05 1.00e+00 1.664208550e+02 1.664226512e+02 4.2e-10 0.78
61 6.8e-07 9.5e-03 4.4e-05 1.00e+00 1.664209732e+02 1.664225898e+02 3.8e-10 0.79
62 6.1e-07 9.3e-03 3.9e-05 1.00e+00 1.664210796e+02 1.664225345e+02 3.4e-10 0.80
63 5.5e-07 9.2e-03 3.5e-05 1.00e+00 1.664211752e+02 1.664224847e+02 3.1e-10 0.82
64 4.9e-07 9.0e-03 3.2e-05 1.00e+00 1.664212613e+02 1.664224398e+02 2.8e-10 0.83
65 4.4e-07 8.9e-03 2.9e-05 1.00e+00 1.664213387e+02 1.664223994e+02 2.5e-10 0.83
66 4.0e-07 8.8e-03 2.6e-05 1.00e+00 1.664214083e+02 1.664223629e+02 2.3e-10 0.85
67 3.6e-07 8.7e-03 2.3e-05 1.00e+00 1.664214710e+02 1.664223301e+02 2.0e-10 0.86
68 3.2e-07 8.6e-03 2.1e-05 1.00e+00 1.664215273e+02 1.664223006e+02 1.8e-10 0.87
69 2.9e-07 8.5e-03 1.9e-05 1.00e+00 1.664215780e+02 1.664222740e+02 1.6e-10 0.88
70 2.6e-07 8.4e-03 1.7e-05 1.00e+00 1.664216237e+02 1.664222500e+02 1.5e-10 0.90
71 2.4e-07 8.4e-03 1.5e-05 1.00e+00 1.664216647e+02 1.664222284e+02 1.3e-10 0.91
72 2.1e-07 8.3e-03 1.4e-05 1.00e+00 1.664217017e+02 1.664222090e+02 1.2e-10 0.92
73 1.9e-07 8.2e-03 1.2e-05 1.00e+00 1.664217349e+02 1.664221915e+02 1.1e-10 0.94
74 1.7e-07 8.2e-03 1.1e-05 1.00e+00 1.664217648e+02 1.664221758e+02 9.7e-11 0.95
75 1.5e-07 8.1e-03 1.0e-05 1.00e+00 1.664217917e+02 1.664221616e+02 8.7e-11 0.97
76 1.4e-07 8.1e-03 9.0e-06 9.99e-01 1.664218160e+02 1.664221488e+02 7.9e-11 0.98
77 1.3e-07 8.0e-03 8.1e-06 1.00e+00 1.664218378e+02 1.664221373e+02 7.1e-11 0.99
78 1.1e-07 8.0e-03 7.3e-06 1.00e+00 1.664218574e+02 1.664221270e+02 6.4e-11 1.01
79 1.0e-07 8.0e-03 6.5e-06 1.00e+00 1.664218750e+02 1.664221177e+02 5.7e-11 1.02
80 9.1e-08 7.9e-03 5.9e-06 1.00e+00 1.664218909e+02 1.664221093e+02 5.2e-11 1.03
81 8.2e-08 7.9e-03 5.3e-06 1.00e+00 1.664219052e+02 1.664221018e+02 4.6e-11 1.04
82 7.4e-08 7.9e-03 4.8e-06 9.99e-01 1.664219181e+02 1.664220950e+02 4.2e-11 1.05
83 6.7e-08 7.9e-03 4.3e-06 1.00e+00 1.664219297e+02 1.664220889e+02 3.8e-11 1.06
84 6.0e-08 7.8e-03 3.9e-06 9.99e-01 1.664219401e+02 1.664220834e+02 3.4e-11 1.07
85 5.4e-08 7.8e-03 3.5e-06 1.00e+00 1.664219495e+02 1.664220784e+02 3.0e-11 1.09
86 4.9e-08 7.8e-03 3.1e-06 9.99e-01 1.664219579e+02 1.664220740e+02 2.7e-11 1.10
87 4.4e-08 7.8e-03 2.8e-06 9.99e-01 1.664219655e+02 1.664220700e+02 2.5e-11 1.11
88 3.9e-08 7.7e-03 2.5e-06 1.00e+00 1.664219723e+02 1.664220664e+02 2.2e-11 1.12
89 3.5e-08 7.7e-03 2.3e-06 1.00e+00 1.664219785e+02 1.664220631e+02 2.0e-11 1.13
90 3.2e-08 7.7e-03 2.1e-06 1.00e+00 1.664219840e+02 1.664220602e+02 1.8e-11 1.14
91 2.9e-08 7.7e-03 1.8e-06 1.00e+00 1.664219890e+02 1.664220576e+02 1.6e-11 1.15
92 2.6e-08 7.7e-03 1.7e-06 1.00e+00 1.664219935e+02 1.664220552e+02 1.5e-11 1.17
93 2.3e-08 7.7e-03 1.5e-06 9.99e-01 1.664219975e+02 1.664220531e+02 1.3e-11 1.17
94 2.1e-08 7.6e-03 1.3e-06 9.98e-01 1.664220012e+02 1.664220511e+02 1.2e-11 1.18
95 1.9e-08 7.6e-03 1.2e-06 1.00e+00 1.664220044e+02 1.664220494e+02 1.1e-11 1.19
96 1.7e-08 7.6e-03 1.1e-06 1.00e+00 1.664220074e+02 1.664220479e+02 9.6e-12 1.21
97 1.5e-08 7.6e-03 9.8e-07 1.00e+00 1.664220100e+02 1.664220465e+02 8.6e-12 1.22
98 1.4e-08 7.6e-03 8.8e-07 1.00e+00 1.664220124e+02 1.664220452e+02 7.8e-12 1.23
99 1.3e-08 6.8e-03 8.0e-07 1.01e+00 1.664220146e+02 1.664220441e+02 7.0e-12 1.24
100 1.1e-08 6.1e-03 7.2e-07 1.00e+00 1.664220165e+02 1.664220430e+02 6.3e-12 1.26
101 1.0e-08 5.5e-03 6.4e-07 9.99e-01 1.664220183e+02 1.664220421e+02 5.7e-12 1.27
102 9.1e-09 5.0e-03 5.8e-07 9.95e-01 1.664220198e+02 1.664220413e+02 5.1e-12 1.28
103 8.2e-09 4.5e-03 5.2e-07 1.00e+00 1.664220212e+02 1.664220406e+02 4.6e-12 1.29
104 7.4e-09 4.0e-03 4.7e-07 1.00e+00 1.664220225e+02 1.664220399e+02 4.1e-12 1.30
105 1.5e-08 3.7e-03 4.2e-07 9.00e-01 1.664220234e+02 1.664220402e+02 3.7e-12 1.31
106 1.7e-08 3.4e-03 3.8e-07 9.02e-01 1.664220242e+02 1.664220413e+02 3.3e-12 1.33
107 1.3e-08 3.0e-03 3.4e-07 1.00e+00 1.664220252e+02 1.664220407e+02 3.0e-12 1.34
108 1.2e-08 2.7e-03 3.1e-07 1.02e+00 1.664220261e+02 1.664220399e+02 2.7e-12 1.35
109 1.1e-08 2.5e-03 2.8e-07 1.00e+00 1.664220269e+02 1.664220393e+02 2.5e-12 1.37
110 1.0e-08 2.2e-03 2.5e-07 1.01e+00 1.664220276e+02 1.664220388e+02 2.2e-12 1.38
111 1.1e-08 2.0e-03 2.2e-07 8.59e-01 1.664220282e+02 1.664220388e+02 2.0e-12 1.39
112 9.5e-09 1.8e-03 2.0e-07 1.00e+00 1.664220288e+02 1.664220383e+02 1.8e-12 1.41
113 8.6e-09 1.6e-03 1.8e-07 1.00e+00 1.664220293e+02 1.664220379e+02 1.6e-12 1.42
114 7.8e-09 1.5e-03 1.6e-07 1.00e+00 1.664220298e+02 1.664220375e+02 1.5e-12 1.43
115 7.0e-09 1.3e-03 1.5e-07 9.96e-01 1.664220302e+02 1.664220371e+02 1.3e-12 1.45
116 6.3e-09 1.2e-03 1.3e-07 1.00e+00 1.664220305e+02 1.664220368e+02 1.2e-12 1.46
117 5.7e-09 1.1e-03 1.2e-07 9.97e-01 1.664220309e+02 1.664220365e+02 1.1e-12 1.47
118 5.2e-09 9.7e-04 1.1e-07 1.00e+00 1.664220312e+02 1.664220363e+02 9.7e-13 1.48
Optimizer terminated. Time: 1.49
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6642203117e+02 nrm: 2e+01 Viol. con: 1e-07 var: 0e+00
Dual. obj: 1.6642203625e+02 nrm: 1e+03 Viol. con: 0e+00 var: 9e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.53 seconds.
Using solver 'mosek'
Solving for 1768 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (313) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
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. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1769
Cones : 0
Scalar variables : 6131
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 482
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
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.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1769
Cones : 0
Scalar variables : 6131
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 873
Optimizer - Cones : 0
Optimizer - Scalar variables : 3462 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 : 1.49e+04 after factor : 1.57e+05
Factor - dense dim. : 0 flops : 3.26e+07
Factor - GP saved nzs : 3.37e+04 GP saved flops : 9.34e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223788450e+05 2.000000000e+00 1.0e+00 0.05
1 1.7e+03 2.2e+03 8.9e+04 -9.71e-01 -1.216464201e+05 2.618823612e+00 7.3e-01 0.06
2 8.8e+02 1.1e+03 4.7e+04 -9.59e-01 -1.193651315e+05 4.610867248e+00 3.8e-01 0.08
3 2.9e+02 3.7e+02 1.5e+04 -9.22e-01 -1.102819975e+05 2.006632579e+01 1.3e-01 0.09
4 2.9e+02 3.7e+02 1.5e+04 -7.69e-01 -1.080008064e+05 2.022086612e+03 1.3e-01 0.10
5 1.2e+02 1.5e+02 6.3e+03 -7.59e-01 -8.679764001e+04 6.271578903e+03 5.2e-02 0.12
6 2.7e+01 3.5e+01 1.4e+03 -4.46e-01 -3.331156973e+04 1.276898522e+04 1.2e-02 0.13
7 1.7e+01 2.2e+01 9.1e+02 4.84e-01 -2.390955460e+04 7.088701501e+03 7.6e-03 0.14
8 9.9e+00 1.3e+01 5.3e+02 6.66e-01 -1.478698502e+04 4.288484843e+03 4.4e-03 0.16
9 3.8e+00 4.9e+00 2.0e+02 8.19e-01 -5.783602810e+03 1.894120710e+03 1.7e-03 0.17
10 1.9e+00 2.5e+00 1.0e+02 9.50e-01 -2.752723046e+03 1.147878748e+03 8.5e-04 0.18
11 8.6e-01 1.1e+00 4.7e+01 9.88e-01 -1.163553864e+03 6.311053338e+02 3.9e-04 0.20
12 8.3e-01 1.1e+00 4.5e+01 9.53e-01 -1.146181136e+03 6.056748478e+02 3.8e-04 0.21
13 5.2e-01 6.8e-01 2.8e+01 9.71e-01 -6.643878606e+02 4.338683157e+02 2.4e-04 0.22
14 3.0e-01 4.0e-01 1.6e+01 1.00e+00 -3.001695787e+02 3.312568167e+02 1.4e-04 0.24
15 1.0e-01 1.6e-01 5.8e+00 1.00e+00 -1.111857075e+01 2.124409044e+02 4.9e-05 0.25
16 8.3e-02 1.3e-01 4.6e+00 1.02e+00 2.954416115e+01 2.070652180e+02 3.9e-05 0.26
17 4.6e-02 9.2e-02 2.6e+00 1.02e+00 9.054315273e+01 1.887141196e+02 2.2e-05 0.28
18 1.2e-02 1.7e-01 6.8e-01 1.02e+00 1.474804520e+02 1.732840791e+02 5.8e-06 0.29
19 4.0e-03 1.9e-01 2.3e-01 1.01e+00 1.599979590e+02 1.685737685e+02 1.9e-06 0.30
20 1.6e-03 1.1e-01 9.4e-02 1.01e+00 1.638684180e+02 1.673751081e+02 8.0e-07 0.32
21 6.4e-04 9.4e-02 3.8e-02 1.01e+00 1.653872518e+02 1.668180858e+02 3.3e-07 0.33
22 2.4e-04 9.6e-02 1.4e-02 1.01e+00 1.660337135e+02 1.665706256e+02 1.3e-07 0.34
23 9.1e-05 9.3e-02 5.6e-03 1.01e+00 1.662643767e+02 1.664734884e+02 5.0e-08 0.36
24 8.2e-05 8.5e-02 5.1e-03 1.01e+00 1.662801856e+02 1.664683641e+02 4.5e-08 0.37
25 7.4e-05 7.7e-02 4.6e-03 1.01e+00 1.662931282e+02 1.664624192e+02 4.0e-08 0.38
26 6.7e-05 7.0e-02 4.1e-03 1.01e+00 1.663048697e+02 1.664571799e+02 3.6e-08 0.39
27 6.0e-05 6.4e-02 3.7e-03 1.01e+00 1.663153795e+02 1.664524151e+02 3.3e-08 0.41
28 5.4e-05 5.8e-02 3.3e-03 1.01e+00 1.663248144e+02 1.664481107e+02 2.9e-08 0.42
29 4.8e-05 5.3e-02 3.0e-03 1.01e+00 1.663332809e+02 1.664442181e+02 2.6e-08 0.43
30 4.4e-05 4.9e-02 2.7e-03 1.01e+00 1.663408801e+02 1.664406994e+02 2.4e-08 0.45
31 3.9e-05 4.5e-02 2.4e-03 1.01e+00 1.663477017e+02 1.664375192e+02 2.1e-08 0.46
32 3.5e-05 4.1e-02 2.2e-03 1.01e+00 1.663538259e+02 1.664346455e+02 1.9e-08 0.47
33 3.2e-05 3.8e-02 2.0e-03 1.01e+00 1.663593248e+02 1.664320492e+02 1.7e-08 0.49
34 2.9e-05 3.5e-02 1.8e-03 1.00e+00 1.663642629e+02 1.664297041e+02 1.6e-08 0.50
35 2.6e-05 3.2e-02 1.6e-03 1.00e+00 1.663686978e+02 1.664275861e+02 1.4e-08 0.51
36 2.3e-05 3.0e-02 1.4e-03 1.00e+00 1.663726813e+02 1.664256736e+02 1.3e-08 0.53
37 2.1e-05 2.8e-02 1.3e-03 1.00e+00 1.663762595e+02 1.664239469e+02 1.1e-08 0.54
38 1.9e-05 2.6e-02 1.2e-03 1.00e+00 1.663794741e+02 1.664223881e+02 1.0e-08 0.55
39 1.7e-05 2.4e-02 1.0e-03 1.00e+00 1.663823623e+02 1.664209811e+02 9.2e-09 0.56
40 1.5e-05 2.2e-02 9.4e-04 1.00e+00 1.663849573e+02 1.664197112e+02 8.3e-09 0.58
41 1.4e-05 2.1e-02 8.5e-04 1.00e+00 1.663872893e+02 1.664185653e+02 7.5e-09 0.59
42 1.2e-05 2.0e-02 7.6e-04 1.00e+00 1.663893850e+02 1.664175315e+02 6.7e-09 0.60
43 1.1e-05 1.8e-02 6.9e-04 1.00e+00 1.663912685e+02 1.664165987e+02 6.0e-09 0.62
44 1.0e-05 1.7e-02 6.2e-04 1.00e+00 1.663929614e+02 1.664157574e+02 5.4e-09 0.63
45 9.0e-06 1.7e-02 5.6e-04 1.00e+00 1.663944832e+02 1.664149986e+02 4.9e-09 0.64
46 8.1e-06 1.6e-02 5.0e-04 1.00e+00 1.663958513e+02 1.664143143e+02 4.4e-09 0.66
47 7.3e-06 1.5e-02 4.5e-04 1.00e+00 1.663970812e+02 1.664136972e+02 4.0e-09 0.67
48 6.5e-06 1.4e-02 4.1e-04 1.00e+00 1.663981870e+02 1.664131409e+02 3.6e-09 0.68
49 5.9e-06 1.4e-02 3.7e-04 1.00e+00 1.663991812e+02 1.664126394e+02 3.2e-09 0.69
50 5.3e-06 1.3e-02 3.3e-04 1.00e+00 1.664000753e+02 1.664121873e+02 2.9e-09 0.71
51 4.8e-06 1.3e-02 3.0e-04 1.00e+00 1.664008792e+02 1.664117798e+02 2.6e-09 0.72
52 4.3e-06 1.2e-02 2.7e-04 1.00e+00 1.664016021e+02 1.664114125e+02 2.3e-09 0.73
53 3.9e-06 1.2e-02 2.4e-04 1.00e+00 1.664022522e+02 1.664110814e+02 2.1e-09 0.74
54 3.5e-06 1.1e-02 2.2e-04 1.00e+00 1.664028368e+02 1.664107829e+02 1.9e-09 0.75
55 3.1e-06 1.1e-02 1.9e-04 1.00e+00 1.664033625e+02 1.664105139e+02 1.7e-09 0.77
56 2.8e-06 1.1e-02 1.7e-04 1.00e+00 1.664038353e+02 1.664102715e+02 1.5e-09 0.78
57 2.5e-06 1.1e-02 1.6e-04 1.00e+00 1.664042606e+02 1.664100531e+02 1.4e-09 0.79
58 2.3e-06 1.0e-02 1.4e-04 1.00e+00 1.664046431e+02 1.664098564e+02 1.2e-09 0.80
59 2.1e-06 1.0e-02 1.3e-04 1.00e+00 1.664049873e+02 1.664096792e+02 1.1e-09 0.82
60 1.8e-06 9.8e-03 1.1e-04 1.00e+00 1.664052969e+02 1.664095196e+02 1.0e-09 0.83
61 1.7e-06 9.7e-03 1.0e-04 1.00e+00 1.664055754e+02 1.664093758e+02 9.1e-10 0.84
62 1.5e-06 9.5e-03 9.3e-05 1.00e+00 1.664058260e+02 1.664092464e+02 8.2e-10 0.85
63 1.3e-06 9.3e-03 8.4e-05 1.00e+00 1.664060515e+02 1.664091298e+02 7.4e-10 0.86
64 1.2e-06 9.2e-03 7.5e-05 1.00e+00 1.664062543e+02 1.664090248e+02 6.6e-10 0.88
65 1.1e-06 9.1e-03 6.8e-05 1.00e+00 1.664064368e+02 1.664089302e+02 6.0e-10 0.89
66 9.8e-07 9.0e-03 6.1e-05 1.00e+00 1.664066010e+02 1.664088451e+02 5.4e-10 0.90
67 8.8e-07 8.9e-03 5.5e-05 1.00e+00 1.664067487e+02 1.664087684e+02 4.8e-10 0.91
68 8.0e-07 8.8e-03 4.9e-05 1.00e+00 1.664068816e+02 1.664086993e+02 4.3e-10 0.93
69 7.2e-07 8.7e-03 4.4e-05 1.00e+00 1.664070012e+02 1.664086371e+02 3.9e-10 0.94
70 6.4e-07 8.6e-03 4.0e-05 1.00e+00 1.664071087e+02 1.664085811e+02 3.5e-10 0.95
71 5.8e-07 8.5e-03 3.6e-05 1.00e+00 1.664072054e+02 1.664085306e+02 3.2e-10 0.96
72 5.2e-07 8.5e-03 3.2e-05 1.00e+00 1.664072925e+02 1.664084851e+02 2.9e-10 0.97
73 4.7e-07 8.4e-03 2.9e-05 1.00e+00 1.664073707e+02 1.664084441e+02 2.6e-10 0.99
74 4.2e-07 8.3e-03 2.6e-05 1.00e+00 1.664074411e+02 1.664084072e+02 2.3e-10 1.00
75 3.8e-07 8.3e-03 2.4e-05 1.00e+00 1.664075045e+02 1.664083739e+02 2.1e-10 1.01
76 3.4e-07 8.2e-03 2.1e-05 1.00e+00 1.664075614e+02 1.664083439e+02 1.9e-10 1.02
77 3.1e-07 8.2e-03 1.9e-05 1.00e+00 1.664076127e+02 1.664083169e+02 1.7e-10 1.03
78 2.8e-07 8.1e-03 1.7e-05 1.00e+00 1.664076588e+02 1.664082926e+02 1.5e-10 1.04
79 2.5e-07 8.1e-03 1.5e-05 1.00e+00 1.664077003e+02 1.664082707e+02 1.4e-10 1.06
80 2.2e-07 8.1e-03 1.4e-05 1.00e+00 1.664077376e+02 1.664082510e+02 1.2e-10 1.07
81 2.0e-07 8.0e-03 1.3e-05 1.00e+00 1.664077712e+02 1.664082333e+02 1.1e-10 1.08
82 1.8e-07 8.0e-03 1.1e-05 1.00e+00 1.664078015e+02 1.664082173e+02 9.9e-11 1.09
83 1.6e-07 8.0e-03 1.0e-05 1.00e+00 1.664078287e+02 1.664082029e+02 9.0e-11 1.11
84 1.5e-07 8.0e-03 9.2e-06 1.00e+00 1.664078531e+02 1.664081899e+02 8.1e-11 1.12
85 1.3e-07 7.9e-03 8.2e-06 1.00e+00 1.664078752e+02 1.664081783e+02 7.3e-11 1.13
86 1.2e-07 7.9e-03 7.4e-06 1.00e+00 1.664078950e+02 1.664081678e+02 6.5e-11 1.14
87 1.1e-07 7.9e-03 6.7e-06 1.00e+00 1.664079128e+02 1.664081583e+02 5.9e-11 1.16
88 9.7e-08 7.9e-03 6.0e-06 1.00e+00 1.664079289e+02 1.664081498e+02 5.3e-11 1.17
89 8.7e-08 7.8e-03 5.4e-06 1.00e+00 1.664079433e+02 1.664081422e+02 4.8e-11 1.18
90 7.8e-08 7.8e-03 4.9e-06 1.00e+00 1.664079563e+02 1.664081353e+02 4.3e-11 1.19
91 7.1e-08 7.8e-03 4.4e-06 1.00e+00 1.664079680e+02 1.664081291e+02 3.9e-11 1.20
92 6.4e-08 7.8e-03 3.9e-06 1.00e+00 1.664079785e+02 1.664081235e+02 3.5e-11 1.21
93 5.7e-08 7.8e-03 3.5e-06 1.00e+00 1.664079880e+02 1.664081185e+02 3.1e-11 1.22
94 5.1e-08 7.8e-03 3.2e-06 1.00e+00 1.664079965e+02 1.664081140e+02 2.8e-11 1.24
95 4.6e-08 7.8e-03 2.9e-06 1.00e+00 1.664080042e+02 1.664081099e+02 2.5e-11 1.25
96 4.2e-08 7.7e-03 2.6e-06 1.00e+00 1.664080111e+02 1.664081062e+02 2.3e-11 1.26
97 3.7e-08 7.7e-03 2.3e-06 1.00e+00 1.664080173e+02 1.664081029e+02 2.0e-11 1.27
98 3.4e-08 7.7e-03 2.1e-06 9.99e-01 1.664080229e+02 1.664080999e+02 1.8e-11 1.28
99 3.0e-08 7.7e-03 1.9e-06 1.00e+00 1.664080279e+02 1.664080973e+02 1.7e-11 1.29
100 2.7e-08 7.7e-03 1.7e-06 9.99e-01 1.664080325e+02 1.664080949e+02 1.5e-11 1.31
101 2.5e-08 7.7e-03 1.5e-06 9.99e-01 1.664080365e+02 1.664080927e+02 1.3e-11 1.32
102 2.2e-08 7.6e-03 1.4e-06 9.98e-01 1.664080402e+02 1.664080908e+02 1.2e-11 1.34
103 2.0e-08 7.6e-03 1.2e-06 1.00e+00 1.664080435e+02 1.664080891e+02 1.1e-11 1.35
104 1.8e-08 7.6e-03 1.1e-06 9.98e-01 1.664080465e+02 1.664080875e+02 9.8e-12 1.36
105 1.6e-08 7.6e-03 1.0e-06 9.98e-01 1.664080491e+02 1.664080861e+02 8.8e-12 1.37
106 1.5e-08 6.8e-03 9.0e-07 1.00e+00 1.664080515e+02 1.664080848e+02 7.9e-12 1.39
107 1.3e-08 6.2e-03 8.1e-07 9.99e-01 1.664080537e+02 1.664080836e+02 7.1e-12 1.40
108 1.2e-08 5.5e-03 7.3e-07 9.97e-01 1.664080557e+02 1.664080826e+02 6.4e-12 1.41
109 1.1e-08 5.0e-03 6.6e-07 9.97e-01 1.664080574e+02 1.664080816e+02 5.8e-12 1.42
110 9.6e-09 4.5e-03 5.9e-07 1.00e+00 1.664080590e+02 1.664080808e+02 5.2e-12 1.44
111 8.6e-09 4.0e-03 5.3e-07 1.01e+00 1.664080605e+02 1.664080800e+02 4.7e-12 1.46
112 7.7e-09 3.6e-03 4.8e-07 1.01e+00 1.664080618e+02 1.664080793e+02 4.3e-12 1.47
113 7.0e-09 3.3e-03 4.3e-07 1.00e+00 1.664080629e+02 1.664080787e+02 3.8e-12 1.48
114 6.3e-09 2.9e-03 3.9e-07 1.01e+00 1.664080640e+02 1.664080781e+02 3.5e-12 1.49
115 5.7e-09 2.6e-03 3.5e-07 9.94e-01 1.664080649e+02 1.664080776e+02 3.1e-12 1.50
116 5.1e-09 2.4e-03 3.1e-07 9.84e-01 1.664080657e+02 1.664080772e+02 2.8e-12 1.52
117 2.1e-08 2.4e-03 3.1e-07 -3.26e-01 1.664080664e+02 1.664080752e+02 2.6e-12 1.53
118 2.1e-08 2.1e-03 2.8e-07 1.02e+00 1.664080676e+02 1.664080744e+02 2.2e-12 1.54
119 1.8e-08 2.0e-03 2.5e-07 9.97e-01 1.664080680e+02 1.664080743e+02 2.0e-12 1.58
120 1.7e-08 1.8e-03 2.3e-07 9.92e-01 1.664080686e+02 1.664080742e+02 1.8e-12 1.59
121 1.5e-08 1.7e-03 2.1e-07 1.03e+00 1.664080691e+02 1.664080741e+02 1.6e-12 1.60
122 1.3e-08 1.5e-03 1.9e-07 1.02e+00 1.664080696e+02 1.664080740e+02 1.5e-12 1.62
123 1.2e-08 1.3e-03 1.7e-07 1.04e+00 1.664080700e+02 1.664080739e+02 1.3e-12 1.63
124 1.1e-08 1.2e-03 1.5e-07 1.01e+00 1.664080703e+02 1.664080738e+02 1.2e-12 1.64
125 9.8e-09 1.1e-03 1.4e-07 9.98e-01 1.664080706e+02 1.664080737e+02 1.1e-12 1.65
126 8.9e-09 9.8e-04 1.2e-07 9.96e-01 1.664080709e+02 1.664080737e+02 9.8e-13 1.67
Optimizer terminated. Time: 1.67
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.6640807086e+02 nrm: 2e+01 Viol. con: 1e-07 var: 0e+00
Dual. obj: 1.6640807369e+02 nrm: 1e+03 Viol. con: 0e+00 var: 4e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.71 seconds.
Solving took 9 GP solves and 24.4 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: 1.4957403142127757e+110 vs 1.49570493199e+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
Solution check warning: Primal solution computed cost did not match solver-returned cost: 7.485942833952247e+74 vs 7.48576841516e+74
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
WEIGHT DIFFERENCES
Total Fuel Weight Percent Diff: [-92.94682601]
Total Aircraft Weight Percent Diff: [-21.48053826]
Engine Weight Percent Diff: -56.27816263501683
Fuselage Weight Percent Diff: -0.8697283781658797
Payload Weight Percent Diff: [-0.0400356]
VT Weight Percent Diff: -8.607712900393501
HT Weight Percent Diff: -93.23330431885311
Wing Weight Percent Diff: 8.267573259901017
WING DIFFERENCES
Wing Span Percent Diff: -0.029994358510184876
Wing Area Percent Diff: 32.89970105408197
HORIZONTAL TAIL DIFFERENCES
HT Area Percent Diff: 40.48862631668246
VERTICAL TAIL DIFFERENCES
VT Span Percent Diff: -11.02232031308826
VT Area Percent Diff: -60.38681772051953
CRUISE SEGMENT 1 DRAG DIFFERENCES
Overall Cd Percent Diff: [-18.54721004]
L/D Percent Diff: [24.01023756]
Nacelle Cd Percent Diff: [-94.27640786]
HT Cd Percent Diff: [-80.7694112] dimensionless
Fuselage Cd Percent Diff: [108.78752887]
VT Cd Percent Diff: [-58.00288783] dimensionless
Wing Cd percent Diff: [-14.229156]
Induced Drag Cd Percent Diff: [1.21939606]
CRUISE SEGMENT 1 TSFC DIFFERENCES
Initial Cruise TSFC Percent Diff: [-90.57036149]
FUSELAGE DIFFERENCES
Weight of HB material: -38.360425524416385
Weight of VB material: 87.8200230270085
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.71260522]
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}[:]/dum[:])^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}[:]/dum[:])^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 1768 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. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1769
Cones : 0
Scalar variables : 6131
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 476
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.03
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1769
Cones : 0
Scalar variables : 6131
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 878
Optimizer - Cones : 0
Optimizer - Scalar variables : 3466 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 : 0.04
Factor - nonzeros before factor : 1.49e+04 after factor : 1.55e+05
Factor - dense dim. : 0 flops : 3.17e+07
Factor - GP saved nzs : 3.36e+04 GP saved flops : 9.32e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.223083000e+05 2.000000000e+00 1.0e+00 0.07
1 1.6e+03 2.0e+03 8.4e+04 -9.71e-01 -1.214169755e+05 2.778937242e+00 6.8e-01 0.09
2 8.2e+02 1.1e+03 4.4e+04 -9.56e-01 -1.189685922e+05 5.116623673e+00 3.6e-01 0.10
3 2.9e+02 3.8e+02 1.6e+04 -9.15e-01 -1.102962345e+05 2.170095046e+01 1.3e-01 0.11
4 2.9e+02 3.8e+02 1.6e+04 -7.69e-01 -1.083159562e+05 1.743975991e+03 1.3e-01 0.13
5 1.1e+02 1.5e+02 6.0e+03 -7.60e-01 -8.473424866e+04 6.747984694e+03 5.0e-02 0.14
6 3.8e+01 4.9e+01 2.0e+03 -4.14e-01 -4.537005734e+04 1.080379792e+04 1.7e-02 0.15
7 2.0e+01 2.7e+01 1.1e+03 2.54e-01 -2.836625497e+04 7.045474557e+03 9.0e-03 0.18
8 9.4e+00 1.2e+01 5.0e+02 5.72e-01 -1.387003547e+04 4.245870985e+03 4.2e-03 0.19
9 4.7e+00 6.2e+00 2.6e+02 8.29e-01 -6.980052804e+03 2.517162242e+03 2.1e-03 0.21
10 1.4e+00 1.9e+00 7.8e+01 9.33e-01 -2.014621384e+03 9.508454525e+02 6.5e-04 0.22
11 6.4e-01 8.4e-01 3.5e+01 9.93e-01 -6.678945647e+02 6.594956157e+02 2.9e-04 0.24
12 4.8e-01 6.4e-01 2.7e+01 9.96e-01 -4.499444859e+02 5.609447906e+02 2.2e-04 0.25
13 3.5e-01 7.8e-01 1.9e+01 9.80e-01 -2.667764900e+02 4.766170471e+02 1.6e-04 0.27
14 1.7e-01 3.9e-01 9.5e+00 9.96e-01 3.398903189e-01 3.641145682e+02 8.0e-05 0.29
15 5.8e-02 1.6e-01 3.3e+00 9.94e-01 1.652792674e+02 2.911850936e+02 2.8e-05 0.30
16 3.3e-02 1.4e-01 1.9e+00 1.00e+00 2.032349806e+02 2.745517815e+02 1.6e-05 0.32
17 4.6e-03 2.1e-01 2.9e-01 1.00e+00 2.458601979e+02 2.569052088e+02 2.6e-06 0.33
18 1.3e-03 1.4e-01 8.6e-02 1.00e+00 2.513276389e+02 2.546006416e+02 7.8e-07 0.35
19 4.6e-04 1.1e-01 3.0e-02 1.00e+00 2.528755707e+02 2.540040947e+02 2.7e-07 0.36
20 1.8e-04 9.1e-02 1.2e-02 1.00e+00 2.533597014e+02 2.538150010e+02 1.1e-07 0.37
21 1.7e-04 8.2e-02 1.1e-02 1.00e+00 2.533933866e+02 2.538031620e+02 9.9e-08 0.39
22 1.5e-04 7.5e-02 9.7e-03 1.00e+00 2.534228246e+02 2.537915997e+02 8.9e-08 0.40
23 1.3e-04 6.8e-02 8.7e-03 1.00e+00 2.534493464e+02 2.537812275e+02 8.0e-08 0.44
24 1.2e-04 6.2e-02 7.8e-03 1.00e+00 2.534731930e+02 2.537718722e+02 7.2e-08 0.45
25 1.1e-04 5.6e-02 7.1e-03 1.00e+00 2.534946426e+02 2.537634424e+02 6.5e-08 0.46
26 9.8e-05 5.2e-02 6.4e-03 1.00e+00 2.535139347e+02 2.537558453e+02 5.8e-08 0.47
27 8.8e-05 4.7e-02 5.7e-03 1.00e+00 2.535312881e+02 2.537490000e+02 5.3e-08 0.49
28 7.9e-05 4.3e-02 5.1e-03 1.00e+00 2.535468982e+02 2.537428327e+02 4.7e-08 0.50
29 7.1e-05 4.0e-02 4.6e-03 1.00e+00 2.535609408e+02 2.537372768e+02 4.3e-08 0.52
30 6.4e-05 3.6e-02 4.2e-03 1.00e+00 2.535735736e+02 2.537322719e+02 3.8e-08 0.53
31 5.8e-05 3.4e-02 3.8e-03 1.00e+00 2.535849385e+02 2.537277637e+02 3.5e-08 0.54
32 5.2e-05 3.1e-02 3.4e-03 1.00e+00 2.535951630e+02 2.537237031e+02 3.1e-08 0.57
33 4.7e-05 2.9e-02 3.0e-03 1.00e+00 2.536043618e+02 2.537200458e+02 2.8e-08 0.58
34 4.2e-05 2.7e-02 2.7e-03 1.00e+00 2.536126378e+02 2.537167517e+02 2.5e-08 0.59
35 3.8e-05 2.5e-02 2.5e-03 1.00e+00 2.536200838e+02 2.537137851e+02 2.3e-08 0.60
36 3.4e-05 2.3e-02 2.2e-03 1.00e+00 2.536267832e+02 2.537111133e+02 2.0e-08 0.62
37 3.1e-05 2.1e-02 2.0e-03 1.00e+00 2.536328109e+02 2.537087072e+02 1.8e-08 0.63
38 2.8e-05 2.0e-02 1.8e-03 1.00e+00 2.536382344e+02 2.537065405e+02 1.7e-08 0.64
39 2.5e-05 1.9e-02 1.6e-03 1.00e+00 2.536431143e+02 2.537045893e+02 1.5e-08 0.66
40 2.2e-05 1.8e-02 1.5e-03 1.00e+00 2.536475051e+02 2.537028323e+02 1.3e-08 0.68
41 2.0e-05 1.7e-02 1.3e-03 1.00e+00 2.536514561e+02 2.537012503e+02 1.2e-08 0.69
42 1.8e-05 1.6e-02 1.2e-03 1.00e+00 2.536550112e+02 2.536998258e+02 1.1e-08 0.71
43 1.6e-05 1.5e-02 1.1e-03 1.00e+00 2.536582102e+02 2.536985432e+02 9.8e-09 0.72
44 1.5e-05 1.4e-02 9.5e-04 1.00e+00 2.536610889e+02 2.536973885e+02 8.8e-09 0.74
45 1.3e-05 1.4e-02 8.6e-04 1.00e+00 2.536636793e+02 2.536963489e+02 7.9e-09 0.75
46 1.2e-05 1.3e-02 7.7e-04 1.00e+00 2.536660103e+02 2.536954129e+02 7.1e-09 0.76
47 1.1e-05 1.2e-02 7.0e-04 1.00e+00 2.536681080e+02 2.536945703e+02 6.4e-09 0.78
48 9.6e-06 1.2e-02 6.3e-04 1.00e+00 2.536699957e+02 2.536938118e+02 5.8e-09 0.79
49 8.7e-06 1.2e-02 5.6e-04 1.00e+00 2.536716945e+02 2.536931290e+02 5.2e-09 0.80
50 7.8e-06 1.1e-02 5.1e-04 1.00e+00 2.536732232e+02 2.536925143e+02 4.7e-09 0.82
51 7.0e-06 1.1e-02 4.6e-04 1.00e+00 2.536745990e+02 2.536919610e+02 4.2e-09 0.83
52 6.3e-06 1.0e-02 4.1e-04 1.00e+00 2.536758371e+02 2.536914629e+02 3.8e-09 0.84
53 5.7e-06 1.0e-02 3.7e-04 1.00e+00 2.536769513e+02 2.536910146e+02 3.4e-09 0.85
54 5.1e-06 9.9e-03 3.3e-04 1.00e+00 2.536779540e+02 2.536906110e+02 3.1e-09 0.87
55 4.6e-06 9.7e-03 3.0e-04 1.00e+00 2.536788564e+02 2.536902477e+02 2.8e-09 0.88
56 4.1e-06 9.5e-03 2.7e-04 1.00e+00 2.536796685e+02 2.536899207e+02 2.5e-09 0.89
57 3.7e-06 9.3e-03 2.4e-04 1.00e+00 2.536803993e+02 2.536896263e+02 2.2e-09 0.91
58 3.4e-06 9.1e-03 2.2e-04 1.00e+00 2.536810570e+02 2.536893613e+02 2.0e-09 0.93
59 3.0e-06 8.9e-03 2.0e-04 1.00e+00 2.536816489e+02 2.536891228e+02 1.8e-09 0.94
60 1.2e-06 3.4e-03 7.6e-05 1.00e+00 2.536849211e+02 2.536878032e+02 7.0e-10 0.96
61 1.0e-06 3.1e-03 6.8e-05 1.00e+00 2.536851269e+02 2.536877209e+02 6.3e-10 0.97
62 3.7e-07 1.1e-03 2.4e-05 1.00e+00 2.536863131e+02 2.536872421e+02 2.2e-10 0.99
63 3.4e-07 1.0e-03 2.2e-05 1.00e+00 2.536863794e+02 2.536872155e+02 2.0e-10 1.01
64 3.0e-07 9.0e-04 2.0e-05 1.00e+00 2.536864389e+02 2.536871914e+02 1.8e-10 1.02
65 2.7e-07 8.1e-04 1.8e-05 1.00e+00 2.536864925e+02 2.536871697e+02 1.6e-10 1.04
66 2.5e-07 7.3e-04 1.6e-05 1.00e+00 2.536865407e+02 2.536871503e+02 1.5e-10 1.05
67 2.2e-07 6.6e-04 1.4e-05 1.00e+00 2.536865841e+02 2.536871327e+02 1.3e-10 1.07
68 2.0e-07 5.9e-04 1.3e-05 1.00e+00 2.536866232e+02 2.536871169e+02 1.2e-10 1.09
69 1.8e-07 5.3e-04 1.2e-05 1.00e+00 2.536866583e+02 2.536871027e+02 1.1e-10 1.10
70 1.6e-07 4.8e-04 1.1e-05 1.00e+00 2.536866900e+02 2.536870899e+02 9.7e-11 1.11
71 1.5e-07 4.3e-04 9.5e-06 1.00e+00 2.536867185e+02 2.536870784e+02 8.7e-11 1.13
72 1.3e-07 3.9e-04 8.5e-06 1.00e+00 2.536867441e+02 2.536870680e+02 7.8e-11 1.14
73 1.2e-07 3.5e-04 7.7e-06 1.00e+00 2.536867672e+02 2.536870587e+02 7.1e-11 1.15
74 1.1e-07 3.1e-04 6.9e-06 1.00e+00 2.536867879e+02 2.536870503e+02 6.3e-11 1.18
75 9.5e-08 2.8e-04 6.2e-06 1.00e+00 2.536868066e+02 2.536870427e+02 5.7e-11 1.19
76 8.6e-08 2.5e-04 5.6e-06 1.00e+00 2.536868234e+02 2.536870359e+02 5.1e-11 1.20
77 7.7e-08 2.3e-04 5.0e-06 1.00e+00 2.536868385e+02 2.536870298e+02 4.6e-11 1.22
78 6.9e-08 2.1e-04 4.5e-06 1.00e+00 2.536868521e+02 2.536870243e+02 4.2e-11 1.23
79 6.3e-08 1.9e-04 4.1e-06 1.00e+00 2.536868644e+02 2.536870193e+02 3.7e-11 1.24
80 5.6e-08 1.7e-04 3.7e-06 1.00e+00 2.536868754e+02 2.536870149e+02 3.4e-11 1.26
81 5.1e-08 1.5e-04 3.3e-06 1.00e+00 2.536868854e+02 2.536870109e+02 3.0e-11 1.28
82 4.6e-08 1.3e-04 3.0e-06 1.00e+00 2.536868943e+02 2.536870072e+02 2.7e-11 1.30
83 4.1e-08 1.2e-04 2.7e-06 1.00e+00 2.536869023e+02 2.536870040e+02 2.5e-11 1.31
84 3.7e-08 1.1e-04 2.4e-06 1.00e+00 2.536869096e+02 2.536870010e+02 2.2e-11 1.33
85 3.3e-08 9.8e-05 2.2e-06 1.00e+00 2.536869161e+02 2.536869984e+02 2.0e-11 1.34
86 3.0e-08 8.8e-05 1.9e-06 1.00e+00 2.536869219e+02 2.536869960e+02 1.8e-11 1.35
87 2.7e-08 8.0e-05 1.8e-06 1.00e+00 2.536869272e+02 2.536869939e+02 1.6e-11 1.37
88 2.4e-08 7.2e-05 1.6e-06 1.00e+00 2.536869319e+02 2.536869920e+02 1.5e-11 1.39
89 2.2e-08 6.5e-05 1.4e-06 1.00e+00 2.536869362e+02 2.536869902e+02 1.3e-11 1.40
90 2.0e-08 5.8e-05 1.3e-06 1.00e+00 2.536869401e+02 2.536869887e+02 1.2e-11 1.42
91 1.8e-08 5.2e-05 1.1e-06 1.00e+00 2.536869435e+02 2.536869873e+02 1.1e-11 1.44
92 1.6e-08 4.7e-05 1.0e-06 1.00e+00 2.536869466e+02 2.536869860e+02 9.5e-12 1.45
93 1.4e-08 4.2e-05 9.3e-07 1.00e+00 2.536869494e+02 2.536869849e+02 8.6e-12 1.47
94 1.3e-08 3.8e-05 8.4e-07 1.00e+00 2.536869520e+02 2.536869839e+02 7.7e-12 1.48
95 1.2e-08 3.4e-05 7.5e-07 1.00e+00 2.536869542e+02 2.536869829e+02 6.9e-12 1.50
96 1.0e-08 3.1e-05 6.8e-07 1.00e+00 2.536869563e+02 2.536869821e+02 6.2e-12 1.52
97 9.4e-09 2.8e-05 6.1e-07 1.00e+00 2.536869581e+02 2.536869814e+02 5.6e-12 1.53
Optimizer terminated. Time: 1.54
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 2.5368695810e+02 nrm: 4e+01 Viol. con: 2e-07 var: 0e+00
Dual. obj: 2.5368698136e+02 nrm: 8e+02 Viol. con: 0e+00 var: 2e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.58 seconds.
Using solver 'mosek'
Solving for 1768 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
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. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1769
Cones : 0
Scalar variables : 6131
Matrix variables : 0
Integer variables : 0
Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 476
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
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.
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1769
Cones : 0
Scalar variables : 6131
Matrix variables : 0
Integer variables : 0
Optimizer - threads : 8
Optimizer - solved problem : the primal
Optimizer - Constraints : 879
Optimizer - Cones : 0
Optimizer - Scalar variables : 3468 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 : 1.49e+04 after factor : 1.56e+05
Factor - dense dim. : 0 flops : 3.19e+07
Factor - GP saved nzs : 3.36e+04 GP saved flops : 9.32e+05
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.2e+05 0.00e+00 -1.219705586e+05 2.000000000e+00 1.0e+00 0.05
1 1.6e+03 2.1e+03 8.4e+04 -9.71e-01 -1.211031020e+05 2.765533663e+00 6.9e-01 0.07
2 7.8e+02 1.0e+03 4.2e+04 -9.57e-01 -1.183621946e+05 5.379607955e+00 3.4e-01 0.08
3 2.9e+02 3.8e+02 1.6e+04 -9.11e-01 -1.100271642e+05 2.234927157e+01 1.3e-01 0.10
4 2.9e+02 3.8e+02 1.6e+04 -7.69e-01 -1.081090538e+05 1.691198782e+03 1.3e-01 0.13
5 1.2e+02 1.6e+02 6.6e+03 -7.61e-01 -8.730500726e+04 6.170178286e+03 5.4e-02 0.14
6 3.9e+01 5.1e+01 2.1e+03 -4.57e-01 -4.641557494e+04 1.102767695e+04 1.7e-02 0.15
7 2.3e+01 3.0e+01 1.2e+03 2.33e-01 -3.095362448e+04 7.311515434e+03 1.0e-02 0.17
8 9.3e+00 1.2e+01 5.0e+02 5.26e-01 -1.383958025e+04 4.015287293e+03 4.1e-03 0.18
9 6.1e+00 7.9e+00 3.2e+02 8.28e-01 -9.007628044e+03 2.852555853e+03 2.7e-03 0.19
10 2.1e+00 2.7e+00 1.1e+02 9.03e-01 -3.047258165e+03 1.195224977e+03 9.4e-04 0.21
11 1.6e+00 2.0e+00 8.5e+01 9.77e-01 -2.209373100e+03 9.993568394e+02 7.0e-04 0.22
12 1.0e+00 1.4e+00 5.6e+01 9.78e-01 -1.412745572e+03 7.362078430e+02 4.7e-04 0.24
13 4.1e-01 7.0e-01 2.2e+01 9.86e-01 -4.532334049e+02 3.966890953e+02 1.9e-04 0.27
14 2.4e-01 4.3e-01 1.3e+01 1.00e+00 -1.803313668e+02 3.208030866e+02 1.1e-04 0.28
15 7.5e-02 4.3e-01 4.2e+00 1.00e+00 5.907667930e+01 2.194258788e+02 3.6e-05 0.29
16 2.7e-02 1.8e-01 1.5e+00 1.01e+00 1.312032677e+02 1.889662771e+02 1.3e-05 0.31
17 8.9e-03 1.1e-01 5.2e-01 1.01e+00 1.583140177e+02 1.780792062e+02 4.6e-06 0.32
18 3.5e-03 9.8e-02 2.1e-01 1.01e+00 1.668085083e+02 1.746024948e+02 1.8e-06 0.34
19 9.2e-04 1.2e-01 5.6e-02 1.01e+00 1.708677782e+02 1.729897946e+02 5.1e-07 0.36
20 3.1e-04 1.0e-01 1.9e-02 1.00e+00 1.718819279e+02 1.726108386e+02 1.8e-07 0.37
21 1.1e-04 1.0e-01 7.1e-03 9.98e-01 1.722145287e+02 1.724820216e+02 6.5e-08 0.40
22 3.7e-05 1.0e-01 2.4e-03 9.99e-01 1.723408997e+02 1.724300134e+02 2.2e-08 0.41
23 3.4e-05 9.2e-02 2.1e-03 1.00e+00 1.723477057e+02 1.724279165e+02 1.9e-08 0.42
24 3.0e-05 8.4e-02 1.9e-03 1.00e+00 1.723534337e+02 1.724256231e+02 1.8e-08 0.44
25 2.7e-05 7.6e-02 1.7e-03 1.00e+00 1.723585613e+02 1.724235306e+02 1.6e-08 0.45
26 2.5e-05 7.0e-02 1.6e-03 1.00e+00 1.723631653e+02 1.724216358e+02 1.4e-08 0.47
27 2.2e-05 6.3e-02 1.4e-03 1.00e+00 1.723673034e+02 1.724199249e+02 1.3e-08 0.49
28 2.0e-05 5.8e-02 1.3e-03 1.00e+00 1.723710236e+02 1.724183812e+02 1.2e-08 0.51
29 1.8e-05 5.3e-02 1.1e-03 1.00e+00 1.723743688e+02 1.724169890e+02 1.0e-08 0.53
30 1.6e-05 4.8e-02 1.0e-03 1.00e+00 1.723773770e+02 1.724157339e+02 9.3e-09 0.55
31 1.5e-05 4.4e-02 9.2e-04 1.00e+00 1.723800823e+02 1.724146024e+02 8.4e-09 0.56
32 1.3e-05 4.1e-02 8.2e-04 1.00e+00 1.723825154e+02 1.724135826e+02 7.6e-09 0.58
33 1.2e-05 3.7e-02 7.4e-04 1.00e+00 1.723847038e+02 1.724126634e+02 6.8e-09 0.59
34 1.1e-05 3.4e-02 6.7e-04 1.00e+00 1.723866721e+02 1.724118351e+02 6.1e-09 0.61
35 9.5e-06 3.2e-02 6.0e-04 1.00e+00 1.723884426e+02 1.724110887e+02 5.5e-09 0.62
36 8.6e-06 2.9e-02 5.4e-04 1.00e+00 1.723900351e+02 1.724104163e+02 5.0e-09 0.64
37 7.7e-06 2.7e-02 4.9e-04 1.00e+00 1.723914678e+02 1.724098104e+02 4.5e-09 0.65
38 6.9e-06 2.5e-02 4.4e-04 1.00e+00 1.723927565e+02 1.724092646e+02 4.0e-09 0.66
39 6.3e-06 2.4e-02 3.9e-04 1.00e+00 1.723939159e+02 1.724087729e+02 3.6e-09 0.68
40 5.6e-06 2.2e-02 3.5e-04 1.00e+00 1.723949589e+02 1.724083301e+02 3.3e-09 0.69
41 5.1e-06 2.1e-02 3.2e-04 1.00e+00 1.723958973e+02 1.724079312e+02 2.9e-09 0.70
42 4.6e-06 1.9e-02 2.9e-04 1.00e+00 1.723967416e+02 1.724075719e+02 2.6e-09 0.72
43 4.1e-06 1.8e-02 2.6e-04 1.00e+00 1.723975012e+02 1.724072484e+02 2.4e-09 0.73
44 3.7e-06 1.7e-02 2.3e-04 1.00e+00 1.723981846e+02 1.724069570e+02 2.1e-09 0.74
45 3.3e-06 1.6e-02 2.1e-04 1.00e+00 1.723987995e+02 1.724066946e+02 1.9e-09 0.76
46 3.0e-06 1.5e-02 1.9e-04 1.00e+00 1.723993528e+02 1.724064584e+02 1.7e-09 0.77
47 2.7e-06 1.5e-02 1.7e-04 1.00e+00 1.723998506e+02 1.724062456e+02 1.6e-09 0.78
48 2.4e-06 1.4e-02 1.5e-04 1.00e+00 1.724002985e+02 1.724060540e+02 1.4e-09 0.79
49 2.2e-06 1.3e-02 1.4e-04 1.00e+00 1.724007016e+02 1.724058815e+02 1.3e-09 0.80
50 2.0e-06 1.3e-02 1.2e-04 1.00e+00 1.724010643e+02 1.724057262e+02 1.1e-09 0.82
51 1.8e-06 1.2e-02 1.1e-04 1.00e+00 1.724013906e+02 1.724055863e+02 1.0e-09 0.83
52 1.6e-06 1.2e-02 1.0e-04 1.00e+00 1.724016843e+02 1.724054604e+02 9.2e-10 0.84
53 1.4e-06 1.1e-02 9.0e-05 1.00e+00 1.724019485e+02 1.724053470e+02 8.3e-10 0.86
54 1.3e-06 1.1e-02 8.1e-05 1.00e+00 1.724021863e+02 1.724052450e+02 7.4e-10 0.87
55 1.2e-06 1.1e-02 7.3e-05 1.00e+00 1.724024003e+02 1.724051531e+02 6.7e-10 0.88
56 1.0e-06 1.0e-02 6.6e-05 1.00e+00 1.724025928e+02 1.724050703e+02 6.0e-10 0.90
57 9.4e-07 1.0e-02 5.9e-05 1.00e+00 1.724027661e+02 1.724049959e+02 5.4e-10 0.91
58 8.4e-07 9.8e-03 5.3e-05 1.00e+00 1.724029220e+02 1.724049288e+02 4.9e-10 0.93
59 7.6e-07 9.6e-03 4.8e-05 1.00e+00 1.724030623e+02 1.724048684e+02 4.4e-10 0.94
60 6.8e-07 9.4e-03 4.3e-05 1.00e+00 1.724031886e+02 1.724048141e+02 4.0e-10 0.96
61 6.2e-07 9.2e-03 3.9e-05 1.00e+00 1.724033022e+02 1.724047651e+02 3.6e-10 0.98
62 5.5e-07 9.1e-03 3.5e-05 1.00e+00 1.724034044e+02 1.724047211e+02 3.2e-10 0.99
63 5.0e-07 8.9e-03 3.1e-05 1.00e+00 1.724034964e+02 1.724046814e+02 2.9e-10 1.01
64 4.5e-07 8.8e-03 2.8e-05 1.00e+00 1.724035792e+02 1.724046457e+02 2.6e-10 1.02
65 4.0e-07 8.7e-03 2.5e-05 1.00e+00 1.724036537e+02 1.724046135e+02 2.3e-10 1.04
66 3.6e-07 8.6e-03 2.3e-05 1.00e+00 1.724037207e+02 1.724045846e+02 2.1e-10 1.06
67 3.3e-07 8.5e-03 2.1e-05 1.00e+00 1.724037810e+02 1.724045585e+02 1.9e-10 1.07
68 2.9e-07 8.4e-03 1.9e-05 1.00e+00 1.724038353e+02 1.724045351e+02 1.7e-10 1.09
69 2.7e-07 8.3e-03 1.7e-05 1.00e+00 1.724038842e+02 1.724045140e+02 1.5e-10 1.10
70 2.4e-07 8.2e-03 1.5e-05 1.00e+00 1.724039281e+02 1.724044949e+02 1.4e-10 1.11
71 2.1e-07 8.1e-03 1.4e-05 1.00e+00 1.724039677e+02 1.724044778e+02 1.2e-10 1.13
72 1.9e-07 8.1e-03 1.2e-05 1.00e+00 1.724040033e+02 1.724044624e+02 1.1e-10 1.15
73 1.7e-07 8.0e-03 1.1e-05 1.00e+00 1.724040353e+02 1.724044485e+02 1.0e-10 1.16
74 1.6e-07 8.0e-03 9.9e-06 9.99e-01 1.724040642e+02 1.724044360e+02 9.0e-11 1.17
75 1.4e-07 7.9e-03 8.9e-06 1.00e+00 1.724040901e+02 1.724044248e+02 8.1e-11 1.19
76 1.3e-07 7.9e-03 8.0e-06 1.00e+00 1.724041135e+02 1.724044147e+02 7.3e-11 1.20
77 1.1e-07 7.8e-03 7.2e-06 1.00e+00 1E
======================================================================
ERROR [43.093s]: test_SPaircraft_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 40, in test_fn
mod.test()
File "SPaircraft.py", line 87, in test
sol = optimize_aircraft(m, substitutions, fixedBPR, pRatOpt, mutategparg)
File "SPaircraft.py", line 62, in optimize_aircraft
sol = m_relax.localsolve(verbosity=4, iteration_limit=200, reltol=0.01, mutategp=mutategparg, x0 = x0)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/constraints/prog_factories.py", line 124, in solvefn
result = progsolve(solver, verbosity, **kwargs)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/constraints/sgp.py", line 149, in localsolve
feas_constrs, None)
File "/Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit/gpkit/constraints/gp.py", line 112, in __init__
+ boundstrs)
ValueError: Geometric Program is not fully bounded:
Mission1.Aircraft.Engine.EngineConstants.Relax1.R has no lower bound
Mission1.Aircraft.Engine.EngineConstants.Relax1.g has no lower bound
----------------------------------------------------------------------
Ran 1 test in 43.093s
FAILED (errors=1)
Generating XML reports...
.724041344e+02 1.724044056e+02 6.6e-11 1.22
78 1.0e-07 7.8e-03 6.5e-06 1.00e+00 1.724041534e+02 1.724043974e+02 5.9e-11 1.23
79 9.2e-08 7.0e-03 5.8e-06 1.01e+00 1.724041707e+02 1.724043898e+02 5.4e-11 1.24
80 8.3e-08 6.3e-03 5.2e-06 9.98e-01 1.724041860e+02 1.724043831e+02 4.8e-11 1.26
81 7.5e-08 5.7e-03 4.7e-06 9.95e-01 1.724041998e+02 1.724043771e+02 4.3e-11 1.27
82 6.8e-08 5.1e-03 4.3e-06 9.94e-01 1.724042122e+02 1.724043717e+02 3.9e-11 1.29
83 6.1e-08 4.6e-03 3.8e-06 9.99e-01 1.724042233e+02 1.724043669e+02 3.5e-11 1.30
84 5.5e-08 4.1e-03 3.4e-06 9.99e-01 1.724042333e+02 1.724043626e+02 3.2e-11 1.31
85 4.9e-08 3.7e-03 3.1e-06 9.94e-01 1.724042423e+02 1.724043586e+02 2.8e-11 1.33
86 4.5e-08 3.4e-03 2.8e-06 9.91e-01 1.724042504e+02 1.724043551e+02 2.6e-11 1.34
87 4.0e-08 3.0e-03 2.5e-06 9.74e-01 1.724042578e+02 1.724043519e+02 2.3e-11 1.35
88 3.7e-08 2.7e-03 2.3e-06 9.78e-01 1.724042644e+02 1.724043489e+02 2.1e-11 1.37
89 3.2e-08 2.4e-03 2.0e-06 1.01e+00 1.724042705e+02 1.724043464e+02 1.9e-11 1.39
90 3.0e-08 2.2e-03 1.8e-06 1.05e+00 1.724042770e+02 1.724043434e+02 1.7e-11 1.40
91 2.7e-08 2.0e-03 1.6e-06 9.74e-01 1.724042816e+02 1.724043414e+02 1.6e-11 1.42
92 2.6e-08 1.8e-03 1.5e-06 1.01e+00 1.724042860e+02 1.724043393e+02 1.4e-11 1.43
93 2.5e-08 1.6e-03 1.3e-06 9.93e-01 1.724042898e+02 1.724043376e+02 1.3e-11 1.45
94 5.6e-08 2.3e-04 1.9e-07 7.69e-01 1.724043192e+02 1.724043264e+02 2.2e-12 1.46
95 2.7e-08 2.3e-04 1.9e-07 -1.73e+00 1.724043193e+02 1.724043245e+02 2.0e-12 1.47
96 4.0e-08 2.3e-04 2.1e-07 1.00e+00 1.724043188e+02 1.724043245e+02 2.0e-12 1.49
97 4.0e-08 2.3e-04 2.1e-07 1.03e+01 1.724043188e+02 1.724043245e+02 2.0e-12 1.51
Optimizer terminated. Time: 1.51
solsta = 7, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : NEAR_OPTIMAL
Primal. obj: 1.7240431885e+02 nrm: 4e+01 Viol. con: 8e-07 var: 0e+00
Dual. obj: 1.7240432452e+02 nrm: 8e+02 Viol. con: 0e+00 var: 1e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.56 seconds.
Cloning into 'solar'...
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.8.0)
Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.4)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2019.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0)
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting git+https://github.com/convexengineering/gpfit.git
Cloning https://github.com/convexengineering/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-M0Tc57
Running command git clone -q https://github.com/convexengineering/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-M0Tc57
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.4)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Building wheels for collected packages: gpfit
Building wheel for gpfit (setup.py): started
Building wheel for gpfit (setup.py): finished with status 'done'
Created wheel for gpfit: filename=gpfit-0.1-cp27-none-any.whl size=25151 sha256=ad75d603de4abae019ace731f56b2fb8fe6b35514b5df11977aba8c7607d3bb9
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-zC46h1/wheels/d5/94/ac/b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting git+https://github.com/convexengineering/gassolar.git
Cloning https://github.com/convexengineering/gassolar.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-hHHtSU
Running command git clone -q https://github.com/convexengineering/gassolar.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-hHHtSU
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.24.2)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.12.0)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.8.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2019.2)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gassolar==0.0.0.0) (1.0.2)
Building wheels for collected packages: gassolar
Building wheel for gassolar (setup.py): started
Building wheel for gassolar (setup.py): finished with status 'done'
Created wheel for gassolar: filename=gassolar-0.0.0.0-cp27-none-any.whl size=4876517 sha256=6dc626e38153a614e36838aa02f45f17386df2a25f91d3a35ad715a3721f15e6
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-ZZYvIM/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Processing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/solar
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from solar==0.0.0.0) (0.9.1.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.24.2)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.12.0)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2.8.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2019.2)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->solar==0.0.0.0) (1.0.2)
Building wheels for collected packages: solar
Building wheel for solar (setup.py): started
Building wheel for solar (setup.py): finished with status 'done'
Created wheel for solar: filename=solar-0.0.0.0-cp27-none-any.whl size=14822 sha256=35b91e5ba31474633f50cf341628d46879ce3f57aa3fb07679a9840e3bd22c46
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-f3HMQD/wheels/55/91/84/60653f7cb392791f8ec648fb5ef240c78233b7566d69a6c92c
Successfully built solar
Installing collected packages: solar
Successfully installed solar-0.0.0.0
Running tests...
----------------------------------------------------------------------
/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped.
warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning)
../Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
tau = np.exp(-0.175/costhsun)
/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
tau = np.exp(-0.175/costhsun)
....
----------------------------------------------------------------------
Ran 6 tests in 258.344s
OK
Generating XML reports...
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
adding test for 'solar/npod_trade.py'
N=1
Beginning signomial solve.
Solving took 5 GP solves and 1.11 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 0.8904 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1632916.9435 but bound is 600000.0000
Warning: Variable Mission.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1259333.2960 but bound is 1000000.0000
N=3
Beginning signomial solve.
Solving took 5 GP solves and 1.18 seconds.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1135 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1036204.4449 but bound is 600000.0000
Warning: Variable Mission1.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1006645.3573 but bound is 1000000.0000
N=5
Beginning signomial solve.
Solving took 5 GP solves and 1.26 seconds.
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1487 but bound is 0.9465
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 989673.4666 but bound is 600000.0000
Warning: Variable Mission2.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1019678.5408 but bound is 1000000.0000
N=7
Beginning signomial solve.
Solving took 5 GP solves and 1.23 seconds.
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 976142.1475 but bound is 600000.0000
Warning: Variable Mission3.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1042059.4123 but bound is 1000000.0000
N=9
Beginning signomial solve.
Solving took 5 GP solves and 1.65 seconds.
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1567 but bound is 0.9465
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1007400.4785 but bound is 600000.0000
Warning: Variable Mission4.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1092545.5150 but bound is 1000000.0000
N=0
Beginning signomial solve.
Solving took 4 GP solves and 0.832 seconds.
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2078 but bound is 600000.0000
N=1
Beginning signomial solve.
Solving took 5 GP solves and 2.16 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 0.8904 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1632919.3776 but bound is 600000.0000
Warning: Variable Mission.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1259329.5070 but bound is 1000000.0000
N=3
Beginning signomial solve.
Solving took 5 GP solves and 2.28 seconds.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1135 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1036209.6021 but bound is 600000.0000
Warning: Variable Mission1.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1006641.3990 but bound is 1000000.0000
N=5
Beginning signomial solve.
Solving took 5 GP solves and 1.59 seconds.
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1487 but bound is 0.9465
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 989673.1341 but bound is 600000.0000
Warning: Variable Mission2.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1019680.6011 but bound is 1000000.0000
N=7
Beginning signomial solve.
Solving took 5 GP solves and 1.79 seconds.
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 976138.7332 but bound is 600000.0000
Warning: Variable Mission3.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1042059.9154 but bound is 1000000.0000
N=9
Beginning signomial solve.
Solving took 5 GP solves and 1.95 seconds.
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.1567 but bound is 0.9465
Warning: Variable Mission4.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1007396.6632 but bound is 600000.0000
Warning: Variable Mission4.Climb.AircraftDrag.TailAero1.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1092544.5684 but bound is 1000000.0000
N=0
Beginning signomial solve.
Solving took 4 GP solves and 1.14 seconds.
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission5.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119116.3963 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 5.9 seconds.
Allowing negative dual variable(s) as small as -3.6246815899639153e-11.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.3227 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 671709.7480 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 5.17 seconds.
Allowing negative dual variable(s) as small as -5.780984487322902e-10.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2812 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 729183.6293 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 5.46 seconds.
Allowing negative dual variable(s) as small as -7.486587934225628e-12.
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2258 but bound is 0.9465
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 802959.5997 but bound is 600000.0000
Using solver 'mosek'
Solving for 7672 variables.
Solving took 2.69 seconds.
Allowing negative dual variable(s) as small as -1.2634497534364602e-11.
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2008 but bound is 0.9465
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 839122.5079 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 5.92 seconds.
Allowing negative dual variable(s) as small as -3.6246815899639153e-11.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.3227 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 671709.7480 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 5.29 seconds.
Allowing negative dual variable(s) as small as -5.780984487322902e-10.
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2812 but bound is 0.9465
Warning: Variable Mission1.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 729183.6293 but bound is 600000.0000
Using solver 'mosek'
Solving for 14852 variables.
Solving took 5.28 seconds.
Allowing negative dual variable(s) as small as -7.486587934225628e-12.
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2258 but bound is 0.9465
Warning: Variable Mission2.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 802959.5997 but bound is 600000.0000
Using solver 'mosek'
Solving for 7672 variables.
Solving took 2.6 seconds.
Allowing negative dual variable(s) as small as -1.2634497534364602e-11.
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.2008 but bound is 0.9465
Warning: Variable Mission3.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 839122.5079 but bound is 600000.0000
Beginning signomial solve.
Solving took 4 GP solves and 0.727 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2076 but bound is 600000.0000
Beginning signomial solve.
Solving took 4 GP solves and 0.762 seconds.
Warning: Variable Mission.Climb.AircraftDrag.WingAero.CL[:] could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465
Warning: Variable Mission.Climb.AircraftDrag.WingAero.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1119121.2076 but bound is 600000.0000
fatal: destination path 'gplibrary' already exists and is not an empty directory.
fatal: destination path 'gplibrary' already exists and is not an empty directory.
fatal: destination path 'gplibrary' already exists and is not an empty directory.
fatal: destination path 'gplibrary' already exists and is not an empty directory.
fatal: destination path 'gplibrary' already exists and is not an empty directory.
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.24.2)
Requirement already satisfied: python-dateutil>=2.5.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.8.0)
Requirement already satisfied: numpy>=1.12.0 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.16.4)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2019.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil>=2.5.0->pandas) (1.12.0)
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Collecting git+https://github.com/hoburg/gpfit.git
Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-Av9cBK
Running command git clone -q https://github.com/hoburg/gpfit.git /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-req-build-Av9cBK
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.16.4)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.2.2)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gpkit (from gpfit==0.1) (0.9.1.0)
Requirement already satisfied: pint>=0.8.1 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.9)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Requirement already satisfied: cvxopt>=1.1.8 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.2.3)
Requirement already satisfied: six in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.12.0)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint>=0.8.1->gpkit->gpfit==0.1) (1.0.2)
Building wheels for collected packages: gpfit
Building wheel for gpfit (setup.py): started
Building wheel for gpfit (setup.py): finished with status 'done'
Created wheel for gpfit: filename=gpfit-0.1-cp27-none-any.whl size=25151 sha256=8fc6d865a8673589e45cc35ff5f70a1044385cce807f4c7c2392591e4c765914
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-aMOljk/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
DEPRECATION: Python 2.7 will reach the end of its life on January 1st, 2020. Please upgrade your Python as Python 2.7 won't be maintained after that date. A future version of pip will drop support for Python 2.7. More details about Python 2 support in pip, can be found at https://pip.pypa.io/en/latest/development/release-process/#python-2-support
Processing /Users/jenkins/workspace/gplibrary_Push_Models/mosek/gplibrary
Requirement already satisfied: numpy>=1.12 in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.16.4)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.2.2)
Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.9)
Requirement already satisfied: funcsigs; python_version == "2.7" in /Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pint->gpkitmodels==0.0.0.0) (1.0.2)
Building wheels for collected packages: gpkitmodels
Building wheel for gpkitmodels (setup.py): started
Building wheel for gpkitmodels (setup.py): finished with status 'done'
Created wheel for gpkitmodels: filename=gpkitmodels-0.0.0.0-cp27-none-any.whl size=65670 sha256=71ca66e701b63b5b0ce24b94a49004e84e3ff18cdf910641d666cb8bd230053d
Stored in directory: /private/var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/pip-ephem-wheel-cache-tQuo6s/wheels/ab/79/3c/c09e2173989dc969f23a5e4c34887060b900152ee1d8be6e1c
Successfully built gpkitmodels
Installing collected packages: gpkitmodels
Found existing installation: gpkitmodels 0.0.0.0
Uninstalling gpkitmodels-0.0.0.0:
Successfully uninstalled gpkitmodels-0.0.0.0
Successfully installed gpkitmodels-0.0.0.0
Running tests...
----------------------------------------------------------------------
../Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped.
warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning)
..............
----------------------------------------------------------------------
Ran 16 tests in 11.227s
OK
Generating XML reports...
adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py'
adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py'
adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py'
adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py'
adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py'
adding test for 'gpkitmodels/SP/SimPleAC/SimPleAC.py'
adding test for 'gpkitmodels/SP/SimPleAC/SimPleAC_mission.py'
adding test for 'gpkitmodels/SP/SimPleAC/SimPleAC_multimission.py'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.0109 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.0474 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.0148 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.00984 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0139 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 0.605 seconds.
Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.0394 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.0342 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.0353 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 1.23 seconds.
Using solver 'mosek'
Solving for 13 variables.
Solving took 0.0146 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 0.459 seconds.
Warning: Variable BladeElementProp.BladeElementPerf.cl[:] could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable BladeElementProp.BladeElementPerf.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1619898.0180 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.0381 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 0.872 seconds.
Warning: Variable BladeElementProp.BladeElementPerf.cl[:] could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable BladeElementProp.BladeElementPerf.Re[:] could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000
Warning: Variable TailAero.Re could cause inaccurate result because it is above upper bound. Solution is 2220953.3838 but bound is 1000000.0000
Warning: Variable TailAero1.Re could cause inaccurate result because it is above upper bound. Solution is 2499787.9776 but bound is 1000000.0000
Warning: Variable TailAero2.Re could cause inaccurate result because it is above upper bound. Solution is 2223878.3883 but bound is 1000000.0000
Warning: Variable TailAero3.Re could cause inaccurate result because it is above upper bound. Solution is 2223877.9590 but bound is 1000000.0000
Warning: Variable TailAero4.Re could cause inaccurate result because it is above upper bound. Solution is 1853897.1004 but bound is 1000000.0000
Warning: Variable TailAero5.Re could cause inaccurate result because it is above upper bound. Solution is 1853897.1004 but bound is 1000000.0000
Warning: Variable TailAero.Re could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000
Warning: Variable TailAero1.Re could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000
Warning: Variable TailAero2.Re could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable TailAero3.Re could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable TailAero4.Re could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable TailAero5.Re could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable WingAero.Re could cause inaccurate result because it is above upper bound. Solution is 1884891.6332 but bound is 700000.0000
Warning: Variable WingAero1.Re could cause inaccurate result because it is above upper bound. Solution is 1910419.6195 but bound is 700000.0000
Warning: Variable WingAero.Re could cause inaccurate result because it is above upper bound. Solution is 1910412.9866 but bound is 700000.0000
Warning: Variable WingAero1.Re could cause inaccurate result because it is above upper bound. Solution is 1910412.9866 but bound is 700000.0000
SP is not converging! Last GP iteration had a higher cost (3e+03) than the previous one (2.7e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (3e+03) than the previous one (2.7e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (3.4e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (3.4e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
SP is not converging! Last GP iteration had a higher cost (4.3e+03) than the previous one (4.3e+03). Results for each iteration are in (Model).program.results. If your model contains SignomialEqualities, note that convergence is not guaranteed: try replacing any SigEqs you can and solving again.
Beginning signomial solve.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.0157 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.0138 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.0104 seconds.
Using solver 'mosek'
Solving for 20 variables.
Solving took 0.00932 seconds.
Solving took 4 GP solves and 0.0542 seconds.
Beginning signomial solve.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.057 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.0445 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.047 seconds.
Using solver 'mosek_cli'
Solving for 20 variables.
Solving took 0.0437 seconds.
Solving took 4 GP solves and 0.206 seconds.
Cloning into 'eVTOL'...
Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 5.737s
OK
Generating XML reports...
adding test for 'models/model_tests.py'
Found no installed solvers, beginning a build.
# Moving to the directory from which GPkit was imported.
Started building gpkit...
Attempting to find and build solvers:
# Looking for mosek
# Found /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h
# Found /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib
# Found /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.c
# Found /Users/jenkins/mosek/8/tools/examples/c/expopt.c
# Found /Users/jenkins/mosek/8/tools/examples/c/dgopt.c
# Found /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.h
# Found /Users/jenkins/mosek/8/tools/examples/c/expopt.h
# Found /Users/jenkins/mosek/8/tools/examples/c/dgopt.h
# Found /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h
# Found mosek version 8, installed to /Users/jenkins/mosek
#
# Building mosek...
# Replacing directory _mosek/lib
# Replacing directory _mosek/build
# Replacing directory /Users/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit
#
# Copying expopt library files to _mosek/build
# Copying /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.c
# Copying /Users/jenkins/mosek/8/tools/examples/c/expopt.c
# Copying /Users/jenkins/mosek/8/tools/examples/c/dgopt.c
# Copying /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.h
# Copying /Users/jenkins/mosek/8/tools/examples/c/expopt.h
# Copying /Users/jenkins/mosek/8/tools/examples/c/dgopt.h
# Copying /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h
#
# Applying expopt patches...
#
# Change in _mosek/build/dgopt.con line 651
# -- printf("Number of Hessian non-zeros: %d\n",nlh[0]->numhesnz);
# ++ MSK_echotask(task,MSK_STREAM_MSG,"Number of Hessian non-zeros: %d\n",n
#
# Change in _mosek/build/expopt.con line 566
# -- printf("Warning: The variable with index '%d' has only positiv
# ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in
#
# Change in _mosek/build/expopt.con line 579
# -- printf("Warning: The variable with index '%d' has only negativ
# ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in
#
# Change in _mosek/build/expopt.con line 1115
# -- printf ("solsta = %d, prosta = %d\n", (int)*solsta,(int)*prosta);
# ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "solsta = %d, prosta = %d\n",
#
# Building expopt library...
# Calling 'gcc -fpic -shared -Wl,-rpath "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin" _mosek/build/scopt-ext.c _mosek/build/expopt.c _mosek/build/dgopt.c "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib" -o /Users/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit/expopt.so'
##
### CALL BEGINS
### CALL ENDS
##
# Calling 'install_name_tool -change libmosek64.8.1.dylib /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib /Users/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit/expopt.so'
##
### CALL BEGINS
### CALL ENDS
##
# Calling 'install_name_tool -change libmosek64.8.1.dylib @executable_path/libmosek64.8.1.dylib /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/mskexpopt'
##
### CALL BEGINS
### CALL ENDS
##
#
# Building Python bindings for expopt and Mosek...
# (if this fails on Windows, verify the mingw version)
# Calling 'python modified_ctypesgen.py -a -l /Users/jenkins/workspace/gplibrary_Push_Models/mosek/build_gpkit/expopt.so -l "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib" -o _mosek/lib/expopt_h.py _mosek/build/expopt.h'
##
### CALL BEGINS
### CALL ENDS
##
# Done building mosek
# Looking for mosek_cli
# Trying to run mskexpopt...
# Calling 'mskexpopt'
##
### CALL BEGINS
### CALL ENDS
##
# Found mosek_cli in system path
# Looking for cvxopt
# Trying to import cvxopt...
# Found cvxopt in Python path
...finished building gpkit.
Replaced found solvers ([u'mosek', u'mosek_cli', u'cvxopt']) with environment var GPKITSOLVERS (mosek, mosek_cli)
Found the following solvers: mosek, mosek_cli
# Replacing directory env
x[:] <= w
GPkit is now installed with solver(s) [u'mosek', u'mosek_cli']
To incorporate new solvers at a later date, run `gpkit.build()`.
If any tests didn't pass, please post the output above
(starting from "Found no installed solvers, beginning a build.")
to gpkit@mit.edu or https://github.com/convexengineering/gpkit/issues/new
so we can prevent others from having these errors.
The same goes for any other bugs you encounter with GPkit:
send 'em our way, along with any interesting models, speculative features,
comments, discussions, or clarifications you feel like sharing.
Finally, we hope you find our documentation (https://gpkit.readthedocs.io/)
and engineering-design models (https://github.com/convexengineering/gplibrary/)
to be useful resources for your own applications.
Enjoy!
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gplibrary']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {})
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
attempt 1
attempt 2
attempt 3
attempt 4
attempt 5
SETTINGS
defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'})
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {})
[Execution node] check if [macys] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
Build step 'Console output (build log) parsing' changed build result to FAILURE
INFO: Starting to record.
INFO: Processing JUnit
INFO: [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/Users/jenkins/workspace/gplibrary_Push_Models/mosek' for the testing framework 'JUnit'.
INFO: Check 'Failed Tests' threshold.
INFO: Check 'Skipped Tests' threshold.
INFO: Setting the build status to FAILURE
INFO: Stopping recording.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: FAILURE