2 4.0e+02 5.1e+02 2.2e+04 -9.35e-01 -1.198179779e+05 1.134152544e+01 1.7e-01 0.15
3 2.8e+02 3.6e+02 1.6e+04 -8.28e-01 -1.157324670e+05 8.423416081e+01 1.2e-01 0.55
4 2.8e+02 3.6e+02 1.6e+04 -7.56e-01 -1.124186829e+05 2.836436851e+03 1.2e-01 0.70
5 6.3e+01 8.2e+01 3.6e+03 -7.47e-01 -6.653512263e+04 1.265850440e+04 2.8e-02 0.77
6 3.9e+01 5.1e+01 2.2e+03 -7.39e-02 -4.844434605e+04 1.112911529e+04 1.7e-02 1.16
7 2.8e+01 3.6e+01 1.6e+03 2.53e-01 -3.796022266e+04 8.631265772e+03 1.2e-02 1.75
8 1.5e+01 2.0e+01 8.6e+02 4.43e-01 -2.324546851e+04 5.309485103e+03 6.8e-03 2.27
9 5.9e+00 7.6e+00 3.3e+02 6.91e-01 -9.448982358e+03 2.651147876e+03 2.6e-03 2.75
10 3.3e+00 4.2e+00 1.8e+02 9.01e-01 -5.020309049e+03 1.803991641e+03 1.5e-03 3.25
11 1.1e+00 1.4e+00 6.3e+01 9.61e-01 -1.685548096e+03 6.933179968e+02 5.0e-04 3.72
12 9.1e-01 1.3e+00 5.2e+01 9.86e-01 -1.368743973e+03 5.972082354e+02 4.1e-04 4.35
13 6.9e-01 1.2e+00 3.9e+01 9.72e-01 -1.052817700e+03 4.579732795e+02 3.1e-04 4.81
14 3.7e-01 6.3e-01 2.1e+01 9.98e-01 -5.484078688e+02 2.640754855e+02 1.7e-04 5.20
15 1.2e-01 2.2e-01 6.7e+00 9.94e-01 -1.704637671e+02 8.550062464e+01 5.4e-05 5.69
16 8.2e-02 1.7e-01 4.8e+00 1.01e+00 -1.180257937e+02 6.425235124e+01 3.9e-05 6.33
17 3.3e-02 1.1e-01 1.9e+00 1.01e+00 -4.285382109e+01 3.068921834e+01 1.6e-05 6.63
18 1.8e-02 8.2e-02 1.1e+00 1.01e+00 -2.020694043e+01 2.029560427e+01 8.7e-06 6.64
19 1.7e-02 7.9e-02 1.0e+00 1.02e+00 -1.893231321e+01 2.022126809e+01 8.5e-06 6.65
20 1.0e-02 6.0e-02 6.2e-01 1.02e+00 -5.882210222e+00 1.716793269e+01 5.0e-06 6.67
21 4.4e-03 6.0e-02 2.6e-01 1.02e+00 4.086967272e+00 1.378686702e+01 2.1e-06 6.68
22 2.2e-03 5.7e-02 1.3e-01 1.01e+00 7.629405382e+00 1.261764404e+01 1.1e-06 6.76
23 6.0e-04 8.3e-02 3.9e-02 9.80e-01 1.031731644e+01 1.179836603e+01 3.4e-07 6.77
24 1.7e-04 8.8e-02 1.2e-02 9.64e-01 1.108842997e+01 1.155999131e+01 1.1e-07 6.84
25 5.7e-05 8.4e-02 4.2e-03 9.80e-01 1.132953813e+01 1.149071928e+01 3.9e-08 6.97
26 2.1e-05 8.3e-02 1.5e-03 9.93e-01 1.141258364e+01 1.147148140e+01 1.4e-08 6.99
27 7.6e-06 8.1e-02 5.7e-04 9.98e-01 1.144298016e+01 1.146497759e+01 5.4e-09 7.00
28 6.8e-06 7.3e-02 5.1e-04 1.00e+00 1.144490439e+01 1.146470388e+01 4.8e-09 7.01
29 6.2e-06 6.7e-02 4.6e-04 1.00e+00 1.144649115e+01 1.146431153e+01 4.3e-09 7.19
30 5.5e-06 6.1e-02 4.1e-04 1.00e+00 1.144791940e+01 1.146395848e+01 3.9e-09 7.37
31 5.0e-06 5.5e-02 3.7e-04 1.00e+00 1.144920223e+01 1.146363794e+01 3.5e-09 7.55
32 4.5e-06 5.0e-02 3.4e-04 1.00e+00 1.145035564e+01 1.146334819e+01 3.2e-09 7.67
33 4.0e-06 4.6e-02 3.0e-04 1.00e+00 1.145139258e+01 1.146308623e+01 2.9e-09 7.79
34 3.6e-06 4.2e-02 2.7e-04 1.00e+00 1.145232495e+01 1.146284947e+01 2.6e-09 7.90
35 3.3e-06 3.9e-02 2.4e-04 1.00e+00 1.145316335e+01 1.146263561e+01 2.3e-09 8.03
36 2.9e-06 3.5e-02 2.2e-04 1.00e+00 1.145391732e+01 1.146244254e+01 2.1e-09 8.08
37 2.7e-06 3.3e-02 2.0e-04 1.00e+00 1.145459544e+01 1.146226828e+01 1.9e-09 8.09
38 2.4e-06 3.0e-02 1.8e-04 1.00e+00 1.145520539e+01 1.146211103e+01 1.7e-09 8.11
39 2.1e-06 2.8e-02 1.6e-04 1.00e+00 1.145575405e+01 1.146196921e+01 1.5e-09 8.12
40 1.9e-06 2.6e-02 1.4e-04 1.00e+00 1.145624762e+01 1.146184134e+01 1.4e-09 8.14
41 1.7e-06 2.4e-02 1.3e-04 1.00e+00 1.145669166e+01 1.146172606e+01 1.2e-09 8.15
42 1.6e-06 2.2e-02 1.2e-04 1.00e+00 1.145709115e+01 1.146162218e+01 1.1e-09 8.17
43 1.4e-06 2.1e-02 1.1e-04 1.00e+00 1.145745059e+01 1.146152855e+01 1.0e-09 8.18
44 1.3e-06 1.9e-02 9.5e-05 1.00e+00 1.145777400e+01 1.146144417e+01 9.0e-10 8.19
45 1.1e-06 1.8e-02 8.5e-05 1.00e+00 1.145806499e+01 1.146136818e+01 8.1e-10 8.20
46 1.0e-06 1.7e-02 7.7e-05 1.00e+00 1.145832685e+01 1.146129967e+01 7.3e-10 8.21
47 9.2e-07 1.6e-02 6.9e-05 1.00e+00 1.145856245e+01 1.146123808e+01 6.5e-10 8.22
48 8.3e-07 1.5e-02 6.2e-05 1.00e+00 1.145877446e+01 1.146118258e+01 5.9e-10 8.24
49 7.5e-07 1.4e-02 5.6e-05 1.00e+00 1.145896525e+01 1.146113259e+01 5.3e-10 8.25
50 6.7e-07 1.3e-02 5.0e-05 1.00e+00 1.145913695e+01 1.146108755e+01 4.8e-10 8.26
51 6.1e-07 1.3e-02 4.5e-05 1.00e+00 1.145929145e+01 1.146104702e+01 4.3e-10 8.28
52 5.5e-07 1.2e-02 4.1e-05 1.00e+00 1.145943051e+01 1.146101048e+01 3.9e-10 8.29
53 4.9e-07 1.2e-02 3.7e-05 1.00e+00 1.145955564e+01 1.146097763e+01 3.5e-10 8.30
54 1.7e-07 4.0e-03 1.3e-05 1.00e+00 1.146029163e+01 1.146078408e+01 1.2e-10 8.31
55 1.5e-07 3.6e-03 1.1e-05 9.92e-01 1.146033082e+01 1.146077423e+01 1.1e-10 8.33
56 5.3e-08 1.2e-03 3.9e-06 1.00e+00 1.146056164e+01 1.146071302e+01 3.7e-11 8.34
57 4.7e-08 1.1e-03 3.5e-06 1.04e+00 1.146057602e+01 1.146070893e+01 3.4e-11 8.35
58 4.3e-08 1.0e-03 3.2e-06 9.92e-01 1.146058652e+01 1.146070617e+01 3.1e-11 8.37
59 2.7e-08 1.1e-04 3.4e-07 9.12e-01 1.146067328e+01 1.146068690e+01 4.5e-12 8.38
60 2.5e-08 9.7e-05 3.1e-07 9.27e-01 1.146067412e+01 1.146068657e+01 4.1e-12 8.39
61 6.9e-09 1.6e-05 5.2e-08 1.11e+00 1.146067960e+01 1.146068148e+01 4.8e-13 8.41
Interior-point optimizer terminated. Time: 8.41.
Optimizer terminated. Time: 8.42
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1460679603e+01 Viol. con: 1e-07 var: 0e+00
Dual. obj: 1.1460681482e+01 Viol. con: 0e+00 var: 1e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 8.45 seconds.
result packing took 2.8% of solve time
solution checking took 0.49% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1012
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1023
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1023
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 830
Optimizer - Cones : 0
Optimizer - Scalar variables : 3579 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.67e+04 after factor : 1.72e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.288303351e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.4e+03 6.0e+04 -9.71e-01 -1.265673728e+05 3.742332983e+00 4.7e-01 0.05
2 3.9e+02 5.0e+02 2.2e+04 -9.35e-01 -1.195102546e+05 1.160401145e+01 1.7e-01 0.06
3 2.8e+02 3.6e+02 1.6e+04 -8.25e-01 -1.156404691e+05 9.624644965e+01 1.2e-01 0.08
4 2.8e+02 3.6e+02 1.6e+04 -7.56e-01 -1.122923407e+05 2.817341291e+03 1.2e-01 0.09
5 7.8e+01 1.0e+02 4.4e+03 -7.46e-01 -7.510775685e+04 1.048210981e+04 3.5e-02 0.10
6 3.8e+01 4.9e+01 2.1e+03 -2.10e-01 -4.735887571e+04 1.109336995e+04 1.7e-02 0.11
7 2.1e+01 2.8e+01 1.2e+03 2.68e-01 -3.058434065e+04 7.169154075e+03 9.4e-03 0.12
8 9.5e+00 1.2e+01 5.4e+02 5.72e-01 -1.502682039e+04 3.817552283e+03 4.2e-03 0.14
9 4.1e+00 5.3e+00 2.3e+02 8.24e-01 -6.410474948e+03 2.056518470e+03 1.8e-03 0.15
10 1.9e+00 2.5e+00 1.1e+02 9.43e-01 -2.868931018e+03 1.160647352e+03 8.6e-04 0.16
11 1.3e+00 1.7e+00 7.3e+01 9.84e-01 -1.948840722e+03 7.929286813e+02 5.8e-04 0.17
12 8.6e-01 1.1e+00 4.9e+01 9.85e-01 -1.300411832e+03 5.479092950e+02 3.9e-04 0.18
13 6.1e-01 9.0e-01 3.5e+01 9.66e-01 -9.312044246e+02 3.904356019e+02 2.8e-04 0.19
14 2.7e-01 4.1e-01 1.6e+01 9.98e-01 -4.042193020e+02 1.896441950e+02 1.2e-04 0.20
15 1.0e-01 1.8e-01 6.0e+00 9.99e-01 -1.511462246e+02 7.778975360e+01 4.8e-05 0.21
16 4.3e-02 1.1e-01 2.5e+00 1.01e+00 -5.987822206e+01 3.694013019e+01 2.1e-05 0.22
17 3.4e-02 9.2e-02 2.0e+00 9.98e-01 -4.521717627e+01 3.102417307e+01 1.6e-05 0.23
18 1.9e-02 7.4e-02 1.1e+00 1.00e+00 -2.102332958e+01 2.060927722e+01 9.0e-06 0.24
19 1.1e-02 5.4e-02 6.6e-01 1.02e+00 -7.720375340e+00 1.707456658e+01 5.4e-06 0.25
20 3.3e-03 8.1e-02 2.0e-01 1.02e+00 5.699061951e+00 1.302376714e+01 1.6e-06 0.26
21 1.9e-03 5.9e-02 1.1e-01 9.98e-01 8.031056494e+00 1.226584052e+01 9.6e-07 0.27
22 5.4e-04 7.7e-02 3.5e-02 9.71e-01 1.029564631e+01 1.164256807e+01 3.1e-07 0.28
23 1.7e-04 7.9e-02 1.2e-02 9.57e-01 1.098502587e+01 1.144335571e+01 1.1e-07 0.29
24 8.7e-05 6.2e-02 6.2e-03 9.72e-01 1.115556290e+01 1.139600781e+01 5.6e-08 0.30
25 4.0e-05 6.0e-02 2.9e-03 9.84e-01 1.126116578e+01 1.137288078e+01 2.6e-08 0.31
26 3.6e-05 5.5e-02 2.6e-03 9.93e-01 1.127276299e+01 1.137336150e+01 2.4e-08 0.32
27 3.2e-05 5.0e-02 2.3e-03 9.93e-01 1.128078465e+01 1.137136195e+01 2.1e-08 0.33
28 2.9e-05 4.6e-02 2.1e-03 9.94e-01 1.128814270e+01 1.136969823e+01 1.9e-08 0.34
29 2.6e-05 4.2e-02 1.9e-03 9.94e-01 1.129473183e+01 1.136816088e+01 1.7e-08 0.36
30 2.3e-05 3.8e-02 1.7e-03 9.95e-01 1.130064678e+01 1.136675695e+01 1.6e-08 0.37
31 2.1e-05 3.5e-02 1.5e-03 9.95e-01 1.130595644e+01 1.136547532e+01 1.4e-08 0.38
32 1.9e-05 3.2e-02 1.4e-03 9.96e-01 1.131072403e+01 1.136430723e+01 1.3e-08 0.39
33 1.7e-05 3.0e-02 1.2e-03 9.96e-01 1.131500568e+01 1.136324388e+01 1.1e-08 0.40
34 1.5e-05 2.8e-02 1.1e-03 9.97e-01 1.131885158e+01 1.136227687e+01 1.0e-08 0.42
35 1.4e-05 2.6e-02 1.0e-03 9.97e-01 1.132230666e+01 1.136139842e+01 9.2e-09 0.43
36 1.2e-05 2.4e-02 9.0e-04 9.97e-01 1.132541113e+01 1.136060108e+01 8.3e-09 0.44
37 1.1e-05 2.2e-02 8.1e-04 9.97e-01 1.132820100e+01 1.135987799e+01 7.4e-09 0.46
38 1.0e-05 2.1e-02 7.3e-04 9.98e-01 1.133070851e+01 1.135922271e+01 6.7e-09 0.47
39 9.1e-06 1.9e-02 6.5e-04 9.98e-01 1.133296253e+01 1.135862937e+01 6.0e-09 0.48
40 8.2e-06 1.8e-02 5.9e-04 9.98e-01 1.133498890e+01 1.135809241e+01 5.4e-09 0.49
41 7.4e-06 1.7e-02 5.3e-04 9.98e-01 1.133681080e+01 1.135760671e+01 4.9e-09 0.50
42 6.6e-06 1.6e-02 4.8e-04 9.98e-01 1.133844900e+01 1.135716757e+01 4.4e-09 0.51
43 6.0e-06 1.5e-02 4.3e-04 9.99e-01 1.133992212e+01 1.135677066e+01 4.0e-09 0.52
44 5.4e-06 1.4e-02 3.9e-04 9.99e-01 1.134124684e+01 1.135641206e+01 3.6e-09 0.53
45 4.8e-06 1.3e-02 3.5e-04 9.99e-01 1.134243816e+01 1.135608811e+01 3.2e-09 0.55
46 4.3e-06 1.3e-02 3.1e-04 9.99e-01 1.134350955e+01 1.135579554e+01 2.9e-09 0.56
47 3.9e-06 1.2e-02 2.8e-04 9.99e-01 1.134447311e+01 1.135553134e+01 2.6e-09 0.57
48 3.5e-06 1.2e-02 2.5e-04 9.99e-01 1.134533973e+01 1.135529286e+01 2.3e-09 0.58
49 3.2e-06 1.1e-02 2.3e-04 9.99e-01 1.134611921e+01 1.135507762e+01 2.1e-09 0.60
50 2.9e-06 1.1e-02 2.1e-04 9.99e-01 1.134682038e+01 1.135488344e+01 1.9e-09 0.61
51 2.6e-06 1.0e-02 1.9e-04 9.99e-01 1.134745115e+01 1.135470830e+01 1.7e-09 0.62
52 2.3e-06 1.0e-02 1.7e-04 9.99e-01 1.134801864e+01 1.135455040e+01 1.5e-09 0.63
53 2.1e-06 9.8e-03 1.5e-04 9.99e-01 1.134852923e+01 1.135440810e+01 1.4e-09 0.64
54 1.9e-06 9.5e-03 1.3e-04 1.00e+00 1.134898867e+01 1.135427986e+01 1.2e-09 0.65
55 1.7e-06 9.2e-03 1.2e-04 1.00e+00 1.134940210e+01 1.135416437e+01 1.1e-09 0.66
56 1.5e-06 9.0e-03 1.1e-04 1.00e+00 1.134977415e+01 1.135406035e+01 1.0e-09 0.67
57 1.4e-06 8.8e-03 9.8e-05 1.00e+00 1.135010897e+01 1.135396668e+01 9.1e-10 0.68
58 1.2e-06 8.6e-03 8.9e-05 1.00e+00 1.135041030e+01 1.135388236e+01 8.2e-10 0.69
59 1.1e-06 8.4e-03 8.0e-05 1.00e+00 1.135068150e+01 1.135380644e+01 7.3e-10 0.70
60 9.9e-07 8.3e-03 7.2e-05 1.00e+00 1.135092559e+01 1.135373809e+01 6.6e-10 0.72
61 8.9e-07 8.1e-03 6.5e-05 1.00e+00 1.135114528e+01 1.135367658e+01 5.9e-10 0.73
62 8.1e-07 8.0e-03 5.8e-05 1.00e+00 1.135134300e+01 1.135362122e+01 5.3e-10 0.74
63 7.2e-07 7.9e-03 5.2e-05 1.00e+00 1.135152097e+01 1.135357141e+01 4.8e-10 0.75
64 6.5e-07 7.8e-03 4.7e-05 1.00e+00 1.135168114e+01 1.135352659e+01 4.3e-10 0.76
65 5.9e-07 7.7e-03 4.2e-05 1.00e+00 1.135182531e+01 1.135348624e+01 3.9e-10 0.77
66 5.3e-07 7.6e-03 3.8e-05 1.00e+00 1.135195508e+01 1.135344991e+01 3.5e-10 0.78
67 4.8e-07 7.6e-03 3.4e-05 1.00e+00 1.135207188e+01 1.135341722e+01 3.2e-10 0.79
68 4.3e-07 7.5e-03 3.1e-05 9.99e-01 1.135217699e+01 1.135338784e+01 2.8e-10 0.81
69 3.9e-07 7.4e-03 2.8e-05 1.00e+00 1.135227160e+01 1.135336139e+01 2.6e-10 0.82
70 3.5e-07 7.4e-03 2.5e-05 1.00e+00 1.135235675e+01 1.135333756e+01 2.3e-10 0.83
71 3.1e-07 7.3e-03 2.3e-05 1.00e+00 1.135243340e+01 1.135331612e+01 2.1e-10 0.84
72 2.8e-07 7.3e-03 2.0e-05 1.00e+00 1.135250238e+01 1.135329682e+01 1.9e-10 0.85
73 2.5e-07 7.2e-03 1.8e-05 1.00e+00 1.135256446e+01 1.135327947e+01 1.7e-10 0.86
74 2.3e-07 7.2e-03 1.6e-05 1.00e+00 1.135262033e+01 1.135326384e+01 1.5e-10 0.87
75 2.0e-07 7.2e-03 1.5e-05 1.00e+00 1.135267062e+01 1.135324978e+01 1.4e-10 0.88
76 1.8e-07 7.1e-03 1.3e-05 9.99e-01 1.135271587e+01 1.135323714e+01 1.2e-10 0.89
77 1.7e-07 7.1e-03 1.2e-05 1.00e+00 1.135275661e+01 1.135322573e+01 1.1e-10 0.90
78 1.5e-07 7.1e-03 1.1e-05 1.00e+00 1.135279327e+01 1.135321547e+01 9.9e-11 0.91
79 1.3e-07 7.0e-03 9.7e-06 1.00e+00 1.135282626e+01 1.135320623e+01 8.9e-11 0.93
80 1.2e-07 7.0e-03 8.7e-06 9.99e-01 1.135285595e+01 1.135319794e+01 8.0e-11 0.94
81 1.1e-07 7.0e-03 7.8e-06 1.00e+00 1.135288267e+01 1.135319046e+01 7.2e-11 0.95
82 9.8e-08 7.0e-03 7.1e-06 1.00e+00 1.135290689e+01 1.135318365e+01 6.5e-11 0.96
83 8.8e-08 7.0e-03 6.4e-06 9.99e-01 1.135292851e+01 1.135317761e+01 5.9e-11 0.97
84 7.9e-08 7.0e-03 5.7e-06 1.00e+00 1.135294798e+01 1.135317215e+01 5.3e-11 0.98
85 7.1e-08 6.9e-03 5.1e-06 1.00e+00 1.135296549e+01 1.135316725e+01 4.7e-11 1.00
86 6.4e-08 6.9e-03 4.6e-06 1.00e+00 1.135298125e+01 1.135316283e+01 4.3e-11 1.01
87 5.8e-08 6.9e-03 4.2e-06 1.00e+00 1.135299546e+01 1.135315885e+01 3.8e-11 1.02
88 5.2e-08 6.9e-03 3.8e-06 1.00e+00 1.135300826e+01 1.135315525e+01 3.5e-11 1.03
89 4.7e-08 6.2e-03 3.4e-06 1.00e+00 1.135301985e+01 1.135315199e+01 3.1e-11 1.04
90 4.2e-08 5.6e-03 3.0e-06 9.99e-01 1.135303017e+01 1.135314911e+01 2.8e-11 1.06
91 3.8e-08 5.0e-03 2.7e-06 1.00e+00 1.135303948e+01 1.135314649e+01 2.5e-11 1.07
92 3.4e-08 4.5e-03 2.5e-06 1.00e+00 1.135304789e+01 1.135314413e+01 2.3e-11 1.08
93 3.1e-08 4.1e-03 2.2e-06 9.95e-01 1.135305541e+01 1.135314204e+01 2.0e-11 1.09
94 2.8e-08 3.7e-03 2.0e-06 1.00e+00 1.135306221e+01 1.135314013e+01 1.8e-11 1.10
95 2.5e-08 3.3e-03 1.8e-06 1.00e+00 1.135306838e+01 1.135313839e+01 1.7e-11 1.11
96 2.2e-08 3.0e-03 1.6e-06 1.00e+00 1.135307385e+01 1.135313685e+01 1.5e-11 1.12
97 2.0e-08 2.7e-03 1.5e-06 1.00e+00 1.135307877e+01 1.135313547e+01 1.3e-11 1.13
98 1.8e-08 2.4e-03 1.3e-06 9.98e-01 1.135308320e+01 1.135313424e+01 1.2e-11 1.14
99 1.6e-08 2.2e-03 1.2e-06 9.94e-01 1.135308718e+01 1.135313313e+01 1.1e-11 1.15
100 1.5e-08 2.0e-03 1.1e-06 9.87e-01 1.135309076e+01 1.135313214e+01 9.8e-12 1.16
101 1.3e-08 1.8e-03 9.5e-07 9.76e-01 1.135309398e+01 1.135313127e+01 8.8e-12 1.17
102 1.2e-08 1.6e-03 8.6e-07 1.00e+00 1.135309692e+01 1.135313043e+01 8.0e-12 1.18
103 1.1e-08 1.4e-03 7.7e-07 1.00e+00 1.135309957e+01 1.135312968e+01 7.2e-12 1.19
104 9.6e-09 1.3e-03 7.0e-07 1.00e+00 1.135310196e+01 1.135312900e+01 6.5e-12 1.20
105 1.7e-09 1.3e-04 7.2e-08 9.85e-01 1.135312093e+01 1.135312376e+01 7.1e-13 1.22
Interior-point optimizer terminated. Time: 1.22.
Optimizer terminated. Time: 1.23
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1353120934e+01 Viol. con: 3e-08 var: 0e+00
Dual. obj: 1.1353123755e+01 Viol. con: 0e+00 var: 1e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.24 seconds.
result packing took 12% of solve time
solution checking took 3.4% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : MACOSX/64-X86
Cores : 4
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1010
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1022
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1022
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.01
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 831
Optimizer - Cones : 0
Optimizer - Scalar variables : 3581 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.02 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.02
Factor - nonzeros before factor : 1.67e+04 after factor : 1.72e+05
Factor - dense dim. : 0 flops : 0.00e+00
Factor - GP saved nzs : 0 GP saved flops : 0.00e+00
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+03 3.0e+03 1.3e+05 0.00e+00 -1.288985034e+05 2.000000000e+00 1.0e+00 0.04
1 1.1e+03 1.4e+03 6.0e+04 -9.71e-01 -1.266282944e+05 3.737426691e+00 4.7e-01 0.05
2 3.8e+02 4.9e+02 2.1e+04 -9.35e-01 -1.194486041e+05 1.174191101e+01 1.7e-01 0.06
3 2.8e+02 3.6e+02 1.6e+04 -8.23e-01 -1.156781632e+05 1.085339377e+02 1.2e-01 0.07
4 2.8e+02 3.6e+02 1.5e+04 -7.56e-01 -1.122806824e+05 2.801484603e+03 1.2e-01 0.08
5 7.6e+01 9.7e+01 4.2e+03 -7.45e-01 -7.365219700e+04 1.085717423e+04 3.3e-02 0.09
6 3.6e+01 4.7e+01 2.0e+03 -1.87e-01 -4.561204813e+04 1.110550275e+04 1.6e-02 0.10
7 2.0e+01 2.6e+01 1.1e+03 3.00e-01 -2.892814856e+04 7.177331070e+03 8.9e-03 0.11
8 9.6e+00 1.2e+01 5.4e+02 6.00e-01 -1.510736245e+04 3.892361122e+03 4.3e-03 0.12
9 4.3e+00 5.6e+00 2.4e+02 8.25e-01 -6.842384844e+03 2.132585795e+03 1.9e-03 0.13
10 1.6e+00 2.1e+00.
----------------------------------------------------------------------
Ran 1 test in 40.534s
OK
Generating XML reports...
8.8e+01 9.39e-01 -2.339529261e+03 9.782558027e+02 7.0e-04 0.14
11 1.1e+00 1.5e+00 6.3e+01 9.89e-01 -1.684012552e+03 7.027895004e+02 5.1e-04 0.16
12 7.6e-01 9.9e-01 4.3e+01 9.84e-01 -1.147570987e+03 4.848956762e+02 3.4e-04 0.17
13 5.9e-01 7.8e-01 3.4e+01 9.85e-01 -8.859756441e+02 3.927306362e+02 2.7e-04 0.18
14 2.2e-01 2.9e-01 1.2e+01 9.88e-01 -3.278709583e+02 1.435115220e+02 9.9e-05 0.19
15 9.0e-02 1.4e-01 5.2e+00 1.01e+00 -1.297892977e+02 6.742676684e+01 4.2e-05 0.21
16 3.5e-02 1.0e-01 2.1e+00 1.00e+00 -4.773566858e+01 3.088091974e+01 1.7e-05 0.22
17 2.9e-02 8.5e-02 1.7e+00 9.96e-01 -3.728117696e+01 2.759537478e+01 1.4e-05 0.23
18 1.8e-02 6.6e-02 1.1e+00 1.01e+00 -1.941564065e+01 2.038451219e+01 8.6e-06 0.24
19 1.5e-02 5.8e-02 9.1e-01 1.02e+00 -1.489369004e+01 1.923866537e+01 7.4e-06 0.26
20 5.6e-03 6.6e-02 3.3e-01 1.02e+00 1.832457387e+00 1.412847305e+01 2.7e-06 0.27
21 1.9e-03 7.7e-02 1.2e-01 1.02e+00 8.069997183e+00 1.234740762e+01 1.0e-06 0.28
22 1.4e-03 5.9e-02 8.5e-02 9.65e-01 8.871363650e+00 1.204757354e+01 7.4e-07 0.29
23 4.9e-04 6.6e-02 3.2e-02 9.60e-01 1.038315619e+01 1.161090172e+01 2.9e-07 0.31
24 1.9e-04 6.2e-02 1.3e-02 9.58e-01 1.092696305e+01 1.143054927e+01 1.2e-07 0.32
25 1.7e-04 5.6e-02 1.2e-02 9.76e-01 1.096496881e+01 1.141800367e+01 1.1e-07 0.34
26 1.6e-04 5.1e-02 1.1e-02 9.74e-01 1.099986846e+01 1.140813333e+01 9.5e-08 0.35
27 1.4e-04 4.7e-02 9.5e-03 9.76e-01 1.103389579e+01 1.140187355e+01 8.6e-08 0.36
28 1.3e-04 4.3e-02 8.6e-03 9.78e-01 1.106463423e+01 1.139627853e+01 7.7e-08 0.38
29 1.1e-04 3.9e-02 7.7e-03 9.80e-01 1.109230507e+01 1.139117304e+01 7.0e-08 0.39
30 1.0e-04 3.6e-02 7.0e-03 9.81e-01 1.111715892e+01 1.138646212e+01 6.3e-08 0.41
31 9.2e-05 3.3e-02 6.3e-03 9.83e-01 1.113947419e+01 1.138211386e+01 5.6e-08 0.42
32 8.3e-05 3.0e-02 5.6e-03 9.85e-01 1.115950397e+01 1.137810042e+01 5.1e-08 0.43
33 7.5e-05 2.8e-02 5.1e-03 9.86e-01 1.117747832e+01 1.137439760e+01 4.6e-08 0.45
34 6.7e-05 2.6e-02 4.6e-03 9.87e-01 1.119360528e+01 1.137098328e+01 4.1e-08 0.46
35 6.1e-05 2.4e-02 4.1e-03 9.88e-01 1.120807312e+01 1.136783750e+01 3.7e-08 0.47
36 5.5e-05 2.2e-02 3.7e-03 9.90e-01 1.122105182e+01 1.136494206e+01 3.3e-08 0.49
37 4.9e-05 2.1e-02 3.3e-03 9.90e-01 1.123269437e+01 1.136227977e+01 3.0e-08 0.50
38 4.4e-05 1.9e-02 3.0e-03 9.91e-01 1.124313850e+01 1.135983457e+01 2.7e-08 0.51
39 4.0e-05 1.8e-02 2.7e-03 9.92e-01 1.125250777e+01 1.135759103e+01 2.4e-08 0.52
40 3.6e-05 1.7e-02 2.4e-03 9.93e-01 1.126091310e+01 1.135553461e+01 2.2e-08 0.54
41 3.2e-05 1.6e-02 2.2e-03 9.94e-01 1.126845392e+01 1.135365143e+01 2.0e-08 0.55
42 2.9e-05 1.5e-02 2.0e-03 9.94e-01 1.127521955e+01 1.135192856e+01 1.8e-08 0.56
43 2.6e-05 1.4e-02 1.8e-03 9.95e-01 1.128129021e+01 1.135035388e+01 1.6e-08 0.58
44 2.3e-05 1.4e-02 1.6e-03 9.95e-01 1.128673809e+01 1.134891628e+01 1.4e-08 0.59
45 2.1e-05 1.3e-02 1.4e-03 9.96e-01 1.129162798e+01 1.134760547e+01 1.3e-08 0.60
46 1.9e-05 1.2e-02 1.3e-03 9.96e-01 1.129601779e+01 1.134641152e+01 1.2e-08 0.62
47 1.7e-05 1.2e-02 1.2e-03 9.97e-01 1.129995936e+01 1.134532511e+01 1.1e-08 0.63
48 1.5e-05 1.1e-02 1.0e-03 9.97e-01 1.130349904e+01 1.134433749e+01 9.5e-09 0.64
49 1.4e-05 1.1e-02 9.4e-04 9.97e-01 1.130667832e+01 1.134344049e+01 8.5e-09 0.65
50 1.2e-05 1.1e-02 8.5e-04 9.98e-01 1.130953432e+01 1.134262646e+01 7.7e-09 0.66
51 1.1e-05 1.0e-02 7.6e-04 9.98e-01 1.131210029e+01 1.134188822e+01 6.9e-09 0.67
52 1.0e-05 1.0e-02 6.9e-04 9.98e-01 1.131440600e+01 1.134121924e+01 6.2e-09 0.69
53 9.1e-06 9.7e-03 6.2e-04 9.98e-01 1.131647809e+01 1.134061332e+01 5.6e-09 0.70
54 8.2e-06 9.5e-03 5.6e-04 9.98e-01 1.131834042e+01 1.134006487e+01 5.0e-09 0.71
55 7.4e-06 9.2e-03 5.0e-04 9.99e-01 1.132001439e+01 1.133956858e+01 4.5e-09 0.72
56 6.6e-06 9.0e-03 4.5e-04 9.99e-01 1.132151916e+01 1.133911968e+01 4.1e-09 0.73
57 6.0e-06 8.8e-03 4.1e-04 9.99e-01 1.132287191e+01 1.133871384e+01 3.7e-09 0.74
58 5.4e-06 8.7e-03 3.7e-04 9.99e-01 1.132408804e+01 1.133834698e+01 3.3e-09 0.75
59 4.8e-06 8.5e-03 3.3e-04 9.99e-01 1.132518140e+01 1.133801538e+01 3.0e-09 0.76
60 4.3e-06 8.4e-03 3.0e-04 9.99e-01 1.132616443e+01 1.133771582e+01 2.7e-09 0.77
61 3.9e-06 8.2e-03 2.7e-04 9.99e-01 1.132704830e+01 1.133744521e+01 2.4e-09 0.78
62 3.5e-06 8.1e-03 2.4e-04 9.99e-01 1.132784307e+01 1.133720082e+01 2.2e-09 0.79
63 3.2e-06 8.0e-03 2.2e-04 1.00e+00 1.132855780e+01 1.133698019e+01 1.9e-09 0.80
64 2.9e-06 7.9e-03 1.9e-04 1.00e+00 1.132920060e+01 1.133678109e+01 1.8e-09 0.82
65 2.6e-06 7.8e-03 1.7e-04 1.00e+00 1.132977876e+01 1.133660150e+01 1.6e-09 0.83
66 2.3e-06 7.8e-03 1.6e-04 1.00e+00 1.133029883e+01 1.133643955e+01 1.4e-09 0.84
67 2.1e-06 7.7e-03 1.4e-04 1.00e+00 1.133076669e+01 1.133629356e+01 1.3e-09 0.85
68 1.9e-06 7.6e-03 1.3e-04 1.00e+00 1.133118761e+01 1.133616199e+01 1.2e-09 0.86
69 1.7e-06 7.6e-03 1.1e-04 1.00e+00 1.133156632e+01 1.133604344e+01 1.0e-09 0.87
70 1.5e-06 7.5e-03 1.0e-04 1.00e+00 1.133190707e+01 1.133593662e+01 9.3e-10 0.88
71 1.4e-06 7.4e-03 9.3e-05 1.00e+00 1.133221368e+01 1.133584041e+01 8.4e-10 0.89
72 1.2e-06 7.4e-03 8.4e-05 1.00e+00 1.133248958e+01 1.133575373e+01 7.6e-10 0.90
73 1.1e-06 7.4e-03 7.5e-05 1.00e+00 1.133273788e+01 1.133567560e+01 6.8e-10 0.91
74 9.9e-07 7.3e-03 6.8e-05 1.00e+00 1.133296131e+01 1.133560524e+01 6.1e-10 0.93
75 9.0e-07 7.3e-03 6.1e-05 9.99e-01 1.133316235e+01 1.133554198e+01 5.5e-10 0.94
76 8.1e-07 7.3e-03 5.5e-05 1.00e+00 1.133334328e+01 1.133548498e+01 5.0e-10 0.95
77 7.3e-07 7.2e-03 4.9e-05 1.00e+00 1.133350609e+01 1.133543367e+01 4.5e-10 0.96
78 6.5e-07 7.2e-03 4.4e-05 1.00e+00 1.133365262e+01 1.133538747e+01 4.0e-10 0.97
79 5.9e-07 7.2e-03 4.0e-05 1.00e+00 1.133378448e+01 1.133534589e+01 3.6e-10 0.98
80 5.3e-07 7.1e-03 3.6e-05 1.00e+00 1.133390315e+01 1.133530840e+01 3.3e-10 0.99
81 4.8e-07 7.1e-03 3.2e-05 1.00e+00 1.133400995e+01 1.133527467e+01 2.9e-10 1.00
82 4.3e-07 7.1e-03 2.9e-05 1.00e+00 1.133410605e+01 1.133524433e+01 2.6e-10 1.01
83 3.9e-07 7.1e-03 2.6e-05 1.00e+00 1.133419254e+01 1.133521700e+01 2.4e-10 1.02
84 3.5e-07 7.1e-03 2.4e-05 1.00e+00 1.133427037e+01 1.133519240e+01 2.1e-10 1.03
85 3.1e-07 7.0e-03 2.1e-05 1.00e+00 1.133434043e+01 1.133517022e+01 1.9e-10 1.04
86 2.8e-07 7.0e-03 1.9e-05 1.00e+00 1.133440347e+01 1.133515029e+01 1.7e-10 1.05
87 2.5e-07 7.0e-03 1.7e-05 1.00e+00 1.133446020e+01 1.133513233e+01 1.6e-10 1.06
88 2.3e-07 6.3e-03 1.5e-05 1.00e+00 1.133451157e+01 1.133511599e+01 1.4e-10 1.07
89 2.0e-07 5.7e-03 1.4e-05 9.99e-01 1.133455748e+01 1.133510149e+01 1.3e-10 1.09
90 1.8e-07 5.1e-03 1.3e-05 9.99e-01 1.133459879e+01 1.133508843e+01 1.1e-10 1.10
91 1.7e-07 4.6e-03 1.1e-05 1.00e+00 1.133463598e+01 1.133507664e+01 1.0e-10 1.11
92 1.5e-07 4.1e-03 1.0e-05 1.00e+00 1.133466944e+01 1.133506604e+01 9.2e-11 1.12
93 1.3e-07 3.7e-03 9.1e-06 1.00e+00 1.133469970e+01 1.133505641e+01 8.3e-11 1.14
94 1.2e-07 3.4e-03 8.2e-06 1.00e+00 1.133472679e+01 1.133504781e+01 7.5e-11 1.15
95 1.1e-07 3.0e-03 7.4e-06 1.01e+00 1.133475168e+01 1.133503986e+01 6.7e-11 1.16
96 9.8e-08 2.7e-03 6.7e-06 1.00e+00 1.133477356e+01 1.133503291e+01 6.0e-11 1.17
97 8.8e-08 2.4e-03 6.0e-06 1.00e+00 1.133479326e+01 1.133502666e+01 5.4e-11 1.18
98 7.9e-08 2.2e-03 5.4e-06 1.00e+00 1.133481103e+01 1.133502101e+01 4.9e-11 1.19
99 7.1e-08 2.0e-03 4.9e-06 9.99e-01 1.133482697e+01 1.133501597e+01 4.4e-11 1.21
100 6.4e-08 1.8e-03 4.4e-06 1.01e+00 1.133484160e+01 1.133501129e+01 4.0e-11 1.22
101 5.8e-08 1.6e-03 3.9e-06 9.94e-01 1.133485447e+01 1.133500724e+01 3.6e-11 1.23
102 5.2e-08 1.4e-03 3.5e-06 9.95e-01 1.133486606e+01 1.133500359e+01 3.2e-11 1.24
103 4.7e-08 1.3e-03 3.2e-06 1.01e+00 1.133487701e+01 1.133500006e+01 2.9e-11 1.25
104 4.2e-08 1.2e-03 2.9e-06 1.01e+00 1.133488652e+01 1.133499702e+01 2.6e-11 1.26
105 3.8e-08 1.1e-03 2.6e-06 1.00e+00 1.133489503e+01 1.133499431e+01 2.4e-11 1.27
106 3.4e-08 9.5e-04 2.3e-06 1.00e+00 1.133490263e+01 1.133499189e+01 2.1e-11 1.28
107 3.1e-08 8.5e-04 2.1e-06 9.99e-01 1.133490940e+01 1.133498974e+01 1.9e-11 1.29
108 2.8e-08 7.7e-04 1.9e-06 9.92e-01 1.133491550e+01 1.133498783e+01 1.7e-11 1.30
109 2.5e-08 6.9e-04 1.7e-06 1.01e+00 1.133492120e+01 1.133498600e+01 1.6e-11 1.31
110 5.1e-09 1.3e-04 3.2e-07 9.93e-01 1.133496107e+01 1.133497345e+01 3.0e-12 1.33
111 3.7e-10 7.3e-06 1.8e-08 9.90e-01 1.133496988e+01 1.133497058e+01 1.8e-13 1.34
Interior-point optimizer terminated. Time: 1.34.
Optimizer terminated. Time: 1.35
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1334969879e+01 Viol. con: 7e-09 var: 0e+00
Dual. obj: 1.1334970575e+01 Viol. con: 0e+00 var: 6e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.37 seconds.
result packing took 14% of solve time
solution checking took 4.7% of solve time
Solving took 6 GP solves and 33.7 seconds.
Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2418946.53881 force_pound * meter but the right hand side evaluated to 2375461.28989 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%)
Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.3818423 force_pound but the right hand side evaluated to 32399.9999977 force_pound (Allowable error: 0.1%, Actual error: 1.2%)
Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116791 meter but the right hand side evaluated to 2.08160550576 meter (Allowable error: 0.1%, Actual error: 6%)
Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1243582.22235 joule / kilogram but the right hand side evaluated to 1.56115513569 megajoule / kilogram (Allowable error: 0.1%, Actual error: 12%)
Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 664761.587283 joule / kilogram but the right hand side evaluated to 0.667340387706 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.17%)
Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.399891873 meter but the right hand side evaluated to 16.322891803 meter (Allowable error: 0.1%, Actual error: 13%)
Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.903627206914813 but the right hand side evaluated to 4.788859035560741 (Allowable error: 0.1%, Actual error: 56%)
Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.019810392174843 but the right hand side evaluated to 4.788859025113859 (Allowable error: 0.1%, Actual error: 52%)
Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.14491099052252 but the right hand side evaluated to 4.788859038093812 (Allowable error: 0.1%, Actual error: 41%)
Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.3622351786 meter but the right hand side evaluated to 18.1377245919 meter (Allowable error: 0.1%, Actual error: 1.2%)
Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3622351786 meter but the right hand side evaluated to 18.242060269 meter (Allowable error: 0.1%, Actual error: 0.65%)
Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.29603434839584697 but the right hand side evaluated to 0.18973871788830335 (Allowable error: 0.1%, Actual error: 2.2%)
Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23301948093763514 but the right hand side evaluated to 0.17434607893885992 (Allowable error: 0.1%, Actual error: 1.2%)
Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.563249916214875 but the right hand side evaluated to 4.730640188876133 (Allowable error: 0.1%, Actual error: 37%)
Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.583099947070909 but the right hand side evaluated to 4.757852783521045 (Allowable error: 0.1%, Actual error: 37%)
Solves with these variables bounded:
value near lower bound: CruiseAlt_Mission
value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission
Cloning into 'solar'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0)
Collecting git+https://github.com/convexengineering/gpfit.git
Cloning https://github.com/convexengineering/gpfit.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-QHYkPi
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
Running setup.py bdist_wheel for gpfit: started
Running setup.py bdist_wheel for gpfit: finished with status 'done'
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-kpcxxt/wheels/d5/94/ac/b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
Collecting git+https://github.com/convexengineering/gassolar.git
Cloning https://github.com/convexengineering/gassolar.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-qpu0Np
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2018.4)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.7.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0)
Building wheels for collected packages: gassolar
Running setup.py bdist_wheel for gassolar: started
Running setup.py bdist_wheel for gassolar: finished with status 'done'
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-JNR5uQ/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/solar
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in /Users/jenkins/workspace/gplibrary_PR_Models/mosek (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2018.4)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2.7.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.11.0)
Building wheels for collected packages: solar
Running setup.py bdist_wheel for solar: started
Running setup.py bdist_wheel for solar: finished with status 'done'
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-9RTTfD/wheels/1f/1c/61/aec93436439dcd4a965e159a026d3a7ed265e591b64e6d6bfc
Successfully built solar
Installing collected packages: solar
Successfully installed solar-0.0.0.0
Running tests...
----------------------------------------------------------------------
../Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
tau = np.exp(-0.175/costhsun)
/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
tau = np.exp(-0.175/costhsun)
adding test for 'solar/solar.py'
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
adding test for 'solar/npod_trade.py'
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 9 GP solves and 3.03 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0624 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1388463.0666 but bound is 600000.0000
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1248776.3286 but bound is 1000000.0000
Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 82150.9611 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.29645501011 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194399 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 9 GP solves and 3.09 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0624 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1388463.0656 but bound is 600000.0000
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1248776.3277 but bound is 1000000.0000
Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 82150.9611 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.29645501012 meter ** 2 / second ** 2 but the right hand side evaluated to 2.296451944 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.11 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2510 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 765970.5631 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.65/GustL.65_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.49/GustL.49_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.58/GustL.58_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.69/GustL.69_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.46/GustL.46_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.71/GustL.71_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.78/GustL.78_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.48/GustL.48_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.52/GustL.52_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.75/GustL.75_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.40/GustL.40_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.59/GustL.59_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.64/GustL.64_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.66/GustL.66_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.67/GustL.67_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.44/GustL.44_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.55/GustL.55_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.54/GustL.54_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.53/GustL.53_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.62/GustL.62_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.60/GustL.60_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.51/GustL.51_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.41/GustL.41_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.47/GustL.47_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.70/GustL.70_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.50/GustL.50_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.74/GustL.74_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.68/GustL.68_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.76/GustL.76_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.79/GustL.79_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.63/GustL.63_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.77/GustL.77_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.56/GustL.56_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.57/GustL.57_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.42/GustL.42_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.61/GustL.61_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.45/GustL.45_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.43/GustL.43_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.72/GustL.72_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.73/GustL.73_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 1.97 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1911 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 862671.9761 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.90/GustL.90_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.118/GustL.118_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.119/GustL.119_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.104/GustL.104_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.102/GustL.102_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.93/GustL.93_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.105/GustL.105_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.85/GustL.85_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.106/GustL.106_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.117/GustL.117_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.91/GustL.91_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.109/GustL.109_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.116/GustL.116_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.114/GustL.114_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.96/GustL.96_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.101/GustL.101_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.87/GustL.87_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.100/GustL.100_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.99/GustL.99_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.88/GustL.88_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.98/GustL.98_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.113/GustL.113_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.89/GustL.89_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.81/GustL.81_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.95/GustL.95_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.107/GustL.107_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.94/GustL.94_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.115/GustL.115_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.110/GustL.110_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.84/GustL.84_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.82/GustL.82_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.83/GustL.83_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.97/GustL.97_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.112/GustL.112_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.86/GustL.86_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.92/GustL.92_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.111/GustL.111_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.103/GustL.103_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.108/GustL.108_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.80/GustL.80_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 1.87 seconds.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1202 but bound is 0.9465
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 987087.2996 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 6269 variables.
Solving took 0.821 seconds.
Warning: Va.riable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.0863 but bound is 0.9465
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1058302.4686 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.03 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2510 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 765970.5422 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.65/GustL.65_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.49/GustL.49_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.58/GustL.58_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.69/GustL.69_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.46/GustL.46_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.71/GustL.71_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.78/GustL.78_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.48/GustL.48_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.52/GustL.52_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.75/GustL.75_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.40/GustL.40_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.59/GustL.59_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.64/GustL.64_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.66/GustL.66_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.67/GustL.67_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.44/GustL.44_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.55/GustL.55_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.54/GustL.54_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.53/GustL.53_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.62/GustL.62_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.60/GustL.60_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.51/GustL.51_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.41/GustL.41_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.47/GustL.47_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.70/GustL.70_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.50/GustL.50_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.74/GustL.74_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.68/GustL.68_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.76/GustL.76_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.79/GustL.79_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.63/GustL.63_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.77/GustL.77_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.56/GustL.56_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.57/GustL.57_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.42/GustL.42_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.61/GustL.61_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.45/GustL.45_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.43/GustL.43_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSeg..ment.72/GustL.72_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.73/GustL.73_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 1.98 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1911 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 862671.9718 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.90/GustL.90_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.118/GustL.118_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.119/GustL.119_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.104/GustL.104_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.102/GustL.102_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.93/GustL.93_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.105/GustL.105_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.85/GustL.85_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.106/GustL.106_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.117/GustL.117_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.91/GustL.91_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.109/GustL.109_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.116/GustL.116_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.114/GustL.114_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.96/GustL.96_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.101/GustL.101_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.87/GustL.87_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.100/GustL.100_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.99/GustL.99_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.88/GustL.88_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.98/GustL.98_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.113/GustL.113_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.89/GustL.89_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.81/GustL.81_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.95/GustL.95_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.107/GustL.107_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.94/GustL.94_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.115/GustL.115_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.110/GustL.110_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.84/GustL.84_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.82/GustL.82_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.83/GustL.83_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.97/GustL.97_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.112/GustL.112_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.86/GustL.86_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.92/GustL.92_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.111/GustL.111_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.103/GustL.103_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.108/GustL.108_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.80/GustL.80_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 1.96 seconds.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1202 but bound is 0.9465
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 987087.2997 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 6269 variables.
Solving took 0.889 seconds.
Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.0863 but bound is 0.9465
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1058302.4687 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 9 GP solves and 2.52 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0624 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1388463.0468 but bound is 600000.0000
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1248776.3107 but bound is 1000000.0000
Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 82150.9611 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.29645500982 meter ** 2 / second ** 2 but the right hand side evaluated to 2.2964519437 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 9 GP solves and 2.63 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0624 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1388463.0656 but bound is 600000.0000
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above uppe.EE
======================================================================
ERROR [9.354s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn
mod.test()
File "solar.py", line 654, in test
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 61, in __init__
cs = self.setup(*args, **kwargs) # pylint: disable=no-member
File "solar.py", line 633, in setup
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 83, in __init__
CostedConstraintSet.__init__(self, cost, constraints, substitutions)
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/costed.py", line 21, in __init__
ConstraintSet.__init__(self, constraints, subs)
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 58, in __init__
list.__setitem__(self, i, ConstraintSet(constraint))
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 67, in __init__
raise_elementhasnumpybools(constraint)
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 357, in raise_elementhasnumpybools
% (cause, constraint))
ValueError: An ArrayConstraint was created with elements of numpy.bool_
Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]
======================================================================
ERROR [7.830s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
testfn(name, import_dict, path)(self)
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn
mod.test()
File "solar.py", line 654, in test
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 61, in __init__
cs = self.setup(*args, **kwargs) # pylint: disable=no-member
File "solar.py", line 633, in setup
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 83, in __init__
CostedConstraintSet.__init__(self, cost, constraints, substitutions)
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/costed.py", line 21, in __init__
ConstraintSet.__init__(self, constraints, subs)
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 58, in __init__
list.__setitem__(self, i, ConstraintSet(constraint))
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 67, in __init__
raise_elementhasnumpybools(constraint)
File "/Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 357, in raise_elementhasnumpybools
% (cause, constraint))
ValueError: An ArrayConstraint was created with elements of numpy.bool_
Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]
----------------------------------------------------------------------
Ran 8 tests in 230.435s
FAILED (errors=2)
Generating XML reports...
r bound. Solution is 1248776.3277 but bound is 1000000.0000
Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 82150.9611 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.29645501013 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194401 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 702 variables.
Solving took 0.102 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1958 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 838075.6758 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.1/GustL.1_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 8 GP solves and 2.51 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.1418 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1017215.9282 but bound is 600000.0000
Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,), could cause inaccurate result because it is below lower bound. Solution is 78650.4124 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 2.62125883016 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124747931 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00043%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(1... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.95293542206 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215297 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00068%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.04275941611 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521706 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0004%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(3... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.467698134216 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697003878 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00024%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(4... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.139006791927 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006573773 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek_cli'
Solving for 702 variables.
Solving took 0.283 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1958 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 838072.5912 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.1/GustL.1_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 8 GP solves and 3.98 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.1418 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1017215.9574 but bound is 600000.0000
Warning: Constraint [dQ_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2,) [N... >= B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2,)*G_M...] is not tight because the left hand side evaluated to 0.546199983583 meter * newton but the right hand side evaluated to 0.54619937481 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,), could cause inaccurate result because it is below lower bound. Solution is 78650.5577 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 2.62125881924 meter ** 2 / second ** 2 but the right hand side evaluated to 2.6212478085 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00042%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(1... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.9529359766 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292347375 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00064%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.04275932764 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275522741 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00039%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(3... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.467698058867 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697044815 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00022%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(4... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.13900678254 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006562766 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: pytz>=2011k in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: numpy>=1.9.0 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3)
Requirement already satisfied: python-dateutil in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: six>=1.5 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0)
Collecting git+https://github.com/hoburg/gpfit.git
Cloning https://github.com/hoburg/gpfit.git to /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-req-build-0Zl0bo
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
Running setup.py bdist_wheel for gpfit: started
Running setup.py bdist_wheel for gpfit: finished with status 'done'
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-luC0JM/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
Processing /Users/jenkins/workspace/gplibrary_PR_Models/mosek/gplibrary
Requirement already satisfied: numpy>=1.12 in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in /Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.8.1)
Building wheels for collected packages: gpkitmodels
Running setup.py bdist_wheel for gpkitmodels: started
Running setup.py bdist_wheel for gpkitmodels: finished with status 'done'
Stored in directory: /private/var/folders/42/s1whb7rd4mddfcnzk96g_d9h0000gp/T/pip-ephem-wheel-cache-GKzTku/wheels/89/83/63/5c5e519ca7ad1fa93cf087f53642d88b5b0eb066ca83d4bb19
Successfully built gpkitmodels
Installing collected packages: gpkitmodels
Found existing installation: gpkitmodels 0.0.0.0
Uninstalling gpkitmodels-0.0.0.0:
Successfully uninstalled gpkitmodels-0.0.0.0
Successfully installed gpkitmodels-0.0.0.0
Running tests...
----------------------------------------------------------------------
..........
----------------------------------------------------------------------
Ran 10 tests in 16.905s
OK
Generating XML reports...
adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py'
adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py'
adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py'
adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py'
adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.0118 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.236 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.0104 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.00995 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.00994 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 1.55 seconds.
Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006556021 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%)
Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544371544 meter * revolutions_per_minute but the right hand side evaluated to 103.041409433 meter / second (Allowable error: 0.0001%, Actual error: 0.16%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585925008 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573144948 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.003%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.314645033972 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629895209 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0048%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.168936438411 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931603976 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0639642380885 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631380009 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0017%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226356535443 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354005891 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)
Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.228 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.268 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.234 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 4.91 seconds.
Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006568341 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%)
Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544539109 meter * revolutions_per_minute but the right hand side evaluated to 103.041408191 meter / second (Allowable error: 0.0001%, Actual error: 0.16%)
Warning: Constraint [dQ_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [N*m]... >= B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement_...] is not tight because the left hand side evaluated to 74.5041627751 meter * newton but the right hand side evaluated to 74.5040725471 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%)
Warning: Constraint [-B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement... >= dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [lbf]...] is not tight because the left hand side evaluated to 134.449579759 kilogram * meter / second ** 2 but the right hand side evaluated to 30.2255018449 force_pound (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585903433 meter ** 2 / second ** 2 but the right hand side evaluated to 0.42057303321 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0031%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.314644998908 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629685653 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0049%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.16893640237 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931506563 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.063964051843 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639630073546 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0016%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226356673111 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226353930664 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0012%)
Using solver 'mosek'
Solving for 13 variables.
Solving took 0.0105 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 1.04 seconds.
Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619897.4122 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.235 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 3.34 seconds.
Warning: Constraint [omega_BladeElementProp/BladeElementPerf_(0,)*r_BladeElementProp/BladeElementPerf_(0,) [m*rpm]... >= Wt_BladeElementProp/BladeElementPerf_(0,) + vt_BladeElementProp/BladeElementPerf_(0,) [m/s]...] is not tight because the left hand side evaluated to 147.268875342 meter * revolutions_per_minute but the right hand side evaluated to 15.4219435408 meter / second (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Constraint [dQ_BladeElementProp/BladeElementPerf_(3,) [N*m]... >= B_BladeElementProp/BladeElementPerf_(3,)*G_BladeElementProp/BladeElementPerf_(3,)*Wa_BladeElementPro...] is not tight because the left hand side evaluated to 42.7884411703 meter * newton but the right hand side evaluated to 42.7884887635 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3481 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9721 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3856 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9562 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.2729 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.1579 but bound is 700000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Cloning into 'eVTOL'...
Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 1.381s
OK
Generating XML reports...
adding test for 'aircraft_models.py'
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {})
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'})
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'})
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['python', '/Users/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {})
[Execution node] check if [macys_VM] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
Build step 'Console output (build log) parsing' changed build result to FAILURE
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/Users/jenkins/workspace/gplibrary_PR_Models/mosek' for the testing framework 'JUnit'.
[xUnit] [INFO] - Check 'Failed Tests' threshold.
[xUnit] [INFO] - Check 'Skipped Tests' threshold.
[xUnit] [INFO] - Setting the build status to FAILURE
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: FAILURE
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