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 -1.289101987e+05 2.000000000e+00 1.0e+00 0.05
1 1.1e+03 1.4e+03 5.9e+04 -9.71e-01 -1.266148482e+05 3.779171610e+00 4.6e-01 0.08
2 4.0e+02 5.1e+02 2.2e+04 -9.34e-01 -1.198563794e+05 1.137215079e+01 1.7e-01 0.11
3 2.8e+02 3.6e+02 1.6e+04 -8.29e-01 -1.157240237e+05 8.367013494e+01 1.2e-01 0.14
4 2.8e+02 3.6e+02 1.6e+04 -7.56e-01 -1.124198291e+05 2.832600044e+03 1.2e-01 0.18
5 6.3e+01 8.2e+01 3.6e+03 -7.47e-01 -6.640387952e+04 1.269993076e+04 2.8e-02 0.21
6 3.9e+01 5.1e+01 2.2e+03 -7.19e-02 -4.860601037e+04 1.113872194e+04 1.7e-02 0.24
7 2.8e+01 3.7e+01 1.6e+03 2.50e-01 -3.839144568e+04 8.758888904e+03 1.3e-02 0.28
8 1.6e+01 2.1e+01 9.0e+02 4.36e-01 -2.428137596e+04 5.454540196e+03 7.1e-03 0.30
9 6.4e+00 8.3e+00 3.6e+02 6.74e-01 -1.033392267e+04 2.810571263e+03 2.9e-03 0.34
10 3.6e+00 4.7e+00 2.0e+02 8.87e-01 -5.635132479e+03 1.899018503e+03 1.6e-03 0.37
11 1.3e+00 1.7e+00 7.5e+01 9.54e-01 -2.012851477e+03 7.891735701e+02 5.9e-04 0.40
12 1.0e+00 1.3e+00 5.7e+01 9.87e-01 -1.520027693e+03 6.366082104e+02 4.5e-04 0.43
13 8.5e-01 1.5e+00 4.8e+01 9.70e-01 -1.298863706e+03 5.502878441e+02 3.9e-04 0.46
14 2.9e-01 5.1e-01 1.6e+01 9.89e-01 -4.334744810e+02 1.970087469e+02 1.3e-04 0.49
15 1.6e-01 3.0e-01 9.3e+00 1.00e+00 -2.379383425e+02 1.162332574e+02 7.5e-05 0.52
16 7.3e-02 1.6e-01 4.2e+00 1.00e+00 -1.038594679e+02 5.761977378e+01 3.4e-05 0.55
17 3.5e-02 1.0e-01 2.1e+00 1.01e+00 -4.582053451e+01 3.218272093e+01 1.7e-05 0.58
18 1.8e-02 7.9e-02 1.1e+00 1.01e+00 -2.038712153e+01 2.046088815e+01 8.8e-06 0.62
19 1.8e-02 7.6e-02 1.0e+00 1.02e+00 -1.899851691e+01 2.043791424e+01 8.5e-06 0.64
20 9.7e-03 5.8e-02 5.7e-01 1.02e+00 -4.740810660e+00 1.674373473e+01 4.7e-06 0.68
21 4.1e-03 5.8e-02 2.5e-01 1.02e+00 4.583284449e+00 1.368803928e+01 2.0e-06 0.71
22 2.1e-03 5.2e-02 1.3e-01 1.01e+00 7.768933220e+00 1.261358672e+01 1.1e-06 0.74
23 6.0e-04 8.2e-02 3.9e-02 9.87e-01 1.034302452e+01 1.181151690e+01 3.4e-07 0.77
24 1.8e-04 8.8e-02 1.3e-02 9.78e-01 1.109075708e+01 1.156935511e+01 1.1e-07 0.80
25 6.0e-05 8.7e-02 4.3e-03 9.88e-01 1.133248268e+01 1.149489097e+01 3.9e-08 0.84
26 2.2e-05 8.4e-02 1.6e-03 9.96e-01 1.141328717e+01 1.147317407e+01 1.5e-08 0.87
27 8.2e-06 8.1e-02 6.0e-04 9.99e-01 1.144292901e+01 1.146572680e+01 5.6e-09 0.89
28 7.4e-06 7.4e-02 5.4e-04 1.00e+00 1.144485638e+01 1.146537583e+01 5.0e-09 0.93
29 6.7e-06 6.7e-02 4.9e-04 1.00e+00 1.144644856e+01 1.146491646e+01 4.5e-09 0.96
30 6.0e-06 6.1e-02 4.4e-04 1.00e+00 1.144788120e+01 1.146450263e+01 4.1e-09 0.99
31 5.4e-06 5.6e-02 3.9e-04 1.00e+00 1.144916792e+01 1.146412752e+01 3.7e-09 1.02
32 4.9e-06 5.1e-02 3.5e-04 1.00e+00 1.145032478e+01 1.146378860e+01 3.3e-09 1.05
33 4.4e-06 4.6e-02 3.2e-04 1.00e+00 1.145136482e+01 1.146348239e+01 3.0e-09 1.08
34 3.9e-06 4.2e-02 2.9e-04 1.00e+00 1.145229995e+01 1.146320587e+01 2.7e-09 1.11
35 3.5e-06 3.9e-02 2.6e-04 1.00e+00 1.145314082e+01 1.146295624e+01 2.4e-09 1.14
36 3.2e-06 3.6e-02 2.3e-04 1.00e+00 1.145389701e+01 1.146273096e+01 2.2e-09 1.18
37 2.9e-06 3.3e-02 2.1e-04 1.00e+00 1.145457711e+01 1.146252773e+01 1.9e-09 1.21
38 2.6e-06 3.0e-02 1.9e-04 1.00e+00 1.145518883e+01 1.146234444e+01 1.7e-09 1.24
39 2.3e-06 2.8e-02 1.7e-04 1.00e+00 1.145573908e+01 1.146217919e+01 1.6e-09 1.26
40 2.1e-06 2.6e-02 1.5e-04 1.00e+00 1.145623408e+01 1.146203023e+01 1.4e-09 1.29
41 1.9e-06 2.4e-02 1.4e-04 1.00e+00 1.145667940e+01 1.146189598e+01 1.3e-09 1.33
42 1.7e-06 2.2e-02 1.2e-04 1.00e+00 1.145708003e+01 1.146177504e+01 1.1e-09 1.36
43 1.5e-06 2.1e-02 1.1e-04 1.00e+00 1.145744051e+01 1.146166601e+01 1.0e-09 1.39
44 1.4e-06 1.9e-02 1.0e-04 1.00e+00 1.145776484e+01 1.146156783e+01 9.3e-10 1.42
45 1.2e-06 1.8e-02 9.0e-05 1.00e+00 1.145805668e+01 1.146147934e+01 8.4e-10 1.46
46 1.1e-06 1.7e-02 8.1e-05 1.00e+00 1.145831929e+01 1.146139964e+01 7.5e-10 1.48
47 1.0e-06 1.6e-02 7.3e-05 1.00e+00 1.145855559e+01 1.146132789e+01 6.8e-10 1.51
48 9.0e-07 1.5e-02 6.6e-05 1.00e+00 1.145876821e+01 1.146126331e+01 6.1e-10 1.54
49 8.1e-07 1.4e-02 5.9e-05 1.00e+00 1.145895956e+01 1.146120513e+01 5.5e-10 1.58
50 7.3e-07 1.4e-02 5.3e-05 1.00e+00 1.145913175e+01 1.146115272e+01 4.9e-10 1.61
51 6.6e-07 1.3e-02 4.8e-05 1.00e+00 1.145928670e+01 1.146110559e+01 4.4e-10 1.64
52 2.3e-07 4.5e-03 1.7e-05 1.00e+00 1.146019620e+01 1.146082824e+01 1.5e-10 1.67
53 2.1e-07 4.0e-03 1.5e-05 1.00e+00 1.146024499e+01 1.146081381e+01 1.4e-10 1.70
54 7.0e-08 1.4e-03 5.1e-06 9.98e-01 1.146053162e+01 1.146072628e+01 4.8e-11 1.73
55 6.3e-08 1.2e-03 4.6e-06 1.03e+00 1.146054866e+01 1.146072085e+01 4.3e-11 1.76
56 5.7e-08 1.1e-03 4.1e-06 9.72e-01 1.146056180e+01 1.146071690e+01 3.9e-11 1.79
57 5.1e-08 1.0e-03 3.7e-06 9.85e-01 1.146057363e+01 1.146071335e+01 3.5e-11 1.83
58 2.4e-08 1.9e-04 7.2e-07 9.36e-01 1.146066114e+01 1.146068911e+01 7.7e-12 1.85
59 2.7e-08 1.7e-04 6.5e-07 1.16e+00 1.146066443e+01 1.146068691e+01 7.4e-12 1.88
60 4.5e-08 1.7e-04 6.3e-07 1.03e+01 1.146066250e+01 1.146069931e+01 6.0e-12 1.91
61 2.4e-08 4.6e-06 1.7e-08 7.43e-01 1.146068440e+01 1.146068559e+01 8.8e-13 1.94
Interior-point optimizer terminated. Time: 1.94.
Optimizer terminated. Time: 1.98
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1460684401e+01 Viol. con: 9e-07 var: 0e+00
Dual. obj: 1.1460685592e+01 Viol. con: 0e+00 var: 6e-05
* End solution on dual form. *
Transforming to primal solution.
Solving took 2 seconds.
result packing took 13% of solve time
solution checking took 2.8% 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 : Linux/64-X86
Cores : 20
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 : 20
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 : 0.05 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.04
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 -1.288303512e+05 2.000000000e+00 1.0e+00 0.07
1 1.1e+03 1.4e+03 5.9e+04 -9.71e-01 -1.265192982e+05 3.780477836e+00 4.6e-01 0.10
2 3.9e+02 5.0e+02 2.2e+04 -9.34e-01 -1.195799798e+05 1.160505355e+01 1.7e-01 0.13
3 2.8e+02 3.6e+02 1.6e+04 -8.26e-01 -1.156357962e+05 9.406311649e+01 1.2e-01 0.15
4 2.8e+02 3.6e+02 1.6e+04 -7.56e-01 -1.123238469e+05 2.800924851e+03 1.2e-01 0.19
5 7.8e+01 1.0e+02 4.4e+03 -7.46e-01 -7.498490764e+04 1.053043422e+04 3.5e-02 0.22
6 3.8e+01 4.9e+01 2.1e+03 -2.08e-01 -4.716235799e+04 1.110976027e+04 1.7e-02 0.25
7 2.1e+01 2.8e+01 1.2e+03 2.72e-01 -3.073914169e+04 7.248950056e+03 9.5e-03 0.29
8 9.8e+00 1.3e+01 5.5e+02 5.69e-01 -1.536042016e+04 3.891973657e+03 4.3e-03 0.32
9 4.2e+00 5.5e+00 2.4e+02 8.19e-01 -6.676842286e+03 2.109861205e+03 1.9e-03 0.35
10 2.0e+00 2.6e+00 1.1e+02 9.39e-01 -2.962235116e+03 1.171567294e+03 8.8e-04 0.39
11 1.4e+00 1.8e+00 7.8e+01 9.83e-01 -2.096522213e+03 8.360333115e+02 6.2e-04 0.43
12 9.0e-01 1.2e+00 5.1e+01 9.85e-01 -1.355747542e+03 5.626979985e+02 4.0e-04 0.46
13 7.4e-01 1.1e+00 4.2e+01 9.64e-01 -1.126502400e+03 4.651586959e+02 3.3e-04 0.50
14 2.6e-01 3.9e-01 1.5e+01 9.90e-01 -3.944629788e+02 1.817715729e+02 1.2e-04 0.53
15 1.5e-01 2.3e-01 8.6e+00 1.00e+00 -2.188998551e+02 1.081298469e+02 6.9e-05 0.57
16 4.0e-02 1.5e-01 2.4e+00 1.00e+00 -5.532589022e+01 3.458476689e+01 1.9e-05 0.60
17 3.4e-02 1.3e-01 2.0e+00 1.00e+00 -4.532847979e+01 3.084876176e+01 1.6e-05 0.64
18 2.2e-02 9.8e-02 1.3e+00 1.00e+00 -2.692541527e+01 2.266695950e+01 1.1e-05 0.67
19 1.7e-02 7.9e-02 1.0e+00 1.01e+00 -1.840205912e+01 1.996457680e+01 8.3e-06 0.71
20 1.4e-02 6.7e-02 8.6e-01 1.02e+00 -1.345202432e+01 1.877857039e+01 7.0e-06 0.74
21 5.6e-03 6.1e-02 3.4e-01 1.02e+00 1.786299756e+00 1.421254057e+01 2.8e-06 0.77
22 2.2e-03 6.3e-02 1.4e-01 1.02e+00 7.519158852e+00 1.255705054e+01 1.2e-06 0.81
23 8.4e-04 6.1e-02 5.3e-02 9.85e-01 9.794068356e+00 1.178172456e+01 4.6e-07 0.84
24 3.1e-04 7.5e-02 2.1e-02 9.69e-01 1.074591383e+01 1.152793252e+01 1.8e-07 0.88
25 1.4e-04 5.9e-02 1.0e-02 9.56e-01 1.105520572e+01 1.143564274e+01 8.8e-08 0.91
26 6.9e-05 5.8e-02 4.8e-03 9.86e-01 1.120817361e+01 1.139332363e+01 4.3e-08 0.95
27 6.2e-05 5.3e-02 4.3e-03 9.93e-01 1.122429169e+01 1.139130996e+01 3.9e-08 0.98
28 5.6e-05 4.8e-02 3.9e-03 9.90e-01 1.123692308e+01 1.138763934e+01 3.5e-08 1.01
29 5.1e-05 4.4e-02 3.5e-03 9.92e-01 1.124888025e+01 1.138447197e+01 3.2e-08 1.05
30 4.5e-05 4.0e-02 3.2e-03 9.91e-01 1.125949310e+01 1.138163966e+01 2.8e-08 1.08
31 4.1e-05 3.7e-02 2.9e-03 9.92e-01 1.126901645e+01 1.137897910e+01 2.6e-08 1.12
32 3.7e-05 3.4e-02 2.6e-03 9.92e-01 1.127758230e+01 1.137659125e+01 2.3e-08 1.15
33 3.3e-05 3.1e-02 2.3e-03 9.93e-01 1.128524700e+01 1.137439270e+01 2.1e-08 1.19
34 3.0e-05 2.9e-02 2.1e-03 9.93e-01 1.129213125e+01 1.137238957e+01 1.9e-08 1.22
35 2.7e-05 2.7e-02 1.9e-03 9.94e-01 1.129830881e+01 1.137056608e+01 1.7e-08 1.25
36 2.4e-05 2.5e-02 1.7e-03 9.94e-01 1.130385151e+01 1.136890420e+01 1.5e-08 1.29
37 2.2e-05 2.3e-02 1.5e-03 9.95e-01 1.130882766e+01 1.136739290e+01 1.4e-08 1.32
38 2.0e-05 2.1e-02 1.4e-03 9.95e-01 1.131329614e+01 1.136602015e+01 1.2e-08 1.36
39 1.8e-05 2.0e-02 1.2e-03 9.95e-01 1.131730961e+01 1.136477441e+01 1.1e-08 1.39
40 1.6e-05 1.9e-02 1.1e-03 9.96e-01 1.132091536e+01 1.136364499e+01 9.9e-09 1.43
41 1.4e-05 1.8e-02 1.0e-03 9.96e-01 1.132415565e+01 1.136262189e+01 8.9e-09 1.46
42 1.3e-05 1.7e-02 9.0e-04 9.97e-01 1.132706822e+01 1.136169591e+01 8.0e-09 1.49
43 1.2e-05 1.6e-02 8.1e-04 9.97e-01 1.132968670e+01 1.136085831e+01 7.2e-09 1.53
44 1.0e-05 1.5e-02 7.3e-04 9.97e-01 1.133204116e+01 1.136010111e+01 6.5e-09 1.56
45 9.4e-06 1.4e-02 6.5e-04 9.98e-01 1.133415842e+01 1.135941684e+01 5.9e-09 1.60
46 8.4e-06 1.3e-02 5.9e-04 9.98e-01 1.133606251e+01 1.135879869e+01 5.3e-09 1.63
47 7.6e-06 1.3e-02 5.3e-04 9.98e-01 1.133777497e+01 1.135824043e+01 4.7e-09 1.67
48 6.8e-06 1.2e-02 4.8e-04 9.98e-01 1.133931512e+01 1.135773634e+01 4.3e-09 1.70
49 6.1e-06 1.2e-02 4.3e-04 9.98e-01 1.134070030e+01 1.135728131e+01 3.8e-09 1.74
50 5.5e-06 1.1e-02 3.9e-04 9.99e-01 1.134194613e+01 1.135687055e+01 3.5e-09 1.77
51 5.0e-06 1.1e-02 3.5e-04 9.99e-01 1.134306662e+01 1.135649984e+01 3.1e-09 1.80
52 4.5e-06 1.0e-02 3.1e-04 9.99e-01 1.134407439e+01 1.135616532e+01 2.8e-09 1.84
53 4.0e-06 1.0e-02 2.8e-04 9.99e-01 1.134498080e+01 1.135586347e+01 2.5e-09 1.87
54 3.6e-06 9.8e-03 2.5e-04 9.99e-01 1.134579609e+01 1.135559118e+01 2.3e-09 1.91
55 3.3e-06 9.5e-03 2.3e-04 9.99e-01 1.134652946e+01 1.135534561e+01 2.0e-09 1.94
56 2.9e-06 9.3e-03 2.1e-04 9.99e-01 1.134718920e+01 1.135512419e+01 1.8e-09 1.98
57 2.6e-06 9.0e-03 1.8e-04 9.99e-01 1.134778274e+01 1.135492461e+01 1.7e-09 2.01
58 2.4e-06 8.8e-03 1.7e-04 9.99e-01 1.134831676e+01 1.135474476e+01 1.5e-09 2.04
59 2.1e-06 8.7e-03 1.5e-04 1.00e+00 1.134879729e+01 1.135458271e+01 1.3e-09 2.08
60 1.9e-06 8.5e-03 1.3e-04 1.00e+00 1.134922968e+01 1.135443677e+01 1.2e-09 2.11
61 1.7e-06 8.4e-03 1.2e-04 9.99e-01 1.134961878e+01 1.135430537e+01 1.1e-09 2.15
62 1.6e-06 8.2e-03 1.1e-04 1.00e+00 1.134996894e+01 1.135418704e+01 9.8e-10 2.18
63 1.4e-06 8.1e-03 9.8e-05 1.00e+00 1.135028409e+01 1.135408049e+01 8.8e-10 2.22
64 1.3e-06 8.0e-03 8.8e-05 1.00e+00 1.135056772e+01 1.135398456e+01 7.9e-10 2.25
65 1.1e-06 7.9e-03 8.0e-05 1.00e+00 1.135082299e+01 1.135389823e+01 7.1e-10 2.28
66 1.0e-06 7.8e-03 7.2e-05 1.00e+00 1.135105275e+01 1.135382051e+01 6.4e-10 2.32
67 9.2e-07 7.7e-03 6.4e-05 1.00e+00 1.135125953e+01 1.135375059e+01 5.8e-10 2.35
68 8.3e-07 7.7e-03 5.8e-05 1.00e+00 1.135144565e+01 1.135368765e+01 5.2e-10 2.39
69 7.5e-07 7.6e-03 5.2e-05 1.00e+00 1.135161317e+01 1.135363101e+01 4.7e-10 2.42
70 6.7e-07 7.5e-03 4.7e-05 1.00e+00 1.135176394e+01 1.135358004e+01 4.2e-10 2.46
71 6.1e-07 7.5e-03 4.2e-05 1.00e+00 1.135189965e+01 1.135353416e+01 3.8e-10 2.49
72 5.4e-07 7.4e-03 3.8e-05 1.00e+00 1.135202180e+01 1.135349288e+01 3.4e-10 2.52
73 4.9e-07 7.4e-03 3.4e-05 1.00e+00 1.135213174e+01 1.135345572e+01 3.1e-10 2.56
74 4.4e-07 7.3e-03 3.1e-05 1.00e+00 1.135223069e+01 1.135342227e+01 2.8e-10 2.59
75 4.0e-07 7.3e-03 2.8e-05 1.00e+00 1.135231974e+01 1.135339220e+01 2.5e-10 2.63
76 3.6e-07 7.3e-03 2.5e-05 1.00e+00 1.135239990e+01 1.135336510e+01 2.2e-10 2.66
77 3.2e-07 7.2e-03 2.2e-05 1.00e+00 1.135247204e+01 1.135334074e+01 2.0e-10 2.70
78 2.9e-07 7.2e-03 2.0e-05 1.00e+00 1.135253697e+01 1.135331880e+01 1.8e-10 2.73
79 2.6e-07 7.2e-03 1.8e-05 1.00e+00 1.135259541e+01 1.135329904e+01 1.6e-10 2.76
80 2.3e-07 7.2e-03 1.6e-05 1.00e+00 1.135264801e+01 1.135328127e+01 1.5e-10 2.80
81 2.1e-07 7.1e-03 1.5e-05 1.00e+00 1.135269534e+01 1.135326529e+01 1.3e-10 2.83
82 1.9e-07 7.1e-03 1.3e-05 1.00e+00 1.135273794e+01 1.135325088e+01 1.2e-10 2.87
83 1.7e-07 7.1e-03 1.2e-05 9.99e-01 1.135277627e+01 1.135323794e+01 1.1e-10 2.90
84 1.5e-07 7.1e-03 1.1e-05 1.00e+00 1.135281078e+01 1.135322629e+01 9.6e-11 2.94
85 1.4e-07 7.1e-03 9.7e-06 1.00e+00 1.135284183e+01 1.135321579e+01 8.7e-11 2.97
86 1.2e-07 7.1e-03 8.7e-06 1.00e+00 1.135286978e+01 1.135320633e+01 7.8e-11 3.01
87 1.1e-07 7.0e-03 7.8e-06 9.99e-01 1.135289493e+01 1.135319784e+01 7.0e-11 3.04
88 1.0e-07 7.0e-03 7.1e-06 1.00e+00 1.135291757e+01 1.135319018e+01 6.3e-11 3.07
89 9.1e-08 7.0e-03 6.3e-06 9.98e-01 1.135293794e+01 1.135318330e+01 5.7e-11 3.11
90 8.2e-08 7.0e-03 5.7e-06 1.00e+00 1.135295627e+01 1.135317710e+01 5.1e-11 3.14
91 7.4e-08 7.0e-03 5.1e-06 1.00e+00 1.135297281e+01 1.135317149e+01 4.6e-11 3.18
92 6.6e-08 7.0e-03 4.6e-06 9.99e-01 1.135298765e+01 1.135316648e+01 4.1e-11 3.21
93 6.0e-08 7.0e-03 4.2e-06 9.97e-01 1.135300100e+01 1.135316198e+01 3.7e-11 3.25
94 5.4e-08 7.0e-03 3.7e-06 9.96e-01 1.135301302e+01 1.135315792e+01 3.4e-11 3.28
95 4.8e-08 7.0e-03 3.4e-06 1.00e+00 1.135302384e+01 1.135315425e+01 3.0e-11 3.31
96 4.3e-08 7.0e-03 3.0e-06 1.00e+00 1.135303358e+01 1.135315095e+01 2.7e-11 3.35
97 3.9e-08 6.3e-03 2.7e-06 1.00e+00 1.135304240e+01 1.135314795e+01 2.4e-11 3.38
98 3.5e-08 5.6e-03 2.5e-06 9.94e-01 1.135305027e+01 1.135314530e+01 2.2e-11 3.42
99 3.2e-08 5.1e-03 2.2e-06 1.00e+00 1.135305737e+01 1.135314289e+01 2.0e-11 3.45
100 2.9e-08 4.6e-03 2.0e-06 1.00e+00 1.135306382e+01 1.135314069e+01 1.8e-11 3.49
101 2.6e-08 4.1e-03 1.8e-06 1.00e+00 1.135306960e+01 1.135313873e+01 1.6e-11 3.52
102 2.3e-08 3.7e-03 1.6e-06 1.01e+00 1.135307490e+01 1.135313691e+01 1.5e-11 3.55
103 2.1e-08 3.3e-03 1.5e-06 1.00e+00 1.135307960e+01 1.135313531e+01 1.3e-11 3.59
104 1.9e-08 3.0e-03 1.3e-06 1.01e+00 1.135308389e+01 1.135313384e+01 1.2e-11 3.62
105 1.7e-08 2.7e-03 1.2e-06 1.01e+00 1.135308776e+01 1.135313252e+01 1.1e-11 3.66
106 1.5e-08 2.4e-03 1.1e-06 1.01e+00 1.135309126e+01 1.135313132e+01 9.7e-12 3.69
107 1.4e-08 2.2e-03 9.5e-07 1.00e+00 1.135309425e+01 1.135313031e+01 8.7e-12 3.73
108 1.2e-08 2.0e-03 8.6e-07 1.02e+00 1.135309713e+01 1.135312932e+01 7.9e-12 3.76
109 1.5e-09 2.0e-04 8.9e-08 9.86e-01 1.135311878e+01 1.135312213e+01 8.6e-13 3.79
Interior-point optimizer terminated. Time: 3.80.
Optimizer terminated. Time: 3.87
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1353118779e+01 Viol. con: 2e-08 var: 0e+00
Dual. obj: 1.1353122130e+01 Viol. con: 0e+00 var: 2e-03
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.89 seconds.
result packing took 8.2% of solve time
solution checking took 1.1% 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 : Linux/64-X86
Cores : 20
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: 0.03
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 20
Optimizer - solved problem : the primal
Optimizer - Constraints : 830
Optimizer - Cones : 0
Optimizer - Scalar variables : 3579 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.05 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.03
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 -1.288293950e+05 2.000000000e+00 1.0e+00 0.09
1 1.1e+03 1.4e+03 5.9e+04 -9.71e-01 -1.265119499e+05 3.775532316e+00 4.6e-01 0.13
2 3.8e+02 4.9e+02 2.1e+04 -9.34e-01 -1.194154364e+05 1.178287811e+01 1.7e-01 0.15
3 2.8e+02 3.6e+02 1.6e+04 -8.24e-01 -1.156042359e+05 1.066464878e+02 1.2e-01 0.18
4 2.8e+02 3.6e+02 1.5e+04 -7.56e-01 -1.122478845e+05 2.780033139e+03 1.2e-01 0.22
5 7.6e+01 9.8e+01 4.2e+03 -7.45e-01 -7.375616903e+04 1.084031708e+04 3.4e-02 0.25
6 3.6e+01 4.7e+01 2.0e+03 -1.89e-01 -4.548389366e+04 1.112040299e+04 1.6e-02 0.28
7 2.0e+01 2.6e+01 1.1e+03 3.01e-01 -2.906397476e+04 7.239522891e+03 9.0e-03 0.32
8 9.7e+00 1.3e+01 5.4e+02 5.98e-01 -1.521643449e+04 3.918845262e+03 4.3e-03 0.35
9 4.3e+00 5.6e+00 2.4e+02 8.23e-01 -6.824908321e+03 2.127562803e+03 1.9e-03 0.38
10 1.6e+00 2.1e+00 9.0e+01 9.39e-01 -2.373662871e+03 9.911140065e+02 7.1e-04 0.42
11 1.1e+00 1.5e+00 6.3e+01 9.88e-01 -1.663835792e+03 6.968584959e+02 5.0e-04 0.45
12 7.8e-01 1.0e+00 4.4e+01 9.83e-01 -1.178821201e+03 4.971820821e+02 3.5e-04 0.48
13 5.9e-01 7.7e-01 3.3e+01 9.85e-01 -8.760792082e+02 3.895010902e+02 2.7e-04 0.51
14 2.1e-01 2.9e-01 1.2e+01 9.89e-01 -3.251213984e+02 1.426643493e+02 9.9e-05 0.55
15 8.9e-02 1.4e-01 5.1e+00 1.01e+00 -1.286057557e+02 6.680938297e+01 4.2e-05 0.58
16 3.5e-02 9.9e-02 2.1e+00 1.01e+00 -4.801742277e+01 3.100038491e+01 1.7e-05 0.61
17 2.9e-02 8.4e-02 1.7e+00 9.96e-01 -3.744292559e+01 2.764782544e+01 1.4e-05 0.64
18 1.8e-02 6.6e-02 1.1e+00 1.01e+00 -1.954878839e+01 2.043049001e+01 8.7e-06 0.67
19 1.6e-02 5.8e-02 9.2e-01 1.02e+00 -1.527534278e+01 1.935092090e+01 7.5e-06 0.71
20 5.6e-03 6.6e-02 3.4e-01 1.02e+00 1.703966414e+00 1.416207126e+01 2.8e-06 0.73
21 1.9e-03 7.7e-02 1.2e-01 1.02e+00 8.009408131e+00 1.236803224e+01 1.0e-06 0.77
22 1.4e-03 5.9e-02 8.6e-02 9.66e-01 8.848567578e+00 1.205228490e+01 7.4e-07 0.80
23 4.9e-04 6.6e-02 3.2e-02 9.59e-01 1.037947031e+01 1.161036622e+01 2.9e-07 0.83
24 2.0e-04 6.1e-02 1.3e-02 9.57e-01 1.092222500e+01 1.143145285e+01 1.2e-07 0.86
25 1.8e-04 5.6e-02 1.2e-02 9.75e-01 1.096040414e+01 1.141851136e+01 1.1e-07 0.89
26 1.6e-04 5.1e-02 1.1e-02 9.73e-01 1.099565890e+01 1.140850389e+01 9.6e-08 0.92
27 1.4e-04 4.6e-02 9.6e-03 9.75e-01 1.103008890e+01 1.140220777e+01 8.7e-08 0.95
28 1.3e-04 4.2e-02 8.7e-03 9.77e-01 1.106120368e+01 1.139659204e+01 7.8e-08 0.98
29 1.2e-04 3.9e-02 7.8e-03 9.79e-01 1.108921818e+01 1.139147023e+01 7.0e-08 1.01
30 1.0e-04 3.6e-02 7.0e-03 9.81e-01 1.111438308e+01 1.138674402e+01 6.3e-08 1.04
31 9.3e-05 3.3e-02 6.3e-03 9.82e-01 1.113697917e+01 1.138238085e+01 5.7e-08 1.07
32 8.4e-05 3.0e-02 5.7e-03 9.84e-01 1.115726227e+01 1.137835287e+01 5.1e-08 1.11
33 7.6e-05 2.8e-02 5.1e-03 9.85e-01 1.117546483e+01 1.137463571e+01 4.6e-08 1.14
34 6.8e-05 2.6e-02 4.6e-03 9.87e-01 1.119179736e+01 1.137120750e+01 4.2e-08 1.17
35 6.1e-05 2.4e-02 4.2e-03 9.88e-01 1.120645006e+01 1.136804809e+01 3.7e-08 1.20
36 5.5e-05 2.2e-02 3.7e-03 9.89e-01 1.121959488e+01 1.136513932e+01 3.4e-08 1.23
37 5.0e-05 2.1e-02 3.4e-03 9.90e-01 1.123138668e+01 1.136246406e+01 3.0e-08 1.26
38 4.5e-05 1.9e-02 3.0e-03 9.91e-01 1.124196482e+01 1.136000630e+01 2.7e-08 1.29
39 4.0e-05 1.8e-02 2.7e-03 9.92e-01 1.125145444e+01 1.135775078e+01 2.5e-08 1.32
40 3.6e-05 1.7e-02 2.5e-03 9.93e-01 1.125996777e+01 1.135568289e+01 2.2e-08 1.36
41 3.3e-05 1.6e-02 2.2e-03 9.93e-01 1.126760552e+01 1.135378883e+01 2.0e-08 1.39
42 2.9e-05 1.5e-02 2.0e-03 9.94e-01 1.127445808e+01 1.135205555e+01 1.8e-08 1.42
43 2.6e-05 1.4e-02 1.8e-03 9.95e-01 1.128060672e+01 1.135047102e+01 1.6e-08 1.45
44 2.4e-05 1.4e-02 1.6e-03 9.95e-01 1.128612453e+01 1.134902412e+01 1.5e-08 1.48
45 2.1e-05 1.3e-02 1.4e-03 9.96e-01 1.129107707e+01 1.134770448e+01 1.3e-08 1.51
46 1.9e-05 1.2e-02 1.3e-03 9.96e-01 1.129552307e+01 1.134650224e+01 1.2e-08 1.54
47 1.7e-05 1.2e-02 1.2e-03 9.97e-01 1.129951504e+01 1.134540816e+01 1.1e-08 1.58
48 1.6e-05 1.1e-02 1.1e-03 9.97e-01 1.130309990e+01 1.134441331e+01 9.5e-09 1.61
49 1.4e-05 1.1e-02 9.5e-04 9.97e-01 1.130631973e+01 1.134350961e+01 8.6e-09 1.64
50 1.3e-05 1.1e-02 8.6e-04 9.98e-01 1.130921211e+01 1.134268939e+01 7.7e-09 1.67
51 1.1e-05 1.0e-02 7.7e-04 9.98e-01 1.131181072e+01 1.134194550e+01 7.0e-09 1.70
52 1.0e-05 1.0e-02 6.9e-04 9.98e-01 1.131414572e+01 1.134127129e+01 6.3e-09 1.73
53 9.2e-06 9.7e-03 6.2e-04 9.98e-01 1.131624409e+01 1.134066049e+01 5.6e-09 1.76
54 8.3e-06 9.4e-03 5.6e-04 9.98e-01 1.131813006e+01 1.134010762e+01 5.1e-09 1.80
55 7.5e-06 9.2e-03 5.1e-04 9.99e-01 1.131982524e+01 1.133960739e+01 4.6e-09 1.83
56 6.7e-06 9.0e-03 4.6e-04 9.99e-01 1.132134904e+01 1.133915491e+01 4.1e-09 1.86
57 6.0e-06 8.8e-03 4.1e-04 9.99e-01 1.132271890e+01 1.133874560e+01 3.7e-09 1.89
58 5.4e-06 8.6e-03 3.7e-04 9.99e-01 1.132395043e+01 1.133837571e+01 3.3e-09 1.92
59 4.9e-06 8.5e-03 3.3e-04 9.99e-01 1.132505762e+01 1.133804135e+01 3.0e-09 1.95
60 4.4e-06 8.3e-03 3.0e-04 9.99e-01 1.132605308e+01 1.133773920e+01 2.7e-09 1.98
61 4.0e-06 8.2e-03 2.7e-04 9.99e-01 1.132694812e+01 1.133746631e+01 2.4e-09 2.01
62 3.6e-06 8.1e-03 2.4e-04 9.99e-01 1.132775293e+01 1.133721986e+01 2.2e-09 2.05
63 3.2e-06 8.0e-03 2.2e-04 1.00e+00 1.132847668e+01 1.133699728e+01 2.0e-09 2.08
64 2.9e-06 7.9e-03 2.0e-04 9.99e-01 1.132912757e+01 1.133679651e+01 1.8e-09 2.11
65 2.6e-06 7.8e-03 1.8e-04 1.00e+00 1.132971301e+01 1.133661533e+01 1.6e-09 2.14
66 2.3e-06 7.7e-03 1.6e-04 1.00e+00 1.133023963e+01 1.133645197e+01 1.4e-09 2.17
67 2.1e-06 7.7e-03 1.4e-04 1.00e+00 1.133071338e+01 1.133630465e+01 1.3e-09 2.21
68 1.9e-06 7.6e-03 1.3e-04 1.00e+00 1.133113959e+01 1.133617190e+01 1.2e-09 2.23
69 1.7e-06 7.5e-03 1.2e-04 1.00e+00 1.133152306e+01 1.133605230e+01 1.0e-09 2.27
70 1.5e-06 7.5e-03 1.0e-04 1.00e+00 1.133186810e+01 1.133594447e+01 9.4e-10 2.30
71 1.4e-06 7.4e-03 9.4e-05 1.00e+00 1.133217858e+01 1.133584734e+01 8.5e-10 2.33
72 1.2e-06 7.4e-03 8.4e-05 1.00e+00 1.133245794e+01 1.133575986e+01 7.6e-10 2.36
73 1.1e-06 7.3e-03 7.6e-05 1.00e+00 1.133270933e+01 1.133568110e+01 6.9e-10 2.38
74 1.0e-06 7.3e-03 6.8e-05 1.00e+00 1.133293555e+01 1.133561017e+01 6.2e-10 2.41
75 9.1e-07 7.3e-03 6.2e-05 1.00e+00 1.133313912e+01 1.133554631e+01 5.6e-10 2.45
76 8.2e-07 7.2e-03 5.5e-05 1.00e+00 1.133332231e+01 1.133548880e+01 5.0e-10 2.48
77 7.3e-07 7.2e-03 5.0e-05 1.00e+00 1.133348717e+01 1.133543703e+01 4.5e-10 2.51
78 6.6e-07 7.2e-03 4.5e-05 1.00e+00 1.133363553e+01 1.133539040e+01 4.1e-10 2.53
79 5.9e-07 7.2e-03 4.0e-05 9.99e-01 1.133376902e+01 1.133534850e+01 3.6e-10 2.56
80 5.4e-07 7.1e-03 3.6e-05 9.99e-01 1.133388916e+01 1.133531075e+01 3.3e-10 2.60
81 4.8e-07 7.1e-03 3.3e-05 1.00e+00 1.133399729e+01 1.133527675e+01 3.0e-10 2.63
82 4.3e-07 7.1e-03 2.9e-05 1.00e+00 1.133409459e+01 1.133524614e+01 2.7e-10 2.66
83 3.9e-07 7.1e-03 2.6e-05 1.00e+00 1.133418217e+01 1.133521856e+01 2.4e-10 2.69
84 3.5e-07 7.1e-03 2.4e-05 1.00e+00 1.133426099e+01 1.133519370e+01 2.2e-10 2.72
85 3.2e-07 7.0e-03 2.1e-05 9.99e-01 1.133433190e+01 1.133517139e+01 1.9e-10 2.75
86 2.8e-07 7.0e-03 1.9e-05 9.99e-01 1.133439571e+01 1.133515131e+01 1.7e-10 2.78
87 2.6e-07 7.0e-03 1.7e-05 1.00e+00 1.133445323e+01 1.133513311e+01 1.6e-10 2.81
88 2.3e-07 7.0e-03 1.6e-05 1.00e+00 1.133450513e+01 1.133511668e+01 1.4e-10 2.84
89 2.1e-07 7.0e-03 1.4e-05 9.98e-01 1.133455161e+01 1.133510206e+01 1.3e-10 2.87
90 1.9e-07 7.0e-03 1.3e-05 1.00e+00 1.133459346e+01 1.133508882e+01 1.1e-10 2.90
91 1.7e-07 7.0e-03 1.1e-05 9.99e-01 1.133463111e+01 1.133507695e+01 1.0e-10 2.93
92 1.5e-07 6.9e-03 1.0e-05 9.98e-01 1.133466498e+01 1.133506628e+01 9.3e-11 2.96
93 1.4e-07 6.9e-03 9.2e-06 1.00e+00 1.133469548e+01 1.133505663e+01 8.4e-11 2.99
94 1.2e-07 6.9e-03 8.3e-06 9.99e-01 1.133472292e+01 1.133504798e+01 7.5e-11 3.03
95 1.1e-07 6.2e-03 7.5e-06 1.00e+00 1.133474772e+01 1.133504011e+01 6.8e-11 3.06
96 9.9e-08 5.6e-03 6.7e-06 1.00e+00 1.133476994e+01 1.133503308e+01 6.1e-11 3.09
97 8.9e-08 5.1e-03 6.1e-06 9.97e-01 1.133478992e+01 1.133502678e+01 5.5e-11 3.12
98 8.0e-08 4.5e-03 5.5e-06 1.00e+00 1.133480792e+01 1.133502108e+01 4.9e-11 3.15
99 7.2e-08 4.1e-03 4.9e-06 1.00e+00 1.133482419e+01 1.133501591e+01 4.4e-11 3.19
100 6.5e-08 3.7e-03 4.4e-06 9.95e-01 1.133483874e+01 1.133501134e+01 4.0e-11 3.22
101 5.9e-08 3.3e-03 4.0e-06 1.00e+00 1.133485185e+01 1.133500718e+01 3.6e-11 3.25
102 5.3e-08 3.0e-03 3.6e-06 1.01e+00 1.133486429e+01 1.133500317e+01 3.3e-11 3.28
103 4.7e-08 2.7e-03 3.2e-06 1.01e+00 1.133487502e+01 1.133499976e+01 2.9e-11 3.31
104 4.3e-08 2.4e-03 2.9e-06 1.00e+00 1.133488453e+01 1.133499674e+01 2.6e-11 3.34
105 3.8e-08 2.2e-03 2.6e-06 1.02e+00 1.133489364e+01 1.133499380e+01 2.4e-11 3.37
106 3.5e-08 2.0e-03 2.3e-06 9.94e-01 1.133490125e+01 1.133499142e+01 2.2e-11 3.39
107 3.1e-08 1.8e-03 2.1e-06 9.82e-01 1.133490808e+01 1.133498931e+01 1.9e-11 3.42
108 2.8e-08 1.6e-03 1.9e-06 1.02e+00 1.133491480e+01 1.133498713e+01 1.8e-11 3.46
109 2.5e-08 1.4e-03 1.7e-06 1.01e+00 1.133492057e+01 1.133498528e+01 1.6e-11 3.49
110 5.2e-09 2.7e-04 3.3e-07 9.92e-01 1.133496044e+01 1.133497281e+01 3.1e-12 3.52
111 3.4e-10 1.5e-05 1.8e-08 9.99e-01 1.133496922e+01 1.133496991e+01 1.7e-13 3.55
Interior-point optimizer terminated. Time: 3.56.
Optimizer terminated. Time: 3.65
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1334969224e+01 Viol. con: 5e-09 var: 0e+00
Dual. obj: 1.1334969908e+01 Viol. con: 0e+00 var: 1e-04
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.67 seconds.
result packing took 7.4% of solve time
solution checking took 1.4% of solve time
Solving took 6 GP solves and 26.5 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 2418945.78759 force_pound * meter but the right hand side evaluated to 2375460.00844 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 32774.3857494 force_pound but the right hand side evaluated to 32399.9999979 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 2.21510116793 meter but the right hand side evaluated to 2.08158429962 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 1243576.11683 joule / kilogram but the right hand side evaluated to 1.56106408442 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 664756.820245 joule / kilogram but the right hand side evaluated to 0.667334435663 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 18.3998954878 meter but the right hand side evaluated to 16.322915543 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 10.903620968517039 but the right hand side evaluated to 4.7888597829928 (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.
----------------------------------------------------------------------
Ran 1 test in 31.218s
OK
Generating XML reports...
to 10.019776161831526 but the right hand side evaluated to 4.788859773413604 (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 8.144915406300905 but the right hand side evaluated to 4.788859785321722 (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 18.3622542322 meter but the right hand side evaluated to 18.1377391224 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 18.3622542322 meter but the right hand side evaluated to 18.2420770831 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 0.2960368569035552 but the right hand side evaluated to 0.1897392652154496 (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 0.23302158193946187 but the right hand side evaluated to 0.17434672711234037 (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 7.563245036193752 but the right hand side evaluated to 4.730639724780067 (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 7.583086283715181 but the right hand side evaluated to 4.757852890568745 (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 /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3)
Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: six>=1.5 in /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 /tmp/pip-req-build-Icpdsm
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /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 /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 /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /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 /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: /tmp/pip-ephem-wheel-cache-2G9gHd/wheels/d5/94/ac/b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
Collecting git+https://github.com/convexengineering/gassolar.git
Cloning https://github.com/convexengineering/gassolar.git to /tmp/pip-req-build-39Kh9m
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /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 /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 /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /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 /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 /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 /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: python-dateutil in /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: pytz>=2011k in /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: six>=1.5 in /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: /tmp/pip-ephem-wheel-cache-ZgaQc4/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
Processing /jenkins/workspace/gplibrary_PR_Models/mosek/solar
Requirement already satisfied: numpy in /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 /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 /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /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 /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 /jenkins/workspace/gplibrary_PR_Models/mosek (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.7 in /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 /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: python-dateutil in /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: pytz>=2011k in /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: six>=1.5 in /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: /tmp/pip-ephem-wheel-cache-LdtmZK/wheels/f6/90/b0/8d5ca9b420ff66bedd24921652ee885c8718a479c0dcec7d2e
Successfully built solar
Installing collected packages: solar
Successfully installed solar-0.0.0.0
Running tests...
----------------------------------------------------------------------
../jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
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 5.89 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 1388463.0730 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 1248776.3343 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 2.29645501018 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194407 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 5.73 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 1388463.0598 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 1248776.3225 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 2.29645500999 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194387 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 t/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
tau = np.exp(-0.175/costhsun)
he 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 3.49 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 765970.5511 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 3.16 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 862671.9721 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 3.05 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 987087.2999 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 1.47 seconds.
Warning: V.ariable [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 1058302.4714 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 3.44 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 765970.5684 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 3.12 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 862671.9725 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 3.12 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 987087.2998 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 pur..poses, 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 1.55 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 1058302.4686 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 5.44 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 1388463.0551 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 1248776.3183 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 2.29645500992 meter ** 2 / second ** 2 but the right hand side evaluated to 2.2964519438 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 5.38 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 1388463.0681 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.r bound. Solution is 1248776.3300 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 2.29645501014 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194402 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 0.381 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 838075.6768 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 4.97 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 1017215.9438 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 2.62125883071 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124747986 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 1.95293542216 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215306 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 1.04275941615 meter ** 2 / second ** 2 but the right hand side evaluated to 1.0427552171 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 0.467698134229 meter ** 2 / second ** 2 but tEhe right hand side evaluated to 0.467697003892 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 0.139006791931 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006573777 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 0.567 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 6.76 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]'
InfeasibleE
======================================================================
ERROR [8.945s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
testfn(name, import_dict, path)(self)
File "/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 "/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 "/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 "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 83, in __init__
CostedConstraintSet.__init__(self, cost, constraints, substitutions)
File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/costed.py", line 21, in __init__
ConstraintSet.__init__(self, constraints, subs)
File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 58, in __init__
list.__setitem__(self, i, ConstraintSet(constraint))
File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 67, in __init__
raise_elementhasnumpybools(constraint)
File "/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 [15.747s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
testfn(name, import_dict, path)(self)
File "/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 "/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 "/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 "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 83, in __init__
CostedConstraintSet.__init__(self, cost, constraints, substitutions)
File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/costed.py", line 21, in __init__
ConstraintSet.__init__(self, constraints, subs)
File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 58, in __init__
list.__setitem__(self, i, ConstraintSet(constraint))
File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 67, in __init__
raise_elementhasnumpybools(constraint)
File "/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 242.333s
FAILED (errors=2)
Generating XML reports...
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 /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3)
Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: six>=1.5 in /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 /tmp/pip-req-build-aJovL2
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /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 /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 /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /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 /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: /tmp/pip-ephem-wheel-cache-cUep0J/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
Processing /jenkins/workspace/gplibrary_PR_Models/mosek/gplibrary
Requirement already satisfied: numpy>=1.12 in /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 /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 /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: /tmp/pip-ephem-wheel-cache-EGUor9/wheels/63/f8/98/93b45f0bf8ab3367cc8d67f05c8a0e19f356c1a33a86d02692
Successfully built gpkitmodels
Installing collected packages: gpkitmodels
Found existing installation: gpkitmodels 0.0.0.0
Not uninstalling gpkitmodels at /jenkins/workspace/gplibrary_PR_Models/mosek, outside environment /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit
Can't uninstall 'gpkitmodels'. No files were found to uninstall.
Successfully installed gpkitmodels-0.0.0.0
Running tests...
----------------------------------------------------------------------
...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 0.145 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.449 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.0725 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0867 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0454 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 3.54 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 985.544371523 meter * revolutions_per_minute but the right hand side evaluated to 103.041409431 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 0.420585924998 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573144938 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 0.314645033957 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629895194 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 0.168936438404 meter ** 2 / second ** 2 but the right hand side evaluated to 0.16893160397 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 0.0639642380863 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631379987 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 0.0226356535432 meter ** 2 / second ** 2 but the right hand side evaluated to 0.022635400588 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)
Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.443 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.259 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.24 seco.nds.
Beginning signomial solve.
Solving took 16 GP solves and 6.04 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 0.0945 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 2.44 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 1619897.4166 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.243 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 4.48 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 resul.
----------------------------------------------------------------------
Ran 10 tests in 25.124s
OK
Generating XML reports...
t 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 1.600s
OK
Generating XML reports...
adding test for 'aircraft_models.py'
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['python', '/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', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['python', '/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', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/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', '/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', '/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', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
attempt 1
calling ['python', '/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', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['python', '/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 [reynolds] 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 '/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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