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Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.289122953e+005 2.000000000e+000  1.0e+000 0.06  
1   1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.266169073e+005 3.779171657e+000  4.6e-001 0.09  
2   4.0e+002 5.1e+002 2.2e+004 -9.34e-001 -1.198583278e+005 1.137215136e+001  1.7e-001 0.13  
3   2.8e+002 3.6e+002 1.6e+004 -8.29e-001 -1.157259067e+005 8.367015563e+001  1.2e-001 0.16  
4   2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.124217023e+005 2.832600538e+003  1.2e-001 0.19  
5   6.3e+001 8.2e+001 3.6e+003 -7.47e-001 -6.640516573e+004 1.269993062e+004  2.8e-002 0.22  
6   3.9e+001 5.1e+001 2.2e+003 -7.19e-002 -4.860697656e+004 1.113872237e+004  1.7e-002 0.23  
7   2.8e+001 3.7e+001 1.6e+003 2.50e-001  -3.839220939e+004 8.758887744e+003  1.3e-002 0.25  
8   1.6e+001 2.1e+001 9.0e+002 4.36e-001  -2.428184762e+004 5.454538668e+003  7.1e-003 0.28  
9   6.4e+000 8.3e+000 3.6e+002 6.74e-001  -1.033412747e+004 2.810569798e+003  2.9e-003 0.30  
10  3.6e+000 4.7e+000 2.0e+002 8.87e-001  -5.635240186e+003 1.899015920e+003  1.6e-003 0.31  
11  1.3e+000 1.7e+000 7.5e+001 9.54e-001  -2.012888199e+003 7.891714736e+002  5.9e-004 0.33  
12  1.0e+000 1.3e+000 5.7e+001 9.87e-001  -1.520062385e+003 6.366085611e+002  4.5e-004 0.34  
13  8.5e-001 1.5e+000 4.8e+001 9.70e-001  -1.298891184e+003 5.502872193e+002  3.9e-004 0.37  
14  2.9e-001 5.1e-001 1.6e+001 9.89e-001  -4.334854398e+002 1.970093056e+002  1.3e-004 0.39  
15  1.6e-001 3.0e-001 9.3e+000 1.00e+000  -2.379435761e+002 1.162331341e+002  7.5e-005 0.41  
16  7.3e-002 1.6e-001 4.2e+000 1.00e+000  -1.038622231e+002 5.761988346e+001  3.4e-005 0.42  
17  3.5e-002 1.0e-001 2.1e+000 1.01e+000  -4.582194241e+001 3.218281528e+001  1.7e-005 0.44  
18  1.8e-002 7.9e-002 1.1e+000 1.01e+000  -2.038778273e+001 2.046090101e+001  8.8e-006 0.45  
19  1.8e-002 7.6e-002 1.0e+000 1.02e+000  -1.899914359e+001 2.043792943e+001  8.5e-006 0.48  
20  9.7e-003 5.8e-002 5.7e-001 1.02e+000  -4.741076883e+000 1.674370174e+001  4.7e-006 0.50  
21  4.1e-003 5.8e-002 2.5e-001 1.02e+000  4.583152821e+000  1.368803765e+001  2.0e-006 0.52  
22  2.1e-003 5.2e-002 1.3e-001 1.01e+000  7.768859596e+000  1.261358695e+001  1.1e-006 0.53  
23  6.0e-004 8.2e-002 3.9e-002 9.87e-001  1.034300591e+001  1.181151684e+001  3.4e-007 0.55  
24  1.8e-004 8.8e-002 1.3e-002 9.78e-001  1.109075112e+001  1.156935541e+001  1.1e-007 0.58  
25  6.0e-005 8.7e-002 4.3e-003 9.88e-001  1.133248076e+001  1.149489125e+001  3.9e-008 0.59  
26  2.2e-005 8.4e-002 1.6e-003 9.96e-001  1.141328710e+001  1.147317447e+001  1.5e-008 0.61  
27  8.2e-006 8.1e-002 6.0e-004 9.99e-001  1.144292908e+001  1.146572721e+001  5.6e-009 0.62  
28  7.4e-006 7.4e-002 5.4e-004 1.00e+000  1.144485650e+001  1.146537624e+001  5.0e-009 0.66  
29  6.7e-006 6.7e-002 4.9e-004 1.00e+000  1.144644872e+001  1.146491688e+001  4.5e-009 0.67  
30  6.0e-006 6.1e-002 4.4e-004 1.00e+000  1.144788138e+001  1.146450309e+001  4.1e-009 0.69  
31  5.4e-006 5.6e-002 3.9e-004 1.00e+000  1.144916813e+001  1.146412789e+001  3.7e-009 0.70  
32  4.9e-006 5.1e-002 3.5e-004 1.00e+000  1.145032502e+001  1.146378903e+001  3.3e-009 0.72  
33  4.4e-006 4.6e-002 3.2e-004 1.00e+000  1.145136507e+001  1.146348284e+001  3.0e-009 0.75  
34  3.9e-006 4.2e-002 2.9e-004 1.00e+000  1.145230022e+001  1.146320631e+001  2.7e-009 0.76  
35  3.5e-006 3.9e-002 2.6e-004 1.00e+000  1.145314110e+001  1.146295672e+001  2.4e-009 0.80  
36  3.2e-006 3.6e-002 2.3e-004 1.00e+000  1.145389731e+001  1.146273143e+001  2.2e-009 0.81  
37  2.9e-006 3.3e-002 2.1e-004 1.00e+000  1.145457741e+001  1.146252822e+001  1.9e-009 0.83  
38  2.6e-006 3.0e-002 1.9e-004 1.00e+000  1.145518915e+001  1.146234492e+001  1.7e-009 0.84  
39  2.3e-006 2.8e-002 1.7e-004 1.00e+000  1.145573942e+001  1.146217965e+001  1.6e-009 0.86  
40  2.1e-006 2.6e-002 1.5e-004 1.00e+000  1.145623444e+001  1.146203065e+001  1.4e-009 0.89  
41  1.9e-006 2.4e-002 1.4e-004 1.00e+000  1.145667977e+001  1.146189639e+001  1.3e-009 0.91  
42  1.7e-006 2.2e-002 1.2e-004 1.00e+000  1.145708043e+001  1.146177539e+001  1.1e-009 0.92  
43  1.5e-006 2.1e-002 1.1e-004 1.00e+000  1.145744091e+001  1.146166638e+001  1.0e-009 0.94  
44  1.4e-006 1.9e-002 1.0e-004 1.00e+000  1.145776526e+001  1.146156816e+001  9.3e-010 0.95  
45  1.2e-006 1.8e-002 9.0e-005 1.00e+000  1.145805709e+001  1.146147976e+001  8.4e-010 0.97  
46  1.1e-006 1.7e-002 8.1e-005 1.00e+000  1.145831968e+001  1.146140011e+001  7.5e-010 1.00  
47  1.0e-006 1.6e-002 7.3e-005 1.00e+000  1.145855598e+001  1.146132838e+001  6.8e-010 1.01  
48  9.0e-007 1.5e-002 6.6e-005 1.00e+000  1.145876863e+001  1.146126374e+001  6.1e-010 1.03  
49  8.1e-007 1.4e-002 5.9e-005 1.00e+000  1.145895996e+001  1.146120562e+001  5.5e-010 1.04  
50  7.3e-007 1.4e-002 5.3e-005 9.99e-001  1.145913212e+001  1.146115331e+001  4.9e-010 1.06  
51  6.6e-007 1.3e-002 4.8e-005 1.00e+000  1.145928709e+001  1.146110614e+001  4.4e-010 1.08  
52  2.3e-007 4.5e-003 1.7e-005 9.99e-001  1.146019675e+001  1.146082899e+001  1.5e-010 1.11  
53  2.1e-007 4.0e-003 1.5e-005 9.94e-001  1.146024547e+001  1.146081473e+001  1.4e-010 1.12  
54  7.1e-008 1.4e-003 5.1e-006 9.97e-001  1.146053212e+001  1.146072700e+001  4.8e-011 1.14  
55  6.4e-008 1.2e-003 4.6e-006 9.86e-001  1.146054703e+001  1.146072257e+001  4.3e-011 1.15  
56  5.7e-008 1.1e-003 4.1e-006 1.03e+000  1.146056224e+001  1.146071757e+001  3.9e-011 1.17  
57  5.2e-008 1.0e-003 3.7e-006 1.01e+000  1.146057465e+001  1.146071368e+001  3.5e-011 1.20  
58  2.0e-008 1.9e-004 7.2e-007 9.38e-001  1.146066167e+001  1.146068945e+001  7.7e-012 1.22  
59  1.7e-008 1.7e-004 6.5e-007 3.80e+000  1.146066368e+001  1.146068760e+001  6.9e-012 1.23  
60  5.6e-008 1.4e-005 5.2e-008 5.95e-001  1.146068223e+001  1.146068464e+001  1.6e-012 1.25  
Interior-point optimizer terminated. Time: 1.26. 

Optimizer terminated. Time: 1.28    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1460682228e+001   Viol.  con: 2e-006   var: 0e+000 
  Dual.    obj: 1.1460684636e+001   Viol.  con: 0e+000   var: 1e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.3 seconds.
result packing took 22% of solve time
solution checking took 7% 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               : Windows/64-X86  

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: 0.02    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
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          : 0.02            
Factor     - nonzeros before factor : 1.68e+004         after factor           : 1.72e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.288324415e+005 2.000000000e+000  1.0e+000 0.06  
1   1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265213496e+005 3.780478325e+000  4.6e-001 0.09  
2   3.9e+002 5.0e+002 2.2e+004 -9.34e-001 -1.195820381e+005 1.160497975e+001  1.7e-001 0.11  
3   2.8e+002 3.6e+002 1.6e+004 -8.26e-001 -1.156376925e+005 9.406063860e+001  1.2e-001 0.13  
4   2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.123257602e+005 2.800919474e+003  1.2e-001 0.14  
5   7.8e+001 1.0e+002 4.4e+003 -7.46e-001 -7.498595587e+004 1.053053373e+004  3.5e-002 0.17  
6   3.8e+001 4.9e+001 2.1e+003 -2.08e-001 -4.716319428e+004 1.110976922e+004  1.7e-002 0.19  
7   2.1e+001 2.8e+001 1.2e+003 2.72e-001  -3.073985570e+004 7.248977272e+003  9.5e-003 0.20  
8   9.8e+000 1.3e+001 5.5e+002 5.69e-001  -1.536080569e+004 3.891993678e+003  4.3e-003 0.23  
9   4.2e+000 5.5e+000 2.4e+002 8.19e-001  -6.677072567e+003 2.109882260e+003  1.9e-003 0.27  
10  2.0e+000 2.6e+000 1.1e+002 9.39e-001  -2.962336948e+003 1.171569887e+003  8.8e-004 0.30  
11  1.4e+000 1.8e+000 7.8e+001 9.83e-001  -2.096617830e+003 8.360466480e+002  6.2e-004 0.34  
12  9.0e-001 1.2e+000 5.1e+001 9.85e-001  -1.355787023e+003 5.626987060e+002  4.0e-004 0.38  
13  7.4e-001 1.1e+000 4.2e+001 9.64e-001  -1.126560879e+003 4.651700730e+002  3.3e-004 0.41  
14  2.6e-001 3.9e-001 1.5e+001 9.90e-001  -3.944824430e+002 1.817795259e+002  1.2e-004 0.44  
15  1.5e-001 2.3e-001 8.6e+000 1.00e+000  -2.189139983e+002 1.081347009e+002  6.9e-005 0.47  
16  4.0e-002 1.5e-001 2.4e+000 1.00e+000  -5.533058380e+001 3.458628662e+001  1.9e-005 0.52  
17  3.4e-002 1.3e-001 2.0e+000 1.00e+000  -4.533248822e+001 3.084995658e+001  1.6e-005 0.55  
18  2.2e-002 9.8e-002 1.3e+000 1.00e+000  -2.673494761e+001 2.258139596e+001  1.1e-005 0.59  
19  1.7e-002 7.9e-002 1.0e+000 1.01e+000  -1.833451970e+001 1.993911244e+001  8.3e-006 0.62  
20  1.4e-002 6.7e-002 8.5e-001 1.02e+000  -1.329132889e+001 1.873070088e+001  7.0e-006 0.67  
21  5.6e-003 6.1e-002 3.3e-001 1.02e+000  1.842881431e+000  1.419790190e+001  2.7e-006 0.72  
22  2.2e-003 6.3e-002 1.4e-001 1.02e+000  7.543479496e+000  1.254917527e+001  1.2e-006 0.75  
23  8.2e-004 6.3e-002 5.2e-002 9.85e-001  9.831460651e+000  1.177239700e+001  4.5e-007 0.78  
24  3.0e-004 7.5e-002 2.0e-002 9.69e-001  1.075368841e+001  1.152530689e+001  1.8e-007 0.81  
25  1.5e-004 5.9e-002 1.0e-002 9.56e-001  1.105420217e+001  1.143574670e+001  8.9e-008 0.84  
26  6.9e-005 5.8e-002 4.8e-003 9.86e-001  1.120799282e+001  1.139341482e+001  4.3e-008 0.86  
27  6.2e-005 5.3e-002 4.4e-003 9.94e-001  1.122412071e+001  1.139121081e+001  3.9e-008 0.89  
28  5.6e-005 4.8e-002 3.9e-003 9.92e-001  1.123687359e+001  1.138747346e+001  3.5e-008 0.91  
29  5.1e-005 4.4e-002 3.5e-003 9.91e-001  1.124866029e+001  1.138435494e+001  3.2e-008 0.92  
30  4.6e-005 4.0e-002 3.2e-003 9.90e-001  1.125920970e+001  1.138150042e+001  2.8e-008 0.94  
31  4.1e-005 3.7e-002 2.9e-003 9.90e-001  1.126873562e+001  1.137890219e+001  2.6e-008 0.95  
32  3.7e-005 3.4e-002 2.6e-003 9.90e-001  1.127730646e+001  1.137651918e+001  2.3e-008 0.98  
33  3.3e-005 3.1e-002 2.3e-003 9.90e-001  1.128499653e+001  1.137434200e+001  2.1e-008 1.00  
34  3.0e-005 2.9e-002 2.1e-003 9.90e-001  1.129190197e+001  1.137235214e+001  1.9e-008 1.01  
35  2.7e-005 2.7e-002 1.9e-003 9.91e-001  1.129809896e+001  1.137053806e+001  1.7e-008 1.03  
36  2.4e-005 2.5e-002 1.7e-003 9.91e-001  1.130366079e+001  1.136888299e+001  1.5e-008 1.04  
37  2.2e-005 2.3e-002 1.5e-003 9.91e-001  1.130865496e+001  1.136737741e+001  1.4e-008 1.08  
38  2.0e-005 2.1e-002 1.4e-003 9.92e-001  1.131313850e+001  1.136600801e+001  1.2e-008 1.09  
39  1.8e-005 2.0e-002 1.2e-003 9.92e-001  1.131716512e+001  1.136476383e+001  1.1e-008 1.11  
40  1.6e-005 1.9e-002 1.1e-003 9.92e-001  1.132078225e+001  1.136363505e+001  9.9e-009 1.12  
41  1.4e-005 1.8e-002 1.0e-003 9.93e-001  1.132403187e+001  1.136261164e+001  8.9e-009 1.14  
42  1.3e-005 1.7e-002 9.0e-004 9.93e-001  1.132695205e+001  1.136168477e+001  8.0e-009 1.16  
43  1.2e-005 1.6e-002 8.1e-004 9.94e-001  1.132957687e+001  1.136084608e+001  7.2e-009 1.19  
44  1.0e-005 1.5e-002 7.3e-004 9.94e-001  1.133193688e+001  1.136008784e+001  6.5e-009 1.20  
45  9.4e-006 1.4e-002 6.6e-004 9.95e-001  1.133405941e+001  1.135940297e+001  5.9e-009 1.22  
46  8.4e-006 1.3e-002 5.9e-004 9.96e-001  1.133596887e+001  1.135878477e+001  5.3e-009 1.23  
47  7.6e-006 1.3e-002 5.3e-004 9.96e-001  1.133768703e+001  1.135822693e+001  4.7e-009 1.25  
48  6.8e-006 1.2e-002 4.8e-004 9.97e-001  1.133923324e+001  1.135772365e+001  4.3e-009 1.26  
49  6.2e-006 1.2e-002 4.3e-004 9.97e-001  1.134062472e+001  1.135726964e+001  3.8e-009 1.29  
50  5.5e-006 1.1e-002 3.9e-004 9.98e-001  1.134187684e+001  1.135686003e+001  3.5e-009 1.31  
51  5.0e-006 1.1e-002 3.5e-004 9.98e-001  1.134300345e+001  1.135649045e+001  3.1e-009 1.33  
52  4.5e-006 1.0e-002 3.1e-004 9.98e-001  1.134401702e+001  1.135615697e+001  2.8e-009 1.34  
53  4.0e-006 1.0e-002 2.8e-004 9.98e-001  1.134492884e+001  1.135585609e+001  2.5e-009 1.36  
54  3.6e-006 9.7e-003 2.5e-004 9.99e-001  1.134574911e+001  1.135558467e+001  2.3e-009 1.39  
55  3.3e-006 9.5e-003 2.3e-004 9.99e-001  1.134648704e+001  1.135533987e+001  2.0e-009 1.40  
56  2.9e-006 9.2e-003 2.1e-004 9.99e-001  1.134715093e+001  1.135511915e+001  1.8e-009 1.42  
57  2.6e-006 9.0e-003 1.9e-004 9.99e-001  1.134774823e+001  1.135492020e+001  1.7e-009 1.44  
58  2.4e-006 8.8e-003 1.7e-004 9.99e-001  1.134828567e+001  1.135474091e+001  1.5e-009 1.45  
59  2.1e-006 8.6e-003 1.5e-004 9.99e-001  1.134876929e+001  1.135457935e+001  1.3e-009 1.48  
60  1.9e-006 8.5e-003 1.3e-004 9.99e-001  1.134920448e+001  1.135443383e+001  1.2e-009 1.50  
61  1.7e-006 8.3e-003 1.2e-004 9.99e-001  1.134959612e+001  1.135430278e+001  1.1e-009 1.51  
62  1.6e-006 8.2e-003 1.1e-004 1.00e+000  1.134994858e+001  1.135418476e+001  9.8e-010 1.53  
63  1.4e-006 8.1e-003 9.8e-005 9.99e-001  1.135026578e+001  1.135407855e+001  8.8e-010 1.54  
64  1.3e-006 8.0e-003 8.9e-005 1.00e+000  1.135055128e+001  1.135398289e+001  7.9e-010 1.56  
65  1.1e-006 7.9e-003 8.0e-005 1.00e+000  1.135080823e+001  1.135389677e+001  7.1e-010 1.59  
66  1.0e-006 7.8e-003 7.2e-005 1.00e+000  1.135103950e+001  1.135381928e+001  6.4e-010 1.61  
67  9.2e-007 7.7e-003 6.5e-005 1.00e+000  1.135124766e+001  1.135374952e+001  5.8e-010 1.62  
68  8.3e-007 7.6e-003 5.8e-005 1.00e+000  1.135143502e+001  1.135368672e+001  5.2e-010 1.64  
69  7.5e-007 7.6e-003 5.2e-005 1.00e+000  1.135160365e+001  1.135363024e+001  4.7e-010 1.65  
70  6.7e-007 7.5e-003 4.7e-005 1.00e+000  1.135175543e+001  1.135357939e+001  4.2e-010 1.67  
71  6.1e-007 7.5e-003 4.2e-005 1.00e+000  1.135189205e+001  1.135353363e+001  3.8e-010 1.70  
72  5.5e-007 7.4e-003 3.8e-005 1.00e+000  1.135201501e+001  1.135349246e+001  3.4e-010 1.72  
73  4.9e-007 7.4e-003 3.4e-005 1.00e+000  1.135212568e+001  1.135345538e+001  3.1e-010 1.73  
74  4.4e-007 7.3e-003 3.1e-005 9.99e-001  1.135222529e+001  1.135342206e+001  2.8e-010 1.75  
75  4.0e-007 7.3e-003 2.8e-005 1.00e+000  1.135231494e+001  1.135339204e+001  2.5e-010 1.76  
76  3.6e-007 7.3e-003 2.5e-005 1.00e+000  1.135239564e+001  1.135336503e+001  2.2e-010 1.78  
77  3.2e-007 7.2e-003 2.3e-005 1.00e+000  1.135246826e+001  1.135334073e+001  2.0e-010 1.81  
78  2.9e-007 7.2e-003 2.0e-005 1.00e+000  1.135253362e+001  1.135331884e+001  1.8e-010 1.83  
79  2.6e-007 7.2e-003 1.8e-005 1.00e+000  1.135259245e+001  1.135329915e+001  1.6e-010 1.84  
80  2.3e-007 7.1e-003 1.6e-005 1.00e+000  1.135264540e+001  1.135328142e+001  1.5e-010 1.87  
81  2.1e-007 7.1e-003 1.5e-005 1.00e+000  1.135269305e+001  1.135326547e+001  1.3e-010 1.89  
82  1.9e-007 7.1e-003 1.3e-005 1.00e+000  1.135273594e+001  1.135325111e+001  1.2e-010 1.90  
83  1.7e-007 7.1e-003 1.2e-005 1.00e+000  1.135277454e+001  1.135323817e+001  1.1e-010 1.92  
84  1.5e-007 7.1e-003 1.1e-005 9.99e-001  1.135280927e+001  1.135322656e+001  9.6e-011 1.94  
85  1.4e-007 7.1e-003 9.7e-006 1.00e+000  1.135284054e+001  1.135321610e+001  8.7e-011 1.95  
86  1.2e-007 7.0e-003 8.7e-006 9.97e-001  1.135286866e+001  1.135320671e+001  7.8e-011 1.98  
87  1.1e-007 7.0e-003 7.9e-006 1.00e+000  1.135289398e+001  1.135319822e+001  7.0e-011 2.00  
88  1.0e-007 7.0e-003 7.1e-006 1.00e+000  1.135291677e+001  1.135319059e+001  6.3e-011 2.03  
89  9.1e-008 7.0e-003 6.4e-006 1.00e+000  1.135293728e+001  1.135318371e+001  5.7e-011 2.04  
90  8.2e-008 7.0e-003 5.7e-006 9.99e-001  1.135295574e+001  1.135317753e+001  5.1e-011 2.06  
91  7.4e-008 7.0e-003 5.2e-006 1.00e+000  1.135297235e+001  1.135317195e+001  4.6e-011 2.08  
92  6.6e-008 6.3e-003 4.6e-006 1.00e+000  1.135298750e+001  1.135316684e+001  4.2e-011 2.09  
93  6.0e-008 5.7e-003 4.2e-006 1.00e+000  1.135300094e+001  1.135316234e+001  3.7e-011 2.11  
94  5.4e-008 5.1e-003 3.8e-006 1.00e+000  1.135301303e+001  1.135315829e+001  3.4e-011 2.14  
95  4.8e-008 4.6e-003 3.4e-006 1.00e+000  1.135302391e+001  1.135315463e+001  3.0e-011 2.15  
96  4.4e-008 4.1e-003 3.0e-006 1.00e+000  1.135303370e+001  1.135315135e+001  2.7e-011 2.17  
97  3.9e-008 3.7e-003 2.7e-006 1.01e+000  1.135304278e+001  1.135314828e+001  2.5e-011 2.18  
98  3.5e-008 3.3e-003 2.5e-006 1.00e+000  1.135305068e+001  1.135314563e+001  2.2e-011 2.20  
99  3.2e-008 3.0e-003 2.2e-006 9.95e-001  1.135305779e+001  1.135314326e+001  2.0e-011 2.21  
100 2.9e-008 2.7e-003 2.0e-006 1.00e+000  1.135306420e+001  1.135314111e+001  1.8e-011 2.25  
101 2.6e-008 2.4e-003 1.8e-006 1.00e+000  1.135306997e+001  1.135313917e+001  1.6e-011 2.26  
102 2.3e-008 2.2e-003 1.6e-006 1.00e+000  1.135307521e+001  1.135313740e+001  1.5e-011 2.28  
103 2.1e-008 2.0e-003 1.5e-006 1.01e+000  1.135308000e+001  1.135313578e+001  1.3e-011 2.29  
104 1.9e-008 1.8e-003 1.3e-006 1.01e+000  1.135308431e+001  1.135313433e+001  1.2e-011 2.31  
105 1.7e-008 1.6e-003 1.2e-006 1.00e+000  1.135308810e+001  1.135313306e+001  1.1e-011 2.33  
106 1.5e-008 1.4e-003 1.1e-006 1.01e+000  1.135309163e+001  1.135313186e+001  9.7e-012 2.34  
107 1.4e-008 1.3e-003 9.5e-007 1.01e+000  1.135309481e+001  1.135313077e+001  8.8e-012 2.37  
108 1.2e-008 1.2e-003 8.6e-007 1.00e+000  1.135309755e+001  1.135312986e+001  7.9e-012 2.39  
109 1.1e-008 1.0e-003 7.7e-007 1.02e+000  1.135310019e+001  1.135312896e+001  7.2e-012 2.40  
110 2.0e-009 1.1e-004 8.0e-008 9.91e-001  1.135311959e+001  1.135312257e+001  7.7e-013 2.42  
Interior-point optimizer terminated. Time: 2.43. 

Optimizer terminated. Time: 2.45    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1353119591e+001   Viol.  con: 4e-008   var: 0e+000 
  Dual.    obj: 1.1353122570e+001   Viol.  con: 0e+000   var: 8e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.47 seconds.
result packing took 12% of solve time
solution checking took 3.7% 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               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1900            
  Cones                  : 0               
  Scalar variables       : 6471            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1010
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1022
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 1022            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.02    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 6               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 831
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3581              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.01            
Factor     - nonzeros before factor : 1.67e+004         after factor           : 1.72e+005       
Factor     - dense dim.             : 0                 flops                  : 0.00e+000       
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+000       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.0e+003 1.3e+005 0.00e+000  -1.288989318e+005 2.000000000e+000  1.0e+000 0.08  
1   1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265802117e+005 3.775668869e+000  4.6e-001 0.11  
2   3.9e+002 4.9e+002 2.2e+004 -9.34e-001 -1.195425647e+005 1.174714963e+001  1.7e-001 0.14  
3   2.8e+002 3.6e+002 1.6e+004 -8.25e-001 -1.156771027e+005 1.073495973e+002  1.2e-001 0.17  
4   2.8e+002 3.6e+002 1.5e+004 -7.56e-001 -1.123107964e+005 2.790047089e+003  1.2e-001 0.20  
5   7.4e+001 9.5e+001 4.1e+003 -7.45e-001 -7.260007561e+004 1.112166068e+004  3.3e-002 0.23  
6   3.6e+001 4.6e+001 2.0e+003 -1.71e-001 -4.492718968e+004 1.109794297e+004  1.6e-002 0.27  
7   2.0e+001 2.6e+001 1.1e+003 3.12e-001  -2.924714283e+004 7.332259417e+003  9.0e-003 0.28  
8   9.9e+000 1.3e+001 5.5e+002 5.95e-001  -1.542186486e+004 3.974970857e+003  4.4e-003 0.30  
9   4.3e+000 5.6e+000 2.4e+002 8.20e-001  -6.792441341e+003 2.117897678e+003  1.9e-003 0.33  
10  1.6e+000 2.2e+000 9.3e+001 9.39e-001  -2.451019389e+003 1.018926495e+003  7.4e-004 0.34  
11  1.1e+000 1.4e+000 6.1e+001 9.88e-001  -1.614376764e+003 6.812117657e+002  4.9e-004 0.36  
12  8.2e-001 1.1e+000 4.6e+001 9.82e-001  -1.244408749e+003 5.225492207e+002  3.7e-004 0.37  
13  5.6e-001 7.4e-001 3.2e+001 9.86e-001  -8.393112859e+002 3.762598370e+002  2.6e-004 0.39  
14  2.1e-001 2.8e-001 1.2e+001 9.90e-001  -3.166224681e+002 1.401723025e+002  9.6e-005 0.41  
15  8.6e-002 1.4e-001 5.0e+000 1.01e+000  -1.252936499e+002 6.506679359e+001  4.1e-005 0.42  
16  3.6e-002 9.6e-002 2.1e+000 1.01e+000  -4.909111481e+001 3.144741179e+001  1.7e-005 0.45  
17  2.9e-002 8.1e-002 1.7e+000 9.96e-001  -3.797568783e+001 2.779993397e+001  1.4e-005 0.47  
18  1.8e-002 6.5e-002 1.1e+000 1.01e+000  -1.992742726e+001 2.055570943e+001  8.8e-006 0.50  
19  1.6e-002 5.8e-002 9.5e-001 1.02e+000  -1.632171948e+001 1.965869633e+001  7.8e-006 0.52  
20  5.9e-003 6.8e-002 3.5e-001 1.02e+000  1.277391214e+000  1.428474983e+001  2.9e-006 0.53  
21  2.0e-003 7.8e-002 1.2e-001 1.02e+000  7.855651763e+000  1.242486530e+001  1.1e-006 0.55  
22  1.4e-003 5.8e-002 8.6e-002 9.67e-001  8.829707267e+000  1.205073514e+001  7.4e-007 0.56  
23  4.9e-004 6.7e-002 3.2e-002 9.57e-001  1.038359508e+001  1.160551996e+001  2.8e-007 0.58  
24  2.0e-004 5.9e-002 1.4e-002 9.55e-001  1.090877478e+001  1.143380229e+001  1.2e-007 0.61  
25  1.8e-004 5.4e-002 1.2e-002 9.73e-001  1.094788966e+001  1.142020520e+001  1.1e-007 0.62  
26  1.6e-004 4.9e-002 1.1e-002 9.71e-001  1.098418770e+001  1.140986368e+001  9.9e-008 0.64  
27  1.5e-004 4.5e-002 9.9e-003 9.73e-001  1.101972147e+001  1.140343960e+001  8.9e-008 0.67  
28  1.3e-004 4.1e-002 8.9e-003 9.75e-001  1.105185912e+001  1.139773277e+001  8.0e-008 0.69  
29  1.2e-004 3.8e-002 8.0e-003 9.77e-001  1.108080711e+001  1.139253487e+001  7.2e-008 0.70  
30  1.1e-004 3.4e-002 7.2e-003 9.79e-001  1.110681682e+001  1.138773838e+001  6.5e-008 0.72  
31  9.6e-005 3.2e-002 6.5e-003 9.81e-001  1.113017633e+001  1.138330962e+001  5.8e-008 0.73  
32  8.7e-005 2.9e-002 5.8e-003 9.83e-001  1.115114843e+001  1.137921998e+001  5.3e-008 0.75  
33  7.8e-005 2.7e-002 5.3e-003 9.84e-001  1.116997224e+001  1.137544463e+001  4.7e-008 0.76  
34  7.0e-005 2.5e-002 4.7e-003 9.86e-001  1.118686439e+001  1.137196138e+001  4.3e-008 0.80  
35  6.3e-005 2.3e-002 4.3e-003 9.87e-001  1.120202067e+001  1.136874969e+001  3.8e-008 0.81  
36  5.7e-005 2.2e-002 3.8e-003 9.88e-001  1.121561831e+001  1.136579123e+001  3.5e-008 0.83  
37  5.1e-005 2.0e-002 3.5e-003 9.89e-001  1.122781703e+001  1.136306880e+001  3.1e-008 0.84  
38  4.6e-005 1.9e-002 3.1e-003 9.90e-001  1.123876068e+001  1.136056633e+001  2.8e-008 0.86  
39  4.2e-005 1.8e-002 2.8e-003 9.91e-001  1.124857851e+001  1.135826851e+001  2.5e-008 0.87  
40  3.7e-005 1.7e-002 2.5e-003 9.92e-001  1.125738656e+001  1.135616085e+001  2.3e-008 0.91  
41  3.4e-005 1.6e-002 2.3e-003 9.93e-001  1.126528886e+001  1.135422936e+001  2.0e-008 0.92  
42  3.0e-005 1.5e-002 2.0e-003 9.94e-001  1.127237887e+001  1.135246106e+001  1.8e-008 0.94  
43  2.7e-005 1.4e-002 1.8e-003 9.94e-001  1.127874053e+001  1.135084381e+001  1.7e-008 0.95  
44  2.5e-005 1.3e-002 1.7e-003 9.95e-001  1.128444929e+001  1.134936618e+001  1.5e-008 0.97  
45  2.2e-005 1.3e-002 1.5e-003 9.95e-001  1.128957303e+001  1.134801774e+001  1.3e-008 0.98  
46  2.0e-005 1.2e-002 1.3e-003 9.96e-001  1.129417257e+001  1.134678877e+001  1.2e-008 1.00  
47  1.8e-005 1.2e-002 1.2e-003 9.96e-001  1.129830222e+001  1.134566985e+001  1.1e-008 1.03  
48  1.6e-005 1.1e-002 1.1e-003 9.97e-001  1.130201058e+001  1.134465209e+001  9.8e-009 1.04  
49  1.4e-005 1.1e-002 9.8e-004 9.97e-001  1.130534118e+001  1.134372725e+001  8.8e-009 1.06  
50  1.3e-005 1.0e-002 8.8e-004 9.97e-001  1.130833294e+001  1.134288751e+001  7.9e-009 1.08  
51  1.2e-005 1.0e-002 7.9e-004 9.98e-001  1.131102074e+001  1.134212557e+001  7.1e-009 1.09  
52  1.1e-005 9.8e-003 7.1e-004 9.98e-001  1.131343582e+001  1.134143482e+001  6.4e-009 1.11  
53  9.5e-006 9.6e-003 6.4e-004 9.98e-001  1.131560610e+001  1.134080907e+001  5.8e-009 1.12  
54  8.5e-006 9.3e-003 5.8e-004 9.98e-001  1.131755660e+001  1.134024232e+001  5.2e-009 1.15  
55  7.7e-006 9.1e-003 5.2e-004 9.98e-001  1.131930977e+001  1.133972951e+001  4.7e-009 1.17  
56  6.9e-006 8.9e-003 4.7e-004 9.99e-001  1.132088568e+001  1.133926549e+001  4.2e-009 1.19  
57  6.2e-006 8.7e-003 4.2e-004 9.99e-001  1.132230235e+001  1.133884590e+001  3.8e-009 1.20  
58  5.6e-006 8.5e-003 3.8e-004 9.99e-001  1.132357593e+001  1.133846653e+001  3.4e-009 1.22  
59  5.0e-006 8.4e-003 3.4e-004 9.99e-001  1.132472092e+001  1.133812360e+001  3.1e-009 1.23  
60  4.5e-006 8.3e-003 3.1e-004 9.99e-001  1.132575035e+001  1.133781369e+001  2.8e-009 1.25  
61  4.1e-006 8.1e-003 2.8e-004 9.99e-001  1.132667594e+001  1.133753367e+001  2.5e-009 1.28  
62  3.7e-006 8.0e-003 2.5e-004 9.99e-001  1.132750820e+001  1.133728071e+001  2.2e-009 1.29  
63  3.3e-006 7.9e-003 2.2e-004 9.99e-001  1.132825660e+001  1.133705236e+001  2.0e-009 1.31  
64  3.0e-006 7.8e-003 2.0e-004 1.00e+000  1.132892965e+001  1.133684624e+001  1.8e-009 1.33  
65  2.7e-006 7.8e-003 1.8e-004 9.99e-001  1.132953500e+001  1.133666028e+001  1.6e-009 1.34  
66  2.4e-006 7.7e-003 1.6e-004 1.00e+000  1.133007952e+001  1.133649252e+001  1.5e-009 1.36  
67  2.2e-006 7.6e-003 1.5e-004 1.00e+000  1.133056937e+001  1.133634124e+001  1.3e-009 1.37  
68  2.0e-006 7.6e-003 1.3e-004 1.00e+000  1.133101005e+001  1.133620489e+001  1.2e-009 1.39  
69  1.8e-006 7.5e-003 1.2e-004 1.00e+000  1.133140654e+001  1.133608201e+001  1.1e-009 1.42  
70  1.6e-006 7.4e-003 1.1e-004 1.00e+000  1.133176327e+001  1.133597129e+001  9.6e-010 1.44  
71  1.4e-006 7.4e-003 9.6e-005 1.00e+000  1.133208427e+001  1.133587153e+001  8.7e-010 1.45  
72  1.3e-006 7.3e-003 8.7e-005 1.00e+000  1.133237310e+001  1.133578169e+001  7.8e-010 1.47  
73  1.2e-006 7.3e-003 7.8e-005 1.00e+000  1.133263300e+001  1.133570080e+001  7.0e-010 1.48  
74  1.0e-006 7.3e-003 7.0e-005 1.00e+000  1.133286686e+001  1.133562798e+001  6.3e-010 1.50  
75  9.4e-007 7.2e-003 6.3e-005 1.00e+000  1.133307732e+001  1.133556238e+001  5.7e-010 1.51  
76  8.4e-007 7.2e-003 5.7e-005 1.00e+000  1.133326671e+001  1.133550332e+001  5.1e-010 1.54  
77  7.6e-007 7.2e-003 5.1e-005 1.00e+000  1.133343715e+001  1.133545015e+001  4.6e-010 1.56  
78  6.8e-007 7.1e-003 4.6e-005 1.00e+000  1.133359052e+001  1.133540227e+001  4.1e-010 1.58  
79  6.1e-007 7.1e-003 4.1e-005 1.00e+000  1.133372856e+001  1.133535914e+001  3.7e-010 1.59  
80  5.5e-007 7.1e-003 3.7e-005 1.00e+000  1.133385279e+001  1.133532028e+001  3.4e-010 1.62  
81  5.0e-007 7.1e-003 3.4e-005 1.00e+000  1.133396458e+001  1.133528532e+001  3.0e-010 1.64  
82  4.5e-007 7.1e-003 3.0e-005 1.00e+000  1.133406519e+001  1.133525385e+001  2.7e-010 1.65  
83  4.0e-007 7.0e-003 2.7e-005 1.00e+000  1.133415573e+001  1.133522551e+001  2.5e-010 1.67  
84  3.6e-007 7.0e-003 2.4e-005 9.99e-001  1.133423720e+001  1.133520004e+001  2.2e-010 1.69  
85  3.3e-007 7.0e-003 2.2e-005 9.99e-001  1.133431051e+001  1.133517710e+001  2.0e-010 1.70  
86  2.9e-007 7.0e-003 2.0e-005 1.00e+000  1.133437650e+001  1.133515643e+001  1.8e-010 1.73  
87  2.6e-007 7.0e-003 1.8e-005 1.00e+000  1.133443589e+001  1.133513782e+001  1.6e-010 1.75  
88  2.4e-007 7.0e-003 1.6e-005 9.98e-001  1.133448931e+001  1.133512111e+001  1.4e-010 1.76  
89  2.1e-007 6.9e-003 1.4e-005 9.98e-001  1.133453739e+001  1.133510607e+001  1.3e-010 1.78  
90  1.9e-007 6.9e-003 1.3e-005 9.98e-001  1.133458067e+001  1.133509252e+001  1.2e-010 1.79  
91  1.7e-007 6.9e-003 1.2e-005 1.00e+000  1.133461962e+001  1.133508029e+001  1.1e-010 1.81  
92  1.6e-007 6.9e-003 1.1e-005 1.00e+000  1.133465467e+001  1.133506927e+001  9.5e-011 1.84  
93  1.4e-007 6.9e-003 9.5e-006 1.00e+000  1.133468622e+001  1.133505935e+001  8.5e-011 1.86  
94  1.3e-007 6.9e-003 8.5e-006 9.99e-001  1.133471461e+001  1.133505043e+001  7.7e-011 1.87  
95  1.1e-007 6.2e-003 7.7e-006 1.00e+000  1.133474027e+001  1.133504234e+001  6.9e-011 1.89  
96  1.0e-007 5.6e-003 6.9e-006 9.99e-001  1.133476324e+001  1.133503513e+001  6.2e-011 1.90  
97  9.2e-008 5.0e-003 6.2e-006 9.97e-001  1.133478392e+001  1.133502865e+001  5.6e-011 1.92  
98  8.3e-008 4.5e-003 5.6e-006 9.95e-001  1.133480252e+001  1.133502283e+001  5.0e-011 1.93  
99  7.5e-008 4.1e-003 5.0e-006 1.00e+000  1.133481930e+001  1.133501753e+001  4.5e-011 1.95  
100 6.7e-008 3.7e-003 4.5e-006 9.99e-001  1.133483437e+001  1.133501279e+001  4.1e-011 1.98  
101 6.0e-008 3.3e-003 4.1e-006 1.00e+000  1.133484797e+001  1.133500849e+001  3.7e-011 2.00  
102 5.4e-008 3.0e-003 3.7e-006 1.00e+000  1.133486027e+001  1.133500459e+001  3.3e-011 2.01  
103 4.9e-008 2.7e-003 3.3e-006 1.00e+000  1.133487125e+001  1.133500113e+001  3.0e-011 2.03  
104 4.4e-008 2.4e-003 3.0e-006 9.96e-001  1.133488111e+001  1.133499804e+001  2.7e-011 2.04  
105 4.0e-008 2.2e-003 2.7e-006 9.94e-001  1.133488999e+001  1.133499526e+001  2.4e-011 2.06  
106 3.6e-008 1.9e-003 2.4e-006 1.01e+000  1.133489822e+001  1.133499263e+001  2.2e-011 2.08  
107 3.2e-008 1.8e-003 2.2e-006 1.00e+000  1.133490543e+001  1.133499035e+001  2.0e-011 2.11  
108 2.9e-008 1.6e-003 2.0e-006 9.87e-001  1.133491188e+001  1.133498835e+001  1.8e-011 2.12  
109 2.6e-008 1.4e-003 1.8e-006 9.87e-001  1.133491767e+001  1.133498654e+001  1.6e-011 2.14  
110 2.3e-008 1.3e-003 1.6e-006 1.02e+000  1.133492333e+001  1.133498471e+001  1.4e-011 2.15  
111 4.8e-009 2.4e-004 3.0e-007 9.88e-001  1.133496114e+001  1.133497291e+001  2.8e-012 2.17  
112 3.4e-010 1.4e-005 1.7e-008 1.00e+000  1.133496943e+001  1.133497009e+001  1.5e-013 2.18  
Interior-point optimizer terminated. Time: 2.20. 

Optimizer terminated. Time: 2.21    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1334969431e+001   Viol.  con: 5e-009   var: 0e+000 
  Dual.    obj: 1.1334970094e+001   Viol.  con: 0e+000   var: 1e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.23 seconds.
result packing took 78% of solve time
solution checking took 3.9% of solve time
Solving took 6 GP solves and 24.7 seconds.
Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2418945.71798 force_pound * meter but the right hand side evaluated to 2375460.36735 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 32774.3865504 force_pound but the right hand side evaluated to 32399.999998 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 2.21510116795 meter but the right hand side evaluated to 2.08159110542 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 1243578.05259 joule / kilogram but the right hand side evaluated to 1.56109266467 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 664758.310553 joule / kilogram but the right hand side evaluated to 0.667336301085 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 18.3998942392 meter but the right hand side evaluated to 16.3229078315 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 10.903622924166037 but the right hand side evaluated to 4.788859476106651 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.019786684094244 but the right hand side evaluated to 4.7888594670240785 (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 8.144913995856374 but the right hand side evaluated to 4.788859478311611 (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 18.362248027 meter but the right hand side evaluated to 18.1377342013 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 18.362248027 meter but the right hand side evaluated to 18.2420716184 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 0.29603600380158834 but the right hand side evaluated to 0.189739052424572 (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 0.23302138404753414 but the right hand side evaluated to 0.1743467327215059 (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 7.563246536938309 but the right hand side evaluated to 4.730639761028604 (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 7.583090081765842 but the right hand side evaluated to 4.757852792619396 (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


Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 35.755s

OK

Generating XML reports...
Cloning into 'solar'...
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0)
grin 1.2.1 requires argparse>=1.1, which is not installed.
Collecting git+https://github.com/convexengineering/gpfit.git
  Cloning https://github.com/convexengineering/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-5ek0zp
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-uetw9w\wheels\d5\94\ac\b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
Collecting git+https://github.com/convexengineering/gassolar.git
  Cloning https://github.com/convexengineering/gassolar.git to c:\users\jenkins\appdata\local\temp\pip-req-build-juz9qt
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-otiwke\wheels\fe\11\0a\2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
grin 1.2.1 requires argparse>=1.1, which is not installed.
Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\solar
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in d:\jenkins\workspace\gplibrary_pr_models\mosek (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2017.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-3uajze\wheels\9f\ae\a9\52e286ff9ea1428d6dd1e8c6df0d12b22c44363d9dcc1dd331
Successfully built solar
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: solar
Successfully installed solar-0.0.0.0
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 4.67 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 1388463.0580 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 1248776.3209 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/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 5.59 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 1388463.0786 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 1248776.3394 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 2.29645501028 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194416 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)

Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.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)
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)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 3.74 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 765970.5568 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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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 3.06 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 862671.9760 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 seconds.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1202 but bound is 0.9465
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 987087.2997 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 6269 variables.
Solving took 1.4 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.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.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)
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)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 3.99 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 765970.5365 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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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 3.95 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 862671.9762 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 3.87 seconds.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1202 but bound is 0.9465
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 987087.2997 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 6269 variables.
Solving took 1.62 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 26.9 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 1388463.0670 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 1248776.3289 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 2.29645501007 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194395 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 5.7 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 1388463.0612 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 1248776.3238 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 2.29645501004 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194393 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 0.349 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 838075.6769 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 5.8 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 1017215.9327 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 2.62125883032 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124747946 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 1.95293542208 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215299 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 1.04275941612 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521707 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 0.46769813422 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697003882 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 0.139006791929 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006573774 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 0.653 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]'
Infeasible mono
Running tests...
----------------------------------------------------------------------
..D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
  tau = np.exp(-0.175/costhsun)
....EE
======================================================================
ERROR [10.534s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "d:\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 "d:\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 "d:\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 "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 83, in __init__
    CostedConstraintSet.__init__(self, cost, constraints, substitutions)
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__
    ConstraintSet.__init__(self, constraints, subs)
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__
    list.__setitem__(self, i, ConstraintSet(constraint))
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__
    raise_elementhasnumpybools(constraint)
  File "d:\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 [12.368s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "d:\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 "d:\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 "d:\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 "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 83, in __init__
    CostedConstraintSet.__init__(self, cost, mial 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]'
constraints, substitutions)
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__
    ConstraintSet.__init__(self, constraints, subs)
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__
    list.__setitem__(self, i, ConstraintSet(constraint))
  File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__
    raise_elementhasnumpybools(constraint)
  File "d:\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 507.266s

FAILED (errors=2)

Generating XML reports...
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0)
grin 1.2.1 requires argparse>=1.1, which is not installed.
Collecting git+https://github.com/hoburg/gpfit.git
  Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-gx5a6s
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-zuz2pn\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gplibrary
Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-juw3qj\wheels\4a\da\60\bea5372bf288606a399bdc749979f532f5aff24f4c362a9887
Successfully built gpkitmodels
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: gpkitmodels
  Found existing installation: gpkitmodels 0.0.0.0
    Uninstalling gpkitmodels-0.0.0.0:
      Successfully uninstalled gpkitmodels-0.0.0.0
Successfully installed gpkitmodels-0.0.0.0
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 0.031 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.126 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.039 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.027 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.02 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 2.9 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 985.544371538 meter * revolutions_per_minute but the right hand side evaluated to 103.041409432 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 0.420585925092 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573145032 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 0.314645033966 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629895202 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 0.168936438406 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931603971 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 0.0639642380881 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631380004 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 0.0226356535444 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354005892 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)

Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.091 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.11 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.124 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 5.04 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 0.019 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 1.94 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 1619897.4167 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.088 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 3.38 seconds.
Warning: Constraint [omega_BladeElementProp/BladeElementPerf_(0,)*r_BladeElementProp/BladeElementPerf_(0,) [m*rpm]... >= Wt_BladeElementProp/BladeElementPerf_(0,) + vt_BladeElementProp/BladeElementPerf_(0,) [m/s]...] is not tight because the left hand side evaluated to 147.268875342 meter * revolutions_per_minute but the right hand side evaluated to 15.4219435408 meter / second (Allowable error: 0.0001%, Actual error: 0.00011%)

Warning: Constraint [dQ_BladeElementProp/BladeElementPerf_(3,) [N*m]... >= B_BladeElementProp/BladeElementPerf_(3,)*G_BladeElementProp/BladeElementPerf_(3,)*Wa_BladeElementPro...] is not tight because the left hand side evaluated to 42.7884411703 meter * newton but the right hand side evaluated to 42.7884887635 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%)

Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3481 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9721 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3856 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9562 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.2729 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.1579 but bound is 700000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000

Running tests...
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..........
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Ran 10 tests in 21.734s

OK

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adding test for 'aircraft_models.py'

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 2.783s

OK

Generating XML reports...
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['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 ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['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 ['pip', 'install', 'pandas']
  attempt 1
calling ['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 ['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 ['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 ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
  attempt 1
calling ['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 ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {})


(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>exit 0 
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 'D:\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