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Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3581              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.06              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.04            
Factor     - nonzeros before factor : 1.67e+04          after factor           : 1.72e+05        
Factor     - dense dim.             : 0                 flops                  : 0.00e+00        
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+00        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.3e+05  0.00e+00   -1.289101986e+05  2.000000000e+00   1.0e+00  0.08  
1   1.1e+03  1.4e+03  5.9e+04  -9.71e-01  -1.266148481e+05  3.779171660e+00   4.6e-01  0.13  
2   4.0e+02  5.1e+02  2.2e+04  -9.34e-01  -1.198562621e+05  1.137222373e+01   1.7e-01  0.17  
3   2.8e+02  3.6e+02  1.6e+04  -8.29e-01  -1.157240094e+05  8.367320555e+01   1.2e-01  0.20  
4   2.8e+02  3.6e+02  1.6e+04  -7.56e-01  -1.124197013e+05  2.832680409e+03   1.2e-01  0.24  
5   6.3e+01  8.2e+01  3.6e+03  -7.47e-01  -6.640324331e+04  1.270004769e+04   2.8e-02  0.27  
6   3.9e+01  5.1e+01  2.2e+03  -7.19e-02  -4.860608237e+04  1.113878014e+04   1.7e-02  0.31  
7   2.8e+01  3.7e+01  1.6e+03  2.50e-01   -3.839140660e+04  8.758862150e+03   1.3e-02  0.34  
8   1.6e+01  2.1e+01  9.0e+02  4.36e-01   -2.428153002e+04  5.454554396e+03   7.1e-03  0.38  
9   6.4e+00  8.3e+00  3.6e+02  6.74e-01   -1.033403666e+04  2.810589102e+03   2.9e-03  0.41  
10  3.6e+00  4.7e+00  2.0e+02  8.87e-01   -5.635335184e+03  1.899052609e+03   1.6e-03  0.45  
11  1.3e+00  1.7e+00  7.5e+01  9.54e-01   -2.012985035e+03  7.892065018e+02   5.9e-04  0.48  
12  1.0e+00  1.3e+00  5.7e+01  9.87e-01   -1.520029024e+03  6.366028306e+02   4.5e-04  0.52  
13  8.5e-01  1.5e+00  4.8e+01  9.70e-01   -1.298899286e+03  5.502975739e+02   3.9e-04  0.56  
14  2.9e-01  5.1e-01  1.6e+01  9.89e-01   -4.334606808e+02  1.970004710e+02   1.3e-04  0.59  
15  1.6e-01  3.0e-01  9.3e+00  1.00e+00   -2.379441482e+02  1.162352476e+02   7.5e-05  0.63  
16  7.3e-02  1.6e-01  4.2e+00  1.00e+00   -1.038568093e+02  5.761846863e+01   3.4e-05  0.66  
17  3.5e-02  1.0e-01  2.1e+00  1.01e+00   -4.581798158e+01  3.218150071e+01   1.7e-05  0.70  
18  1.8e-02  7.9e-02  1.1e+00  1.01e+00   -2.038674659e+01  2.046073890e+01   8.8e-06  0.73  
19  1.8e-02  7.6e-02  1.0e+00  1.02e+00   -1.899832273e+01  2.043772596e+01   8.5e-06  0.77  
20  9.7e-03  5.8e-02  5.7e-01  1.02e+00   -4.741714835e+00  1.674420296e+01   4.7e-06  0.80  
21  4.1e-03  5.8e-02  2.5e-01  1.02e+00   4.583125027e+00   1.368808730e+01   2.0e-06  0.83  
22  2.1e-03  5.2e-02  1.3e-01  1.01e+00   7.768898043e+00   1.261360565e+01   1.1e-06  0.86  
23  6.0e-04  8.2e-02  3.9e-02  9.87e-01   1.034300360e+01   1.181152710e+01   3.4e-07  0.90  
24  1.8e-04  8.8e-02  1.3e-02  9.78e-01   1.109075318e+01   1.156935857e+01   1.1e-07  0.93  
25  6.0e-05  8.7e-02  4.3e-03  9.88e-01   1.133248188e+01   1.149489276e+01   3.9e-08  0.97  
26  2.2e-05  8.4e-02  1.6e-03  9.96e-01   1.141328772e+01   1.147317517e+01   1.5e-08  1.00  
27  8.2e-06  8.1e-02  6.0e-04  9.99e-01   1.144292979e+01   1.146572770e+01   5.6e-09  1.03  
28  7.4e-06  7.4e-02  5.4e-04  1.00e+00   1.144485717e+01   1.146537670e+01   5.0e-09  1.06  
29  6.7e-06  6.7e-02  4.9e-04  1.00e+00   1.144644936e+01   1.146491732e+01   4.5e-09  1.10  
30  6.0e-06  6.1e-02  4.4e-04  1.00e+00   1.144788199e+01   1.146450351e+01   4.1e-09  1.14  
31  5.4e-06  5.6e-02  3.9e-04  1.00e+00   1.144916871e+01   1.146412834e+01   3.7e-09  1.17  
32  4.9e-06  5.1e-02  3.5e-04  1.00e+00   1.145032558e+01   1.146378946e+01   3.3e-09  1.21  
33  4.4e-06  4.6e-02  3.2e-04  1.00e+00   1.145136561e+01   1.146348327e+01   3.0e-09  1.24  
34  3.9e-06  4.2e-02  2.9e-04  1.00e+00   1.145230074e+01   1.146320674e+01   2.7e-09  1.28  
35  3.5e-06  3.9e-02  2.6e-04  1.00e+00   1.145314161e+01   1.146295710e+01   2.4e-09  1.31  
36  3.2e-06  3.6e-02  2.3e-04  1.00e+00   1.145389780e+01   1.146273181e+01   2.2e-09  1.35  
37  2.9e-06  3.3e-02  2.1e-04  1.00e+00   1.145457789e+01   1.146252860e+01   1.9e-09  1.38  
38  2.6e-06  3.0e-02  1.9e-04  1.00e+00   1.145518961e+01   1.146234529e+01   1.7e-09  1.42  
39  2.3e-06  2.8e-02  1.7e-04  1.00e+00   1.145573986e+01   1.146218004e+01   1.6e-09  1.45  
40  2.1e-06  2.6e-02  1.5e-04  1.00e+00   1.145623486e+01   1.146203106e+01   1.4e-09  1.49  
41  1.9e-06  2.4e-02  1.4e-04  1.00e+00   1.145668020e+01   1.146189676e+01   1.3e-09  1.52  
42  1.7e-06  2.2e-02  1.2e-04  1.00e+00   1.145708085e+01   1.146177575e+01   1.1e-09  1.56  
43  1.5e-06  2.1e-02  1.1e-04  1.00e+00   1.145744132e+01   1.146166677e+01   1.0e-09  1.59  
44  1.4e-06  1.9e-02  1.0e-04  1.00e+00   1.145776565e+01   1.146156858e+01   9.3e-10  1.63  
45  1.2e-06  1.8e-02  9.0e-05  1.00e+00   1.145805749e+01   1.146148009e+01   8.4e-10  1.66  
46  1.1e-06  1.7e-02  8.1e-05  1.00e+00   1.145832008e+01   1.146140045e+01   7.5e-10  1.70  
47  1.0e-06  1.6e-02  7.3e-05  1.00e+00   1.145855637e+01   1.146132872e+01   6.8e-10  1.73  
48  9.0e-07  1.5e-02  6.6e-05  1.00e+00   1.145876899e+01   1.146126414e+01   6.1e-10  1.76  
49  8.1e-07  1.4e-02  5.9e-05  1.00e+00   1.145896032e+01   1.146120602e+01   5.5e-10  1.79  
50  7.3e-07  1.4e-02  5.3e-05  1.00e+00   1.145913251e+01   1.146115362e+01   4.9e-10  1.82  
51  6.6e-07  1.3e-02  4.8e-05  1.00e+00   1.145928747e+01   1.146110646e+01   4.4e-10  1.86  
52  2.3e-07  4.5e-03  1.7e-05  1.00e+00   1.146019699e+01   1.146082906e+01   1.5e-10  1.89  
53  2.1e-07  4.0e-03  1.5e-05  1.00e+00   1.146024590e+01   1.146081455e+01   1.4e-10  1.93  
54  7.0e-08  1.4e-03  5.1e-06  1.00e+00   1.146053229e+01   1.146072665e+01   4.7e-11  1.96  
55  6.3e-08  1.2e-03  4.6e-06  1.02e+00   1.146054825e+01   1.146072175e+01   4.3e-11  2.00  
56  5.7e-08  1.1e-03  4.1e-06  9.90e-01   1.146056152e+01   1.146071774e+01   3.9e-11  2.04  
57  5.1e-08  1.0e-03  3.7e-06  1.05e+00   1.146057650e+01   1.146071273e+01   3.6e-11  2.07  
58  4.6e-08  9.0e-04  3.4e-06  1.05e+00   1.146058935e+01   1.146070862e+01   3.3e-11  2.10  
59  4.2e-08  8.1e-04  3.0e-06  1.06e+00   1.146060089e+01   1.146070490e+01   3.1e-11  2.13  
60  3.7e-08  7.3e-04  2.7e-06  1.04e+00   1.146061047e+01   1.146070192e+01   2.8e-11  2.16  
61  3.4e-08  6.6e-04  2.4e-06  1.05e+00   1.146061916e+01   1.146069918e+01   2.6e-11  2.20  
62  1.6e-08  7.0e-05  2.6e-07  9.43e-01   1.146067552e+01   1.146068428e+01   3.4e-12  2.24  
63  5.9e-09  1.4e-05  5.2e-08  8.47e-01   1.146068033e+01   1.146068222e+01   8.6e-13  2.28  
Interior-point optimizer terminated. Time: 2.28. 

Optimizer terminated. Time: 2.30    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1460680330e+01    Viol.  con: 1e-07    var: 0e+00  
  Dual.    obj: 1.1460682218e+01    Viol.  con: 0e+00    var: 1e-04  
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.32 seconds.
result packing took 12% of solve time
solution checking took 2.1% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
  Platform               : Linux/64-X86    
  Cores                  : 20              

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

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 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                : 20              
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             : 0.04              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.68e+04          after factor           : 1.72e+05        
Factor     - dense dim.             : 0                 flops                  : 0.00e+00        
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+00        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.3e+05  0.00e+00   -1.289019573e+05  2.000000000e+00   1.0e+00  0.06  
1   1.1e+03  1.4e+03  5.9e+04  -9.71e-01  -1.265895961e+05  3.780619651e+00   4.6e-01  0.12  
2   3.9e+02  5.0e+02  2.2e+04  -9.34e-01  -1.197208259e+05  1.155029319e+01   1.7e-01  0.16  
3   2.8e+02  3.6e+02  1.6e+04  -8.27e-01  -1.157127753e+05  9.417170582e+01   1.2e-01  0.19  
4   2.8e+02  3.6e+02  1.6e+04  -7.57e-01  -1.123932994e+05  2.811276203e+03   1.2e-01  0.23  
5   7.6e+01  9.8e+01  4.2e+03  -7.47e-01  -7.376612454e+04  1.082767662e+04   3.3e-02  0.27  
6   3.7e+01  4.8e+01  2.1e+03  -1.88e-01  -4.660432113e+04  1.110741017e+04   1.6e-02  0.30  
7   2.2e+01  2.8e+01  1.2e+03  2.82e-01   -3.096793060e+04  7.346525933e+03   9.6e-03  0.34  
8   1.0e+01  1.3e+01  5.6e+02  5.65e-01   -1.574606897e+04  3.981872681e+03   4.4e-03  0.38  
9   4.4e+00  5.7e+00  2.5e+02  8.13e-01   -6.958492336e+03  2.167138824e+03   2.0e-03  0.41  
10  2.0e+00  2.6e+00  1.1e+02  9.36e-01   -3.050796503e+03  1.180729566e+03   9.0e-04  0.45  
11  1.5e+00  1.9e+00  8.2e+01  9.82e-01   -2.218872007e+03  8.695220178e+02   6.5e-04  0.48  
12  9.1e-01  1.2e+00  5.1e+01  9.85e-01   -1.370772404e+03  5.641491996e+02   4.1e-04  0.52  
13  7.7e-01  1.2e+00  4.4e+01  9.63e-01   -1.183386499e+03  4.845446882e+02   3.5e-04  0.56  
14  3.1e-01  4.8e-01  1.8e+01  9.89e-01   -4.667283349e+02  2.156581012e+02   1.4e-04  0.59  
15  1.6e-01  2.5e-01  9.0e+00  1.00e+00   -2.293401975e+02  1.130414199e+02   7.2e-05  0.63  
16  4.8e-02  1.5e-01  2.8e+00  1.00e+00   -6.729597976e+01  4.025135376e+01   2.3e-05  0.66  
17  3.8e-02  1.2e-01  2.3e+00  1.00e+00   -5.211581810e+01  3.388214513e+01   1.8e-05  0.70  
18  1.9e-02  8.8e-02  1.2e+00  1.00e+00   -2.289530103e+01  2.097975044e+01   9.4e-06  0.73  
19  1.5e-02  7.0e-02  8.6e-01  1.02e+00   -1.404741145e+01  1.855048605e+01   7.1e-06  0.77  
20  6.1e-03  5.3e-02  3.7e-01  1.03e+00   9.893164020e-01   1.458086367e+01   3.0e-06  0.81  
21  2.3e-03  6.6e-02  1.4e-01  1.02e+00   7.379546275e+00   1.257548428e+01   1.2e-06  0.84  
22  9.1e-04  6.0e-02  5.7e-02  9.85e-01   9.669264196e+00   1.180959413e+01   5.0e-07  0.88  
23  3.1e-04  7.8e-02  2.1e-02  9.66e-01   1.073877300e+01   1.152846524e+01   1.8e-07  0.91  
24  1.4e-04  6.2e-02  9.5e-03  9.55e-01   1.106593818e+01   1.143047699e+01   8.4e-08  0.95  
25  6.1e-05  6.2e-02  4.3e-03  9.85e-01   1.122221543e+01   1.138775617e+01   3.9e-08  0.99  
26  3.2e-05  5.6e-02  2.3e-03  9.91e-01   1.128377561e+01   1.137133377e+01   2.0e-08  1.02  
27  2.9e-05  5.1e-02  2.0e-03  9.91e-01   1.129248930e+01   1.137142896e+01   1.8e-08  1.06  
28  2.6e-05  4.7e-02  1.8e-03  9.94e-01   1.129843164e+01   1.136947684e+01   1.7e-08  1.10  
29  2.3e-05  4.3e-02  1.6e-03  9.93e-01   1.130399014e+01   1.136794652e+01   1.5e-08  1.14  
30  2.1e-05  3.9e-02  1.5e-03  9.94e-01   1.130895129e+01   1.136653518e+01   1.3e-08  1.17  
31  1.9e-05  3.6e-02  1.3e-03  9.94e-01   1.131340184e+01   1.136524534e+01   1.2e-08  1.21  
32  1.7e-05  3.3e-02  1.2e-03  9.95e-01   1.131740164e+01   1.136407530e+01   1.1e-08  1.25  
33  1.5e-05  3.0e-02  1.1e-03  9.95e-01   1.132099597e+01   1.136301479e+01   9.8e-09  1.29  
34  1.4e-05  2.8e-02  9.7e-04  9.95e-01   1.132422604e+01   1.136205375e+01   8.8e-09  1.32  
35  1.2e-05  2.6e-02  8.8e-04  9.96e-01   1.132712947e+01   1.136118351e+01   7.9e-09  1.36  
36  1.1e-05  2.4e-02  7.9e-04  9.96e-01   1.132973989e+01   1.136039625e+01   7.1e-09  1.39  
37  1.0e-05  2.2e-02  7.1e-04  9.96e-01   1.133208724e+01   1.135968436e+01   6.4e-09  1.43  
38  9.0e-06  2.1e-02  6.4e-04  9.97e-01   1.133419831e+01   1.135904101e+01   5.8e-09  1.47  
39  8.1e-06  1.9e-02  5.8e-04  9.97e-01   1.133609704e+01   1.135845981e+01   5.2e-09  1.50  
40  7.3e-06  1.8e-02  5.2e-04  9.97e-01   1.133780489e+01   1.135793495e+01   4.7e-09  1.54  
41  6.6e-06  1.7e-02  4.7e-04  9.98e-01   1.133934109e+01   1.135746104e+01   4.2e-09  1.58  
42  5.9e-06  1.6e-02  4.2e-04  9.98e-01   1.134072290e+01   1.135703322e+01   3.8e-09  1.61  
43  5.3e-06  1.5e-02  3.8e-04  9.98e-01   1.134196586e+01   1.135664706e+01   3.4e-09  1.65  
44  4.8e-06  1.4e-02  3.4e-04  9.98e-01   1.134308389e+01   1.135629855e+01   3.1e-09  1.69  
45  4.3e-06  1.4e-02  3.1e-04  9.99e-01   1.134408958e+01   1.135598403e+01   2.8e-09  1.72  
46  3.9e-06  1.3e-02  2.8e-04  9.99e-01   1.134499420e+01   1.135570028e+01   2.5e-09  1.76  
47  3.5e-06  1.2e-02  2.5e-04  9.99e-01   1.134580795e+01   1.135544432e+01   2.2e-09  1.80  
48  3.2e-06  1.2e-02  2.2e-04  9.99e-01   1.134654001e+01   1.135521344e+01   2.0e-09  1.83  
49  2.8e-06  1.1e-02  2.0e-04  9.99e-01   1.134719861e+01   1.135500528e+01   1.8e-09  1.87  
50  2.6e-06  1.1e-02  1.8e-04  9.99e-01   1.134779118e+01   1.135481764e+01   1.6e-09  1.91  
51  2.3e-06  1.1e-02  1.6e-04  9.99e-01   1.134832436e+01   1.135464856e+01   1.5e-09  1.95  
52  2.1e-06  1.0e-02  1.5e-04  9.99e-01   1.134880415e+01   1.135449624e+01   1.3e-09  1.98  
53  1.9e-06  9.8e-03  1.3e-04  9.99e-01   1.134923591e+01   1.135435904e+01   1.2e-09  2.01  
54  1.7e-06  9.6e-03  1.2e-04  9.99e-01   1.134962446e+01   1.135423551e+01   1.1e-09  2.04  
55  1.5e-06  9.3e-03  1.1e-04  9.99e-01   1.134997415e+01   1.135412429e+01   9.6e-10  2.08  
56  1.4e-06  9.1e-03  9.6e-05  9.99e-01   1.135028887e+01   1.135402416e+01   8.7e-10  2.11  
57  1.2e-06  8.9e-03  8.6e-05  9.99e-01   1.135057212e+01   1.135393402e+01   7.8e-10  2.15  
58  1.1e-06  8.7e-03  7.8e-05  1.00e+00   1.135082707e+01   1.135385288e+01   7.0e-10  2.19  
59  9.9e-07  8.5e-03  7.0e-05  1.00e+00   1.135105654e+01   1.135377986e+01   6.3e-10  2.23  
60  8.9e-07  8.3e-03  6.3e-05  1.00e+00   1.135126307e+01   1.135371413e+01   5.7e-10  2.27  
61  8.0e-07  8.2e-03  5.7e-05  1.00e+00   1.135144898e+01   1.135365497e+01   5.1e-10  2.30  
62  7.2e-07  8.1e-03  5.1e-05  1.00e+00   1.135161630e+01   1.135360175e+01   4.6e-10  2.34  
63  6.5e-07  8.0e-03  4.6e-05  1.00e+00   1.135176690e+01   1.135355387e+01   4.1e-10  2.38  
64  5.8e-07  7.9e-03  4.1e-05  1.00e+00   1.135190245e+01   1.135351076e+01   3.7e-10  2.42  
65  5.3e-07  7.8e-03  3.7e-05  1.00e+00   1.135202446e+01   1.135347197e+01   3.4e-10  2.45  
66  4.7e-07  7.7e-03  3.3e-05  1.00e+00   1.135213429e+01   1.135343704e+01   3.0e-10  2.48  
67  4.3e-07  7.6e-03  3.0e-05  1.00e+00   1.135223313e+01   1.135340562e+01   2.7e-10  2.51  
68  3.8e-07  7.5e-03  2.7e-05  1.00e+00   1.135232209e+01   1.135337735e+01   2.4e-10  2.54  
69  3.4e-07  7.5e-03  2.4e-05  1.00e+00   1.135240216e+01   1.135335191e+01   2.2e-10  2.58  
70  3.1e-07  7.4e-03  2.2e-05  1.00e+00   1.135247423e+01   1.135332901e+01   2.0e-10  2.61  
71  2.8e-07  7.4e-03  2.0e-05  1.00e+00   1.135253908e+01   1.135330841e+01   1.8e-10  2.65  
72  2.5e-07  7.3e-03  1.8e-05  9.99e-01   1.135259745e+01   1.135328988e+01   1.6e-10  2.68  
73  2.3e-07  7.3e-03  1.6e-05  1.00e+00   1.135265000e+01   1.135327317e+01   1.4e-10  2.72  
74  2.0e-07  7.2e-03  1.4e-05  1.00e+00   1.135269728e+01   1.135325815e+01   1.3e-10  2.75  
75  1.8e-07  7.2e-03  1.3e-05  1.00e+00   1.135273984e+01   1.135324461e+01   1.2e-10  2.79  
76  1.6e-07  7.2e-03  1.2e-05  1.00e+00   1.135277814e+01   1.135323244e+01   1.1e-10  2.82  
77  1.5e-07  7.1e-03  1.1e-05  9.98e-01   1.135281261e+01   1.135322151e+01   9.5e-11  2.86  
78  1.3e-07  7.1e-03  9.5e-06  1.00e+00   1.135284363e+01   1.135321165e+01   8.5e-11  2.90  
79  1.2e-07  7.1e-03  8.5e-06  1.00e+00   1.135287155e+01   1.135320277e+01   7.7e-11  2.93  
80  1.1e-07  7.1e-03  7.7e-06  1.00e+00   1.135289668e+01   1.135319478e+01   6.9e-11  2.97  
81  9.7e-08  7.0e-03  6.9e-06  9.98e-01   1.135291928e+01   1.135318761e+01   6.2e-11  3.01  
82  8.8e-08  7.0e-03  6.2e-06  1.00e+00   1.135293966e+01   1.135318111e+01   5.6e-11  3.05  
83  7.9e-08  7.0e-03  5.6e-06  9.98e-01   1.135295797e+01   1.135317529e+01   5.0e-11  3.09  
84  7.1e-08  7.0e-03  5.0e-06  1.00e+00   1.135297447e+01   1.135317002e+01   4.5e-11  3.12  
85  6.4e-08  7.0e-03  4.5e-06  1.00e+00   1.135298931e+01   1.135316530e+01   4.1e-11  3.16  
86  5.8e-08  7.0e-03  4.1e-06  9.98e-01   1.135300265e+01   1.135316106e+01   3.7e-11  3.20  
87  5.2e-08  6.9e-03  3.7e-06  9.96e-01   1.135301466e+01   1.135315725e+01   3.3e-11  3.23  
88  4.7e-08  6.9e-03  3.3e-06  9.99e-01   1.135302547e+01   1.135315381e+01   3.0e-11  3.27  
89  4.2e-08  6.2e-03  3.0e-06  1.01e+00   1.135303550e+01   1.135315058e+01   2.7e-11  3.31  
90  3.8e-08  5.6e-03  2.7e-06  9.96e-01   1.135304422e+01   1.135314781e+01   2.4e-11  3.34  
91  3.4e-08  5.1e-03  2.4e-06  1.00e+00   1.135305212e+01   1.135314529e+01   2.2e-11  3.37  
92  3.1e-08  4.6e-03  2.2e-06  1.01e+00   1.135305931e+01   1.135314298e+01   2.0e-11  3.41  
93  2.8e-08  4.1e-03  1.9e-06  9.97e-01   1.135306565e+01   1.135314096e+01   1.8e-11  3.45  
94  2.5e-08  3.7e-03  1.8e-06  1.00e+00   1.135307142e+01   1.135313912e+01   1.6e-11  3.48  
95  2.2e-08  3.3e-03  1.6e-06  1.00e+00   1.135307663e+01   1.135313745e+01   1.4e-11  3.52  
96  2.0e-08  3.0e-03  1.4e-06  1.00e+00   1.135308124e+01   1.135313598e+01   1.3e-11  3.56  
97  1.8e-08  2.7e-03  1.3e-06  1.00e+00   1.135308543e+01   1.135313463e+01   1.2e-11  3.60  
98  1.6e-08  2.4e-03  1.1e-06  9.97e-01   1.135308916e+01   1.135313345e+01   1.0e-11  3.64  
99  1.5e-08  2.2e-03  1.0e-06  1.01e+00   1.135309268e+01   1.135313231e+01   9.5e-12  3.67  
100 1.3e-08  2.0e-03  9.3e-07  9.78e-01   1.135309568e+01   1.135313138e+01   8.5e-12  3.71  
101 1.2e-08  1.8e-03  8.4e-07  9.86e-01   1.135309838e+01   1.135313054e+01   7.7e-12  3.75  
102 1.1e-08  1.6e-03  7.5e-07  1.02e+00   1.135310101e+01   1.135312967e+01   7.0e-12  3.79  
103 2.1e-09  1.7e-04  8.2e-08  1.01e+00   1.135312031e+01   1.135312339e+01   7.2e-13  3.82  
Interior-point optimizer terminated. Time: 3.83. 

Optimizer terminated. Time: 3.84    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1353120309e+01    Viol.  con: 5e-08    var: 0e+00  
  Dual.    obj: 1.1353123390e+01    Viol.  con: 0e+00    var: 1e-03  
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.87 seconds.
result packing took 6.8% of solve time
solution checking took 1.7% 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               : Linux/64-X86    
  Cores                  : 20              

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

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1012
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1023
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Eliminator - elim's                 : 1023            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 20              
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 830
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3579              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.05              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.68e+04          after factor           : 1.72e+05        
Factor     - dense dim.             : 0                 flops                  : 0.00e+00        
Factor     - GP saved nzs           : 0                 GP saved flops         : 0.00e+00        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.3e+05  0.00e+00   -1.288314869e+05  2.000000000e+00   1.0e+00  0.08  
1   1.1e+03  1.4e+03  5.9e+04  -9.71e-01  -1.265140038e+05  3.775532469e+00   4.6e-01  0.20  
2   3.8e+02  4.9e+02  2.1e+04  -9.34e-01  -1.194173716e+05  1.178288060e+01   1.7e-01  0.23  
3   2.8e+02  3.6e+02  1.6e+04  -8.24e-01  -1.156061126e+05  1.066497359e+02   1.2e-01  0.26  
4   2.8e+02  3.6e+02  1.5e+04  -7.56e-01  -1.122497066e+05  2.780054152e+03   1.2e-01  0.29  
5   7.6e+01  9.8e+01  4.2e+03  -7.45e-01  -7.375613602e+04  1.084062892e+04   3.4e-02  0.33  
6   3.6e+01  4.7e+01  2.0e+03  -1.89e-01  -4.548415098e+04  1.112036205e+04   1.6e-02  0.37  
7   2.0e+01  2.6e+01  1.1e+03  3.01e-01   -2.906469444e+04  7.239605373e+03   9.0e-03  0.41  
8   9.7e+00  1.3e+01  5.4e+02  5.98e-01   -1.521691043e+04  3.918895403e+03   4.3e-03  0.44  
9   4.3e+00  5.6e+00  2.4e+02  8.23e-01   -6.825046224e+03  2.127561168e+03   1.9e-03  0.48  
10  1.6e+00  2.1e+00  9.0e+01  9.39e-01   -2.373786434e+03  9.911360564e+02   7.1e-04  0.52  
11  1.1e+00  1.5e+00  6.3e+01  9.88e-01   -1.663839409e+03  6.968472925e+02   5.0e-04  0.56  
12  7.8e-01  1.0e+00  4.4e+01  9.83e-01   -1.178894722e+03  4.971999710e+02   3.5e-04  0.60  
13  5.9e-01  7.7e-01  3.3e+01  9.85e-01   -8.760847925e+02  3.894960545e+02   2.7e-04  0.64  
14  2.1e-01  2.9e-01  1.2e+01  9.89e-01   -3.251264659e+02  1.426638706e+02   9.9e-05  0.67  
15  8.9e-02  1.4e-01  5.1e+00  1.01e+00   -1.286086956e+02  6.680925782e+01   4.2e-05  0.71  
16  3.5e-02  9.9e-02  2.1e+00  1.01e+00   -4.801956361e+01  3.100081012e+01   1.7e-05  0.75  
17  2.9e-02  8.4e-02  1.7e+00  9.96e-01   -3.744465390e+01  2.764803902e+01   1.4e-05  0.79  
18  1.8e-02  6.6e-02  1.1e+00  1.01e+00   -1.955018027e+01  2.043076277e+01   8.7e-06  0.83  
19  1.6e-02  5.8e-02  9.2e-01  1.02e+00   -1.527785190e+01  1.935151523e+01   7.5e-06  0.87  
20  5.7e-03  6.6e-02  3.4e-01  1.02e+00   1.702995491e+00   1.416228792e+01   2.8e-06  0.90  
21  1.9e-03  7.7e-02  1.2e-01  1.02e+00   8.009049509e+00   1.236814309e+01   1.0e-06  0.94  
22  1.4e-03  5.9e-02  8.6e-02  9.66e-01   8.848426542e+00   1.205230784e+01   7.4e-07  0.98  
23  4.9e-04  6.6e-02  3.2e-02  9.59e-01   1.037950697e+01   1.161034490e+01   2.9e-07  1.02  
24  2.0e-04  6.1e-02  1.3e-02  9.57e-01   1.092219451e+01   1.143145720e+01   1.2e-07  1.06  
25  1.8e-04  5.6e-02  1.2e-02  9.75e-01   1.096037652e+01   1.141851512e+01   1.1e-07  1.10  
26  1.6e-04  5.1e-02  1.1e-02  9.73e-01   1.099563384e+01   1.140850716e+01   9.6e-08  1.14  
27  1.4e-04  4.6e-02  9.6e-03  9.75e-01   1.103006633e+01   1.140221080e+01   8.7e-08  1.18  
28  1.3e-04  4.2e-02  8.7e-03  9.77e-01   1.106118339e+01   1.139659489e+01   7.8e-08  1.22  
29  1.2e-04  3.9e-02  7.8e-03  9.79e-01   1.108919996e+01   1.139147292e+01   7.0e-08  1.26  
30  1.0e-04  3.6e-02  7.0e-03  9.81e-01   1.111436671e+01   1.138674651e+01   6.3e-08  1.30  
31  9.3e-05  3.3e-02  6.3e-03  9.82e-01   1.113696450e+01   1.138238319e+01   5.7e-08  1.34  
32  8.4e-05  3.0e-02  5.7e-03  9.84e-01   1.115724914e+01   1.137835508e+01   5.1e-08  1.37  
33  7.6e-05  2.8e-02  5.1e-03  9.85e-01   1.117545310e+01   1.137463782e+01   4.6e-08  1.40  
34  6.8e-05  2.6e-02  4.6e-03  9.87e-01   1.119178688e+01   1.137120953e+01   4.2e-08  1.43  
35  6.1e-05  2.4e-02  4.2e-03  9.88e-01   1.120644070e+01   1.136805005e+01   3.7e-08  1.47  
36  5.5e-05  2.2e-02  3.7e-03  9.89e-01   1.121958651e+01   1.136514118e+01   3.4e-08  1.51  
37  5.0e-05  2.1e-02  3.4e-03  9.90e-01   1.123137919e+01   1.136246579e+01   3.0e-08  1.54  
38  4.5e-05  1.9e-02  3.0e-03  9.91e-01   1.124195816e+01   1.136000796e+01   2.7e-08  1.58  
39  4.0e-05  1.8e-02  2.7e-03  9.92e-01   1.125144848e+01   1.135775227e+01   2.5e-08  1.62  
40  3.6e-05  1.7e-02  2.5e-03  9.93e-01   1.125996250e+01   1.135568431e+01   2.2e-08  1.65  
41  3.3e-05  1.6e-02  2.2e-03  9.93e-01   1.126760083e+01   1.135379010e+01   2.0e-08  1.69  
42  2.9e-05  1.5e-02  2.0e-03  9.94e-01   1.127445396e+01   1.135205678e+01   1.8e-08  1.73  
43  2.6e-05  1.4e-02  1.8e-03  9.95e-01   1.128060309e+01   1.135047222e+01   1.6e-08  1.76  
44  2.4e-05  1.4e-02  1.6e-03  9.95e-01   1.128612132e+01   1.134902531e+01   1.5e-08  1.80  
45  2.1e-05  1.3e-02  1.4e-03  9.96e-01   1.129107423e+01   1.134770558e+01   1.3e-08  1.84  
46  1.9e-05  1.2e-02  1.3e-03  9.96e-01   1.129552058e+01   1.134650336e+01   1.2e-08  1.87  
47  1.7e-05  1.2e-02  1.2e-03  9.97e-01   1.129951284e+01   1.134540920e+01   1.1e-08  1.91  
48  1.6e-05  1.1e-02  1.1e-03  9.97e-01   1.130309798e+01   1.134441436e+01   9.5e-09  1.94  
49  1.4e-05  1.1e-02  9.5e-04  9.97e-01   1.130631804e+01   1.134351069e+01   8.6e-09  1.98  
50  1.3e-05  1.1e-02  8.6e-04  9.98e-01   1.130921063e+01   1.134269042e+01   7.7e-09  2.02  
51  1.1e-05  1.0e-02  7.7e-04  9.98e-01   1.131180943e+01   1.134194645e+01   7.0e-09  2.06  
52  1.0e-05  1.0e-02  6.9e-04  9.98e-01   1.131414462e+01   1.134127218e+01   6.3e-09  2.09  
53  9.2e-06  9.7e-03  6.2e-04  9.98e-01   1.131624316e+01   1.134066144e+01   5.6e-09  2.13  
54  8.3e-06  9.4e-03  5.6e-04  9.99e-01   1.131812927e+01   1.134010844e+01   5.1e-09  2.17  
55  7.5e-06  9.2e-03  5.1e-04  9.99e-01   1.131982459e+01   1.133960820e+01   4.6e-09  2.20  
56  6.7e-06  9.0e-03  4.6e-04  9.99e-01   1.132134851e+01   1.133915568e+01   4.1e-09  2.24  
57  6.0e-06  8.8e-03  4.1e-04  9.99e-01   1.132271847e+01   1.133874646e+01   3.7e-09  2.28  
58  5.4e-06  8.6e-03  3.7e-04  9.99e-01   1.132395008e+01   1.133837652e+01   3.3e-09  2.32  
59  4.9e-06  8.5e-03  3.3e-04  9.99e-01   1.132505735e+01   1.133804216e+01   3.0e-09  2.35  
60  4.4e-06  8.3e-03  3.0e-04  9.99e-01   1.132605289e+01   1.133773999e+01   2.7e-09  2.39  
61  4.0e-06  8.2e-03  2.7e-04  9.99e-01   1.132694802e+01   1.133746703e+01   2.4e-09  2.42  
62  3.6e-06  8.1e-03  2.4e-04  1.00e+00   1.132775290e+01   1.133722051e+01   2.2e-09  2.45  
63  3.2e-06  8.0e-03  2.2e-04  1.00e+00   1.132847670e+01   1.133699795e+01   2.0e-09  2.48  
64  2.9e-06  7.9e-03  2.0e-04  9.99e-01   1.132912764e+01   1.133679717e+01   1.8e-09  2.52  
65  2.6e-06  7.8e-03  1.8e-04  1.00e+00   1.132971312e+01   1.133661602e+01   1.6e-09  2.56  
66  2.3e-06  7.7e-03  1.6e-04  9.99e-01   1.133023976e+01   1.133645271e+01   1.4e-09  2.59  
67  2.1e-06  7.7e-03  1.4e-04  1.00e+00   1.133071355e+01   1.133630536e+01   1.3e-09  2.63  
68  1.9e-06  7.6e-03  1.3e-04  1.00e+00   1.133113981e+01   1.133617255e+01   1.2e-09  2.67  
69  1.7e-06  7.5e-03  1.2e-04  1.00e+00   1.133152333e+01   1.133605287e+01   1.0e-09  2.71  
70  1.5e-06  7.5e-03  1.0e-04  9.99e-01   1.133186837e+01   1.133594515e+01   9.4e-10  2.75  
71  1.4e-06  7.4e-03  9.4e-05  1.00e+00   1.133217886e+01   1.133584804e+01   8.5e-10  2.79  
72  1.2e-06  7.4e-03  8.4e-05  1.00e+00   1.133245825e+01   1.133576055e+01   7.6e-10  2.83  
73  1.1e-06  7.3e-03  7.6e-05  1.00e+00   1.133270965e+01   1.133568181e+01   6.9e-10  2.87  
74  1.0e-06  7.3e-03  6.8e-05  9.99e-01   1.133293587e+01   1.133561094e+01   6.2e-10  2.91  
75  9.1e-07  7.3e-03  6.2e-05  1.00e+00   1.133313947e+01   1.133554701e+01   5.6e-10  2.95  
76  8.2e-07  7.2e-03  5.5e-05  1.00e+00   1.133332267e+01   1.133548952e+01   5.0e-10  2.99  
77  7.3e-07  7.2e-03  5.0e-05  1.00e+00   1.133348756e+01   1.133543768e+01   4.5e-10  3.02  
78  6.6e-07  7.2e-03  4.5e-05  1.00e+00   1.133363593e+01   1.133539107e+01   4.1e-10  3.06  
79  5.9e-07  7.2e-03  4.0e-05  1.00e+00   1.133376946e+01   1.133534908e+01   3.6e-10  3.10  
80  5.4e-07  7.1e-03  3.6e-05  1.00e+00   1.133388961e+01   1.133531131e+01   3.3e-10  3.14  
81  4.8e-07  7.1e-03  3.3e-05  1.00e+00   1.133399775e+01   1.133527727e+01   3.0e-10  3.18  
82  4.3e-07  7.1e-03  2.9e-05  9.99e-01   1.133409505e+01   1.133524670e+01   2.7e-10  3.22  
83  3.9e-07  7.1e-03  2.6e-05  1.00e+00   1.133418265e+01   1.133521908e+01   2.4e-10  3.26  
84  3.5e-07  7.0e-03  2.4e-05  9.99e-01   1.133426145e+01   1.133519430e+01   2.2e-10  3.29  
85  3.2e-07  7.0e-03  2.1e-05  9.99e-01   1.133433237e+01   1.133517199e+01   1.9e-10  3.33  
86  2.8e-07  7.0e-03  1.9e-05  9.97e-01   1.133439618e+01   1.133515194e+01   1.7e-10  3.39  
87  2.6e-07  7.0e-03  1.7e-05  9.99e-01   1.133445361e+01   1.133513385e+01   1.6e-10  3.43  
88  2.3e-07  7.0e-03  1.6e-05  9.97e-01   1.133450529e+01   1.133511760e+01   1.4e-10  3.46  
89  2.1e-07  7.0e-03  1.4e-05  9.99e-01   1.133455181e+01   1.133510292e+01   1.3e-10  3.50  
90  1.9e-07  7.0e-03  1.3e-05  9.99e-01   1.133459368e+01   1.133508970e+01   1.1e-10  3.54  
91  1.7e-07  7.0e-03  1.1e-05  1.00e+00   1.133463146e+01   1.133507771e+01   1.0e-10  3.58  
92  1.5e-07  6.9e-03  1.0e-05  1.00e+00   1.133466536e+01   1.133506700e+01   9.3e-11  3.62  
93  1.4e-07  6.9e-03  9.2e-06  9.97e-01   1.133469586e+01   1.133505739e+01   8.3e-11  3.66  
94  1.2e-07  6.9e-03  8.3e-06  9.97e-01   1.133472331e+01   1.133504873e+01   7.5e-11  3.70  
95  1.1e-07  6.2e-03  7.5e-06  1.00e+00   1.133474815e+01   1.133504083e+01   6.8e-11  3.74  
96  9.9e-08  5.6e-03  6.7e-06  1.00e+00   1.133477038e+01   1.133503377e+01   6.1e-11  3.77  
97  8.9e-08  5.0e-03  6.1e-06  9.96e-01   1.133479037e+01   1.133502747e+01   5.5e-11  3.81  
98  8.0e-08  4.5e-03  5.5e-06  1.00e+00   1.133480837e+01   1.133502176e+01   4.9e-11  3.84  
99  7.2e-08  4.1e-03  4.9e-06  1.00e+00   1.133482457e+01   1.133501661e+01   4.4e-11  3.87  
100 6.5e-08  3.7e-03  4.4e-06  1.00e+00   1.133483934e+01   1.133501190e+01   4.0e-11  3.91  
101 5.9e-08  3.3e-03  4.0e-06  9.99e-01   1.133485244e+01   1.133500775e+01   3.6e-11  3.94  
102 5.3e-08  3.0e-03  3.6e-06  9.98e-01   1.133486423e+01   1.133500402e+01   3.2e-11  3.98  
103 4.7e-08  2.7e-03  3.2e-06  9.87e-01   1.133487482e+01   1.133500071e+01   2.9e-11  4.02  
104 4.3e-08  2.4e-03  2.9e-06  1.01e+00   1.133488454e+01   1.133499760e+01   2.6e-11  4.05  
105 3.8e-08  2.2e-03  2.6e-06  1.01e+00   1.133489333e+01   1.133499478e+01   2.4e-11  4.08  
106 3.5e-08  2.0e-03  2.3e-06  1.00e+00   1.133490103e+01   1.133499233e+01   2.1e-11  4.11  
107 3.1e-08  1.8e-03  2.1e-06  1.00e+00   1.133490796e+01   1.133499012e+01   1.9e-11  4.15  
108 6.8e-09  3.4e-04  4.1e-07  9.74e-01   1.133495860e+01   1.133497454e+01   3.9e-12  4.19  
109 4.1e-09  5.4e-06  6.7e-09  8.81e-01   1.133497056e+01   1.133497084e+01   2.7e-13  4.23  
Interior-point optimizer terminated. Time: 4.23. 

Optimizer terminated. Time: 4.27    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1334970562e+01    Viol.  con: 2e-07    var: 0e+00  
  Dual.    obj: 1.1334970839e+01    Viol.  con: 0e+00    var: 5e-05  
* End solution on dual form. *
Transforming to primal solution.
Solving took 4.29 seconds.
result packing took 8.3% of solve time
solution checking took 1.5% of solve time
Solving took 6 GP solves and 30.1 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 2418948.16213 force_pound * meter but the right hand side evaluated to 2375461.31276 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 32774.3388516 force_pound but the right hand side evaluated to 32399.9999966 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 2.21510116766 meter but the right hand side evaluated to 2.08160211767 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 1243581.23361 joule / kilogram but the right hand side evaluated to 1.56113982189 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 664760.840655 joule / kilogram but the right hand side evaluated to 0.66733943775 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 18.399892984 meter but the right hand side evaluated to 16.3228962138 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 10.903625520217833 but the right hand side evaluated to 4.788858714373786 (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 10.019802899072115 but the right hand side evaluated to 4.788858696068545 (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 8.144911225641298 but the right hand side evaluated to 4.7888587186508715 (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 18.3622389719 meter but the right hand side evaluated to 18.1377278115 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 18.3622389719 meter but the right hand side evaluated to 18.2420660326 meter (Allowable.
----------------------------------------------------------------------
Ran 1 test in 35.922s

OK

Generating XML reports...
 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 0.2960348292679722 but the right hand side evaluated to 0.1897388589844243 (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 0.23301769643489045 but the right hand side evaluated to 0.17434551720189867 (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 7.563248753227961 but the right hand side evaluated to 4.730639750309998 (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 7.583100031550655 but the right hand side evaluated to 4.757853001134199 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: CruiseAlt_Mission
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission

Cloning into 'solar'...
Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3)
Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
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Collecting git+https://github.com/convexengineering/gpfit.git
  Cloning https://github.com/convexengineering/gpfit.git to /tmp/pip-req-build-x5uG1T
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: /tmp/pip-ephem-wheel-cache-T_vS5Z/wheels/d5/94/ac/b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
Collecting git+https://github.com/convexengineering/gassolar.git
  Cloning https://github.com/convexengineering/gassolar.git to /tmp/pip-req-build-0UwHAT
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.7.2)
Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2018.4)
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Building wheels for collected packages: gassolar
  Running setup.py bdist_wheel for gassolar: started
  Running setup.py bdist_wheel for gassolar: finished with status 'done'
  Stored in directory: /tmp/pip-ephem-wheel-cache-CYBfKK/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
Processing /jenkins/workspace/gplibrary_PR_Models/mosek/solar
Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.1)
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Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2018.4)
Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.11.0)
Building wheels for collected packages: solar
  Running setup.py bdist_wheel for solar: started
  Running setup.py bdist_wheel for solar: finished with status 'done'
  Stored in directory: /tmp/pip-ephem-wheel-cache-HYkg3y/wheels/f6/90/b0/8d5ca9b420ff66bedd24921652ee885c8718a479c0dcec7d2e
Successfully built solar
Installing collected packages: solar
Successfully installed solar-0.0.0.0

Running tests...
----------------------------------------------------------------------
../jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
adding test for 'solar/solar.py'
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
adding test for 'solar/npod_trade.py'
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 9 GP solves and 5.99 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 1.0624 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 1388463.0625 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 1248776.3249 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 2.29645501003 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194391 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 9.7 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 1388463.0562 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 1248776.3192 but bound is 1000000.0000
Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 82150.9611 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.29645500999 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194387 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)

Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,).
  (to raise th/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
  tau = np.exp(-0.175/costhsun)
e error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 3.73 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2510 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 765970.5439 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.65/GustL.65_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.49/GustL.49_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.58/GustL.58_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.69/GustL.69_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.46/GustL.46_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.71/GustL.71_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.78/GustL.78_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.48/GustL.48_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.52/GustL.52_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.75/GustL.75_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.40/GustL.40_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.59/GustL.59_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.64/GustL.64_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.66/GustL.66_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.67/GustL.67_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.44/GustL.44_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.55/GustL.55_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.54/GustL.54_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.53/GustL.53_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.62/GustL.62_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.60/GustL.60_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.51/GustL.51_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.41/GustL.41_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.47/GustL.47_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.70/GustL.70_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.50/GustL.50_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.74/GustL.74_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.68/GustL.68_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.76/GustL.76_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.79/GustL.79_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.63/GustL.63_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.77/GustL.77_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.56/GustL.56_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.57/GustL.57_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.42/GustL.42_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.61/GustL.61_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.45/GustL.45_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.43/GustL.43_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.72/GustL.72_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.73/GustL.73_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.09 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 862671.9697 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 3.66 seconds.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1202 but bound is 0.9465
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 987087.2998 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,).
  (to raise the error directly for debugging 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 1.8 seconds.
Warning: Var.iable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.0863 but bound is 0.9465
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1058302.4686 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 5.5 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 765970.5466 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.65/GustL.65_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.49/GustL.49_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.58/GustL.58_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.69/GustL.69_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.46/GustL.46_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.71/GustL.71_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.78/GustL.78_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.48/GustL.48_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.52/GustL.52_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.75/GustL.75_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.40/GustL.40_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.59/GustL.59_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.64/GustL.64_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.66/GustL.66_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.67/GustL.67_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.44/GustL.44_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.55/GustL.55_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.54/GustL.54_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.53/GustL.53_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.62/GustL.62_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.60/GustL.60_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.51/GustL.51_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.41/GustL.41_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.47/GustL.47_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.70/GustL.70_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.50/GustL.50_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.74/GustL.74_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.68/GustL.68_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.76/GustL.76_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.79/GustL.79_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.63/GustL.63_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.77/GustL.77_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.56/GustL.56_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.57/GustL.57_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.42/GustL.42_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.61/GustL.61_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.45/GustL.45_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.43/GustL.43_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.72/GustL.72_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.73/GustL.73_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 3.46 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 862671.9724 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 3.3 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 purpose..s, 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 1.72 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 9.09 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0624 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1388463.0549 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 1248776.3180 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 2.29645500995 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194384 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 7.7 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 1388463.0562 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 bo.und. Solution is 1248776.3192 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 2.29645501 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645194389 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 0.387 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1958 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 838075.6768 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.1/GustL.1_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 8 GP solves and 8.61 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 1017215.9376 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 2.62125883049 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124747963 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 1.95293542211 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215302 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 1.04275941613 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521708 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 0.467698134223 meter ** 2 / second ** 2 but the rigEht hand side evaluated to 0.467697003885 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 0.139006573775 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 0.579 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 6.68 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 monomE
======================================================================
ERROR [12.317s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn
    mod.test()
  File "solar.py", line 654, in test
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 61, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
  File "solar.py", line 633, in setup
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 83, in __init__
    CostedConstraintSet.__init__(self, cost, constraints, substitutions)
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/costed.py", line 21, in __init__
    ConstraintSet.__init__(self, constraints, subs)
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 58, in __init__
    list.__setitem__(self, i, ConstraintSet(constraint))
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 67, in __init__
    raise_elementhasnumpybools(constraint)
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 357, in raise_elementhasnumpybools
    % (cause, constraint))
ValueError: An ArrayConstraint was created with elements of numpy.bool_
Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]

======================================================================
ERROR [15.960s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn
    mod.test()
  File "solar.py", line 654, in test
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 61, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
  File "solar.py", line 633, in setup
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/model.py", line 83, in __init__
    CostedConstraintSet.__init__(self, cost, constraints, substitutions)
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/costed.py", line 21, in __init__
    ConstraintSet.__init__(self, constraints, subs)
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 58, in __init__
    list.__setitem__(self, i, ConstraintSet(constraint))
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 67, in __init__
    raise_elementhasnumpybools(constraint)
  File "/jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/constraints/set.py", line 357, in raise_elementhasnumpybools
    % (cause, constraint))
ValueError: An ArrayConstraint was created with elements of numpy.bool_
Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]

----------------------------------------------------------------------
Ran 8 tests in 288.392s

FAILED (errors=2)

Generating XML reports...
ial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0)
Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2)
Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.3)
Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4)
Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0)
Collecting git+https://github.com/hoburg/gpfit.git
  Cloning https://github.com/hoburg/gpfit.git to /tmp/pip-req-build-WcgIIz
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages
Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: /tmp/pip-ephem-wheel-cache-OWCCa_/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
Processing /jenkins/workspace/gplibrary_PR_Models/mosek/gplibrary
Requirement already satisfied: numpy>=1.12 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.8.1)
Building wheels for collected packages: gpkitmodels
  Running setup.py bdist_wheel for gpkitmodels: started
  Running setup.py bdist_wheel for gpkitmodels: finished with status 'done'
  Stored in directory: /tmp/pip-ephem-wheel-cache-mQ3UP2/wheels/63/f8/98/93b45f0bf8ab3367cc8d67f05c8a0e19f356c1a33a86d02692
Successfully built gpkitmodels
Installing collected packages: gpkitmodels
  Found existing installation: gpkitmodels 0.0.0.0
    Not uninstalling gpkitmodels at /jenkins/workspace/gplibrary_PR_Models/mosek, outside environment /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit
    Can't uninstall 'gpkitmodels'. No files were found to uninstall.
Successfully installed gpkitmodels-0.0.0.0

Running tests...
----------------------------------------------------------------------
...adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py'
adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py'
adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py'
adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py'
adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.155 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.453 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.0865 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0528 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.0269 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 3.31 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 985.544371507 meter * revolutions_per_minute but the right hand side evaluated to 103.04140943 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 0.420585924965 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573144906 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 0.314645033951 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629895187 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 0.168936438403 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931603968 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 0.063964238084 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631379963 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 0.0226356535421 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354005869 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)

Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.448 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.232 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.249 sec.onds.
Beginning signomial solve.
Solving took 16 GP solves and 5.69 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 1.....3 variables.
Solving took 0.1 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 2.36 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 1619897.4183 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.27 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 4.23 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 b.
----------------------------------------------------------------------
Ran 10 tests in 24.185s

OK

Generating XML reports...
ecause it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Cloning into 'eVTOL'...

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 1.625s

OK

Generating XML reports...
adding test for 'aircraft_models.py'
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git']
  attempt 1

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

calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})

calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})

calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'})

calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})

calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'})

calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
  attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
  attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'})

calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas']
  attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
  attempt 1

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

[Execution node] check if [reynolds] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
Build step 'Console output (build log) parsing' changed build result to FAILURE
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/jenkins/workspace/gplibrary_PR_Models/mosek' for the testing framework 'JUnit'.
[xUnit] [INFO] - Check 'Failed Tests' threshold.
[xUnit] [INFO] - Check 'Skipped Tests' threshold.
[xUnit] [INFO] - Setting the build status to FAILURE
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: FAILURE