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Optimizer  - threads                : 4               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 929
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3608              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.03            
Factor     - nonzeros before factor : 1.53e+004         after factor           : 1.76e+005       
Factor     - dense dim.             : 0                 flops                  : 3.97e+007       
Factor     - GP saved nzs           : 3.48e+004         GP saved flops         : 1.07e+006       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.230870165e+005 2.000000000e+000  1.0e+000 0.09  
1   1.5e+003 2.1e+003 8.3e+004 -9.71e-001 -1.221537972e+005 2.806585523e+000  6.8e-001 0.19  
2   6.6e+002 9.0e+002 3.6e+004 -9.55e-001 -1.184791658e+005 6.186470118e+000  2.9e-001 0.28  
3   2.9e+002 3.9e+002 1.5e+004 -8.94e-001 -1.107344872e+005 2.621625169e+001  1.3e-001 0.38  
4   2.9e+002 3.9e+002 1.5e+004 -7.64e-001 -1.083962619e+005 2.074599046e+003  1.3e-001 0.47  
5   1.1e+002 1.5e+002 5.8e+003 -7.55e-001 -8.287604151e+004 8.042521438e+003  4.8e-002 0.56  
6   4.5e+001 6.1e+001 2.4e+003 -3.85e-001 -5.005630541e+004 1.130981986e+004  2.0e-002 0.64  
7   2.7e+001 3.7e+001 1.5e+003 1.78e-001  -3.514341489e+004 8.030757850e+003  1.2e-002 0.75  
8   1.3e+001 1.8e+001 7.0e+002 4.63e-001  -1.861159862e+004 4.839057831e+003  5.7e-003 0.86  
9   5.1e+000 7.0e+000 2.8e+002 7.51e-001  -7.579708230e+003 2.417900447e+003  2.3e-003 0.95  
10  3.4e+000 4.6e+000 1.8e+002 9.25e-001  -4.941328367e+003 1.771993811e+003  1.5e-003 1.05  
11  1.1e+000 1.5e+000 5.9e+001 9.59e-001  -1.561885901e+003 6.117841506e+002  4.9e-004 1.11  
12  9.0e-001 1.4e+000 4.9e+001 9.84e-001  -1.271506957e+003 5.442384380e+002  4.1e-004 1.20  
13  6.6e-001 1.1e+000 3.6e+001 9.71e-001  -9.475468873e+002 4.128846732e+002  3.0e-004 1.30  
14  3.5e-001 6.0e-001 1.9e+001 9.99e-001  -4.736854310e+002 2.355178789e+002  1.6e-004 1.41  
15  1.3e-001 2.5e-001 7.2e+000 9.95e-001  -1.763291353e+002 9.338427147e+001  6.0e-005 1.49  
16  7.7e-002 1.6e-001 4.3e+000 1.01e+000  -1.015208624e+002 5.938815576e+001  3.6e-005 1.56  
17  2.7e-002 1.1e-001 1.5e+000 1.01e+000  -3.124961680e+001 2.620192511e+001  1.3e-005 1.64  
18  1.5e-002 8.9e-002 8.6e-001 1.01e+000  -1.374083394e+001 1.819352793e+001  7.3e-006 1.72  
19  1.3e-002 6.5e-002 7.2e-001 1.03e+000  -8.268230779e+000 1.811726490e+001  6.1e-006 1.88  
20  4.7e-003 6.7e-002 2.7e-001 1.01e+000  3.846901399e+000  1.382056100e+001  2.3e-006 1.97  
21  2.5e-003 5.9e-002 1.5e-001 1.02e+000  7.423272874e+000  1.269362366e+001  1.3e-006 2.09  
22  7.7e-004 7.6e-002 4.8e-002 9.90e-001  1.011955186e+001  1.189320440e+001  4.4e-007 2.19  
23  2.4e-004 8.6e-002 1.6e-002 9.76e-001  1.100793651e+001  1.159934758e+001  1.5e-007 2.25  
24  9.3e-005 7.8e-002 6.4e-003 9.85e-001  1.127681756e+001  1.151306937e+001  6.0e-008 2.33  
25  4.6e-005 6.7e-002 3.1e-003 9.93e-001  1.136980676e+001  1.148633243e+001  3.0e-008 2.41  
26  4.1e-005 6.1e-002 2.8e-003 9.97e-001  1.138013467e+001  1.148503310e+001  2.7e-008 2.52  
27  3.7e-005 5.6e-002 2.5e-003 9.97e-001  1.138808069e+001  1.148251118e+001  2.4e-008 2.59  
28  3.3e-005 5.1e-002 2.3e-003 9.97e-001  1.139546263e+001  1.148047255e+001  2.2e-008 2.69  
29  3.0e-005 4.6e-002 2.1e-003 9.97e-001  1.140207755e+001  1.147860388e+001  2.0e-008 2.73  
30  2.7e-005 4.3e-002 1.8e-003 9.98e-001  1.140801853e+001  1.147690703e+001  1.8e-008 2.83  
31  2.4e-005 3.9e-002 1.7e-003 9.98e-001  1.141335289e+001  1.147536422e+001  1.6e-008 2.94  
32  2.2e-005 3.6e-002 1.5e-003 9.98e-001  1.141814388e+001  1.147396384e+001  1.4e-008 3.03  
33  2.0e-005 3.3e-002 1.3e-003 9.98e-001  1.142244704e+001  1.147269316e+001  1.3e-008 3.13  
34  1.8e-005 3.0e-002 1.2e-003 9.98e-001  1.142631252e+001  1.147154086e+001  1.2e-008 3.19  
35  1.6e-005 2.8e-002 1.1e-003 9.99e-001  1.142978517e+001  1.147049606e+001  1.0e-008 3.23  
36  1.4e-005 2.6e-002 9.8e-004 9.99e-001  1.143290535e+001  1.146954976e+001  9.4e-009 3.30  
37  1.3e-005 2.4e-002 8.8e-004 9.99e-001  1.143570893e+001  1.146869243e+001  8.5e-009 3.34  
38  1.2e-005 2.3e-002 8.0e-004 9.99e-001  1.143822836e+001  1.146791634e+001  7.6e-009 3.41  
39  1.0e-005 2.1e-002 7.2e-004 9.99e-001  1.144049255e+001  1.146721401e+001  6.9e-009 3.45  
40  9.4e-006 2.0e-002 6.5e-004 9.99e-001  1.144252745e+001  1.146657861e+001  6.2e-009 3.52  
41  8.5e-006 1.8e-002 5.8e-004 9.99e-001  1.144435637e+001  1.146600410e+001  5.6e-009 3.56  
42  7.6e-006 1.7e-002 5.2e-004 1.00e+000  1.144600021e+001  1.146548434e+001  5.0e-009 3.64  
43  6.8e-006 1.6e-002 4.7e-004 1.00e+000  1.144747781e+001  1.146501432e+001  4.5e-009 3.69  
44  6.2e-006 1.5e-002 4.2e-004 1.00e+000  1.144880601e+001  1.146458968e+001  4.1e-009 3.73  
45  5.5e-006 1.5e-002 3.8e-004 1.00e+000  1.144999990e+001  1.146420600e+001  3.6e-009 3.78  
46  5.0e-006 1.4e-002 3.4e-004 9.99e-001  1.145107309e+001  1.146385968e+001  3.3e-009 3.84  
47  4.5e-006 1.3e-002 3.1e-004 9.99e-001  1.145203790e+001  1.146354676e+001  3.0e-009 3.89  
48  4.0e-006 1.3e-002 2.8e-004 9.99e-001  1.145290537e+001  1.146326419e+001  2.7e-009 3.95  
49  3.6e-006 1.2e-002 2.5e-004 9.99e-001  1.145368545e+001  1.146300887e+001  2.4e-009 4.00  
50  3.3e-006 1.2e-002 2.3e-004 1.00e+000  1.145438703e+001  1.146277833e+001  2.2e-009 4.05  
51  2.9e-006 1.1e-002 2.0e-004 1.00e+000  1.145501805e+001  1.146257031e+001  1.9e-009 4.09  
52  2.7e-006 1.1e-002 1.8e-004 9.99e-001  1.145558557e+001  1.146238298e+001  1.7e-009 4.13  
53  2.4e-006 1.0e-002 1.6e-004 9.99e-001  1.145609605e+001  1.146221411e+001  1.6e-009 4.14  
54  2.1e-006 1.0e-002 1.5e-004 1.00e+000  1.145655535e+001  1.146206156e+001  1.4e-009 4.16  
55  1.9e-006 9.9e-003 1.3e-004 1.00e+000  1.145696864e+001  1.146192376e+001  1.3e-009 4.17  
56  1.7e-006 9.6e-003 1.2e-004 1.00e+000  1.145734044e+001  1.146179976e+001  1.1e-009 4.24  
57  1.6e-006 9.4e-003 1.1e-004 9.99e-001  1.145767485e+001  1.146168845e+001  1.0e-009 4.28  
58  1.4e-006 9.2e-003 9.7e-005 9.99e-001  1.145797571e+001  1.146158823e+001  9.3e-010 4.34  
59  1.3e-006 9.0e-003 8.7e-005 1.00e+000  1.145824655e+001  1.146149744e+001  8.3e-010 4.42  
60  1.1e-006 8.8e-003 7.8e-005 1.00e+000  1.145849024e+001  1.146141582e+001  7.5e-010 4.52  
61  1.0e-006 8.7e-003 7.1e-005 1.00e+000  1.145870953e+001  1.146134222e+001  6.8e-010 4.63  
62  9.3e-007 8.5e-003 6.4e-005 1.00e+000  1.145890682e+001  1.146127612e+001  6.1e-010 4.72  
63  8.3e-007 8.4e-003 5.7e-005 1.00e+000  1.145908474e+001  1.146121633e+001  5.5e-010 4.78  
64  7.5e-007 8.3e-003 5.1e-005 1.00e+000  1.145924445e+001  1.146116283e+001  4.9e-010 4.84  
65  6.7e-007 8.2e-003 4.6e-005 1.00e+000  1.145938815e+001  1.146111473e+001  4.4e-010 4.91  
66  6.1e-007 8.1e-003 4.2e-005 9.97e-001  1.145951742e+001  1.146107160e+001  4.0e-010 4.97  
67  5.5e-007 8.1e-003 3.8e-005 1.01e+000  1.145963752e+001  1.146103078e+001  3.6e-010 5.02  
68  4.9e-007 8.0e-003 3.4e-005 1.01e+000  1.145974383e+001  1.146099489e+001  3.3e-010 5.08  
69  4.4e-007 8.0e-003 3.0e-005 9.96e-001  1.145983752e+001  1.146096369e+001  2.9e-010 5.14  
70  4.0e-007 7.9e-003 2.7e-005 9.96e-001  1.145992183e+001  1.146093560e+001  2.6e-010 5.22  
71  3.6e-007 7.9e-003 2.5e-005 1.01e+000  1.145999937e+001  1.146090936e+001  2.4e-010 5.28  
72  1.3e-007 2.7e-003 8.5e-006 1.01e+000  1.146044446e+001  1.146075739e+001  8.2e-011 5.34  
73  1.1e-007 2.5e-003 7.7e-006 1.05e+000  1.146047315e+001  1.146074760e+001  7.5e-011 5.41  
74  8.6e-008 4.7e-004 1.5e-006 9.30e-001  1.146064372e+001  1.146069866e+001  1.7e-011 5.47  
75  7.8e-008 4.3e-004 1.3e-006 1.41e+000  1.146064746e+001  1.146069671e+001  1.5e-011 5.53  
76  6.4e-008 3.8e-004 1.2e-006 1.89e+000  1.146065091e+001  1.146069336e+001  1.3e-011 5.61  
77  2.9e-007 1.4e-005 4.5e-008 8.69e-001  1.146069140e+001  1.146069384e+001  3.4e-012 5.69  
Interior-point optimizer terminated. Time: 5.70. 

Optimizer terminated. Time: 5.72    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1460691403e+001   nrm: 1e+002   Viol.  con: 6e-006   var: 0e+000 
  Dual.    obj: 1.1460693841e+001   nrm: 8e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 5.76 seconds.
result packing took 10% of solve time
solution checking took 2.5% of solve time
Using solver 'mosek'
Solving for 1899 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'.
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. *
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.
Freed constraints in eliminator : 487
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 0
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 4               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 929
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3607              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.08              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.05            
Factor     - nonzeros before factor : 1.53e+004         after factor           : 1.76e+005       
Factor     - dense dim.             : 0                 flops                  : 3.97e+007       
Factor     - GP saved nzs           : 3.48e+004         GP saved flops         : 1.07e+006       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.232431305e+005 2.000000000e+000  1.0e+000 0.11  
1   1.6e+003 2.1e+003 8.4e+004 -9.71e-001 -1.223419061e+005 2.779016751e+000  6.8e-001 0.20  
2   7.2e+002 9.8e+002 3.9e+004 -9.56e-001 -1.191367240e+005 5.690202207e+000  3.2e-001 0.30  
3   2.9e+002 3.9e+002 1.5e+004 -9.03e-001 -1.109285001e+005 2.473234205e+001  1.3e-001 0.39  
4   2.9e+002 3.9e+002 1.5e+004 -7.66e-001 -1.085781162e+005 2.085558056e+003  1.3e-001 0.48  
5   1.4e+002 1.9e+002 7.3e+003 -7.56e-001 -9.040762795e+004 6.353542155e+003  6.0e-002 0.56  
6   4.2e+001 5.8e+001 2.3e+003 -4.98e-001 -4.821236471e+004 1.186391396e+004  1.9e-002 0.64  
7   2.3e+001 3.2e+001 1.3e+003 2.09e-001  -3.104082601e+004 7.511036055e+003  1.0e-002 0.73  
8   1.1e+001 1.5e+001 5.9e+002 5.41e-001  -1.587397071e+004 4.212438796e+003  4.8e-003 0.83  
9   4.7e+000 6.5e+000 2.6e+002 8.02e-001  -6.974381080e+003 2.244430460e+003  2.1e-003 0.91  
10  2.2e+000 3.0e+000 1.2e+002 9.33e-001  -3.083736769e+003 1.212875338e+003  9.7e-004 0.98  
11  1.4e+000 2.0e+000 7.8e+001 9.84e-001  -2.021275759e+003 8.322644163e+002  6.4e-004 1.05  
12  9.4e-001 1.3e+000 5.1e+001 9.86e-001  -1.320204541e+003 5.693760107e+002  4.2e-004 1.13  
13  7.9e-001 1.2e+000 4.3e+001 9.64e-001  -1.125161408e+003 4.817188196e+002  3.6e-004 1.20  
14  3.2e-001 5.0e-001 1.7e+001 9.90e-001  -4.401504198e+002 2.103865269e+002  1.4e-004 1.28  
15  1.6e-001 2.6e-001 8.6e+000 1.00e+000  -2.129669045e+002 1.090525566e+002  7.2e-005 1.39  
16  4.9e-002 1.5e-001 2.8e+000 1.00e+000  -6.339885183e+001 3.964814142e+001  2.3e-005 1.47  
17  3.9e-002 1.3e-001 2.2e+000 1.00e+000  -4.943860941e+001 3.363687221e+001  1.9e-005 1.56  
18  2.1e-002 9.0e-002 1.2e+000 1.00e+000  -2.263270660e+001 2.131853819e+001  1.0e-005 1.64  
19  1.5e-002 6.9e-002 8.4e-001 1.02e+000  -1.278740729e+001 1.834995409e+001  7.2e-006 1.72  
20  7.2e-003 4.9e-002 4.1e-001 1.03e+000  -2.741923173e-002 1.504344336e+001  3.5e-006 1.78  
21  2.6e-003 6.9e-002 1.5e-001 1.02e+000  7.281056827e+000  1.268478354e+001  1.3e-006 1.86  
22  1.4e-003 5.2e-002 8.3e-002 9.94e-001  9.025580337e+000  1.204655749e+001  7.3e-007 1.95  
23  4.7e-004 7.3e-002 2.9e-002 9.80e-001  1.053669534e+001  1.161381453e+001  2.7e-007 2.05  
24  1.8e-004 7.0e-002 1.2e-002 9.82e-001  1.102006535e+001  1.145837344e+001  1.1e-007 2.14  
25  8.2e-005 6.7e-002 5.4e-003 9.93e-001  1.120037722e+001  1.140031685e+001  5.0e-008 2.17  
26  3.8e-005 6.4e-002 2.5e-003 9.98e-001  1.128107082e+001  1.137542780e+001  2.4e-008 2.22  
27  3.5e-005 5.9e-002 2.3e-003 9.99e-001  1.129027624e+001  1.137522350e+001  2.1e-008 2.27  
28  3.1e-005 5.4e-002 2.1e-003 1.00e+000  1.129657249e+001  1.137303085e+001  1.9e-008 2.31  
29  2.8e-005 4.9e-002 1.9e-003 1.00e+000  1.130233240e+001  1.137115280e+001  1.7e-008 2.36  
30  2.5e-005 4.5e-002 1.7e-003 1.00e+000  1.130748778e+001  1.136943237e+001  1.6e-008 2.41  
31  2.3e-005 4.1e-002 1.5e-003 1.00e+000  1.131211439e+001  1.136786954e+001  1.4e-008 2.45  
32  2.0e-005 3.8e-002 1.4e-003 1.00e+000  1.131626662e+001  1.136645052e+001  1.3e-008 2.47  
33  1.8e-005 3.5e-002 1.2e-003 1.00e+000  1.131999412e+001  1.136516315e+001  1.1e-008 2.50  
34  1.7e-005 3.2e-002 1.1e-003 1.00e+000  1.132334111e+001  1.136399610e+001  1.0e-008 2.56  
35  1.5e-005 3.0e-002 9.9e-004 1.00e+000  1.132634707e+001  1.136293896e+001  9.2e-009 2.64  
36  1.3e-005 2.7e-002 8.9e-004 1.00e+000  1.132904727e+001  1.136198204e+001  8.3e-009 2.70  
37  1.2e-005 2.5e-002 8.0e-004 1.00e+000  1.133147325e+001  1.136111628e+001  7.5e-009 2.73  
38  1.1e-005 2.4e-002 7.2e-004 1.00e+000  1.133365322e+001  1.136033338e+001  6.7e-009 2.77  
39  9.8e-006 2.2e-002 6.5e-004 1.00e+000  1.133561244e+001  1.135962581e+001  6.1e-009 2.80  
40  8.8e-006 2.0e-002 5.8e-004 1.00e+000  1.133737347e+001  1.135898653e+001  5.5e-009 2.86  
41  7.9e-006 1.9e-002 5.3e-004 1.00e+000  1.133895653e+001  1.135840924e+001  4.9e-009 2.92  
42  7.1e-006 1.8e-002 4.7e-004 1.00e+000  1.134037975e+001  1.135788782e+001  4.4e-009 2.95  
43  6.4e-006 1.7e-002 4.3e-004 1.00e+000  1.134165936e+001  1.135741713e+001  4.0e-009 2.98  
44  5.8e-006 1.6e-002 3.8e-004 1.00e+000  1.134280988e+001  1.135699241e+001  3.6e-009 3.02  
45  5.2e-006 1.5e-002 3.4e-004 1.00e+000  1.134384440e+001  1.135660911e+001  3.2e-009 3.03  
46  4.7e-006 1.4e-002 3.1e-004 1.00e+000  1.134477466e+001  1.135626327e+001  2.9e-009 3.06  
47  4.2e-006 1.4e-002 2.8e-004 1.00e+000  1.134561122e+001  1.135595125e+001  2.6e-009 3.08  
48  3.8e-006 1.3e-002 2.5e-004 1.00e+000  1.134636356e+001  1.135566988e+001  2.4e-009 3.11  
49  3.4e-006 1.2e-002 2.3e-004 1.00e+000  1.134704028e+001  1.135541600e+001  2.1e-009 3.14  
50  3.1e-006 1.2e-002 2.0e-004 1.00e+000  1.134764895e+001  1.135518735e+001  1.9e-009 3.19  
51  2.8e-006 1.1e-002 1.8e-004 1.00e+000  1.134819650e+001  1.135498131e+001  1.7e-009 3.20  
52  2.5e-006 1.1e-002 1.6e-004 1.00e+000  1.134868916e+001  1.135479554e+001  1.5e-009 3.23  
53  2.2e-006 1.1e-002 1.5e-004 1.00e+000  1.134913242e+001  1.135462822e+001  1.4e-009 3.27  
54  2.0e-006 1.0e-002 1.3e-004 1.00e+000  1.134953127e+001  1.135447756e+001  1.3e-009 3.30  
55  1.8e-006 1.0e-002 1.2e-004 1.00e+000  1.134989016e+001  1.135434196e+001  1.1e-009 3.31  
56  1.6e-006 9.8e-003 1.1e-004 1.00e+000  1.135021315e+001  1.135421980e+001  1.0e-009 3.33  
57  1.5e-006 9.5e-003 9.7e-005 1.00e+000  1.135050380e+001  1.135410989e+001  9.1e-010 3.36  
58  1.3e-006 9.3e-003 8.8e-005 9.99e-001  1.135076538e+001  1.135401099e+001  8.2e-010 3.39  
59  1.2e-006 9.1e-003 7.9e-005 1.00e+000  1.135100082e+001  1.135392189e+001  7.4e-010 3.44  
60  1.1e-006 8.9e-003 7.1e-005 1.00e+000  1.135121271e+001  1.135384172e+001  6.6e-010 3.47  
61  9.6e-007 8.8e-003 6.4e-005 9.99e-001  1.135140338e+001  1.135376969e+001  6.0e-010 3.50  
62  8.7e-007 8.6e-003 5.7e-005 9.98e-001  1.135157498e+001  1.135370493e+001  5.4e-010 3.53  
63  7.8e-007 8.5e-003 5.2e-005 1.00e+000  1.135172948e+001  1.135364647e+001  4.8e-010 3.56  
64  7.0e-007 8.4e-003 4.7e-005 1.00e+000  1.135186853e+001  1.135359388e+001  4.4e-010 3.59  
65  6.3e-007 8.3e-003 4.2e-005 9.99e-001  1.135199368e+001  1.135354658e+001  3.9e-010 3.64  
66  5.7e-007 8.2e-003 3.8e-005 9.99e-001  1.135210632e+001  1.135350399e+001  3.5e-010 3.70  
67  5.1e-007 8.1e-003 3.4e-005 9.98e-001  1.135220768e+001  1.135346573e+001  3.2e-010 3.75  
68  4.6e-007 8.0e-003 3.1e-005 9.98e-001  1.135229892e+001  1.135343126e+001  2.9e-010 3.81  
69  4.1e-007 7.9e-003 2.7e-005 9.99e-001  1.135238106e+001  1.135340020e+001  2.6e-010 3.86  
70  3.7e-007 7.8e-003 2.5e-005 9.96e-001  1.135245495e+001  1.135337235e+001  2.3e-010 3.89  
71  3.4e-007 7.8e-003 2.2e-005 1.00e+000  1.135252149e+001  1.135334717e+001  2.1e-010 3.92  
72  3.0e-007 7.7e-003 2.0e-005 1.00e+000  1.135258137e+001  1.135332450e+001  1.9e-010 3.97  
73  2.7e-007 7.7e-003 1.8e-005 1.00e+000  1.135263530e+001  1.135330403e+001  1.7e-010 4.03  
74  2.4e-007 7.6e-003 1.6e-005 9.98e-001  1.135268379e+001  1.135328571e+001  1.5e-010 4.08  
75  2.2e-007 7.6e-003 1.5e-005 1.00e+000  1.135272746e+001  1.135326915e+001  1.4e-010 4.13  
76  2.0e-007 7.6e-003 1.3e-005 1.00e+000  1.135276675e+001  1.135325428e+001  1.2e-010 4.14  
77  1.8e-007 7.5e-003 1.2e-005 1.00e+000  1.135280230e+001  1.135324079e+001  1.1e-010 4.17  
78  1.6e-007 7.5e-003 1.1e-005 1.00e+000  1.135283405e+001  1.135322896e+001  1.0e-010 4.22  
79  1.4e-007 7.5e-003 9.6e-006 9.97e-001  1.135286267e+001  1.135321813e+001  9.0e-011 4.25  
80  1.3e-007 7.5e-003 8.6e-006 1.00e+000  1.135288853e+001  1.135320829e+001  8.1e-011 4.28  
81  1.2e-007 7.4e-003 7.8e-006 1.00e+000  1.135291171e+001  1.135319949e+001  7.3e-011 4.34  
82  1.1e-007 7.4e-003 7.0e-006 1.00e+000  1.135293258e+001  1.135319156e+001  6.6e-011 4.41  
83  9.5e-008 7.4e-003 6.3e-006 1.00e+000  1.135295146e+001  1.135318437e+001  5.9e-011 4.44  
84  8.5e-008 6.7e-003 5.7e-006 1.01e+000  1.135296869e+001  1.135317779e+001  5.3e-011 4.47  
85  7.7e-008 6.0e-003 5.1e-006 1.01e+000  1.135298440e+001  1.135317177e+001  4.8e-011 4.50  
86  6.9e-008 5.4e-003 4.6e-006 9.99e-001  1.135299799e+001  1.135316664e+001  4.3e-011 4.53  
87  6.2e-008 4.9e-003 4.1e-006 1.03e+000  1.135301155e+001  1.135316135e+001  3.9e-011 4.56  
88  5.6e-008 4.4e-003 3.7e-006 1.01e+000  1.135302306e+001  1.135315693e+001  3.6e-011 4.59  
89  5.0e-008 3.9e-003 3.3e-006 1.00e+000  1.135303286e+001  1.135315322e+001  3.2e-011 4.61  
90  4.5e-008 3.5e-003 3.0e-006 1.02e+000  1.135304239e+001  1.135314954e+001  2.9e-011 4.64  
91  4.1e-008 3.2e-003 2.7e-006 1.02e+000  1.135305073e+001  1.135314635e+001  2.7e-011 4.66  
92  3.7e-008 2.9e-003 2.4e-006 1.03e+000  1.135305851e+001  1.135314334e+001  2.4e-011 4.69  
93  3.3e-008 2.6e-003 2.2e-006 1.05e+000  1.135306598e+001  1.135314032e+001  2.2e-011 4.70  
94  3.0e-008 2.3e-003 2.0e-006 1.02e+000  1.135307201e+001  1.135313803e+001  2.0e-011 4.75  
95  2.7e-008 2.1e-003 1.8e-006 9.65e-001  1.135307680e+001  1.135313637e+001  1.8e-011 4.76  
96  7.1e-008 1.9e-003 1.6e-006 1.02e+000  1.135308036e+001  1.135313918e+001  1.7e-011 4.80  
97  7.4e-008 1.7e-003 1.4e-006 9.64e-001  1.135308446e+001  1.135313636e+001  1.5e-011 4.81  
98  6.6e-008 1.5e-003 1.3e-006 9.89e-001  1.135308803e+001  1.135313478e+001  1.3e-011 4.84  
99  6.2e-008 1.4e-003 1.2e-006 9.79e-001  1.135309128e+001  1.135313312e+001  1.2e-011 4.86  
100 2.7e-008 1.7e-004 1.5e-007 9.40e-001  1.135311634e+001  1.135312146e+001  1.3e-012 4.88  
101 1.7e-009 9.7e-006 8.3e-009 9.52e-001  1.135312004e+001  1.135312034e+001  9.4e-014 4.91  
Interior-point optimizer terminated. Time: 4.91. 

Optimizer terminated. Time: 4.94    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1353120043e+001   nrm: 4e+001   Viol.  con: 2e-008   var: 0e+000 
  Dual.    obj: 1.1353120339e+001   nrm: 8e+002   Viol.  con: 0e+000   var: 7e-005 
* End solution on dual form. *
Transforming to primal solution.
Solving took 5.01 seconds.
result packing took 6% of solve time
solution checking took 1.4% of solve time
Using solver 'mosek'
Solving for 1899 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6216) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'.
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. *
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.
Freed constraints in eliminator : 487
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 0
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.03    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer  - threads                : 4               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 929
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3608              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          : 0.03            
Factor     - nonzeros before factor : 1.53e+004         after factor           : 1.76e+005       
Factor     - dense dim.             : 0                 flops                  : 3.97e+007       
Factor     - GP saved nzs           : 3.48e+004         GP saved flops         : 1.07e+006       
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+003 3.1e+003 1.2e+005 0.00e+000  -1.230179603e+005 2.000000000e+000  1.0e+000 0.09  
1   1.5e+003 2.1e+003 8.3e+004 -9.71e-001 -1.220992460e+005 2.793905100e+000  6.8e-001 0.13  
2   6.9e+002 9.4e+002 3.7e+004 -9.56e-001 -1.186951124e+005 5.885349252e+000  3.0e-001 0.16  
3   3.0e+002 4.1e+002 1.6e+004 -9.00e-001 -1.112618189e+005 2.390069083e+001  1.3e-001 0.17  
4   2.8e+002 3.8e+002 1.5e+004 -7.78e-001 -1.080957128e+005 2.169743869e+003  1.2e-001 0.19  
5   1.5e+002 2.0e+002 8.0e+003 -7.53e-001 -9.292748721e+004 5.775554373e+003  6.6e-002 0.22  
6   4.2e+001 5.8e+001 2.3e+003 -5.39e-001 -4.784883219e+004 1.227123986e+004  1.9e-002 0.23  
7   2.1e+001 2.9e+001 1.2e+003 2.10e-001  -2.859269735e+004 7.783879740e+003  9.5e-003 0.25  
8   1.0e+001 1.4e+001 5.7e+002 5.83e-001  -1.522693676e+004 4.288267346e+003  4.7e-003 0.28  
9   3.8e+000 5.2e+000 2.1e+002 8.14e-001  -5.625502258e+003 1.873864319e+003  1.7e-003 0.31  
10  1.8e+000 2.6e+000 1.0e+002 9.53e-001  -2.526233268e+003 1.151335271e+003  8.3e-004 0.34  
11  9.7e-001 1.3e+000 5.3e+001 9.87e-001  -1.341544576e+003 6.090696312e+002  4.4e-004 0.41  
12  9.0e-001 1.3e+000 4.9e+001 9.70e-001  -1.275669299e+003 5.623444883e+002  4.1e-004 0.47  
13  4.9e-001 7.0e-001 2.7e+001 9.82e-001  -6.883125363e+002 3.101906460e+002  2.2e-004 0.50  
14  1.9e-001 4.5e-001 1.0e+001 9.97e-001  -2.666444922e+002 1.249851453e+002  8.8e-005 0.55  
15  8.3e-002 2.2e-001 4.7e+000 1.01e+000  -1.116757593e+002 6.252911537e+001  3.9e-005 0.59  
16  3.4e-002 1.2e-001 1.9e+000 1.01e+000  -4.181341353e+001 2.928353745e+001  1.6e-005 0.66  
17  2.8e-002 1.0e-001 1.6e+000 9.96e-001  -3.247011223e+001 2.668772479e+001  1.4e-005 0.72  
18  1.1e-002 9.4e-002 6.2e-001 1.01e+000  -6.988903277e+000 1.600936457e+001  5.3e-006 0.80  
19  4.5e-003 8.6e-002 2.7e-001 1.04e+000  4.342927280e+000  1.390916420e+001  2.3e-006 0.83  
20  1.9e-003 6.2e-002 1.1e-001 9.89e-001  8.151113858e+000  1.222240838e+001  9.8e-007 0.86  
21  1.1e-003 4.8e-002 6.8e-002 9.57e-001  9.323750103e+000  1.184872635e+001  6.0e-007 0.91  
22  3.4e-004 7.5e-002 2.2e-002 9.52e-001  1.068496182e+001  1.151795175e+001  2.0e-007 0.94  
23  1.8e-004 5.8e-002 1.2e-002 9.66e-001  1.096353484e+001  1.142105251e+001  1.1e-007 0.97  
24  1.6e-004 5.3e-002 1.1e-002 9.76e-001  1.100141955e+001  1.141329111e+001  1.0e-007 1.02  
25  1.5e-004 4.8e-002 9.7e-003 9.76e-001  1.103387833e+001  1.140506138e+001  9.0e-008 1.05  
26  1.3e-004 4.4e-002 8.7e-003 9.77e-001  1.106457623e+001  1.139910788e+001  8.1e-008 1.11  
27  1.2e-004 4.0e-002 7.8e-003 9.79e-001  1.109220938e+001  1.139368127e+001  7.3e-008 1.19  
28  1.1e-004 3.7e-002 7.1e-003 9.81e-001  1.111706226e+001  1.138871415e+001  6.5e-008 1.25  
29  9.6e-005 3.4e-002 6.4e-003 9.83e-001  1.113938108e+001  1.138413852e+001  5.9e-008 1.30  
30  8.7e-005 3.1e-002 5.7e-003 9.84e-001  1.115941878e+001  1.137992434e+001  5.3e-008 1.33  
31  7.8e-005 2.9e-002 5.1e-003 9.86e-001  1.117740318e+001  1.137604296e+001  4.8e-008 1.38  
32  7.0e-005 2.7e-002 4.6e-003 9.87e-001  1.119354151e+001  1.137246974e+001  4.3e-008 1.42  
33  6.3e-005 2.5e-002 4.2e-003 9.88e-001  1.120802081e+001  1.136918172e+001  3.9e-008 1.45  
34  5.7e-005 2.3e-002 3.8e-003 9.90e-001  1.122101057e+001  1.136615877e+001  3.5e-008 1.50  
35  5.1e-005 2.1e-002 3.4e-003 9.91e-001  1.123266318e+001  1.136338153e+001  3.1e-008 1.56  
36  4.6e-005 2.0e-002 3.0e-003 9.91e-001  1.124311631e+001  1.136083260e+001  2.8e-008 1.59  
37  4.1e-005 1.9e-002 2.7e-003 9.92e-001  1.125249339e+001  1.135849527e+001  2.5e-008 1.64  
38  3.7e-005 1.7e-002 2.5e-003 9.93e-001  1.126090543e+001  1.135635412e+001  2.3e-008 1.67  
39  3.4e-005 1.6e-002 2.2e-003 9.94e-001  1.126845174e+001  1.135439398e+001  2.1e-008 1.70  
40  3.0e-005 1.5e-002 2.0e-003 9.94e-001  1.127522183e+001  1.135260123e+001  1.9e-008 1.72  
41  2.7e-005 1.5e-002 1.8e-003 9.95e-001  1.128129598e+001  1.135096300e+001  1.7e-008 1.74  
42  2.4e-005 1.4e-002 1.6e-003 9.95e-001  1.128674651e+001  1.134946786e+001  1.5e-008 1.77  
43  2.2e-005 1.3e-002 1.5e-003 9.96e-001  1.129163813e+001  1.134810452e+001  1.4e-008 1.78  
44  2.0e-005 1.3e-002 1.3e-003 9.96e-001  1.129602903e+001  1.134686262e+001  1.2e-008 1.84  
45  1.8e-005 1.2e-002 1.2e-003 9.97e-001  1.129997128e+001  1.134573285e+001  1.1e-008 1.91  
46  1.6e-005 1.2e-002 1.1e-003 9.97e-001  1.130351122e+001  1.134470588e+001  9.9e-009 1.95  
47  1.4e-005 1.1e-002 9.6e-004 9.97e-001  1.130669043e+001  1.134377312e+001  8.9e-009 2.00  
48  1.3e-005 1.1e-002 8.6e-004 9.98e-001  1.130954616e+001  1.134292673e+001  8.0e-009 2.05  
49  1.2e-005 1.0e-002 7.7e-004 9.98e-001  1.131211167e+001  1.134215916e+001  7.2e-009 2.08  
50  1.1e-005 1.0e-002 7.0e-004 9.98e-001  1.131441682e+001  1.134146351e+001  6.5e-009 2.11  
51  9.5e-006 9.8e-003 6.3e-004 9.98e-001  1.131648831e+001  1.134083375e+001  5.8e-009 2.14  
52  8.5e-006 9.5e-003 5.6e-004 9.98e-001  1.131834995e+001  1.134026361e+001  5.2e-009 2.23  
53  7.7e-006 9.3e-003 5.1e-004 9.99e-001  1.132002324e+001  1.133974775e+001  4.7e-009 2.28  
54  6.9e-006 9.1e-003 4.6e-004 9.99e-001  1.132152733e+001  1.133928127e+001  4.3e-009 2.30  
55  6.2e-006 8.9e-003 4.1e-004 9.99e-001  1.132287942e+001  1.133885943e+001  3.8e-009 2.34  
56  5.6e-006 8.7e-003 3.7e-004 9.99e-001  1.132409495e+001  1.133847814e+001  3.4e-009 2.36  
57  5.0e-006 8.5e-003 3.3e-004 9.99e-001  1.132518774e+001  1.133813349e+001  3.1e-009 2.38  
58  4.5e-006 8.4e-003 3.0e-004 9.99e-001  1.132617023e+001  1.133782220e+001  2.8e-009 2.41  
59  4.1e-006 8.3e-003 2.7e-004 9.99e-001  1.132705358e+001  1.133754099e+001  2.5e-009 2.44  
60  3.7e-006 8.2e-003 2.4e-004 9.99e-001  1.132784783e+001  1.133728714e+001  2.3e-009 2.45  
61  3.3e-006 8.1e-003 2.2e-004 1.00e+000  1.132856208e+001  1.133705783e+001  2.0e-009 2.47  
62  3.0e-006 8.0e-003 2.0e-004 9.99e-001  1.132920442e+001  1.133685098e+001  1.8e-009 2.48  
63  2.7e-006 7.9e-003 1.8e-004 1.00e+000  1.132978215e+001  1.133666434e+001  1.6e-009 2.50  
64  2.4e-006 7.8e-003 1.6e-004 1.00e+000  1.133030184e+001  1.133649596e+001  1.5e-009 2.53  
65  2.2e-006 7.7e-003 1.4e-004 1.00e+000  1.133076933e+001  1.133634423e+001  1.3e-009 2.55  
66  2.0e-006 7.7e-003 1.3e-004 1.00e+000  1.133118989e+001  1.133620752e+001  1.2e-009 2.56  
67  1.8e-006 7.6e-003 1.2e-004 1.00e+000  1.133156830e+001  1.133608424e+001  1.1e-009 2.59  
68  1.6e-006 7.5e-003 1.0e-004 1.00e+000  1.133190877e+001  1.133597323e+001  9.7e-010 2.61  
69  1.4e-006 7.5e-003 9.4e-005 1.00e+000  1.133221512e+001  1.133587321e+001  8.8e-010 2.64  
70  1.3e-006 7.4e-003 8.5e-005 1.00e+000  1.133249080e+001  1.133578308e+001  7.9e-010 2.69  
71  1.2e-006 7.4e-003 7.6e-005 1.00e+000  1.133273887e+001  1.133570189e+001  7.1e-010 2.72  
72  1.0e-006 7.4e-003 6.9e-005 1.00e+000  1.133296209e+001  1.133562884e+001  6.4e-010 2.77  
73  9.3e-007 7.3e-003 6.2e-005 1.00e+000  1.133316300e+001  1.133556292e+001  5.7e-010 2.78  
74  8.4e-007 7.3e-003 5.6e-005 1.00e+000  1.133334377e+001  1.133550371e+001  5.2e-010 2.81  
75  7.6e-007 7.3e-003 5.0e-005 1.00e+000  1.133350644e+001  1.133545037e+001  4.7e-010 2.88  
76  6.8e-007 7.2e-003 4.5e-005 1.00e+000  1.133365285e+001  1.133540231e+001  4.2e-010 2.89  
77  6.1e-007 7.2e-003 4.1e-005 9.99e-001  1.133378457e+001  1.133535920e+001  3.8e-010 2.91  
78  5.5e-007 7.2e-003 3.7e-005 1.00e+000  1.133390314e+001  1.133532026e+001  3.4e-010 2.94  
79  5.0e-007 7.2e-003 3.3e-005 1.00e+000  1.133400984e+001  1.133528525e+001  3.1e-010 2.95  
80  4.5e-007 7.2e-003 3.0e-005 1.00e+000  1.133410586e+001  1.133525370e+001  2.7e-010 2.97  
81  4.0e-007 7.1e-003 2.7e-005 1.00e+000  1.133419228e+001  1.133522530e+001  2.5e-010 3.03  
82  3.6e-007 7.1e-003 2.4e-005 9.99e-001  1.133427002e+001  1.133519984e+001  2.2e-010 3.05  
83  3.3e-007 7.1e-003 2.2e-005 9.98e-001  1.133433999e+001  1.133517692e+001  2.0e-010 3.06  
84  2.9e-007 7.1e-003 1.9e-005 9.99e-001  1.133440296e+001  1.133515624e+001  1.8e-010 3.08  
85  2.6e-007 7.1e-003 1.7e-005 9.99e-001  1.133445964e+001  1.133513762e+001  1.6e-010 3.11  
86  2.4e-007 7.0e-003 1.6e-005 9.96e-001  1.133451062e+001  1.133512092e+001  1.5e-010 3.13  
87  2.1e-007 7.0e-003 1.4e-005 1.00e+000  1.133455653e+001  1.133510581e+001  1.3e-010 3.16  
88  1.9e-007 7.0e-003 1.3e-005 9.98e-001  1.133459783e+001  1.133509223e+001  1.2e-010 3.17  
89  1.7e-007 7.0e-003 1.1e-005 9.99e-001  1.133463497e+001  1.133508013e+001  1.1e-010 3.19  
90  1.6e-007 7.0e-003 1.0e-005 9.99e-001  1.133466843e+001  1.133506910e+001  9.6e-011 3.20  
91  1.4e-007 6.3e-003 9.3e-006 1.00e+000  1.133469863e+001  1.133505909e+001  8.6e-011 3.22  
92  1.3e-007 5.7e-003 8.4e-006 1.00e+000  1.133472575e+001  1.133505011e+001  7.8e-011 3.23  
93  1.1e-007 5.1e-003 7.5e-006 9.97e-001  1.133475012e+001  1.133504210e+001  7.0e-011 3.28  
94  1.0e-007 4.6e-003 6.8e-006 1.00e+000  1.133477206e+001  1.133503484e+001  6.3e-011 3.34  
95  9.2e-008 4.1e-003 6.1e-006 9.99e-001  1.133479180e+001  1.133502832e+001  5.7e-011 3.36  
96  8.3e-008 3.7e-003 5.5e-006 1.00e+000  1.133480957e+001  1.133502244e+001  5.1e-011 3.38  
97  7.4e-008 3.3e-003 4.9e-006 9.95e-001  1.133482556e+001  1.133501719e+001  4.6e-011 3.41  
98  6.7e-008 3.0e-003 4.4e-006 1.00e+000  1.133484003e+001  1.133501238e+001  4.1e-011 3.44  
99  6.0e-008 2.7e-003 4.0e-006 9.99e-001  1.133485297e+001  1.133500810e+001  3.7e-011 3.45  
100 5.4e-008 2.4e-003 3.6e-006 9.91e-001  1.133486461e+001  1.133500429e+001  3.3e-011 3.47  
101 4.9e-008 2.2e-003 3.2e-006 1.00e+000  1.133487510e+001  1.133500080e+001  3.0e-011 3.50  
102 4.4e-008 2.0e-003 2.9e-006 9.95e-001  1.133488453e+001  1.133499769e+001  2.7e-011 3.53  
103 4.0e-008 1.8e-003 2.6e-006 1.01e+000  1.133489351e+001  1.133499464e+001  2.5e-011 3.55  
104 3.6e-008 1.6e-003 2.4e-006 1.00e+000  1.133490111e+001  1.133499212e+001  2.2e-011 3.56  
105 3.2e-008 1.4e-003 2.1e-006 9.95e-001  1.133490794e+001  1.133498986e+001  2.0e-011 3.58  
106 2.9e-008 1.3e-003 1.9e-006 1.01e+000  1.133491441e+001  1.133498768e+001  1.8e-011 3.61  
107 2.6e-008 1.2e-003 1.7e-006 1.02e+000  1.133492025e+001  1.133498598e+001  1.6e-011 3.64  
108 2.4e-008 1.0e-003 1.5e-006 1.00e+000  1.133492515e+001  1.133498441e+001  1.5e-011 3.69  
109 5.4e-009 2.0e-004 2.9e-007 9.94e-001  1.133496103e+001  1.133497233e+001  2.8e-012 3.72  
110 1.7e-009 2.1e-005 3.1e-008 9.88e-001  1.133496860e+001  1.133496980e+001  3.3e-013 3.78  
Interior-point optimizer terminated. Time: 3.80. 

Optimizer terminated. Time: 3.81    
solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.1334968597e+001   nrm: 6e+001   Viol.  con: 2e-008   var: 0e+000 
  Dual.    obj: 1.1334969799e+001   nrm: 8e+002   Viol.  con: 0e+000   var: 2e-004 
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.84 seconds.
result packing took 48% of solve time
solution checking took 1.9% of solve time
Solving took 6 GP solves and 59.3 seconds.
Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2418946.2635 force_pound * meter but the right hand side evaluated to 2375459.66779 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 32774.3794235 force_pound but the right hand side evaluated to 32399.9999958 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 2.21510116758 meter but the right hand side evaluated to 2.08157167501 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 1243573.42934 joule / kilogram but the right hand side evaluated to 1.56102234323 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 664754.463578 joule / kilogram but the right hand side evaluated to 0.667331536006 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 18.3998991534 meter but the right hand side evaluated to 16.3229313391 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 10.903618645686173 but the right hand side evaluated to 4.788860357107787 (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 10.019759040689513 but the right hand side evaluated to 4.7888603380081225 (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 8.144918096604439 but the right hand side evaluated to 4.788860361733324 (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 18.3622673353 meter but the right hand side evaluated to 18.1377489679 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 18.3622673353 meter but the right hand side evaluated to 18.2420897438 meter (Allowable error: 0.1%, Actual error: 0.65%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.2960382488746074 but the right hand side evaluated to 0.18973949731983578 (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 0.23302233177712495 but the right hand side evaluated to 0.1743469987647433 (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 7.563242765076594 but the right hand side evaluated to 4.7306394764189506 (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 7.583082296679405 but the right hand side evaluated to 4.757853360254244 (Allowable error: 0.1%, Actual error: 37%)


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


Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 72.283s

OK

Generating XML reports...
Cloning into 'solar'...
Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.3)
Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0)
grin 1.2.1 requires argparse>=1.1, which is not installed.
Collecting git+https://github.com/convexengineering/gpfit.git
  Cloning https://github.com/convexengineering/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-zvsx2m
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-pkkjuq\wheels\d5\94\ac\b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
Collecting git+https://github.com/convexengineering/gassolar.git
  Cloning https://github.com/convexengineering/gassolar.git to c:\users\jenkins\appdata\local\temp\pip-req-build-ocvbfu
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3)
Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0)
Building wheels for collected packages: gassolar
  Running setup.py bdist_wheel for gassolar: started
  Running setup.py bdist_wheel for gassolar: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-vvqxaa\wheels\fe\11\0a\2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
grin 1.2.1 requires argparse>=1.1, which is not installed.
Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\solar
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in c:\users\jenkins\workspace\gplibrary_pr_models\mosek (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2017.3)
Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.11.0)
Building wheels for collected packages: solar
  Running setup.py bdist_wheel for solar: started
  Running setup.py bdist_wheel for solar: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-f1az8x\wheels\f4\d5\5c\e37fedf74a44fbd5641b13d5622b97d759218ff594b631174a
Successfully built solar
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: solar
Successfully installed solar-0.0.0.0
adding test for 'solar/solar.py'
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
adding test for 'solar/npod_trade.py'
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 9 GP solves and 6.68 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 1388462.0896 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 1248775.4404 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 82150.9619 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 2.29645501791 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645195168 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 10.3 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 1388485.8163 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 1248796.8045 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 82150.9545 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 2.29645531143 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645224572 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)

Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 6.89 seconds.
Allowing negative dual variable(s) as small as -4.335401144357795e-11.
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 765970.5293 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.65/GustL.65_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.58/GustL.58_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.69/GustL.69_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.46/GustL.46_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.78/GustL.78_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.48/GustL.48_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.52/GustL.52_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.71/GustL.71_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.75/GustL.75_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.59/GustL.59_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.66/GustL.66_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.49/GustL.49_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.67/GustL.67_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.64/GustL.64_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.40/GustL.40_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.55/GustL.55_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.54/GustL.54_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.53/GustL.53_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.60/GustL.60_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.51/GustL.51_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.41/GustL.41_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.47/GustL.47_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.70/GustL.70_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.50/GustL.50_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.74/GustL.74_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.68/GustL.68_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.76/GustL.76_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.79/GustL.79_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.63/GustL.63_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.44/GustL.44_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.77/GustL.77_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.56/GustL.56_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.57/GustL.57_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.42/GustL.42_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.62/GustL.62_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.61/GustL.61_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.45/GustL.45_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.43/GustL.43_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.72/GustL.72_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.73/GustL.73_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 3.74 seconds.
Allowing negative dual variable(s) as small as -1.459213136685068e-11.
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 862671.9701 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 3.92 seconds.
Allowing negative dual variable(s) as small as -4.0916036806802364e-11.
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 987087.3059 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 2.67 seconds.
Allowing negative dual variable(s) as small as -3.199434053316174e-11.
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 1058302.5363 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.18 seconds.
Allowing negative dual variable(s) as small as -5.1212530748668e-11.
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 765970.5367 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.65/GustL.65_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.58/GustL.58_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.69/GustL.69_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.46/GustL.46_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.78/GustL.78_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.48/GustL.48_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.52/GustL.52_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.71/GustL.71_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.75/GustL.75_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.59/GustL.59_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.66/GustL.66_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.49/GustL.49_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.67/GustL.67_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.64/GustL.64_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.40/GustL.40_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.55/GustL.55_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.54/GustL.54_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.53/GustL.53_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.60/GustL.60_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.51/GustL.51_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.41/GustL.41_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.47/GustL.47_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.70/GustL.70_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.50/GustL.50_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.74/GustL.74_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.68/GustL.68_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.76/GustL.76_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.79/GustL.79_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.63/GustL.63_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.44/GustL.44_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.77/GustL.77_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.56/GustL.56_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.57/GustL.57_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.42/GustL.42_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.62/GustL.62_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.61/GustL.61_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.45/GustL.45_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.43/GustL.43_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.72/GustL.72_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.73/GustL.73_(0,).
  (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.16 seconds.
Allowing negative dual variable(s) as small as -7.328713655900363e-11.
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 862671.9919 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 4.09 seconds.
Allowing negative dual variable(s) as small as -1.8730345273519065e-11.
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 987087.2992 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 2.81 seconds.
Allowing negative dual variable(s) as small as -3.448659928759393e-11.
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 1058302.4683 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 12 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 1388461.6064 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 1248775.0066 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 82150.9606 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 2.29645499564 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645192897 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 11.6 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 1388485.7622 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 1248796.7557 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 82150.9545 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 2.29645531178 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645224609 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 0.863 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 838075.6771 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 10.5 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 1017215.7080 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 2.62125883684 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124748598 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 1.95293542403 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215494 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 1.04275941736 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521831 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 0.467698134702 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697004364 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 0.139006791868 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006573713 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 1.06 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 12.3 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.
Running tests...
----------------------------------------------------------------------
..C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
  tau = np.exp(-0.175/costhsun)
....EE
======================================================================
ERROR [64.237s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn
    mod.test()
  File "solar.py", line 654, in test
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
  File "solar.py", line 633, in setup
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 83, in __init__
    CostedConstraintSet.__init__(self, cost, constraints, substitutions)
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__
    ConstraintSet.__init__(self, constraints, subs)
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__
    list.__setitem__(self, i, ConstraintSet(constraint))
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__
    raise_elementhasnumpybools(constraint)
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 357, in raise_elementhasnumpybools
    % (cause, constraint))
ValueError: An ArrayConstraint was created with elements of numpy.bool_
Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]

======================================================================
ERROR [19.698s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn
    mod.test()
  File "solar.py", line 654, in test
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
  File "solar.py", line 633, in setup
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.13900678254 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006562766 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)

Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
\gpkit\constraints\model.py", line 83, in __init__
    CostedConstraintSet.__init__(self, cost, constraints, substitutions)
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__
    ConstraintSet.__init__(self, constraints, subs)
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__
    list.__setitem__(self, i, ConstraintSet(constraint))
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__
    raise_elementhasnumpybools(constraint)
  File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 357, in raise_elementhasnumpybools
    % (cause, constraint))
ValueError: An ArrayConstraint was created with elements of numpy.bool_
Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]

----------------------------------------------------------------------
Ran 8 tests in 754.040s

FAILED (errors=2)

Generating XML reports...
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.3)
Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0)
grin 1.2.1 requires argparse>=1.1, which is not installed.
Collecting git+https://github.com/hoburg/gpfit.git
  Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-0fjno_
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-0ikub_\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gplibrary
Requirement already satisfied: numpy>=1.12 in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1)
Building wheels for collected packages: gpkitmodels
  Running setup.py bdist_wheel for gpkitmodels: started
  Running setup.py bdist_wheel for gpkitmodels: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-g4zrwz\wheels\a3\80\70\6d80d6b876aaa160fc8dda3c238a4f64c571e65f335a009034
Successfully built gpkitmodels
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: gpkitmodels
  Found existing installation: gpkitmodels 0.0.0.0
    Uninstalling gpkitmodels-0.0.0.0:
      Successfully uninstalled gpkitmodels-0.0.0.0
Successfully installed gpkitmodels-0.0.0.0
adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py'
adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py'
adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py'
adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py'
adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.434 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.661 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.185 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.092 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.135 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 9.45 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 100.00655602 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 985.544372634 meter * revolutions_per_minute but the right hand side evaluated to 103.041409551 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 0.420585894291 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573114258 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 0.314645013884 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629875092 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 0.168936427278 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931592839 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 0.063964233833 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631337446 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 0.0226356538648 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354009094 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)

Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.523 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.485 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.675 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 11 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 100.006573035 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 985.544253301 meter * revolutions_per_minute but the right hand side evaluated to 103.041408907 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 0.420585197736 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420572696752 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 0.314644844733 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629685653 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 0.168936363968 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 0.0639642995251 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639632491352 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 0.0226356652666 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226353885393 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0012%)

Using solver 'mosek'
Solving for 13 variables.
Solving took 0.036 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 5.75 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 1619897.7902 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.379 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 6.42 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 1619891.9379 but bound is 700000.0000
Warning: Constraint [0.151*B_BladeElementProp/BladeElementPerf_(1,)**-2*F_BladeElementProp/BladeElementPerf_(1,)**2*R_Pro... >= 0.00633*B_BladeElementProp/BladeElementPerf_(1,)**2*G_BladeElementProp/BladeElementPerf_(1,)**2*r_Bl...] is not tight because the left hand side evaluated to 3.18328390896 meter ** 2 / second ** 2 but the right hand side evaluated to 3.18327922145 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00015%)

Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3838 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9776 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3883 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9590 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 1884891.6332 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.1579 but bound is 700000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000

Running tests...
----------------------------------------------------------------------
..........
----------------------------------------------------------------------
Ran 10 tests in 55.557s

OK

Generating XML reports...
Cloning into 'eVTOL'...
adding test for 'aircraft_models.py'

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 11.530s

OK

Generating XML reports...
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git']
  attempt 1

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

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

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

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
  attempt 1

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

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
  attempt 1

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

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

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

calling ['pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git']
  attempt 1

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

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
  attempt 1

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

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
  attempt 1

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


(venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>exit 0 
Build step 'Console output (build log) parsing' changed build result to FAILURE
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek' for the testing framework 'JUnit'.
[xUnit] [INFO] - Check 'Failed Tests' threshold.
[xUnit] [INFO] - Check 'Skipped Tests' threshold.
[xUnit] [INFO] - Setting the build status to FAILURE
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: FAILURE