Transforming to primal solution.
Solving took 7.85 seconds.
result packing took 4.5% of solve time
solution checking took 1.2% of solve time
Using solver 'mosek'
Solving for 1899 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6215) 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 : 3607 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 -1.233077111e+005 2.000000000e+000 1.0e+000 0.06
1 1.6e+003 2.1e+003 8.4e+004 -9.71e-001 -1.223909672e+005 2.791894501e+000 6.8e-001 0.09
2 6.8e+002 9.4e+002 3.7e+004 -9.56e-001 -1.189136286e+005 5.989386607e+000 3.0e-001 0.11
3 2.9e+002 3.9e+002 1.6e+004 -8.98e-001 -1.109631602e+005 2.525211054e+001 1.3e-001 0.13
4 2.9e+002 3.9e+002 1.5e+004 -7.65e-001 -1.086302791e+005 2.068926820e+003 1.3e-001 0.16
5 1.1e+002 1.5e+002 6.0e+003 -7.55e-001 -8.374365502e+004 7.889430305e+003 4.9e-002 0.17
6 4.5e+001 6.1e+001 2.4e+003 -3.96e-001 -5.019494636e+004 1.143610118e+004 2.0e-002 0.19
7 2.8e+001 3.8e+001 1.5e+003 1.76e-001 -3.558939452e+004 8.115385874e+003 1.2e-002 0.20
8 1.3e+001 1.8e+001 7.1e+002 4.56e-001 -1.881438153e+004 4.885634316e+003 5.8e-003 0.22
9 5.2e+000 7.1e+000 2.8e+002 7.48e-001 -7.630413398e+003 2.426809112e+003 2.3e-003 0.25
10 3.4e+000 4.7e+000 1.9e+002 9.25e-001 -5.001656506e+003 1.788917037e+003 1.5e-003 0.27
11 1.1e+000 1.5e+000 5.9e+001 9.58e-001 -1.556954044e+003 6.120662006e+002 4.9e-004 0.28
12 8.9e-001 1.4e+000 4.9e+001 9.85e-001 -1.268689550e+003 5.446789915e+002 4.0e-004 0.30
13 6.6e-001 1.1e+000 3.6e+001 9.71e-001 -9.473281228e+002 4.133286946e+002 3.0e-004 0.33
14 3.4e-001 5.7e-001 1.9e+001 9.99e-001 -4.716258855e+002 2.344442263e+002 1.6e-004 0.36
15 1.3e-001 2.4e-001 7.4e+000 9.96e-001 -1.823507724e+002 9.633453742e+001 6.2e-005 0.38
16 7.7e-002 1.5e-001 4.3e+000 1.01e+000 -1.013606618e+002 5.928676608e+001 3.6e-005 0.41
17 2.8e-002 1.1e-001 1.6e+000 1.01e+000 -3.170023468e+001 2.645486769e+001 1.3e-005 0.44
18 1.6e-002 8.7e-002 8.9e-001 1.01e+000 -1.443836123e+001 1.849355037e+001 7.5e-006 0.45
19 1.3e-002 6.9e-002 7.7e-001 1.03e+000 -9.873394887e+000 1.835823378e+001 6.5e-006 0.47
20 5.0e-003 6.7e-002 2.9e-001 1.02e+000 3.345494935e+000 1.396912097e+001 2.5e-006 0.52
21 2.5e-003 6.2e-002 1.5e-001 1.02e+000 7.350323693e+000 1.271306853e+001 1.3e-006 0.53
22 8.0e-004 7.4e-002 5.0e-002 9.86e-001 1.007229316e+001 1.189316564e+001 4.5e-007 0.55
23 2.5e-004 8.6e-002 1.6e-002 9.73e-001 1.099667619e+001 1.159975201e+001 1.5e-007 0.58
24 8.3e-005 8.5e-002 5.7e-003 9.83e-001 1.129453792e+001 1.150613656e+001 5.4e-008 0.59
25 3.2e-005 7.9e-002 2.3e-003 9.93e-001 1.139420716e+001 1.147869520e+001 2.2e-008 0.61
26 1.3e-005 7.5e-002 9.3e-004 9.97e-001 1.143329442e+001 1.146830042e+001 9.0e-009 0.63
27 5.9e-006 7.0e-002 4.1e-004 9.99e-001 1.144865207e+001 1.146415943e+001 4.0e-009 0.64
28 5.3e-006 6.4e-002 3.7e-004 1.00e+000 1.145002652e+001 1.146398401e+001 3.6e-009 0.69
29 4.8e-006 5.8e-002 3.4e-004 1.00e+000 1.145109586e+001 1.146365783e+001 3.2e-009 0.70
30 4.3e-006 5.3e-002 3.0e-004 1.00e+000 1.145205996e+001 1.146336615e+001 2.9e-009 0.73
31 3.9e-006 4.8e-002 2.7e-004 1.00e+000 1.145292622e+001 1.146310184e+001 2.6e-009 0.75
32 3.5e-006 4.4e-002 2.4e-004 1.00e+000 1.145370519e+001 1.146286336e+001 2.4e-009 0.77
33 3.1e-006 4.0e-002 2.2e-004 1.00e+000 1.145440572e+001 1.146264797e+001 2.1e-009 0.78
34 2.8e-006 3.7e-002 2.0e-004 1.00e+000 1.145503573e+001 1.146245392e+001 1.9e-009 0.80
35 2.5e-006 3.4e-002 1.8e-004 1.00e+000 1.145560241e+001 1.146227883e+001 1.7e-009 0.83
36 2.3e-006 3.1e-002 1.6e-004 1.00e+000 1.145611214e+001 1.146212103e+001 1.6e-009 0.89
37 2.1e-006 2.9e-002 1.4e-004 1.00e+000 1.145657073e+001 1.146197864e+001 1.4e-009 0.91
38 1.8e-006 2.7e-002 1.3e-004 9.99e-001 1.145698322e+001 1.146185062e+001 1.3e-009 0.92
39 1.7e-006 2.5e-002 1.2e-004 1.00e+000 1.145735454e+001 1.146173445e+001 1.1e-009 0.94
40 1.5e-006 2.3e-002 1.1e-004 1.00e+000 1.145768845e+001 1.146163050e+001 1.0e-009 0.95
41 1.3e-006 2.2e-002 9.5e-005 1.00e+000 1.145798896e+001 1.146153659e+001 9.2e-010 0.98
42 1.2e-006 2.0e-002 8.5e-005 1.00e+000 1.145825929e+001 1.146145221e+001 8.3e-010 1.00
43 1.1e-006 1.9e-002 7.7e-005 1.00e+000 1.145850256e+001 1.146137616e+001 7.4e-010 1.02
44 9.8e-007 1.8e-002 6.9e-005 9.99e-001 1.145872141e+001 1.146130788e+001 6.7e-010 1.03
45 8.8e-007 1.7e-002 6.2e-005 1.00e+000 1.145891843e+001 1.146124604e+001 6.0e-010 1.05
46 8.0e-007 1.6e-002 5.6e-005 9.98e-001 1.145909565e+001 1.146119070e+001 5.4e-010 1.06
47 7.2e-007 1.5e-002 5.0e-005 1.00e+000 1.145925517e+001 1.146114067e+001 4.9e-010 1.08
48 6.5e-007 1.4e-002 4.5e-005 9.93e-001 1.145939859e+001 1.146109612e+001 4.4e-010 1.13
49 5.8e-007 1.3e-002 4.1e-005 1.00e+000 1.145952777e+001 1.146105562e+001 4.0e-010 1.14
50 5.2e-007 1.3e-002 3.7e-005 1.00e+000 1.145964405e+001 1.146101907e+001 3.6e-010 1.16
51 4.7e-007 1.2e-002 3.3e-005 9.93e-001 1.145974858e+001 1.146098655e+001 3.2e-010 1.17
52 1.6e-007 4.2e-003 1.1e-005 9.98e-001 1.146036502e+001 1.146079279e+001 1.1e-010 1.19
53 1.5e-007 3.8e-003 1.0e-005 9.94e-001 1.146039778e+001 1.146078246e+001 1.0e-010 1.20
54 7.2e-008 1.4e-003 3.9e-006 1.09e+000 1.146057970e+001 1.146071647e+001 3.6e-011 1.24
55 6.4e-008 1.3e-003 3.5e-006 9.35e-001 1.146059065e+001 1.146071411e+001 3.3e-011 1.25
56 5.0e-008 2.4e-004 6.7e-007 9.72e-001 1.146067150e+001 1.146069550e+001 6.7e-012 1.27
57 4.3e-008 2.2e-004 6.0e-007 1.00e+000 1.146067336e+001 1.146069496e+001 6.0e-012 1.28
58 1.7e-008 1.3e-005 3.5e-008 9.53e-001 1.146068922e+001 1.146069051e+001 5.2e-013 1.30
Interior-point optimizer terminated. Time: 1.30.
Optimizer terminated. Time: 1.33
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1460689222e+001 nrm: 1e+002 Viol. con: 5e-007 var: 0e+000
Dual. obj: 1.1460690508e+001 nrm: 8e+002 Viol. con: 0e+000 var: 9e-005
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.37 seconds.
result packing took 20% of solve time
solution checking took 5.9% of solve time
Using solver 'mosek'
Solving for 1899 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6215) 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 : 3607 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.05 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.03
Factor - nonzeros before factor : 1.53e+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 -1.232431026e+005 2.000000000e+000 1.0e+000 0.09
1 1.6e+003 2.1e+003 8.4e+004 -9.71e-001 -1.223419531e+005 2.778950136e+000 6.8e-001 0.13
2 7.2e+002 9.8e+002 3.9e+004 -9.56e-001 -1.191336129e+005 5.692850614e+000 3.2e-001 0.14
3 2.9e+002 3.9e+002 1.5e+004 -9.03e-001 -1.109286085e+005 2.474616581e+001 1.3e-001 0.17
4 2.9e+002 3.9e+002 1.5e+004 -7.66e-001 -1.085783492e+005 2.085489611e+003 1.3e-001 0.19
5 1.4e+002 1.9e+002 7.3e+003 -7.56e-001 -9.041732622e+004 6.351799209e+003 6.0e-002 0.20
6 4.2e+001 5.8e+001 2.3e+003 -4.99e-001 -4.826123235e+004 1.185406778e+004 1.9e-002 0.22
7 2.3e+001 3.2e+001 1.3e+003 2.08e-001 -3.105817588e+004 7.510012590e+003 1.0e-002 0.27
8 1.1e+001 1.5e+001 5.9e+002 5.41e-001 -1.585866515e+004 4.209590038e+003 4.8e-003 0.31
9 4.7e+000 6.5e+000 2.6e+002 8.02e-001 -6.975664285e+003 2.245625308e+003 2.1e-003 0.34
10 2.2e+000 3.0e+000 1.2e+002 9.33e-001 -3.084315196e+003 1.212783694e+003 9.7e-004 0.41
11 1.4e+000 2.0e+000 7.8e+001 9.84e-001 -2.022103155e+003 8.325182003e+002 6.4e-004 0.44
12 9.4e-001 1.3e+000 5.1e+001 9.86e-001 -1.320315765e+003 5.694009820e+002 4.2e-004 0.45
13 7.9e-001 1.2e+000 4.3e+001 9.64e-001 -1.125404795e+003 4.818052188e+002 3.6e-004 0.48
14 3.2e-001 5.0e-001 1.7e+001 9.90e-001 -4.404948808e+002 2.105525218e+002 1.4e-004 0.52
15 1.6e-001 2.6e-001 8.6e+000 1.00e+000 -2.130665440e+002 1.090956025e+002 7.2e-005 0.55
16 4.9e-002 1.5e-001 2.8e+000 1.00e+000 -6.344512603e+001 3.967169520e+001 2.3e-005 0.56
17 3.9e-002 1.3e-001 2.2e+000 1.00e+000 -4.946305378e+001 3.365014668e+001 1.9e-005 0.59
18 2.1e-002 9.0e-002 1.2e+000 1.00e+000 -2.266161789e+001 2.132969362e+001 1.0e-005 0.61
19 1.5e-002 6.9e-002 8.5e-001 1.02e+000 -1.286698302e+001 1.837467849e+001 7.2e-006 0.64
20 7.3e-003 4.9e-002 4.2e-001 1.03e+000 -1.033234457e-001 1.507023746e+001 3.6e-006 0.66
21 2.6e-003 6.9e-002 1.5e-001 1.02e+000 7.280752652e+000 1.268541519e+001 1.3e-006 0.69
22 1.4e-003 5.2e-002 8.4e-002 9.94e-001 9.002589472e+000 1.205333081e+001 7.4e-007 0.70
23 4.7e-004 7.3e-002 3.0e-002 9.80e-001 1.052993128e+001 1.161598245e+001 2.7e-007 0.72
24 1.8e-004 7.1e-002 1.2e-002 9.82e-001 1.101943461e+001 1.145844454e+001 1.1e-007 0.73
25 8.3e-005 6.7e-002 5.4e-003 9.93e-001 1.119955977e+001 1.140049957e+001 5.1e-008 0.77
26 3.9e-005 6.4e-002 2.6e-003 9.98e-001 1.128069463e+001 1.137551677e+001 2.4e-008 0.78
27 3.5e-005 5.9e-002 2.3e-003 9.99e-001 1.128995430e+001 1.137532058e+001 2.2e-008 0.81
28 3.1e-005 5.4e-002 2.1e-003 1.00e+000 1.129628352e+001 1.137311921e+001 1.9e-008 0.83
29 2.8e-005 4.9e-002 1.9e-003 1.00e+000 1.130207373e+001 1.137123387e+001 1.7e-008 0.86
30 2.5e-005 4.5e-002 1.7e-003 1.00e+000 1.130725615e+001 1.136950657e+001 1.6e-008 0.88
31 2.3e-005 4.1e-002 1.5e-003 1.00e+000 1.131190701e+001 1.136793763e+001 1.4e-008 0.89
32 2.1e-005 3.8e-002 1.4e-003 1.00e+000 1.131608086e+001 1.136651270e+001 1.3e-008 0.91
33 1.8e-005 3.5e-002 1.2e-003 1.00e+000 1.131982782e+001 1.136522014e+001 1.1e-008 0.92
34 1.7e-005 3.2e-002 1.1e-003 1.00e+000 1.132319219e+001 1.136404828e+001 1.0e-008 0.95
35 1.5e-005 3.0e-002 9.9e-004 1.00e+000 1.132621375e+001 1.136298677e+001 9.3e-009 0.97
36 1.3e-005 2.7e-002 8.9e-004 1.00e+000 1.132892792e+001 1.136202566e+001 8.4e-009 0.98
37 1.2e-005 2.5e-002 8.0e-004 1.00e+000 1.133136647e+001 1.136115605e+001 7.5e-009 1.00
38 1.1e-005 2.4e-002 7.2e-004 1.00e+000 1.133355774e+001 1.136036972e+001 6.8e-009 1.02
39 9.8e-006 2.2e-002 6.5e-004 1.00e+000 1.133552709e+001 1.135965905e+001 6.1e-009 1.03
40 8.8e-006 2.0e-002 5.9e-004 1.00e+000 1.133729721e+001 1.135901687e+001 5.5e-009 1.06
41 8.0e-006 1.9e-002 5.3e-004 1.00e+000 1.133888844e+001 1.135843703e+001 4.9e-009 1.08
42 7.2e-006 1.8e-002 4.7e-004 1.00e+000 1.134031899e+001 1.135791324e+001 4.4e-009 1.09
43 6.4e-006 1.7e-002 4.3e-004 1.00e+000 1.134160518e+001 1.135744060e+001 4.0e-009 1.11
44 5.8e-006 1.6e-002 3.8e-004 1.00e+000 1.134276160e+001 1.135701404e+001 3.6e-009 1.13
45 5.2e-006 1.5e-002 3.5e-004 1.00e+000 1.134380142e+001 1.135662905e+001 3.2e-009 1.16
46 4.7e-006 1.4e-002 3.1e-004 1.00e+000 1.134473646e+001 1.135628160e+001 2.9e-009 1.17
47 4.2e-006 1.4e-002 2.8e-004 1.00e+000 1.134557733e+001 1.135596813e+001 2.6e-009 1.19
48 3.8e-006 1.3e-002 2.5e-004 1.00e+000 1.134633355e+001 1.135568545e+001 2.4e-009 1.20
49 3.4e-006 1.2e-002 2.3e-004 1.00e+000 1.134701369e+001 1.135543061e+001 2.1e-009 1.22
50 3.1e-006 1.2e-002 2.0e-004 1.00e+000 1.134762549e+001 1.135520086e+001 1.9e-009 1.24
51 2.8e-006 1.1e-002 1.8e-004 1.00e+000 1.134817585e+001 1.135499385e+001 1.7e-009 1.27
52 2.5e-006 1.1e-002 1.7e-004 1.00e+000 1.134867098e+001 1.135480739e+001 1.6e-009 1.28
53 2.2e-006 1.1e-002 1.5e-004 1.00e+000 1.134911651e+001 1.135463932e+001 1.4e-009 1.30
54 2.0e-006 1.0e-002 1.3e-004 1.00e+000 1.134951737e+001 1.135448804e+001 1.3e-009 1.31
55 1.8e-006 1.0e-002 1.2e-004 1.00e+000 1.134987808e+001 1.135435186e+001 1.1e-009 1.33
56 1.6e-006 9.8e-003 1.1e-004 1.00e+000 1.135020271e+001 1.135422918e+001 1.0e-009 1.36
57 1.5e-006 9.5e-003 9.8e-005 1.00e+000 1.135049488e+001 1.135411866e+001 9.2e-010 1.38
58 1.3e-006 9.3e-003 8.8e-005 9.99e-001 1.135075776e+001 1.135401938e+001 8.2e-010 1.41
59 1.2e-006 9.1e-003 7.9e-005 1.00e+000 1.135099439e+001 1.135392990e+001 7.4e-010 1.44
60 1.1e-006 8.9e-003 7.1e-005 1.00e+000 1.135120735e+001 1.135384939e+001 6.7e-010 1.45
61 9.7e-007 8.8e-003 6.4e-005 9.99e-001 1.135139900e+001 1.135377703e+001 6.0e-010 1.47
62 8.7e-007 8.6e-003 5.8e-005 9.99e-001 1.135157151e+001 1.135371183e+001 5.4e-010 1.49
63 7.8e-007 8.5e-003 5.2e-005 1.00e+000 1.135172680e+001 1.135365307e+001 4.9e-010 1.50
64 7.0e-007 8.4e-003 4.7e-005 1.00e+000 1.135186657e+001 1.135360022e+001 4.4e-010 1.52
65 6.3e-007 8.3e-003 4.2e-005 9.99e-001 1.135199234e+001 1.135355271e+001 3.9e-010 1.58
66 5.7e-007 8.2e-003 3.8e-005 1.00e+000 1.135210556e+001 1.135350991e+001 3.6e-010 1.61
67 5.1e-007 8.1e-003 3.4e-005 1.00e+000 1.135220746e+001 1.135347141e+001 3.2e-010 1.64
68 4.6e-007 8.0e-003 3.1e-005 1.00e+000 1.135229919e+001 1.135343672e+001 2.9e-010 1.66
69 4.2e-007 7.9e-003 2.8e-005 9.99e-001 1.135238172e+001 1.135340555e+001 2.6e-010 1.70
70 3.7e-007 7.9e-003 2.5e-005 1.00e+000 1.135245604e+001 1.135337739e+001 2.3e-010 1.75
71 3.4e-007 7.8e-003 2.2e-005 1.00e+000 1.135252292e+001 1.135335209e+001 2.1e-010 1.77
72 3.0e-007 7.7e-003 2.0e-005 1.00e+000 1.135258310e+001 1.135332937e+001 1.9e-010 1.78
73 2.7e-007 7.7e-003 1.8e-005 9.99e-001 1.135263724e+001 1.135330896e+001 1.7e-010 1.80
74 2.5e-007 7.7e-003 1.6e-005 1.00e+000 1.135268604e+001 1.135329047e+001 1.5e-010 1.83
75 2.2e-007 7.6e-003 1.5e-005 9.99e-001 1.135272991e+001 1.135327391e+001 1.4e-010 1.84
76 2.0e-007 7.6e-003 1.3e-005 9.95e-001 1.135276936e+001 1.135325908e+001 1.2e-010 1.86
77 1.8e-007 7.5e-003 1.2e-005 9.95e-001 1.135280488e+001 1.135324572e+001 1.1e-010 1.89
78 1.6e-007 7.5e-003 1.1e-005 9.94e-001 1.135283683e+001 1.135323373e+001 1.0e-010 1.95
79 1.5e-007 7.5e-003 9.6e-006 9.93e-001 1.135286559e+001 1.135322292e+001 9.0e-011 2.00
80 1.3e-007 7.4e-003 8.7e-006 9.93e-001 1.135289146e+001 1.135321325e+001 8.1e-011 2.05
81 1.2e-007 7.4e-003 7.8e-006 9.94e-001 1.135291476e+001 1.135320449e+001 7.3e-011 2.11
82 1.1e-007 7.4e-003 7.0e-006 9.99e-001 1.135293575e+001 1.135319651e+001 6.6e-011 2.14
83 9.5e-008 6.6e-003 6.3e-006 1.01e+000 1.135295496e+001 1.135318916e+001 5.9e-011 2.19
84 8.6e-008 6.0e-003 5.7e-006 1.00e+000 1.135297200e+001 1.135318268e+001 5.3e-011 2.25
85 7.7e-008 5.4e-003 5.1e-006 9.86e-001 1.135298724e+001 1.135317699e+001 4.8e-011 2.30
86 6.9e-008 4.8e-003 4.6e-006 9.82e-001 1.135300095e+001 1.135317188e+001 4.3e-011 2.36
87 6.3e-008 4.3e-003 4.1e-006 1.00e+000 1.135301348e+001 1.135316706e+001 3.9e-011 2.42
88 5.6e-008 3.9e-003 3.7e-006 1.00e+000 1.135302471e+001 1.135316276e+001 3.5e-011 2.45
89 5.1e-008 3.5e-003 3.4e-006 1.02e+000 1.135303570e+001 1.135315846e+001 3.2e-011 2.50
90 4.6e-008 3.2e-003 3.0e-006 9.93e-001 1.135304459e+001 1.135315511e+001 2.9e-011 2.52
91 4.1e-008 2.9e-003 2.7e-006 9.75e-001 1.135305257e+001 1.135315216e+001 2.6e-011 2.53
92 3.7e-008 2.6e-003 2.4e-006 9.99e-001 1.135305977e+001 1.135314941e+001 2.3e-011 2.58
93 3.3e-008 2.3e-003 2.2e-006 9.52e-001 1.135306621e+001 1.135314710e+001 2.1e-011 2.59
94 3.0e-008 2.1e-003 2.0e-006 1.02e+000 1.135307243e+001 1.135314466e+001 1.9e-011 2.63
95 2.7e-008 1.9e-003 1.8e-006 1.02e+000 1.135307812e+001 1.135314229e+001 1.7e-011 2.64
96 2.4e-008 1.7e-003 1.6e-006 9.93e-001 1.135308276e+001 1.135314054e+001 1.6e-011 2.67
97 2.2e-008 1.5e-003 1.4e-006 9.53e-001 1.135308692e+001 1.135313905e+001 1.4e-011 2.69
98 2.0e-008 1.4e-003 1.3e-006 9.48e-001 1.135309066e+001 1.135313772e+001 1.3e-011 2.70
99 1.8e-008 1.2e-003 1.2e-006 1.04e+000 1.135309461e+001 1.135313613e+001 1.2e-011 2.77
100 1.6e-008 1.1e-003 1.1e-006 1.13e+000 1.135309936e+001 1.135313407e+001 1.1e-011 2.78
101 2.2e-008 8.0e-005 7.6e-008 8.72e-001 1.135312476e+001 1.135312762e+001 1.9e-012 2.81
102 2.2e-008 7.2e-005 6.9e-008 9.47e-001 1.135312402e+001 1.135312610e+001 1.5e-012 2.91
103 7.4e-009 4.3e-006 4.1e-009 1.00e+000 1.135312456e+001 1.135312468e+001 9.4e-014 2.94
Interior-point optimizer terminated. Time: 2.95.
Optimizer terminated. Time: 2.97
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1353124559e+001 nrm: 4e+001 Viol. con: 7e-008 var: 0e+000
Dual. obj: 1.1353124683e+001 nrm: 8e+002 Viol. con: 0e+000 var: 3e-005
* End solution on dual form. *
Transforming to primal solution.
Solving took 3 seconds.
result packing took 13% of solve time
solution checking took 2.8% 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 : 0.02
Lin. dep. - number : 0
Presolve terminated. Time: 0.05
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 : 0.05 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 -1.230179556e+005 2.000000000e+000 1.0e+000 0.11
1 1.5e+003 2.1e+003 8.3e+004 -9.71e-001 -1.220991743e+005 2.793962899e+000 6.8e-001 0.14
2 6.9e+002 9.4e+002 3.7e+004 -9.56e-001 -1.186976852e+005 5.883138646e+000 3.0e-001 0.19
3 3.0e+002 4.1e+002 1.6e+004 -9.00e-001 -1.112572403e+005 2.390134570e+001 1.3e-001 0.22
4 2.8e+002 3.8e+002 1.5e+004 -7.78e-001 -1.081041296e+005 2.168457188e+003 1.2e-001 0.23
5 1.5e+002 2.0e+002 8.0e+003 -7.53e-001 -9.295145595e+004 5.769454091e+003 6.6e-002 0.27
6 4.2e+001 5.8e+001 2.3e+003 -5.39e-001 -4.795051819e+004 1.225786017e+004 1.9e-002 0.28
7 2.2e+001 2.9e+001 1.2e+003 2.09e-001 -2.863213812e+004 7.786858693e+003 9.5e-003 0.30
8 1.1e+001 1.4e+001 5.7e+002 5.82e-001 -1.523939674e+004 4.289996173e+003 4.7e-003 0.31
9 3.8e+000 5.2e+000 2.1e+002 8.14e-001 -5.622505805e+003 1.872958878e+003 1.7e-003 0.33
10 1.8e+000 2.6e+000 1.0e+002 9.53e-001 -2.530304055e+003 1.153325989e+003 8.3e-004 0.36
11 9.6e-001 1.3e+000 5.3e+001 9.87e-001 -1.337472284e+003 6.074705589e+002 4.4e-004 0.38
12 9.0e-001 1.3e+000 4.9e+001 9.69e-001 -1.273592954e+003 5.615267699e+002 4.1e-004 0.39
13 4.9e-001 7.0e-001 2.7e+001 9.82e-001 -6.887430815e+002 3.104832483e+002 2.2e-004 0.41
14 1.9e-001 4.4e-001 1.0e+001 9.97e-001 -2.668057530e+002 1.250516527e+002 8.8e-005 0.42
15 8.4e-002 2.2e-001 4.7e+000 1.01e+000 -1.118259481e+002 6.257865469e+001 3.9e-005 0.45
16 3.4e-002 1.2e-001 1.9e+000 1.01e+000 -4.180551488e+001 2.927422600e+001 1.6e-005 0.47
17 2.8e-002 1.0e-001 1.6e+000 9.96e-001 -3.248567431e+001 2.669190643e+001 1.4e-005 0.48
18 1.1e-002 9.4e-002 6.2e-001 1.01e+000 -6.973560407e+000 1.600448669e+001 5.3e-006 0.50
19 4.5e-003 8.6e-002 2.7e-001 1.04e+000 4.334500116e+000 1.391030045e+001 2.3e-006 0.52
20 1.9e-003 6.2e-002 1.1e-001 9.89e-001 8.149913380e+000 1.222230321e+001 9.8e-007 0.53
21 1.1e-003 4.8e-002 6.8e-002 9.57e-001 9.322384415e+000 1.184885231e+001 6.0e-007 0.56
22 3.4e-004 7.5e-002 2.2e-002 9.52e-001 1.068414954e+001 1.151808200e+001 2.0e-007 0.58
23 1.8e-004 5.8e-002 1.2e-002 9.66e-001 1.096353766e+001 1.142095314e+001 1.1e-007 0.59
24 1.6e-004 5.3e-002 1.1e-002 9.76e-001 1.100142609e+001 1.141320477e+001 1.0e-007 0.61
25 1.5e-004 4.8e-002 9.7e-003 9.76e-001 1.103388081e+001 1.140498098e+001 9.0e-008 0.64
26 1.3e-004 4.4e-002 8.7e-003 9.77e-001 1.106457734e+001 1.139903531e+001 8.1e-008 0.66
27 1.2e-004 4.0e-002 7.8e-003 9.79e-001 1.109220971e+001 1.139361614e+001 7.3e-008 0.67
28 1.1e-004 3.7e-002 7.1e-003 9.81e-001 1.111706209e+001 1.138865580e+001 6.5e-008 0.69
29 9.6e-005 3.4e-002 6.3e-003 9.83e-001 1.113938048e+001 1.138408606e+001 5.9e-008 0.70
30 8.7e-005 3.1e-002 5.7e-003 9.84e-001 1.115941801e+001 1.137987728e+001 5.3e-008 0.73
31 7.8e-005 2.9e-002 5.1e-003 9.86e-001 1.117740241e+001 1.137600091e+001 4.8e-008 0.78
32 7.0e-005 2.7e-002 4.6e-003 9.87e-001 1.119354069e+001 1.137243208e+001 4.3e-008 0.84
33 6.3e-005 2.5e-002 4.2e-003 9.88e-001 1.120802005e+001 1.136914808e+001 3.9e-008 0.92
34 5.7e-005 2.3e-002 3.8e-003 9.90e-001 1.122100983e+001 1.136612861e+001 3.5e-008 1.00
35 5.1e-005 2.1e-002 3.4e-003 9.91e-001 1.123266262e+001 1.136335471e+001 3.1e-008 1.02
36 4.6e-005 2.0e-002 3.0e-003 9.91e-001 1.124311575e+001 1.136080846e+001 2.8e-008 1.05
37 4.1e-005 1.9e-002 2.7e-003 9.92e-001 1.125249308e+001 1.135847392e+001 2.5e-008 1.06
38 3.7e-005 1.7e-002 2.5e-003 9.93e-001 1.126090514e+001 1.135633482e+001 2.3e-008 1.08
39 3.4e-005 1.6e-002 2.2e-003 9.94e-001 1.126845164e+001 1.135437671e+001 2.1e-008 1.09
40 3.0e-005 1.5e-002 2.0e-003 9.94e-001 1.127522197e+001 1.135258604e+001 1.9e-008 1.11
41 2.7e-005 1.5e-002 1.8e-003 9.95e-001 1.128129623e+001 1.135094964e+001 1.7e-008 1.13
42 2.4e-005 1.4e-002 1.6e-003 9.95e-001 1.128674678e+001 1.134945585e+001 1.5e-008 1.14
43 2.2e-005 1.3e-002 1.5e-003 9.96e-001 1.129163854e+001 1.134809389e+001 1.4e-008 1.16
44 2.0e-005 1.3e-002 1.3e-003 9.96e-001 1.129602959e+001 1.134685349e+001 1.2e-008 1.19
45 1.8e-005 1.2e-002 1.2e-003 9.97e-001 1.129997186e+001 1.134572481e+001 1.1e-008 1.20
46 1.6e-005 1.2e-002 1.1e-003 9.97e-001 1.130351185e+001 1.134469879e+001 9.9e-009 1.22
47 1.4e-005 1.1e-002 9.6e-004 9.97e-001 1.130669116e+001 1.134376704e+001 8.9e-009 1.24
48 1.3e-005 1.1e-002 8.6e-004 9.98e-001 1.130954692e+001 1.134292139e+001 8.0e-009 1.25
49 1.2e-005 1.0e-002 7.7e-004 9.98e-001 1.131211251e+001 1.134215458e+001 7.2e-009 1.27
50 1.1e-005 1.0e-002 7.0e-004 9.98e-001 1.131441771e+001 1.134145961e+001 6.5e-009 1.30
51 9.5e-006 9.8e-003 6.3e-004 9.98e-001 1.131648924e+001 1.134083025e+001 5.8e-009 1.31
52 8.5e-006 9.5e-003 5.6e-004 9.99e-001 1.131835098e+001 1.134026061e+001 5.2e-009 1.34
53 7.7e-006 9.3e-003 5.1e-004 9.99e-001 1.132002432e+001 1.133974522e+001 4.7e-009 1.38
54 6.9e-006 9.1e-003 4.6e-004 9.99e-001 1.132152846e+001 1.133927916e+001 4.3e-009 1.39
55 6.2e-006 8.9e-003 4.1e-004 9.99e-001 1.132288059e+001 1.133885765e+001 3.8e-009 1.41
56 5.6e-006 8.7e-003 3.7e-004 9.99e-001 1.132409615e+001 1.133847667e+001 3.4e-009 1.42
57 5.0e-006 8.5e-003 3.3e-004 9.99e-001 1.132518897e+001 1.133813239e+001 3.1e-009 1.44
58 4.5e-006 8.4e-003 3.0e-004 9.99e-001 1.132617146e+001 1.133782147e+001 2.8e-009 1.49
59 4.1e-006 8.3e-003 2.7e-004 9.99e-001 1.132705483e+001 1.133754050e+001 2.5e-009 1.55
60 3.7e-006 8.2e-003 2.4e-004 9.99e-001 1.132784913e+001 1.133728676e+001 2.3e-009 1.56
61 3.3e-006 8.1e-003 2.2e-004 1.00e+000 1.132856340e+001 1.133705768e+001 2.0e-009 1.59
62 3.0e-006 8.0e-003 2.0e-004 1.00e+000 1.132920578e+001 1.133685086e+001 1.8e-009 1.63
63 2.7e-006 7.9e-003 1.8e-004 1.00e+000 1.132978353e+001 1.133666440e+001 1.6e-009 1.64
64 2.4e-006 7.8e-003 1.6e-004 1.00e+000 1.133030324e+001 1.133649615e+001 1.5e-009 1.66
65 2.2e-006 7.7e-003 1.4e-004 1.00e+000 1.133077074e+001 1.133634453e+001 1.3e-009 1.67
66 2.0e-006 7.7e-003 1.3e-004 1.00e+000 1.133119133e+001 1.133620790e+001 1.2e-009 1.69
67 1.8e-006 7.6e-003 1.2e-004 1.00e+000 1.133156975e+001 1.133608474e+001 1.1e-009 1.70
68 1.6e-006 7.5e-003 1.0e-004 1.00e+000 1.133191024e+001 1.133597374e+001 9.7e-010 1.72
69 1.4e-006 7.5e-003 9.4e-005 1.00e+000 1.133221660e+001 1.133587384e+001 8.8e-010 1.75
70 1.3e-006 7.4e-003 8.5e-005 1.00e+000 1.133249226e+001 1.133578386e+001 7.9e-010 1.77
71 1.2e-006 7.4e-003 7.6e-005 1.00e+000 1.133274032e+001 1.133570281e+001 7.1e-010 1.78
72 1.0e-006 7.4e-003 6.9e-005 1.00e+000 1.133296355e+001 1.133562982e+001 6.4e-010 1.80
73 9.3e-007 7.3e-003 6.2e-005 1.00e+000 1.133316445e+001 1.133556403e+001 5.7e-010 1.81
74 8.4e-007 7.3e-003 5.6e-005 1.00e+000 1.133334521e+001 1.133550489e+001 5.2e-010 1.83
75 7.6e-007 7.3e-003 5.0e-005 1.00e+000 1.133350791e+001 1.133545154e+001 4.7e-010 1.84
76 6.8e-007 7.2e-003 4.5e-005 1.00e+000 1.133365430e+001 1.133540359e+001 4.2e-010 1.86
77 6.1e-007 7.2e-003 4.1e-005 9.99e-001 1.133378603e+001 1.133536049e+001 3.8e-010 1.88
78 5.5e-007 7.2e-003 3.6e-005 1.00e+000 1.133390460e+001 1.133532162e+001 3.4e-010 1.89
79 5.0e-007 7.2e-003 3.3e-005 1.00e+000 1.133401132e+001 1.133528655e+001 3.1e-010 1.91
80 4.5e-007 7.1e-003 3.0e-005 9.99e-001 1.133410733e+001 1.133525510e+001 2.7e-010 1.92
81 4.0e-007 7.1e-003 2.7e-005 1.00e+000 1.133419374e+001 1.133522676e+001 2.5e-010 1.94
82 3.6e-007 7.1e-003 2.4e-005 1.00e+000 1.133427150e+001 1.133520124e+001 2.2e-010 1.95
83 3.3e-007 7.1e-003 2.2e-005 1.00e+000 1.133434149e+001 1.133517825e+001 2.0e-010 1.99
84 2.9e-007 7.1e-003 1.9e-005 1.00e+000 1.133440448e+001 1.133515754e+001 1.8e-010 2.00
85 2.6e-007 7.1e-003 1.7e-005 1.00e+000 1.133446133e+001 1.133513883e+001 1.6e-010 2.02
86 2.4e-007 7.1e-003 1.6e-005 1.00e+000 1.133451232e+001 1.133512209e+001 1.5e-010 2.03
87 2.1e-007 7.0e-003 1.4e-005 9.97e-001 1.133455819e+001 1.133510708e+001 1.3e-010 2.05
88 1.9e-007 7.0e-003 1.3e-005 1.00e+000 1.133459949e+001 1.133509350e+001 1.2e-010 2.06
89 1.7e-007 7.0e-003 1.1e-005 9.98e-001 1.133463664e+001 1.133508132e+001 1.1e-010 2.08
90 1.6e-007 7.0e-003 1.0e-005 9.96e-001 1.133467007e+001 1.133507037e+001 9.6e-011 2.09
91 1.4e-007 7.0e-003 9.3e-006 1.00e+000 1.133470018e+001 1.133506044e+001 8.6e-011 2.11
92 1.3e-007 7.0e-003 8.3e-006 9.95e-001 1.133472725e+001 1.133505157e+001 7.8e-011 2.14
93 1.1e-007 7.0e-003 7.5e-006 9.98e-001 1.133475163e+001 1.133504354e+001 7.0e-011 2.16
94 1.0e-007 7.0e-003 6.8e-006 1.00e+000 1.133477358e+001 1.133503630e+001 6.3e-011 2.17
95 9.2e-008 6.9e-003 6.1e-006 9.95e-001 1.133479331e+001 1.133502982e+001 5.7e-011 2.22
96 8.3e-008 6.9e-003 5.5e-006 9.98e-001 1.133481108e+001 1.133502397e+001 5.1e-011 2.25
97 7.4e-008 6.9e-003 4.9e-006 1.00e+000 1.133482707e+001 1.133501868e+001 4.6e-011 2.27
98 6.7e-008 6.2e-003 4.4e-006 1.01e+000 1.133484182e+001 1.133501375e+001 4.1e-011 2.28
99 6.0e-008 5.6e-003 4.0e-006 1.01e+000 1.133485524e+001 1.133500925e+001 3.7e-011 2.30
100 5.4e-008 5.0e-003 3.6e-006 9.83e-001 1.133486679e+001 1.133500552e+001 3.4e-011 2.31
101 4.9e-008 4.5e-003 3.2e-006 1.00e+000 1.133487732e+001 1.133500201e+001 3.0e-011 2.34
102 4.4e-008 4.1e-003 2.9e-006 1.02e+000 1.133488732e+001 1.133499863e+001 2.8e-011 2.38
103 4.0e-008 3.7e-003 2.6e-006 1.01e+000 1.133489594e+001 1.133499576e+001 2.5e-011 2.39
104 3.6e-008 3.3e-003 2.4e-006 1.01e+000 1.133490359e+001 1.133499321e+001 2.2e-011 2.41
105 3.2e-008 3.0e-003 2.1e-006 1.00e+000 1.133491033e+001 1.133499099e+001 2.0e-011 2.42
106 2.9e-008 2.7e-003 1.9e-006 9.99e-001 1.133491639e+001 1.133498898e+001 1.8e-011 2.44
107 1.1e-007 2.5e-003 1.8e-006 1.01e+000 1.133492338e+001 1.133497895e+001 1.6e-011 2.47
108 2.0e-008 4.7e-004 3.4e-007 1.00e+000 1.133496179e+001 1.133497244e+001 3.0e-012 2.48
109 1.2e-009 2.6e-005 1.9e-008 9.90e-001 1.133497044e+001 1.133497104e+001 1.8e-013 2.50
Interior-point optimizer terminated. Time: 2.50.
Optimizer terminated. Time: 2.52
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1334970439e+001 nrm: 5e+001 Viol. con: 1e-008 var: 0e+000
Dual. obj: 1.1334971037e+001 nrm: 8e+002 Viol. con: 0e+000 var: 2e-004
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.56 seconds.
result packing took 72% of solve time
solution checking took 3.3% of solve time
Solving took 6 GP solves and 45.8 seconds.
Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2418945.24546 force_pound * meter but the right hand side evaluated to 2375463.46832 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 32774.4494772 force_pound but the right hand side evaluated to 32399.9999983 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 2.21510116801 meter but the right hand side evaluated to 2.08163799485 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 1243585.11889 joule / kilogram but the right hand side evaluated to 1.5612453679 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 664768.948101 joule / kilogram but the right hand side evaluated to 0.667348960596 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 18.3998846711 meter but the right hand side evaluated to 16.3228538601 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 10.903638454726586 but the right hand side evaluated to 4.7888567104431745 (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 10.019875156016207 but the right hand side evaluated to 4.788856703434532 (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 8.144905507897082 but the right hand side evaluated to 4.7888567121676475 (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 18.3622045037 meter but the right hand side evaluated to 18.1376992949 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 18.3622045037 meter but the right hand side evaluated to 18.2420306092 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 0.2960301088493189 but the right hand side evaluated to 0.18973756114239743 (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 0.23302056648262948 but the right hand side evaluated to 0.17434671984925168 (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 7.563261738189791 but the right hand side evaluated to 4.73063931874231 (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 7.58309922089107 but the right hand side evaluated to 4.757850808429351 (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 57.803s
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-nfxzwn
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-bjfwuw\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-hfuzxm
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-k9sfey\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-8v8r2d\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 5.59 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0624 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1388461.0993 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 1248774.5487 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 82150.9623 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 2.29645500327 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645193703 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 9 GP solves and 5.71 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0624 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1388463.4586 but bound is 600000.0000
Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1248776.6745 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 82150.9601 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 2.29645501839 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645195175 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 5.38 seconds.
Allowing negative dual variable(s) as small as -8.19247542299993e-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 765970.6061 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 3.48 seconds.
Allowing negative dual variable(s) as small as -7.834061262334159e-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 862671.9975 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 5.92 seconds.
Allowing negative dual variable(s) as small as -2.918435053034562e-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 1.8 seconds.
Allowing negative dual variable(s) as small as -3.12870574518503e-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 1058302.4851 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 3.68 seconds.
Allowing negative dual variable(s) as small as -1.0471123535107248e-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 765970.5160 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 3.63 seconds.
Allowing negative dual variable(s) as small as -8.117145612342004e-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 862671.9978 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 3.38 seconds.
Allowing negative dual variable(s) as small as -6.930846963973269e-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 987087.3138 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek'
Solving for 6269 variables.
Solving took 1.75 seconds.
Allowing negative dual variable(s) as small as -2.0105004462850625e-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 1058302.4804 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 9 GP solves and 5.11 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0624 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 1388461.1258 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 1248774.5739 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 82150.9608 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 2.29645499448 meter ** 2 / second ** 2 but the right hand side evaluated to 2.2964519278 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 9 GP solves and 5.23 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 1388485.8708 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 1248796.8535 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 2.29645531221 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645224651 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 0.422 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1958 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 838075.6769 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.1/GustL.1_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 8 GP solves and 4.8 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.1418 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1017215.3805 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 78650.4125 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 2.62125882769 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124747684 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 1.95293542382 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215473 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 1.0427594177 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521865 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 0.46769813495 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697004612 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 0.139006791945 meter ** 2 / second ** 2 but the right hand side evaluated to 0.13900657379 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Using solver 'mosek_cli'
Solving for 702 variables.
Solving took 0.43 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1958 but bound is 0.9465
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 838072.5912 but bound is 600000.0000
Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.1/GustL.1_(0,).
(to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True)
Beginning signomial solve.
Solving took 8 GP solves and 6.01 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.1418 but bound is 0.9465
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1017215.9574 but bound is 600000.0000
Warning: Constraint [dQ_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2,) [N... >= B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2,)*G_M...] is not tight because the left hand side evaluated to 0.546199983583 meter * newton but the right hand side evaluated to 0.54619937481 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,), could cause inaccurate result because it is below lower bound. Solution is 78650.5577 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 2.62125881924 meter ** 2 / second ** 2 but the right hand side evaluated to 2.6212478085 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00042%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(1... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.9529359766 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292347375 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00064%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.04275932764 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275522741 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00039%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(3... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.467698058867 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697044815 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00022%)
Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(4... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/Ai
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 [37.575s]: 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 [11.053s]: 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\gpkitrcraftDrag.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 519.843s
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-cnr3wn
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-h4dhmq\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-8bktga\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 0.032 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.103 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.023 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.025 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.027 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 2.41 seconds.
Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006556021 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%)
Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544375341 meter * revolutions_per_minute but the right hand side evaluated to 103.041410023 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 0.420585906135 meter ** 2 / second ** 2 but the right hand side evaluated to 0.42057312607 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 0.314645036828 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629898059 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 0.168936439983 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931605546 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 0.0639642366761 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631365881 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 0.0226356536661 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354007108 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)
Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.13 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.134 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.134 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 4.48 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 100.006572888 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 985.544273012 meter * revolutions_per_minute but the right hand side evaluated to 103.041409265 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 0.420585155677 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420572612637 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 0.314644832147 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 0.063964388845 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639632465767 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0018%)
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 0.0226356607395 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 0.029 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 1.45 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 1619898.0082 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.083 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 2.77 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 18.561s
OK
Generating XML reports...
Cloning into 'eVTOL'...
adding test for 'aircraft_models.py'
Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 2.552s
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
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