Skipping 39 KB..
Full LogMax payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.850697530618287e-13.
Allowing negative dual variable(s) as small as -3.394875526530061e-13.
Allowing negative dual variable(s) as small as -1.0229282698670517e-12.
Allowing negative dual variable(s) as small as -1.0224360420807432e-12.
Allowing negative dual variable(s) as small as -2.825253052340937e-13.
Allowing negative dual variable(s) as small as -1.1550551639281925e-12.
Allowing negative dual variable(s) as small as -1.1171121536493467e-12.
Allowing negative dual variable(s) as small as -1.1164533653042902e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.2103043719145778e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.145447845799072e-11.
Allowing negative dual variable(s) as small as -1.4547436733749435e-12.
Allowing negative dual variable(s) as small as -6.4632319386302305e-12.
Allowing negative dual variable(s) as small as -6.468757461645472e-12.
Solving took 4 GP solves and 4.72 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.42 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Running tests...
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....
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Ran 4 tests in 87.759s
OK
Generating XML reports...
Cloning into 'turbofan'...
Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\turbofan
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.8.1)
Building wheels for collected packages: turbofan
Running setup.py bdist_wheel for turbofan: started
Running setup.py bdist_wheel for turbofan: finished with status 'done'
Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-xdjw7c\wheels\3a\4a\df\1e137b486523078491de3a0319a07f314f5e9aa745dfaf6fd5
Successfully built turbofan
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: turbofan
Successfully installed turbofan-0.0.0.0
adding test for 'turbofan/engine_validation.py'
Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528311 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%)
Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485052 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%)
Running tests...
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.
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Ran 1 test in 3.258s
OK
Generating XML reports...
Cloning into 'SPaircraft'...
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Collecting git+https://github.com/hoburg/turbofan.git
Cloning https://github.com/hoburg/turbofan.git to c:\users\jenkins\appdata\local\temp\pip-req-build-bav2tl
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.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 turbofan==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.8.1)
Building wheels for collected packages: turbofan
Running setup.py bdist_wheel for turbofan: started
Running setup.py bdist_wheel for turbofan: finished with status 'done'
Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-4tswha\wheels\49\e6\3a\5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5
Successfully built turbofan
grin 1.2.1 requires argparse>=1.1, which is not installed.
adding test for 'SP_aircraft.py'
Beginning signomial solve.
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
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 : 485
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: 0.01
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 : 3606 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 : 1.52e+004 after factor : 1.75e+005
Factor - dense dim. : 0 flops : 3.95e+007
Factor - GP saved nzs : -1.40e+005 GP saved flops : -3.84e+007
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+003 3.5e+003 1.2e+005 0.00e+000 -1.241488813e+005 2.000000000e+000 1.0e+000 0.06
1 1.5e+003 2.3e+003 8.0e+004 -9.71e-001 -1.230686685e+005 2.971062159e+000 6.4e-001 0.14
2 6.4e+002 1.0e+003 3.5e+004 -9.53e-001 -1.193008499e+005 6.575658302e+000 2.8e-001 0.22
3 2.9e+002 4.5e+002 1.6e+004 -8.91e-001 -1.118074281e+005 2.808647532e+001 1.3e-001 0.34
4 2.9e+002 4.5e+002 1.6e+004 -7.65e-001 -1.098743216e+005 1.714956975e+003 1.3e-001 0.42
5 1.0e+002 1.6e+002 5.5e+003 -7.58e-001 -8.115733064e+004 8.827734773e+003 4.5e-002 0.47
6 3.6e+001 5.7e+001 2.0e+003 -3.54e-001 -4.316716147e+004 1.174864646e+004 1.6e-002 0.55
7 1.6e+001 2.6e+001 9.0e+002 2.99e-001 -2.298794343e+004 6.536824455e+003 7.3e-003 0.61
8 8.0e+000 1.2e+001 4.3e+002 6.71e-001 -1.157952520e+004 3.817312180e+003 3.5e-003 0.67
9 3.6e+000 5.5e+000 1.9e+002 8.63e-001 -5.013780258e+003 2.102850781e+003 1.6e-003 0.73
10 1.8e+000 2.8e+000 1.0e+002 9.56e-001 -2.270091911e+003 1.453144911e+003 8.2e-004 0.78
11 6.7e-001 1.0e+000 3.7e+001 9.85e-001 -6.169576210e+002 7.675330084e+002 3.1e-004 0.86
12 5.7e-001 9.2e-001 3.2e+001 9.80e-001 -4.755569191e+002 7.122017146e+002 2.6e-004 0.97
13 4.2e-001 7.3e-001 2.3e+001 9.75e-001 -2.607244656e+002 6.225214478e+002 1.9e-004 1.05
14 2.1e-001 4.5e-001 1.2e+001 9.88e-001 4.360976403e+001 4.905463213e+002 9.7e-005 1.13
15 6.3e-002 1.9e-001 3.6e+000 1.00e+000 2.632298615e+002 3.980237586e+002 3.0e-005 1.17
16 1.9e-002 1.4e-001 1.1e+000 1.00e+000 3.277475301e+002 3.698728767e+002 9.5e-006 1.26
17 4.8e-003 1.4e-001 2.9e-001 1.00e+000 3.497760880e+002 3.605589517e+002 2.5e-006 1.34
18 2.8e-003 1.1e-001 1.7e-001 1.00e+000 3.528662850e+002 3.591631240e+002 1.4e-006 1.45
19 4.6e-004 1.7e-001 2.8e-002 1.00e+000 3.565847855e+002 3.576459316e+002 2.5e-007 1.55
20 1.7e-004 1.1e-001 1.1e-002 9.92e-001 3.570645779e+002 3.574613625e+002 9.2e-008 1.63
21 4.9e-005 1.1e-001 3.1e-003 1.00e+000 3.572660308e+002 3.573815503e+002 2.7e-008 1.70
22 3.1e-005 8.6e-002 2.0e-003 9.82e-001 3.572956556e+002 3.573692848e+002 1.7e-008 1.78
23 1.1e-005 8.1e-002 7.1e-004 9.71e-001 3.573293307e+002 3.573561571e+002 6.2e-009 1.86
24 5.3e-006 7.0e-002 3.3e-004 1.01e+000 3.573396196e+002 3.573521388e+002 2.9e-009 1.92
25 2.3e-006 6.9e-002 1.4e-004 1.00e+000 3.573447240e+002 3.573501463e+002 1.3e-009 2.00
26 2.1e-006 6.8e-002 1.3e-004 1.00e+000 3.573451249e+002 3.573500036e+002 1.1e-009 2.11
27 1.9e-006 6.2e-002 1.2e-004 1.00e+000 3.573454730e+002 3.573498635e+002 1.0e-009 2.19
28 1.7e-006 5.6e-002 1.0e-004 1.00e+000 3.573457873e+002 3.573497388e+002 9.2e-010 2.28
29 1.5e-006 5.1e-002 9.4e-005 1.00e+000 3.573460703e+002 3.573496266e+002 8.3e-010 2.33
30 1.4e-006 4.7e-002 8.5e-005 1.00e+000 3.573463249e+002 3.573495257e+002 7.5e-010 2.39
31 1.2e-006 4.2e-002 7.6e-005 1.00e+000 3.573465541e+002 3.573494348e+002 6.7e-010 2.45
32 1.1e-006 3.9e-002 6.9e-005 1.00e+000 3.573467603e+002 3.573493530e+002 6.0e-010 2.52
33 9.9e-007 3.6e-002 6.2e-005 1.00e+000 3.573469459e+002 3.573492793e+002 5.4e-010 2.59
34 8.9e-007 3.3e-002 5.6e-005 1.00e+000 3.573471130e+002 3.573492130e+002 4.9e-010 2.69
35 8.0e-007 3.0e-002 5.0e-005 1.00e+000 3.573472632e+002 3.573491534e+002 4.4e-010 2.77
36 7.2e-007 2.8e-002 4.5e-005 1.00e+000 3.573473983e+002 3.573491002e+002 4.0e-010 2.83
37 6.5e-007 2.6e-002 4.1e-005 1.00e+000 3.573475201e+002 3.573490517e+002 3.6e-010 2.91
38 5.8e-007 2.4e-002 3.6e-005 1.00e+000 3.573476296e+002 3.573490081e+002 3.2e-010 2.98
39 5.3e-007 2.2e-002 3.3e-005 1.00e+000 3.573477261e+002 3.573489755e+002 2.9e-010 3.06
40 4.7e-007 2.0e-002 3.0e-005 1.00e+000 3.573478150e+002 3.573489393e+002 2.6e-010 3.14
41 6.5e-007 2.0e-002 2.9e-005 1.02e+000 3.573478365e+002 3.573489271e+002 2.5e-010 3.22
42 5.2e-007 1.9e-002 2.6e-005 9.99e-001 3.573479146e+002 3.573488947e+002 2.3e-010 3.30
43 5.6e-007 1.9e-002 2.6e-005 1.10e+000 3.573479122e+002 3.573489005e+002 2.3e-010 3.38
44 5.1e-007 1.7e-002 2.3e-005 1.00e+000 3.573479803e+002 3.573488787e+002 2.1e-010 3.45
45 4.6e-007 1.6e-002 2.1e-005 1.00e+000 3.573480436e+002 3.573488528e+002 1.9e-010 3.55
46 6.5e-007 1.6e-002 2.0e-005 1.04e+000 3.573480836e+002 3.573488069e+002 1.8e-010 3.63
47 6.0e-007 1.5e-002 1.8e-005 1.00e+000 3.573481368e+002 3.573487872e+002 1.6e-010 3.72
48 6.4e-007 1.5e-002 1.8e-005 1.94e+000 3.573481434e+002 3.573487736e+002 1.6e-010 3.80
49 5.7e-007 1.3e-002 1.6e-005 1.00e+000 3.573481906e+002 3.573487573e+002 1.4e-010 3.88
50 5.9e-007 1.3e-002 1.6e-005 1.18e+000 3.573481926e+002 3.573487553e+002 1.4e-010 3.94
51 5.4e-007 1.3e-002 1.5e-005 1.00e+000 3.573482350e+002 3.573487406e+002 1.3e-010 4.01
52 4.9e-007 1.3e-002 1.3e-005 1.00e+000 3.573482732e+002 3.573487276e+002 1.2e-010 4.08
53 5.6e-007 1.2e-002 1.3e-005 9.85e-001 3.573482770e+002 3.573487253e+002 1.2e-010 4.16
54 5.1e-007 1.2e-002 1.3e-005 8.67e-001 3.573482816e+002 3.573487255e+002 1.1e-010 4.22
55 5.0e-007 1.2e-002 1.3e-005 9.58e-001 3.573482818e+002 3.573487251e+002 1.1e-010 4.30
56 4.5e-007 1.2e-002 1.2e-005 9.99e-001 3.573482868e+002 3.573487388e+002 1.1e-010 4.38
57 4.1e-007 1.1e-002 1.1e-005 9.95e-001 3.573483186e+002 3.573487288e+002 9.7e-011 4.45
58 4.1e-007 1.0e-002 1.0e-005 8.83e-001 3.573483473e+002 3.573487199e+002 8.8e-011 4.55
59 4.6e-007 1.0e-002 1.0e-005 1.00e+000 3.573483373e+002 3.573487193e+002 8.7e-011 4.63
60 4.0e-007 9.8e-003 9.2e-006 9.93e-001 3.573483640e+002 3.573487116e+002 7.8e-011 4.70
61 3.6e-007 9.7e-003 8.3e-006 9.94e-001 3.573483896e+002 3.573487003e+002 7.1e-011 4.78
62 3.3e-007 9.5e-003 7.4e-006 1.00e+000 3.573484121e+002 3.573486916e+002 6.4e-011 4.86
63 3.0e-007 9.3e-003 6.7e-006 1.00e+000 3.573484323e+002 3.573486840e+002 5.7e-011 4.95
64 1.7e-006 8.8e-003 6.4e-006 9.71e-001 3.573484461e+002 3.573486677e+002 5.4e-011 5.01
65 1.7e-006 8.8e-003 6.6e-006 1.00e+000 3.573484374e+002 3.573486677e+002 5.4e-011 5.08
66 1.6e-006 8.8e-003 6.3e-006 1.00e+000 3.573484434e+002 3.573486623e+002 4.8e-011 5.16
67 1.4e-006 8.5e-003 5.7e-006 1.00e+000 3.573484601e+002 3.573486581e+002 4.4e-011 5.23
68 1.3e-006 8.4e-003 5.7e-006 1.00e+000 3.573484557e+002 3.573486538e+002 3.9e-011 5.31
69 1.2e-006 8.4e-003 5.1e-006 9.99e-001 3.573484715e+002 3.573486499e+002 3.5e-011 5.41
70 1.0e-006 7.5e-003 4.6e-006 1.01e+000 3.573484863e+002 3.573486461e+002 3.2e-011 5.47
71 9.4e-007 6.8e-003 4.1e-006 1.00e+000 3.573484991e+002 3.573486429e+002 2.9e-011 5.56
72 1.1e-006 6.8e-003 4.1e-006 9.99e-001 3.573484997e+002 3.573486427e+002 2.9e-011 5.66
73 1.2e-006 6.7e-003 3.5e-006 1.00e+000 3.573485214e+002 3.573486426e+002 2.9e-011 5.72
74 1.1e-006 6.2e-003 3.1e-006 1.00e+000 3.573485292e+002 3.573486425e+002 2.6e-011 5.80
75 1.2e-006 6.2e-003 3.2e-006 1.00e+000 3.573485274e+002 3.573486424e+002 2.6e-011 5.84
76 1.7e-006 6.1e-003 3.2e-006 9.70e-001 3.573485285e+002 3.573486412e+002 2.6e-011 5.94
77 1.5e-006 6.1e-003 2.9e-006 1.01e+000 3.573485370e+002 3.573486393e+002 2.3e-011 6.00
78 1.5e-006 6.1e-003 3.1e-006 1.00e+000 3.573485290e+002 3.573486393e+002 2.3e-011 6.08
79 4.7e-006 6.0e-003 1.4e-006 1.00e+000 3.573486896e+002 3.573486391e+002 2.3e-011 6.13
80 4.3e-006 6.0e-003 1.4e-006 1.06e+000 3.573486914e+002 3.573486401e+002 2.3e-011 6.20
81 4.4e-006 6.0e-003 1.5e-006 1.00e+000 3.573486959e+002 3.573486401e+002 2.3e-011 6.28
82 5.7e-006 5.3e-003 1.4e-006 1.00e+000 3.573486835e+002 3.573486355e+002 2.0e-011 6.33
83 5.1e-006 5.3e-003 7.4e-007 1.00e+000 3.573486094e+002 3.573486355e+002 2.0e-011 6.41
84 4.9e-006 5.1e-003 7.1e-007 9.50e-001 3.573486096e+002 3.573486346e+002 1.9e-011 6.55
85 5.6e-006 5.0e-003 7.0e-007 1.01e+000 3.573486109e+002 3.573486370e+002 1.9e-011 6.64
86 5.1e-006 4.5e-003 6.3e-007 1.00e+000 3.573486111e+002 3.573486347e+002 1.7e-011 6.73
87 4.6e-006 4.5e-003 5.7e-007 9.82e-001 3.573486117e+002 3.573486332e+002 1.5e-011 6.88
88 4.1e-006 4.2e-003 5.1e-007 1.64e+000 3.573486127e+002 3.573486326e+002 1.4e-011 6.97
89 3.8e-006 3.7e-003 1.2e-006 1.00e+000 3.573485834e+002 3.573486308e+002 1.3e-011 7.03
90 3.9e-006 3.7e-003 1.2e-006 1.16e+000 3.573485840e+002 3.573486278e+002 1.2e-011 7.11
91 3.8e-006 3.7e-003 1.2e-006 1.05e+000 3.573485840e+002 3.573486277e+002 1.2e-011 7.17
92 4.3e-006 3.7e-003 1.2e-006 1.03e+000 3.573485841e+002 3.573486277e+002 1.2e-011 7.25
93 4.7e-006 3.7e-003 1.2e-006 1.03e+000 3.573485842e+002 3.573486272e+002 1.2e-011 7.33
94 4.3e-006 3.7e-003 1.0e-006 1.00e+000 3.573485904e+002 3.573486272e+002 1.2e-011 7.42
95 4.3e-006 3.7e-003 1.0e-006 1.03e+000 3.573485910e+002 3.573486261e+002 1.2e-011 7.51
96 2.9e-006 3.3e-003 2.5e-006 1.00e+000 3.573487095e+002 3.573486250e+002 1.1e-011 7.58
97 2.9e-006 3.3e-003 2.5e-006 1.08e+000 3.573487183e+002 3.573486272e+002 1.1e-011 7.64
98 2.9e-006 3.3e-003 2.5e-006 1.09e+000 3.573487204e+002 3.573486277e+002 1.1e-011 7.73
99 2.9e-006 3.3e-003 2.6e-006 1.00e+000 3.573487254e+002 3.573486277e+002 1.1e-011 7.81
100 3.5e-006 3.3e-003 2.9e-006 1.00e+000 3.573487376e+002 3.573486277e+002 1.1e-011 7.94
101 3.6e-006 3.3e-003 2.9e-006 2.08e+000 3.573487377e+002 3.573486278e+002 1.1e-011 8.05
102 3.7e-006 3.3e-003 2.9e-006 4.27e-002 3.573487374e+002 3.573486277e+002 1.1e-011 8.14
103 4.2e-006 3.2e-003 1.0e-005 1.00e+000 3.573490165e+002 3.573486273e+002 1.1e-011 8.19
104 4.1e-006 3.1e-003 1.0e-005 9.24e-001 3.573489925e+002 3.573486258e+002 1.0e-011 8.27
105 3.8e-006 3.1e-003 8.4e-006 1.00e+000 3.573489289e+002 3.573486256e+002 1.0e-011 8.34
106 3.8e-006 3.1e-003 8.4e-006 1.00e+000 3.573489295e+002 3.573486256e+002 1.0e-011 8.42
107 4.3e-006 2.9e-003 1.3e-005 1.00e+000 3.573490941e+002 3.573486250e+002 9.6e-012 8.50
108 4.3e-006 2.9e-003 1.3e-005 9.02e-001 3.573491182e+002 3.573486263e+002 9.5e-012 8.58
109 4.2e-006 2.9e-003 1.3e-005 5.01e-001 3.573491229e+002 3.573486266e+002 9.5e-012 8.67
110 4.2e-006 2.9e-003 1.3e-005 1.03e+000 3.573491176e+002 3.573486263e+002 9.5e-012 8.73
111 4.3e-006 2.9e-003 1.3e-005 1.00e+000 3.573491212e+002 3.573486263e+002 9.5e-012 8.81
112 3.8e-006 2.5e-003 1.3e-005 1.00e+000 3.573491112e+002 3.573486248e+002 8.3e-012 8.91
113 3.8e-006 2.5e-003 1.3e-005 1.00e+000 3.573491071e+002 3.573486248e+002 8.3e-012 9.02
114 3.8e-006 2.5e-003 1.3e-005 2.13e+000 3.573490914e+002 3.573486240e+002 8.3e-012 9.11
115 4.2e-006 2.5e-003 1.3e-005 1.25e+000 3.573490874e+002 3.573486239e+002 8.3e-012 9.20
116 4.2e-006 2.5e-003 1.3e-005 1.00e+000 3.573490839e+002 3.573486238e+002 8.3e-012 9.30
117 4.2e-006 2.5e-003 1.4e-005 1.00e+000 3.573491275e+002 3.573486238e+002 8.3e-012 9.45
118 4.1e-006 2.5e-003 1.4e-005 1.03e+000 3.573491278e+002 3.573486239e+002 8.3e-012 9.58
119 3.7e-006 2.3e-003 1.3e-005 1.00e+000 3.573490833e+002 3.573486229e+002 7.5e-012 9.67
120 3.3e-006 2.0e-003 1.1e-005 9.22e-001 3.573490264e+002 3.573486216e+002 6.7e-012 9.78
121 4.3e-006 2.0e-003 5.2e-006 1.00e+000 3.573488071e+002 3.573486215e+002 6.6e-012 9.89
122 5.3e-006 2.0e-003 5.2e-006 2.39e+000 3.573487937e+002 3.573486203e+002 6.6e-012 9.98
123 5.2e-006 2.0e-003 5.5e-006 1.00e+000 3.573488041e+002 3.573486203e+002 6.6e-012 10.06
124 2.5e-005 2.0e-003 1.9e-005 1.00e+000 3.573479822e+002 3.573486203e+002 6.5e-012 10.16
125 2.3e-005 1.8e-003 1.7e-005 1.00e+000 3.573480450e+002 3.573486197e+002 5.9e-012 10.22
126 2.6e-005 1.6e-003 1.6e-005 1.49e+000 3.573480772e+002 3.573486197e+002 5.3e-012 10.28
127 2.6e-005 1.6e-003 1.6e-005 1.00e+000 3.573480604e+002 3.573486197e+002 5.3e-012 10.34
128 2.6e-005 1.6e-003 1.6e-005 1.00e+000 3.573480576e+002 3.573486197e+002 5.3e-012 10.41
129 2.5e-005 1.6e-003 1.5e-005 2.26e-001 3.573481199e+002 3.573486185e+002 5.1e-012 10.48
130 2.3e-005 1.4e-003 1.2e-005 1.00e+000 3.573482146e+002 3.573486181e+002 4.6e-012 10.55
131 2.0e-005 1.3e-003 1.1e-005 8.73e-001 3.573482757e+002 3.573486171e+002 4.1e-012 10.61
132 2.0e-005 1.2e-003 1.1e-005 1.64e+000 3.573482991e+002 3.573486167e+002 4.0e-012 10.70
133 1.8e-005 1.1e-003 9.9e-006 -9.91e-001 3.573483297e+002 3.573486165e+002 3.6e-012 10.78
134 1.6e-005 1.0e-003 8.9e-006 9.75e-001 3.573483701e+002 3.573486160e+002 3.2e-012 10.88
135 1.4e-005 9.1e-004 7.7e-006 1.00e+000 3.573484029e+002 3.573486158e+002 2.9e-012 11.00
136 1.3e-005 8.2e-004 7.0e-006 1.13e+000 3.573484253e+002 3.573486159e+002 2.8e-012 11.11
137 1.3e-005 8.2e-004 7.0e-006 9.01e-001 3.573484249e+002 3.573486159e+002 2.8e-012 11.25
138 1.3e-005 8.2e-004 7.0e-006 9.02e-001 3.573484254e+002 3.573486159e+002 2.8e-012 11.34
139 1.1e-005 7.4e-004 6.3e-006 1.03e+000 3.573484448e+002 3.573486157e+002 2.5e-012 11.44
140 2.4e-006 1.5e-004 2.3e-006 1.00e+000 3.573485515e+002 3.573486147e+002 5.0e-013 11.52
Interior-point optimizer terminated. Time: 11.53.
Optimizer terminated. Time: 11.56
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 3.5734855149e+002 nrm: 9e+001 Viol. con: 4e-005 var: 0e+000
Dual. obj: 3.5734861465e+002 nrm: 8e+002 Viol. con: 0e+000 var: 8e-004
* End solution on dual form. *
Transforming to primal solution.
Solving took 11.6 seconds.
result packing took 3.7% of solve time
solution checking took 1% of solve time
Using solver 'mosek'
Solving for 1899 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6216) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 487
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 0
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.03
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 929
Optimizer - Cones : 0
Optimizer - Scalar variables : 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 : 0.02
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 -1.234758023e+005 2.000000000e+000 1.0e+000 0.08
1 1.5e+003 2.0e+003 8.0e+004 -9.71e-001 -1.224174053e+005 2.927903375e+000 6.5e-001 0.20
2 7.1e+002 9.7e+002 3.8e+004 -9.53e-001 -1.192652434e+005 6.047890044e+000 3.1e-001 0.30
3 2.9e+002 4.0e+002 1.6e+004 -9.01e-001 -1.111484942e+005 2.515365505e+001 1.3e-001 0.42
4 2.9e+002 4.0e+002 1.6e+004 -7.65e-001 -1.092627577e+005 1.672591927e+003 1.3e-001 0.50
5 1.2e+002 1.6e+002 6.4e+003 -7.58e-001 -8.564990880e+004 7.659097644e+003 5.2e-002 0.56
6 3.5e+001 4.8e+001 1.9e+003 -4.31e-001 -4.091383899e+004 1.290801655e+004 1.5e-002 0.63
7 1.5e+001 2.1e+001 8.3e+002 3.29e-001 -2.129513764e+004 6.272280303e+003 6.8e-003 0.72
8 6.9e+000 9.4e+000 3.7e+002 7.04e-001 -1.003202763e+004 3.298427008e+003 3.1e-003 0.78
9 2.8e+000 3.8e+000 1.5e+002 8.93e-001 -3.935718467e+003 1.598481613e+003 1.2e-003 0.86
10 1.2e+000 1.6e+000 6.5e+001 9.75e-001 -1.631236230e+003 7.616880549e+002 5.3e-004 0.92
11 9.1e-001 1.3e+000 5.0e+001 9.87e-001 -1.230600733e+003 6.193602096e+002 4.1e-004 1.00
12 7.2e-001 1.2e+000 3.9e+001 9.70e-001 -9.738066749e+002 5.013872498e+002 3.2e-004 1.06
13 3.7e-001 6.4e-001 2.0e+001 9.91e-001 -4.737212941e+002 2.805130926e+002 1.7e-004 1.13
14 1.2e-001 2.4e-001 6.8e+000 9.98e-001 -1.373856340e+002 1.176223750e+002 5.7e-005 1.19
15 4.1e-002 1.3e-001 2.3e+000 1.00e+000 -2.387412111e+001 6.392425014e+001 2.0e-005 1.27
16 2.5e-002 9.2e-002 1.4e+000 1.00e+000 4.617287457e-002 5.311040678e+001 1.2e-005 1.30
17 1.6e-002 9.0e-002 9.3e-001 1.00e+000 1.225121284e+001 4.734759667e+001 7.9e-006 1.34
18 3.8e-003 1.3e-001 2.2e-001 1.00e+000 3.045537052e+001 3.887117559e+001 1.9e-006 1.45
19 2.1e-003 9.4e-002 1.2e-001 1.00e+000 3.309946169e+001 3.769689880e+001 1.1e-006 1.53
20 7.8e-004 9.4e-002 4.6e-002 1.00e+000 3.505613456e+001 3.679522131e+001 4.0e-007 1.59
21 2.3e-004 1.0e-001 1.4e-002 1.00e+000 3.589054243e+001 3.640903287e+001 1.2e-007 1.69
22 9.2e-005 8.9e-002 5.5e-003 1.00e+000 3.610364550e+001 3.630879643e+001 4.8e-008 1.75
23 8.3e-005 8.0e-002 4.9e-003 1.00e+000 3.611852217e+001 3.630315570e+001 4.3e-008 1.84
24 7.4e-005 7.3e-002 4.4e-003 1.00e+000 3.613100873e+001 3.629717020e+001 3.9e-008 1.92
25 6.7e-005 6.6e-002 4.0e-003 1.00e+000 3.614226785e+001 3.629180637e+001 3.5e-008 2.03
26 6.0e-005 6.1e-002 3.6e-003 1.00e+000 3.615238978e+001 3.628696883e+001 3.1e-008 2.17
27 5.4e-005 5.5e-002 3.2e-003 1.00e+000 3.616149741e+001 3.628261396e+001 2.8e-008 2.34
28 4.9e-005 5.0e-002 2.9e-003 1.00e+000 3.616969172e+001 3.627869286e+001 2.5e-008 2.47
29 4.4e-005 4.6e-002 2.6e-003 1.00e+000 3.617706475e+001 3.627516271e+001 2.3e-008 2.61
30 3.9e-005 4.2e-002 2.4e-003 1.00e+000 3.618369898e+001 3.627198464e+001 2.1e-008 2.70
31 3.6e-005 3.9e-002 2.1e-003 1.00e+000 3.618966858e+001 3.626912364e+001 1.8e-008 2.77
32 3.2e-005 3.6e-002 1.9e-003 1.00e+000 3.619504026e+001 3.626654816e+001 1.7e-008 2.89
33 2.9e-005 3.3e-002 1.7e-003 1.00e+000 3.619987400e+001 3.626422978e+001 1.5e-008 3.03
34 2.6e-005 3.0e-002 1.5e-003 1.00e+000 3.620422376e+001 3.626214289e+001 1.3e-008 3.20
35 2.3e-005 2.8e-002 1.4e-003 1.00e+000 3.620813806e+001 3.626026441e+001 1.2e-008 3.38
36 2.1e-005 2.6e-002 1.3e-003 1.00e+000 3.621166054e+001 3.625857355e+001 1.1e-008 3.50
37 1.9e-005 2.4e-002 1.1e-003 1.00e+000 3.621483045e+001 3.625705160e+001 9.8e-009 3.64
38 1.7e-005 2.2e-002 1.0e-003 1.00e+000 3.621768311e+001 3.625568169e+001 8.8e-009 3.81
39 1.5e-005 2.1e-002 9.1e-004 1.00e+000 3.622025029e+001 3.625444865e+001 8.0e-009 3.95
40 1.4e-005 1.9e-002 8.2e-004 1.00e+000 3.622256056e+001 3.625333880e+001 7.2e-009 4.06
41 1.2e-005 1.8e-002 7.4e-004 1.00e+000 3.622463965e+001 3.625233983e+001 6.4e-009 4.19
42 1.1e-005 1.7e-002 6.7e-004 1.00e+000 3.622651068e+001 3.625144067e+001 5.8e-009 4.36
43 1.0e-005 1.6e-002 6.0e-004 1.00e+000 3.622819449e+001 3.625063133e+001 5.2e-009 4.52
44 9.0e-006 1.5e-002 5.4e-004 1.00e+000 3.622970980e+001 3.624990285e+001 4.7e-009 4.56
45 8.1e-006 1.4e-002 4.9e-004 1.00e+000 3.623107348e+001 3.624924714e+001 4.2e-009 4.67
46 7.3e-006 1.4e-002 4.4e-004 1.00e+000 3.623230069e+001 3.624865692e+001 3.8e-009 4.84
47 6.6e-006 1.3e-002 3.9e-004 1.00e+000 3.623340510e+001 3.624812565e+001 3.4e-009 5.02
48 5.9e-006 1.3e-002 3.5e-004 1.00e+000 3.623439899e+001 3.624764745e+001 3.1e-009 5.09
49 5.3e-006 1.2e-002 3.2e-004 1.00e+000 3.623529341e+001 3.624721700e+001 2.8e-009 5.19
50 4.8e-006 1.2e-002 2.9e-004 1.00e+000 3.623609833e+001 3.624682954e+001 2.5e-009 5.23
51 4.3e-006 1.1e-002 2.6e-004 1.00e+000 3.623682270e+001 3.624648077e+001 2.2e-009 5.30
52 3.9e-006 1.1e-002 2.3e-004 1.00e+000 3.623747458e+001 3.624616683e+001 2.0e-009 5.38
53 3.5e-006 1.0e-002 2.1e-004 1.00e+000 3.623806121e+001 3.624588423e+001 1.8e-009 5.44
54 3.2e-006 1.0e-002 1.9e-004 1.00e+000 3.623858915e+001 3.624562986e+001 1.6e-009 5.48
55 2.8e-006 9.8e-003 1.7e-004 1.00e+000 3.623906424e+001 3.624540089e+001 1.5e-009 5.56
56 2.6e-006 9.6e-003 1.5e-004 1.00e+000 3.623949180e+001 3.624519477e+001 1.3e-009 5.64
57 2.3e-006 9.3e-003 1.4e-004 1.00e+000 3.623987656e+001 3.624500924e+001 1.2e-009 5.67
58 2.1e-006 9.1e-003 1.2e-004 1.00e+000 3.624022282e+001 3.624484224e+001 1.1e-009 5.73
59 1.9e-006 9.0e-003 1.1e-004 1.00e+000 3.624053443e+001 3.624469191e+001 9.7e-010 5.80
60 1.7e-006 8.8e-003 1.0e-004 1.00e+000 3.624081486e+001 3.624455659e+001 8.7e-010 5.86
61 1.5e-006 8.6e-003 9.0e-005 1.00e+000 3.624106722e+001 3.624443478e+001 7.8e-010 5.92
62 1.4e-006 8.5e-003 8.1e-005 1.00e+000 3.624129433e+001 3.624432514e+001 7.1e-010 6.00
63 1.2e-006 8.4e-003 7.3e-005 1.00e+000 3.624149871e+001 3.624422644e+001 6.4e-010 6.11
64 1.1e-006 8.3e-003 6.6e-005 1.00e+000 3.624168264e+001 3.624413760e+001 5.7e-010 6.19
65 9.9e-007 8.2e-003 5.9e-005 1.00e+000 3.624184817e+001 3.624405763e+001 5.1e-010 6.30
66 8.9e-007 8.1e-003 5.3e-005 1.00e+000 3.624199713e+001 3.624398565e+001 4.6e-010 6.36
67 8.0e-007 8.0e-003 4.8e-005 1.00e+000 3.624213118e+001 3.624392086e+001 4.2e-010 6.44
68 7.2e-007 7.9e-003 4.3e-005 1.00e+000 3.624225183e+001 3.624386254e+001 3.8e-010 6.56
69 6.5e-007 7.9e-003 3.9e-005 1.00e+000 3.624236040e+001 3.624381004e+001 3.4e-010 6.69
70 5.8e-007 7.8e-003 3.5e-005 1.00e+000 3.624245810e+001 3.624376278e+001 3.0e-010 6.78
71 5.3e-007 7.7e-003 3.1e-005 1.00e+000 3.624254603e+001 3.624372025e+001 2.7e-010 6.89
72 4.7e-007 7.7e-003 2.8e-005 1.00e+000 3.624262517e+001 3.624368195e+001 2.5e-010 7.02
73 4.3e-007 7.6e-003 2.5e-005 1.00e+000 3.624269638e+001 3.624364749e+001 2.2e-010 7.08
74 3.8e-007 7.6e-003 2.3e-005 1.00e+000 3.624276047e+001 3.624361647e+001 2.0e-010 7.16
75 3.4e-007 7.6e-003 2.1e-005 1.00e+000 3.624281815e+001 3.624358855e+001 1.8e-010 7.25
76 3.1e-007 7.5e-003 1.9e-005 1.00e+000 3.624287006e+001 3.624356342e+001 1.6e-010 7.33
77 2.8e-007 7.5e-003 1.7e-005 1.00e+000 3.624291677e+001 3.624354080e+001 1.5e-010 7.41
78 2.5e-007 7.5e-003 1.5e-005 1.00e+000 3.624295881e+001 3.624352043e+001 1.3e-010 7.47
79 2.3e-007 7.4e-003 1.4e-005 1.00e+000 3.624299664e+001 3.624350211e+001 1.2e-010 7.53
80 2.0e-007 7.4e-003 1.2e-005 1.00e+000 3.624303069e+001 3.624348561e+001 1.1e-010 7.59
81 1.8e-007 7.4e-003 1.1e-005 1.00e+000 3.624306133e+001 3.624347076e+001 9.5e-011 7.67
82 1.6e-007 7.4e-003 9.8e-006 1.00e+000 3.624308891e+001 3.624345740e+001 8.6e-011 7.75
83 1.5e-007 7.3e-003 8.9e-006 1.00e+000 3.624311373e+001 3.624344537e+001 7.7e-011 7.81
84 1.3e-007 7.3e-003 8.0e-006 1.00e+000 3.624313606e+001 3.624343454e+001 7.0e-011 7.91
85 1.2e-007 7.3e-003 7.2e-006 1.00e+000 3.624315616e+001 3.624342479e+001 6.3e-011 8.08
86 1.1e-007 7.3e-003 6.5e-006 1.00e+000 3.624317425e+001 3.624341602e+001 5.6e-011 8.20
87 9.7e-008 7.3e-003 5.8e-006 1.00e+000 3.624319053e+001 3.624340812e+001 5.1e-011 8.30
88 8.8e-008 7.3e-003 5.2e-006 1.00e+000 3.624320518e+001 3.624340102e+001 4.6e-011 8.42
89 7.9e-008 7.3e-003 4.7e-006 1.00e+000 3.624321837e+001 3.624339462e+001 4.1e-011 8.56
90 7.1e-008 7.2e-003 4.2e-006 1.00e+000 3.624323024e+001 3.624338887e+001 3.7e-011 8.72
91 6.4e-008 7.2e-003 3.8e-006 1.00e+000 3.624324091e+001 3.624338368e+001 3.3e-011 8.94
92 5.7e-008 7.2e-003 3.4e-006 9.99e-001 3.624325053e+001 3.624337902e+001 3.0e-011 9.00
93 5.2e-008 7.2e-003 3.1e-006 1.00e+000 3.624325918e+001 3.624337482e+001 2.7e-011 9.16
94 4.7e-008 7.2e-003 2.8e-006 1.00e+000 3.624326696e+001 3.624337104e+001 2.4e-011 9.28
95 4.2e-008 7.2e-003 2.5e-006 9.99e-001 3.624327397e+001 3.624336764e+001 2.2e-011 9.34
96 3.8e-008 7.2e-003 2.3e-006 9.99e-001 3.624328027e+001 3.624336458e+001 2.0e-011 9.45
97 3.4e-008 7.2e-003 2.0e-006 9.98e-001 3.624328594e+001 3.624336183e+001 1.8e-011 9.53
98 3.1e-008 6.5e-003 1.8e-006 1.00e+000 3.624329106e+001 3.624335934e+001 1.6e-011 9.61
99 2.7e-008 5.8e-003 1.6e-006 1.00e+000 3.624329565e+001 3.624335711e+001 1.4e-011 9.67
100 2.5e-008 5.2e-003 1.5e-006 9.97e-001 3.624329979e+001 3.624335511e+001 1.3e-011 9.75
101 2.2e-008 4.7e-003 1.3e-006 1.00e+000 3.624330351e+001 3.624335330e+001 1.2e-011 9.83
102 2.0e-008 4.2e-003 1.2e-006 1.00e+000 3.624330687e+001 3.624335166e+001 1.0e-011 9.94
103 1.8e-008 3.8e-003 1.1e-006 9.98e-001 3.624330988e+001 3.624335020e+001 9.4e-012 10.00
104 1.6e-008 3.4e-003 9.7e-007 1.00e+000 3.624331259e+001 3.624334888e+001 8.5e-012 10.06
105 1.5e-008 3.1e-003 8.7e-007 1.00e+000 3.624331503e+001 3.624334769e+001 7.6e-012 10.14
106 1.3e-008 2.8e-003 7.9e-007 1.00e+000 3.624331723e+001 3.624334662e+001 6.9e-012 10.20
107 1.2e-008 2.5e-003 7.1e-007 1.00e+000 3.624331921e+001 3.624334566e+001 6.2e-012 10.27
108 1.1e-008 2.2e-003 6.4e-007 1.00e+000 3.624332099e+001 3.624334480e+001 5.5e-012 10.36
109 9.6e-009 2.0e-003 5.7e-007 1.00e+000 3.624332259e+001 3.624334402e+001 5.0e-012 10.52
110 8.6e-009 1.8e-003 5.2e-007 9.99e-001 3.624332403e+001 3.624334332e+001 4.5e-012 10.63
111 7.8e-009 1.6e-003 4.6e-007 9.99e-001 3.624332533e+001 3.624334269e+001 4.0e-012 10.72
112 7.0e-009 1.5e-003 4.2e-007 1.00e+000 3.624332650e+001 3.624334212e+001 3.6e-012 10.80
113 6.3e-009 1.3e-003 3.8e-007 1.00e+000 3.624332755e+001 3.624334161e+001 3.3e-012 10.86
114 5.7e-009 1.2e-003 3.4e-007 1.00e+000 3.624332850e+001 3.624334114e+001 2.9e-012 10.92
115 5.1e-009 1.1e-003 3.0e-007 1.00e+000 3.624332935e+001 3.624334073e+001 2.7e-012 11.02
116 4.6e-009 9.7e-004 2.7e-007 9.97e-001 3.624333011e+001 3.624334036e+001 2.4e-012 11.11
117 4.1e-009 8.7e-004 2.5e-007 1.00e+000 3.624333080e+001 3.624334002e+001 2.2e-012 11.20
118 3.7e-009 7.8e-004 2.2e-007 1.00e+000 3.624333142e+001 3.624333972e+001 1.9e-012 11.30
119 3.3e-009 7.1e-004 2.0e-007 1.01e+000 3.624333200e+001 3.624333944e+001 1.7e-012 11.36
120 3.0e-009 6.4e-004 1.8e-007 1.00e+000 3.624333250e+001 3.624333919e+001 1.6e-012 11.45
121 2.7e-009 5.7e-004 1.6e-007 1.01e+000 3.624333297e+001 3.624333896e+001 1.4e-012 11.52
122 2.4e-009 5.1e-004 1.5e-007 9.96e-001 3.624333338e+001 3.624333876e+001 1.3e-012 11.61
123 2.2e-009 4.6e-004 1.3e-007 9.94e-001 3.624333374e+001 3.624333859e+001 1.2e-012 11.69
124 2.0e-009 4.2e-004 1.2e-007 9.88e-001 3.624333407e+001 3.624333843e+001 1.0e-012 11.75
125 1.8e-009 3.8e-004 1.1e-007 1.00e+000 3.624333436e+001 3.624333829e+001 9.4e-013 11.84
Interior-point optimizer terminated. Time: 11.84.
Optimizer terminated. Time: 11.98
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 3.6243334359e+001 nrm: 2e+002 Viol. con: 3e-008 var: 0e+000
Dual. obj: 3.6243338288e+001 nrm: 8e+002 Viol. con: 0e+000 var: 3e-003
* End solution on dual form. *
Transforming to primal solution.
Solving took 12 seconds.
result packing took 3.3% of solve time
solution checking took 0.66% 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 -1.232670644e+005 2.000000000e+000 1.0e+000 0.08
1 1.5e+003 2.1e+003 8.2e+004 -9.71e-001 -1.222858201e+005 2.848186257e+000 6.6e-001 0.16
2 6.9e+002 9.5e+002 3.7e+004 -9.55e-001 -1.189353449e+005 6.007497694e+000 3.0e-001 0.25
3 2.9e+002 3.9e+002 1.6e+004 -8.99e-001 -1.109051987e+005 2.517772565e+001 1.3e-001 0.34
4 2.9e+002 3.9e+002 1.6e+004 -7.64e-001 -1.087669448e+005 1.890325175e+003 1.3e-001 0.41
5 1.1e+002 1.5e+002 6.1e+003 -7.55e-001 -8.412802017e+004 7.782716198e+003 5.0e-002 0.47
6 4.3e+001 5.8e+001 2.3e+003 -4.05e-001 -4.824107653e+004 1.171636734e+004 1.9e-002 0.55
7 2.1e+001 2.8e+001 1.1e+003 2.01e-001 -2.781411785e+004 7.289115114e+003 9.1e-003 0.61
8 8.5e+000 1.2e+001 4.6e+002 5.86e-001 -1.238753117e+004 3.709126972e+003 3.7e-003 0.70
9 3.9e+000 5.3e+000 2.1e+002 8.57e-001 -5.638110372e+003 2.044493757e+003 1.7e-003 0.83
10 2.0e+000 2.8e+000 1.1e+002 9.52e-001 -2.782228554e+003 1.272078043e+003 9.1e-004 0.91
11 9.2e-001 1.2e+000 5.0e+001 9.85e-001 -1.247249193e+003 5.981598659e+002 4.1e-004 0.98
12 8.7e-001 1.3e+000 4.8e+001 9.63e-001 -1.215540552e+003 5.625538246e+002 3.9e-004 1.06
13 4.3e-001 6.3e-001 2.4e+001 9.80e-001 -5.889261162e+002 2.990688022e+002 2.0e-004 1.13
14 1.8e-001 2.7e-001 9.9e+000 1.00e+000 -2.437426785e+002 1.275912664e+002 8.2e-005 1.20
15 8.3e-002 1.5e-001 4.6e+000 1.00e+000 -1.042386276e+002 6.940197650e+001 3.9e-005 1.27
16 3.1e-002 1.0e-001 1.8e+000 1.00e+000 -3.164613284e+001 3.408676512e+001 1.5e-005 1.33
17 1.2e-002 1.0e-001 7.1e-001 1.00e+000 -5.104216658e+000 2.143946798e+001 6.1e-006 1.45
18 1.1e-002 9.1e-002 6.4e-001 1.00e+000 -2.787131628e+000 2.113429564e+001 5.5e-006 1.52
19 6.0e-003 6.7e-002 3.5e-001 1.00e+000 4.843782342e+000 1.776305019e+001 3.0e-006 1.61
20 3.5e-003 5.2e-002 2.0e-001 1.01e+000 8.846699369e+000 1.635873129e+001 1.7e-006 1.70
21 2.7e-003 4.3e-002 1.6e-001 1.02e+000 1.013096383e+001 1.585686396e+001 1.3e-006 1.83
22 2.1e-003 3.7e-002 1.2e-001 1.02e+000 1.111038482e+001 1.551021980e+001 1.0e-006 1.91
23 9.2e-004 4.8e-002 5.4e-002 1.02e+000 1.289739525e+001 1.487656928e+001 4.7e-007 2.00
24 5.1e-004 4.6e-002 3.0e-002 1.02e+000 1.350585938e+001 1.460875867e+001 2.6e-007 2.09
25 3.0e-004 4.5e-002 1.8e-002 1.01e+000 1.383471222e+001 1.447332330e+001 1.5e-007 2.22
26 2.0e-004 4.1e-002 1.2e-002 1.01e+000 1.398079681e+001 1.441222360e+001 1.0e-007 2.31
27 1.8e-004 3.8e-002 1.1e-002 1.01e+000 1.401708151e+001 1.440560504e+001 9.4e-008 2.36
28 1.6e-004 3.5e-002 9.7e-003 1.01e+000 1.404334059e+001 1.439288026e+001 8.4e-008 2.45
29 1.5e-004 3.2e-002 8.7e-003 1.01e+000 1.406782521e+001 1.438233516e+001 7.6e-008 2.61
30 1.3e-004 2.9e-002 7.9e-003 1.01e+000 1.408961817e+001 1.437261171e+001 6.8e-008 2.73
31 1.2e-004 2.7e-002 7.1e-003 1.01e+000 1.410917909e+001 1.436382152e+001 6.2e-008 2.83
32 1.1e-004 2.5e-002 6.4e-003 1.01e+000 1.412672148e+001 1.435585815e+001 5.5e-008 2.89
33 9.6e-005 2.4e-002 5.7e-003 1.00e+000 1.414246051e+001 1.434864989e+001 5.0e-008 3.02
34 8.6e-005 2.2e-002 5.2e-003 1.00e+000 1.415658361e+001 1.434212708e+001 4.5e-008 3.08
35 7.8e-005 2.1e-002 4.6e-003 1.00e+000 1.416925798e+001 1.433622531e+001 4.0e-008 3.22
36 7.0e-005 1.9e-002 4.2e-003 1.00e+000 1.418063313e+001 1.433088610e+001 3.6e-008 3.31
37 6.3e-005 1.8e-002 3.8e-003 1.00e+000 1.419084273e+001 1.432605614e+001 3.3e-008 3.45
38 5.7e-005 1.7e-002 3.4e-003 1.00e+000 1.420000660e+001 1.432168719e+001 2.9e-008 3.53
39 5.1e-005 1.6e-002 3.0e-003 1.00e+000 1.420823226e+001 1.431773560e+001 2.7e-008 3.61
40 4.6e-005 1.5e-002 2.7e-003 1.00e+000 1.421561648e+001 1.431416206e+001 2.4e-008 3.73
41 4.1e-005 1.5e-002 2.5e-003 1.00e+000 1.422224646e+001 1.431093160e+001 2.1e-008 3.83
42 3.7e-005 1.4e-002 2.2e-003 1.00e+000 1.422820065e+001 1.430801254e+001 1.9e-008 3.94
43 3.3e-005 1.3e-002 2.0e-003 1.00e+000 1.423354933e+001 1.430537610e+001 1.7e-008 4.02
44 3.0e-005 1.3e-002 1.8e-003 1.00e+000 1.423835521e+001 1.430299613e+001 1.6e-008 4.05
45 2.7e-005 1.2e-002 1.6e-003 1.00e+000 1.424267411e+001 1.430084863e+001 1.4e-008 4.06
46 2.4e-005 1.2e-002 1.5e-003 1.00e+000 1.424655593e+001 1.429891097e+001 1.3e-008 4.09
47 2.2e-005 1.1e-002 1.3e-003 1.00e+000 1.425004540e+001 1.429716384e+001 1.1e-008 4.13
48 2.0e-005 1.1e-002 1.2e-003 1.00e+000 1.425318243e+001 1.429558770e+001 1.0e-008 4.20
49 1.8e-005 1.1e-002 1.1e-003 1.00e+000 1.425600306e+001 1.429416663e+001 9.3e-009 4.30
50 1.6e-005 1.0e-002 9.6e-004 1.00e+000 1.425853929e+001 1.429288548e+001 8.3e-009 4.38
51 1.4e-005 1.0e-002 8.6e-004 1.00e+000 1.426081991e+001 1.429173075e+001 7.5e-009 4.47
52 1.3e-005 1.0e-002 7.7e-004 1.00e+000 1.426287070e+001 1.429069031e+001 6.7e-009 4.59
53 1.2e-005 9.7e-003 7.0e-004 1.00e+000 1.426471484e+001 1.428975210e+001 6.1e-009 4.67
54 1.0e-005 9.5e-003 6.3e-004 1.00e+000 1.426637319e+001 1.428890659e+001 5.5e-009 4.78
55 9.4e-006 9.4e-003 5.6e-004 1.00e+000 1.426786436e+001 1.428814443e+001 4.9e-009 4.86
56 8.5e-006 9.2e-003 5.1e-004 1.00e+000 1.426920517e+001 1.428745728e+001 4.4e-009 4.95
57 7.7e-006 9.0e-003 4.6e-004 1.00e+000 1.427041079e+001 1.428683735e+001 4.0e-009 5.03
58 6.9e-006 8.9e-003 4.1e-004 1.00e+000 1.427149482e+001 1.428627836e+001 3.6e-009 5.13
59 6.2e-006 8.8e-003 3.7e-004 1.00e+000 1.427246948e+001 1.428577445e+001 3.2e-009 5.22
60 5.6e-006 8.7e-003 3.3e-004 1.00e+000 1.427334578e+001 1.428532067e+001 2.9e-009 5.33
61 5.0e-006 8.6e-003 3.0e-004 1.00e+000 1.427413380e+001 1.428491141e+001 2.6e-009 5.42
62 4.5e-006 8.5e-003 2.7e-004 1.00e+000 1.427484261e+001 1.428454221e+001 2.4e-009 5.52
63 4.1e-006 8.4e-003 2.4e-004 1.00e+000 1.427548013e+001 1.428420977e+001 2.1e-009 5.63
64 3.7e-006 8.3e-003 2.2e-004 1.00e+000 1.427605365e+001 1.428391016e+001 1.9e-009 5.72
65 3.3e-006 8.2e-003 2.0e-004 9.99e-001 1.427656951e+001 1.428364080e+001 1.7e-009 5.80
66 3.0e-006 8.2e-003 1.8e-004 1.00e+000 1.427703364e+001 1.428339802e+001 1.5e-009 5.91
67 2.7e-006 8.1e-003 1.6e-004 9.98e-001 1.427745114e+001 1.428317986e+001 1.4e-009 6.02
68 2.4e-006 8.1e-003 1.4e-004 9.99e-001 1.427782687e+001 1.428298305e+001 1.3e-009 6.11
69 2.2e-006 8.0e-003 1.3e-004 1.00e+000 1.427816503e+001 1.428280541e+001 1.1e-009 6.22
70 1.9e-006 8.0e-003 1.2e-004 9.99e-001 1.427846926e+001 1.428264581e+001 1.0e-009 6.28
71 1.8e-006 7.9e-003 1.0e-004 9.97e-001 1.427874295e+001 1.428250236e+001 9.1e-010 6.36
72 1.6e-006 7.9e-003 9.4e-005 1.00e+000 1.427898937e+001 1.428237247e+001 8.2e-010 6.45
73 1.4e-006 7.9e-003 8.5e-005 1.00e+000 1.427921107e+001 1.428225585e+001 7.4e-010 6.53
74 1.3e-006 7.8e-003 7.6e-005 1.00e+000 1.427941054e+001 1.428215091e+001 6.7e-010 6.63
75 1.1e-006 7.0e-003 6.9e-005 1.01e+000 1.427959235e+001 1.428205467e+001 6.0e-010 6.72
76 1.0e-006 6.3e-003 6.2e-005 1.00e+000 1.427975395e+001 1.428196938e+001 5.4e-010 6.78
77 9.3e-007 5.7e-003 5.6e-005 1.00e+000 1.427990060e+001 1.428189182e+001 4.9e-010 6.84
78 8.4e-007 5.1e-003 5.0e-005 1.00e+000 1.428003108e+001 1.428182301e+001 4.4e-010 6.92
79 7.5e-007 4.6e-003 4.5e-005 9.99e-001 1.428014844e+001 1.428176126e+001 3.9e-010 7.00
80 6.8e-007 4.2e-003 4.1e-005 9.91e-001 1.428025394e+001 1.428170619e+001 3.5e-010 7.08
81 6.1e-007 3.7e-003 3.6e-005 1.00e+000 1.428034932e+001 1.428165573e+001 3.2e-010 7.14
82 5.5e-007 3.4e-003 3.3e-005 9.97e-001 1.428043481e+001 1.428161078e+001 2.9e-010 7.25
83 4.9e-007 3.0e-003 3.0e-005 1.00e+000 1.428051176e+001 1.428157013e+001 2.6e-010 7.31
84 4.4e-007 2.7e-003 2.7e-005 1.01e+000 1.428058262e+001 1.428153247e+001 2.3e-010 7.41
85 4.0e-007 2.5e-003 2.4e-005 9.99e-001 1.428064478e+001 1.428149968e+001 2.1e-010 7.47
86 3.6e-007 2.2e-003 2.2e-005 9.96e-001 1.428070069e+001 1.428147025e+001 1.9e-010 7.56
87 3.2e-007 2.0e-003 1.9e-005 9.84e-001 1.428075094e+001 1.428144408e+001 1.7e-010 7.64
88 2.9e-007 1.8e-003 1.7e-005 1.02e+000 1.428080091e+001 1.428141698e+001 1.5e-010 7.75
89 2.6e-007 1.6e-003 1.6e-005 1.00e+000 1.428084134e+001 1.428139559e+001 1.4e-010 7.86
90 2.4e-007 1.5e-003 1.4e-005 1.01e+000 1.428087836e+001 1.428137591e+001 1.3e-010 7.94
91 2.1e-007 1.3e-003 1.3e-005 9.82e-001 1.428091085e+001 1.428135906e+001 1.1e-010 8.02
92 1.9e-007 1.2e-003 1.1e-005 9.93e-001 1.428094012e+001 1.428134368e+001 1.0e-010 8.11
93 1.7e-007 1.1e-003 1.0e-005 9.76e-001 1.428096642e+001 1.428133006e+001 9.2e-011 8.19
94 1.6e-007 9.5e-004 9.3e-006 9.93e-001 1.428099014e+001 1.428131756e+001 8.2e-011 8.27
95 1.4e-007 8.6e-004 8.3e-006 1.04e+000 1.428101505e+001 1.428130386e+001 7.6e-011 8.34
96 1.3e-007 7.7e-004 7.5e-006 1.00e+000 1.428103397e+001 1.428129383e+001 6.8e-011 8.42
97 1.1e-007 6.9e-004 6.8e-006 9.93e-001 1.428105093e+001 1.428128493e+001 6.1e-011 8.50
98 1.0e-007 6.2e-004 6.1e-006 1.01e+000 1.428106648e+001 1.428127664e+001 5.5e-011 8.56
99 9.2e-008 5.6e-004 5.5e-006 1.02e+000 1.428108145e+001 1.428126855e+001 5.0e-011 8.64
100 8.3e-008 5.1e-004 4.9e-006 9.72e-001 1.428109364e+001 1.428126228e+001 4.5e-011 8.73
101 7.4e-008 4.6e-004 4.4e-006 1.02e+000 1.428110570e+001 1.428125574e+001 4.1e-011 8.80
102 6.7e-008 4.1e-004 4.0e-006 1.00e+000 1.428111564e+001 1.428125048e+001 3.7e-011 8.88
103 6.0e-008 3.7e-004 3.6e-006 1.02e+000 1.428112527e+001 1.428124526e+001 3.4e-011 8.94
104 5.4e-008 3.3e-004 3.2e-006 1.01e+000 1.428113343e+001 1.428124090e+001 3.0e-011 9.02
105 4.9e-008 3.0e-004 2.9e-006 1.08e+000 1.428114288e+001 1.428123558e+001 2.8e-011 9.08
106 4.4e-008 2.7e-004 2.6e-006 1.05e+000 1.428115032e+001 1.428123154e+001 2.6e-011 9.14
107 4.0e-008 2.4e-004 2.4e-006 1.05e+000 1.428115689e+001 1.428122799e+001 2.4e-011 9.22
108 3.6e-008 2.2e-004 2.1e-006 9.87e-001 1.428116157e+001 1.428122561e+001 2.2e-011 9.30
109 3.2e-008 2.0e-004 1.9e-006 1.01e+000 1.428116590e+001 1.428122334e+001 2.0e-011 9.38
110 2.9e-008 1.8e-004 1.7e-006 9.89e-001 1.428116968e+001 1.428122140e+001 1.8e-011 9.45
111 2.6e-008 1.6e-004 1.5e-006 9.91e-001 1.428117309e+001 1.428121966e+001 1.6e-011 9.52
112 2.3e-008 1.4e-004 1.4e-006 9.80e-001 1.428117615e+001 1.428121810e+001 1.4e-011 9.59
113 2.1e-008 1.3e-004 1.3e-006 9.90e-001 1.428117891e+001 1.428121669e+001 1.3e-011 9.67
114 1.9e-008 1.2e-004 1.1e-006 9.77e-001 1.428118139e+001 1.428121543e+001 1.2e-011 9.75
115 1.7e-008 1.0e-004 1.0e-006 9.92e-001 1.428118362e+001 1.428121427e+001 1.0e-011 9.78
116 1.5e-008 9.4e-005 9.1e-007 9.94e-001 1.428118564e+001 1.428121323e+001 9.4e-012 9.88
117 1.4e-008 8.4e-005 8.2e-007 9.65e-001 1.428118744e+001 1.428121232e+001 8.4e-012 9.97
118 1.2e-008 7.6e-005 7.4e-007 1.01e+000 1.428118917e+001 1.428121139e+001 7.6e-012 10.03
119 1.1e-008 6.8e-005 6.7e-007 1.04e+000 1.428119089e+001 1.428121044e+001 7.0e-012 10.13
120 1.0e-008 6.1e-005 6.0e-007 9.70e-001 1.428119217e+001 1.428120979e+001 6.3e-012 10.19
121 9.1e-009 5.5e-005 5.4e-007 9.53e-001 1.428119333e+001 1.428120922e+001 5.7e-012 10.27
122 8.2e-009 5.0e-005 4.9e-007 1.07e+000 1.428119466e+001 1.428120846e+001 5.3e-012 10.34
123 7.4e-009 4.5e-005 4.4e-007 1.07e+000 1.428119585e+001 1.428120778e+001 4.9e-012 10.44
124 6.7e-009 4.0e-005 3.9e-007 1.00e+000 1.428119666e+001 1.428120737e+001 4.5e-012 10.55
125 6.0e-009 3.6e-005 3.5e-007 1.03e+000 1.428119746e+001 1.428120694e+001 4.1e-012 10.63
126 5.4e-009 3.3e-005 3.2e-007 1.01e+000 1.428119810e+001 1.428120661e+001 3.7e-012 10.70
127 4.9e-009 2.9e-005 2.9e-007 1.04e+000 1.428119875e+001 1.428120627e+001 3.4e-012 10.80
Interior-point optimizer terminated. Time: 10.80.
Optimizer terminated. Time: 10.83
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.4281198753e+001 nrm: 3e+002 Viol. con: 5e-008 var: 0e+000
Dual. obj: 1.4281206267e+001 nrm: 8e+002 Viol. con: 0e+000 var: 2e-004
* End solution on dual form. *
Transforming to primal solution.
Solving took 10.9 seconds.
result packing took 3.4% of solve time
solution checking took 0.75% of solve time
Using solver 'mosek'
Solving for 1899 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 487
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 0
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.03
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 929
Optimizer - Cones : 0
Optimizer - Scalar variables : 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 : 0.01
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 -1.230870217e+005 2.000000000e+000 1.0e+000 0.08
1 1.5e+003 2.1e+003 8.3e+004 -9.71e-001 -1.221538014e+005 2.806586478e+000 6.8e-001 0.28
2 6.6e+002 9.0e+002 3.6e+004 -9.55e-001 -1.184794477e+005 6.186226075e+000 2.9e-001 0.44
3 2.9e+002 3.9e+002 1.5e+004 -8.94e-001 -1.107344883e+005 2.621500905e+001 1.3e-001 0.59
4 2.9e+002 3.9e+002 1.5e+004 -7.64e-001 -1.083962617e+005 2.074597370e+003 1.3e-001 0.73
5 1.1e+002 1.5e+002 5.8e+003 -7.55e-001 -8.287674751e+004 8.042344038e+003 4.8e-002 0.91
6 4.5e+001 6.1e+001 2.4e+003 -3.85e-001 -5.005629520e+004 1.130991128e+004 2.0e-002 1.05
7 2.7e+001 3.7e+001 1.5e+003 1.78e-001 -3.514349845e+004 8.030783305e+003 1.2e-002 1.20
8 1.3e+001 1.8e+001 7.0e+002 4.63e-001 -1.861167287e+004 4.839081555e+003 5.7e-003 1.41
9 5.1e+000 7.0e+000 2.8e+002 7.51e-001 -7.579768903e+003 2.417910248e+003 2.3e-003 1.58
10 3.4e+000 4.6e+000 1.8e+002 9.25e-001 -4.941386389e+003 1.772009624e+003 1.5e-003 1.69
11 1.1e+000 1.5e+000 5.9e+001 9.59e-001 -1.561877897e+003 6.117824150e+002 4.9e-004 1.80
12 9.0e-001 1.4e+000 4.9e+001 9.84e-001 -1.271501861e+003 5.442376145e+002 4.1e-004 1.84
13 6.6e-001 1.1e+000 3.6e+001 9.71e-001 -9.475427919e+002 4.128834765e+002 3.0e-004 1.92
14 3.5e-001 6.0e-001 1.9e+001 9.99e-001 -4.736821973e+002 2.355162554e+002 1.6e-004 1.98
15 1.3e-001 2.5e-001 7.2e+000 9.95e-001 -1.763299653e+002 9.338471217e+001 6.0e-005 2.05
16 7.7e-002 1.6e-001 4.3e+000 1.01e+000 -1.015200502e+002 5.938776890e+001 3.6e-005 2.11
17 2.7e-002 1.1e-001 1.5e+000 1.01e+000 -3.124855916e+001 2.620140869e+001 1.3e-005 2.19
18 1.5e-002 8.9e-002 8.6e-001 1.01e+000 -1.373920800e+001 1.819286167e+001 7.3e-006 2.23
19 1.3e-002 6.5e-002 7.2e-001 1.03e+000 -8.265715798e+000 1.811676895e+001 6.1e-006 2.30
20 4.7e-003 6.7e-002 2.7e-001 1.01e+000 3.848402572e+000 1.381996676e+001 2.3e-006 2.36
21 2.5e-003 5.9e-002 1.5e-001 1.02e+000 7.423545710e+000 1.269348151e+001 1.3e-006 2.42
22 7.7e-004 7.6e-002 4.8e-002 9.90e-001 1.011996228e+001 1.189306866e+001 4.4e-007 2.47
23 2.4e-004 8.6e-002 1.6e-002 9.76e-001 1.100801825e+001 1.159931515e+001 1.5e-007 2.53
24 9.3e-005 7.8e-002 6.4e-003 9.85e-001 1.127687175e+001 1.151304632e+001 6.0e-008 2.59
25 4.6e-005 6.7e-002 3.1e-003 9.93e-001 1.136984030e+001 1.148631628e+001 3.0e-008 2.66
26 4.1e-005 6.1e-002 2.8e-003 9.97e-001 1.138016421e+001 1.148501810e+001 2.7e-008 2.72
27 3.7e-005 5.6e-002 2.5e-003 9.97e-001 1.138810692e+001 1.148249743e+001 2.4e-008 2.78
28 3.3e-005 5.1e-002 2.3e-003 9.97e-001 1.139548584e+001 1.148046033e+001 2.2e-008 2.83
29 3.0e-005 4.6e-002 2.1e-003 9.97e-001 1.140209769e+001 1.147859218e+001 2.0e-008 2.95
30 2.7e-005 4.3e-002 1.8e-003 9.98e-001 1.140803616e+001 1.147689593e+001 1.8e-008 3.05
31 2.4e-005 3.9e-002 1.7e-003 9.98e-001 1.141336834e+001 1.147535396e+001 1.6e-008 3.17
32 2.2e-005 3.6e-002 1.5e-003 9.98e-001 1.141815725e+001 1.147395384e+001 1.4e-008 3.28
33 2.0e-005 3.3e-002 1.3e-003 9.98e-001 1.142245872e+001 1.147268393e+001 1.3e-008 3.41
34 1.8e-005 3.0e-002 1.2e-003 9.99e-001 1.142632252e+001 1.147153175e+001 1.2e-008 3.55
35 1.6e-005 2.8e-002 1.1e-003 9.99e-001 1.142979382e+001 1.147048744e+001 1.0e-008 3.67
36 1.4e-005 2.6e-002 9.8e-004 9.99e-001 1.143291272e+001 1.146954179e+001 9.4e-009 3.78
37 1.3e-005 2.4e-002 8.8e-004 9.99e-001 1.143571508e+001 1.146868498e+001 8.5e-009 3.91
38 1.2e-005 2.3e-002 8.0e-004 9.99e-001 1.143823341e+001 1.146790911e+001 7.6e-009 4.03
39 1.0e-005 2.1e-002 7.2e-004 9.99e-001 1.144049667e+001 1.146720712e+001 6.9e-009 4.16
40 9.4e-006 2.0e-002 6.4e-004 9.99e-001 1.144253073e+001 1.146657199e+001 6.2e-009 4.27
41 8.4e-006 1.8e-002 5.8e-004 1.00e+000 1.144435890e+001 1.146599746e+001 5.6e-009 4.36
42 7.6e-006 1.7e-002 5.2e-004 9.99e-001 1.144600207e+001 1.146547853e+001 5.0e-009 4.42
43 6.8e-006 1.6e-002 4.7e-004 9.99e-001 1.144747893e+001 1.146500918e+001 4.5e-009 4.47
44 6.2e-006 1.5e-002 4.2e-004 1.00e+000 1.144880648e+001 1.146458465e+001 4.1e-009 4.53
45 5.5e-006 1.5e-002 3.8e-004 1.00e+000 1.144999990e+001 1.146420090e+001 3.6e-009 4.59
46 5.0e-006 1.4e-002 3.4e-004 9.99e-001 1.145107273e+001 1.146385448e+001 3.3e-009 4.66
47 4.5e-006 1.3e-002 3.1e-004 1.00e+000 1.145203723e+001 1.146354130e+001 3.0e-009 4.72
48 4.0e-006 1.3e-002 2.8e-004 9.99e-001 1.145290441e+001 1.146325875e+001 2.7e-009 4.81
49 3.6e-006 1.2e-002 2.5e-004 1.00e+000 1.145368427e+001 1.146300309e+001 2.4e-009 4.92
50 3.3e-006 1.2e-002 2.2e-004 9.99e-001 1.145438554e+001 1.146277296e+001 2.2e-009 5.02
51 2.9e-006 1.1e-002 2.0e-004 1.00e+000 1.145501629e+001 1.146256500e+001 1.9e-009 5.13
52 2.7e-006 1.1e-002 1.8e-004 1.00e+000 1.145558360e+001 1.146237767e+001 1.7e-009 5.23
53 2.4e-006 1.0e-002 1.6e-004 1.00e+000 1.145609392e+001 1.146220863e+001 1.6e-009 5.34
54 2.1e-006 1.0e-002 1.5e-004 1.00e+000 1.145655300e+001 1.146205633e+001 1.4e-009 5.44
55 1.9e-006 9.9e-003 1.3e-004 9.99e-001 1.145696593e+001 1.146191934e+001 1.3e-009 5.55
56 1.7e-006 9.6e-003 1.2e-004 9.99e-001 1.145733746e+001 1.146179578e+001 1.1e-009 5.66
57 1.6e-006 9.4e-003 1.1e-004 1.00e+000 1.145767178e+001 1.146168428e+001 1.0e-009 5.77
58 1.4e-006 9.2e-003 9.7e-005 9.98e-001 1.145797252e+001 1.146158411e+001 9.3e-010 5.88
59 1.3e-006 9.0e-003 8.7e-005 1.00e+000 1.145824321e+001 1.146149352e+001 8.3e-010 6.00
60 1.1e-006 8.8e-003 7.8e-005 9.99e-001 1.145848672e+001 1.146141219e+001 7.5e-010 6.11
61 1.0e-006 8.7e-003 7.1e-005 9.98e-001 1.145870582e+001 1.146133902e+001 6.8e-010 6.23
62 9.2e-007 8.5e-003 6.4e-005 1.00e+000 1.145890304e+001 1.146127292e+001 6.1e-010 6.36
63 8.3e-007 8.4e-003 5.7e-005 9.98e-001 1.145908046e+001 1.146121357e+001 5.5e-010 6.47
64 7.5e-007 8.3e-003 5.1e-005 1.00e+000 1.145924021e+001 1.146115983e+001 4.9e-010 6.58
65 6.7e-007 8.2e-003 4.6e-005 1.00e+000 1.145938485e+001 1.146111102e+001 4.4e-010 6.64
66 6.1e-007 8.1e-003 4.2e-005 1.00e+000 1.145951410e+001 1.146106763e+001 4.0e-010 6.80
67 5.5e-007 8.0e-003 3.8e-005 9.94e-001 1.145963031e+001 1.146102895e+001 3.6e-010 7.02
68 4.9e-007 7.9e-003 3.4e-005 9.93e-001 1.145973490e+001 1.146099409e+001 3.2e-010 7.20
69 4.4e-007 7.8e-003 3.0e-005 9.97e-001 1.145982907e+001 1.146096253e+001 2.9e-010 7.33
70 4.0e-007 7.1e-003 2.7e-005 1.03e+000 1.145992276e+001 1.146092984e+001 2.7e-010 7.41
71 3.6e-007 7.0e-003 2.5e-005 9.91e-001 1.145999809e+001 1.146090487e+001 2.4e-010 7.48
72 1.2e-007 2.4e-003 8.5e-006 9.97e-001 1.146044385e+001 1.146075600e+001 8.2e-011 7.56
73 1.1e-007 2.2e-003 7.6e-006 9.65e-001 1.146046724e+001 1.146074835e+001 7.4e-011 7.61
74 1.0e-007 2.0e-003 6.9e-006 1.07e+000 1.146049455e+001 1.146073781e+001 6.9e-011 7.69
75 9.1e-008 1.8e-003 6.2e-006 9.36e-001 1.146051276e+001 1.146073174e+001 6.2e-011 7.80
76 8.3e-008 1.6e-003 5.6e-006 1.06e+000 1.146053358e+001 1.146072400e+001 5.7e-011 7.89
77 7.5e-008 1.4e-003 5.0e-006 1.04e+000 1.146055054e+001 1.146071817e+001 5.3e-011 8.02
78 6.9e-008 1.3e-003 4.5e-006 1.14e+000 1.146057155e+001 1.146070917e+001 5.1e-011 8.14
79 8.8e-008 2.1e-005 7.5e-008 7.85e-001 1.146068299e+001 1.146068559e+001 6.0e-012 8.28
Interior-point optimizer terminated. Time: 8.30.
Optimizer terminated. Time: 8.34
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1460682990e+001 nrm: 1e+002 Viol. con: 2e-006 var: 0e+000
Dual. obj: 1.1460685595e+001 nrm: 8e+002 Viol. con: 0e+000 var: 1e-004
* End solution on dual form. *
Transforming to primal solution.
Solving took 8.38 seconds.
result packing took 3.8% of solve time
solution checking took 0.97% of solve time
Using solver 'mosek'
Solving for 1899 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6216) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (6268) of matrix 'A'.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 487
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 0
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.03
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 4
Optimizer - solved problem : the primal
Optimizer - Constraints : 929
Optimizer - Cones : 0
Optimizer - Scalar variables : 3607 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.06 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.03
Factor - nonzeros before factor : 1.53e+004 after factor : 1.76e+005
Factor - dense dim. : 0 flops : 3.97e+007
Factor - GP saved nzs : 3.48e+004 GP saved flops : 1.07e+006
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+003 3.1e+003 1.2e+005 0.00e+000 -1.230224292e+005 2.000000000e+000 1.0e+000 0.09
1 1.6e+003 2.1e+003 8.4e+004 -9.71e-001 -1.221078166e+005 2.791148786e+000 6.8e-001 0.17
2 7.0e+002 9.6e+002 3.8e+004 -9.56e-001 -1.187969215e+005 5.799367419e+000 3.1e-001 0.23
3 2.9e+002 3.9e+002 1.5e+004 -9.01e-001 -1.107028852e+005 2.527989772e+001 1.3e-001 0.30
4 2.9e+002 3.9e+002 1.5e+004 -7.65e-001 -1.083499972e+005 2.088225652e+003 1.3e-001 0.34
5 1.4e+002 1.8e+002 7.3e+003 -7.56e-001 -9.013700576e+004 6.370703958e+003 6.0e-002 0.41
6 4.3e+001 5.8e+001 2.3e+003 -4.97e-001 -4.846908479e+004 1.174265748e+004 1.9e-002 0.47
7 2.3e+001 3.2e+001 1.3e+003 2.03e-001 -3.104759305e+004 7.485946994e+003 1.0e-002 0.53
8 1.1e+001 1.5e+001 5.8e+002 5.40e-001 -1.573225440e+004 4.181970028e+003 4.8e-003 0.59
9 4.7e+000 6.4e+000 2.5e+002 8.04e-001 -6.938462690e+003 2.240878115e+003 2.1e-003 0.64
10 2.2e+000 3.0e+000 1.2e+002 9.34e-001 -3.068812959e+003 1.209364934e+003 9.7e-004 0.70
11 1.4e+000 1.9e+000 7.7e+001 9.84e-001 -1.999479250e+003 8.254867562e+002 6.4e-004 0.75
12 9.4e-001 1.3e+000 5.1e+001 9.86e-001 -1.316974476e+003 5.684373484e+002 4.2e-004 0.81
13 7.8e-001 1.2e+000 4.3e+001 9.64e-001 -1.116562816e+003 4.784309519e+002 3.5e-004 0.86
14 3.1e-001 4.9e-001 1.7e+001 9.90e-001 -4.317304021e+002 2.063996289e+002 1.4e-004 0.92
15 1.5e-001 2.5e-001 8.5e+000 1.00e+000 -2.108389250e+002 1.081513365e+002 7.1e-005 0.98
16 4.8e-002 1.5e-001 2.7e+000 1.00e+000 -6.192813914e+001 3.891007657e+001 2.3e-005 1.03
17 3.9e-002 1.3e-001 2.2e+000 1.00e+000 -4.879644528e+001 3.332884759e+001 1.9e-005 1.09
18 2.1e-002 9.0e-002 1.2e+000 1.00e+000 -2.297336025e+001 2.142844084e+001 1.0e-005 1.14
19 1.5e-002 7.0e-002 8.6e-001 1.02e+000 -1.327809251e+001 1.845257847e+001 7.3e-006 1.20
20 7.7e-003 4.8e-002 4.4e-001 1.03e+000 -6.659184240e-001 1.527623979e+001 3.7e-006 1.26
21 2.6e-003 7.3e-002 1.5e-001 1.02e+000 7.285064453e+000 1.268755322e+001 1.3e-006 1.31
22 1.5e-003 5.4e-002 8.9e-002 9.94e-001 8.864113786e+000 1.209403295e+001 7.8e-007 1.36
23 4.9e-004 7.4e-002 3.1e-002 9.81e-001 1.049749404e+001 1.162669250e+001 2.8e-007 1.44
24 1.8e-004 7.3e-002 1.2e-002 9.83e-001 1.101837117e+001 1.145790191e+001 1.1e-007 1.48
25 8.3e-005 6.8e-002 5.5e-003 9.94e-001 1.119788557e+001 1.140059758e+001 5.1e-008 1.55
26 3.9e-005 6.5e-002 2.6e-003 9.98e-001 1.127980749e+001 1.137561208e+001 2.4e-008 1.59
27 3.5e-005 5.9e-002 2.3e-003 9.99e-001 1.128921002e+001 1.137546132e+001 2.2e-008 1.66
28 3.2e-005 5.4e-002 2.1e-003 1.00e+000 1.129561425e+001 1.137324636e+001 2.0e-008 1.70
29 2.8e-005 4.9e-002 1.9e-003 1.00e+000 1.130147318e+001 1.137135020e+001 1.8e-008 1.76
30 2.6e-005 4.5e-002 1.7e-003 1.00e+000 1.130671681e+001 1.136961242e+001 1.6e-008 1.81
31 2.3e-005 4.1e-002 1.5e-003 1.00e+000 1.131142251e+001 1.136803383e+001 1.4e-008 1.86
32 2.1e-005 3.8e-002 1.4e-003 1.00e+000 1.131564549e+001 1.136660004e+001 1.3e-008 1.92
33 1.9e-005 3.5e-002 1.2e-003 1.00e+000 1.131943641e+001 1.136529909e+001 1.2e-008 1.97
34 1.7e-005 3.2e-002 1.1e-003 1.00e+000 1.132284025e+001 1.136411974e+001 1.1e-008 2.03
35 1.5e-005 3.0e-002 1.0e-003 1.00e+000 1.132589712e+001 1.136305109e+001 9.5e-009 2.08
36 1.4e-005 2.7e-002 9.1e-004 1.00e+000 1.132864302e+001 1.136208360e+001 8.5e-009 2.16
37 1.2e-005 2.5e-002 8.1e-004 1.00e+000 1.133111001e+001 1.136120816e+001 7.7e-009 2.20
38 1.1e-005 2.4e-002 7.3e-004 1.00e+000 1.133332679e+001 1.136041658e+001 6.9e-009 2.28
39 9.9e-006 2.2e-002 6.6e-004 1.00e+000 1.133531902e+001 1.135970095e+001 6.2e-009 2.34
40 8.9e-006 2.1e-002 5.9e-004 1.00e+000 1.133710971e+001 1.135905437e+001 5.6e-009 2.42
41 8.0e-006 1.9e-002 5.3e-004 1.00e+000 1.133871942e+001 1.135847048e+001 5.0e-009 2.48
42 7.2e-006 1.8e-002 4.8e-004 1.00e+000 1.134016655e+001 1.135794317e+001 4.5e-009 2.55
43 6.5e-006 1.7e-002 4.3e-004 1.00e+000 1.134146763e+001 1.135746715e+001 4.1e-009 2.59
44 5.9e-006 1.6e-002 3.9e-004 1.00e+000 1.134263746e+001 1.135703758e+001 3.7e-009 2.66
45 5.3e-006 1.5e-002 3.5e-004 1.00e+000 1.134368933e+001 1.135664990e+001 3.3e-009 2.70
46 4.7e-006 1.4e-002 3.2e-004 1.00e+000 1.134463519e+001 1.135630003e+001 3.0e-009 2.77
47 4.3e-006 1.4e-002 2.8e-004 1.00e+000 1.134548578e+001 1.135598437e+001 2.7e-009 2.81
48 3.8e-006 1.3e-002 2.6e-004 1.00e+000 1.134625074e+001 1.135569968e+001 2.4e-009 2.88
49 3.5e-006 1.3e-002 2.3e-004 1.00e+000 1.134693875e+001 1.135544297e+001 2.2e-009 2.94
50 3.1e-006 1.2e-002 2.1e-004 1.00e+000 1.134755762e+001 1.135521155e+001 1.9e-009 2.98
51 2.8e-006 1.2e-002 1.9e-004 1.00e+000 1.134811433e+001 1.135500306e+001 1.8e-009 3.03
52 2.5e-006 1.1e-002 1.7e-004 1.00e+000 1.134861518e+001 1.135481520e+001 1.6e-009 3.09
53 2.3e-006 1.1e-002 1.5e-004 1.00e+000 1.134906582e+001 1.135464599e+001 1.4e-009 3.17
54 2.0e-006 1.0e-002 1.4e-004 1.00e+000 1.134947132e+001 1.135449352e+001 1.3e-009 3.23
55 1.8e-006 1.0e-002 1.2e-004 1.00e+000 1.134983619e+001 1.135435632e+001 1.2e-009 3.30
56 1.7e-006 9.8e-003 1.1e-004 1.00e+000 1.135016456e+001 1.135423269e+001 1.0e-009 3.33
57 1.5e-006 9.6e-003 9.9e-005 1.00e+000 1.135046006e+001 1.135412146e+001 9.3e-010 3.38
58 1.3e-006 9.4e-003 8.9e-005 1.00e+000 1.135072603e+001 1.135402123e+001 8.4e-010 3.44
59 1.2e-006 9.2e-003 8.0e-005 1.00e+000 1.135096539e+001 1.135393105e+001 7.5e-010 3.48
60 1.1e-006 9.0e-003 7.2e-005 1.00e+000 1.135118080e+001 1.135384995e+001 6.8e-010 3.56
61 9.8e-007 8.8e-003 6.5e-005 1.00e+000 1.135137470e+001 1.135377686e+001 6.1e-010 3.61
62 8.8e-007 8.7e-003 5.9e-005 1.00e+000 1.135154922e+001 1.135371108e+001 5.5e-010 3.67
63 7.9e-007 8.5e-003 5.3e-005 9.99e-001 1.135170625e+001 1.135365205e+001 5.0e-010 3.72
64 7.1e-007 8.4e-003 4.7e-005 1.00e+000 1.135184762e+001 1.135359881e+001 4.5e-010 3.78
65 6.4e-007 8.3e-003 4.3e-005 1.00e+000 1.135197485e+001 1.135355093e+001 4.0e-010 3.83
66 5.8e-007 8.2e-003 3.8e-005 9.99e-001 1.135208935e+001 1.135350791e+001 3.6e-010 3.89
67 5.2e-007 8.1e-003 3.5e-005 1.00e+000 1.135219244e+001 1.135346904e+001 3.2e-010 3.95
68 4.7e-007 8.0e-003 3.1e-005 1.00e+000 1.135228523e+001 1.135343404e+001 2.9e-010 4.01
69 4.2e-007 8.0e-003 2.8e-005 1.00e+000 1.135236872e+001 1.135340265e+001 2.6e-010 4.06
70 3.8e-007 7.9e-003 2.5e-005 1.00e+000 1.135244388e+001 1.135337435e+001 2.4e-010 4.13
71 3.4e-007 7.8e-003 2.3e-005 9.98e-001 1.135251148e+001 1.135334901e+001 2.1e-010 4.17
72 3.1e-007 7.8e-003 2.0e-005 1.00e+000 1.135257235e+001 1.135332612e+001 1.9e-010 4.22
73 2.8e-007 7.7e-003 1.8e-005 9.97e-001 1.135262711e+001 1.135330560e+001 1.7e-010 4.25
74 2.5e-007 7.7e-003 1.7e-005 9.97e-001 1.135267640e+001 1.135328713e+001 1.6e-010 4.31
75 2.2e-007 7.6e-003 1.5e-005 9.96e-001 1.135272075e+001 1.135327053e+001 1.4e-010 4.41
76 2.0e-007 7.6e-003 1.3e-005 9.97e-001 1.135276067e+001 1.135325555e+001 1.3e-010 4.48
77 1.8e-007 7.5e-003 1.2e-005 9.99e-001 1.135279661e+001 1.135324205e+001 1.1e-010 4.53
78 1.6e-007 7.5e-003 1.1e-005 9.97e-001 1.135282895e+001 1.135322991e+001 1.0e-010 4.61
79 1.5e-007 6.8e-003 9.8e-006 1.00e+000 1.135285843e+001 1.135321874e+001 9.2e-011 4.70
80 1.3e-007 6.1e-003 8.8e-006 1.00e+000 1.135288460e+001 1.135320888e+001 8.3e-011 4.80
81 1.2e-007 5.5e-003 7.9e-006 1.00e+000 1.135290815e+001 1.135320000e+001 7.4e-011 4.88
82 1.1e-007 4.9e-003 7.1e-006 9.97e-001 1.135292934e+001 1.135319205e+001 6.7e-011 4.97
83 9.6e-008 4.4e-003 6.4e-006 1.00e+000 1.135294842e+001 1.135318485e+001 6.0e-011 5.03
84 8.7e-008 4.0e-003 5.8e-006 1.00e+000 1.135296559e+001 1.135317836e+001 5.4e-011 5.11
85 7.8e-008 3.6e-003 5.2e-006 9.95e-001 1.135298103e+001 1.135317257e+001 4.9e-011 5.14
86 7.0e-008 3.2e-003 4.7e-006 1.00e+000 1.135299516e+001 1.135316721e+001 4.4e-011 5.16
87 6.3e-008 2.9e-003 4.2e-006 9.90e-001 1.135300763e+001 1.135316256e+001 4.0e-011 5.17
88 5.7e-008 2.6e-003 3.8e-006 1.01e+000 1.135301949e+001 1.135315801e+001 3.6e-011 5.19
89 5.1e-008 2.4e-003 3.4e-006 9.86e-001 1.135302953e+001 1.135315429e+001 3.2e-011 5.20
90 4.6e-008 2.1e-003 3.1e-006 9.94e-001 1.135303857e+001 1.135315089e+001 2.9e-011 5.23
91 4.1e-008 1.9e-003 2.8e-006 9.86e-001 1.135304671e+001 1.135314787e+001 2.6e-011 5.25
92 3.7e-008 1.7e-003 2.5e-006 1.01e+000 1.135305434e+001 1.135314494e+001 2.4e-011 5.26
93 3.4e-008 1.5e-003 2.2e-006 1.01e+000 1.135306104e+001 1.135314239e+001 2.1e-011 5.28
94 3.0e-008 1.4e-003 2.0e-006 9.72e-001 1.135306692e+001 1.135314024e+001 1.9e-011 5.30
95 2.7e-008 1.3e-003 1.8e-006 1.02e+000 1.135307275e+001 1.135313796e+001 1.7e-011 5.31
96 2.5e-008 1.1e-003 1.6e-006 1.00e+000 1.135307749e+001 1.135313613e+001 1.6e-011 5.34
97 2.3e-008 1.0e-003 1.5e-006 1.01e+000 1.135308182e+001 1.135313450e+001 1.4e-011 5.36
98 2.0e-008 9.1e-004 1.3e-006 9.62e-001 1.135308562e+001 1.135313313e+001 1.3e-011 5.39
99 1.8e-008 8.2e-004 1.2e-006 1.02e+000 1.135308932e+001 1.135313169e+001 1.2e-011 5.41
100 1.2e-007 7.4e-004 1.1e-006 1.10e+000 1.135309242e+001 1.135313605e+001 1.1e-011 5.44
101 9.9e-008 6.7e-004 9.6e-007 1.25e+000 1.135309805e+001 1.135312972e+001 1.1e-011 5.45
102 3.4e-007 6.0e-004 8.7e-007 1.00e+000 1.135310036e+001 1.135312823e+001 9.7e-012 5.47
103 4.3e-007 5.1e-004 7.4e-007 8.13e-001 1.135310162e+001 1.135313806e+001 7.6e-012 5.48
104 7.7e-007 4.9e-004 3.4e-007 1.00e+000 1.135315420e+001 1.135313742e+001 7.3e-012 5.51
105 7.2e-007 4.4e-004 3.0e-007 1.03e+000 1.135313754e+001 1.135312618e+001 5.7e-012 5.53
106 6.2e-007 4.2e-004 2.9e-007 9.99e-001 1.135313665e+001 1.135312589e+001 5.4e-012 5.55
107 6.4e-008 4.4e-005 4.7e-008 1.00e+000 1.135312240e+001 1.135312064e+001 5.7e-013 5.56
Interior-point optimizer terminated. Time: 5.58.
Optimizer terminated. Time: 5.61
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1353122399e+001 nrm: 4e+001 Viol. con: 1e-006 var: 0e+000
Dual. obj: 1.1353120642e+001 nrm: 8e+002 Viol. con: 0e+000 var: 3e-004
* End solution on dual form. *
Transforming to primal solution.
Solving took 5.65 seconds.
result packing took 5.3% 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 '' (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: 0.05
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 : 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 -1.230179634e+005 2.000000000e+000 1.0e+000 0.11
1 1.6e+003 2.1e+003 8.3e+004 -9.71e-001 -1.221016117e+005 2.791953667e+000 6.8e-001 0.14
2 7.0e+002 9.5e+002 3.8e+004 -9.56e-001 -1.187479369e+005 5.837290614e+000 3.1e-001 0.19
3 3.0e+002 4.1e+002 1.6e+004 -9.00e-001 -1.112044149e+005 2.381657397e+001 1.3e-001 0.23
4 2.8e+002 3.9e+002 1.5e+004 -7.77e-001 -1.081858590e+005 2.157237135e+003 1.3e-001 0.28
5 1.5e+002 2.0e+002 8.1e+003 -7.54e-001 -9.322897604e+004 5.698955404e+003 6.7e-002 0.33
6 4.4e+001 6.0e+001 2.4e+003 -5.43e-001 -4.915264671e+004 1.209704720e+004 1.9e-002 0.36
7 2.2e+001 3.0e+001 1.2e+003 1.87e-001 -2.906839376e+004 7.820419846e+003 9.7e-003 0.39
8 1.1e+001 1.4e+001 5.7e+002 5.74e-001 -1.535984808e+004 4.305634588e+003 4.7e-003 0.44
9 3.8e+000 5.2e+000 2.1e+002 8.12e-001 -5.612396307e+003 1.869520856e+003 1.7e-003 0.45
10 1.9e+000 2.6e+000 1.0e+002 9.53e-001 -2.568902864e+003 1.171233642e+003 8.4e-004 0.48
11 9.5e-001 1.3e+000 5.2e+001 9.87e-001 -1.314221492e+003 5.991056242e+002 4.3e-004 0.50
12 8.9e-001 1.3e+000 4.9e+001 9.67e-001 -1.260257016e+003 5.567557798e+002 4.0e-004 0.52
13 4.9e-001 7.2e-001 2.7e+001 9.82e-001 -6.871056510e+002 3.108597607e+002 2.2e-004 0.53
14 1.9e-001 4.4e-001 1.0e+001 9.97e-001 -2.647721195e+002 1.242373026e+002 8.7e-005 0.56
15 8.5e-002 2.2e-001 4.7e+000 1.01e+000 -1.131668827e+002 6.318259713e+001 4.0e-005 0.58
16 3.8e-002 1.2e-001 2.2e+000 1.00e+000 -4.796108636e+001 3.234756785e+001 1.8e-005 0.61
17 2.8e-002 9.5e-002 1.6e+000 9.96e-001 -3.315236455e+001 2.641123955e+001 1.4e-005 0.64
18 1.9e-002 7.2e-002 1.1e+000 1.01e+000 -1.923192231e+001 2.084692200e+001 9.2e-006 0.66
19 1.7e-002 6.6e-002 9.9e-001 1.02e+000 -1.639828297e+001 2.011795655e+001 8.4e-006 0.67
20 6.8e-003 6.5e-002 3.9e-001 1.02e+000 5.234496685e-001 1.467235610e+001 3.3e-006 0.69
21 2.1e-003 8.3e-002 1.3e-001 1.02e+000 7.902174947e+000 1.250285656e+001 1.1e-006 0.72
22 1.4e-003 6.0e-002 8.4e-002 9.70e-001 8.972595911e+000 1.205266856e+001 7.5e-007 0.73
23 5.0e-004 6.8e-002 3.1e-002 9.59e-001 1.043477303e+001 1.160960472e+001 2.9e-007 0.75
24 2.2e-004 5.7e-002 1.4e-002 9.59e-001 1.089913913e+001 1.144639598e+001 1.3e-007 0.77
25 2.0e-004 5.2e-002 1.3e-002 9.75e-001 1.093985147e+001 1.143220106e+001 1.2e-007 0.80
26 1.8e-004 4.7e-002 1.2e-002 9.73e-001 1.097704650e+001 1.142073947e+001 1.1e-007 0.81
27 1.6e-004 4.3e-002 1.1e-002 9.75e-001 1.101340492e+001 1.141333209e+001 9.8e-008 0.83
28 1.5e-004 4.0e-002 9.5e-003 9.77e-001 1.104626708e+001 1.140672398e+001 8.8e-008 0.84
29 1.3e-004 3.6e-002 8.6e-003 9.79e-001 1.107585808e+001 1.140070751e+001 7.9e-008 0.91
30 1.2e-004 3.3e-002 7.7e-003 9.81e-001 1.110243546e+001 1.139516419e+001 7.1e-008 0.94
31 1.1e-004 3.1e-002 6.9e-003 9.82e-001 1.112629719e+001 1.139005550e+001 6.4e-008 0.98
32 9.7e-005 2.8e-002 6.2e-003 9.84e-001 1.114771342e+001 1.138534661e+001 5.8e-008 1.02
33 8.7e-005 2.6e-002 5.6e-003 9.85e-001 1.116693036e+001 1.138100784e+001 5.2e-008 1.03
34 7.8e-005 2.4e-002 5.1e-003 9.87e-001 1.118417010e+001 1.137701150e+001 4.7e-008 1.05
35 7.1e-005 2.3e-002 4.6e-003 9.88e-001 1.119963377e+001 1.137333288e+001 4.2e-008 1.08
36 6.4e-005 2.1e-002 4.1e-003 9.89e-001 1.121350286e+001 1.136994908e+001 3.8e-008 1.09
37 5.7e-005 2.0e-002 3.7e-003 9.90e-001 1.122594120e+001 1.136683912e+001 3.4e-008 1.11
38 5.1e-005 1.9e-002 3.3e-003 9.91e-001 1.123709662e+001 1.136398413e+001 3.1e-008 1.13
39 4.6e-005 1.7e-002 3.0e-003 9.92e-001 1.124710143e+001 1.136136540e+001 2.8e-008 1.14
40 4.2e-005 1.6e-002 2.7e-003 9.93e-001 1.125607478e+001 1.135896586e+001 2.5e-008 1.17
41 3.8e-005 1.5e-002 2.4e-003 9.93e-001 1.126412342e+001 1.135676933e+001 2.2e-008 1.19
42 3.4e-005 1.5e-002 2.2e-003 9.94e-001 1.127134285e+001 1.135476012e+001 2.0e-008 1.20
43 3.0e-005 1.4e-002 2.0e-003 9.95e-001 1.127781905e+001 1.135292403e+001 1.8e-008 1.22
44 2.7e-005 1.3e-002 1.8e-003 9.95e-001 1.128362918e+001 1.135124781e+001 1.6e-008 1.24
45 2.5e-005 1.3e-002 1.6e-003 9.96e-001 1.128884254e+001 1.134971912e+001 1.5e-008 1.27
46 2.2e-005 1.2e-002 1.4e-003 9.96e-001 1.129352133e+001 1.134832637e+001 1.3e-008 1.28
47 2.0e-005 1.2e-002 1.3e-003 9.97e-001 1.129772122e+001 1.134705887e+001 1.2e-008 1.30
48 1.8e-005 1.1e-002 1.2e-003 9.97e-001 1.130149195e+001 1.134590655e+001 1.1e-008 1.31
49 1.6e-005 1.1e-002 1.0e-003 9.97e-001 1.130487789e+001 1.134485986e+001 9.7e-009 1.33
50 1.5e-005 1.1e-002 9.4e-004 9.98e-001 1.130791879e+001 1.134390966e+001 8.7e-009 1.36
51 1.3e-005 1.0e-002 8.5e-004 9.98e-001 1.131065036e+001 1.134304804e+001 7.8e-009 1.38
52 1.2e-005 9.9e-003 7.6e-004 9.98e-001 1.131310432e+001 1.134226703e+001 7.1e-009 1.39
53 1.1e-005 9.6e-003 6.8e-004 9.98e-001 1.131530926e+001 1.134155948e+001 6.4e-009 1.45
54 9.5e-006 9.4e-003 6.2e-004 9.98e-001 1.131729072e+001 1.134091906e+001 5.7e-009 1.49
55 8.6e-006 9.2e-003 5.5e-004 9.99e-001 1.131907150e+001 1.134033953e+001 5.2e-009 1.50
56 7.7e-006 9.0e-003 5.0e-004 9.99e-001 1.132067209e+001 1.133981548e+001 4.6e-009 1.53
57 6.9e-006 8.8e-003 4.5e-004 9.99e-001 1.132211080e+001 1.133934168e+001 4.2e-009 1.55
58 6.3e-006 8.7e-003 4.0e-004 9.99e-001 1.132340412e+001 1.133891323e+001 3.8e-009 1.58
59 5.6e-006 8.5e-003 3.6e-004 9.99e-001 1.132456680e+001 1.133852615e+001 3.4e-009 1.59
60 5.1e-006 8.4e-003 3.3e-004 9.99e-001 1.132561205e+001 1.133817640e+001 3.0e-009 1.63
61 4.6e-006 8.3e-003 2.9e-004 9.99e-001 1.132655179e+001 1.133786051e+001 2.7e-009 1.64
62 4.1e-006 8.2e-003 2.7e-004 1.00e+000 1.132739673e+001 1.133757513e+001 2.5e-009 1.66
63 3.7e-006 8.1e-003 2.4e-004 9.99e-001 1.132815648e+001 1.133731756e+001 2.2e-009 1.67
64 3.3e-006 8.0e-003 2.2e-004 1.00e+000 1.132883970e+001 1.133708499e+001 2.0e-009 1.69
65 3.0e-006 7.9e-003 1.9e-004 1.00e+000 1.132945415e+001 1.133687522e+001 1.8e-009 1.70
66 2.7e-006 7.8e-003 1.7e-004 1.00e+000 1.133000681e+001 1.133668606e+001 1.6e-009 1.74
67 2.4e-006 7.8e-003 1.6e-004 1.00e+000 1.133050394e+001 1.133651546e+001 1.5e-009 1.75
68 2.2e-006 7.7e-003 1.4e-004 1.00e+000 1.133095117e+001 1.133636169e+001 1.3e-009 1.77
69 2.0e-006 7.7e-003 1.3e-004 1.00e+000 1.133135353e+001 1.133622310e+001 1.2e-009 1.78
70 1.8e-006 7.6e-003 1.1e-004 9.99e-001 1.133171551e+001 1.133609837e+001 1.1e-009 1.80
71 1.6e-006 7.6e-003 1.0e-004 1.00e+000 1.133204125e+001 1.133598579e+001 9.6e-010 1.83
72 1.4e-006 7.5e-003 9.3e-005 1.00e+000 1.133233433e+001 1.133588450e+001 8.6e-010 1.84
73 1.3e-006 7.5e-003 8.3e-005 1.00e+000 1.133259807e+001 1.133579322e+001 7.7e-010 1.86
74 1.2e-006 7.4e-003 7.5e-005 1.00e+000 1.133283540e+001 1.133571102e+001 7.0e-010 1.92
75 1.0e-006 7.4e-003 6.7e-005 1.00e+000 1.133304894e+001 1.133563707e+001 6.3e-010 1.97
76 9.4e-007 7.4e-003 6.1e-005 1.00e+000 1.133324112e+001 1.133557046e+001 5.6e-010 1.99
77 8.4e-007 7.4e-003 5.5e-005 1.00e+000 1.133341409e+001 1.133551037e+001 5.1e-010 2.00
78 7.6e-007 7.3e-003 4.9e-005 1.00e+000 1.133356973e+001 1.133545636e+001 4.6e-010 2.03
79 6.8e-007 7.3e-003 4.4e-005 9.99e-001 1.133370976e+001 1.133540784e+001 4.1e-010 2.05
80 6.2e-007 7.3e-003 4.0e-005 1.00e+000 1.133383581e+001 1.133536405e+001 3.7e-010 2.06
81 5.5e-007 7.3e-003 3.6e-005 1.00e+000 1.133394927e+001 1.133532455e+001 3.3e-010 2.09
82 5.0e-007 7.2e-003 3.2e-005 9.99e-001 1.133405133e+001 1.133528915e+001 3.0e-010 2.11
83 4.5e-007 7.2e-003 2.9e-005 1.00e+000 1.133414319e+001 1.133525724e+001 2.7e-010 2.13
84 4.0e-007 7.2e-003 2.6e-005 1.00e+000 1.133422586e+001 1.133522851e+001 2.4e-010 2.14
85 3.6e-007 7.2e-003 2.4e-005 1.00e+000 1.133430027e+001 1.133520258e+001 2.2e-010 2.16
86 3.3e-007 7.2e-003 2.1e-005 1.00e+000 1.133436722e+001 1.133517931e+001 2.0e-010 2.19
87 2.9e-007 7.2e-003 1.9e-005 1.00e+000 1.133442746e+001 1.133515838e+001 1.8e-010 2.22
88 2.7e-007 7.1e-003 1.7e-005 9.99e-001 1.133448168e+001 1.133513953e+001 1.6e-010 2.23
89 2.4e-007 7.1e-003 1.5e-005 9.97e-001 1.133453046e+001 1.133512262e+001 1.4e-010 2.25
90 2.1e-007 7.1e-003 1.4e-005 9.99e-001 1.133457437e+001 1.133510734e+001 1.3e-010 2.27
91 1.9e-007 7.1e-003 1.3e-005 1.00e+000 1.133461389e+001 1.133509357e+001 1.2e-010 2.31
92 1.7e-007 7.1e-003 1.1e-005 1.00e+000 1.133464946e+001 1.133508116e+001 1.0e-010 2.34
93 1.6e-007 7.1e-003 1.0e-005 9.96e-001 1.133468145e+001 1.133507007e+001 9.4e-011 2.38
94 1.4e-007 7.1e-003 9.1e-006 9.99e-001 1.133471025e+001 1.133506004e+001 8.5e-011 2.39
95 1.3e-007 6.4e-003 8.2e-006 1.00e+000 1.133473636e+001 1.133505089e+001 7.6e-011 2.41
96 1.1e-007 5.7e-003 7.4e-006 9.96e-001 1.133475966e+001 1.133504280e+001 6.9e-011 2.42
97 1.0e-007 5.1e-003 6.6e-006 1.01e+000 1.133478118e+001 1.133503520e+001 6.2e-011 2.44
98 9.2e-008 4.6e-003 6.0e-006 1.00e+000 1.133480004e+001 1.133502860e+001 5.6e-011 2.47
99 8.3e-008 4.2e-003 5.4e-006 1.00e+000 1.133481698e+001 1.133502269e+001 5.0e-011 2.50
100 7.5e-008 3.8e-003 4.8e-006 9.89e-001 1.133483221e+001 1.133501744e+001 4.5e-011 2.53
101 6.7e-008 3.4e-003 4.4e-006 1.00e+000 1.133484608e+001 1.133501256e+001 4.1e-011 2.55
102 6.1e-008 3.0e-003 3.9e-006 1.01e+000 1.133485872e+001 1.133500810e+001 3.7e-011 2.58
103 5.5e-008 2.7e-003 3.5e-006 9.94e-001 1.133486978e+001 1.133500426e+001 3.3e-011 2.59
104 4.9e-008 2.5e-003 3.2e-006 1.00e+000 1.133487986e+001 1.133500071e+001 3.0e-011 2.63
105 4.4e-008 2.2e-003 2.9e-006 1.01e+000 1.133488920e+001 1.133499741e+001 2.7e-011 2.64
106 4.0e-008 2.0e-003 2.6e-006 1.03e+000 1.133489817e+001 1.133499417e+001 2.5e-011 2.66
107 3.6e-008 1.8e-003 2.3e-006 1.00e+000 1.133490541e+001 1.133499163e+001 2.2e-011 2.69
108 3.2e-008 1.6e-003 2.1e-006 9.96e-001 1.133491181e+001 1.133498941e+001 2.0e-011 2.70
109 2.9e-008 1.5e-003 1.9e-006 1.01e+000 1.133491790e+001 1.133498726e+001 1.8e-011 2.72
110 2.9e-008 1.3e-003 1.7e-006 9.95e-001 1.133492329e+001 1.133498455e+001 1.6e-011 2.77
111 9.4e-009 2.5e-004 3.2e-007 9.78e-001 1.133496067e+001 1.133497245e+001 3.2e-012 2.83
112 2.6e-009 1.8e-005 2.3e-008 9.91e-001 1.133496873e+001 1.133496957e+001 2.3e-013 2.84
Interior-point optimizer terminated. Time: 2.86.
Optimizer terminated. Time: 2.88
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1334968728e+001 nrm: 3e+001 Viol. con: 3e-008 var: 0e+000
Dual. obj: 1.1334969574e+001 nrm: 8e+002 Viol. con: 0e+000 var: 1e-004
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.9 seconds.
result packing took 80% of solve time
solution checking took 2.5% of solve time
Solving took 6 GP solves and 64.2 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 2418944.75949 force_pound * meter but the right hand side evaluated to 2375459.08054 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 32774.4047186 force_pound but the right hand side evaluated to 32399.9999973 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 2.21510116784 meter but the right hand side evaluated to 2.08157340855 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 1243571.69331 joule / kilogram but the right hand side evaluated to 1.56099920823 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 664753.494572 joule / kilogram but the right hand side evaluated to 0.667330233396 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 18.3998967983 meter but the right hand side evaluated to 16.3229270075 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 10.903613865068582 but the right hand side evaluated to 4.788858089614199 (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 10.019749379361047 but the right hand side evaluated to 4.788858077539498 (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 8.144916199000138 but the right hand side evaluated to 4.788858092548781 (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 18.3622635884 meter but the right hand side evaluated to 18.1377459918 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 18.3622635884 meter but the right hand side evaluated to 18.2420849739 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 0.2960380315481004 but the right hand side evaluated to 0.18973948649583408 (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 0.23302323137158787 but the right hand side evaluated to 0.17434727559879898 (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 7.5632397785103604 but the right hand side evaluated to 4.730637385942778 (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 7.5830763680686095 but the right hand side evaluated to 4.757850794353063 (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 77.808s
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-pqtlf6
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-fvislo\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-tbmcqv
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-airryp\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-wiy6oi\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'
Beginning signomial solve.
Solving took 10 GP solves and 8.74 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 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 1372748.9970 but bound is 600000.0000
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 79493.7398 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.11826036768 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825742619 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%)
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 1.63010984803 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010573086 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%)
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985253825 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983804204 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Beginning signomial solve.
Solving took 10 GP solves and 8.14 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 1.0537 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 1372749.3895 but bound is 600000.0000
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 79493.7398 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.11826036886 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825742738 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%)
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 1.63010984805 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010573088 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%)
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985253833 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983804213 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.55 seconds.
Allowing negative dual variable(s) as small as -1.008925446035673e-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 1.2985 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 720429.8060 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.76 seconds.
Allowing negative dual variable(s) as small as -9.552288988147781e-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 1.2521 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 791679.4842 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 6.19 seconds.
Allowing negative dual variable(s) as small as -8.884418412573821e-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 1.1920 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 883741.3415 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 2.23 seconds.
Allowing negative dual variable(s) as small as -4.392636105017619e-12.
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 1.1637 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 933393.0279 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 5.1 seconds.
Allowing negative dual variable(s) as small as -4.946568278625319e-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 1.2985 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 720429.8187 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 6.62 seconds.
Allowing negative dual variable(s) as small as -1.8896985478909342e-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 1.2521 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 791679.4740 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 6.75 seconds.
Allowing negative dual variable(s) as small as -2.2410135290443622e-10.
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 1.1920 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 883741.7435 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 2.24 seconds.
Allowing negative dual variable(s) as small as -4.586650412859091e-12.
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 1.1637 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 933393.0284 but bound is 600000.0000
Beginning signomial solve.
Solving took 10 GP solves and 11.6 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 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 1372749.6395 but bound is 600000.0000
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 79493.7397 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.11826036384 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825742232 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%)
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 1.63010984371 meter ** 2 / second ** 2 but the right hand side evaluated to 1.6301057265 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%)
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.911985251452 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983801814 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Beginning signomial solve.
Solving took 10 GP solves and 8.22 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 1.0537 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 1372945.2797 but bound is 600000.0000
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 79493.7395 but bound is 50000.0000
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 2.1182607519 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781039 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%)
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 1.63010986176 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010574456 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00025%)
Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(2,)**...] is not tight because the left hand side evaluated to 0.91198526179 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983812157 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Using solver 'mosek'
Solving for 702 variables.
Solving took 0.517 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 1.2555 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 773120.5089 but bound is 600000.0000
Beginning signomial solve.
Solving took 9 GP solves and 7.05 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 1.0784 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 1002038.3574 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 76735.5640 but bound is 50000.0000
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 1.39813215739 meter ** 2 / second ** 2 but the right hand side evaluated to 1.39812954599 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00019%)
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 0.803919025969 meter ** 2 / second ** 2 but the right hand side evaluated to 0.803918044533 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%)
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]'
Using solver 'mosek_cli'
Solving for 702 variables.
Solving took 0.544 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 1.2555 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 773120.3442 but bound is 600000.0000
Beginning signomial solve.
Solving took 9 GP solves and 8.23 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 1.0784 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 1002041.5231 but bound is 600000.0000
Warning: Constraint [dQ_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,) [N... >= B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,)*G_M...] is not tight because the left hand side evaluated to 0.0359295931977 meter * newton but the right hand side evaluated to 0.0359295529168 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 76735.5213 but bound is 50000.0000
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/BladeElement
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 [12.497s]: 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 [13.562s]: 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\gpkitPerf_...] is not tight because the left hand side evaluated to 1.39813162962 meter ** 2 / second ** 2 but the right hand side evaluated to 1.39812837496 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00023%)
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 640.862s
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-7lvamn
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-1ks48x\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-1bcqhs\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 0.049 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.08 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.022 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.025 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.02 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 2.77 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 100.006556014 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 985.544331496 meter * revolutions_per_minute but the right hand side evaluated to 103.041406096 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 0.420585713834 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420572933188 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 0.314644953235 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629814033 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 0.168936400431 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931565825 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 0.0639642247721 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631246433 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 0.0226356523748 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226353994103 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)
Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.119 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.124 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.147 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 4.85 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 100.006542977 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0065%)
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 985.544016771 meter * revolutions_per_minute but the right hand side evaluated to 103.041408907 meter / second (Allowable error: 0.0001%, Actual error: 0.16%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585442562 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420572949095 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 0.314645011495 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314630000283 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 0.168936455229 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931641708 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0028%)
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 0.0639643035678 meter ** 2 / second ** 2 but the right hand side evaluated to 0.063963228667 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 0.0226356680048 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354066477 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0012%)
Using solver 'mosek'
Solving for 13 variables.
Solving took 0.035 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 1.78 seconds.
Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619897.8921 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.085 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 3.11 seconds.
Warning: Constraint [dQ_BladeElementProp/BladeElementPerf_(3,) [N*m]... >= B_BladeElementProp/BladeElementPerf_(3,)*G_BladeElementProp/BladeElementPerf_(3,)*Wa_BladeElementPro...] is not tight because the left hand side evaluated to 42.7884411703 meter * newton but the right hand side evaluated to 42.7884844846 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0001%)
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 3.18328269931 meter ** 2 / second ** 2 but the right hand side evaluated to 3.18327922145 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%)
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...
----------------------------------------------------------------------
..........
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Ran 10 tests in 21.508s
OK
Generating XML reports...
Cloning into 'eVTOL'...
adding test for 'aircraft_models.py'
Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 2.260s
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
![[Jenkins]](/csi/static/a404d988/images/svgs/logo.svg){kind=logo}
