Skipping 40 KB..
Full LogRequirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
Running setup.py bdist_wheel for gpfit: started
Running setup.py bdist_wheel for gpfit: finished with status 'done'
Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-3hfm99\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
adding test for 'model/jho.py'
adding test for 'model/print_perf.py'
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.057065877167588e-14.
Allowing negative dual variable(s) as small as -7.563394355258879e-14.
Allowing negative dual variable(s) as small as -1.5110048628974582e-13.
Allowing negative dual variable(s) as small as -1.5022141516829457e-13.
Solving took 4 GP solves and 9.21 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.236219444149093e-14.
Allowing negative dual variable(s) as small as -7.451331218710777e-14.
Allowing negative dual variable(s) as small as -1.50637748802529e-13.
Allowing negative dual variable(s) as small as -1.4962293556908257e-13.
Solving took 4 GP solves and 5.2 seconds.
Allowing negative dual variable(s) as small as -5.173327044527554e-13.
Allowing negative dual variable(s) as small as -1.430536245017322e-12.
Allowing negative dual variable(s) as small as -4.449357549063393e-13.
Allowing negative dual variable(s) as small as -4.449895313340946e-13.
Allowing negative dual variable(s) as small as -1.298180530087678e-12.
Allowing negative dual variable(s) as small as -1.0910113958095824e-12.
Allowing negative dual variable(s) as small as -1.0914000822884184e-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
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 -2.54065856462483e-14.
Allowing negative dual variable(s) as small as -5.696073675709152e-12.
Allowing negative dual variable(s) as small as -2.0878964510413173e-11.
Allowing negative dual variable(s) as small as -2.0880853369321595e-11.
Solving took 4 GP solves and 3.75 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 6.93 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.169788208636561e-13.
Allowing negative dual variable(s) as small as -1.4299880723989133e-12.
Allowing negative dual variable(s) as small as -4.44208905769905e-13.
Allowing negative dual variable(s) as small as -4.4462697412761543e-13.
Allowing negative dual variable(s) as small as -1.2970511166846e-12.
Allowing negative dual variable(s) as small as -1.0914550513385635e-12.
Allowing negative dual variable(s) as small as -1.0914336925557655e-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
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 -2.5046884740746408e-14.
Allowing negative dual variable(s) as small as -5.696090650937629e-12.
Allowing negative dual variable(s) as small as -2.0878972809059655e-11.
Allowing negative dual variable(s) as small as -2.0880856852215195e-11.
Solving took 4 GP solves and 6.92 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 4.02 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Running tests...
----------------------------------------------------------------------
....
----------------------------------------------------------------------
Ran 4 tests in 117.162s
OK
Generating XML reports...
Cloning into 'turbofan'...
Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\turbofan
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\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-zmu3ur\wheels\e5\cb\a8\3b11c975e79b3f632de8c1b88ce438a834a6b07b3850d6b107
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 24184.7528315 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 26232.8485055 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%)
Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 3.890s
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-pps_jr
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\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-7kzvmy\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. *
Computer
Platform : Windows/64-X86
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1015
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1025
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1025
Lin. dep. - tries : 1 time : 0.01
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 : 6
Optimizer - solved problem : the primal
Optimizer - Constraints : 826
Optimizer - Cones : 0
Optimizer - Scalar variables : 3575 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 : 1.67e+004 after factor : 1.69e+005
Factor - dense dim. : 0 flops : 0.00e+000
Factor - GP saved nzs : 0 GP saved flops : 0.00e+000
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.290114216e+005 2.000000000e+000 1.0e+000 0.11
1 1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.268199332e+005 3.700570996e+000 4.8e-001 0.14
2 3.9e+002 5.0e+002 2.2e+004 -9.36e-001 -1.196731173e+005 1.153832762e+001 1.7e-001 0.17
3 2.8e+002 3.7e+002 1.6e+004 -8.23e-001 -1.157725499e+005 8.911193657e+001 1.2e-001 0.19
4 2.8e+002 3.6e+002 1.6e+004 -7.55e-001 -1.127836302e+005 2.530618096e+003 1.2e-001 0.20
5 6.9e+001 9.0e+001 3.9e+003 -7.46e-001 -7.044561375e+004 1.168298555e+004 3.1e-002 0.23
6 3.1e+001 4.1e+001 1.8e+003 -1.39e-001 -4.096532654e+004 1.098732371e+004 1.4e-002 0.25
7 1.6e+001 2.1e+001 9.1e+002 3.72e-001 -2.384884033e+004 6.701248905e+003 7.2e-003 0.27
8 7.3e+000 9.5e+000 4.1e+002 6.70e-001 -1.130515668e+004 3.761163374e+003 3.3e-003 0.30
9 3.4e+000 4.4e+000 1.9e+002 8.75e-001 -5.068498667e+003 2.154890886e+003 1.5e-003 0.31
10 1.7e+000 2.2e+000 9.8e+001 9.56e-001 -2.274239213e+003 1.449630149e+003 7.8e-004 0.33
11 6.5e-001 8.4e-001 3.7e+001 9.85e-001 -6.386409604e+002 7.708877882e+002 2.9e-004 0.34
12 5.5e-001 7.6e-001 3.2e+001 9.80e-001 -4.977186201e+002 7.157125316e+002 2.5e-004 0.37
13 3.9e-001 9.4e-001 2.2e+001 9.74e-001 -2.511527669e+002 6.146396419e+002 1.8e-004 0.39
14 2.1e-001 6.0e-001 1.2e+001 9.86e-001 2.118551310e+001 4.971611734e+002 9.8e-005 0.41
15 6.4e-002 2.4e-001 3.8e+000 1.00e+000 2.547904550e+002 4.008091633e+002 3.1e-005 0.42
16 2.0e-002 1.4e-001 1.2e+000 1.00e+000 3.243515273e+002 3.710547149e+002 9.9e-006 0.45
17 4.6e-003 1.5e-001 2.8e-001 1.00e+000 3.496092054e+002 3.605442939e+002 2.4e-006 0.47
18 2.7e-003 1.2e-001 1.7e-001 1.00e+000 3.526527396e+002 3.591730387e+002 1.4e-006 0.48
19 6.5e-004 1.3e-001 4.1e-002 9.94e-001 3.562031755e+002 3.577903302e+002 3.5e-007 0.52
20 2.4e-004 9.9e-002 1.5e-002 9.98e-001 3.569203948e+002 3.575142357e+002 1.3e-007 0.53
21 1.2e-004 7.9e-002 7.5e-003 1.00e+000 3.571413806e+002 3.574309326e+002 6.3e-008 0.55
22 1.1e-004 7.2e-002 6.8e-003 1.00e+000 3.571621285e+002 3.574227098e+002 5.7e-008 0.56
23 9.5e-005 6.6e-002 6.1e-003 1.00e+000 3.571807621e+002 3.574152867e+002 5.1e-008 0.59
24 8.6e-005 6.0e-002 5.5e-003 1.00e+000 3.571975379e+002 3.574086184e+002 4.6e-008 0.61
25 7.7e-005 5.4e-002 4.9e-003 1.00e+000 3.572126371e+002 3.574026145e+002 4.2e-008 0.62
26 7.0e-005 4.9e-002 4.4e-003 1.00e+000 3.572262247e+002 3.573972063e+002 3.7e-008 0.66
27 6.3e-005 4.5e-002 4.0e-003 1.00e+000 3.572384517e+002 3.573923352e+002 3.4e-008 0.67
28 5.6e-005 4.1e-002 3.6e-003 1.00e+000 3.572494550e+002 3.573879494e+002 3.0e-008 0.69
29 5.1e-005 3.8e-002 3.2e-003 1.00e+000 3.572593579e+002 3.573840020e+002 2.7e-008 0.70
30 4.6e-005 3.5e-002 2.9e-003 1.00e+000 3.572682711e+002 3.573804497e+002 2.5e-008 0.73
31 4.1e-005 3.2e-002 2.6e-003 1.00e+000 3.572762938e+002 3.573772537e+002 2.2e-008 0.75
32 3.7e-005 2.9e-002 2.4e-003 1.00e+000 3.572835153e+002 3.573743784e+002 2.0e-008 0.76
33 3.3e-005 2.7e-002 2.1e-003 1.00e+000 3.572900158e+002 3.573717920e+002 1.8e-008 0.80
34 3.0e-005 2.5e-002 1.9e-003 1.00e+000 3.572958675e+002 3.573694655e+002 1.6e-008 0.81
35 2.7e-005 2.3e-002 1.7e-003 1.00e+000 3.573011351e+002 3.573673728e+002 1.4e-008 0.83
36 2.4e-005 2.2e-002 1.5e-003 1.00e+000 3.573058769e+002 3.573654906e+002 1.3e-008 0.84
37 2.2e-005 2.0e-002 1.4e-003 1.00e+000 3.573101455e+002 3.573637976e+002 1.2e-008 0.87
38 2.0e-005 1.9e-002 1.3e-003 1.00e+000 3.573139881e+002 3.573622748e+002 1.1e-008 0.89
39 1.8e-005 1.8e-002 1.1e-003 1.00e+000 3.573174472e+002 3.573609051e+002 9.5e-009 0.91
40 1.6e-005 1.7e-002 1.0e-003 1.00e+000 3.573205611e+002 3.573596730e+002 8.6e-009 0.92
41 1.4e-005 1.6e-002 9.1e-004 1.00e+000 3.573233641e+002 3.573585648e+002 7.7e-009 0.94
42 1.3e-005 1.5e-002 8.2e-004 1.00e+000 3.573258873e+002 3.573575679e+002 6.9e-009 0.97
43 1.2e-005 1.4e-002 7.4e-004 1.00e+000 3.573281586e+002 3.573566712e+002 6.2e-009 0.98
44 1.0e-005 1.3e-002 6.7e-004 1.00e+000 3.573302032e+002 3.573558645e+002 5.6e-009 1.00
45 9.4e-006 1.3e-002 6.0e-004 1.00e+000 3.573320436e+002 3.573551388e+002 5.1e-009 1.03
46 8.5e-006 1.2e-002 5.4e-004 1.00e+000 3.573337002e+002 3.573544859e+002 4.5e-009 1.04
47 7.6e-006 1.2e-002 4.9e-004 1.00e+000 3.573351914e+002 3.573538985e+002 4.1e-009 1.06
48 6.9e-006 1.1e-002 4.4e-004 1.00e+000 3.573365336e+002 3.573533701e+002 3.7e-009 1.08
49 6.2e-006 1.1e-002 3.9e-004 1.00e+000 3.573377418e+002 3.573528946e+002 3.3e-009 1.11
50 5.6e-006 1.0e-002 3.5e-004 1.00e+000 3.573388292e+002 3.573524668e+002 3.0e-009 1.12
51 5.0e-006 1.0e-002 3.2e-004 1.00e+000 3.573398079e+002 3.573520818e+002 2.7e-009 1.14
52 4.5e-006 9.8e-003 2.9e-004 1.00e+000 3.573406889e+002 3.573517354e+002 2.4e-009 1.17
53 4.0e-006 9.5e-003 2.6e-004 1.00e+000 3.573414818e+002 3.573514236e+002 2.2e-009 1.19
54 3.6e-006 9.3e-003 2.3e-004 1.00e+000 3.573421954e+002 3.573511431e+002 2.0e-009 1.20
55 3.3e-006 9.1e-003 2.1e-004 1.00e+000 3.573428376e+002 3.573508905e+002 1.8e-009 1.22
56 3.0e-006 8.9e-003 1.9e-004 1.00e+000 3.573434156e+002 3.573506633e+002 1.6e-009 1.23
57 2.7e-006 8.7e-003 1.7e-004 1.00e+000 3.573439358e+002 3.573504587e+002 1.4e-009 1.26
58 2.4e-006 8.6e-003 1.5e-004 1.00e+000 3.573444040e+002 3.573502746e+002 1.3e-009 1.28
59 2.2e-006 8.5e-003 1.4e-004 1.00e+000 3.573448253e+002 3.573501089e+002 1.2e-009 1.29
60 1.9e-006 8.3e-003 1.2e-004 1.00e+000 3.573452045e+002 3.573499597e+002 1.0e-009 1.31
61 1.7e-006 8.2e-003 1.1e-004 1.00e+000 3.573455458e+002 3.573498255e+002 9.4e-010 1.33
62 1.6e-006 8.1e-003 1.0e-004 1.00e+000 3.573458529e+002 3.573497046e+002 8.4e-010 1.34
63 1.4e-006 8.1e-003 9.0e-005 1.00e+000 3.573461292e+002 3.573495959e+002 7.6e-010 1.36
64 1.3e-006 8.0e-003 8.1e-005 1.00e+000 3.573463780e+002 3.573494980e+002 6.8e-010 1.39
65 1.1e-006 7.9e-003 7.3e-005 1.00e+000 3.573466018e+002 3.573494098e+002 6.1e-010 1.40
66 1.0e-006 7.8e-003 6.6e-005 1.00e+000 3.573468033e+002 3.573493304e+002 5.5e-010 1.42
67 9.3e-007 7.8e-003 5.9e-005 1.00e+000 3.573469846e+002 3.573492590e+002 5.0e-010 1.44
68 8.3e-007 7.7e-003 5.3e-005 1.00e+000 3.573471477e+002 3.573491948e+002 4.5e-010 1.45
69 7.5e-007 7.7e-003 4.8e-005 1.00e+000 3.573472945e+002 3.573491369e+002 4.0e-010 1.47
70 6.8e-007 7.6e-003 4.3e-005 1.00e+000 3.573474267e+002 3.573490848e+002 3.6e-010 1.50
71 6.1e-007 7.6e-003 3.9e-005 1.00e+000 3.573475456e+002 3.573490379e+002 3.3e-010 1.51
72 5.5e-007 7.6e-003 3.5e-005 1.00e+000 3.573476526e+002 3.573489957e+002 2.9e-010 1.53
73 4.9e-007 7.5e-003 3.1e-005 1.00e+000 3.573477488e+002 3.573489577e+002 2.6e-010 1.54
74 4.4e-007 7.5e-003 2.8e-005 1.00e+000 3.573478355e+002 3.573489234e+002 2.4e-010 1.56
75 4.0e-007 7.5e-003 2.5e-005 1.00e+000 3.573479134e+002 3.573488926e+002 2.1e-010 1.58
76 3.6e-007 7.5e-003 2.3e-005 1.00e+000 3.573479836e+002 3.573488648e+002 1.9e-010 1.59
77 3.2e-007 7.4e-003 2.1e-005 1.00e+000 3.573480467e+002 3.573488398e+002 1.7e-010 1.62
78 2.9e-007 7.4e-003 1.9e-005 1.00e+000 3.573481036e+002 3.573488174e+002 1.6e-010 1.64
79 2.6e-007 7.4e-003 1.7e-005 1.00e+000 3.573481547e+002 3.573487971e+002 1.4e-010 1.65
80 2.4e-007 7.4e-003 1.5e-005 9.99e-001 3.573482007e+002 3.573487789e+002 1.3e-010 1.67
81 2.1e-007 7.4e-003 1.3e-005 1.00e+000 3.573482421e+002 3.573487624e+002 1.1e-010 1.69
82 1.9e-007 7.3e-003 1.2e-005 9.98e-001 3.573482793e+002 3.573487477e+002 1.0e-010 1.72
83 1.7e-007 7.3e-003 1.1e-005 9.98e-001 3.573483128e+002 3.573487344e+002 9.2e-011 1.73
84 1.5e-007 7.3e-003 9.8e-006 9.99e-001 3.573483430e+002 3.573487224e+002 8.3e-011 1.75
85 1.4e-007 7.3e-003 8.9e-006 1.00e+000 3.573483701e+002 3.573487116e+002 7.5e-011 1.76
86 1.3e-007 7.3e-003 8.0e-006 9.99e-001 3.573483946e+002 3.573487019e+002 6.7e-011 1.78
87 1.1e-007 7.3e-003 7.2e-006 1.00e+000 3.573484166e+002 3.573486932e+002 6.1e-011 1.79
88 1.0e-007 6.5e-003 6.5e-006 1.01e+000 3.573484368e+002 3.573486851e+002 5.5e-011 1.83
89 9.1e-008 5.9e-003 5.8e-006 9.93e-001 3.573484545e+002 3.573486781e+002 4.9e-011 1.84
90 8.2e-008 5.3e-003 5.2e-006 1.00e+000 3.573484707e+002 3.573486716e+002 4.4e-011 1.86
91 7.4e-008 4.8e-003 4.7e-006 1.00e+000 3.573484852e+002 3.573486658e+002 4.0e-011 1.87
92 6.6e-008 4.3e-003 4.2e-006 9.95e-001 3.573484981e+002 3.573486607e+002 3.6e-011 1.89
93 6.0e-008 3.9e-003 3.8e-006 9.95e-001 3.573485097e+002 3.573486561e+002 3.2e-011 1.90
94 6.5e-009 4.1e-004 4.1e-007 9.99e-001 3.573486032e+002 3.573486189e+002 3.5e-012 1.93
95 5.9e-009 3.7e-004 3.7e-007 1.04e+000 3.573486045e+002 3.573486183e+002 3.2e-012 1.95
96 5.3e-009 3.3e-004 3.3e-007 1.01e+000 3.573486055e+002 3.573486179e+002 2.9e-012 1.97
97 4.9e-009 3.1e-004 3.0e-007 1.16e+000 3.573486068e+002 3.573486173e+002 2.8e-012 1.98
98 4.4e-009 2.8e-004 2.7e-007 9.94e-001 3.573486076e+002 3.573486170e+002 2.5e-012 2.00
99 4.0e-009 2.5e-004 2.5e-007 9.95e-001 3.573486082e+002 3.573486168e+002 2.3e-012 2.01
100 3.6e-009 2.2e-004 2.2e-007 1.01e+000 3.573486089e+002 3.573486165e+002 2.1e-012 2.04
101 3.2e-009 2.0e-004 2.0e-007 9.96e-001 3.573486094e+002 3.573486163e+002 1.9e-012 2.06
102 2.9e-009 1.8e-004 1.8e-007 9.96e-001 3.573486099e+002 3.573486161e+002 1.7e-012 2.08
103 2.6e-009 1.6e-004 1.6e-007 9.80e-001 3.573486104e+002 3.573486159e+002 1.5e-012 2.09
104 2.4e-009 1.5e-004 1.5e-007 1.01e+000 3.573486108e+002 3.573486158e+002 1.4e-012 2.11
105 2.1e-009 1.3e-004 1.3e-007 1.01e+000 3.573486112e+002 3.573486156e+002 1.2e-012 2.12
106 1.9e-009 1.2e-004 1.2e-007 1.00e+000 3.573486115e+002 3.573486155e+002 1.1e-012 2.14
107 1.7e-009 1.1e-004 1.1e-007 9.89e-001 3.573486118e+002 3.573486154e+002 9.9e-013 2.17
Interior-point optimizer terminated. Time: 2.17.
Optimizer terminated. Time: 2.18
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 3.5734861178e+002 Viol. con: 2e-008 var: 0e+000
Dual. obj: 3.5734861540e+002 Viol. con: 0e+000 var: 7e-004
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.22 seconds.
result packing took 14% of solve time
solution checking took 6% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Windows/64-X86
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1012
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1023
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1023
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.03
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 6
Optimizer - solved problem : the primal
Optimizer - Constraints : 830
Optimizer - Cones : 0
Optimizer - Scalar variables : 3579 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.05 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.01
Factor - nonzeros before factor : 1.67e+004 after factor : 1.72e+005
Factor - dense dim. : 0 flops : 0.00e+000
Factor - GP saved nzs : 0 GP saved flops : 0.00e+000
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.289216044e+005 2.000000000e+000 1.0e+000 0.08
1 1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.266775833e+005 3.803741943e+000 4.7e-001 0.11
2 4.4e+002 5.7e+002 2.5e+004 -9.35e-001 -1.207998731e+005 1.084180437e+001 1.9e-001 0.13
3 2.9e+002 3.7e+002 1.6e+004 -8.43e-001 -1.159533006e+005 6.141738742e+001 1.3e-001 0.14
4 2.9e+002 3.7e+002 1.6e+004 -7.60e-001 -1.137614550e+005 1.946615993e+003 1.3e-001 0.16
5 8.6e+001 1.1e+002 4.9e+003 -7.56e-001 -7.873791092e+004 1.029432263e+004 3.8e-002 0.19
6 2.8e+001 3.7e+001 1.6e+003 -2.75e-001 -3.706476093e+004 1.220641355e+004 1.3e-002 0.20
7 1.4e+001 1.8e+001 7.7e+002 4.35e-001 -2.030567968e+004 6.163510157e+003 6.0e-003 0.22
8 7.6e+000 9.8e+000 4.3e+002 7.35e-001 -1.180252607e+004 3.699008326e+003 3.4e-003 0.25
9 2.9e+000 3.7e+000 1.6e+002 8.69e-001 -4.542574255e+003 1.611196608e+003 1.3e-003 0.30
10 1.4e+000 1.8e+000 7.9e+001 9.69e-001 -2.009195296e+003 9.676511718e+002 6.2e-004 0.34
11 9.6e-001 1.2e+000 5.5e+001 9.89e-001 -1.381391298e+003 6.944429098e+002 4.3e-004 0.37
12 8.4e-001 1.1e+000 4.8e+001 9.74e-001 -1.220057850e+003 6.089998944e+002 3.8e-004 0.42
13 3.5e-001 4.5e-001 2.0e+001 9.84e-001 -4.954113010e+002 2.767217208e+002 1.6e-004 0.45
14 1.9e-001 2.6e-001 1.1e+001 1.01e+000 -2.547989981e+002 1.739608087e+002 8.8e-005 0.48
15 7.8e-002 1.3e-001 4.5e+000 9.99e-001 -8.253876751e+001 9.184541748e+001 3.6e-005 0.53
16 2.3e-002 1.1e-001 1.4e+000 1.00e+000 -6.410287003e-001 5.294698693e+001 1.1e-005 0.56
17 1.5e-002 8.3e-002 8.7e-001 1.00e+000 1.306853704e+001 4.649502312e+001 7.1e-006 0.61
18 2.8e-003 1.4e-001 1.7e-001 1.00e+000 3.161974934e+001 3.829726333e+001 1.4e-006 0.64
19 1.4e-003 9.8e-002 8.9e-002 1.00e+000 3.387244537e+001 3.730607182e+001 7.5e-007 0.69
20 4.6e-004 1.0e-001 2.8e-002 1.00e+000 3.549091322e+001 3.658198764e+001 2.4e-007 0.72
21 2.1e-004 7.9e-002 1.3e-002 1.00e+000 3.589091635e+001 3.640150521e+001 1.1e-007 0.75
22 1.9e-004 7.1e-002 1.2e-002 1.00e+000 3.592728045e+001 3.638680181e+001 1.0e-007 0.78
23 1.7e-004 6.5e-002 1.1e-002 1.00e+000 3.595898820e+001 3.637252750e+001 9.1e-008 0.80
24 1.6e-004 5.9e-002 9.7e-003 1.00e+000 3.598754980e+001 3.635971288e+001 8.1e-008 0.81
25 1.4e-004 5.4e-002 8.7e-003 1.00e+000 3.601322413e+001 3.634815219e+001 7.3e-008 0.83
26 1.3e-004 4.9e-002 7.9e-003 1.00e+000 3.603631278e+001 3.633773265e+001 6.6e-008 0.84
27 1.1e-004 4.5e-002 7.1e-003 1.00e+000 3.605707751e+001 3.632834275e+001 5.9e-008 0.86
28 1.0e-004 4.1e-002 6.4e-003 1.00e+000 3.607575368e+001 3.631988203e+001 5.3e-008 0.89
29 9.2e-005 3.8e-002 5.7e-003 1.00e+000 3.609255254e+001 3.631225958e+001 4.8e-008 0.91
30 8.3e-005 3.5e-002 5.2e-003 1.00e+000 3.610766373e+001 3.630539317e+001 4.3e-008 0.92
31 7.4e-005 3.2e-002 4.6e-003 1.00e+000 3.612125756e+001 3.629920845e+001 3.9e-008 0.94
32 6.7e-005 3.0e-002 4.2e-003 1.00e+000 3.613348700e+001 3.629363825e+001 3.5e-008 0.95
33 6.0e-005 2.7e-002 3.8e-003 1.00e+000 3.614448946e+001 3.628862190e+001 3.2e-008 0.97
34 5.4e-005 2.5e-002 3.4e-003 1.00e+000 3.615438842e+001 3.628410465e+001 2.8e-008 1.00
35 4.9e-005 2.3e-002 3.1e-003 1.00e+000 3.616329487e+001 3.628003707e+001 2.6e-008 1.01
36 4.4e-005 2.2e-002 2.7e-003 1.00e+000 3.617130855e+001 3.627637461e+001 2.3e-008 1.03
37 3.9e-005 2.0e-002 2.5e-003 1.00e+000 3.617851916e+001 3.627307707e+001 2.1e-008 1.04
38 3.6e-005 1.9e-002 2.2e-003 1.00e+000 3.618500735e+001 3.627010824e+001 1.9e-008 1.06
39 3.2e-005 1.8e-002 2.0e-003 1.00e+000 3.619084562e+001 3.626743545e+001 1.7e-008 1.08
40 2.9e-005 1.7e-002 1.8e-003 1.00e+000 3.619609919e+001 3.626502926e+001 1.5e-008 1.09
41 2.6e-005 1.6e-002 1.6e-003 1.00e+000 3.620082670e+001 3.626286315e+001 1.4e-008 1.12
42 2.3e-005 1.5e-002 1.5e-003 1.00e+000 3.620508089e+001 3.626091322e+001 1.2e-008 1.14
43 2.1e-005 1.4e-002 1.3e-003 1.00e+000 3.620890922e+001 3.625915792e+001 1.1e-008 1.15
44 1.9e-005 1.3e-002 1.2e-003 1.00e+000 3.621235434e+001 3.625757788e+001 9.9e-009 1.17
45 1.7e-005 1.3e-002 1.1e-003 1.00e+000 3.621545465e+001 3.625615560e+001 8.9e-009 1.20
46 1.5e-005 1.2e-002 9.6e-004 1.00e+000 3.621824467e+001 3.625487534e+001 8.0e-009 1.22
47 1.4e-005 1.2e-002 8.6e-004 1.00e+000 3.622075548e+001 3.625372294e+001 7.2e-009 1.23
48 1.2e-005 1.1e-002 7.8e-004 1.00e+000 3.622301502e+001 3.625268563e+001 6.5e-009 1.25
49 1.1e-005 1.1e-002 7.0e-004 1.00e+000 3.622504844e+001 3.625175191e+001 5.9e-009 1.26
50 1.0e-005 1.1e-002 6.3e-004 1.00e+000 3.622687838e+001 3.625091144e+001 5.3e-009 1.29
51 9.0e-006 1.0e-002 5.7e-004 1.00e+000 3.622852519e+001 3.625015491e+001 4.7e-009 1.33
52 8.1e-006 9.9e-003 5.1e-004 1.00e+000 3.623000721e+001 3.624947393e+001 4.3e-009 1.36
53 7.3e-006 9.6e-003 4.6e-004 1.00e+000 3.623134092e+001 3.624886095e+001 3.8e-009 1.39
54 6.6e-006 9.4e-003 4.1e-004 1.00e+000 3.623254116e+001 3.624830918e+001 3.5e-009 1.42
55 5.9e-006 9.2e-003 3.7e-004 1.00e+000 3.623362128e+001 3.624781251e+001 3.1e-009 1.44
56 5.3e-006 9.0e-003 3.3e-004 1.00e+000 3.623459332e+001 3.624736541e+001 2.8e-009 1.45
57 4.8e-006 8.8e-003 3.0e-004 1.00e+000 3.623546808e+001 3.624696295e+001 2.5e-009 1.48
58 4.3e-006 8.6e-003 2.7e-004 1.00e+000 3.623625529e+001 3.624660069e+001 2.3e-009 1.50
59 3.9e-006 8.5e-003 2.4e-004 1.00e+000 3.623696372e+001 3.624627459e+001 2.0e-009 1.51
60 3.5e-006 8.4e-003 2.2e-004 1.00e+000 3.623760125e+001 3.624598104e+001 1.8e-009 1.54
61 3.1e-006 8.3e-003 2.0e-004 1.00e+000 3.623817499e+001 3.624571678e+001 1.7e-009 1.56
62 2.8e-006 8.1e-003 1.8e-004 1.00e+000 3.623869130e+001 3.624547891e+001 1.5e-009 1.58
63 2.6e-006 8.1e-003 1.6e-004 1.00e+000 3.623915594e+001 3.624526480e+001 1.3e-009 1.59
64 2.3e-006 8.0e-003 1.4e-004 1.00e+000 3.623957408e+001 3.624507206e+001 1.2e-009 1.61
65 2.1e-006 7.9e-003 1.3e-004 1.00e+000 3.623995038e+001 3.624489856e+001 1.1e-009 1.64
66 1.9e-006 7.8e-003 1.2e-004 1.00e+000 3.624028902e+001 3.624474238e+001 9.8e-010 1.65
67 1.7e-006 7.7e-003 1.0e-004 1.00e+000 3.624059376e+001 3.624460181e+001 8.8e-010 1.67
68 1.5e-006 7.7e-003 9.4e-005 1.00e+000 3.624086801e+001 3.624447526e+001 7.9e-010 1.69
69 1.4e-006 7.6e-003 8.5e-005 1.00e+000 3.624111482e+001 3.624436135e+001 7.1e-010 1.70
70 1.2e-006 7.6e-003 7.6e-005 1.00e+000 3.624133693e+001 3.624425880e+001 6.4e-010 1.72
71 1.1e-006 7.5e-003 6.9e-005 1.00e+000 3.624153681e+001 3.624416650e+001 5.8e-010 1.73
72 9.9e-007 7.5e-003 6.2e-005 1.00e+000 3.624171669e+001 3.624408341e+001 5.2e-010 1.76
73 8.9e-007 7.5e-003 5.6e-005 1.00e+000 3.624187857e+001 3.624400861e+001 4.7e-010 1.78
74 8.0e-007 7.4e-003 5.0e-005 1.00e+000 3.624202425e+001 3.624394128e+001 4.2e-010 1.79
75 7.2e-007 7.4e-003 4.5e-005 1.00e+000 3.624215535e+001 3.624388069e+001 3.8e-010 1.81
76 6.5e-007 7.4e-003 4.1e-005 1.00e+000 3.624227334e+001 3.624382613e+001 3.4e-010 1.83
77 5.8e-007 7.3e-003 3.7e-005 1.00e+000 3.624237952e+001 3.624377705e+001 3.1e-010 1.84
78 5.3e-007 7.3e-003 3.3e-005 1.00e+000 3.624247507e+001 3.624373286e+001 2.8e-010 1.87
79 4.7e-007 7.3e-003 3.0e-005 1.00e+000 3.624256107e+001 3.624369306e+001 2.5e-010 1.89
80 4.3e-007 7.3e-003 2.7e-005 1.00e+000 3.624263846e+001 3.624365725e+001 2.2e-010 1.90
81 3.8e-007 7.2e-003 2.4e-005 1.00e+000 3.624270810e+001 3.624362502e+001 2.0e-010 1.92
82 3.4e-007 7.2e-003 2.2e-005 1.00e+000 3.624277078e+001 3.624359600e+001 1.8e-010 1.93
83 3.1e-007 7.2e-003 1.9e-005 1.00e+000 3.624282719e+001 3.624356989e+001 1.6e-010 1.95
84 2.8e-007 7.2e-003 1.7e-005 1.00e+000 3.624287795e+001 3.624354639e+001 1.5e-010 1.97
85 2.5e-007 7.2e-003 1.6e-005 1.00e+000 3.624292363e+001 3.624352524e+001 1.3e-010 1.98
86 2.3e-007 7.2e-003 1.4e-005 1.00e+000 3.624296475e+001 3.624350620e+001 1.2e-010 2.01
87 2.0e-007 7.1e-003 1.3e-005 9.99e-001 3.624300174e+001 3.624348907e+001 1.1e-010 2.03
88 1.8e-007 7.1e-003 1.1e-005 1.00e+000 3.624303504e+001 3.624347364e+001 9.6e-011 2.04
89 1.6e-007 7.1e-003 1.0e-005 1.00e+000 3.624306501e+001 3.624345974e+001 8.7e-011 2.06
90 1.5e-007 7.1e-003 9.3e-006 9.99e-001 3.624309198e+001 3.624344724e+001 7.8e-011 2.08
91 1.3e-007 7.1e-003 8.4e-006 1.00e+000 3.624311625e+001 3.624343598e+001 7.0e-011 2.09
92 1.2e-007 7.1e-003 7.5e-006 1.00e+000 3.624313810e+001 3.624342585e+001 6.3e-011 2.11
93 1.1e-007 7.1e-003 6.8e-006 1.00e+000 3.624315776e+001 3.624341674e+001 5.7e-011 2.14
94 9.7e-008 7.1e-003 6.1e-006 1.00e+000 3.624317545e+001 3.624340852e+001 5.1e-011 2.15
95 8.8e-008 7.1e-003 5.5e-006 1.00e+000 3.624319137e+001 3.624340114e+001 4.6e-011 2.17
96 7.9e-008 7.1e-003 4.9e-006 1.00e+000 3.624320572e+001 3.624339447e+001 4.1e-011 2.18
97 7.1e-008 7.1e-003 4.4e-006 1.00e+000 3.624321861e+001 3.624338848e+001 3.7e-011 2.21
98 6.4e-008 7.0e-003 4.0e-006 1.00e+000 3.624323022e+001 3.624338310e+001 3.4e-011 2.23
99 5.7e-008 7.0e-003 3.6e-006 1.00e+000 3.624324066e+001 3.624337825e+001 3.0e-011 2.25
100 5.2e-008 7.0e-003 3.2e-006 9.99e-001 3.624325006e+001 3.624337390e+001 2.7e-011 2.26
101 4.7e-008 7.0e-003 2.9e-006 9.99e-001 3.624325851e+001 3.624336998e+001 2.4e-011 2.28
102 4.2e-008 7.0e-003 2.6e-006 9.98e-001 3.624326612e+001 3.624336645e+001 2.2e-011 2.29
103 3.8e-008 6.3e-003 2.4e-006 1.00e+000 3.624327303e+001 3.624336323e+001 2.0e-011 2.31
104 3.4e-008 5.7e-003 2.1e-006 9.97e-001 3.624327919e+001 3.624336038e+001 1.8e-011 2.34
105 3.1e-008 5.1e-003 1.9e-006 9.97e-001 3.624328473e+001 3.624335782e+001 1.6e-011 2.36
106 2.7e-008 4.6e-003 1.7e-006 1.00e+000 3.624328974e+001 3.624335549e+001 1.4e-011 2.37
107 2.5e-008 4.1e-003 1.5e-006 1.01e+000 3.624329433e+001 3.624335334e+001 1.3e-011 2.39
108 2.2e-008 3.7e-003 1.4e-006 9.99e-001 3.624329836e+001 3.624335147e+001 1.2e-011 2.40
109 2.0e-008 3.4e-003 1.3e-006 9.96e-001 3.624330198e+001 3.624334979e+001 1.1e-011 2.43
110 1.8e-008 3.0e-003 1.1e-006 1.00e+000 3.624330525e+001 3.624334828e+001 9.5e-012 2.45
111 1.6e-008 2.7e-003 1.0e-006 9.99e-001 3.624330818e+001 3.624334691e+001 8.6e-012 2.48
112 1.5e-008 2.4e-003 9.1e-007 9.90e-001 3.624331082e+001 3.624334570e+001 7.7e-012 2.51
113 1.3e-008 2.2e-003 8.2e-007 9.96e-001 3.624331320e+001 3.624334459e+001 6.9e-012 2.54
114 1.2e-008 2.0e-003 7.4e-007 1.00e+000 3.624331534e+001 3.624334360e+001 6.2e-012 2.57
115 1.1e-008 1.8e-003 6.7e-007 1.00e+000 3.624331727e+001 3.624334270e+001 5.6e-012 2.61
116 9.6e-009 1.6e-003 6.0e-007 1.00e+000 3.624331901e+001 3.624334189e+001 5.1e-012 2.62
117 8.6e-009 1.4e-003 5.4e-007 1.00e+000 3.624332057e+001 3.624334116e+001 4.5e-012 2.65
118 7.8e-009 1.3e-003 4.9e-007 9.97e-001 3.624332197e+001 3.624334051e+001 4.1e-012 2.68
119 7.0e-009 1.2e-003 4.4e-007 1.00e+000 3.624332324e+001 3.624333992e+001 3.7e-012 2.71
120 6.3e-009 1.1e-003 3.9e-007 9.98e-001 3.624332438e+001 3.624333939e+001 3.3e-012 2.75
121 5.7e-009 9.5e-004 3.5e-007 9.99e-001 3.624332540e+001 3.624333892e+001 3.0e-012 2.76
122 5.1e-009 8.5e-004 3.2e-007 9.99e-001 3.624332632e+001 3.624333849e+001 2.7e-012 2.78
123 4.6e-009 7.7e-004 2.9e-007 9.98e-001 3.624332715e+001 3.624333810e+001 2.4e-012 2.81
124 4.1e-009 6.9e-004 2.6e-007 9.99e-001 3.624332790e+001 3.624333775e+001 2.2e-012 2.82
125 3.7e-009 6.2e-004 2.3e-007 9.98e-001 3.624332857e+001 3.624333744e+001 2.0e-012 2.84
126 3.3e-009 5.6e-004 2.1e-007 9.95e-001 3.624332917e+001 3.624333716e+001 1.8e-012 2.86
127 3.0e-009 5.0e-004 1.9e-007 9.97e-001 3.624332972e+001 3.624333691e+001 1.6e-012 2.87
128 2.7e-009 4.5e-004 1.7e-007 9.97e-001 3.624333021e+001 3.624333668e+001 1.4e-012 2.89
129 2.4e-009 4.1e-004 1.5e-007 1.00e+000 3.624333065e+001 3.624333647e+001 1.3e-012 2.92
130 2.2e-009 3.7e-004 1.4e-007 1.00e+000 3.624333105e+001 3.624333629e+001 1.2e-012 2.93
131 2.0e-009 3.3e-004 1.2e-007 9.97e-001 3.624333140e+001 3.624333612e+001 1.0e-012 2.95
132 1.8e-009 3.0e-004 1.1e-007 9.99e-001 3.624333173e+001 3.624333597e+001 9.4e-013 2.96
Interior-point optimizer terminated. Time: 2.98.
Optimizer terminated. Time: 3.00
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 3.6243331725e+001 Viol. con: 3e-008 var: 0e+000
Dual. obj: 3.6243335969e+001 Viol. con: 0e+000 var: 2e-003
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.02 seconds.
result packing took 11% of solve time
solution checking took 2.7% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Windows/64-X86
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1012
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1023
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1023
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.05
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 6
Optimizer - solved problem : the primal
Optimizer - Constraints : 830
Optimizer - Cones : 0
Optimizer - Scalar variables : 3579 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.06 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.03
Factor - nonzeros before factor : 1.68e+004 after factor : 1.72e+005
Factor - dense dim. : 0 flops : 0.00e+000
Factor - GP saved nzs : 0 GP saved flops : 0.00e+000
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.288884984e+005 2.000000000e+000 1.0e+000 0.11
1 1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.266359820e+005 3.774599270e+000 4.7e-001 0.16
2 4.2e+002 5.5e+002 2.4e+004 -9.35e-001 -1.204536049e+005 1.083248753e+001 1.9e-001 0.20
3 2.8e+002 3.7e+002 1.6e+004 -8.37e-001 -1.157889801e+005 6.665177304e+001 1.3e-001 0.25
4 2.8e+002 3.7e+002 1.6e+004 -7.58e-001 -1.132120824e+005 2.261947282e+003 1.2e-001 0.30
5 7.5e+001 9.8e+001 4.3e+003 -7.51e-001 -7.370050810e+004 1.114794052e+004 3.3e-002 0.33
6 3.0e+001 3.9e+001 1.7e+003 -1.92e-001 -3.984938966e+004 1.107249692e+004 1.3e-002 0.36
7 1.4e+001 1.8e+001 7.8e+002 3.92e-001 -2.070980721e+004 5.965041872e+003 6.1e-003 0.41
8 9.0e+000 1.2e+001 5.1e+002 7.29e-001 -1.410231463e+004 4.103526421e+003 4.0e-003 0.44
9 3.6e+000 4.7e+000 2.1e+002 8.34e-001 -5.837350395e+003 1.819161802e+003 1.6e-003 0.47
10 2.0e+000 2.6e+000 1.1e+002 9.52e-001 -2.940338371e+003 1.325304056e+003 8.9e-004 0.50
11 9.0e-001 1.2e+000 5.1e+001 9.84e-001 -1.324730082e+003 6.203743379e+002 4.1e-004 0.53
12 8.6e-001 1.2e+000 4.9e+001 9.64e-001 -1.286315407e+003 5.821375483e+002 3.9e-004 0.55
13 3.8e-001 5.3e-001 2.2e+001 9.81e-001 -5.626757791e+002 2.744796639e+002 1.7e-004 0.58
14 1.5e-001 2.3e-001 8.6e+000 1.00e+000 -2.179596274e+002 1.114771293e+002 6.9e-005 0.59
15 8.6e-002 1.5e-001 5.0e+000 1.00e+000 -1.179899807e+002 7.375584632e+001 4.0e-005 0.61
16 2.6e-002 1.2e-001 1.6e+000 1.00e+000 -2.807369557e+001 3.131489199e+001 1.3e-005 0.64
17 1.1e-002 9.3e-002 6.9e-001 1.00e+000 -5.277056577e+000 2.122045170e+001 5.7e-006 0.67
18 1.0e-002 8.5e-002 6.3e-001 1.01e+000 -3.411073132e+000 2.059177433e+001 5.2e-006 0.72
19 6.6e-003 6.5e-002 4.0e-001 1.01e+000 2.894366096e+000 1.822581880e+001 3.3e-006 0.75
20 4.5e-003 4.7e-002 2.8e-001 1.01e+000 6.709113238e+000 1.712856197e+001 2.3e-006 0.78
21 1.8e-003 5.9e-002 1.1e-001 1.01e+000 1.119385296e+001 1.545046106e+001 9.4e-007 0.83
22 1.0e-003 4.8e-002 6.2e-002 1.02e+000 1.264895074e+001 1.495383896e+001 5.1e-007 0.86
23 4.6e-004 5.4e-002 2.9e-002 1.02e+000 1.351659651e+001 1.458946317e+001 2.4e-007 0.91
24 2.6e-004 5.0e-002 1.6e-002 1.01e+000 1.385885930e+001 1.445533799e+001 1.4e-007 0.94
25 1.3e-004 5.2e-002 8.5e-003 1.01e+000 1.406163449e+001 1.437394268e+001 7.1e-008 0.98
26 9.0e-005 4.6e-002 5.6e-003 1.01e+000 1.413613042e+001 1.434341585e+001 4.7e-008 1.03
27 8.1e-005 4.2e-002 5.1e-003 1.00e+000 1.415437837e+001 1.434100893e+001 4.3e-008 1.06
28 7.3e-005 3.9e-002 4.6e-003 1.00e+000 1.416702758e+001 1.433496238e+001 3.8e-008 1.09
29 6.5e-005 3.6e-002 4.1e-003 1.00e+000 1.417864516e+001 1.432976637e+001 3.4e-008 1.12
30 5.9e-005 3.3e-002 3.7e-003 1.00e+000 1.418904693e+001 1.432503926e+001 3.1e-008 1.16
31 5.3e-005 3.0e-002 3.3e-003 1.00e+000 1.419838738e+001 1.432076665e+001 2.8e-008 1.19
32 4.8e-005 2.8e-002 3.0e-003 1.00e+000 1.420677259e+001 1.431690282e+001 2.5e-008 1.22
33 4.3e-005 2.6e-002 2.7e-003 1.00e+000 1.421430101e+001 1.431340919e+001 2.3e-008 1.25
34 3.9e-005 2.4e-002 2.4e-003 1.00e+000 1.422106126e+001 1.431025126e+001 2.0e-008 1.28
35 3.5e-005 2.2e-002 2.2e-003 1.00e+000 1.422713308e+001 1.430739830e+001 1.8e-008 1.31
36 3.1e-005 2.1e-002 2.0e-003 1.00e+000 1.423258791e+001 1.430482195e+001 1.7e-008 1.36
37 2.8e-005 2.0e-002 1.8e-003 1.00e+000 1.423748954e+001 1.430249627e+001 1.5e-008 1.39
38 2.5e-005 1.8e-002 1.6e-003 1.00e+000 1.424189486e+001 1.430039763e+001 1.3e-008 1.42
39 2.3e-005 1.7e-002 1.4e-003 1.00e+000 1.424585462e+001 1.429850504e+001 1.2e-008 1.45
40 2.0e-005 1.6e-002 1.3e-003 1.00e+000 1.424941425e+001 1.429679761e+001 1.1e-008 1.48
41 1.8e-005 1.5e-002 1.2e-003 1.00e+000 1.425261467e+001 1.429525831e+001 9.8e-009 1.51
42 1.7e-005 1.5e-002 1.0e-003 1.00e+000 1.425549227e+001 1.429387019e+001 8.8e-009 1.54
43 1.5e-005 1.4e-002 9.4e-004 1.00e+000 1.425807988e+001 1.429261906e+001 7.9e-009 1.56
44 1.3e-005 1.3e-002 8.5e-004 1.00e+000 1.426040678e+001 1.429149104e+001 7.1e-009 1.58
45 1.2e-005 1.3e-002 7.6e-004 1.00e+000 1.426249936e+001 1.429047406e+001 6.4e-009 1.61
46 1.1e-005 1.2e-002 6.9e-004 1.00e+000 1.426438118e+001 1.428955778e+001 5.8e-009 1.62
47 9.8e-006 1.2e-002 6.2e-004 1.00e+000 1.426607334e+001 1.428873205e+001 5.2e-009 1.65
48 8.8e-006 1.1e-002 5.6e-004 1.00e+000 1.426759498e+001 1.428798743e+001 4.7e-009 1.70
49 7.9e-006 1.1e-002 5.0e-004 1.00e+000 1.426896330e+001 1.428731586e+001 4.2e-009 1.75
50 7.1e-006 1.1e-002 4.5e-004 1.00e+000 1.427019363e+001 1.428671054e+001 3.8e-009 1.79
51 6.4e-006 1.0e-002 4.0e-004 1.00e+000 1.427129980e+001 1.428616501e+001 3.4e-009 1.84
52 5.8e-006 1.0e-002 3.6e-004 1.00e+000 1.427229444e+001 1.428567283e+001 3.1e-009 1.89
53 5.2e-006 9.7e-003 3.3e-004 1.00e+000 1.427318878e+001 1.428522939e+001 2.8e-009 1.92
54 4.7e-006 9.5e-003 3.0e-004 9.99e-001 1.427399296e+001 1.428483003e+001 2.5e-009 1.95
55 4.2e-006 9.3e-003 2.7e-004 1.00e+000 1.427471640e+001 1.428446926e+001 2.2e-009 2.00
56 3.8e-006 9.1e-003 2.4e-004 1.00e+000 1.427536709e+001 1.428414454e+001 2.0e-009 2.03
57 3.4e-006 8.9e-003 2.2e-004 9.99e-001 1.427595232e+001 1.428385250e+001 1.8e-009 2.06
58 3.1e-006 8.8e-003 1.9e-004 1.00e+000 1.427647896e+001 1.428358876e+001 1.6e-009 2.09
59 2.8e-006 8.7e-003 1.7e-004 1.00e+000 1.427695283e+001 1.428335113e+001 1.5e-009 2.12
60 2.5e-006 8.5e-003 1.6e-004 1.00e+000 1.427737916e+001 1.428313733e+001 1.3e-009 2.17
61 2.2e-006 8.4e-003 1.4e-004 1.00e+000 1.427776269e+001 1.428294503e+001 1.2e-009 2.20
62 2.0e-006 8.3e-003 1.3e-004 9.99e-001 1.427810775e+001 1.428277203e+001 1.1e-009 2.25
63 1.8e-006 8.2e-003 1.1e-004 1.00e+000 1.427841825e+001 1.428261617e+001 9.6e-010 2.29
64 1.6e-006 8.1e-003 1.0e-004 9.99e-001 1.427869762e+001 1.428247597e+001 8.6e-010 2.34
65 1.5e-006 8.1e-003 9.3e-005 9.98e-001 1.427894897e+001 1.428234990e+001 7.8e-010 2.37
66 1.3e-006 8.0e-003 8.3e-005 1.00e+000 1.427917529e+001 1.428223575e+001 7.0e-010 2.42
67 1.2e-006 7.9e-003 7.5e-005 1.00e+000 1.427937890e+001 1.428213331e+001 6.3e-010 2.46
68 1.1e-006 7.9e-003 6.8e-005 9.99e-001 1.427956207e+001 1.428204117e+001 5.7e-010 2.51
69 9.7e-007 7.8e-003 6.1e-005 9.97e-001 1.427972687e+001 1.428195837e+001 5.1e-010 2.56
70 8.7e-007 7.8e-003 5.5e-005 9.96e-001 1.427987515e+001 1.428188389e+001 4.6e-010 2.61
71 7.8e-007 7.7e-003 4.9e-005 1.00e+000 1.428000866e+001 1.428181652e+001 4.1e-010 2.65
72 7.0e-007 7.7e-003 4.4e-005 9.96e-001 1.428012874e+001 1.428175616e+001 3.7e-010 2.70
73 6.3e-007 7.7e-003 4.0e-005 1.00e+000 1.428023720e+001 1.428170121e+001 3.4e-010 2.75
74 5.7e-007 7.7e-003 3.6e-005 1.01e+000 1.428033596e+001 1.428165107e+001 3.0e-010 2.79
75 5.1e-007 6.9e-003 3.2e-005 1.01e+000 1.428042628e+001 1.428160506e+001 2.7e-010 2.82
76 4.6e-007 6.2e-003 2.9e-005 9.94e-001 1.428050456e+001 1.428156580e+001 2.5e-010 2.86
77 4.2e-007 5.6e-003 2.6e-005 1.01e+000 1.428057664e+001 1.428152913e+001 2.2e-010 2.90
78 3.7e-007 5.0e-003 2.4e-005 1.00e+000 1.428063994e+001 1.428149715e+001 2.0e-010 2.92
79 3.4e-007 4.5e-003 2.1e-005 1.00e+000 1.428069689e+001 1.428146840e+001 1.8e-010 2.95
80 3.0e-007 4.1e-003 1.9e-005 1.00e+000 1.428074814e+001 1.428144249e+001 1.6e-010 2.96
81 2.7e-007 3.7e-003 1.7e-005 1.02e+000 1.428079724e+001 1.428141730e+001 1.5e-010 2.98
82 2.5e-007 3.3e-003 1.5e-005 1.00e+000 1.428083846e+001 1.428139649e+001 1.3e-010 3.00
83 2.2e-007 3.0e-003 1.4e-005 9.94e-001 1.428087551e+001 1.428137789e+001 1.2e-010 3.01
84 2.0e-007 2.7e-003 1.3e-005 9.90e-001 1.428090884e+001 1.428136120e+001 1.1e-010 3.04
85 1.8e-007 2.4e-003 1.1e-005 9.99e-001 1.428093887e+001 1.428134601e+001 9.6e-011 3.06
86 1.6e-007 2.2e-003 1.0e-005 9.94e-001 1.428096588e+001 1.428133242e+001 8.6e-011 3.07
87 1.4e-007 1.9e-003 9.1e-006 9.69e-001 1.428099011e+001 1.428132050e+001 7.8e-011 3.09
88 1.3e-007 1.8e-003 8.2e-006 1.01e+000 1.428101295e+001 1.428130876e+001 7.0e-011 3.11
89 1.2e-007 1.6e-003 7.4e-006 1.03e+000 1.428103500e+001 1.428129728e+001 6.4e-011 3.14
90 1.1e-007 1.4e-003 6.7e-006 9.76e-001 1.428105236e+001 1.428128869e+001 5.8e-011 3.15
91 9.5e-008 1.3e-003 6.0e-006 1.01e+000 1.428106873e+001 1.428128029e+001 5.2e-011 3.17
92 8.6e-008 1.1e-003 5.4e-006 9.98e-001 1.428108276e+001 1.428127318e+001 4.7e-011 3.18
93 7.7e-008 1.0e-003 4.8e-006 1.02e+000 1.428109647e+001 1.428126610e+001 4.3e-011 3.20
94 6.9e-008 9.3e-004 4.4e-006 1.04e+000 1.428110993e+001 1.428125901e+001 3.9e-011 3.21
95 6.3e-008 8.4e-004 3.9e-006 1.02e+000 1.428112077e+001 1.428125345e+001 3.6e-011 3.26
96 5.6e-008 7.5e-004 3.5e-006 1.07e+000 1.428113227e+001 1.428124732e+001 3.3e-011 3.29
97 5.1e-008 6.8e-004 3.2e-006 9.88e-001 1.428113994e+001 1.428124354e+001 3.0e-011 3.34
98 4.6e-008 6.1e-004 2.9e-006 9.63e-001 1.428114681e+001 1.428124023e+001 2.7e-011 3.39
99 4.1e-008 5.5e-004 2.6e-006 8.16e-001 1.428115287e+001 1.428123772e+001 2.4e-011 3.42
100 3.7e-008 4.9e-004 2.3e-006 8.69e-001 1.428115838e+001 1.428123526e+001 2.2e-011 3.45
101 3.3e-008 4.5e-004 2.1e-006 1.08e+000 1.428116525e+001 1.428123145e+001 2.0e-011 3.50
102 3.0e-008 4.0e-004 1.9e-006 1.01e+000 1.428116985e+001 1.428122907e+001 1.8e-011 3.54
103 2.7e-008 3.6e-004 1.7e-006 1.04e+000 1.428117444e+001 1.428122664e+001 1.7e-011 3.59
104 2.4e-008 3.2e-004 1.5e-006 1.02e+000 1.428117817e+001 1.428122470e+001 1.5e-011 3.63
105 2.2e-008 2.9e-004 1.4e-006 1.02e+000 1.428118150e+001 1.428122297e+001 1.4e-011 3.68
106 2.0e-008 2.6e-004 1.2e-006 9.95e-001 1.428118425e+001 1.428122158e+001 1.3e-011 3.71
107 1.8e-008 2.4e-004 1.1e-006 1.01e+000 1.428118682e+001 1.428122027e+001 1.1e-011 3.76
108 1.6e-008 2.1e-004 1.0e-006 1.02e+000 1.428118923e+001 1.428121902e+001 1.0e-011 3.79
109 1.4e-008 1.9e-004 9.0e-007 1.00e+000 1.428119122e+001 1.428121801e+001 9.3e-012 3.81
110 1.3e-008 1.7e-004 8.1e-007 9.74e-001 1.428119300e+001 1.428121714e+001 8.3e-012 3.84
111 1.2e-008 1.6e-004 7.3e-007 9.91e-001 1.428119460e+001 1.428121633e+001 7.5e-012 3.85
112 1.0e-008 1.4e-004 6.6e-007 9.79e-001 1.428119604e+001 1.428121562e+001 6.8e-012 3.87
113 9.4e-009 1.3e-004 5.9e-007 9.85e-001 1.428119733e+001 1.428121497e+001 6.1e-012 3.88
114 8.5e-009 1.1e-004 5.3e-007 1.03e+000 1.428119865e+001 1.428121428e+001 5.6e-012 3.90
115 7.6e-009 1.0e-004 4.8e-007 9.86e-001 1.428119969e+001 1.428121376e+001 5.0e-012 3.93
116 6.9e-009 9.2e-005 4.3e-007 9.82e-001 1.428120062e+001 1.428121330e+001 4.5e-012 3.95
117 6.2e-009 8.3e-005 3.9e-007 1.03e+000 1.428120156e+001 1.428121280e+001 4.1e-012 3.96
118 5.6e-009 7.4e-005 3.5e-007 9.36e-001 1.428120230e+001 1.428121245e+001 3.7e-012 3.98
119 5.0e-009 6.7e-005 3.1e-007 9.69e-001 1.428120297e+001 1.428121212e+001 3.3e-012 3.99
120 4.5e-009 6.0e-005 2.8e-007 9.02e-001 1.428120357e+001 1.428121185e+001 3.0e-012 4.01
121 4.1e-009 5.4e-005 2.5e-007 9.44e-001 1.428120411e+001 1.428121159e+001 2.7e-012 4.03
122 2.4e-009 3.4e-006 1.6e-008 8.38e-001 1.428120896e+001 1.428120947e+001 3.5e-013 4.06
Interior-point optimizer terminated. Time: 4.06.
Optimizer terminated. Time: 4.07
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.4281208958e+001 Viol. con: 5e-008 var: 0e+000
Dual. obj: 1.4281209469e+001 Viol. con: 0e+000 var: 2e-005
* End solution on dual form. *
Transforming to primal solution.
Solving took 4.1 seconds.
result packing took 10% of solve time
solution checking took 2% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Windows/64-X86
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1010
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1022
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1022
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.03
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 6
Optimizer - solved problem : the primal
Optimizer - Constraints : 831
Optimizer - Cones : 0
Optimizer - Scalar variables : 3581 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.05 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.03
Factor - nonzeros before factor : 1.68e+004 after factor : 1.72e+005
Factor - dense dim. : 0 flops : 0.00e+000
Factor - GP saved nzs : 0 GP saved flops : 0.00e+000
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.289122955e+005 2.000000000e+000 1.0e+000 0.08
1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.266169077e+005 3.779171593e+000 4.6e-001 0.16
2 4.0e+002 5.1e+002 2.2e+004 -9.34e-001 -1.198582125e+005 1.137222280e+001 1.7e-001 0.20
3 2.8e+002 3.6e+002 1.6e+004 -8.29e-001 -1.157258926e+005 8.367317113e+001 1.2e-001 0.23
4 2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.124215764e+005 2.832679601e+003 1.2e-001 0.28
5 6.3e+001 8.2e+001 3.6e+003 -7.47e-001 -6.640452667e+004 1.270004796e+004 2.8e-002 0.31
6 3.9e+001 5.1e+001 2.2e+003 -7.19e-002 -4.860706085e+004 1.113877961e+004 1.7e-002 0.34
7 2.8e+001 3.7e+001 1.6e+003 2.50e-001 -3.839217795e+004 8.758864219e+003 1.3e-002 0.38
8 1.6e+001 2.1e+001 9.0e+002 4.36e-001 -2.428203302e+004 5.454557190e+003 7.1e-003 0.42
9 6.4e+000 8.3e+000 3.6e+002 6.74e-001 -1.033426529e+004 2.810591791e+003 2.9e-003 0.45
10 3.6e+000 4.7e+000 2.0e+002 8.87e-001 -5.635484405e+003 1.899057471e+003 1.6e-003 0.48
11 1.3e+000 1.7e+000 7.5e+001 9.54e-001 -2.013046291e+003 7.892105355e+002 5.9e-004 0.52
12 1.0e+000 1.3e+000 5.7e+001 9.87e-001 -1.520063746e+003 6.366021648e+002 4.5e-004 0.55
13 8.5e-001 1.5e+000 4.8e+001 9.70e-001 -1.298933325e+003 5.502987724e+002 3.9e-004 0.58
14 2.9e-001 5.1e-001 1.6e+001 9.89e-001 -4.334689227e+002 1.969994148e+002 1.3e-004 0.62
15 1.6e-001 3.0e-001 9.3e+000 1.00e+000 -2.379504686e+002 1.162354913e+002 7.5e-005 0.66
16 7.3e-002 1.6e-001 4.2e+000 1.00e+000 -1.038589339e+002 5.761827102e+001 3.4e-005 0.70
17 3.5e-002 1.0e-001 2.1e+000 1.01e+000 -4.581883836e+001 3.218133007e+001 1.7e-005 0.73
18 1.8e-002 7.9e-002 1.1e+000 1.01e+000 -2.038732365e+001 2.046071587e+001 8.8e-006 0.77
19 1.8e-002 7.6e-002 1.0e+000 1.02e+000 -1.899890089e+001 2.043769863e+001 8.5e-006 0.81
20 9.7e-003 5.8e-002 5.7e-001 1.02e+000 -4.742162142e+000 1.674426286e+001 4.7e-006 0.84
21 4.1e-003 5.8e-002 2.5e-001 1.02e+000 4.582971093e+000 1.368809105e+001 2.0e-006 0.87
22 2.1e-003 5.2e-002 1.3e-001 1.01e+000 7.768824286e+000 1.261360630e+001 1.1e-006 0.91
23 6.0e-004 8.2e-002 3.9e-002 9.87e-001 1.034297992e+001 1.181152747e+001 3.4e-007 0.94
24 1.8e-004 8.8e-002 1.3e-002 9.78e-001 1.109074572e+001 1.156935827e+001 1.1e-007 0.97
25 6.0e-005 8.7e-002 4.3e-003 9.88e-001 1.133247896e+001 1.149489225e+001 3.9e-008 1.00
26 2.2e-005 8.4e-002 1.6e-003 9.96e-001 1.141328629e+001 1.147317463e+001 1.5e-008 1.01
27 8.2e-006 8.1e-002 6.0e-004 9.99e-001 1.144292895e+001 1.146572708e+001 5.6e-009 1.04
28 7.4e-006 7.4e-002 5.4e-004 1.00e+000 1.144485635e+001 1.146537608e+001 5.0e-009 1.06
29 6.7e-006 6.7e-002 4.9e-004 1.00e+000 1.144644856e+001 1.146491668e+001 4.5e-009 1.08
30 6.0e-006 6.1e-002 4.4e-004 1.00e+000 1.144788122e+001 1.146450288e+001 4.1e-009 1.09
31 5.4e-006 5.6e-002 3.9e-004 1.00e+000 1.144916796e+001 1.146412769e+001 3.7e-009 1.11
32 4.9e-006 5.1e-002 3.5e-004 1.00e+000 1.145032483e+001 1.146378885e+001 3.3e-009 1.14
33 4.4e-006 4.6e-002 3.2e-004 1.00e+000 1.145136488e+001 1.146348264e+001 3.0e-009 1.16
34 3.9e-006 4.2e-002 2.9e-004 1.00e+000 1.145230001e+001 1.146320613e+001 2.7e-009 1.17
35 3.5e-006 3.9e-002 2.6e-004 1.00e+000 1.145314089e+001 1.146295652e+001 2.4e-009 1.19
36 3.2e-006 3.6e-002 2.3e-004 1.00e+000 1.145389709e+001 1.146273121e+001 2.2e-009 1.20
37 2.9e-006 3.3e-002 2.1e-004 1.00e+000 1.145457720e+001 1.146252797e+001 1.9e-009 1.23
38 2.6e-006 3.0e-002 1.9e-004 1.00e+000 1.145518893e+001 1.146234467e+001 1.7e-009 1.25
39 2.3e-006 2.8e-002 1.7e-004 1.00e+000 1.145573920e+001 1.146217940e+001 1.6e-009 1.28
40 2.1e-006 2.6e-002 1.5e-004 1.00e+000 1.145623420e+001 1.146203044e+001 1.4e-009 1.29
41 1.9e-006 2.4e-002 1.4e-004 1.00e+000 1.145667953e+001 1.146189616e+001 1.3e-009 1.31
42 1.7e-006 2.2e-002 1.2e-004 1.00e+000 1.145708019e+001 1.146177517e+001 1.1e-009 1.33
43 1.5e-006 2.1e-002 1.1e-004 1.00e+000 1.145744066e+001 1.146166617e+001 1.0e-009 1.34
44 1.4e-006 1.9e-002 1.0e-004 1.00e+000 1.145776500e+001 1.146156798e+001 9.3e-010 1.36
45 1.2e-006 1.8e-002 9.0e-005 1.00e+000 1.145805684e+001 1.146147951e+001 8.4e-010 1.39
46 1.1e-006 1.7e-002 8.1e-005 1.00e+000 1.145831944e+001 1.146139983e+001 7.5e-010 1.40
47 1.0e-006 1.6e-002 7.3e-005 1.00e+000 1.145855575e+001 1.146132805e+001 6.8e-010 1.42
48 9.0e-007 1.5e-002 6.6e-005 9.99e-001 1.145876836e+001 1.146126353e+001 6.1e-010 1.44
49 8.1e-007 1.4e-002 5.9e-005 1.00e+000 1.145895970e+001 1.146120538e+001 5.5e-010 1.45
50 7.3e-007 1.4e-002 5.3e-005 1.00e+000 1.145913188e+001 1.146115301e+001 4.9e-010 1.48
51 6.6e-007 1.3e-002 4.8e-005 1.00e+000 1.145928684e+001 1.146110586e+001 4.4e-010 1.50
52 2.3e-007 4.5e-003 1.7e-005 1.00e+000 1.146019640e+001 1.146082850e+001 1.5e-010 1.51
53 2.1e-007 4.0e-003 1.5e-005 1.00e+000 1.146024518e+001 1.146081407e+001 1.4e-010 1.53
54 7.1e-008 1.4e-003 5.2e-006 1.01e+000 1.146053016e+001 1.146072508e+001 4.8e-011 1.54
55 6.4e-008 1.3e-003 4.6e-006 1.01e+000 1.146054604e+001 1.146072040e+001 4.3e-011 1.56
56 5.8e-008 1.1e-003 4.2e-006 9.99e-001 1.146055948e+001 1.146071642e+001 3.9e-011 1.59
57 5.2e-008 1.0e-003 3.8e-006 1.03e+000 1.146057342e+001 1.146071207e+001 3.6e-011 1.61
58 4.7e-008 9.1e-004 3.4e-006 1.01e+000 1.146058470e+001 1.146070871e+001 3.2e-011 1.62
59 4.2e-008 8.2e-004 3.0e-006 1.00e+000 1.146059440e+001 1.146070585e+001 2.9e-011 1.64
60 1.5e-008 1.6e-004 5.8e-007 9.72e-001 1.146066454e+001 1.146068622e+001 5.9e-012 1.65
61 1.3e-008 1.4e-004 5.3e-007 9.91e-001 1.146066615e+001 1.146068569e+001 5.3e-012 1.67
62 1.6e-009 7.9e-006 3.0e-008 9.87e-001 1.146067979e+001 1.146068090e+001 3.3e-013 1.70
Interior-point optimizer terminated. Time: 1.70.
Optimizer terminated. Time: 1.72
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1460679791e+001 Viol. con: 3e-008 var: 0e+000
Dual. obj: 1.1460680896e+001 Viol. con: 0e+000 var: 6e-005
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.74 seconds.
result packing took 15% of solve time
solution checking took 3.8% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Windows/64-X86
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1012
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1023
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1023
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.02
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 6
Optimizer - solved problem : the primal
Optimizer - Constraints : 830
Optimizer - Cones : 0
Optimizer - Scalar variables : 3579 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.05 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.03
Factor - nonzeros before factor : 1.67e+004 after factor : 1.72e+005
Factor - dense dim. : 0 flops : 0.00e+000
Factor - GP saved nzs : 0 GP saved flops : 0.00e+000
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.288303345e+005 2.000000000e+000 1.0e+000 0.08
1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265192762e+005 3.780479936e+000 4.6e-001 0.09
2 3.9e+002 5.0e+002 2.2e+004 -9.34e-001 -1.195799066e+005 1.160517488e+001 1.7e-001 0.11
3 2.8e+002 3.6e+002 1.6e+004 -8.26e-001 -1.156357827e+005 9.406817449e+001 1.2e-001 0.14
4 2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.123238000e+005 2.800935213e+003 1.2e-001 0.17
5 7.8e+001 1.0e+002 4.4e+003 -7.46e-001 -7.498388138e+004 1.053068490e+004 3.5e-002 0.20
6 3.8e+001 4.9e+001 2.1e+003 -2.08e-001 -4.716200950e+004 1.110975347e+004 1.7e-002 0.23
7 2.1e+001 2.8e+001 1.2e+003 2.72e-001 -3.073919275e+004 7.248970091e+003 9.5e-003 0.27
8 9.8e+000 1.3e+001 5.5e+002 5.69e-001 -1.536034095e+004 3.891969378e+003 4.3e-003 0.30
9 4.2e+000 5.5e+000 2.4e+002 8.19e-001 -6.676929471e+003 2.109893560e+003 1.9e-003 0.31
10 2.0e+000 2.6e+000 1.1e+002 9.39e-001 -2.962273732e+003 1.171566017e+003 8.8e-004 0.33
11 1.4e+000 1.8e+000 7.8e+001 9.83e-001 -2.096575137e+003 8.360471175e+002 6.2e-004 0.34
12 9.0e-001 1.2e+000 5.1e+001 9.85e-001 -1.355755875e+003 5.626980070e+002 4.0e-004 0.38
13 7.4e-001 1.1e+000 4.2e+001 9.64e-001 -1.126538217e+003 4.651708978e+002 3.3e-004 0.39
14 2.6e-001 3.9e-001 1.5e+001 9.90e-001 -3.944746667e+002 1.817810751e+002 1.2e-004 0.41
15 1.5e-001 2.3e-001 8.6e+000 1.00e+000 -2.189171791e+002 1.081385416e+002 6.9e-005 0.42
16 4.0e-002 1.5e-001 2.4e+000 1.00e+000 -5.533033125e+001 3.458681090e+001 1.9e-005 0.44
17 3.4e-002 1.3e-001 2.0e+000 1.00e+000 -4.533266770e+001 3.085051631e+001 1.6e-005 0.45
18 2.2e-002 9.8e-002 1.3e+000 1.00e+000 -2.663137861e+001 2.253536175e+001 1.1e-005 0.48
19 1.7e-002 7.9e-002 1.0e+000 1.01e+000 -1.829489267e+001 1.992450020e+001 8.3e-006 0.50
20 1.4e-002 6.7e-002 8.5e-001 1.02e+000 -1.320023270e+001 1.870377391e+001 7.0e-006 0.52
21 5.6e-003 6.1e-002 3.3e-001 1.02e+000 1.875167820e+000 1.418963027e+001 2.7e-006 0.53
22 2.2e-003 6.3e-002 1.4e-001 1.02e+000 7.558141440e+000 1.254449204e+001 1.1e-006 0.55
23 8.1e-004 6.3e-002 5.1e-002 9.85e-001 9.853098376e+000 1.176697179e+001 4.5e-007 0.56
24 3.0e-004 7.5e-002 2.0e-002 9.69e-001 1.075853564e+001 1.152367559e+001 1.8e-007 0.58
25 1.5e-004 5.8e-002 1.0e-002 9.56e-001 1.105383528e+001 1.143572931e+001 8.9e-008 0.59
26 7.2e-005 5.7e-002 5.0e-003 9.86e-001 1.120381147e+001 1.139458728e+001 4.4e-008 0.62
27 6.4e-005 5.2e-002 4.5e-003 9.93e-001 1.122035487e+001 1.139220258e+001 4.0e-008 0.64
28 5.8e-005 4.8e-002 4.0e-003 9.92e-001 1.123362489e+001 1.138836400e+001 3.6e-008 0.66
29 5.2e-005 4.4e-002 3.6e-003 9.93e-001 1.124581043e+001 1.138516547e+001 3.2e-008 0.69
30 4.7e-005 4.0e-002 3.3e-003 9.93e-001 1.125671305e+001 1.138221835e+001 2.9e-008 0.70
31 4.2e-005 3.7e-002 2.9e-003 9.93e-001 1.126648340e+001 1.137952550e+001 2.6e-008 0.72
32 3.8e-005 3.4e-002 2.6e-003 9.92e-001 1.127522986e+001 1.137706597e+001 2.4e-008 0.73
33 3.4e-005 3.1e-002 2.4e-003 9.91e-001 1.128305711e+001 1.137482642e+001 2.1e-008 0.77
34 3.1e-005 2.9e-002 2.1e-003 9.90e-001 1.129006416e+001 1.137279605e+001 1.9e-008 0.78
35 2.8e-005 2.7e-002 1.9e-003 9.88e-001 1.129638767e+001 1.137096532e+001 1.7e-008 0.80
36 2.5e-005 2.5e-002 1.7e-003 9.87e-001 1.130214734e+001 1.136928387e+001 1.6e-008 0.81
37 2.2e-005 2.3e-002 1.6e-003 9.88e-001 1.130726271e+001 1.136774612e+001 1.4e-008 0.83
38 2.0e-005 2.1e-002 1.4e-003 9.88e-001 1.131190325e+001 1.136634434e+001 1.3e-008 0.84
39 1.8e-005 2.0e-002 1.3e-003 9.88e-001 1.131604575e+001 1.136508310e+001 1.1e-008 0.87
40 1.6e-005 1.9e-002 1.1e-003 9.89e-001 1.131976960e+001 1.136391278e+001 1.0e-008 0.89
41 1.5e-005 1.7e-002 1.0e-003 9.89e-001 1.132313406e+001 1.136287568e+001 9.2e-009 0.91
42 1.3e-005 1.6e-002 9.2e-004 9.89e-001 1.132613504e+001 1.136192319e+001 8.3e-009 0.92
43 1.2e-005 1.5e-002 8.3e-004 9.90e-001 1.132883865e+001 1.136105558e+001 7.4e-009 0.94
44 1.1e-005 1.5e-002 7.5e-004 9.90e-001 1.133127621e+001 1.136027907e+001 6.7e-009 0.95
45 9.7e-006 1.4e-002 6.7e-004 9.91e-001 1.133346218e+001 1.135957547e+001 6.0e-009 1.00
46 8.7e-006 1.3e-002 6.1e-004 9.91e-001 1.133542582e+001 1.135893651e+001 5.4e-009 1.04
47 7.8e-006 1.3e-002 5.5e-004 9.92e-001 1.133719364e+001 1.135836037e+001 4.9e-009 1.08
48 7.0e-006 1.2e-002 4.9e-004 9.93e-001 1.133878466e+001 1.135784154e+001 4.4e-009 1.11
49 6.3e-006 1.1e-002 4.4e-004 9.93e-001 1.134021623e+001 1.135737399e+001 4.0e-009 1.14
50 5.7e-006 1.1e-002 4.0e-004 9.94e-001 1.134150483e+001 1.135695278e+001 3.6e-009 1.19
51 5.1e-006 1.1e-002 3.6e-004 9.95e-001 1.134266518e+001 1.135657340e+001 3.2e-009 1.20
52 4.6e-006 1.0e-002 3.2e-004 9.96e-001 1.134371017e+001 1.135623159e+001 2.9e-009 1.22
53 4.2e-006 9.9e-003 2.9e-004 9.97e-001 1.134465117e+001 1.135592352e+001 2.6e-009 1.23
54 3.7e-006 9.6e-003 2.6e-004 9.97e-001 1.134549835e+001 1.135564569e+001 2.3e-009 1.26
55 3.4e-006 9.4e-003 2.4e-004 9.98e-001 1.134626090e+001 1.135539513e+001 2.1e-009 1.28
56 3.0e-006 9.1e-003 2.1e-004 9.98e-001 1.134694717e+001 1.135516918e+001 1.9e-009 1.29
57 2.7e-006 8.9e-003 1.9e-004 9.98e-001 1.134756475e+001 1.135496548e+001 1.7e-009 1.31
58 2.5e-006 8.7e-003 1.7e-004 9.99e-001 1.134812051e+001 1.135478187e+001 1.5e-009 1.34
59 2.2e-006 8.6e-003 1.5e-004 9.99e-001 1.134862064e+001 1.135461644e+001 1.4e-009 1.36
60 2.0e-006 8.4e-003 1.4e-004 9.99e-001 1.134907073e+001 1.135446740e+001 1.2e-009 1.37
61 1.8e-006 8.3e-003 1.3e-004 9.99e-001 1.134947579e+001 1.135433317e+001 1.1e-009 1.39
62 1.6e-006 8.1e-003 1.1e-004 9.99e-001 1.134984035e+001 1.135421226e+001 1.0e-009 1.40
63 1.4e-006 8.0e-003 1.0e-004 9.99e-001 1.135016845e+001 1.135410342e+001 9.1e-010 1.42
64 1.3e-006 7.9e-003 9.1e-005 9.99e-001 1.135046376e+001 1.135400542e+001 8.2e-010 1.44
65 1.2e-006 7.8e-003 8.2e-005 9.99e-001 1.135072956e+001 1.135391720e+001 7.3e-010 1.45
66 1.1e-006 7.7e-003 7.4e-005 9.99e-001 1.135096879e+001 1.135383780e+001 6.6e-010 1.48
67 9.5e-007 7.7e-003 6.6e-005 1.00e+000 1.135118412e+001 1.135376633e+001 5.9e-010 1.50
68 8.6e-007 7.6e-003 6.0e-005 1.00e+000 1.135137794e+001 1.135370201e+001 5.3e-010 1.51
69 7.7e-007 7.5e-003 5.4e-005 1.00e+000 1.135155239e+001 1.135364412e+001 4.8e-010 1.53
70 6.9e-007 7.5e-003 4.8e-005 1.00e+000 1.135170941e+001 1.135359202e+001 4.3e-010 1.54
71 6.2e-007 7.4e-003 4.4e-005 1.00e+000 1.135185074e+001 1.135354513e+001 3.9e-010 1.56
72 5.6e-007 7.4e-003 3.9e-005 1.00e+000 1.135197795e+001 1.135350295e+001 3.5e-010 1.58
73 5.1e-007 7.3e-003 3.5e-005 1.00e+000 1.135209245e+001 1.135346497e+001 3.2e-010 1.59
74 4.5e-007 7.3e-003 3.2e-005 1.00e+000 1.135219551e+001 1.135343079e+001 2.8e-010 1.62
75 4.1e-007 7.3e-003 2.9e-005 1.00e+000 1.135228826e+001 1.135340005e+001 2.6e-010 1.64
76 3.7e-007 7.2e-003 2.6e-005 9.99e-001 1.135237174e+001 1.135337239e+001 2.3e-010 1.65
77 3.3e-007 7.2e-003 2.3e-005 1.00e+000 1.135244688e+001 1.135334747e+001 2.1e-010 1.67
78 3.0e-007 7.2e-003 2.1e-005 1.00e+000 1.135251451e+001 1.135332506e+001 1.9e-010 1.69
79 2.7e-007 7.1e-003 1.9e-005 9.99e-001 1.135257537e+001 1.135330491e+001 1.7e-010 1.70
80 2.4e-007 7.1e-003 1.7e-005 1.00e+000 1.135263015e+001 1.135328675e+001 1.5e-010 1.72
81 2.2e-007 7.1e-003 1.5e-005 1.00e+000 1.135267946e+001 1.135327038e+001 1.4e-010 1.75
82 2.0e-007 7.1e-003 1.4e-005 1.00e+000 1.135272383e+001 1.135325567e+001 1.2e-010 1.76
83 1.8e-007 7.1e-003 1.2e-005 1.00e+000 1.135276377e+001 1.135324244e+001 1.1e-010 1.78
84 1.6e-007 7.0e-003 1.1e-005 9.99e-001 1.135279971e+001 1.135323053e+001 9.9e-011 1.79
85 1.4e-007 7.0e-003 1.0e-005 1.00e+000 1.135283205e+001 1.135321981e+001 8.9e-011 1.81
86 1.3e-007 7.0e-003 9.0e-006 1.00e+000 1.135286117e+001 1.135321015e+001 8.0e-011 1.83
87 1.2e-007 7.0e-003 8.1e-006 1.00e+000 1.135288737e+001 1.135320146e+001 7.2e-011 1.86
88 1.0e-007 7.0e-003 7.3e-006 1.00e+000 1.135291095e+001 1.135319362e+001 6.5e-011 1.87
89 9.4e-008 7.0e-003 6.5e-006 1.00e+000 1.135293217e+001 1.135318657e+001 5.9e-011 1.89
90 8.4e-008 7.0e-003 5.9e-006 1.00e+000 1.135295127e+001 1.135318022e+001 5.3e-011 1.90
91 7.6e-008 7.0e-003 5.3e-006 1.00e+000 1.135296852e+001 1.135317448e+001 4.7e-011 1.92
92 6.8e-008 7.0e-003 4.8e-006 1.00e+000 1.135298402e+001 1.135316932e+001 4.3e-011 1.95
93 6.1e-008 7.0e-003 4.3e-006 1.00e+000 1.135299794e+001 1.135316469e+001 3.8e-011 1.97
94 5.5e-008 7.0e-003 3.9e-006 1.00e+000 1.135301048e+001 1.135316052e+001 3.5e-011 1.98
95 5.0e-008 6.9e-003 3.5e-006 9.99e-001 1.135302175e+001 1.135315679e+001 3.1e-011 2.00
96 4.5e-008 6.9e-003 3.1e-006 9.99e-001 1.135303188e+001 1.135315343e+001 2.8e-011 2.01
97 4.0e-008 6.9e-003 2.8e-006 9.98e-001 1.135304100e+001 1.135315040e+001 2.5e-011 2.04
98 3.6e-008 6.9e-003 2.5e-006 1.00e+000 1.135304921e+001 1.135314768e+001 2.3e-011 2.06
99 3.3e-008 6.9e-003 2.3e-006 9.98e-001 1.135305660e+001 1.135314523e+001 2.0e-011 2.08
100 2.9e-008 6.9e-003 2.1e-006 9.96e-001 1.135306325e+001 1.135314303e+001 1.8e-011 2.09
101 2.6e-008 6.2e-003 1.8e-006 1.00e+000 1.135306930e+001 1.135314100e+001 1.7e-011 2.11
102 2.4e-008 5.6e-003 1.7e-006 9.96e-001 1.135307468e+001 1.135313922e+001 1.5e-011 2.12
103 2.1e-008 5.0e-003 1.5e-006 1.01e+000 1.135307968e+001 1.135313754e+001 1.3e-011 2.14
104 1.9e-008 4.5e-003 1.3e-006 1.01e+000 1.135308418e+001 1.135313602e+001 1.2e-011 2.17
105 1.7e-008 4.1e-003 1.2e-006 1.00e+000 1.135308810e+001 1.135313472e+001 1.1e-011 2.18
106 1.6e-008 3.7e-003 1.1e-006 1.00e+000 1.135309160e+001 1.135313355e+001 9.9e-012 2.20
107 1.4e-008 3.3e-003 9.8e-007 1.00e+000 1.135309475e+001 1.135313251e+001 8.9e-012 2.21
108 1.3e-008 3.0e-003 8.8e-007 1.02e+000 1.135309781e+001 1.135313147e+001 8.1e-012 2.23
109 1.1e-008 2.7e-003 8.0e-007 1.01e+000 1.135310043e+001 1.135313059e+001 7.3e-012 2.25
110 1.5e-009 2.7e-004 8.2e-008 9.99e-001 1.135312076e+001 1.135312386e+001 7.5e-013 2.26
Interior-point optimizer terminated. Time: 2.28.
Optimizer terminated. Time: 2.29
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1353120764e+001 Viol. con: 2e-008 var: 0e+000
Dual. obj: 1.1353123858e+001 Viol. con: 0e+000 var: 2e-003
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.32 seconds.
result packing took 12% of solve time
solution checking took 2.9% of solve time
Using solver 'mosek'
Solving for 1899 variables.
Number of Hessian non-zeros: 1953
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Computer
Platform : Windows/64-X86
Problem
Name :
Objective sense : max
Type : GECO (general convex optimization problem)
Constraints : 1900
Cones : 0
Scalar variables : 6471
Matrix variables : 0
Integer variables : 0
Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Total number of eliminations : 1010
Eliminator terminated.
Eliminator started.
Total number of eliminations : 1022
Eliminator terminated.
Eliminator - tries : 2 time : 0.00
Eliminator - elim's : 1022
Lin. dep. - tries : 1 time : 0.00
Lin. dep. - number : 0
Presolve terminated. Time: 0.05
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Optimizer - threads : 6
Optimizer - solved problem : the primal
Optimizer - Constraints : 831
Optimizer - Cones : 0
Optimizer - Scalar variables : 3581 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.05 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.03
Factor - nonzeros before factor : 1.68e+004 after factor : 1.72e+005
Factor - dense dim. : 0 flops : 0.00e+000
Factor - GP saved nzs : 0 GP saved flops : 0.00e+000
ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME
0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.289005967e+005 2.000000000e+000 1.0e+000 0.11
1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265819987e+005 3.775575047e+000 4.6e-001 0.14
2 3.8e+002 4.9e+002 2.1e+004 -9.34e-001 -1.194852981e+005 1.178222185e+001 1.7e-001 0.19
3 2.8e+002 3.6e+002 1.6e+004 -8.24e-001 -1.156698971e+005 1.068079073e+002 1.2e-001 0.23
4 2.8e+002 3.6e+002 1.5e+004 -7.56e-001 -1.123119373e+005 2.781235980e+003 1.2e-001 0.28
5 7.6e+001 9.8e+001 4.2e+003 -7.45e-001 -7.369377882e+004 1.086808071e+004 3.3e-002 0.31
6 3.6e+001 4.7e+001 2.0e+003 -1.88e-001 -4.546711925e+004 1.112166497e+004 1.6e-002 0.36
7 2.0e+001 2.6e+001 1.1e+003 3.02e-001 -2.909763090e+004 7.248148002e+003 9.0e-003 0.41
8 9.7e+000 1.3e+001 5.4e+002 5.97e-001 -1.525014701e+004 3.925579323e+003 4.3e-003 0.47
9 4.3e+000 5.6e+000 2.4e+002 8.22e-001 -6.824936236e+003 2.126884560e+003 1.9e-003 0.52
10 1.6e+000 2.1e+000 9.0e+001 9.39e-001 -2.382143670e+003 9.941010591e+002 7.2e-004 0.58
11 1.1e+000 1.5e+000 6.3e+001 9.88e-001 -1.660105626e+003 6.956185059e+002 5.0e-004 0.61
12 7.8e-001 1.0e+000 4.4e+001 9.83e-001 -1.186333696e+003 4.998677940e+002 3.5e-004 0.66
13 5.9e-001 7.7e-001 3.3e+001 9.85e-001 -8.730261588e+002 3.883103948e+002 2.6e-004 0.70
14 2.1e-001 2.9e-001 1.2e+001 9.89e-001 -3.245192041e+002 1.424670684e+002 9.8e-005 0.75
15 8.9e-002 1.4e-001 5.1e+000 1.01e+000 -1.284356539e+002 6.667865160e+001 4.2e-005 0.78
16 3.5e-002 9.9e-002 2.1e+000 1.01e+000 -4.749559058e+001 3.075632409e+001 1.7e-005 0.83
17 2.9e-002 8.4e-002 1.7e+000 9.96e-001 -3.703720662e+001 2.753542638e+001 1.4e-005 0.86
18 1.8e-002 6.6e-002 1.0e+000 1.01e+000 -1.902016087e+001 2.024555755e+001 8.5e-006 0.87
19 1.5e-002 5.7e-002 8.8e-001 1.02e+000 -1.416591622e+001 1.901541937e+001 7.2e-006 0.91
20 5.4e-003 6.6e-002 3.2e-001 1.02e+000 2.105379149e+000 1.405615777e+001 2.6e-006 0.92
21 1.8e-003 7.8e-002 1.1e-001 1.02e+000 8.169667306e+000 1.230700005e+001 9.7e-007 0.97
22 1.3e-003 6.0e-002 8.3e-002 9.63e-001 8.936572922e+000 1.202341761e+001 7.2e-007 1.00
23 4.8e-004 6.6e-002 3.1e-002 9.59e-001 1.040613534e+001 1.160353334e+001 2.8e-007 1.04
24 1.9e-004 6.2e-002 1.3e-002 9.58e-001 1.093932131e+001 1.142614389e+001 1.1e-007 1.08
25 1.7e-004 5.7e-002 1.1e-002 9.76e-001 1.097683910e+001 1.141480382e+001 1.0e-007 1.12
26 1.5e-004 5.2e-002 1.0e-002 9.75e-001 1.101078543e+001 1.140547183e+001 9.2e-008 1.14
27 1.4e-004 4.7e-002 9.2e-003 9.76e-001 1.104373246e+001 1.139946303e+001 8.3e-008 1.17
28 1.2e-004 4.3e-002 8.3e-003 9.78e-001 1.107347274e+001 1.139407019e+001 7.5e-008 1.19
29 1.1e-004 3.9e-002 7.5e-003 9.80e-001 1.110023820e+001 1.138914310e+001 6.7e-008 1.22
30 9.9e-005 3.6e-002 6.7e-003 9.82e-001 1.112427730e+001 1.138459629e+001 6.1e-008 1.23
31 8.9e-005 3.3e-002 6.0e-003 9.83e-001 1.114585998e+001 1.138039928e+001 5.5e-008 1.25
32 8.0e-005 3.1e-002 5.4e-003 9.85e-001 1.116523161e+001 1.137652556e+001 4.9e-008 1.26
33 7.2e-005 2.8e-002 4.9e-003 9.86e-001 1.118261499e+001 1.137295185e+001 4.4e-008 1.29
34 6.5e-005 2.6e-002 4.4e-003 9.88e-001 1.119821166e+001 1.136965700e+001 4.0e-008 1.31
35 5.8e-005 2.4e-002 4.0e-003 9.89e-001 1.121220388e+001 1.136662190e+001 3.6e-008 1.33
36 5.2e-005 2.3e-002 3.6e-003 9.90e-001 1.122475605e+001 1.136382877e+001 3.2e-008 1.36
37 4.7e-005 2.1e-002 3.2e-003 9.91e-001 1.123601629e+001 1.136126111e+001 2.9e-008 1.37
38 4.3e-005 2.0e-002 2.9e-003 9.92e-001 1.124611772e+001 1.135890327e+001 2.6e-008 1.39
39 3.8e-005 1.8e-002 2.6e-003 9.92e-001 1.125517982e+001 1.135674032e+001 2.4e-008 1.40
40 3.4e-005 1.7e-002 2.3e-003 9.93e-001 1.126330979e+001 1.135475813e+001 2.1e-008 1.44
41 3.1e-005 1.6e-002 2.1e-003 9.94e-001 1.127060376e+001 1.135294320e+001 1.9e-008 1.45
42 2.8e-005 1.5e-002 1.9e-003 9.94e-001 1.127714814e+001 1.135128308e+001 1.7e-008 1.48
43 2.5e-005 1.5e-002 1.7e-003 9.95e-001 1.128302057e+001 1.134976610e+001 1.5e-008 1.53
44 2.3e-005 1.4e-002 1.5e-003 9.96e-001 1.128829088e+001 1.134838153e+001 1.4e-008 1.56
45 2.0e-005 1.3e-002 1.4e-003 9.96e-001 1.129302169e+001 1.134711932e+001 1.3e-008 1.59
46 1.8e-005 1.3e-002 1.2e-003 9.96e-001 1.129726898e+001 1.134596997e+001 1.1e-008 1.62
47 1.6e-005 1.2e-002 1.1e-003 9.97e-001 1.130108280e+001 1.134492441e+001 1.0e-008 1.64
48 1.5e-005 1.2e-002 1.0e-003 9.97e-001 1.130450793e+001 1.134397411e+001 9.2e-009 1.65
49 1.3e-005 1.1e-002 9.1e-004 9.97e-001 1.130758449e+001 1.134311123e+001 8.2e-009 1.69
50 1.2e-005 1.1e-002 8.2e-004 9.98e-001 1.131034834e+001 1.134232817e+001 7.4e-009 1.70
51 1.1e-005 1.0e-002 7.4e-004 9.98e-001 1.131283167e+001 1.134161824e+001 6.7e-009 1.72
52 9.7e-006 1.0e-002 6.6e-004 9.98e-001 1.131506319e+001 1.134097492e+001 6.0e-009 1.75
53 8.8e-006 9.7e-003 6.0e-004 9.98e-001 1.131706870e+001 1.134039242e+001 5.4e-009 1.76
54 7.9e-006 9.5e-003 5.4e-004 9.99e-001 1.131887125e+001 1.133986514e+001 4.9e-009 1.78
55 7.1e-006 9.2e-003 4.8e-004 9.99e-001 1.132049152e+001 1.133938811e+001 4.4e-009 1.79
56 6.4e-006 9.0e-003 4.4e-004 9.99e-001 1.132194805e+001 1.133895668e+001 3.9e-009 1.83
57 5.7e-006 8.8e-003 3.9e-004 9.99e-001 1.132325745e+001 1.133856666e+001 3.5e-009 1.84
58 5.2e-006 8.7e-003 3.5e-004 9.99e-001 1.132443463e+001 1.133821404e+001 3.2e-009 1.86
59 4.7e-006 8.5e-003 3.2e-004 9.99e-001 1.132549300e+001 1.133789539e+001 2.9e-009 1.87
60 4.2e-006 8.4e-003 2.9e-004 9.99e-001 1.132644458e+001 1.133760748e+001 2.6e-009 1.90
61 3.8e-006 8.2e-003 2.6e-004 9.99e-001 1.132730019e+001 1.133734747e+001 2.3e-009 1.92
62 3.4e-006 8.1e-003 2.3e-004 1.00e+000 1.132806958e+001 1.133711260e+001 2.1e-009 1.93
63 3.1e-006 8.0e-003 2.1e-004 1.00e+000 1.132876150e+001 1.133690059e+001 1.9e-009 1.97
64 2.7e-006 7.9e-003 1.9e-004 9.99e-001 1.132938380e+001 1.133670936e+001 1.7e-009 1.98
65 2.5e-006 7.8e-003 1.7e-004 1.00e+000 1.132994355e+001 1.133653682e+001 1.5e-009 2.00
66 2.2e-006 7.8e-003 1.5e-004 1.00e+000 1.133044708e+001 1.133638122e+001 1.4e-009 2.03
67 2.0e-006 7.7e-003 1.4e-004 1.00e+000 1.133090006e+001 1.133624101e+001 1.2e-009 2.04
68 1.8e-006 7.6e-003 1.2e-004 1.00e+000 1.133130762e+001 1.133611459e+001 1.1e-009 2.06
69 1.6e-006 7.6e-003 1.1e-004 1.00e+000 1.133167431e+001 1.133600070e+001 1.0e-009 2.11
70 1.5e-006 7.5e-003 1.0e-004 1.00e+000 1.133200424e+001 1.133589813e+001 9.0e-010 2.15
71 1.3e-006 7.4e-003 9.0e-005 1.00e+000 1.133230111e+001 1.133580575e+001 8.1e-010 2.20
72 1.2e-006 7.4e-003 8.1e-005 1.00e+000 1.133256827e+001 1.133572249e+001 7.3e-010 2.23
73 1.1e-006 7.4e-003 7.3e-005 1.00e+000 1.133280868e+001 1.133564749e+001 6.6e-010 2.26
74 9.6e-007 7.3e-003 6.5e-005 1.00e+000 1.133302501e+001 1.133557998e+001 5.9e-010 2.29
75 8.6e-007 7.3e-003 5.9e-005 1.00e+000 1.133321970e+001 1.133551917e+001 5.3e-010 2.32
76 7.8e-007 7.2e-003 5.3e-005 1.00e+000 1.133339490e+001 1.133546439e+001 4.8e-010 2.37
77 7.0e-007 7.2e-003 4.8e-005 1.00e+000 1.133355257e+001 1.133541507e+001 4.3e-010 2.40
78 6.3e-007 7.2e-003 4.3e-005 1.00e+000 1.133369445e+001 1.133537072e+001 3.9e-010 2.43
79 5.7e-007 7.2e-003 3.9e-005 1.00e+000 1.133382213e+001 1.133533079e+001 3.5e-010 2.45
80 5.1e-007 7.1e-003 3.5e-005 1.00e+000 1.133393702e+001 1.133529486e+001 3.1e-010 2.48
81 4.6e-007 7.1e-003 3.1e-005 1.00e+000 1.133404043e+001 1.133526247e+001 2.8e-010 2.50
82 4.1e-007 7.1e-003 2.8e-005 1.00e+000 1.133413350e+001 1.133523332e+001 2.5e-010 2.51
83 3.7e-007 7.1e-003 2.5e-005 9.99e-001 1.133421723e+001 1.133520712e+001 2.3e-010 2.54
84 3.3e-007 7.1e-003 2.3e-005 9.99e-001 1.133429259e+001 1.133518353e+001 2.1e-010 2.56
85 3.0e-007 7.0e-003 2.1e-005 1.00e+000 1.133436041e+001 1.133516228e+001 1.9e-010 2.57
86 2.7e-007 7.0e-003 1.8e-005 1.00e+000 1.133442146e+001 1.133514309e+001 1.7e-010 2.61
87 2.4e-007 7.0e-003 1.7e-005 1.00e+000 1.133447639e+001 1.133512586e+001 1.5e-010 2.62
88 2.2e-007 7.0e-003 1.5e-005 9.98e-001 1.133452581e+001 1.133511039e+001 1.4e-010 2.65
89 2.0e-007 7.0e-003 1.3e-005 1.00e+000 1.133457030e+001 1.133509642e+001 1.2e-010 2.68
90 1.8e-007 7.0e-003 1.2e-005 1.00e+000 1.133461033e+001 1.133508384e+001 1.1e-010 2.71
91 1.6e-007 7.0e-003 1.1e-005 1.00e+000 1.133464636e+001 1.133507251e+001 9.9e-011 2.75
92 1.4e-007 6.9e-003 9.8e-006 9.99e-001 1.133467878e+001 1.133506233e+001 8.9e-011 2.78
93 1.3e-007 6.9e-003 8.8e-006 1.00e+000 1.133470797e+001 1.133505314e+001 8.0e-011 2.79
94 1.2e-007 6.2e-003 8.0e-006 1.00e+000 1.133473445e+001 1.133504477e+001 7.2e-011 2.82
95 1.0e-007 5.6e-003 7.2e-006 1.00e+000 1.133475806e+001 1.133503734e+001 6.5e-011 2.84
96 9.4e-008 5.1e-003 6.4e-006 1.00e+000 1.133477936e+001 1.133503062e+001 5.8e-011 2.86
97 8.5e-008 4.6e-003 5.8e-006 9.97e-001 1.133479847e+001 1.133502464e+001 5.3e-011 2.89
98 7.6e-008 4.1e-003 5.2e-006 1.00e+000 1.133481567e+001 1.133501922e+001 4.7e-011 2.90
99 6.9e-008 3.7e-003 4.7e-006 1.00e+000 1.133483131e+001 1.133501427e+001 4.3e-011 2.92
100 6.2e-008 3.3e-003 4.2e-006 1.00e+000 1.133484525e+001 1.133500987e+001 3.8e-011 2.95
101 5.6e-008 3.0e-003 3.8e-006 1.00e+000 1.133485777e+001 1.133500593e+001 3.5e-011 2.96
102 5.0e-008 2.7e-003 3.4e-006 9.98e-001 1.133486904e+001 1.133500239e+001 3.1e-011 2.98
103 4.5e-008 2.4e-003 3.1e-006 9.98e-001 1.133487917e+001 1.133499921e+001 2.8e-011 3.00
104 4.1e-008 2.2e-003 2.8e-006 1.00e+000 1.133488832e+001 1.133499631e+001 2.5e-011 3.03
105 3.7e-008 2.0e-003 2.5e-006 1.00e+000 1.133489666e+001 1.133499367e+001 2.3e-011 3.04
106 3.3e-008 1.8e-003 2.2e-006 1.01e+000 1.133490426e+001 1.133499125e+001 2.0e-011 3.06
107 3.0e-008 1.6e-003 2.0e-006 1.00e+000 1.133491090e+001 1.133498915e+001 1.8e-011 3.09
108 2.7e-008 1.4e-003 1.8e-006 1.00e+000 1.133491692e+001 1.133498725e+001 1.7e-011 3.10
109 2.4e-008 1.3e-003 1.6e-006 1.01e+000 1.133492245e+001 1.133498549e+001 1.5e-011 3.13
110 2.2e-008 1.2e-003 1.5e-006 1.01e+000 1.133492742e+001 1.133498391e+001 1.4e-011 3.15
111 4.5e-009 2.2e-004 2.9e-007 1.01e+000 1.133496198e+001 1.133497287e+001 2.6e-012 3.17
112 4.2e-010 1.3e-005 1.6e-008 9.87e-001 1.133496994e+001 1.133497056e+001 1.6e-013 3.20
Interior-point optimizer terminated. Time: 3.20.
Optimizer terminated. Time: 3.21
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1334969941e+001 Viol. con: 9e-009 var: 0e+000
Dual. obj: 1.1334970555e+001 Viol. con: 0e+000 var: 1e-004
* End solution on dual form. *
Transforming to primal solution.
Solving took 3.24 seconds.
result packing took 75% of solve time
solution checking took 2.1% of solve time
Solving took 6 GP solves and 26.9 seconds.
Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2418945.71588 force_pound * meter but the right hand side evaluated to 2375461.22556 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 32774.3845623 force_pound but the right hand side evaluated to 32399.999998 force_pound (Allowable error: 0.1%, Actual error: 1.2%)
Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116795 meter but the right hand side evaluated to 2.08160628556 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 1243582.16896 joule / kilogram but the right hand side evaluated to 1.56115456592 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 664761.570382 joule / kilogram but the right hand side evaluated to 0.667340361492 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 18.3998914132 meter but the right hand side evaluated to 16.3228905505 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 10.90362675596269 but the right hand side evaluated to 4.7888587124712165 (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 10.019809984597675 but the right hand side evaluated to 4.78885870341629 (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 8.144910635376501 but the right hand side evaluated to 4.78885871466922 (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 18.3622341209 meter but the right hand side evaluated to 18.1377231812 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 18.3622341209 meter but the right hand side evaluated to 18.2420594876 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 0.2960341009456968 but the right hand side evaluated to 0.18973857917499398 (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 0.2330207924058918 but the right hand side evaluated to 0.1743466917680405 (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 7.563249684223192 but the right hand side evaluated to 4.730639769280703 (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 7.583098426248488 but the right hand side evaluated to 4.7578525277677945 (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 38.563s
OK
Generating XML reports...
Cloning into 'solar'...
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0)
grin 1.2.1 requires argparse>=1.1, which is not installed.
Collecting git+https://github.com/convexengineering/gpfit.git
Cloning https://github.com/convexengineering/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-qqy6yl
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
Running setup.py bdist_wheel for gpfit: started
Running setup.py bdist_wheel for gpfit: finished with status 'done'
Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-4emdls\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-n_mg7k
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0)
Building wheels for collected packages: gassolar
Running setup.py bdist_wheel for gassolar: started
Running setup.py bdist_wheel for gassolar: finished with status 'done'
Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-bgtb4j\wheels\fe\11\0a\2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
grin 1.2.1 requires argparse>=1.1, which is not installed.
Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\solar
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in d:\jenkins\workspace\gplibrary_pr_models\mosek (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2017.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.11.0)
Building wheels for collected packages: solar
Running setup.py bdist_wheel for solar: started
Running setup.py bdist_wheel for solar: finished with status 'done'
Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-oqmxyx\wheels\9f\ae\a9\52e286ff9ea1428d6dd1e8c6df0d12b22c44363d9dcc1dd331
Successfully built solar
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: solar
Successfully installed solar-0.0.0.0
adding test for 'solar/solar.py'
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
adding test for 'solar/npod_trade.py'
Beginning signomial solve.
Solving took 10 GP solves and 43.2 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 1372945.2648 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 2.1182607549 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781342 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 1.63010986522 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010574808 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 0.911985264136 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983814521 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Beginning signomial solve.
Solving took 10 GP solves and 14.3 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 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 1372945.2713 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 2.11826075491 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781344 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 1.63010986523 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010574808 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 0.911985264137 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983814522 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Using solver 'mosek'
Solving for 12129 variables.
Solving took 6.73 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2985 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 720429.8138 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 9.27 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2521 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 791679.4791 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 20.3 seconds.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1920 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 883741.3308 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 8.04 seconds.
Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.1637 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 933393.0301 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 6.61 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 1.2985 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 720429.8221 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 6.85 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2521 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 791679.4785 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 30.5 seconds.
Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1920 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 883741.3297 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 12.4 seconds.
Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.1637 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 933393.0320 but bound is 600000.0000
Beginning signomial solve.
Solving took 10 GP solves and 14.7 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 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 1372945.2748 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 2.11826075492 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781344 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 1.63010986522 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010574808 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 0.911985264136 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983814521 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Beginning signomial solve.
Solving took 10 GP solves and 23.8 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 1372945.2692 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 2.11826075491 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781344 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 1.63010986523 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010574808 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 0.911985264138 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983814523 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Using solver 'mosek'
Solving for 702 variables.
Solving took 4.43 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2555 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 773120.5118 but bound is 600000.0000
Beginning signomial solve.
Solving took 9 GP solves and 9.7 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 1002038.7385 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 76735.5639 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 1.39813215993 meter ** 2 / second ** 2 but the right hand side evaluated to 1.39812954853 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 0.803919027517 meter ** 2 / second ** 2 but the right hand side evaluated to 0.803918046082 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 2.53 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 61 seconds.
Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.0784 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/BladeElementPerf_...] 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_Missio
Running tests...
----------------------------------------------------------------------
..D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
tau = np.exp(-0.175/costhsun)
D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
tau = np.exp(-0.175/costhsun)
....EE
======================================================================
ERROR [19.444s]: test_solar_solar_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
testfn(name, import_dict, path)(self)
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn
mod.test()
File "solar.py", line 654, in test
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__
cs = self.setup(*args, **kwargs) # pylint: disable=no-member
File "solar.py", line 633, in setup
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 83, in __init__
CostedConstraintSet.__init__(self, cost, constraints, substitutions)
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__
ConstraintSet.__init__(self, constraints, subs)
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__
list.__setitem__(self, i, ConstraintSet(constraint))
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__
raise_elementhasnumpybools(constraint)
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 357, in raise_elementhasnumpybools
% (cause, constraint))
ValueError: An ArrayConstraint was created with elements of numpy.bool_
Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]
======================================================================
ERROR [68.434s]: test_solar_solar_py_mosek_cli (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
testfn(name, import_dict, path)(self)
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda>
lambda self: getattr(self, name)())) # pylint:disable=undefined-variable
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn
mod.test()
File "solar.py", line 654, in test
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__
cs = self.setup(*args, **kwargs) # pylint: disable=no-member
File "solar.py", line 633, in setup
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 83, in __init__
CostedConstraintSet.__init__(self, cost, n.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
constraints, substitutions)
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__
ConstraintSet.__init__(self, constraints, subs)
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__
list.__setitem__(self, i, ConstraintSet(constraint))
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__
raise_elementhasnumpybools(constraint)
File "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 357, in raise_elementhasnumpybools
% (cause, constraint))
ValueError: An ArrayConstraint was created with elements of numpy.bool_
Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]
----------------------------------------------------------------------
Ran 8 tests in 820.105s
FAILED (errors=2)
Generating XML reports...
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3)
Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0)
grin 1.2.1 requires argparse>=1.1, which is not installed.
Collecting git+https://github.com/hoburg/gpfit.git
Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-53rc0m
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
Running setup.py bdist_wheel for gpfit: started
Running setup.py bdist_wheel for gpfit: finished with status 'done'
Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-h7nlbc\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gplibrary
Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.3)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1)
Building wheels for collected packages: gpkitmodels
Running setup.py bdist_wheel for gpkitmodels: started
Running setup.py bdist_wheel for gpkitmodels: finished with status 'done'
Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-bi0vls\wheels\4a\da\60\bea5372bf288606a399bdc749979f532f5aff24f4c362a9887
Successfully built gpkitmodels
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: gpkitmodels
Found existing installation: gpkitmodels 0.0.0.0
Uninstalling gpkitmodels-0.0.0.0:
Successfully uninstalled gpkitmodels-0.0.0.0
Successfully installed gpkitmodels-0.0.0.0
adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py'
adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py'
adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py'
adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py'
adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.534 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.482 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 2.05 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 4.19 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.36 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 44.1 seconds.
Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006556021 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%)
Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544371526 meter * revolutions_per_minute but the right hand side evaluated to 103.041409432 meter / second (Allowable error: 0.0001%, Actual error: 0.16%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585924973 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573144914 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 0.314645033964 meter ** 2 / second ** 2 but the right hand side evaluated to 0.3146298952 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 0.168936438408 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931603974 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 0.0639642380864 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631379987 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 0.0226356535431 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354005879 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)
Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.638 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.587 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 1.24 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 41.7 seconds.
Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006568341 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%)
Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544539109 meter * revolutions_per_minute but the right hand side evaluated to 103.041408191 meter / second (Allowable error: 0.0001%, Actual error: 0.16%)
Warning: Constraint [dQ_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [N*m]... >= B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement_...] is not tight because the left hand side evaluated to 74.5041627751 meter * newton but the right hand side evaluated to 74.5040725471 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%)
Warning: Constraint [-B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement... >= dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [lbf]...] is not tight because the left hand side evaluated to 134.449579759 kilogram * meter / second ** 2 but the right hand side evaluated to 30.2255018449 force_pound (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585903433 meter ** 2 / second ** 2 but the right hand side evaluated to 0.42057303321 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0031%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.314644998908 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629685653 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0049%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.16893640237 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931506563 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.063964051843 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639630073546 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0016%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226356673111 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226353930664 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0012%)
Using solver 'mosek'
Solving for 13 variables.
Solving took 0.225 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 18.2 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 1619897.4138 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 5.44 seconds.
Warning: Constraint [omega_BladeElementProp/BladeElementPerf_(0,)*r_BladeElementProp/BladeElementPerf_(0,) [m*rpm]... >= Wt_BladeElementProp/BladeElementPerf_(0,) + vt_BladeElementProp/BladeElementPerf_(0,) [m/s]...] is not tight because the left hand side evaluated to 147.268875342 meter * revolutions_per_minute but the right hand side evaluated to 15.4219435408 meter / second (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Constraint [dQ_BladeElementProp/BladeElementPerf_(3,) [N*m]... >= B_BladeElementProp/BladeElementPerf_(3,)*G_BladeElementProp/BladeElementPerf_(3,)*Wa_BladeElementPro...] is not tight because the left hand side evaluated to 42.7884411703 meter * newton but the right hand side evaluated to 42.7884887635 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%)
Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3481 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9721 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3856 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9562 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.2729 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.1579 but bound is 700000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Running tests...
----------------------------------------------------------------------
..........
----------------------------------------------------------------------
Ran 10 tests in 128.222s
OK
Generating XML reports...
Cloning into 'eVTOL'...
adding test for 'aircraft_models.py'
Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 2.429s
OK
Generating XML reports...
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {})
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})
calling ['pip', 'install', 'pandas']
attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})
calling ['pip', 'install', 'pandas']
attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'})
calling ['pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})
calling ['pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'})
calling ['pip', 'install', 'pandas']
attempt 1
calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
attempt 1
calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
attempt 1
calling ['pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'})
calling ['pip', 'install', 'pandas']
attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
attempt 1
calling ['pip', 'install', '.']
attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
attempt 1
SETTINGS
defaultdict(<type 'str'>, {})
(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>exit 0
Build step 'Console output (build log) parsing' changed build result to FAILURE
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'D:\jenkins\workspace\gplibrary_PR_Models\mosek' for the testing framework 'JUnit'.
[xUnit] [INFO] - Check 'Failed Tests' threshold.
[xUnit] [INFO] - Check 'Skipped Tests' threshold.
[xUnit] [INFO] - Setting the build status to FAILURE
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: FAILURE
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