Skipping 33 KB..
Full LogRequirement 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-h0nsjc\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: gpfit
Successfully installed gpfit-0.1
Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gassolar
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.2)
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-bqb60g\wheels\08\33\b8\d36cec4e8239569444cd725d0dbfe83a0cfc534951775e5535
Successfully built gassolar
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: gassolar
Successfully installed gassolar-0.0.0.0
adding test for 'gassolar/gas/gas.py'
adding test for 'gassolar/solar/solar.py'
Using solver 'mosek'
Solving for 592 variables.
Solving took 0.185 seconds.
Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Beginning signomial solve.
Solving took 4 GP solves and 4.19 seconds.
Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Using solver 'mosek'
Solving for 592 variables.
Solving took 0.277 seconds.
Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Beginning signomial solve.
Solving took 4 GP solves and 6.16 seconds.
Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Using solver 'mosek'
Solving for 1250 variables.
Solving took 0.511 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1496 but bound is 150000.0000
Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.1345 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 7.2 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0580 but bound is 150000.0000
Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.9086 but bound is 150000.0000
Using solver 'mosek_cli'
Solving for 1250 variables.
Solving took 0.682 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.0147 but bound is 150000.0000
Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.3302 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 16 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134552.5355 but bound is 150000.0000
Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.8810 but bound is 150000.0000
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)
..
----------------------------------------------------------------------
Ran 4 tests in 78.242s
OK
Generating XML reports...
Cloning into 'jho'...
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) (1.14.2)
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-lqdw4u
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) (1.14.2)
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-aqklxx\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 -5.080267803658778e-14.
Allowing negative dual variable(s) as small as -7.71518265940685e-14.
Allowing negative dual variable(s) as small as -1.5210792694841935e-13.
Allowing negative dual variable(s) as small as -1.4981158674709505e-13.
Solving took 4 GP solves and 4.49 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.1423709040987475e-14.
Allowing negative dual variable(s) as small as -7.687210243356724e-14.
Allowing negative dual variable(s) as small as -1.51310821511208e-13.
Allowing negative dual variable(s) as small as -1.4949933652141922e-13.
Solving took 4 GP solves and 5.55 seconds.
Allowing negative dual variable(s) as small as -5.168088179630104e-13.
Allowing negative dual variable(s) as small as -1.432036780824042e-12.
Allowing negative dual variable(s) as small as -4.431767453016988e-13.
Allowing negative dual variable(s) as small as -4.450866758487493e-13.
Allowing negative dual variable(s) as small as -1.2978605820265776e-12.
Allowing negative dual variable(s) as small as -1.0908599327660862e-12.
Allowing negative dual variable(s) as small as -1.0899060516947334e-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 -2.445910401469118e-14.
Allowing negative dual variable(s) as small as -5.696060652471709e-12.
Allowing negative dual variable(s) as small as -2.0879038473938932e-11.
Allowing negative dual variable(s) as small as -2.088076471228883e-11.
Solving took 4 GP solves and 14.3 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.25 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.153030779858625e-13.
Allowing negative dual variable(s) as small as -1.4308606383073297e-12.
Allowing negative dual variable(s) as small as -4.444274809278781e-13.
Allowing negative dual variable(s) as small as -4.4511963559479284e-13.
Allowing negative dual variable(s) as small as -1.2966054011714911e-12.
Allowing negative dual variable(s) as small as -1.0917407386110134e-12.
Allowing negative dual variable(s) as small as -1.0910146484160999e-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 -2.3941039711788254e-14.
Allowing negative dual variable(s) as small as -5.696115113143267e-12.
Allowing negative dual variable(s) as small as -2.0878937322852558e-11.
Allowing negative dual variable(s) as small as -2.088080902304399e-11.
Solving took 4 GP solves and 5.22 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.03 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Running tests...
----------------------------------------------------------------------
....
----------------------------------------------------------------------
Ran 4 tests in 131.183s
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) (1.14.2)
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-mbdeny\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 3.873s
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-jnms30
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) (1.14.2)
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-gbgteh\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 : 0.00
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 : 826
Optimizer - Cones : 0
Optimizer - Scalar variables : 3575 conic : 0
Optimizer - Semi-definite variables: 0 scalarized : 0
Factor - setup time : 0.08 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.05
Factor - nonzeros before factor : 1.67e+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 0.13
1 1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.268199332e+005 3.700570996e+000 4.8e-001 0.73
2 3.9e+002 5.0e+002 2.2e+004 -9.36e-001 -1.196731173e+005 1.153832762e+001 1.7e-001 1.69
3 2.8e+002 3.7e+002 1.6e+004 -8.23e-001 -1.157725499e+005 8.911193657e+001 1.2e-001 1.73
4 2.8e+002 3.6e+002 1.6e+004 -7.55e-001 -1.127836302e+005 2.530618096e+003 1.2e-001 1.78
5 6.9e+001 9.0e+001 3.9e+003 -7.46e-001 -7.044561375e+004 1.168298555e+004 3.1e-002 1.83
6 3.1e+001 4.1e+001 1.8e+003 -1.39e-001 -4.096532654e+004 1.098732371e+004 1.4e-002 1.86
7 1.6e+001 2.1e+001 9.1e+002 3.72e-001 -2.384884033e+004 6.701248905e+003 7.2e-003 2.00
8 7.3e+000 9.5e+000 4.1e+002 6.70e-001 -1.130515668e+004 3.761163374e+003 3.3e-003 2.03
9 3.4e+000 4.4e+000 1.9e+002 8.75e-001 -5.068498667e+003 2.154890886e+003 1.5e-003 2.17
10 1.7e+000 2.2e+000 9.8e+001 9.56e-001 -2.274239213e+003 1.449630149e+003 7.8e-004 2.64
11 6.5e-001 8.4e-001 3.7e+001 9.85e-001 -6.386409604e+002 7.708877882e+002 2.9e-004 2.71
12 5.5e-001 7.6e-001 3.2e+001 9.80e-001 -4.977186201e+002 7.157125316e+002 2.5e-004 3.98
13 3.9e-001 9.4e-001 2.2e+001 9.74e-001 -2.511527669e+002 6.146396419e+002 1.8e-004 4.03
14 2.1e-001 6.0e-001 1.2e+001 9.86e-001 2.118551311e+001 4.971611734e+002 9.8e-005 4.07
15 6.4e-002 2.4e-001 3.8e+000 1.00e+000 2.547904550e+002 4.008091633e+002 3.1e-005 4.12
16 2.0e-002 1.4e-001 1.2e+000 1.00e+000 3.243515273e+002 3.710547149e+002 9.9e-006 4.15
17 4.6e-003 1.5e-001 2.8e-001 1.00e+000 3.496092054e+002 3.605442939e+002 2.4e-006 4.29
18 2.7e-003 1.2e-001 1.7e-001 1.00e+000 3.526527396e+002 3.591730387e+002 1.4e-006 4.34
19 6.5e-004 1.3e-001 4.1e-002 9.94e-001 3.562031755e+002 3.577903302e+002 3.5e-007 4.37
20 2.4e-004 9.9e-002 1.5e-002 9.98e-001 3.569203947e+002 3.575142357e+002 1.3e-007 4.42
21 1.2e-004 7.9e-002 7.5e-003 1.00e+000 3.571413806e+002 3.574309325e+002 6.3e-008 4.46
22 1.1e-004 7.2e-002 6.8e-003 1.00e+000 3.571621286e+002 3.574227098e+002 5.7e-008 4.49
23 9.5e-005 6.6e-002 6.1e-003 1.00e+000 3.571807621e+002 3.574152867e+002 5.1e-008 5.40
24 8.6e-005 6.0e-002 5.5e-003 1.00e+000 3.571975379e+002 3.574086184e+002 4.6e-008 6.94
25 7.7e-005 5.4e-002 4.9e-003 1.00e+000 3.572126371e+002 3.574026145e+002 4.2e-008 8.00
26 7.0e-005 4.9e-002 4.4e-003 1.00e+000 3.572262247e+002 3.573972063e+002 3.7e-008 8.39
27 6.3e-005 4.5e-002 4.0e-003 1.00e+000 3.572384517e+002 3.573923352e+002 3.4e-008 8.47
28 5.6e-005 4.1e-002 3.6e-003 1.00e+000 3.572494550e+002 3.573879495e+002 3.0e-008 8.50
29 5.1e-005 3.8e-002 3.2e-003 1.00e+000 3.572593579e+002 3.573840020e+002 2.7e-008 8.55
30 4.6e-005 3.5e-002 2.9e-003 1.00e+000 3.572682711e+002 3.573804497e+002 2.5e-008 8.60
31 4.1e-005 3.2e-002 2.6e-003 1.00e+000 3.572762938e+002 3.573772537e+002 2.2e-008 8.63
32 3.7e-005 2.9e-002 2.4e-003 1.00e+000 3.572835153e+002 3.573743784e+002 2.0e-008 8.67
33 3.3e-005 2.7e-002 2.1e-003 1.00e+000 3.572900159e+002 3.573717920e+002 1.8e-008 8.71
34 3.0e-005 2.5e-002 1.9e-003 1.00e+000 3.572958675e+002 3.573694655e+002 1.6e-008 8.74
35 2.7e-005 2.3e-002 1.7e-003 1.00e+000 3.573011351e+002 3.573673728e+002 1.4e-008 8.77
36 2.4e-005 2.2e-002 1.5e-003 1.00e+000 3.573058769e+002 3.573654906e+002 1.3e-008 8.81
37 2.2e-005 2.0e-002 1.4e-003 1.00e+000 3.573101455e+002 3.573637976e+002 1.2e-008 8.85
38 2.0e-005 1.9e-002 1.3e-003 1.00e+000 3.573139881e+002 3.573622748e+002 1.1e-008 8.88
39 1.8e-005 1.8e-002 1.1e-003 1.00e+000 3.573174472e+002 3.573609051e+002 9.5e-009 8.92
40 1.6e-005 1.7e-002 1.0e-003 1.00e+000 3.573205611e+002 3.573596730e+002 8.6e-009 8.95
41 1.4e-005 1.6e-002 9.1e-004 1.00e+000 3.573233641e+002 3.573585648e+002 7.7e-009 8.99
42 1.3e-005 1.5e-002 8.2e-004 1.00e+000 3.573258873e+002 3.573575679e+002 6.9e-009 9.03
43 1.2e-005 1.4e-002 7.4e-004 1.00e+000 3.573281586e+002 3.573566712e+002 6.2e-009 9.06
44 1.0e-005 1.3e-002 6.7e-004 1.00e+000 3.573302032e+002 3.573558645e+002 5.6e-009 9.10
45 9.4e-006 1.3e-002 6.0e-004 1.00e+000 3.573320436e+002 3.573551388e+002 5.1e-009 9.13
46 8.5e-006 1.2e-002 5.4e-004 1.00e+000 3.573337002e+002 3.573544859e+002 4.5e-009 9.17
47 7.6e-006 1.2e-002 4.9e-004 1.00e+000 3.573351914e+002 3.573538985e+002 4.1e-009 9.20
48 6.9e-006 1.1e-002 4.4e-004 1.00e+000 3.573365336e+002 3.573533701e+002 3.7e-009 9.25
49 6.2e-006 1.1e-002 3.9e-004 1.00e+000 3.573377418e+002 3.573528946e+002 3.3e-009 9.28
50 5.6e-006 1.0e-002 3.5e-004 1.00e+000 3.573388292e+002 3.573524667e+002 3.0e-009 9.33
51 5.0e-006 1.0e-002 3.2e-004 1.00e+000 3.573398079e+002 3.573520818e+002 2.7e-009 9.36
52 4.5e-006 9.8e-003 2.9e-004 1.00e+000 3.573406889e+002 3.573517354e+002 2.4e-009 9.41
53 4.0e-006 9.5e-003 2.6e-004 1.00e+000 3.573414818e+002 3.573514236e+002 2.2e-009 9.45
54 3.6e-006 9.3e-003 2.3e-004 1.00e+000 3.573421954e+002 3.573511430e+002 2.0e-009 9.48
55 3.3e-006 9.1e-003 2.1e-004 1.00e+000 3.573428376e+002 3.573508905e+002 1.8e-009 9.52
56 3.0e-006 8.9e-003 1.9e-004 1.00e+000 3.573434156e+002 3.573506633e+002 1.6e-009 9.56
57 2.7e-006 8.7e-003 1.7e-004 1.00e+000 3.573439358e+002 3.573504588e+002 1.4e-009 9.59
58 2.4e-006 8.6e-003 1.5e-004 1.00e+000 3.573444040e+002 3.573502746e+002 1.3e-009 9.63
59 2.2e-006 8.5e-003 1.4e-004 1.00e+000 3.573448253e+002 3.573501089e+002 1.2e-009 9.67
60 1.9e-006 8.3e-003 1.2e-004 1.00e+000 3.573452045e+002 3.573499598e+002 1.0e-009 9.70
61 1.7e-006 8.2e-003 1.1e-004 1.00e+000 3.573455458e+002 3.573498255e+002 9.4e-010 9.75
62 1.6e-006 8.1e-003 1.0e-004 1.00e+000 3.573458529e+002 3.573497046e+002 8.4e-010 9.80
63 1.4e-006 8.1e-003 9.0e-005 1.00e+000 3.573461293e+002 3.573495959e+002 7.6e-010 9.83
64 1.3e-006 8.0e-003 8.1e-005 1.00e+000 3.573463780e+002 3.573494979e+002 6.8e-010 9.86
65 1.1e-006 7.9e-003 7.3e-005 1.00e+000 3.573466018e+002 3.573494098e+002 6.1e-010 9.91
66 1.0e-006 7.8e-003 6.6e-005 1.00e+000 3.573468033e+002 3.573493304e+002 5.5e-010 9.94
67 9.3e-007 7.8e-003 5.9e-005 1.00e+000 3.573469846e+002 3.573492590e+002 5.0e-010 9.97
68 8.3e-007 7.7e-003 5.3e-005 1.00e+000 3.573471477e+002 3.573491947e+002 4.5e-010 10.02
69 7.5e-007 7.7e-003 4.8e-005 1.00e+000 3.573472945e+002 3.573491369e+002 4.0e-010 10.05
70 6.8e-007 7.6e-003 4.3e-005 1.00e+000 3.573474267e+002 3.573490848e+002 3.6e-010 10.08
71 6.1e-007 7.6e-003 3.9e-005 1.00e+000 3.573475456e+002 3.573490379e+002 3.3e-010 10.12
72 5.5e-007 7.6e-003 3.5e-005 1.00e+000 3.573476526e+002 3.573489956e+002 2.9e-010 10.16
73 4.9e-007 7.5e-003 3.1e-005 1.00e+000 3.573477489e+002 3.573489576e+002 2.6e-010 10.20
74 4.4e-007 7.5e-003 2.8e-005 9.99e-001 3.573478355e+002 3.573489234e+002 2.4e-010 10.23
75 4.0e-007 7.5e-003 2.5e-005 1.00e+000 3.573479135e+002 3.573488926e+002 2.1e-010 10.27
76 3.6e-007 7.4e-003 2.3e-005 9.99e-001 3.573479836e+002 3.573488648e+002 1.9e-010 10.31
77 3.2e-007 7.4e-003 2.1e-005 1.00e+000 3.573480467e+002 3.573488399e+002 1.7e-010 10.34
78 2.9e-007 7.4e-003 1.9e-005 1.00e+000 3.573481036e+002 3.573488173e+002 1.6e-010 10.37
79 2.6e-007 7.4e-003 1.7e-005 1.00e+000 3.573481547e+002 3.573487971e+002 1.4e-010 10.42
80 2.4e-007 7.4e-003 1.5e-005 1.00e+000 3.573482007e+002 3.573487788e+002 1.3e-010 10.45
81 2.1e-007 7.4e-003 1.3e-005 9.99e-001 3.573482421e+002 3.573487624e+002 1.1e-010 10.48
82 1.9e-007 7.3e-003 1.2e-005 1.00e+000 3.573482794e+002 3.573487476e+002 1.0e-010 10.53
83 1.7e-007 7.3e-003 1.1e-005 9.99e-001 3.573483130e+002 3.573487343e+002 9.2e-011 10.56
84 1.5e-007 7.3e-003 9.8e-006 9.99e-001 3.573483431e+002 3.573487223e+002 8.3e-011 10.59
85 1.4e-007 7.3e-003 8.9e-006 9.98e-001 3.573483702e+002 3.573487116e+002 7.5e-011 10.64
86 1.3e-007 7.3e-003 8.0e-006 9.98e-001 3.573483947e+002 3.573487019e+002 6.7e-011 10.67
87 1.1e-007 7.3e-003 7.2e-006 1.00e+000 3.573484166e+002 3.573486931e+002 6.1e-011 10.70
88 1.0e-007 7.3e-003 6.5e-006 9.98e-001 3.573484364e+002 3.573486853e+002 5.4e-011 10.75
89 9.1e-008 7.3e-003 5.8e-006 9.98e-001 3.573484542e+002 3.573486782e+002 4.9e-011 10.78
90 8.2e-008 7.2e-003 5.2e-006 1.00e+000 3.573484702e+002 3.573486718e+002 4.4e-011 10.81
91 7.4e-008 7.2e-003 4.7e-006 9.97e-001 3.573484846e+002 3.573486661e+002 4.0e-011 10.86
92 6.6e-008 7.2e-003 4.2e-006 9.98e-001 3.573484976e+002 3.573486609e+002 3.6e-011 10.89
93 6.0e-008 7.2e-003 3.8e-006 9.99e-001 3.573485093e+002 3.573486563e+002 3.2e-011 10.92
94 6.6e-009 7.7e-004 4.1e-007 9.99e-001 3.573486032e+002 3.573486189e+002 3.5e-012 10.97
95 5.9e-009 6.9e-004 3.7e-007 1.03e+000 3.573486044e+002 3.573486184e+002 3.2e-012 11.00
96 5.3e-009 6.2e-004 3.3e-007 1.05e+000 3.573486057e+002 3.573486178e+002 2.9e-012 12.53
97 4.7e-009 5.6e-004 3.0e-007 9.35e-001 3.573486065e+002 3.573486175e+002 2.6e-012 12.56
98 4.3e-009 5.1e-004 2.7e-007 1.02e+000 3.573486074e+002 3.573486172e+002 2.4e-012 12.62
99 3.9e-009 4.5e-004 2.4e-007 1.00e+000 3.573486081e+002 3.573486169e+002 2.2e-012 12.65
100 3.5e-009 4.1e-004 2.2e-007 9.97e-001 3.573486087e+002 3.573486166e+002 1.9e-012 12.68
101 3.6e-010 4.2e-005 2.2e-008 9.99e-001 3.573486138e+002 3.573486146e+002 2.0e-013 12.82
Interior-point optimizer terminated. Time: 12.84.
Optimizer terminated. Time: 12.86
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 3.5734861380e+002 Viol. con: 5e-009 var: 0e+000
Dual. obj: 3.5734861461e+002 Viol. con: 0e+000 var: 3e-004
* End solution on dual form. *
Transforming to primal solution.
Solving took 12.9 seconds.
result packing took 2.8% of solve time
solution checking took 1.5% 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 : 0.03 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 -1.289236955e+005 2.000000000e+000 1.0e+000 0.08
1 1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.266796380e+005 3.803741916e+000 4.7e-001 0.90
2 4.4e+002 5.7e+002 2.5e+004 -9.35e-001 -1.208018327e+005 1.084180419e+001 1.9e-001 0.95
3 2.9e+002 3.7e+002 1.6e+004 -8.43e-001 -1.159551820e+005 6.141738318e+001 1.3e-001 1.00
4 2.9e+002 3.7e+002 1.6e+004 -7.60e-001 -1.137633315e+005 1.946615931e+003 1.3e-001 1.03
5 8.6e+001 1.1e+002 4.9e+003 -7.56e-001 -7.873935576e+004 1.029432233e+004 3.8e-002 1.06
6 2.8e+001 3.7e+001 1.6e+003 -2.75e-001 -3.706555808e+004 1.220641405e+004 1.3e-002 1.09
7 1.4e+001 1.8e+001 7.7e+002 4.35e-001 -2.030610938e+004 6.163510527e+003 6.0e-003 1.29
8 7.6e+000 9.8e+000 4.3e+002 7.35e-001 -1.180277788e+004 3.699008504e+003 3.4e-003 1.33
9 2.9e+000 3.7e+000 1.6e+002 8.69e-001 -4.542673700e+003 1.611196655e+003 1.3e-003 1.37
10 1.4e+000 1.8e+000 7.9e+001 9.69e-001 -2.009243310e+003 9.676512207e+002 6.2e-004 1.40
11 9.6e-001 1.2e+000 5.5e+001 9.89e-001 -1.381424703e+003 6.944429219e+002 4.3e-004 2.00
12 8.4e-001 1.1e+000 4.8e+001 9.74e-001 -1.220087282e+003 6.089999086e+002 3.8e-004 3.40
13 3.5e-001 4.5e-001 2.0e+001 9.84e-001 -4.954236510e+002 2.767217312e+002 1.6e-004 5.30
14 1.9e-001 2.6e-001 1.1e+001 1.01e+000 -2.548056990e+002 1.739607574e+002 8.8e-005 6.89
15 7.8e-002 1.3e-001 4.5e+000 9.99e-001 -8.254141363e+001 9.184536852e+001 3.6e-005 8.27
16 2.3e-002 1.1e-001 1.4e+000 1.00e+000 -6.418944435e-001 5.294700612e+001 1.1e-005 9.56
17 1.5e-002 8.3e-002 8.7e-001 1.00e+000 1.306801378e+001 4.649503146e+001 7.1e-006 10.64
18 2.8e-003 1.4e-001 1.7e-001 1.00e+000 3.161968083e+001 3.829724885e+001 1.4e-006 10.69
19 1.4e-003 9.8e-002 8.9e-002 1.00e+000 3.387241740e+001 3.730606050e+001 7.5e-007 10.72
20 4.6e-004 1.0e-001 2.8e-002 1.00e+000 3.549089982e+001 3.658198539e+001 2.4e-007 10.75
21 2.1e-004 7.9e-002 1.3e-002 1.00e+000 3.589091177e+001 3.640150283e+001 1.1e-007 10.78
22 1.9e-004 7.1e-002 1.2e-002 1.00e+000 3.592727626e+001 3.638679960e+001 1.0e-007 10.83
23 1.7e-004 6.5e-002 1.1e-002 1.00e+000 3.595898436e+001 3.637252545e+001 9.1e-008 10.86
24 1.6e-004 5.9e-002 9.7e-003 1.00e+000 3.598754627e+001 3.635971097e+001 8.1e-008 10.90
25 1.4e-004 5.4e-002 8.7e-003 1.00e+000 3.601322089e+001 3.634815041e+001 7.3e-008 10.94
26 1.3e-004 4.9e-002 7.9e-003 1.00e+000 3.603630979e+001 3.633773098e+001 6.6e-008 11.64
27 1.1e-004 4.5e-002 7.1e-003 1.00e+000 3.605707475e+001 3.632834118e+001 5.9e-008 13.03
28 1.0e-004 4.1e-002 6.4e-003 1.00e+000 3.607575113e+001 3.631988057e+001 5.3e-008 13.82
29 9.2e-005 3.8e-002 5.7e-003 1.00e+000 3.609255017e+001 3.631225819e+001 4.8e-008 13.85
30 8.3e-005 3.5e-002 5.2e-003 1.00e+000 3.610766153e+001 3.630539185e+001 4.3e-008 13.90
31 7.4e-005 3.2e-002 4.6e-003 1.00e+000 3.612125552e+001 3.629920720e+001 3.9e-008 13.93
32 6.7e-005 3.0e-002 4.2e-003 1.00e+000 3.613348510e+001 3.629363705e+001 3.5e-008 13.96
33 6.0e-005 2.7e-002 3.8e-003 1.00e+000 3.614448769e+001 3.628862075e+001 3.2e-008 13.99
34 5.4e-005 2.5e-002 3.4e-003 1.00e+000 3.615438676e+001 3.628410354e+001 2.8e-008 14.02
35 4.9e-005 2.3e-002 3.1e-003 1.00e+000 3.616329330e+001 3.628003601e+001 2.6e-008 14.06
36 4.4e-005 2.2e-002 2.7e-003 1.00e+000 3.617130707e+001 3.627637359e+001 2.3e-008 14.09
37 3.9e-005 2.0e-002 2.5e-003 1.00e+000 3.617851777e+001 3.627307608e+001 2.1e-008 14.12
38 3.6e-005 1.9e-002 2.2e-003 1.00e+000 3.618500603e+001 3.627010729e+001 1.9e-008 14.15
39 3.2e-005 1.8e-002 2.0e-003 1.00e+000 3.619084436e+001 3.626743452e+001 1.7e-008 14.18
40 2.9e-005 1.7e-002 1.8e-003 1.00e+000 3.619609799e+001 3.626502835e+001 1.5e-008 14.21
41 2.6e-005 1.6e-002 1.6e-003 1.00e+000 3.620082556e+001 3.626286227e+001 1.4e-008 14.24
42 2.3e-005 1.5e-002 1.5e-003 1.00e+000 3.620507980e+001 3.626091237e+001 1.2e-008 14.27
43 2.1e-005 1.4e-002 1.3e-003 1.00e+000 3.620890817e+001 3.625915710e+001 1.1e-008 14.31
44 1.9e-005 1.3e-002 1.2e-003 1.00e+000 3.621235333e+001 3.625757707e+001 9.9e-009 14.32
45 1.7e-005 1.3e-002 1.1e-003 1.00e+000 3.621545367e+001 3.625615481e+001 8.9e-009 14.88
46 1.5e-005 1.2e-002 9.6e-004 1.00e+000 3.621824372e+001 3.625487457e+001 8.0e-009 18.19
47 1.4e-005 1.2e-002 8.6e-004 1.00e+000 3.622075456e+001 3.625372219e+001 7.2e-009 18.20
48 1.2e-005 1.1e-002 7.8e-004 1.00e+000 3.622301412e+001 3.625268488e+001 6.5e-009 18.22
49 1.1e-005 1.1e-002 7.0e-004 1.00e+000 3.622504757e+001 3.625175118e+001 5.9e-009 18.24
50 1.0e-005 1.1e-002 6.3e-004 1.00e+000 3.622687753e+001 3.625091073e+001 5.3e-009 18.27
51 9.0e-006 1.0e-002 5.7e-004 1.00e+000 3.622852436e+001 3.625015420e+001 4.7e-009 18.28
52 8.1e-006 9.9e-003 5.1e-004 1.00e+000 3.623000639e+001 3.624947323e+001 4.3e-009 18.31
53 7.3e-006 9.6e-003 4.6e-004 1.00e+000 3.623134011e+001 3.624886027e+001 3.8e-009 18.53
54 6.6e-006 9.4e-003 4.1e-004 1.00e+000 3.623254037e+001 3.624830850e+001 3.5e-009 18.56
55 5.9e-006 9.2e-003 3.7e-004 1.00e+000 3.623362051e+001 3.624781183e+001 3.1e-009 18.58
56 5.3e-006 9.0e-003 3.3e-004 1.00e+000 3.623459255e+001 3.624736475e+001 2.8e-009 18.61
57 4.8e-006 8.8e-003 3.0e-004 1.00e+000 3.623546732e+001 3.624696230e+001 2.5e-009 18.63
58 4.3e-006 8.6e-003 2.7e-004 1.00e+000 3.623625454e+001 3.624660003e+001 2.3e-009 18.66
59 3.9e-006 8.5e-003 2.4e-004 1.00e+000 3.623696298e+001 3.624627393e+001 2.0e-009 21.39
60 3.5e-006 8.4e-003 2.2e-004 1.00e+000 3.623760052e+001 3.624598039e+001 1.8e-009 22.00
61 3.1e-006 8.3e-003 2.0e-004 1.00e+000 3.623817426e+001 3.624571615e+001 1.7e-009 22.78
62 2.8e-006 8.1e-003 1.8e-004 1.00e+000 3.623869058e+001 3.624547828e+001 1.5e-009 24.13
63 2.6e-006 8.1e-003 1.6e-004 1.00e+000 3.623915522e+001 3.624526418e+001 1.3e-009 25.93
64 2.3e-006 8.0e-003 1.4e-004 1.00e+000 3.623957337e+001 3.624507142e+001 1.2e-009 27.97
65 2.1e-006 7.9e-003 1.3e-004 1.00e+000 3.623994967e+001 3.624489792e+001 1.1e-009 29.20
66 1.9e-006 7.8e-003 1.2e-004 1.00e+000 3.624028831e+001 3.624474175e+001 9.8e-010 30.45
67 1.7e-006 7.7e-003 1.0e-004 1.00e+000 3.624059307e+001 3.624460116e+001 8.8e-010 32.06
68 1.5e-006 7.7e-003 9.4e-005 1.00e+000 3.624086732e+001 3.624447460e+001 7.9e-010 32.18
69 1.4e-006 7.6e-003 8.5e-005 1.00e+000 3.624111413e+001 3.624436070e+001 7.1e-010 32.24
70 1.2e-006 7.6e-003 7.6e-005 1.00e+000 3.624133624e+001 3.624425816e+001 6.4e-010 32.31
71 1.1e-006 7.5e-003 6.9e-005 1.00e+000 3.624153612e+001 3.624416587e+001 5.8e-010 32.40
72 9.9e-007 7.5e-003 6.2e-005 1.00e+000 3.624171600e+001 3.624408277e+001 5.2e-010 33.65
73 8.9e-007 7.5e-003 5.6e-005 1.00e+000 3.624187788e+001 3.624400798e+001 4.7e-010 33.68
74 8.0e-007 7.4e-003 5.0e-005 1.00e+000 3.624202357e+001 3.624394066e+001 4.2e-010 33.70
75 7.2e-007 7.4e-003 4.5e-005 1.00e+000 3.624215468e+001 3.624388004e+001 3.8e-010 33.73
76 6.5e-007 7.4e-003 4.1e-005 1.00e+000 3.624227266e+001 3.624382550e+001 3.4e-010 33.76
77 5.8e-007 7.3e-003 3.7e-005 1.00e+000 3.624237884e+001 3.624377639e+001 3.1e-010 33.79
78 5.3e-007 7.3e-003 3.3e-005 1.00e+000 3.624247440e+001 3.624373219e+001 2.8e-010 33.81
79 4.7e-007 7.3e-003 3.0e-005 1.00e+000 3.624256039e+001 3.624369241e+001 2.5e-010 33.84
80 4.3e-007 7.3e-003 2.7e-005 1.00e+000 3.624263778e+001 3.624365661e+001 2.2e-010 33.85
81 3.8e-007 7.2e-003 2.4e-005 1.00e+000 3.624270743e+001 3.624362437e+001 2.0e-010 33.88
82 3.4e-007 7.2e-003 2.2e-005 1.00e+000 3.624277011e+001 3.624359536e+001 1.8e-010 33.91
83 3.1e-007 7.2e-003 1.9e-005 1.00e+000 3.624282652e+001 3.624356925e+001 1.6e-010 33.93
84 2.8e-007 7.2e-003 1.7e-005 1.00e+000 3.624287728e+001 3.624354573e+001 1.5e-010 33.96
85 2.5e-007 7.2e-003 1.6e-005 1.00e+000 3.624292297e+001 3.624352456e+001 1.3e-010 33.98
86 2.3e-007 7.2e-003 1.4e-005 1.00e+000 3.624296409e+001 3.624350551e+001 1.2e-010 34.01
87 2.0e-007 7.2e-003 1.3e-005 1.00e+000 3.624300109e+001 3.624348838e+001 1.1e-010 34.02
88 1.8e-007 7.1e-003 1.1e-005 1.00e+000 3.624303439e+001 3.624347294e+001 9.6e-011 34.09
89 1.6e-007 7.1e-003 1.0e-005 9.99e-001 3.624306435e+001 3.624345907e+001 8.7e-011 34.13
90 1.5e-007 7.1e-003 9.3e-006 1.00e+000 3.624309132e+001 3.624344656e+001 7.8e-011 34.18
91 1.3e-007 7.1e-003 8.4e-006 1.00e+000 3.624311560e+001 3.624343531e+001 7.0e-011 34.24
92 1.2e-007 7.1e-003 7.5e-006 9.99e-001 3.624313744e+001 3.624342519e+001 6.3e-011 34.29
93 1.1e-007 7.1e-003 6.8e-006 1.00e+000 3.624315710e+001 3.624341606e+001 5.7e-011 34.32
94 9.7e-008 7.1e-003 6.1e-006 9.99e-001 3.624317479e+001 3.624340787e+001 5.1e-011 34.35
95 8.8e-008 7.1e-003 5.5e-006 1.00e+000 3.624319071e+001 3.624340048e+001 4.6e-011 34.38
96 7.9e-008 7.1e-003 4.9e-006 1.00e+000 3.624320505e+001 3.624339381e+001 4.1e-011 34.40
97 7.1e-008 7.1e-003 4.4e-006 1.00e+000 3.624321795e+001 3.624338783e+001 3.7e-011 34.43
98 6.4e-008 7.0e-003 4.0e-006 1.00e+000 3.624322955e+001 3.624338245e+001 3.4e-011 34.46
99 5.7e-008 7.0e-003 3.6e-006 1.00e+000 3.624324000e+001 3.624337759e+001 3.0e-011 34.49
100 5.2e-008 7.0e-003 3.2e-006 1.00e+000 3.624324940e+001 3.624337323e+001 2.7e-011 34.51
101 4.7e-008 7.0e-003 2.9e-006 9.99e-001 3.624325786e+001 3.624336931e+001 2.4e-011 34.74
102 4.2e-008 7.0e-003 2.6e-006 1.00e+000 3.624326547e+001 3.624336577e+001 2.2e-011 34.77
103 3.8e-008 7.0e-003 2.4e-006 1.00e+000 3.624327232e+001 3.624336259e+001 2.0e-011 34.82
104 3.4e-008 6.3e-003 2.1e-006 1.00e+000 3.624327858e+001 3.624335967e+001 1.8e-011 34.85
105 3.1e-008 5.7e-003 1.9e-006 9.98e-001 3.624328411e+001 3.624335711e+001 1.6e-011 34.88
106 2.7e-008 5.1e-003 1.7e-006 1.00e+000 3.624328910e+001 3.624335479e+001 1.4e-011 34.91
107 2.5e-008 4.6e-003 1.5e-006 9.97e-001 3.624329358e+001 3.624335272e+001 1.3e-011 34.94
108 2.2e-008 4.1e-003 1.4e-006 9.95e-001 3.624329762e+001 3.624335085e+001 1.2e-011 34.98
109 2.0e-008 3.7e-003 1.3e-006 1.01e+000 3.624330135e+001 3.624334911e+001 1.1e-011 35.05
110 1.8e-008 3.4e-003 1.1e-006 9.90e-001 3.624330460e+001 3.624334761e+001 9.5e-012 35.07
111 1.6e-008 3.0e-003 1.0e-006 1.00e+000 3.624330754e+001 3.624334625e+001 8.6e-012 35.10
112 1.5e-008 2.7e-003 9.1e-007 1.00e+000 3.624331021e+001 3.624334500e+001 7.7e-012 35.13
113 1.3e-008 2.4e-003 8.2e-007 1.00e+000 3.624331259e+001 3.624334390e+001 6.9e-012 35.15
114 1.2e-008 2.2e-003 7.4e-007 1.00e+000 3.624331472e+001 3.624334290e+001 6.2e-012 35.18
115 1.1e-008 2.0e-003 6.7e-007 1.00e+000 3.624331665e+001 3.624334201e+001 5.6e-012 35.19
116 9.6e-009 1.8e-003 6.0e-007 9.99e-001 3.624331838e+001 3.624334121e+001 5.1e-012 35.24
117 8.6e-009 1.6e-003 5.4e-007 1.00e+000 3.624331994e+001 3.624334048e+001 4.6e-012 35.26
118 7.8e-009 1.4e-003 4.9e-007 1.00e+000 3.624332134e+001 3.624333983e+001 4.1e-012 35.29
119 7.0e-009 1.3e-003 4.4e-007 1.00e+000 3.624332261e+001 3.624333923e+001 3.7e-012 35.30
120 6.3e-009 1.2e-003 3.9e-007 1.00e+000 3.624332376e+001 3.624333870e+001 3.3e-012 35.33
121 5.7e-009 1.1e-003 3.5e-007 1.00e+000 3.624332478e+001 3.624333822e+001 3.0e-012 35.38
122 5.1e-009 9.5e-004 3.2e-007 1.00e+000 3.624332570e+001 3.624333779e+001 2.7e-012 35.41
123 4.6e-009 8.5e-004 2.9e-007 9.98e-001 3.624332653e+001 3.624333741e+001 2.4e-012 35.46
124 4.1e-009 7.7e-004 2.6e-007 9.99e-001 3.624332727e+001 3.624333707e+001 2.2e-012 35.49
125 3.7e-009 6.9e-004 2.3e-007 9.99e-001 3.624332794e+001 3.624333676e+001 2.0e-012 35.54
126 3.3e-009 6.2e-004 2.1e-007 1.00e+000 3.624332854e+001 3.624333648e+001 1.8e-012 35.57
127 3.0e-009 5.6e-004 1.9e-007 9.98e-001 3.624332908e+001 3.624333623e+001 1.6e-012 35.62
128 2.7e-009 5.0e-004 1.7e-007 9.97e-001 3.624332957e+001 3.624333600e+001 1.4e-012 35.65
129 2.4e-009 4.5e-004 1.5e-007 1.00e+000 3.624333001e+001 3.624333579e+001 1.3e-012 35.69
130 2.2e-009 4.1e-004 1.4e-007 9.96e-001 3.624333040e+001 3.624333561e+001 1.2e-012 35.72
131 2.0e-009 3.7e-004 1.2e-007 1.00e+000 3.624333076e+001 3.624333545e+001 1.0e-012 35.77
132 1.8e-009 3.3e-004 1.1e-007 1.00e+000 3.624333108e+001 3.624333530e+001 9.4e-013 35.80
Interior-point optimizer terminated. Time: 35.82.
Optimizer terminated. Time: 35.83
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 3.6243331082e+001 Viol. con: 3e-008 var: 0e+000
Dual. obj: 3.6243335296e+001 Viol. con: 0e+000 var: 3e-003
* End solution on dual form. *
Transforming to primal solution.
Solving took 35.9 seconds.
result packing took 0.98% of solve time
solution checking took 0.2% 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 : 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 : 0.05 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 -1.288863851e+005 2.000000000e+000 1.0e+000 0.11
1 1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.266339057e+005 3.774599262e+000 4.7e-001 0.16
2 4.2e+002 5.5e+002 2.4e+004 -9.35e-001 -1.204516295e+005 1.083248796e+001 1.9e-001 0.20
3 2.8e+002 3.7e+002 1.6e+004 -8.37e-001 -1.157870809e+005 6.665178357e+001 1.3e-001 0.45
4 2.8e+002 3.7e+002 1.6e+004 -7.58e-001 -1.132101893e+005 2.261947473e+003 1.2e-001 0.48
5 7.5e+001 9.8e+001 4.3e+003 -7.51e-001 -7.369911662e+004 1.114794070e+004 3.3e-002 0.53
6 3.0e+001 3.9e+001 1.7e+003 -1.92e-001 -3.984856262e+004 1.107249725e+004 1.3e-002 0.55
7 1.4e+001 1.8e+001 7.8e+002 3.92e-001 -2.070937035e+004 5.965041619e+003 6.1e-003 0.58
8 9.0e+000 1.2e+001 5.1e+002 7.29e-001 -1.410201946e+004 4.103527081e+003 4.0e-003 0.61
9 3.6e+000 4.7e+000 2.1e+002 8.34e-001 -5.837225058e+003 1.819161735e+003 1.6e-003 1.73
10 2.0e+000 2.6e+000 1.1e+002 9.52e-001 -2.940269237e+003 1.325304222e+003 8.9e-004 4.80
11 9.0e-001 1.2e+000 5.1e+001 9.84e-001 -1.324698496e+003 6.203743338e+002 4.1e-004 5.07
12 8.6e-001 1.2e+000 4.9e+001 9.64e-001 -1.286285096e+003 5.821375484e+002 3.9e-004 5.10
13 3.8e-001 5.3e-001 2.2e+001 9.81e-001 -5.626623022e+002 2.744796707e+002 1.7e-004 5.15
14 1.5e-001 2.3e-001 8.6e+000 1.00e+000 -2.179544166e+002 1.114771452e+002 6.9e-005 5.18
15 8.6e-002 1.5e-001 5.0e+000 1.00e+000 -1.179869660e+002 7.375585493e+001 4.0e-005 5.21
16 2.6e-002 1.2e-001 1.6e+000 1.00e+000 -2.807278562e+001 3.131489618e+001 1.3e-005 5.26
17 1.1e-002 9.3e-002 6.9e-001 1.00e+000 -5.276649947e+000 2.122045128e+001 5.7e-006 5.29
18 1.0e-002 8.5e-002 6.3e-001 1.01e+000 -3.410702961e+000 2.059177339e+001 5.2e-006 5.32
19 6.6e-003 6.5e-002 4.0e-001 1.01e+000 2.894601953e+000 1.822581800e+001 3.3e-006 5.35
20 4.5e-003 4.7e-002 2.8e-001 1.01e+000 6.709274040e+000 1.712856113e+001 2.3e-006 5.38
21 1.8e-003 5.9e-002 1.1e-001 1.01e+000 1.119391840e+001 1.545046065e+001 9.4e-007 5.41
22 1.0e-003 4.8e-002 6.2e-002 1.02e+000 1.264898616e+001 1.495383871e+001 5.1e-007 5.44
23 4.6e-004 5.4e-002 2.9e-002 1.02e+000 1.351661294e+001 1.458946296e+001 2.4e-007 5.46
24 2.6e-004 5.0e-002 1.6e-002 1.01e+000 1.385886780e+001 1.445533790e+001 1.4e-007 5.49
25 1.3e-004 5.2e-002 8.5e-003 1.01e+000 1.406163996e+001 1.437394304e+001 7.1e-008 5.51
26 9.0e-005 4.6e-002 5.6e-003 1.01e+000 1.413613393e+001 1.434341593e+001 4.7e-008 5.54
27 8.1e-005 4.2e-002 5.1e-003 1.00e+000 1.415438150e+001 1.434100898e+001 4.3e-008 5.57
28 7.3e-005 3.9e-002 4.6e-003 1.00e+000 1.416703040e+001 1.433496274e+001 3.8e-008 5.59
29 6.5e-005 3.6e-002 4.1e-003 1.00e+000 1.417864765e+001 1.432976680e+001 3.4e-008 5.62
30 5.9e-005 3.3e-002 3.7e-003 1.00e+000 1.418904914e+001 1.432503962e+001 3.1e-008 5.63
31 5.3e-005 3.0e-002 3.3e-003 1.00e+000 1.419838937e+001 1.432076735e+001 2.8e-008 5.66
32 4.8e-005 2.8e-002 3.0e-003 1.00e+000 1.420677430e+001 1.431690344e+001 2.5e-008 5.68
33 4.3e-005 2.6e-002 2.7e-003 1.00e+000 1.421430255e+001 1.431340975e+001 2.3e-008 5.71
34 3.9e-005 2.4e-002 2.4e-003 1.00e+000 1.422106264e+001 1.431025188e+001 2.0e-008 5.72
35 3.5e-005 2.2e-002 2.2e-003 1.00e+000 1.422713431e+001 1.430739880e+001 1.8e-008 5.76
36 3.1e-005 2.1e-002 2.0e-003 1.00e+000 1.423258903e+001 1.430482240e+001 1.7e-008 5.77
37 2.8e-005 2.0e-002 1.8e-003 1.00e+000 1.423749055e+001 1.430249679e+001 1.5e-008 5.80
38 2.5e-005 1.8e-002 1.6e-003 1.00e+000 1.424189575e+001 1.430039819e+001 1.3e-008 5.82
39 2.3e-005 1.7e-002 1.4e-003 1.00e+000 1.424585542e+001 1.429850541e+001 1.2e-008 5.85
40 2.0e-005 1.6e-002 1.3e-003 1.00e+000 1.424941499e+001 1.429679810e+001 1.1e-008 5.88
41 1.8e-005 1.5e-002 1.2e-003 1.00e+000 1.425261531e+001 1.429525866e+001 9.8e-009 5.91
42 1.7e-005 1.5e-002 1.0e-003 1.00e+000 1.425549289e+001 1.429387034e+001 8.8e-009 5.93
43 1.5e-005 1.4e-002 9.4e-004 1.00e+000 1.425808050e+001 1.429261894e+001 7.9e-009 5.94
44 1.3e-005 1.3e-002 8.5e-004 1.00e+000 1.426040734e+001 1.429149140e+001 7.1e-009 5.97
45 1.2e-005 1.3e-002 7.6e-004 1.00e+000 1.426249978e+001 1.429047459e+001 6.4e-009 5.99
46 1.1e-005 1.2e-002 6.9e-004 1.00e+000 1.426438149e+001 1.428955857e+001 5.8e-009 6.01
47 9.8e-006 1.2e-002 6.2e-004 1.00e+000 1.426607355e+001 1.428873299e+001 5.2e-009 6.02
48 8.8e-006 1.1e-002 5.6e-004 1.00e+000 1.426759518e+001 1.428798802e+001 4.7e-009 6.05
49 7.9e-006 1.1e-002 5.0e-004 1.00e+000 1.426896353e+001 1.428731628e+001 4.2e-009 9.11
50 7.1e-006 1.1e-002 4.5e-004 1.00e+000 1.427019382e+001 1.428671108e+001 3.8e-009 9.14
51 6.4e-006 1.0e-002 4.0e-004 1.00e+000 1.427130001e+001 1.428616529e+001 3.4e-009 9.16
52 5.8e-006 1.0e-002 3.6e-004 1.00e+000 1.427229468e+001 1.428567293e+001 3.1e-009 9.19
53 5.2e-006 9.7e-003 3.3e-004 1.00e+000 1.427318902e+001 1.428522947e+001 2.8e-009 9.20
54 4.7e-006 9.5e-003 3.0e-004 1.00e+000 1.427399326e+001 1.428482972e+001 2.5e-009 9.23
55 4.2e-006 9.3e-003 2.7e-004 1.00e+000 1.427471658e+001 1.428446951e+001 2.2e-009 9.27
56 3.8e-006 9.1e-003 2.4e-004 1.00e+000 1.427536719e+001 1.428414497e+001 2.0e-009 9.28
57 3.4e-006 9.0e-003 2.2e-004 1.00e+000 1.427595251e+001 1.428385245e+001 1.8e-009 9.31
58 3.1e-006 8.8e-003 1.9e-004 1.00e+000 1.427647905e+001 1.428358916e+001 1.6e-009 9.34
59 2.8e-006 8.7e-003 1.7e-004 9.99e-001 1.427695272e+001 1.428335229e+001 1.5e-009 9.36
60 2.5e-006 8.5e-003 1.6e-004 1.00e+000 1.427737901e+001 1.428313844e+001 1.3e-009 9.39
61 2.2e-006 8.4e-003 1.4e-004 1.00e+000 1.427776253e+001 1.428294619e+001 1.2e-009 9.41
62 2.0e-006 8.3e-003 1.3e-004 1.00e+000 1.427810761e+001 1.428277305e+001 1.1e-009 9.44
63 1.8e-006 8.2e-003 1.1e-004 1.00e+000 1.427841818e+001 1.428261688e+001 9.6e-010 9.47
64 1.6e-006 8.1e-003 1.0e-004 1.00e+000 1.427869763e+001 1.428247639e+001 8.6e-010 9.48
65 1.5e-006 8.1e-003 9.3e-005 1.00e+000 1.427894993e+001 1.428234907e+001 7.8e-010 9.52
66 1.3e-006 8.0e-003 8.3e-005 9.96e-001 1.427917600e+001 1.428223581e+001 7.0e-010 9.53
67 1.2e-006 7.9e-003 7.5e-005 9.98e-001 1.427937945e+001 1.428213359e+001 6.3e-010 9.58
68 1.1e-006 7.9e-003 6.8e-005 9.99e-001 1.427956257e+001 1.428204145e+001 5.7e-010 9.61
69 9.7e-007 7.8e-003 6.1e-005 9.99e-001 1.427972736e+001 1.428195848e+001 5.1e-010 9.66
70 8.7e-007 7.8e-003 5.5e-005 1.00e+000 1.427987569e+001 1.428188365e+001 4.6e-010 9.69
71 7.8e-007 7.7e-003 4.9e-005 9.99e-001 1.428000913e+001 1.428181640e+001 4.1e-010 9.73
72 7.0e-007 7.7e-003 4.4e-005 1.00e+000 1.428012926e+001 1.428175568e+001 3.7e-010 9.77
73 6.3e-007 7.7e-003 4.0e-005 1.00e+000 1.428023737e+001 1.428170099e+001 3.4e-010 9.78
74 5.7e-007 7.6e-003 3.6e-005 1.00e+000 1.428033462e+001 1.428165191e+001 3.0e-010 9.81
75 5.1e-007 7.6e-003 3.2e-005 9.97e-001 1.428042210e+001 1.428160786e+001 2.7e-010 9.84
76 4.6e-007 7.6e-003 2.9e-005 1.00e+000 1.428050088e+001 1.428156797e+001 2.4e-010 9.86
77 4.2e-007 6.8e-003 2.6e-005 1.01e+000 1.428057350e+001 1.428153100e+001 2.2e-010 9.91
78 3.7e-007 6.1e-003 2.4e-005 9.96e-001 1.428063708e+001 1.428149900e+001 2.0e-010 9.92
79 3.4e-007 5.5e-003 2.1e-005 9.97e-001 1.428069430e+001 1.428147013e+001 1.8e-010 9.95
80 3.0e-007 5.0e-003 1.9e-005 1.01e+000 1.428074744e+001 1.428144302e+001 1.6e-010 9.97
81 2.7e-007 4.5e-003 1.7e-005 1.02e+000 1.428079759e+001 1.428141719e+001 1.5e-010 9.98
82 2.5e-007 4.0e-003 1.5e-005 9.91e-001 1.428083872e+001 1.428139661e+001 1.3e-010 10.02
83 2.2e-007 3.6e-003 1.4e-005 9.98e-001 1.428087576e+001 1.428137793e+001 1.2e-010 10.05
84 2.0e-007 3.3e-003 1.3e-005 1.01e+000 1.428090972e+001 1.428136067e+001 1.1e-010 10.30
85 1.8e-007 2.9e-003 1.1e-005 9.85e-001 1.428093961e+001 1.428134578e+001 9.6e-011 10.31
86 1.6e-007 2.6e-003 1.0e-005 1.00e+000 1.428096658e+001 1.428133209e+001 8.7e-011 10.34
87 1.4e-007 2.4e-003 9.1e-006 1.04e+000 1.428099489e+001 1.428131726e+001 7.9e-011 10.36
88 1.3e-007 2.1e-003 8.2e-006 9.94e-001 1.428101630e+001 1.428130653e+001 7.1e-011 10.39
89 1.2e-007 1.9e-003 7.4e-006 9.94e-001 1.428103557e+001 1.428129686e+001 6.4e-011 10.40
90 1.1e-007 1.7e-003 6.7e-006 1.00e+000 1.428105310e+001 1.428128797e+001 5.8e-011 10.44
91 9.5e-008 1.6e-003 6.0e-006 1.02e+000 1.428107040e+001 1.428127903e+001 5.3e-011 10.45
92 8.6e-008 1.4e-003 5.4e-006 9.45e-001 1.428108417e+001 1.428127246e+001 4.8e-011 10.47
93 7.7e-008 1.3e-003 4.8e-006 9.71e-001 1.428109661e+001 1.428126632e+001 4.3e-011 10.50
94 6.9e-008 1.1e-003 4.4e-006 1.03e+000 1.428110947e+001 1.428125959e+001 3.9e-011 10.51
95 6.3e-008 1.0e-003 3.9e-006 1.01e+000 1.428111967e+001 1.428125440e+001 3.5e-011 10.55
96 5.6e-008 9.2e-004 3.5e-006 1.01e+000 1.428112902e+001 1.428124961e+001 3.2e-011 10.56
97 5.1e-008 8.3e-004 3.2e-006 1.08e+000 1.428114000e+001 1.428124365e+001 3.0e-011 10.59
98 4.6e-008 7.5e-004 2.9e-006 1.04e+000 1.428114830e+001 1.428123933e+001 2.7e-011 10.61
99 4.1e-008 6.7e-004 2.6e-006 9.64e-001 1.428115435e+001 1.428123643e+001 2.5e-011 10.64
100 3.7e-008 6.0e-004 2.3e-006 9.31e-001 1.428115977e+001 1.428123390e+001 2.2e-011 10.65
101 3.4e-008 5.4e-004 2.1e-006 9.75e-001 1.428116468e+001 1.428123148e+001 2.0e-011 10.67
102 3.1e-008 4.9e-004 1.9e-006 9.11e-001 1.428116907e+001 1.428122945e+001 1.8e-011 10.70
103 2.8e-008 4.4e-004 1.7e-006 8.56e-001 1.428117299e+001 1.428122773e+001 1.6e-011 10.72
104 2.5e-008 4.0e-004 1.5e-006 1.01e+000 1.428117680e+001 1.428122573e+001 1.5e-011 10.75
105 2.2e-008 3.6e-004 1.4e-006 1.00e+000 1.428118007e+001 1.428122403e+001 1.3e-011 10.76
106 2.0e-008 3.2e-004 1.2e-006 9.91e-001 1.428118296e+001 1.428122255e+001 1.2e-011 10.78
107 1.8e-008 2.9e-004 1.1e-006 9.90e-001 1.428118557e+001 1.428122122e+001 1.1e-011 10.81
108 1.6e-008 2.6e-004 1.0e-006 9.92e-001 1.428118792e+001 1.428122002e+001 9.7e-012 10.83
109 1.5e-008 2.3e-004 9.0e-007 9.82e-001 1.428119003e+001 1.428121894e+001 8.7e-012 10.86
110 1.3e-008 2.1e-004 8.1e-007 9.84e-001 1.428119193e+001 1.428121797e+001 7.8e-012 10.87
111 1.2e-008 1.9e-004 7.3e-007 1.01e+000 1.428119374e+001 1.428121702e+001 7.1e-012 10.89
112 1.1e-008 1.7e-004 6.6e-007 1.00e+000 1.428119530e+001 1.428121621e+001 6.4e-012 10.92
113 9.5e-009 1.5e-004 5.9e-007 1.04e+000 1.428119691e+001 1.428121533e+001 5.9e-012 10.95
114 8.6e-009 1.4e-004 5.3e-007 1.02e+000 1.428119821e+001 1.428121465e+001 5.3e-012 10.98
115 7.7e-009 1.2e-004 4.8e-007 9.69e-001 1.428119929e+001 1.428121411e+001 4.8e-012 11.72
116 7.0e-009 1.1e-004 4.3e-007 1.01e+000 1.428120029e+001 1.428121360e+001 4.3e-012 11.75
117 6.2e-009 1.0e-004 3.9e-007 1.01e+000 1.428120121e+001 1.428121312e+001 3.9e-012 11.76
118 5.6e-009 9.1e-005 3.5e-007 9.73e-001 1.428120199e+001 1.428121272e+001 3.5e-012 11.79
119 5.0e-009 8.2e-005 3.1e-007 1.07e+000 1.428120293e+001 1.428121220e+001 3.3e-012 11.81
120 4.6e-009 7.3e-005 2.8e-007 1.02e+000 1.428120360e+001 1.428121185e+001 3.0e-012 11.82
121 4.1e-009 6.6e-005 2.5e-007 9.65e-001 1.428120415e+001 1.428121159e+001 2.7e-012 11.86
122 3.7e-009 5.9e-005 2.3e-007 1.00e+000 1.428120465e+001 1.428121133e+001 2.4e-012 11.89
123 3.3e-009 5.3e-005 2.1e-007 1.01e+000 1.428120510e+001 1.428121110e+001 2.2e-012 11.93
124 3.0e-009 4.8e-005 1.9e-007 1.21e+000 1.428120551e+001 1.428121085e+001 2.0e-012 11.97
125 2.7e-009 4.3e-005 1.7e-007 1.06e+000 1.428120596e+001 1.428121061e+001 1.8e-012 12.01
126 1.8e-009 4.6e-006 1.8e-008 8.83e-001 1.428120883e+001 1.428120936e+001 2.7e-013 12.04
Interior-point optimizer terminated. Time: 12.06.
Optimizer terminated. Time: 12.26
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.4281208833e+001 Viol. con: 3e-008 var: 0e+000
Dual. obj: 1.4281209357e+001 Viol. con: 0e+000 var: 3e-005
* End solution on dual form. *
Transforming to primal solution.
Solving took 12.3 seconds.
result packing took 2.7% of solve time
solution checking took 0.56% 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 : 0.06 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.05
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 -1.289101986e+005 2.000000000e+000 1.0e+000 0.11
1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.266148481e+005 3.779171637e+000 4.6e-001 0.16
2 4.0e+002 5.1e+002 2.2e+004 -9.34e-001 -1.198563789e+005 1.137215115e+001 1.7e-001 0.17
3 2.8e+002 3.6e+002 1.6e+004 -8.29e-001 -1.157240237e+005 8.367014824e+001 1.2e-001 0.20
4 2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.124198287e+005 2.832600369e+003 1.2e-001 0.23
5 6.3e+001 8.2e+001 3.6e+003 -7.47e-001 -6.640387933e+004 1.269993082e+004 2.8e-002 0.25
6 3.9e+001 5.1e+001 2.2e+003 -7.19e-002 -4.860600793e+004 1.113872245e+004 1.7e-002 0.30
7 2.8e+001 3.7e+001 1.6e+003 2.50e-001 -3.839144491e+004 8.758888451e+003 1.3e-002 0.33
8 1.6e+001 2.1e+001 9.0e+002 4.36e-001 -2.428137303e+004 5.454539765e+003 7.1e-003 0.34
9 6.4e+000 8.3e+000 3.6e+002 6.74e-001 -1.033392064e+004 2.810570868e+003 2.9e-003 0.37
10 3.6e+000 4.7e+000 2.0e+002 8.87e-001 -5.635129562e+003 1.899017954e+003 1.6e-003 0.39
11 1.3e+000 1.7e+000 7.5e+001 9.54e-001 -2.012850108e+003 7.891732297e+002 5.9e-004 0.42
12 1.0e+000 1.3e+000 5.7e+001 9.87e-001 -1.520027715e+003 6.366082764e+002 4.5e-004 0.44
13 8.5e-001 1.5e+000 4.8e+001 9.70e-001 -1.298863336e+003 5.502877413e+002 3.9e-004 0.45
14 2.9e-001 5.1e-001 1.6e+001 9.89e-001 -4.334746838e+002 1.970088629e+002 1.3e-004 0.48
15 1.6e-001 3.0e-001 9.3e+000 1.00e+000 -2.379382697e+002 1.162332333e+002 7.5e-005 0.50
16 7.3e-002 1.6e-001 4.2e+000 1.00e+000 -1.038595321e+002 5.761980497e+001 3.4e-005 0.53
17 3.5e-002 1.0e-001 2.1e+000 1.01e+000 -4.582057947e+001 3.218274305e+001 1.7e-005 0.55
18 1.8e-002 7.9e-002 1.1e+000 1.01e+000 -2.038712901e+001 2.046089189e+001 8.8e-006 0.58
19 1.8e-002 7.6e-002 1.0e+000 1.02e+000 -1.899852226e+001 2.043791813e+001 8.5e-006 0.59
20 9.7e-003 5.8e-002 5.7e-001 1.02e+000 -4.740799143e+000 1.674372898e+001 4.7e-006 0.62
21 4.1e-003 5.8e-002 2.5e-001 1.02e+000 4.583283488e+000 1.368803997e+001 2.0e-006 0.64
22 2.1e-003 5.2e-002 1.3e-001 1.01e+000 7.768931718e+000 1.261358743e+001 1.1e-006 0.67
23 6.0e-004 8.2e-002 3.9e-002 9.87e-001 1.034302500e+001 1.181151724e+001 3.4e-007 0.69
24 1.8e-004 8.8e-002 1.3e-002 9.78e-001 1.109075722e+001 1.156935541e+001 1.1e-007 0.72
25 6.0e-005 8.7e-002 4.3e-003 9.88e-001 1.133248288e+001 1.149489124e+001 3.9e-008 0.73
26 2.2e-005 8.4e-002 1.6e-003 9.96e-001 1.141328782e+001 1.147317441e+001 1.5e-008 0.75
27 8.2e-006 8.1e-002 6.0e-004 9.99e-001 1.144292934e+001 1.146572714e+001 5.6e-009 0.78
28 7.4e-006 7.4e-002 5.4e-004 1.00e+000 1.144485672e+001 1.146537616e+001 5.0e-009 0.80
29 6.7e-006 6.7e-002 4.9e-004 1.00e+000 1.144644890e+001 1.146491680e+001 4.5e-009 0.83
30 6.0e-006 6.1e-002 4.4e-004 1.00e+000 1.144788154e+001 1.146450298e+001 4.1e-009 0.84
31 5.4e-006 5.6e-002 3.9e-004 1.00e+000 1.144916826e+001 1.146412782e+001 3.7e-009 0.87
32 4.9e-006 5.1e-002 3.5e-004 1.00e+000 1.145032513e+001 1.146378892e+001 3.3e-009 0.90
33 4.4e-006 4.6e-002 3.2e-004 1.00e+000 1.145136517e+001 1.146348269e+001 3.0e-009 0.95
34 3.9e-006 4.2e-002 2.9e-004 1.00e+000 1.145230030e+001 1.146320621e+001 2.7e-009 0.98
35 3.5e-006 3.9e-002 2.6e-004 1.00e+000 1.145314116e+001 1.146295658e+001 2.4e-009 1.01
36 3.2e-006 3.6e-002 2.3e-004 1.00e+000 1.145389735e+001 1.146273127e+001 2.2e-009 1.03
37 2.9e-006 3.3e-002 2.1e-004 1.00e+000 1.145457746e+001 1.146252801e+001 1.9e-009 1.06
38 2.6e-006 3.0e-002 1.9e-004 1.00e+000 1.145518918e+001 1.146234473e+001 1.7e-009 1.09
39 2.3e-006 2.8e-002 1.7e-004 1.00e+000 1.145573944e+001 1.146217946e+001 1.6e-009 1.12
40 2.1e-006 2.6e-002 1.5e-004 1.00e+000 1.145623445e+001 1.146203046e+001 1.4e-009 1.15
41 1.9e-006 2.4e-002 1.4e-004 1.00e+000 1.145667976e+001 1.146189623e+001 1.3e-009 1.17
42 1.7e-006 2.2e-002 1.2e-004 1.00e+000 1.145708040e+001 1.146177527e+001 1.1e-009 1.20
43 1.5e-006 2.1e-002 1.1e-004 1.00e+000 1.145744086e+001 1.146166630e+001 1.0e-009 1.22
44 1.4e-006 1.9e-002 1.0e-004 1.00e+000 1.145776519e+001 1.146156812e+001 9.3e-010 1.23
45 1.2e-006 1.8e-002 9.0e-005 1.00e+000 1.145805703e+001 1.146147965e+001 8.4e-010 1.26
46 1.1e-006 1.7e-002 8.1e-005 1.00e+000 1.145831961e+001 1.146140003e+001 7.5e-010 1.68
47 1.0e-006 1.6e-002 7.3e-005 1.00e+000 1.145855589e+001 1.146132832e+001 6.8e-010 1.70
48 9.0e-007 1.5e-002 6.6e-005 1.00e+000 1.145876852e+001 1.146126372e+001 6.1e-010 1.72
49 8.1e-007 1.4e-002 5.9e-005 1.00e+000 1.145895987e+001 1.146120552e+001 5.5e-010 1.75
50 7.3e-007 1.4e-002 5.3e-005 1.00e+000 1.145913208e+001 1.146115309e+001 4.9e-010 1.76
51 6.6e-007 1.3e-002 4.8e-005 1.00e+000 1.145928702e+001 1.146110598e+001 4.4e-010 1.79
52 2.3e-007 4.5e-003 1.7e-005 1.00e+000 1.146019641e+001 1.146082839e+001 1.5e-010 1.81
53 2.1e-007 4.0e-003 1.5e-005 1.00e+000 1.146024522e+001 1.146081397e+001 1.4e-010 1.83
54 7.1e-008 1.4e-003 5.1e-006 1.00e+000 1.146053143e+001 1.146072570e+001 4.7e-011 1.86
55 6.4e-008 1.2e-003 4.6e-006 9.91e-001 1.146054642e+001 1.146072134e+001 4.3e-011 1.87
56 5.7e-008 1.1e-003 4.1e-006 9.96e-001 1.146055983e+001 1.146071730e+001 3.8e-011 1.90
57 5.1e-008 1.0e-003 3.7e-006 9.93e-001 1.146057191e+001 1.146071368e+001 3.5e-011 1.92
58 4.6e-008 9.1e-004 3.4e-006 1.01e+000 1.146058303e+001 1.146071028e+001 3.1e-011 1.93
59 4.2e-008 8.1e-004 3.0e-006 1.01e+000 1.146059341e+001 1.146070709e+001 2.8e-011 1.97
60 3.8e-008 7.3e-004 2.7e-006 1.01e+000 1.146060243e+001 1.146070433e+001 2.6e-011 1.98
61 1.3e-008 1.4e-004 5.2e-007 9.57e-001 1.146066634e+001 1.146068640e+001 5.4e-012 2.01
62 1.2e-008 1.3e-004 4.7e-007 1.12e+000 1.146066856e+001 1.146068522e+001 5.1e-012 2.03
63 4.5e-009 7.6e-006 2.8e-008 9.34e-001 1.146068025e+001 1.146068129e+001 4.7e-013 2.06
Interior-point optimizer terminated. Time: 2.06.
Optimizer terminated. Time: 2.21
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1460680255e+001 Viol. con: 1e-007 var: 0e+000
Dual. obj: 1.1460681290e+001 Viol. con: 0e+000 var: 5e-005
* End solution on dual form. *
Transforming to primal solution.
Solving took 2.25 seconds.
result packing took 21% of solve time
solution checking took 5% 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 : 0.06 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 -1.288303353e+005 2.000000000e+000 1.0e+000 0.11
1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265192773e+005 3.780479840e+000 4.6e-001 1.06
2 3.9e+002 5.0e+002 2.2e+004 -9.34e-001 -1.195797425e+005 1.160529907e+001 1.7e-001 1.08
3 2.8e+002 3.6e+002 1.6e+004 -8.26e-001 -1.156357595e+005 9.407499810e+001 1.2e-001 1.11
4 2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.123237028e+005 2.800961808e+003 1.2e-001 1.12
5 7.8e+001 1.0e+002 4.4e+003 -7.46e-001 -7.498276369e+004 1.053091029e+004 3.5e-002 1.14
6 3.8e+001 4.9e+001 2.1e+003 -2.08e-001 -4.716144850e+004 1.110972506e+004 1.7e-002 1.17
7 2.1e+001 2.8e+001 1.2e+003 2.72e-001 -3.073924961e+004 7.249027006e+003 9.5e-003 1.19
8 9.8e+000 1.3e+001 5.5e+002 5.69e-001 -1.536055969e+004 3.892021981e+003 4.3e-003 1.22
9 4.2e+000 5.5e+000 2.4e+002 8.19e-001 -6.677118506e+003 2.109932620e+003 1.9e-003 1.25
10 2.0e+000 2.6e+000 1.1e+002 9.39e-001 -2.962333319e+003 1.171572467e+003 8.8e-004 1.26
11 1.4e+000 1.8e+000 7.8e+001 9.83e-001 -2.096663009e+003 8.360719902e+002 6.2e-004 1.29
12 9.0e-001 1.2e+000 5.1e+001 9.85e-001 -1.355772274e+003 5.626998638e+002 4.0e-004 1.31
13 7.4e-001 1.1e+000 4.2e+001 9.64e-001 -1.126598062e+003 4.651917451e+002 3.3e-004 1.34
14 2.6e-001 3.9e-001 1.5e+001 9.90e-001 -3.944931632e+002 1.817950710e+002 1.2e-004 1.36
15 1.5e-001 2.3e-001 8.6e+000 1.00e+000 -2.189268728e+002 1.081444237e+002 6.9e-005 1.37
16 4.0e-002 1.5e-001 2.4e+000 1.00e+000 -5.533582787e+001 3.458932603e+001 1.9e-005 1.40
17 3.4e-002 1.3e-001 2.0e+000 1.00e+000 -4.533826658e+001 3.085282127e+001 1.6e-005 1.45
18 2.1e-002 9.7e-002 1.3e+000 1.00e+000 -2.612303565e+001 2.230775867e+001 1.0e-005 1.48
19 1.7e-002 7.9e-002 1.0e+000 1.01e+000 -1.807133244e+001 1.984094178e+001 8.2e-006 1.53
20 1.4e-002 6.6e-002 8.3e-001 1.02e+000 -1.269390723e+001 1.855355131e+001 6.8e-006 1.56
21 5.5e-003 6.0e-002 3.3e-001 1.02e+000 2.057571001e+000 1.414256630e+001 2.7e-006 1.61
22 2.1e-003 6.3e-002 1.3e-001 1.02e+000 7.652447424e+000 1.251447743e+001 1.1e-006 1.65
23 7.3e-004 6.8e-002 4.7e-002 9.85e-001 9.982205236e+000 1.173398925e+001 4.1e-007 1.69
24 2.8e-004 7.5e-002 1.9e-002 9.68e-001 1.079314381e+001 1.151196068e+001 1.7e-007 1.72
25 1.4e-004 5.7e-002 9.9e-003 9.55e-001 1.105514545e+001 1.143427276e+001 8.8e-008 1.73
26 8.1e-005 5.7e-002 5.7e-003 9.85e-001 1.118337245e+001 1.139990650e+001 5.0e-008 1.76
27 7.4e-005 5.3e-002 5.1e-003 9.86e-001 1.119906034e+001 1.139534483e+001 4.6e-008 1.78
28 5.1e-005 4.6e-002 3.6e-003 9.72e-001 1.124504491e+001 1.138208500e+001 3.2e-008 1.81
29 4.6e-005 4.2e-002 3.2e-003 9.52e-001 1.125768008e+001 1.138146832e+001 2.9e-008 1.84
30 4.2e-005 3.6e-002 2.9e-003 9.73e-001 1.126749983e+001 1.137906802e+001 2.6e-008 1.90
31 3.7e-005 3.2e-002 2.6e-003 9.93e-001 1.127634800e+001 1.137672851e+001 2.3e-008 1.94
32 3.4e-005 3.0e-002 2.4e-003 9.95e-001 1.128409012e+001 1.137450068e+001 2.1e-008 1.97
33 3.0e-005 2.7e-002 2.1e-003 9.95e-001 1.129105321e+001 1.137246945e+001 1.9e-008 2.00
34 2.7e-005 2.5e-002 1.9e-003 9.96e-001 1.129730428e+001 1.137061728e+001 1.7e-008 2.03
35 2.5e-005 2.4e-002 1.7e-003 9.95e-001 1.130291190e+001 1.136893112e+001 1.5e-008 3.48
36 2.2e-005 2.2e-002 1.5e-003 9.95e-001 1.130794109e+001 1.136739891e+001 1.4e-008 3.53
37 2.0e-005 2.0e-002 1.4e-003 9.95e-001 1.131244939e+001 1.136600968e+001 1.2e-008 3.57
38 1.8e-005 1.9e-002 1.3e-003 9.94e-001 1.131648629e+001 1.136475455e+001 1.1e-008 4.65
39 1.6e-005 1.8e-002 1.1e-003 9.92e-001 1.132009192e+001 1.136362816e+001 1.0e-008 4.70
40 1.5e-005 1.7e-002 1.0e-003 9.88e-001 1.132329524e+001 1.136263265e+001 9.1e-009 4.73
41 1.3e-005 1.6e-002 9.1e-004 9.81e-001 1.132613297e+001 1.136178221e+001 8.2e-009 4.76
42 8.5e-006 1.0e-002 5.9e-004 9.79e-001 1.133566714e+001 1.135880194e+001 5.3e-009 4.79
43 7.6e-006 9.6e-003 5.3e-004 9.89e-001 1.133734526e+001 1.135817814e+001 4.8e-009 4.84
44 6.9e-006 8.6e-003 4.8e-004 9.78e-001 1.133909201e+001 1.135768545e+001 4.3e-009 4.87
45 6.2e-006 8.2e-003 4.3e-004 9.84e-001 1.134034369e+001 1.135727074e+001 3.9e-009 4.90
46 4.1e-006 5.4e-003 2.9e-004 9.92e-001 1.134457294e+001 1.135588245e+001 2.6e-009 4.95
47 3.7e-006 5.4e-003 2.6e-004 9.94e-001 1.134540482e+001 1.135557952e+001 2.3e-009 4.98
48 3.3e-006 4.9e-003 2.3e-004 9.92e-001 1.134617617e+001 1.135532403e+001 2.1e-009 5.01
49 3.0e-006 4.4e-003 2.1e-004 9.88e-001 1.134687301e+001 1.135510038e+001 1.9e-009 5.04
50 2.7e-006 4.0e-003 1.9e-004 9.86e-001 1.134749776e+001 1.135490506e+001 1.7e-009 5.09
51 2.4e-006 3.6e-003 1.7e-004 9.88e-001 1.134805696e+001 1.135472994e+001 1.5e-009 5.12
52 2.2e-006 3.2e-003 1.5e-004 9.91e-001 1.134855976e+001 1.135457100e+001 1.4e-009 5.15
53 2.0e-006 2.9e-003 1.4e-004 9.93e-001 1.134901374e+001 1.135442790e+001 1.2e-009 5.20
54 1.8e-006 2.6e-003 1.2e-004 9.95e-001 1.134942357e+001 1.135429895e+001 1.1e-009 5.23
55 1.6e-006 2.3e-003 1.1e-004 9.97e-001 1.134979299e+001 1.135418238e+001 1.0e-009 5.26
56 1.4e-006 2.1e-003 1.0e-004 9.98e-001 1.135012568e+001 1.135407701e+001 9.0e-010 5.30
57 1.3e-006 1.9e-003 9.1e-005 9.98e-001 1.135042516e+001 1.135398191e+001 8.1e-010 5.34
58 1.2e-006 1.7e-003 8.2e-005 9.98e-001 1.135069474e+001 1.135389617e+001 7.3e-010 5.59
59 1.0e-006 1.5e-003 7.3e-005 9.99e-001 1.135093739e+001 1.135381893e+001 6.6e-010 6.58
60 9.4e-007 1.4e-003 6.6e-005 9.99e-001 1.135115580e+001 1.135374939e+001 5.9e-010 6.60
61 8.5e-007 1.2e-003 5.9e-005 9.99e-001 1.135135241e+001 1.135368677e+001 5.3e-010 6.63
62 7.6e-007 1.1e-003 5.4e-005 9.99e-001 1.135152938e+001 1.135363042e+001 4.8e-010 6.66
63 6.9e-007 1.0e-003 4.8e-005 1.00e+000 1.135168867e+001 1.135357969e+001 4.3e-010 6.68
64 6.2e-007 9.1e-004 4.3e-005 9.99e-001 1.135183206e+001 1.135353405e+001 3.9e-010 6.69
65 5.6e-007 8.2e-004 3.9e-005 9.99e-001 1.135196111e+001 1.135349299e+001 3.5e-010 6.72
66 5.0e-007 7.3e-004 3.5e-005 1.00e+000 1.135207728e+001 1.135345601e+001 3.1e-010 6.75
67 4.5e-007 6.6e-004 3.2e-005 9.99e-001 1.135218183e+001 1.135342274e+001 2.8e-010 6.79
68 4.1e-007 6.0e-004 2.8e-005 9.99e-001 1.135227595e+001 1.135339281e+001 2.5e-010 7.05
69 3.6e-007 5.4e-004 2.6e-005 1.00e+000 1.135236065e+001 1.135336586e+001 2.3e-010 7.08
70 3.3e-007 4.8e-004 2.3e-005 1.00e+000 1.135243689e+001 1.135334160e+001 2.1e-010 7.11
71 3.0e-007 4.3e-004 2.1e-005 1.00e+000 1.135250552e+001 1.135331977e+001 1.9e-010 7.16
72 2.7e-007 3.9e-004 1.9e-005 1.00e+000 1.135256728e+001 1.135330012e+001 1.7e-010 7.19
73 2.4e-007 3.5e-004 1.7e-005 1.00e+000 1.135262287e+001 1.135328244e+001 1.5e-010 7.22
74 2.2e-007 3.2e-004 1.5e-005 1.00e+000 1.135267290e+001 1.135326652e+001 1.4e-010 7.25
75 1.9e-007 2.8e-004 1.4e-005 9.99e-001 1.135271792e+001 1.135325221e+001 1.2e-010 7.27
76 1.7e-007 2.6e-004 1.2e-005 1.00e+000 1.135275845e+001 1.135323931e+001 1.1e-010 7.30
77 1.6e-007 2.3e-004 1.1e-005 9.99e-001 1.135279492e+001 1.135322772e+001 9.9e-011 7.32
78 1.4e-007 2.1e-004 9.9e-006 1.00e+000 1.135282775e+001 1.135321724e+001 8.9e-011 7.35
79 1.3e-007 1.9e-004 8.9e-006 1.00e+000 1.135285730e+001 1.135320783e+001 8.0e-011 7.36
80 1.1e-007 1.7e-004 8.0e-006 9.98e-001 1.135288388e+001 1.135319939e+001 7.2e-011 7.38
81 1.0e-007 1.5e-004 7.2e-006 1.00e+000 1.135290781e+001 1.135319177e+001 6.5e-011 7.41
82 9.3e-008 1.4e-004 6.5e-006 1.00e+000 1.135292935e+001 1.135318490e+001 5.8e-011 7.43
83 8.3e-008 1.2e-004 5.9e-006 9.99e-001 1.135294872e+001 1.135317874e+001 5.2e-011 7.46
84 7.5e-008 1.1e-004 5.3e-006 1.00e+000 1.135296617e+001 1.135317317e+001 4.7e-011 7.47
85 6.8e-008 9.9e-005 4.7e-006 9.98e-001 1.135298186e+001 1.135316818e+001 4.2e-011 7.49
86 6.1e-008 8.9e-005 4.3e-006 9.98e-001 1.135299598e+001 1.135316369e+001 3.8e-011 7.54
87 5.5e-008 8.0e-005 3.8e-006 1.00e+000 1.135300870e+001 1.135315963e+001 3.4e-011 7.57
88 4.9e-008 7.2e-005 3.5e-006 1.00e+000 1.135302014e+001 1.135315598e+001 3.1e-011 7.61
89 4.4e-008 6.5e-005 3.1e-006 9.93e-001 1.135303043e+001 1.135315273e+001 2.8e-011 7.66
90 4.0e-008 5.9e-005 2.8e-006 1.00e+000 1.135303974e+001 1.135314974e+001 2.5e-011 7.71
91 3.6e-008 5.3e-005 2.5e-006 1.00e+000 1.135304811e+001 1.135314706e+001 2.3e-011 7.74
92 3.2e-008 4.7e-005 2.3e-006 1.01e+000 1.135305585e+001 1.135314456e+001 2.0e-011 7.79
93 2.9e-008 4.3e-005 2.0e-006 1.00e+000 1.135306264e+001 1.135314239e+001 1.8e-011 7.83
94 2.6e-008 3.8e-005 1.8e-006 1.00e+000 1.135306878e+001 1.135314042e+001 1.7e-011 7.86
95 2.4e-008 3.5e-005 1.7e-006 9.97e-001 1.135307421e+001 1.135313869e+001 1.5e-011 7.91
96 2.1e-008 3.1e-005 1.5e-006 9.99e-001 1.135307910e+001 1.135313714e+001 1.3e-011 7.94
97 1.9e-008 2.8e-005 1.3e-006 1.00e+000 1.135308350e+001 1.135313573e+001 1.2e-011 7.99
98 1.7e-008 2.5e-005 1.2e-006 9.96e-001 1.135308745e+001 1.135313448e+001 1.1e-011 8.03
99 1.5e-008 2.3e-005 1.1e-006 9.94e-001 1.135309101e+001 1.135313335e+001 9.8e-012 10.09
100 1.4e-008 2.0e-005 9.8e-007 1.00e+000 1.135309422e+001 1.135313232e+001 8.8e-012 10.13
101 1.3e-008 1.8e-005 8.8e-007 1.01e+000 1.135309720e+001 1.135313136e+001 7.9e-012 10.17
102 1.1e-008 1.7e-005 7.9e-007 1.03e+000 1.135310017e+001 1.135313037e+001 7.3e-012 10.23
103 1.5e-009 1.7e-006 8.2e-008 9.90e-001 1.135312077e+001 1.135312390e+001 7.8e-013 10.28
Interior-point optimizer terminated. Time: 10.33.
Optimizer terminated. Time: 10.55
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1353120765e+001 Viol. con: 3e-008 var: 0e+000
Dual. obj: 1.1353123896e+001 Viol. con: 0e+000 var: 1e-005
* End solution on dual form. *
Transforming to primal solution.
Solving took 10.6 seconds.
result packing took 4.7% of solve time
solution checking took 0.95% 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 : 0.06 dense det. time : 0.00
Factor - ML order time : 0.00 GP order time : 0.05
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 -1.288985036e+005 2.000000000e+000 1.0e+000 0.11
1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.265799435e+005 3.775575012e+000 4.6e-001 0.17
2 3.8e+002 4.9e+002 2.1e+004 -9.34e-001 -1.194833589e+005 1.178222132e+001 1.7e-001 3.12
3 2.8e+002 3.6e+002 1.6e+004 -8.24e-001 -1.156680191e+005 1.068050679e+002 1.2e-001 3.15
4 2.8e+002 3.6e+002 1.5e+004 -7.56e-001 -1.123101101e+005 2.781216356e+003 1.2e-001 3.17
5 7.6e+001 9.8e+001 4.2e+003 -7.45e-001 -7.369370635e+004 1.086779341e+004 3.3e-002 3.18
6 3.6e+001 4.7e+001 2.0e+003 -1.88e-001 -4.546681447e+004 1.112170240e+004 1.6e-002 3.20
7 2.0e+001 2.6e+001 1.1e+003 3.02e-001 -2.909690667e+004 7.248067754e+003 9.0e-003 3.21
8 9.7e+000 1.3e+001 5.4e+002 5.97e-001 -1.524966339e+004 3.925529610e+003 4.3e-003 3.25
9 4.3e+000 5.6e+000 2.4e+002 8.22e-001 -6.824811555e+003 2.126890357e+003 1.9e-003 3.48
10 1.6e+000 2.1e+000 9.0e+001 9.39e-001 -2.382019420e+003 9.940760446e+002 7.2e-004 3.51
11 1.1e+000 1.5e+000 6.3e+001 9.88e-001 -1.660108535e+003 6.956310279e+002 5.0e-004 3.57
12 7.8e-001 1.0e+000 4.4e+001 9.83e-001 -1.186246730e+003 4.998444983e+002 3.5e-004 3.63
13 5.9e-001 7.7e-001 3.3e+001 9.85e-001 -8.730304573e+002 3.883188174e+002 2.6e-004 3.68
14 2.1e-001 2.9e-001 1.2e+001 9.89e-001 -3.245170204e+002 1.424684506e+002 9.8e-005 3.71
15 8.9e-002 1.4e-001 5.1e+000 1.01e+000 -1.284348376e+002 6.667982175e+001 4.2e-005 3.73
16 3.5e-002 9.9e-002 2.1e+000 1.01e+000 -4.749300952e+001 3.075570935e+001 1.7e-005 3.76
17 2.9e-002 8.4e-002 1.7e+000 9.96e-001 -3.703525421e+001 2.753513885e+001 1.4e-005 3.79
18 1.8e-002 6.6e-002 1.0e+000 1.01e+000 -1.901830866e+001 2.024511857e+001 8.5e-006 3.81
19 1.5e-002 5.7e-002 8.8e-001 1.02e+000 -1.416263610e+001 1.901458778e+001 7.2e-006 3.84
20 5.4e-003 6.6e-002 3.2e-001 1.02e+000 2.106644394e+000 1.405587189e+001 2.6e-006 3.85
21 1.8e-003 7.8e-002 1.1e-001 1.02e+000 8.170166205e+000 1.230683999e+001 9.7e-007 3.88
22 1.3e-003 6.0e-002 8.3e-002 9.63e-001 8.936990366e+000 1.202328886e+001 7.2e-007 3.90
23 4.8e-004 6.6e-002 3.1e-002 9.59e-001 1.040638984e+001 1.160345185e+001 2.8e-007 3.92
24 1.9e-004 6.2e-002 1.3e-002 9.58e-001 1.093939037e+001 1.142612412e+001 1.1e-007 3.95
25 1.7e-004 5.7e-002 1.1e-002 9.76e-001 1.097690596e+001 1.141479090e+001 1.0e-007 3.96
26 1.5e-004 5.2e-002 1.0e-002 9.75e-001 1.101084689e+001 1.140546137e+001 9.2e-008 3.99
27 1.4e-004 4.7e-002 9.2e-003 9.76e-001 1.104378784e+001 1.139945350e+001 8.3e-008 4.01
28 1.2e-004 4.3e-002 8.3e-003 9.78e-001 1.107352257e+001 1.139406148e+001 7.5e-008 4.03
29 1.1e-004 3.9e-002 7.5e-003 9.80e-001 1.110028294e+001 1.138913506e+001 6.7e-008 4.06
30 9.9e-005 3.6e-002 6.7e-003 9.82e-001 1.112431740e+001 1.138458875e+001 6.1e-008 4.09
31 8.9e-005 3.3e-002 6.0e-003 9.83e-001 1.114589600e+001 1.138039234e+001 5.5e-008 4.13
32 8.0e-005 3.1e-002 5.4e-003 9.85e-001 1.116526392e+001 1.137651912e+001 4.9e-008 4.18
33 7.2e-005 2.8e-002 4.9e-003 9.86e-001 1.118264396e+001 1.137294586e+001 4.4e-008 4.21
34 6.5e-005 2.6e-002 4.4e-003 9.88e-001 1.119823768e+001 1.136965151e+001 4.0e-008 4.26
35 5.8e-005 2.4e-002 4.0e-003 9.89e-001 1.121222723e+001 1.136661684e+001 3.6e-008 4.29
36 5.2e-005 2.3e-002 3.6e-003 9.90e-001 1.122477696e+001 1.136382403e+001 3.2e-008 4.34
37 4.7e-005 2.1e-002 3.2e-003 9.91e-001 1.123603507e+001 1.136125671e+001 2.9e-008 4.38
38 4.3e-005 2.0e-002 2.9e-003 9.92e-001 1.124613460e+001 1.135889923e+001 2.6e-008 4.45
39 3.8e-005 1.8e-002 2.6e-003 9.92e-001 1.125519499e+001 1.135673666e+001 2.4e-008 5.65
40 3.4e-005 1.7e-002 2.3e-003 9.93e-001 1.126332337e+001 1.135475470e+001 2.1e-008 5.66
41 3.1e-005 1.6e-002 2.1e-003 9.94e-001 1.127061598e+001 1.135294012e+001 1.9e-008 5.69
42 2.8e-005 1.5e-002 1.9e-003 9.94e-001 1.127715909e+001 1.135128019e+001 1.7e-008 5.71
43 2.5e-005 1.5e-002 1.7e-003 9.95e-001 1.128303039e+001 1.134976337e+001 1.5e-008 5.72
44 2.3e-005 1.4e-002 1.5e-003 9.96e-001 1.128829974e+001 1.134837909e+001 1.4e-008 5.76
45 2.0e-005 1.3e-002 1.4e-003 9.96e-001 1.129302964e+001 1.134711711e+001 1.3e-008 5.77
46 1.8e-005 1.3e-002 1.2e-003 9.96e-001 1.129727612e+001 1.134596795e+001 1.1e-008 5.80
47 1.6e-005 1.2e-002 1.1e-003 9.97e-001 1.130108921e+001 1.134492255e+001 1.0e-008 5.82
48 1.5e-005 1.2e-002 1.0e-003 9.97e-001 1.130451370e+001 1.134397243e+001 9.1e-009 5.85
49 1.3e-005 1.1e-002 9.1e-004 9.97e-001 1.130758967e+001 1.134310966e+001 8.2e-009 5.87
50 1.2e-005 1.1e-002 8.2e-004 9.98e-001 1.131035300e+001 1.134232679e+001 7.4e-009 5.90
51 1.1e-005 1.0e-002 7.4e-004 9.98e-001 1.131283585e+001 1.134161695e+001 6.7e-009 5.94
52 9.7e-006 1.0e-002 6.6e-004 9.98e-001 1.131506695e+001 1.134097381e+001 6.0e-009 6.01
53 8.8e-006 9.7e-003 6.0e-004 9.98e-001 1.131707207e+001 1.134039139e+001 5.4e-009 6.05
54 7.9e-006 9.5e-003 5.4e-004 9.99e-001 1.131887428e+001 1.133986419e+001 4.9e-009 6.12
55 7.1e-006 9.2e-003 4.8e-004 9.99e-001 1.132049425e+001 1.133938725e+001 4.4e-009 6.16
56 6.4e-006 9.0e-003 4.4e-004 9.99e-001 1.132195050e+001 1.133895593e+001 3.9e-009 6.21
57 5.7e-006 8.8e-003 3.9e-004 9.99e-001 1.132325966e+001 1.133856591e+001 3.5e-009 6.27
58 5.2e-006 8.7e-003 3.5e-004 9.99e-001 1.132443663e+001 1.133821336e+001 3.2e-009 6.32
59 4.7e-006 8.5e-003 3.2e-004 9.99e-001 1.132549480e+001 1.133789474e+001 2.9e-009 6.35
60 4.2e-006 8.4e-003 2.9e-004 9.99e-001 1.132644619e+001 1.133760695e+001 2.6e-009 6.40
61 3.8e-006 8.2e-003 2.6e-004 9.99e-001 1.132730165e+001 1.133734691e+001 2.3e-009 6.41
62 3.4e-006 8.1e-003 2.3e-004 9.99e-001 1.132807089e+001 1.133711214e+001 2.1e-009 6.44
63 3.1e-006 8.0e-003 2.1e-004 9.99e-001 1.132876267e+001 1.133690023e+001 1.9e-009 6.47
64 2.7e-006 7.9e-003 1.9e-004 1.00e+000 1.132938486e+001 1.133670895e+001 1.7e-009 6.71
65 2.5e-006 7.8e-003 1.7e-004 1.00e+000 1.132994450e+001 1.133653646e+001 1.5e-009 6.74
66 2.2e-006 7.8e-003 1.5e-004 1.00e+000 1.133044793e+001 1.133638093e+001 1.4e-009 8.30
67 2.0e-006 7.7e-003 1.4e-004 1.00e+000 1.133090083e+001 1.133624075e+001 1.2e-009 8.35
68 1.8e-006 7.6e-003 1.2e-004 1.00e+000 1.133130830e+001 1.133611440e+001 1.1e-009 8.39
69 1.6e-006 7.6e-003 1.1e-004 1.00e+000 1.133167491e+001 1.133600055e+001 1.0e-009 8.44
70 1.5e-006 7.5e-003 1.0e-004 1.00e+000 1.133200480e+001 1.133589794e+001 9.0e-010 8.47
71 1.3e-006 7.4e-003 9.0e-005 1.00e+000 1.133230164e+001 1.133580549e+001 8.1e-010 8.50
72 1.2e-006 7.4e-003 8.1e-005 1.00e+000 1.133256874e+001 1.133572225e+001 7.3e-010 8.64
73 1.1e-006 7.4e-003 7.3e-005 1.00e+000 1.133280910e+001 1.133564731e+001 6.6e-010 8.67
74 9.6e-007 7.3e-003 6.5e-005 1.00e+000 1.133302538e+001 1.133557984e+001 5.9e-010 8.72
75 8.6e-007 7.3e-003 5.9e-005 1.00e+000 1.133322001e+001 1.133551909e+001 5.3e-010 8.75
76 7.8e-007 7.2e-003 5.3e-005 1.00e+000 1.133339517e+001 1.133546437e+001 4.8e-010 8.80
77 7.0e-007 7.2e-003 4.8e-005 1.00e+000 1.133355280e+001 1.133541509e+001 4.3e-010 8.81
78 6.3e-007 7.2e-003 4.3e-005 9.99e-001 1.133369465e+001 1.133537077e+001 3.9e-010 8.85
79 5.7e-007 7.2e-003 3.9e-005 1.00e+000 1.133382231e+001 1.133533081e+001 3.5e-010 9.23
80 5.1e-007 7.1e-003 3.5e-005 1.00e+000 1.133393720e+001 1.133529483e+001 3.1e-010 9.31
81 4.6e-007 7.1e-003 3.1e-005 1.00e+000 1.133404060e+001 1.133526241e+001 2.8e-010 9.33
82 4.1e-007 7.1e-003 2.8e-005 1.00e+000 1.133413365e+001 1.133523327e+001 2.5e-010 9.36
83 3.7e-007 7.1e-003 2.5e-005 1.00e+000 1.133421738e+001 1.133520703e+001 2.3e-010 10.30
84 3.3e-007 7.1e-003 2.3e-005 1.00e+000 1.133429274e+001 1.133518339e+001 2.1e-010 11.78
85 3.0e-007 7.0e-003 2.1e-005 9.99e-001 1.133436054e+001 1.133516218e+001 1.9e-010 11.81
86 2.7e-007 7.0e-003 1.8e-005 9.99e-001 1.133442156e+001 1.133514307e+001 1.7e-010 11.84
87 2.4e-007 7.0e-003 1.7e-005 1.00e+000 1.133447647e+001 1.133512584e+001 1.5e-010 11.87
88 2.2e-007 7.0e-003 1.5e-005 1.00e+000 1.133452590e+001 1.133511033e+001 1.4e-010 12.65
89 2.0e-007 7.0e-003 1.3e-005 1.00e+000 1.133457038e+001 1.133509636e+001 1.2e-010 12.68
90 1.8e-007 7.0e-003 1.2e-005 1.00e+000 1.133461041e+001 1.133508376e+001 1.1e-010 12.70
91 1.6e-007 7.0e-003 1.1e-005 1.00e+000 1.133464643e+001 1.133507245e+001 9.9e-011 12.73
92 1.4e-007 7.0e-003 9.8e-006 9.99e-001 1.133467884e+001 1.133506228e+001 8.9e-011 12.74
93 1.3e-007 6.9e-003 8.8e-006 1.00e+000 1.133470804e+001 1.133505308e+001 8.0e-011 12.78
94 1.2e-007 6.9e-003 8.0e-006 9.99e-001 1.133473429e+001 1.133504484e+001 7.2e-011 12.79
95 1.0e-007 6.2e-003 7.2e-006 1.00e+000 1.133475821e+001 1.133503727e+001 6.5e-011 12.82
96 9.4e-008 5.6e-003 6.4e-006 9.99e-001 1.133477944e+001 1.133503061e+001 5.8e-011 12.84
97 8.5e-008 5.1e-003 5.8e-006 1.00e+000 1.133479859e+001 1.133502457e+001 5.3e-011 12.85
98 7.6e-008 4.5e-003 5.2e-006 1.00e+000 1.133481577e+001 1.133501916e+001 4.7e-011 12.89
99 6.9e-008 4.1e-003 4.7e-006 9.99e-001 1.133483124e+001 1.133501430e+001 4.3e-011 12.90
100 6.2e-008 3.7e-003 4.2e-006 1.01e+000 1.133484554e+001 1.133500975e+001 3.8e-011 12.95
101 5.6e-008 3.3e-003 3.8e-006 1.00e+000 1.133485803e+001 1.133500582e+001 3.5e-011 12.96
102 5.0e-008 3.0e-003 3.4e-006 9.98e-001 1.133486927e+001 1.133500229e+001 3.1e-011 12.99
103 4.5e-008 2.7e-003 3.1e-006 1.00e+000 1.133487954e+001 1.133499904e+001 2.8e-011 13.01
104 4.1e-008 2.4e-003 2.8e-006 1.00e+000 1.133488867e+001 1.133499616e+001 2.5e-011 13.03
105 3.7e-008 2.2e-003 2.5e-006 1.01e+000 1.133489709e+001 1.133499348e+001 2.3e-011 13.06
106 3.3e-008 2.0e-003 2.2e-006 9.98e-001 1.133490442e+001 1.133499118e+001 2.1e-011 13.07
107 3.0e-008 1.8e-003 2.0e-006 9.98e-001 1.133491102e+001 1.133498911e+001 1.8e-011 13.10
108 2.7e-008 1.6e-003 1.8e-006 9.97e-001 1.133491695e+001 1.133498725e+001 1.7e-011 13.12
109 2.4e-008 1.4e-003 1.6e-006 1.01e+000 1.133492240e+001 1.133498552e+001 1.5e-011 13.15
110 2.2e-008 1.3e-003 1.5e-006 1.00e+000 1.133492720e+001 1.133498401e+001 1.3e-011 13.17
111 4.4e-009 2.5e-004 2.8e-007 9.77e-001 1.133496229e+001 1.133497328e+001 2.7e-012 13.18
112 4.7e-010 1.4e-005 1.6e-008 9.92e-001 1.133496995e+001 1.133497056e+001 1.6e-013 13.21
Interior-point optimizer terminated. Time: 13.23.
Optimizer terminated. Time: 13.59
solsta = 1, prosta = 1
Interior-point solution summary
Problem status : PRIMAL_AND_DUAL_FEASIBLE
Solution status : OPTIMAL
Primal. obj: 1.1334969949e+001 Viol. con: 1e-008 var: 0e+000
Dual. obj: 1.1334970565e+001 Viol. con: 0e+000 var: 1e-004
* End solution on dual form. *
Transforming to primal solution.
Solving took 13.6 seconds.
result packing took 25% of solve time
solution checking took 0.61% of solve time
Solving took 6 GP solves and 99.9 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 2418945.89753 force_pound * meter but the right hand side evaluated to 2375461.2666 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 32774.3746107 force_pound but the right hand side evaluated to 32399.9999979 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 2.21510116794 meter but the right hand side evaluated to 2.08160583301 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 1243582.16429 joule / kilogram but the right hand side evaluated to 1.56115473622 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 664761.592145 joule / kilogram but the right hand side evaluated to 0.667340385075 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 18.3998916076 meter but the right hand side evaluated to 16.3228911777 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 10.903626992772605 but the right hand side evaluated to 4.788858948932907 (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 10.019810238577564 but the right hand side evaluated to 4.788858939520405 (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 8.144910840435127 but the right hand side evaluated to 4.788858951213657 (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 18.3622346219 meter but the right hand side evaluated to 18.1377235128 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 18.3622346219 meter but the right hand side evaluated to 18.2420604494 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 0.2960341409051317 but the right hand side evaluated to 0.189738576715031 (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 0.23302074030080266 but the right hand side evaluated to 0.1743467210316258 (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 7.563249779561553 but the right hand side evaluated to 4.73063995980657 (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 7.58309874726689 but the right hand side evaluated to 4.757852883237864 (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 114.883s
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) (1.14.2)
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-yhcxiq
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) (1.14.2)
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-sk84lj\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-kgvz8o
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) (1.14.2)
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-hgrvfj\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) (1.14.2)
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-fqb3nf\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 25.4 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 1372944.8238 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 2.1182607537 meter ** 2 / second ** 2 but the right hand side evaluated to 2.11825781223 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 1.63010986521 meter ** 2 / second ** 2 but the right hand side evaluated to 1.63010574807 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 0.911985264127 meter ** 2 / second ** 2 but the right hand side evaluated to 0.911983814512 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)
Beginning signomial solve.
Solving took 10 GP solves and 26.7 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 1372945.2705 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 1.63010986522 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 0.911985264137 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 16.6 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2985 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 720429.8172 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 6.06 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 791679.4706 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 8.09 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 883741.3401 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 3.17 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
Using solver 'mosek'
Solving for 12129 variables.
Solving took 3.17 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 720429.8208 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 3.72 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 791679.4793 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 4.92 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 883741.3365 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 1.51 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 933393.0303 but bound is 600000.0000
Beginning signomial solve.
Solving took 10 GP solves and 6.98 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 1372945.2651 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 0.911985264137 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%)
Beginning signomial solve.
Solving took 10 GP solves and 6.5 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0537 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 1372945.2750 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 1.63010574807 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%)
Using solver 'mosek'
Solving for 702 variables.
Solving took 0.381 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 6.44 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 1002038.7230 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 1.39813215992 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 0.803919027519 meter ** 2 / second ** 2 but the right hand side evaluated to 0.803918046084 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%)
Using solver 'mosek_cli'
Solving for 702 variables.
Solving took 0.571 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 21.9 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%)
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 [11.085s]: 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 61, in __init__
cs = self.setup(*args, **kwargs) # pylint: disable=no-member
File "solar.py", line 479, in setup
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 "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkitmodels\GP\aircraft\wing\sparloading.py", line 70, in setup
constraints.extend([
UnboundLocalError: local variable 'constraints' referenced before assignment
======================================================================
ERROR [26.964s]: 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 61, in __init__
cs = self.setup(*args, **kwargs) # pylint: disable=no-member
File "solar.py", line 479, in setup
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 "d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkitmodels\GP\aircraft\wing\sparloading.py", line 70, in setup
constraints.extend([
UnboundLocalError: local variable 'constraints' referenced before assignment
----------------------------------------------------------------------
Ran 8 tests in 611.608s
FAILED (errors=2)
Generating XML reports...
Cloning into 'gplibrary'...
Checking out files: 99% (131/132)
Checking out files: 100% (132/132)
Checking out files: 100% (132/132), done.
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) (1.14.2)
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-nmpckp
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) (1.14.2)
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-48val1\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) (1.14.2)
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-08uu5l\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 0.034 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.106 seconds.
Using solver 'mosek'
Solving for 9 variables.
Solving took 0.02 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.024 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.032 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 2.76 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 985.54437151 meter * revolutions_per_minute but the right hand side evaluated to 103.04140943 meter / second (Allowable error: 0.0001%, Actual error: 0.16%)
Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585924923 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573144863 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 0.314645033953 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629895189 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 0.168936438404 meter ** 2 / second ** 2 but the right hand side evaluated to 0.16893160397 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 0.0639642380836 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631379959 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 0.0226356535422 meter ** 2 / second ** 2 but the right hand side evaluated to 0.022635400587 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)
Using solver 'mosek_cli'
Solving for 9 variables.
Solving took 0.083 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.121 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.137 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 5.07 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 0.032 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 1.92 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 1619897.4165 but bound is 700000.0000
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.077 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 3.41 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 21.546s
OK
Generating XML reports...
Cloning into 'eVTOL'...
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adding test for 'aircraft_models.py'
Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 2.888s
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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