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Passed

gpkit.tests.from_paths.TestFiles.test_gassolar_gas_gas_simple_gassimple_py_mosek (from gpkit.tests.from_paths.TestFiles-20171013172918)

Took 0.36 sec.

Standard Output

Using solver 'mosek'
Solving for 554 variables.
Solving took 0.0853 seconds.
Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955
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
Using solver 'mosek'
Solving for 554 variables.
Solving took 0.0886 seconds.
Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955
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
Using solver 'mosek'
Solving for 554 variables.
Solving took 0.0833 seconds.
Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955
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
Using solver 'mosek_cli'
Solving for 554 variables.
Solving took 0.258 seconds.
Warning: Variable P_{ref}_Mission/Aircraft/Engine**-1*P_{sl-max}_Mission/Aircraft/Engine could cause inaccurate result because it is below lower bound. Solution is 0.2682 but bound is 0.2955
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
Warning: Constraint [z_{bre}_Mission/Climb/FlightSegment/BreguetEndurance_(2,)... >= 4.02*BSFC_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(2,)*P_{total}_Mission/Climb/FlightSeg...] is not tight because the left hand side evaluated to 0.000749180961118 but the right hand side evaluated to 0.000749181778306 (Allowable error: 0.0001%, Actual error: 0.00011%)

Using solver 'mosek'
Solving for 79 variables.
Solving took 0.0178 seconds.
Using solver 'mosek_cli'
Solving for 79 variables.
Solving took 0.24 seconds.
Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(0,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(0,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.21497919994 but the right hand side evaluated to 0.214980884457 (Allowable error: 0.0001%, Actual error: 0.00078%)

Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(1,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(1,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.20177138095 but the right hand side evaluated to 0.201764084159 (Allowable error: 0.0001%, Actual error: 0.0036%)

Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(2,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(2,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.197670258036 but the right hand side evaluated to 0.197660144633 (Allowable error: 0.0001%, Actual error: 0.0051%)

Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(3,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(3,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.20177138095 but the right hand side evaluated to 0.201764084159 (Allowable error: 0.0001%, Actual error: 0.0036%)

Warning: Constraint [z_{bre}_Mission/Loiter/FlightSegment/BreguetEndurance_(4,)... >= 2.45*BSFC_Mission/Loiter/FlightSegment/AircraftPerf_(4,)*P_{total}_Mission/Loiter/FlightSegment/Airc...] is not tight because the left hand side evaluated to 0.21497919994 but the right hand side evaluated to 0.214980884457 (Allowable error: 0.0001%, Actual error: 0.00078%)

Using solver 'mosek'
Solving for 1057 variables.
Solving took 0.241 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 135385.4203 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 135386.6378 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Beginning signomial solve.
Solving took 5 GP solves and 2.75 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 137254.6796 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 137255.9458 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Using solver 'mosek_cli'
Solving for 1057 variables.
Solving took 0.509 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 135385.2910 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 135386.6449 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Beginning signomial solve.
Solving took 5 GP solves and 3.46 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 137254.2055 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 137255.5780 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
	

Standard Error

/Users/jenkins/workspace/gpkit_commons_PR_Models/buildnode/macys/optimizer/mosek/gassolar/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)