Passed
gpkit.tests.from_paths.TestFiles.test_gassolar_solar_solar_py_mosek (from gpkit.tests.from_paths.TestFiles-20171013164851)
Standard Output
Using solver 'mosek' Solving for 554 variables. Solving took 0.164 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 0.148 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 0.178 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 0.183 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 0.029 seconds. Using solver 'mosek_cli' Solving for 79 variables. Solving took 0.069 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 0.214978769982 but the right hand side evaluated to 0.214980239515 (Allowable error: 0.0001%, Actual error: 0.00068%) 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 0.201770977408 but the right hand side evaluated to 0.201783656225 (Allowable error: 0.0001%, Actual error: 0.0063%) 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 0.197669862696 but the right hand side evaluated to 0.197679318597 (Allowable error: 0.0001%, Actual error: 0.0048%) 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 0.201770977408 but the right hand side evaluated to 0.201783656225 (Allowable error: 0.0001%, Actual error: 0.0063%) 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 0.214978984961 but the right hand side evaluated to 0.214969490772 (Allowable error: 0.0001%, Actual error: 0.0044%) Using solver 'mosek' Solving for 1057 variables. Solving took 0.499 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 135385.3686 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. Allowing negative dual variable(s) as small as -1.23856030987e-09. Allowing negative dual variable(s) as small as -2.21454660165e-10. Solving took 5 GP solves and 2.53 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 137254.6978 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 137255.9451 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 0.529 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. Allowing negative dual variable(s) as small as -4.557955e-10. Allowing negative dual variable(s) as small as -4.173745e-13. Allowing negative dual variable(s) as small as -2.426222e-09. Allowing negative dual variable(s) as small as -3.89282e-09. Solving took 5 GP solves and 3.99 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
c:\users\jenkins\workspace\gpkit_commons_pr_models\buildnode\windows10x64\optimizer\mosek\gassolar\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun)