Passed

gpkit.tests.from_paths.TestFiles.test_gassolar_gas_gas_py_mosek (from gpkit.tests.from_paths.TestFiles-20190614180218)

Standard Output

Using solver 'mosek'
Solving for 592 variables.
Solving took 0.0901 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 0.703 seconds.
Warning: Variable [P_{shaft-max}_Mission.1/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission.1/Cl 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 0.0804 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 0.618 seconds.
Warning: Variable [P_{shaft-max}_Mission.1/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission.1/Cl 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 0.318 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 102558.3538 but bound is 150000.0000
Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 102558.3827 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 2.32 seconds.
Warning: Variable Re_Mission.1/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 103379.4301 but bound is 150000.0000
Warning: Variable Re_Mission.1/FlightSegment.10/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 103406.0835 but bound is 150000.0000
Using solver 'mosek_cli'
Solving for 1250 variables.
Solving took 0.546 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 102558.6388 but bound is 150000.0000
Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 102558.6388 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 2.68 seconds.
Warning: Variable Re_Mission.1/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 103379.2971 but bound is 150000.0000
Warning: Variable Re_Mission.1/FlightSegment.10/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 103406.1793 but bound is 150000.0000
	

Standard Error

/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped.
  warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning)
/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)