Passed

gpkit.tests.from_paths.TestFiles.test_gassolar_solar_solar_py_mosek (from gpkit.tests.from_paths.TestFiles-20171101154519)

Took 16 sec.

Standard Output

\mathcal{V}_Mission/Aircraft/Fuselage has no lower bound
Using solver 'mosek'
Solving for 575 variables.
Solving took 1.48 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 0.1410 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
\mathcal{V}_Mission/Aircraft/Fuselage has no lower bound
Using solver 'mosek'
Solving for 575 variables.
Solving took 1.21 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 0.1410 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
\mathcal{V}_Mission/Aircraft/Fuselage has no lower bound
Using solver 'mosek'
Solving for 575 variables.
Solving took 0.174 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 0.1410 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
\mathcal{V}_Mission/Aircraft/Fuselage has no lower bound
Using solver 'mosek_cli'
Solving for 575 variables.
Solving took 0.225 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 0.1410 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_(0,)... >= 4.02*BSFC_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)*P_{total}_Mission/Climb/FlightSeg...] is not tight because the left hand side evaluated to 0.000696022897127 but the right hand side evaluated to 0.000696023865138 (Allowable error: 0.0001%, Actual error: 0.00014%)

Warning: Constraint [z_{bre}_Mission/Climb/FlightSegment/BreguetEndurance_(4,)... >= 4.02*BSFC_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(4,)*P_{total}_Mission/Climb/FlightSeg...] is not tight because the left hand side evaluated to 0.000820827155425 but the right hand side evaluated to 0.000820828009721 (Allowable error: 0.0001%, Actual error: 0.0001%)

Warning: Constraint [z_{bre}_Mission/Climb/FlightSegment/BreguetEndurance_(8,)... >= 4.02*BSFC_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(8,)*P_{total}_Mission/Climb/FlightSeg...] is not tight because the left hand side evaluated to 0.00122871545603 but the right hand side evaluated to 0.00122871704202 (Allowable error: 0.0001%, Actual error: 0.00013%)

Using solver 'mosek'
Solving for 79 variables.
Solving took 0.038 seconds.
Using solver 'mosek_cli'
Solving for 79 variables.
Solving took 0.078 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 0.214977910069 but the right hand side evaluated to 0.214978949638 (Allowable error: 0.0001%, Actual error: 0.00048%)

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 0.201770170325 but the right hand side evaluated to 0.201782445526 (Allowable error: 0.0001%, Actual error: 0.0061%)

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 0.197669269687 but the right hand side evaluated to 0.197678132524 (Allowable error: 0.0001%, Actual error: 0.0045%)

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 0.201770372096 but the right hand side evaluated to 0.201782445526 (Allowable error: 0.0001%, Actual error: 0.006%)

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 0.214978340025 but the right hand side evaluated to 0.214968200959 (Allowable error: 0.0001%, Actual error: 0.0047%)

Using solver 'mosek'
Solving for 1188 variables.
Solving took 2.1 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 130051.7616 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 130053.4106 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Beginning signomial solve.
Solving took 4 GP solves and 2.93 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 132099.7690 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 132101.4444 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Using solver 'mosek_cli'
Solving for 1188 variables.
Solving took 0.563 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 130052.0456 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 130053.3461 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Beginning signomial solve.
Solving took 4 GP solves and 2.54 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 132099.4068 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 132102.0488 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude

Standard Error

D:\jenkins\workspace\gpkit_commons_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)