Using solver 'mosek'
Solving for 575 variables.
Solving took 9.49 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 0.2658 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
Beginning signomial solve.
Solving took 4 GP solves and 20.9 seconds.
Warning: Variable P_{ref}_Mission.1/Aircraft.1/Engine.1**-1*P_{sl-max}_Mission.1/Aircraft.1/Engine.1 could cause inaccurate result because it is below lower bound. Solution is 0.2680 but bound is 0.2955
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 575 variables.
Solving took 5.4 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 0.2658 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
Beginning signomial solve.
Solving took 4 GP solves and 17.8 seconds.
Warning: Variable P_{ref}_Mission.1/Aircraft.1/Engine.1**-1*P_{sl-max}_Mission.1/Aircraft.1/Engine.1 could cause inaccurate result because it is below lower bound. Solution is 0.2680 but bound is 0.2955
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 79 variables.
Solving took 1.43 seconds.
Using solver 'mosek_cli'
Solving for 79 variables.
Solving took 1.45 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 0.214978555003 but the right hand side evaluated to 0.214980024535 (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 0.201770775637 but the right hand side evaluated to 0.201763277105 (Allowable error: 0.0001%, Actual error: 0.0037%)

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 0.197679120917 (Allowable error: 0.0001%, Actual error: 0.0047%)

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 0.201763277105 (Allowable error: 0.0001%, Actual error: 0.0038%)

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 0.214978769982 but the right hand side evaluated to 0.214980024535 (Allowable error: 0.0001%, Actual error: 0.00058%)

Using solver 'mosek'
Solving for 1188 variables.
Solving took 0.789 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 130051.7624 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 130053.4104 but bound is 150000.0000
1 is a constraining latitude
11 is a constraining latitude
Beginning signomial solve.
Solving took 4 GP solves and 2.86 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 132099.7709 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 132101.4445 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 0.711 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 4.19 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

/Users/jenkins/workspace/gplibrary_PR_Models/buildnode/macys/optimizer/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)