Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171016093527)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.48438464781e-13.
Allowing negative dual variable(s) as small as -3.36647810323e-13.
Allowing negative dual variable(s) as small as -5.21676452037e-13.
Allowing negative dual variable(s) as small as -5.4175544259e-13.
Solving took 4 GP solves and 2.86 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.48687831281e-13.
Allowing negative dual variable(s) as small as -3.37023811636e-13.
Allowing negative dual variable(s) as small as -5.45741837138e-13.
Allowing negative dual variable(s) as small as -5.36242057703e-13.
Solving took 4 GP solves and 2.64 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000
Allowing negative dual variable(s) as small as -8.57188452164e-13.
Allowing negative dual variable(s) as small as -7.72677928584e-13.
Allowing negative dual variable(s) as small as -7.38573265047e-13.
Allowing negative dual variable(s) as small as -7.40963713997e-13.
Allowing negative dual variable(s) as small as -7.41205707921e-13.
Allowing negative dual variable(s) as small as -1.5210369856e-12.
Allowing negative dual variable(s) as small as -1.04771649256e-12.
Allowing negative dual variable(s) as small as -1.06172915511e-12.
Allowing negative dual variable(s) as small as -1.06049956143e-12.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -1.48838558665e-12.
Allowing negative dual variable(s) as small as -1.14066742163e-13.
Allowing negative dual variable(s) as small as -6.93737602087e-15.
Allowing negative dual variable(s) as small as -1.62405570762e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.50673062453e-14.
Allowing negative dual variable(s) as small as -1.0810979109e-12.
Solving took 4 GP solves and 2.55 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Solving took 4 GP solves and 1.74 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.56776455338e-13.
Allowing negative dual variable(s) as small as -7.72753389056e-13.
Allowing negative dual variable(s) as small as -7.38518621257e-13.
Allowing negative dual variable(s) as small as -7.41347955246e-13.
Allowing negative dual variable(s) as small as -7.41762554157e-13.
Allowing negative dual variable(s) as small as -1.52109770092e-12.
Allowing negative dual variable(s) as small as -1.04905320542e-12.
Allowing negative dual variable(s) as small as -1.061081778e-12.
Allowing negative dual variable(s) as small as -1.06327631162e-12.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -1.48049996741e-12.
Allowing negative dual variable(s) as small as -1.13952250413e-13.
Allowing negative dual variable(s) as small as -6.2141047516e-15.
Allowing negative dual variable(s) as small as -1.60776340158e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.49241646652e-14.
Allowing negative dual variable(s) as small as -1.08101979286e-12.
Solving took 4 GP solves and 2.26 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Solving took 4 GP solves and 1.91 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
	

Standard Error