Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171018105908)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.60143423101e-14.
Allowing negative dual variable(s) as small as -1.18171358116e-12.
Allowing negative dual variable(s) as small as -1.13149593861e-12.
Allowing negative dual variable(s) as small as -1.12203779254e-12.
Solving took 4 GP solves and 7.26 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.53911429014e-14.
Allowing negative dual variable(s) as small as -1.19370529086e-12.
Allowing negative dual variable(s) as small as -1.14825380107e-12.
Allowing negative dual variable(s) as small as -1.13707090618e-12.
Solving took 4 GP solves and 9.44 seconds.
Allowing negative dual variable(s) as small as -1.56921264177e-12.
Allowing negative dual variable(s) as small as -3.96066946601e-12.
Allowing negative dual variable(s) as small as -1.78666630102e-12.
Allowing negative dual variable(s) as small as -2.08273242402e-12.
Allowing negative dual variable(s) as small as -2.08098469012e-12.
Allowing negative dual variable(s) as small as -4.70043491976e-13.
Allowing negative dual variable(s) as small as -8.92672220865e-13.
Allowing negative dual variable(s) as small as -9.40715495952e-13.
Allowing negative dual variable(s) as small as -9.43087947146e-13.
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 = 21.712
speed at top of climb [m/s] = 26.507
design loiter speed [m/s] = 25.048
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 -2.32862340521e-13.
Allowing negative dual variable(s) as small as -9.25695067475e-14.
Allowing negative dual variable(s) as small as -1.202335757e-13.
Allowing negative dual variable(s) as small as -1.18989345287e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.166
optimum loiter speed for min power, end of loiter [m/s] = 17.158
optimum cruise speed, inbound [m/s] = 35.697
optimum cruise speed, outbound [m/s] = 25.443
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.6184717757e-13.
Allowing negative dual variable(s) as small as -2.01656353023e-12.
Allowing negative dual variable(s) as small as -1.26470676231e-14.
Allowing negative dual variable(s) as small as -1.70055480216e-14.
Solving took 4 GP solves and 5.91 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 1021559.0193 but bound is 1000000.0000
Max Speed [m/s]: 73.83
Beginning signomial solve.
Solving took 4 GP solves and 1.97 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56983714222e-12.
Allowing negative dual variable(s) as small as -3.96076574316e-12.
Allowing negative dual variable(s) as small as -1.78690569286e-12.
Allowing negative dual variable(s) as small as -2.08271507679e-12.
Allowing negative dual variable(s) as small as -2.08091183174e-12.
Allowing negative dual variable(s) as small as -4.74835448738e-13.
Allowing negative dual variable(s) as small as -8.94500185727e-13.
Allowing negative dual variable(s) as small as -9.39979864778e-13.
Allowing negative dual variable(s) as small as -9.4357898231e-13.
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 = 21.712
speed at top of climb [m/s] = 26.507
design loiter speed [m/s] = 25.048
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 -2.33122332202e-13.
Allowing negative dual variable(s) as small as -9.12979544396e-14.
Allowing negative dual variable(s) as small as -1.2031380666e-13.
Allowing negative dual variable(s) as small as -1.19540770512e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.166
optimum loiter speed for min power, end of loiter [m/s] = 17.158
optimum cruise speed, inbound [m/s] = 35.697
optimum cruise speed, outbound [m/s] = 25.443
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.61723189311e-13.
Allowing negative dual variable(s) as small as -2.01692647318e-12.
Allowing negative dual variable(s) as small as -1.27271074721e-14.
Allowing negative dual variable(s) as small as -1.70164671233e-14.
Solving took 4 GP solves and 23.5 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 1021559.0193 but bound is 1000000.0000
Max Speed [m/s]: 73.83
Beginning signomial solve.
Solving took 4 GP solves and 2.73 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error