Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171011222013)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.58326128386e-12.
Allowing negative dual variable(s) as small as -5.01693131483e-12.
Allowing negative dual variable(s) as small as -4.78298086901e-12.
Allowing negative dual variable(s) as small as -1.07114547267e-11.
Solving took 4 GP solves and 2.78 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 1155331.2268 but bound is 1000000.0000
Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.2259923779e-12.
Allowing negative dual variable(s) as small as -4.97397782684e-12.
Allowing negative dual variable(s) as small as -8.91426385832e-12.
Allowing negative dual variable(s) as small as -1.96559079776e-11.
Solving took 4 GP solves and 5.96 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 1155331.2266 but bound is 1000000.0000
Allowing negative dual variable(s) as small as -1.61638966101e-11.
Allowing negative dual variable(s) as small as -6.10381190036e-12.
Allowing negative dual variable(s) as small as -1.16488971247e-11.
Allowing negative dual variable(s) as small as -6.58614135451e-12.
Allowing negative dual variable(s) as small as -6.60797111474e-12.
Allowing negative dual variable(s) as small as -1.10166838759e-11.
Allowing negative dual variable(s) as small as -1.16806978586e-11.
Allowing negative dual variable(s) as small as -1.10543330132e-11.
Allowing negative dual variable(s) as small as -1.11160854827e-11.
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 -1.79887838566e-11.
Allowing negative dual variable(s) as small as -6.27697351561e-12.
Allowing negative dual variable(s) as small as -1.04084588171e-11.
Allowing negative dual variable(s) as small as -1.04263696201e-11.
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 -5.91634641262e-12.
Allowing negative dual variable(s) as small as -1.23253561135e-13.
Allowing negative dual variable(s) as small as -8.83949693473e-14.
Allowing negative dual variable(s) as small as -9.08041127379e-14.
Solving took 4 GP solves and 5.96 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.
Allowing negative dual variable(s) as small as -9.90973479491e-11.
Allowing negative dual variable(s) as small as -8.92988595395e-11.
Allowing negative dual variable(s) as small as -8.98746181643e-11.
Allowing negative dual variable(s) as small as -8.47864855581e-11.
Solving took 4 GP solves and 1.56 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -1.61430521728e-11.
Allowing negative dual variable(s) as small as -6.13082501433e-12.
Allowing negative dual variable(s) as small as -1.1669283595e-11.
Allowing negative dual variable(s) as small as -6.61326549078e-12.
Allowing negative dual variable(s) as small as -6.61901783383e-12.
Allowing negative dual variable(s) as small as -1.10113662979e-11.
Allowing negative dual variable(s) as small as -1.16825492422e-11.
Allowing negative dual variable(s) as small as -1.10539772865e-11.
Allowing negative dual variable(s) as small as -1.11122103272e-11.
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 -1.79868845512e-11.
Allowing negative dual variable(s) as small as -6.27746281606e-12.
Allowing negative dual variable(s) as small as -1.04097331883e-11.
Allowing negative dual variable(s) as small as -1.04257689721e-11.
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 -5.9163468895e-12.
Allowing negative dual variable(s) as small as -2.15950926553e-13.
Allowing negative dual variable(s) as small as -8.83704913657e-14.
Allowing negative dual variable(s) as small as -9.08296356405e-14.
Solving took 4 GP solves and 7.93 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.
Allowing negative dual variable(s) as small as -9.91035261667e-11.
Allowing negative dual variable(s) as small as -8.93118010103e-11.
Allowing negative dual variable(s) as small as -8.98862048161e-11.
Allowing negative dual variable(s) as small as -8.47962902152e-11.
Solving took 4 GP solves and 1.5 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
	

Standard Error