Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171018111805)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.45298526955e-14.
Allowing negative dual variable(s) as small as -1.19373738325e-12.
Allowing negative dual variable(s) as small as -1.14169004112e-12.
Allowing negative dual variable(s) as small as -1.14143026628e-12.
Solving took 4 GP solves and 14.6 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.54613992021e-14.
Allowing negative dual variable(s) as small as -1.18197639176e-12.
Allowing negative dual variable(s) as small as -1.1350712037e-12.
Allowing negative dual variable(s) as small as -1.13861481008e-12.
Solving took 4 GP solves and 20.7 seconds.
Allowing negative dual variable(s) as small as -1.57001495138e-12.
Allowing negative dual variable(s) as small as -3.96044221723e-12.
Allowing negative dual variable(s) as small as -1.78702799086e-12.
Allowing negative dual variable(s) as small as -2.08239415295e-12.
Allowing negative dual variable(s) as small as -2.08121367362e-12.
Allowing negative dual variable(s) as small as -4.76474111902e-13.
Allowing negative dual variable(s) as small as -8.9312400791e-13.
Allowing negative dual variable(s) as small as -9.41853908233e-13.
Allowing negative dual variable(s) as small as -9.44351151097e-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 -2.35982023852e-13.
Allowing negative dual variable(s) as small as -9.29305460709e-14.
Allowing negative dual variable(s) as small as -1.20347525348e-13.
Allowing negative dual variable(s) as small as -1.20569895214e-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 -9.60853434069e-13.
Allowing negative dual variable(s) as small as -2.01690541632e-12.
Allowing negative dual variable(s) as small as -1.28106338675e-14.
Allowing negative dual variable(s) as small as -1.72865041386e-14.
Solving took 4 GP solves and 21.5 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 1.45 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56937917523e-12.
Allowing negative dual variable(s) as small as -3.96107105449e-12.
Allowing negative dual variable(s) as small as -1.78685972269e-12.
Allowing negative dual variable(s) as small as -2.0827194136e-12.
Allowing negative dual variable(s) as small as -2.08152852593e-12.
Allowing negative dual variable(s) as small as -4.76375666345e-13.
Allowing negative dual variable(s) as small as -8.92024952168e-13.
Allowing negative dual variable(s) as small as -9.42817980805e-13.
Allowing negative dual variable(s) as small as -9.43904351382e-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 -2.34196776555e-13.
Allowing negative dual variable(s) as small as -9.29892014084e-14.
Allowing negative dual variable(s) as small as -1.19974668221e-13.
Allowing negative dual variable(s) as small as -1.20910117855e-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 -9.61310017227e-13.
Allowing negative dual variable(s) as small as -2.01682528996e-12.
Allowing negative dual variable(s) as small as -1.24369780942e-14.
Allowing negative dual variable(s) as small as -1.77510156834e-14.
Solving took 4 GP solves and 32.8 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 137 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error