Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171016200542)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.47453920874e-14.
Allowing negative dual variable(s) as small as -1.19462599535e-12.
Allowing negative dual variable(s) as small as -1.14007718197e-12.
Allowing negative dual variable(s) as small as -1.13723613859e-12.
Solving took 4 GP solves and 24.7 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.57328834261e-14.
Allowing negative dual variable(s) as small as -1.18891918879e-12.
Allowing negative dual variable(s) as small as -1.13684105532e-12.
Allowing negative dual variable(s) as small as -1.13515707251e-12.
Solving took 4 GP solves and 28.6 seconds.
Allowing negative dual variable(s) as small as -1.56959341358e-12.
Allowing negative dual variable(s) as small as -3.96077181469e-12.
Allowing negative dual variable(s) as small as -1.7870566138e-12.
Allowing negative dual variable(s) as small as -2.08209924996e-12.
Allowing negative dual variable(s) as small as -2.08121454098e-12.
Allowing negative dual variable(s) as small as -4.70081872733e-13.
Allowing negative dual variable(s) as small as -8.9276958222e-13.
Allowing negative dual variable(s) as small as -9.41011157884e-13.
Allowing negative dual variable(s) as small as -9.42920763171e-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 -2.35845848059e-13.
Allowing negative dual variable(s) as small as -9.2893141096e-14.
Allowing negative dual variable(s) as small as -1.19782222335e-13.
Allowing negative dual variable(s) as small as -1.20864472944e-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 -9.61767590778e-13.
Allowing negative dual variable(s) as small as -2.01671313579e-12.
Allowing negative dual variable(s) as small as -1.32988465588e-14.
Allowing negative dual variable(s) as small as -1.74847318182e-14.
Solving took 4 GP solves and 2.4 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 1.95 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56930544948e-12.
Allowing negative dual variable(s) as small as -3.96082645848e-12.
Allowing negative dual variable(s) as small as -1.78648155297e-12.
Allowing negative dual variable(s) as small as -2.08192317552e-12.
Allowing negative dual variable(s) as small as -2.08128826673e-12.
Allowing negative dual variable(s) as small as -4.76220408593e-13.
Allowing negative dual variable(s) as small as -8.92878652958e-13.
Allowing negative dual variable(s) as small as -9.41636742538e-13.
Allowing negative dual variable(s) as small as -9.43203523097e-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 -2.35181448968e-13.
Allowing negative dual variable(s) as small as -9.20166720597e-14.
Allowing negative dual variable(s) as small as -1.20116807126e-13.
Allowing negative dual variable(s) as small as -1.2012905861e-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 -9.61714127752e-13.
Allowing negative dual variable(s) as small as -2.01707719788e-12.
Allowing negative dual variable(s) as small as -1.24526506918e-14.
Allowing negative dual variable(s) as small as -1.75172604244e-14.
Solving took 4 GP solves and 4.22 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 1.95 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error