Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171115180901)

Standard Output

Allowing negative dual variable(s) as small as -1.21175638967e-13.
Allowing negative dual variable(s) as small as -8.15918513308e-14.
Allowing negative dual variable(s) as small as -2.06232600442e-14.
Allowing negative dual variable(s) as small as -2.06831080041e-14.
Allowing negative dual variable(s) as small as -1.04669007836e-12.
Allowing negative dual variable(s) as small as -1.64441095289e-12.
Allowing negative dual variable(s) as small as -1.46568672997e-12.
Allowing negative dual variable(s) as small as -1.46422349072e-12.
MTOW [lbs] = 132.53
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 = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.1216975699e-12.
Allowing negative dual variable(s) as small as -1.6573582784e-12.
Allowing negative dual variable(s) as small as -1.63922868335e-12.
Allowing negative dual variable(s) as small as -1.63803606096e-12.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.25444586304e-11.
Allowing negative dual variable(s) as small as -4.86404146735e-11.
Allowing negative dual variable(s) as small as -4.13825648708e-12.
Allowing negative dual variable(s) as small as -4.13939883336e-12.
Solving took 4 GP solves and 14.4 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 8.74 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21199057734e-13.
Allowing negative dual variable(s) as small as -8.14504713675e-14.
Allowing negative dual variable(s) as small as -2.07689768161e-14.
Allowing negative dual variable(s) as small as -2.07256087292e-14.
Allowing negative dual variable(s) as small as -1.04410143725e-12.
Allowing negative dual variable(s) as small as -1.64585966383e-12.
Allowing negative dual variable(s) as small as -1.46543476139e-12.
Allowing negative dual variable(s) as small as -1.46640837494e-12.
MTOW [lbs] = 132.53
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 = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.12376124031e-12.
Allowing negative dual variable(s) as small as -1.65560143719e-12.
Allowing negative dual variable(s) as small as -1.641330084e-12.
Allowing negative dual variable(s) as small as -1.63712381325e-12.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.25445087236e-11.
Allowing negative dual variable(s) as small as -4.86405516669e-11.
Allowing negative dual variable(s) as small as -4.13814352697e-12.
Allowing negative dual variable(s) as small as -4.13934303446e-12.
Solving took 4 GP solves and 15.3 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 7.88 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
	

Standard Error