Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171115192302)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.97409620174e-14.
Allowing negative dual variable(s) as small as -2.03201171167e-12.
Allowing negative dual variable(s) as small as -2.15421430694e-12.
Allowing negative dual variable(s) as small as -2.16857001106e-12.
Solving took 4 GP solves and 2.66 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.01422342746e-13.
Allowing negative dual variable(s) as small as -2.09753048264e-12.
Allowing negative dual variable(s) as small as -2.16318456203e-12.
Allowing negative dual variable(s) as small as -2.16751226342e-12.
Solving took 4 GP solves and 2.82 seconds.
Allowing negative dual variable(s) as small as -1.21212935522e-13.
Allowing negative dual variable(s) as small as -8.15406769883e-14.
Allowing negative dual variable(s) as small as -2.05981065537e-14.
Allowing negative dual variable(s) as small as -2.07611705605e-14.
Allowing negative dual variable(s) as small as -1.04359446432e-12.
Allowing negative dual variable(s) as small as -1.64691155678e-12.
Allowing negative dual variable(s) as small as -1.46315056425e-12.
Allowing negative dual variable(s) as small as -1.46976831747e-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 -1.12454186588e-12.
Allowing negative dual variable(s) as small as -1.65809466851e-12.
Allowing negative dual variable(s) as small as -1.6347741303e-12.
Allowing negative dual variable(s) as small as -1.63483766455e-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 -1.25445460816e-11.
Allowing negative dual variable(s) as small as -4.86405884123e-11.
Allowing negative dual variable(s) as small as -4.13823349712e-12.
Allowing negative dual variable(s) as small as -4.13942520848e-12.
Solving took 4 GP solves and 2.4 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.89 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21167832712e-13.
Allowing negative dual variable(s) as small as -8.13394490651e-14.
Allowing negative dual variable(s) as small as -2.07004552388e-14.
Allowing negative dual variable(s) as small as -2.06683628545e-14.
Allowing negative dual variable(s) as small as -1.04674602319e-12.
Allowing negative dual variable(s) as small as -1.64491055325e-12.
Allowing negative dual variable(s) as small as -1.46737548327e-12.
Allowing negative dual variable(s) as small as -1.46703374275e-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 -1.12424240924e-12.
Allowing negative dual variable(s) as small as -1.65549518538e-12.
Allowing negative dual variable(s) as small as -1.6369277895e-12.
Allowing negative dual variable(s) as small as -1.63832836186e-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 -1.25443510905e-11.
Allowing negative dual variable(s) as small as -4.86408333585e-11.
Allowing negative dual variable(s) as small as -4.13819129284e-12.
Allowing negative dual variable(s) as small as -4.13946521354e-12.
Solving took 4 GP solves and 2.32 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.78 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
	

Standard Error