Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171115180956)

Standard Output

Allowing negative dual variable(s) as small as -1.21134872966e-13.
Allowing negative dual variable(s) as small as -8.1382817152e-14.
Allowing negative dual variable(s) as small as -2.07221392823e-14.
Allowing negative dual variable(s) as small as -2.05686162547e-14.
Allowing negative dual variable(s) as small as -1.04649470513e-12.
Allowing negative dual variable(s) as small as -1.6471277467e-12.
Allowing negative dual variable(s) as small as -1.46450690117e-12.
Allowing negative dual variable(s) as small as -1.46574419269e-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 -1.13169716653e-12.
Allowing negative dual variable(s) as small as -1.65434419636e-12.
Allowing negative dual variable(s) as small as -1.63504366296e-12.
Allowing negative dual variable(s) as small as -1.64076803359e-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 -1.25445698033e-11.
Allowing negative dual variable(s) as small as -4.86405968411e-11.
Allowing negative dual variable(s) as small as -4.13818927991e-12.
Allowing negative dual variable(s) as small as -4.13941169686e-12.
Solving took 4 GP solves and 2.96 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.82 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21114923646e-13.
Allowing negative dual variable(s) as small as -8.14582776232e-14.
Allowing negative dual variable(s) as small as -2.06206579589e-14.
Allowing negative dual variable(s) as small as -2.07516295814e-14.
Allowing negative dual variable(s) as small as -1.03920843285e-12.
Allowing negative dual variable(s) as small as -1.64634126644e-12.
Allowing negative dual variable(s) as small as -1.46239921214e-12.
Allowing negative dual variable(s) as small as -1.46779637056e-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 -1.1271981612e-12.
Allowing negative dual variable(s) as small as -1.65860142461e-12.
Allowing negative dual variable(s) as small as -1.63594094868e-12.
Allowing negative dual variable(s) as small as -1.6389248899e-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 -1.25444629358e-11.
Allowing negative dual variable(s) as small as -4.86406004485e-11.
Allowing negative dual variable(s) as small as -4.13814078108e-12.
Allowing negative dual variable(s) as small as -4.13940376258e-12.
Solving took 4 GP solves and 2.64 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.68 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
	

Standard Error