Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171205104026)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.17679257636e-13.
Allowing negative dual variable(s) as small as -6.81579792605e-13.
Allowing negative dual variable(s) as small as -1.19862713505e-12.
Allowing negative dual variable(s) as small as -1.18537731714e-12.
Solving took 4 GP solves and 1.91 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.17679257636e-13.
Allowing negative dual variable(s) as small as -6.81579792605e-13.
Allowing negative dual variable(s) as small as -1.19862713505e-12.
Allowing negative dual variable(s) as small as -1.18537731714e-12.
Solving took 4 GP solves and 2.11 seconds.
Allowing negative dual variable(s) as small as -9.5725836112e-14.
Allowing negative dual variable(s) as small as -7.33029739339e-13.
Allowing negative dual variable(s) as small as -7.32822981984e-13.
Allowing negative dual variable(s) as small as -5.95630889391e-10.
Allowing negative dual variable(s) as small as -4.87301415582e-13.
Allowing negative dual variable(s) as small as -3.64114391849e-14.
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 -1.90055490876e-14.
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 -8.88423020754e-12.
Allowing negative dual variable(s) as small as -2.87609104575e-12.
Allowing negative dual variable(s) as small as -4.72558199966e-12.
Allowing negative dual variable(s) as small as -4.72780174951e-12.
Solving took 4 GP solves and 3.02 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 2.84 seconds.
Max payload weight [lbf] = 9.228
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -9.5725836112e-14.
Allowing negative dual variable(s) as small as -7.33029739339e-13.
Allowing negative dual variable(s) as small as -7.32822981984e-13.
Allowing negative dual variable(s) as small as -5.95630889391e-10.
Allowing negative dual variable(s) as small as -4.87301415582e-13.
Allowing negative dual variable(s) as small as -3.64114391849e-14.
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 -1.90055490876e-14.
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 -8.88423020754e-12.
Allowing negative dual variable(s) as small as -2.87609104575e-12.
Allowing negative dual variable(s) as small as -4.72558199966e-12.
Allowing negative dual variable(s) as small as -4.72780174951e-12.
Solving took 4 GP solves and 2.94 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 2.96 seconds.
Max payload weight [lbf] = 9.228
Max take off weight [lbf] = 140.364
	

Standard Error