Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180110084330)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.952935205385865e-13.
Allowing negative dual variable(s) as small as -4.4202380471147773e-13.
Allowing negative dual variable(s) as small as -8.173453233673023e-14.
Allowing negative dual variable(s) as small as -8.380210587966008e-14.
Solving took 4 GP solves and 225 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.220367986693894e-13.
Allowing negative dual variable(s) as small as -4.952084749210162e-13.
Allowing negative dual variable(s) as small as -7.717286011621471e-14.
Allowing negative dual variable(s) as small as -8.22224233143487e-14.
Solving took 4 GP solves and 287 seconds.
MTOW [lbs] = 132.52
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 = 20.351
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] = 27.299
optimum loiter speed for min power, start of loiter [m/s] = 23.617
optimum loiter speed for min power, end of loiter [m/s] = 16.684
optimum cruise speed, inbound [m/s] = 31.019
optimum cruise speed, outbound [m/s] = 23.408
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.0273297855127176e-12.
Allowing negative dual variable(s) as small as -1.107122793183996e-12.
Allowing negative dual variable(s) as small as -2.4832777023630637e-12.
Allowing negative dual variable(s) as small as -2.482111002073339e-12.
Solving took 4 GP solves and 102 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 52.6 seconds.
Max payload weight [lbf] = 9.202
Max take off weight [lbf] = 140.328
MTOW [lbs] = 132.52
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 = 20.351
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] = 27.299
optimum loiter speed for min power, start of loiter [m/s] = 23.617
optimum loiter speed for min power, end of loiter [m/s] = 16.684
optimum cruise speed, inbound [m/s] = 31.019
optimum cruise speed, outbound [m/s] = 23.408
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.0271390229925875e-12.
Allowing negative dual variable(s) as small as -1.1071644457479359e-12.
Allowing negative dual variable(s) as small as -2.4832202114708416e-12.
Allowing negative dual variable(s) as small as -2.482010985584289e-12.
Solving took 4 GP solves and 63.9 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 32.9 seconds.
Max payload weight [lbf] = 9.202
Max take off weight [lbf] = 140.328
	

Standard Error