Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180110090622)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.9915566551741435e-13.
Allowing negative dual variable(s) as small as -4.800053583775554e-13.
Allowing negative dual variable(s) as small as -9.062824275762882e-14.
Allowing negative dual variable(s) as small as -1.0795617871872665e-13.
Solving took 4 GP solves and 2.68 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.9056314646003223e-13.
Allowing negative dual variable(s) as small as -4.718736252434796e-13.
Allowing negative dual variable(s) as small as -8.699638232023688e-14.
Allowing negative dual variable(s) as small as -1.4872131304244363e-13.
Solving took 4 GP solves and 2.8 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 -5.027304399061786e-12.
Allowing negative dual variable(s) as small as -1.107190483904694e-12.
Allowing negative dual variable(s) as small as -2.483434031665436e-12.
Allowing negative dual variable(s) as small as -2.4819386855319764e-12.
Solving took 4 GP solves and 2.31 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.59 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 -5.027411538704184e-12.
Allowing negative dual variable(s) as small as -1.1072140989715051e-12.
Allowing negative dual variable(s) as small as -2.4831202985828544e-12.
Allowing negative dual variable(s) as small as -2.4819663291321526e-12.
Solving took 4 GP solves and 2.31 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.6 seconds.
Max payload weight [lbf] = 9.202
Max take off weight [lbf] = 140.328
	

Standard Error