Skip to content

Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171120112434)

Took 25 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.03763785758e-13.
Allowing negative dual variable(s) as small as -1.99518136387e-12.
Allowing negative dual variable(s) as small as -2.16451726334e-12.
Allowing negative dual variable(s) as small as -2.15356291827e-12.
Solving took 4 GP solves and 4.3 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.00577532414e-13.
Allowing negative dual variable(s) as small as -2.03671107757e-12.
Allowing negative dual variable(s) as small as -2.15526294728e-12.
Allowing negative dual variable(s) as small as -2.16674074516e-12.
Solving took 4 GP solves and 21.9 seconds.
Allowing negative dual variable(s) as small as -1.21091504879e-13.
Allowing negative dual variable(s) as small as -8.14790943049e-14.
Allowing negative dual variable(s) as small as -2.09103567794e-14.
Allowing negative dual variable(s) as small as -2.07438233257e-14.
Allowing negative dual variable(s) as small as -1.04499547036e-12.
Allowing negative dual variable(s) as small as -1.64912332921e-12.
Allowing negative dual variable(s) as small as -1.46674794706e-12.
Allowing negative dual variable(s) as small as -1.4637648732e-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 -1.12435516626e-12.
Allowing negative dual variable(s) as small as -1.65437628874e-12.
Allowing negative dual variable(s) as small as -1.63481337842e-12.
Allowing negative dual variable(s) as small as -1.63589996584e-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 -1.25445655857e-11.
Allowing negative dual variable(s) as small as -4.86406468872e-11.
Allowing negative dual variable(s) as small as -4.13824355944e-12.
Allowing negative dual variable(s) as small as -4.13945514143e-12.
Solving took 4 GP solves and 3.8 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.65 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21203394543e-13.
Allowing negative dual variable(s) as small as -8.14201137067e-14.
Allowing negative dual variable(s) as small as -2.06579545137e-14.
Allowing negative dual variable(s) as small as -2.06267294911e-14.
Allowing negative dual variable(s) as small as -1.04153426335e-12.
Allowing negative dual variable(s) as small as -1.64705033466e-12.
Allowing negative dual variable(s) as small as -1.46549048938e-12.
Allowing negative dual variable(s) as small as -1.46697389479e-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 -1.12627311991e-12.
Allowing negative dual variable(s) as small as -1.65583931115e-12.
Allowing negative dual variable(s) as small as -1.63609425487e-12.
Allowing negative dual variable(s) as small as -1.63563997416e-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 -1.25445402051e-11.
Allowing negative dual variable(s) as small as -4.86406995624e-11.
Allowing negative dual variable(s) as small as -4.1382071953e-12.
Allowing negative dual variable(s) as small as -4.13938552624e-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 14.6 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
	

Standard Error