Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180402113157)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.05770380973847e-14.
Allowing negative dual variable(s) as small as -7.965893569772398e-14.
Allowing negative dual variable(s) as small as -1.4951278062835804e-13.
Allowing negative dual variable(s) as small as -1.469961305455847e-13.
Solving took 4 GP solves and 3.19 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.9432987964978e-14.
Allowing negative dual variable(s) as small as -8.251602526265778e-14.
Allowing negative dual variable(s) as small as -1.4954747509787758e-13.
Allowing negative dual variable(s) as small as -1.4717220497839634e-13.
Solving took 4 GP solves and 2.95 seconds.
Allowing negative dual variable(s) as small as -5.249602835766254e-13.
Allowing negative dual variable(s) as small as -5.109732081898244e-13.
Allowing negative dual variable(s) as small as -5.156135934880623e-13.
Allowing negative dual variable(s) as small as -5.155511434429272e-13.
Allowing negative dual variable(s) as small as -2.3156476736119203e-13.
Allowing negative dual variable(s) as small as -1.916175551563981e-14.
Allowing negative dual variable(s) as small as -1.260344042672279e-12.
Allowing negative dual variable(s) as small as -1.2586424957827802e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -2.02546313055052e-14.
Allowing negative dual variable(s) as small as -1.1310635587846729e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.434130231323337e-11.
Allowing negative dual variable(s) as small as -6.449652839282983e-12.
Allowing negative dual variable(s) as small as -1.9339319135154884e-11.
Allowing negative dual variable(s) as small as -1.9354586531519935e-11.
Solving took 4 GP solves and 2.78 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.83 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.253349838474364e-13.
Allowing negative dual variable(s) as small as -5.118162837991491e-13.
Allowing negative dual variable(s) as small as -5.16090642443956e-13.
Allowing negative dual variable(s) as small as -5.141616299386698e-13.
Allowing negative dual variable(s) as small as -2.380292143944196e-13.
Allowing negative dual variable(s) as small as -1.7961001609612115e-14.
Allowing negative dual variable(s) as small as -1.2610969126608529e-12.
Allowing negative dual variable(s) as small as -1.2586780576140377e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -2.04116237800811e-14.
Allowing negative dual variable(s) as small as -1.1412507223973467e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.434123826335476e-11.
Allowing negative dual variable(s) as small as -6.449679122080061e-12.
Allowing negative dual variable(s) as small as -1.9339112068951203e-11.
Allowing negative dual variable(s) as small as -1.9354606817270807e-11.
Solving took 4 GP solves and 2.97 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.74 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error