Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180420143516)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.10480155211124e-14.
Allowing negative dual variable(s) as small as -8.585233218783017e-14.
Allowing negative dual variable(s) as small as -1.4821043697876846e-13.
Allowing negative dual variable(s) as small as -1.4961816507952364e-13.
Solving took 4 GP solves and 2.98 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.972572255154908e-14.
Allowing negative dual variable(s) as small as -8.457427466690426e-14.
Allowing negative dual variable(s) as small as -1.5054450741569525e-13.
Allowing negative dual variable(s) as small as -1.486415157625487e-13.
Solving took 4 GP solves and 2.93 seconds.
Allowing negative dual variable(s) as small as -5.262110192028047e-13.
Allowing negative dual variable(s) as small as -5.104319744653196e-13.
Allowing negative dual variable(s) as small as -5.153932836066133e-13.
Allowing negative dual variable(s) as small as -5.167706540465389e-13.
Allowing negative dual variable(s) as small as -2.3708986163217816e-13.
Allowing negative dual variable(s) as small as -1.844000212941621e-14.
Allowing negative dual variable(s) as small as -1.2594758135725526e-12.
Allowing negative dual variable(s) as small as -1.2596225061264898e-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 -2.1518811038623298e-14.
Allowing negative dual variable(s) as small as -1.149236955599875e-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 -5.4341189432328866e-11.
Allowing negative dual variable(s) as small as -6.449673910868672e-12.
Allowing negative dual variable(s) as small as -1.9339088553437233e-11.
Allowing negative dual variable(s) as small as -1.9354482306286297e-11.
Solving took 4 GP solves and 2.43 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.63 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.236609756931188e-13.
Allowing negative dual variable(s) as small as -5.117867935000575e-13.
Allowing negative dual variable(s) as small as -5.153603238605697e-13.
Allowing negative dual variable(s) as small as -5.144235731835423e-13.
Allowing negative dual variable(s) as small as -2.427246771630198e-13.
Allowing negative dual variable(s) as small as -1.8912931117054388e-14.
Allowing negative dual variable(s) as small as -1.2603665940774667e-12.
Allowing negative dual variable(s) as small as -1.2590469031931173e-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 -1.8507764765196555e-14.
Allowing negative dual variable(s) as small as -1.137412646706748e-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 -5.4341225522496925e-11.
Allowing negative dual variable(s) as small as -6.4495135119452196e-12.
Allowing negative dual variable(s) as small as -1.9339189836846035e-11.
Allowing negative dual variable(s) as small as -1.9354523231424297e-11.
Solving took 4 GP solves and 2.3 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.99 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error