Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180605125422)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.222081447819882e-14.
Allowing negative dual variable(s) as small as -7.84905994366536e-14.
Allowing negative dual variable(s) as small as -1.5087106911004788e-13.
Allowing negative dual variable(s) as small as -1.4810505252760287e-13.
Solving took 4 GP solves and 22.3 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.297541919024873e-14.
Allowing negative dual variable(s) as small as -7.555978412399078e-14.
Allowing negative dual variable(s) as small as -1.5259278215995487e-13.
Allowing negative dual variable(s) as small as -1.4901101186293175e-13.
Solving took 4 GP solves and 17.7 seconds.
Allowing negative dual variable(s) as small as -5.188141583012396e-13.
Allowing negative dual variable(s) as small as -1.4275178261691224e-12.
Allowing negative dual variable(s) as small as -4.4540933441528097e-13.
Allowing negative dual variable(s) as small as -4.4316807168431893e-13.
Allowing negative dual variable(s) as small as -1.2961689013768485e-12.
Allowing negative dual variable(s) as small as -1.0913420774721905e-12.
Allowing negative dual variable(s) as small as -1.0920474594056095e-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 -2.469812548921979e-15.
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 -2.541623049278133e-14.
Allowing negative dual variable(s) as small as -5.695972194941673e-12.
Allowing negative dual variable(s) as small as -2.0878956970575863e-11.
Allowing negative dual variable(s) as small as -2.088093075838094e-11.
Solving took 4 GP solves and 5.5 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.2 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.182104745315996e-13.
Allowing negative dual variable(s) as small as -1.4288448896282446e-12.
Allowing negative dual variable(s) as small as -4.433259315206328e-13.
Allowing negative dual variable(s) as small as -4.445784018702881e-13.
Allowing negative dual variable(s) as small as -1.296617110554954e-12.
Allowing negative dual variable(s) as small as -1.0918680239460632e-12.
Allowing negative dual variable(s) as small as -1.0902314207666963e-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
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 -2.487555273952732e-14.
Allowing negative dual variable(s) as small as -5.695872395243426e-12.
Allowing negative dual variable(s) as small as -2.0878999602141145e-11.
Allowing negative dual variable(s) as small as -2.0880952599363714e-11.
Solving took 4 GP solves and 9.82 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.32 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error