Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171120111931)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.00113927565e-13.
Allowing negative dual variable(s) as small as -2.09821786681e-12.
Allowing negative dual variable(s) as small as -2.18464525983e-12.
Allowing negative dual variable(s) as small as -2.18518389147e-12.
Solving took 4 GP solves and 4.69 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.02827035081e-13.
Allowing negative dual variable(s) as small as -2.04678591784e-12.
Allowing negative dual variable(s) as small as -2.18863989432e-12.
Allowing negative dual variable(s) as small as -2.18477102729e-12.
Solving took 4 GP solves and 26.2 seconds.
Allowing negative dual variable(s) as small as -1.21230282757e-13.
Allowing negative dual variable(s) as small as -8.16282805238e-14.
Allowing negative dual variable(s) as small as -2.05937697451e-14.
Allowing negative dual variable(s) as small as -2.07490274962e-14.
Allowing negative dual variable(s) as small as -1.04293700412e-12.
Allowing negative dual variable(s) as small as -1.64530650389e-12.
Allowing negative dual variable(s) as small as -1.46168472291e-12.
Allowing negative dual variable(s) as small as -1.47183589101e-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 -1.12813274347e-12.
Allowing negative dual variable(s) as small as -1.65959173487e-12.
Allowing negative dual variable(s) as small as -1.63751390919e-12.
Allowing negative dual variable(s) as small as -1.63829193267e-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 -1.25445541538e-11.
Allowing negative dual variable(s) as small as -4.86404432066e-11.
Allowing negative dual variable(s) as small as -4.13828062635e-12.
Allowing negative dual variable(s) as small as -4.13947268312e-12.
Solving took 4 GP solves and 2.66 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 3.81 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21214670246e-13.
Allowing negative dual variable(s) as small as -8.15094519657e-14.
Allowing negative dual variable(s) as small as -2.06102496181e-14.
Allowing negative dual variable(s) as small as -2.05946371068e-14.
Allowing negative dual variable(s) as small as -1.04353396584e-12.
Allowing negative dual variable(s) as small as -1.64820804574e-12.
Allowing negative dual variable(s) as small as -1.4591652539e-12.
Allowing negative dual variable(s) as small as -1.46709315703e-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 -1.12682606301e-12.
Allowing negative dual variable(s) as small as -1.6540189357e-12.
Allowing negative dual variable(s) as small as -1.63516943041e-12.
Allowing negative dual variable(s) as small as -1.63865058675e-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 -1.25444562194e-11.
Allowing negative dual variable(s) as small as -4.86404258959e-11.
Allowing negative dual variable(s) as small as -4.13819573906e-12.
Allowing negative dual variable(s) as small as -4.13939693505e-12.
Solving took 4 GP solves and 13.4 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 2.01 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
	

Standard Error