Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180424150402)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.649675164145275e-14.
Allowing negative dual variable(s) as small as -8.007299250739619e-14.
Allowing negative dual variable(s) as small as -1.3446568077751797e-13.
Allowing negative dual variable(s) as small as -1.3199413350512001e-13.
Solving took 4 GP solves and 3.05 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.319481392514815e-14.
Allowing negative dual variable(s) as small as -7.732681682470766e-14.
Allowing negative dual variable(s) as small as -1.3303269076614388e-13.
Allowing negative dual variable(s) as small as -1.275515066831434e-13.
Solving took 4 GP solves and 3.33 seconds.
Allowing negative dual variable(s) as small as -5.847934983482794e-13.
Allowing negative dual variable(s) as small as -3.4060601561414217e-13.
Allowing negative dual variable(s) as small as -1.0245168428901774e-12.
Allowing negative dual variable(s) as small as -1.0219568247205046e-12.
Allowing negative dual variable(s) as small as -2.736215659430996e-13.
Allowing negative dual variable(s) as small as -1.1529004747407035e-12.
Allowing negative dual variable(s) as small as -1.1179210226801295e-12.
Allowing negative dual variable(s) as small as -1.1163783114088999e-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 -1.2109287639457122e-12.
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 -6.145432740866988e-11.
Allowing negative dual variable(s) as small as -1.4548197716884276e-12.
Allowing negative dual variable(s) as small as -6.463221690656534e-12.
Allowing negative dual variable(s) as small as -6.468845813905194e-12.
Solving took 4 GP solves and 4.25 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.46 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.835280175725543e-13.
Allowing negative dual variable(s) as small as -3.3924772713245233e-13.
Allowing negative dual variable(s) as small as -1.0230683487877368e-12.
Allowing negative dual variable(s) as small as -1.0214316371881527e-12.
Allowing negative dual variable(s) as small as -2.841284607764394e-13.
Allowing negative dual variable(s) as small as -1.1541295805335416e-12.
Allowing negative dual variable(s) as small as -1.117867923878732e-12.
Allowing negative dual variable(s) as small as -1.1163779590431938e-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 -1.2095948700129033e-12.
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 -6.145440322150679e-11.
Allowing negative dual variable(s) as small as -1.4547476820642455e-12.
Allowing negative dual variable(s) as small as -6.463221178744232e-12.
Allowing negative dual variable(s) as small as -6.468774774681276e-12.
Solving took 4 GP solves and 3.76 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error