Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180424135633)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.211889947398518e-14.
Allowing negative dual variable(s) as small as -7.124856260531942e-14.
Allowing negative dual variable(s) as small as -1.4971617695591632e-13.
Allowing negative dual variable(s) as small as -1.476765758290366e-13.
Solving took 4 GP solves and 1.69 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.148615908612264e-14.
Allowing negative dual variable(s) as small as -7.370189528121962e-14.
Allowing negative dual variable(s) as small as -1.5150988103007634e-13.
Allowing negative dual variable(s) as small as -1.5017024082575325e-13.
Solving took 4 GP solves and 1.59 seconds.
Allowing negative dual variable(s) as small as -5.17880877071164e-13.
Allowing negative dual variable(s) as small as -1.4295075539960678e-12.
Allowing negative dual variable(s) as small as -4.4506585916703756e-13.
Allowing negative dual variable(s) as small as -4.44881978478584e-13.
Allowing negative dual variable(s) as small as -1.2976898201844111e-12.
Allowing negative dual variable(s) as small as -1.0902099535636811e-12.
Allowing negative dual variable(s) as small as -1.0912704117085892e-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 -2.5136234328824883e-14.
Allowing negative dual variable(s) as small as -5.696009409148922e-12.
Allowing negative dual variable(s) as small as -2.0878860595114185e-11.
Allowing negative dual variable(s) as small as -2.0880658325215352e-11.
Solving took 4 GP solves and 1.58 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.35 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.180664924830936e-13.
Allowing negative dual variable(s) as small as -1.4301910350456026e-12.
Allowing negative dual variable(s) as small as -4.4337797322491213e-13.
Allowing negative dual variable(s) as small as -4.448524881794924e-13.
Allowing negative dual variable(s) as small as -1.2979851568561962e-12.
Allowing negative dual variable(s) as small as -1.092672285117613e-12.
Allowing negative dual variable(s) as small as -1.092597258327277e-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 -2.4709600032798008e-14.
Allowing negative dual variable(s) as small as -5.696087180405416e-12.
Allowing negative dual variable(s) as small as -2.0878992090785318e-11.
Allowing negative dual variable(s) as small as -2.08807484605059e-11.
Solving took 4 GP solves and 1.62 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.5 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error