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Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428102201)

Took 11 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.4556086370964838e-13.
Allowing negative dual variable(s) as small as -8.073262110913637e-14.
Allowing negative dual variable(s) as small as -1.318112285986217e-13.
Allowing negative dual variable(s) as small as -1.3076063669348326e-13.
Solving took 4 GP solves and 7.17 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.649100536993858e-14.
Allowing negative dual variable(s) as small as -7.327038281657039e-14.
Allowing negative dual variable(s) as small as -1.3151253090010195e-13.
Allowing negative dual variable(s) as small as -1.3077830918889477e-13.
Solving took 4 GP solves and 5.19 seconds.
Allowing negative dual variable(s) as small as -5.842600708794166e-13.
Allowing negative dual variable(s) as small as -3.386219256384937e-13.
Allowing negative dual variable(s) as small as -1.0219676667422295e-12.
Allowing negative dual variable(s) as small as -1.0236776704086736e-12.
Allowing negative dual variable(s) as small as -2.823683127595178e-13.
Allowing negative dual variable(s) as small as -1.1539772772333617e-12.
Allowing negative dual variable(s) as small as -1.116975246020016e-12.
Allowing negative dual variable(s) as small as -1.1169847598940796e-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 -1.209527107377123e-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 -6.145433836689393e-11.
Allowing negative dual variable(s) as small as -1.4548110008475472e-12.
Allowing negative dual variable(s) as small as -6.463252076785612e-12.
Allowing negative dual variable(s) as small as -6.468785751063602e-12.
Solving took 4 GP solves and 5.78 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.72 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.826940492614785e-13.
Allowing negative dual variable(s) as small as -3.405587443994218e-13.
Allowing negative dual variable(s) as small as -1.0224186948459835e-12.
Allowing negative dual variable(s) as small as -1.023048833148632e-12.
Allowing negative dual variable(s) as small as -2.768075482370569e-13.
Allowing negative dual variable(s) as small as -1.1536421774469008e-12.
Allowing negative dual variable(s) as small as -1.1162308057033332e-12.
Allowing negative dual variable(s) as small as -1.1161377540518796e-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 -1.2091560933936985e-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 -6.145438394118402e-11.
Allowing negative dual variable(s) as small as -1.4547879423078521e-12.
Allowing negative dual variable(s) as small as -6.463147376578249e-12.
Allowing negative dual variable(s) as small as -6.46884022740527e-12.
Solving took 4 GP solves and 6.89 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 4.28 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error