Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171110164747)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.12142933828e-13.
Allowing negative dual variable(s) as small as -1.07878116162e-13.
Allowing negative dual variable(s) as small as -1.51788304148e-16.
Allowing negative dual variable(s) as small as -2.36356073602e-16.
Solving took 4 GP solves and 1.78 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.09465821824e-13.
Allowing negative dual variable(s) as small as -1.05807723694e-13.
Allowing negative dual variable(s) as small as -1.86916454537e-16.
Solving took 4 GP solves and 1.88 seconds.
Allowing negative dual variable(s) as small as -3.88034743226e-12.
Allowing negative dual variable(s) as small as -1.71298305401e-12.
Allowing negative dual variable(s) as small as -7.75775277351e-13.
Allowing negative dual variable(s) as small as -7.70448808918e-13.
Allowing negative dual variable(s) as small as -7.7009579269e-13.
Allowing negative dual variable(s) as small as -2.50791358167e-13.
Allowing negative dual variable(s) as small as -1.01696114637e-12.
Allowing negative dual variable(s) as small as -1.05849281163e-12.
Allowing negative dual variable(s) as small as -1.04779325407e-12.
MTOW [lbs] = 141.59
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.59982356823e-13.
Allowing negative dual variable(s) as small as -1.46636717525e-13.
Allowing negative dual variable(s) as small as -1.46396458324e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.00387754076e-13.
Allowing negative dual variable(s) as small as -2.09978509418e-15.
Allowing negative dual variable(s) as small as -9.11303094669e-14.
Allowing negative dual variable(s) as small as -8.68393859811e-14.
Solving took 4 GP solves and 2.62 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.48 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.88168490406e-12.
Allowing negative dual variable(s) as small as -1.71244095293e-12.
Allowing negative dual variable(s) as small as -7.75336392311e-13.
Allowing negative dual variable(s) as small as -7.70161712182e-13.
Allowing negative dual variable(s) as small as -7.70333449807e-13.
Allowing negative dual variable(s) as small as -2.54512556863e-13.
Allowing negative dual variable(s) as small as -1.01661561114e-12.
Allowing negative dual variable(s) as small as -1.05898243733e-12.
Allowing negative dual variable(s) as small as -1.04748729222e-12.
MTOW [lbs] = 141.59
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.5497030702e-13.
Allowing negative dual variable(s) as small as -1.47099021332e-13.
Allowing negative dual variable(s) as small as -1.46837294927e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.00447767207e-13.
Allowing negative dual variable(s) as small as -2.06363902195e-15.
Allowing negative dual variable(s) as small as -8.73281266916e-14.
Allowing negative dual variable(s) as small as -8.89710548777e-14.
Solving took 4 GP solves and 2.48 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.44 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error