Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180424145252)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.074803424709451e-14.
Allowing negative dual variable(s) as small as -7.32920668600201e-14.
Allowing negative dual variable(s) as small as -1.506013196095335e-13.
Allowing negative dual variable(s) as small as -1.497933721505973e-13.
Solving took 4 GP solves and 7.02 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.079573914268387e-14.
Allowing negative dual variable(s) as small as -7.106988608729381e-14.
Allowing negative dual variable(s) as small as -1.5086066076919202e-13.
Allowing negative dual variable(s) as small as -1.488496825796659e-13.
Solving took 4 GP solves and 8.33 seconds.
Allowing negative dual variable(s) as small as -5.163716676470642e-13.
Allowing negative dual variable(s) as small as -1.4297382722183727e-12.
Allowing negative dual variable(s) as small as -4.448975909898678e-13.
Allowing negative dual variable(s) as small as -4.462732267063174e-13.
Allowing negative dual variable(s) as small as -1.2963119076433993e-12.
Allowing negative dual variable(s) as small as -1.0908608001278242e-12.
Allowing negative dual variable(s) as small as -1.0903739933523782e-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 -2.3902106689400657e-14.
Allowing negative dual variable(s) as small as -5.695985459954083e-12.
Allowing negative dual variable(s) as small as -2.0878948889193332e-11.
Allowing negative dual variable(s) as small as -2.0880758656188545e-11.
Solving took 4 GP solves and 8.65 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.57 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.177646505982736e-13.
Allowing negative dual variable(s) as small as -1.4290079536349864e-12.
Allowing negative dual variable(s) as small as -4.443060502845597e-13.
Allowing negative dual variable(s) as small as -4.437908374121946e-13.
Allowing negative dual variable(s) as small as -1.2980563889389285e-12.
Allowing negative dual variable(s) as small as -1.0912993599065945e-12.
Allowing negative dual variable(s) as small as -1.092105681062272e-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 -2.4368763292185298e-14.
Allowing negative dual variable(s) as small as -5.696030617159855e-12.
Allowing negative dual variable(s) as small as -2.0879078290601972e-11.
Allowing negative dual variable(s) as small as -2.088084711522736e-11.
Solving took 4 GP solves and 15.9 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 4.04 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error