Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428144923)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.069035469151828e-14.
Allowing negative dual variable(s) as small as -7.462910497912922e-14.
Allowing negative dual variable(s) as small as -1.5120456969830443e-13.
Allowing negative dual variable(s) as small as -1.4907346190806692e-13.
Solving took 4 GP solves and 3.18 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.207206194013381e-14.
Allowing negative dual variable(s) as small as -7.525317174961188e-14.
Allowing negative dual variable(s) as small as -1.534644807066332e-13.
Allowing negative dual variable(s) as small as -1.4952709209703485e-13.
Solving took 4 GP solves and 3.15 seconds.
Allowing negative dual variable(s) as small as -5.198168284703542e-13.
Allowing negative dual variable(s) as small as -1.429186630153012e-12.
Allowing negative dual variable(s) as small as -4.4593148618155e-13.
Allowing negative dual variable(s) as small as -4.440735973387788e-13.
Allowing negative dual variable(s) as small as -1.2966185200177782e-12.
Allowing negative dual variable(s) as small as -1.0910996498664227e-12.
Allowing negative dual variable(s) as small as -1.0903083991209428e-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 -2.4497708917690833e-14.
Allowing negative dual variable(s) as small as -5.696033540614663e-12.
Allowing negative dual variable(s) as small as -2.0878972634650277e-11.
Allowing negative dual variable(s) as small as -2.0880742185341718e-11.
Solving took 4 GP solves and 2.98 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.89 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.190257945653087e-13.
Allowing negative dual variable(s) as small as -1.4279098736746931e-12.
Allowing negative dual variable(s) as small as -4.447778950700254e-13.
Allowing negative dual variable(s) as small as -4.4413084321348606e-13.
Allowing negative dual variable(s) as small as -1.2971778599185635e-12.
Allowing negative dual variable(s) as small as -1.09069231511022e-12.
Allowing negative dual variable(s) as small as -1.090988952824612e-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 -2.4256622800353288e-14.
Allowing negative dual variable(s) as small as -5.696074793475005e-12.
Allowing negative dual variable(s) as small as -2.0878899035481034e-11.
Allowing negative dual variable(s) as small as -2.088068565785683e-11.
Solving took 4 GP solves and 2.95 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.09 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error