Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180111113207)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.0299872853800647e-13.
Allowing negative dual variable(s) as small as -4.4536423160490557e-13.
Allowing negative dual variable(s) as small as -4.660182829907544e-14.
Allowing negative dual variable(s) as small as -8.149275525226596e-14.
Solving took 4 GP solves and 41.8 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.3534060984709004e-13.
Allowing negative dual variable(s) as small as -5.112440418925113e-13.
Allowing negative dual variable(s) as small as -9.358898205025223e-14.
Allowing negative dual variable(s) as small as -7.952839775615672e-14.
Solving took 4 GP solves and 16.9 seconds.
MTOW [lbs] = 132.52
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 = 20.351
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.299
optimum loiter speed for min power, start of loiter [m/s] = 23.617
optimum loiter speed for min power, end of loiter [m/s] = 16.684
optimum cruise speed, inbound [m/s] = 31.019
optimum cruise speed, outbound [m/s] = 23.408
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.0273601589892405e-12.
Allowing negative dual variable(s) as small as -1.1071861670327111e-12.
Allowing negative dual variable(s) as small as -2.4833512552432796e-12.
Allowing negative dual variable(s) as small as -2.482046452212021e-12.
Solving took 4 GP solves and 6.08 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 4.54 seconds.
Max payload weight [lbf] = 9.202
Max take off weight [lbf] = 140.328
MTOW [lbs] = 132.52
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 = 20.351
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.299
optimum loiter speed for min power, start of loiter [m/s] = 23.617
optimum loiter speed for min power, end of loiter [m/s] = 16.684
optimum cruise speed, inbound [m/s] = 31.019
optimum cruise speed, outbound [m/s] = 23.408
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.027359989185604e-12.
Allowing negative dual variable(s) as small as -1.1072413620934149e-12.
Allowing negative dual variable(s) as small as -2.4835058740337523e-12.
Allowing negative dual variable(s) as small as -2.4821051056619263e-12.
Solving took 4 GP solves and 5.65 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 4.43 seconds.
Max payload weight [lbf] = 9.202
Max take off weight [lbf] = 140.328
	

Standard Error