Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171207123849)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.40299098065e-13.
Allowing negative dual variable(s) as small as -6.44119957025e-13.
Allowing negative dual variable(s) as small as -9.34315342108e-13.
Allowing negative dual variable(s) as small as -9.84461210468e-13.
Solving took 4 GP solves and 2.13 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.40299098065e-13.
Allowing negative dual variable(s) as small as -6.44119957025e-13.
Allowing negative dual variable(s) as small as -9.34315342108e-13.
Allowing negative dual variable(s) as small as -9.84461210468e-13.
Solving took 4 GP solves and 1.94 seconds.
Allowing negative dual variable(s) as small as -9.2474964318e-14.
Allowing negative dual variable(s) as small as -6.00321698222e-10.
Allowing negative dual variable(s) as small as -4.3979224559e-13.
MTOW [lbs] = 132.53
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 = 20.352
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] = 27.301
Allowing negative dual variable(s) as small as -1.94964216212e-14.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.76570800781e-12.
Allowing negative dual variable(s) as small as -2.89910846688e-12.
Allowing negative dual variable(s) as small as -4.21180041458e-12.
Allowing negative dual variable(s) as small as -4.21367984978e-12.
Solving took 4 GP solves and 3.74 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 3.46 seconds.
Max payload weight [lbf] = 9.228
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -9.2474964318e-14.
Allowing negative dual variable(s) as small as -6.00321698222e-10.
Allowing negative dual variable(s) as small as -4.3979224559e-13.
MTOW [lbs] = 132.53
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 = 20.352
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] = 27.301
Allowing negative dual variable(s) as small as -1.94964216212e-14.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.76570800781e-12.
Allowing negative dual variable(s) as small as -2.89910846688e-12.
Allowing negative dual variable(s) as small as -4.21180041458e-12.
Allowing negative dual variable(s) as small as -4.21367984978e-12.
Solving took 4 GP solves and 6.35 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 4.54 seconds.
Max payload weight [lbf] = 9.228
Max take off weight [lbf] = 140.364
	

Standard Error