Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180605124830)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.3279429479413665e-14.
Allowing negative dual variable(s) as small as -7.394605761046336e-14.
Allowing negative dual variable(s) as small as -1.5148039073098474e-13.
Allowing negative dual variable(s) as small as -1.4950757645793011e-13.
Solving took 4 GP solves and 1.69 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.1192557137813566e-14.
Allowing negative dual variable(s) as small as -7.324132619834778e-14.
Allowing negative dual variable(s) as small as -1.5305638700890967e-13.
Allowing negative dual variable(s) as small as -1.4896590905255636e-13.
Solving took 4 GP solves and 2.05 seconds.
Allowing negative dual variable(s) as small as -5.172615807902403e-13.
Allowing negative dual variable(s) as small as -1.4291502009600165e-12.
Allowing negative dual variable(s) as small as -4.4536596632838155e-13.
Allowing negative dual variable(s) as small as -4.4259908238419854e-13.
Allowing negative dual variable(s) as small as -1.2962308093208974e-12.
Allowing negative dual variable(s) as small as -1.0911432347937566e-12.
Allowing negative dual variable(s) as small as -1.09049173770831e-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 -2.4604324743003495e-14.
Allowing negative dual variable(s) as small as -5.69585288460711e-12.
Allowing negative dual variable(s) as small as -2.0878937318590923e-11.
Allowing negative dual variable(s) as small as -2.0880822170662928e-11.
Solving took 4 GP solves and 2.85 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.37 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.17509646247305e-13.
Allowing negative dual variable(s) as small as -1.4279862015076361e-12.
Allowing negative dual variable(s) as small as -4.4460268799895175e-13.
Allowing negative dual variable(s) as small as -4.456816860010093e-13.
Allowing negative dual variable(s) as small as -1.2959334126649846e-12.
Allowing negative dual variable(s) as small as -1.0913094429867987e-12.
Allowing negative dual variable(s) as small as -1.0898938002101843e-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 -2.5254253546948193e-14.
Allowing negative dual variable(s) as small as -5.695883425703512e-12.
Allowing negative dual variable(s) as small as -2.0878922164483283e-11.
Allowing negative dual variable(s) as small as -2.0880687120259213e-11.
Solving took 4 GP solves and 1.33 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.26 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error