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Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180124110218)

Took 16 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.448029180565861e-14.
Allowing negative dual variable(s) as small as -9.089300492814978e-14.
Allowing negative dual variable(s) as small as -3.145443974728046e-14.
Allowing negative dual variable(s) as small as -3.483368107848328e-14.
Solving took 4 GP solves and 7.2 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.448029180565861e-14.
Allowing negative dual variable(s) as small as -9.089300492814978e-14.
Allowing negative dual variable(s) as small as -3.145443974728046e-14.
Allowing negative dual variable(s) as small as -3.483368107848328e-14.
Solving took 4 GP solves and 6.51 seconds.
Allowing negative dual variable(s) as small as -1.4740205583896326e-13.
Allowing negative dual variable(s) as small as -1.4296151068515783e-12.
Allowing negative dual variable(s) as small as -1.2563465892623249e-12.
Allowing negative dual variable(s) as small as -1.2566128693158873e-12.
Allowing negative dual variable(s) as small as -1.434057299992686e-12.
Allowing negative dual variable(s) as small as -1.7645513956249248e-12.
Allowing negative dual variable(s) as small as -1.74011196077406e-13.
Allowing negative dual variable(s) as small as -2.340636365283366e-13.
MTOW [lbs] = 134.67
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 = 20.615
speed at top of climb [m/s] = 25.153
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.521
Allowing negative dual variable(s) as small as -1.2274959694524856e-12.
Allowing negative dual variable(s) as small as -1.738461805067537e-13.
Allowing negative dual variable(s) as small as -5.2057750471457e-14.
Allowing negative dual variable(s) as small as -5.535025562886098e-14.
optimum loiter speed for min power, start of loiter [m/s] = 23.910
optimum loiter speed for min power, end of loiter [m/s] = 16.760
optimum cruise speed, inbound [m/s] = 31.821
optimum cruise speed, outbound [m/s] = 23.768
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.488755928047649e-11.
Allowing negative dual variable(s) as small as -1.884175633993909e-12.
Allowing negative dual variable(s) as small as -2.8432553776142424e-12.
Allowing negative dual variable(s) as small as -2.8418457191452528e-12.
Solving took 4 GP solves and 4.31 seconds.
Max Speed [m/s]: 66.56
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.0477924911332934e-12.
Solving took 4 GP solves and 3.91 seconds.
Max payload weight [lbf] = 12.624
Max take off weight [lbf] = 145.409
Allowing negative dual variable(s) as small as -1.4740205583896326e-13.
Allowing negative dual variable(s) as small as -1.4296151068515783e-12.
Allowing negative dual variable(s) as small as -1.2563465892623249e-12.
Allowing negative dual variable(s) as small as -1.2566128693158873e-12.
Allowing negative dual variable(s) as small as -1.434057299992686e-12.
Allowing negative dual variable(s) as small as -1.7645513956249248e-12.
Allowing negative dual variable(s) as small as -1.74011196077406e-13.
Allowing negative dual variable(s) as small as -2.340636365283366e-13.
MTOW [lbs] = 134.67
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 = 20.615
speed at top of climb [m/s] = 25.153
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.521
Allowing negative dual variable(s) as small as -1.2274959694524856e-12.
Allowing negative dual variable(s) as small as -1.738461805067537e-13.
Allowing negative dual variable(s) as small as -5.2057750471457e-14.
Allowing negative dual variable(s) as small as -5.535025562886098e-14.
optimum loiter speed for min power, start of loiter [m/s] = 23.910
optimum loiter speed for min power, end of loiter [m/s] = 16.760
optimum cruise speed, inbound [m/s] = 31.821
optimum cruise speed, outbound [m/s] = 23.768
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.488755928047649e-11.
Allowing negative dual variable(s) as small as -1.884175633993909e-12.
Allowing negative dual variable(s) as small as -2.8432553776142424e-12.
Allowing negative dual variable(s) as small as -2.8418457191452528e-12.
Solving took 4 GP solves and 3.85 seconds.
Max Speed [m/s]: 66.56
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.0477924911332934e-12.
Solving took 4 GP solves and 3.32 seconds.
Max payload weight [lbf] = 12.624
Max take off weight [lbf] = 145.409
	

Standard Error