Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171207123757)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.27261524771e-13.
Allowing negative dual variable(s) as small as -1.01601257789e-12.
Allowing negative dual variable(s) as small as -3.0217670163e-11.
Allowing negative dual variable(s) as small as -2.87745838441e-11.
Solving took 4 GP solves and 3.3 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.26466154058e-13.
Allowing negative dual variable(s) as small as -1.01954143912e-12.
Allowing negative dual variable(s) as small as -3.02160798552e-11.
Allowing negative dual variable(s) as small as -2.8772405682e-11.
Solving took 4 GP solves and 3.19 seconds.
Allowing negative dual variable(s) as small as -6.96141169883e-13.
Allowing negative dual variable(s) as small as -3.80193489538e-13.
Allowing negative dual variable(s) as small as -2.8748379545e-14.
Allowing negative dual variable(s) as small as -2.87141187563e-14.
Allowing negative dual variable(s) as small as -1.16885559391e-13.
Allowing negative dual variable(s) as small as -5.83278786978e-10.
Allowing negative dual variable(s) as small as -2.86085445698e-14.
Allowing negative dual variable(s) as small as -3.07499251756e-14.
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 -5.01274754209e-10.
Allowing negative dual variable(s) as small as -4.84333201285e-10.
Allowing negative dual variable(s) as small as -5.96148919888e-11.
Allowing negative dual variable(s) as small as -5.95298931948e-11.
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 -5.44118429016e-12.
Allowing negative dual variable(s) as small as -2.90973270186e-12.
Allowing negative dual variable(s) as small as -3.02526682047e-12.
Allowing negative dual variable(s) as small as -3.02603313808e-12.
Solving took 4 GP solves and 2.71 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.97 seconds.
Max payload weight [lbf] = 9.228
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -6.96241783844e-13.
Allowing negative dual variable(s) as small as -3.80071625214e-13.
Allowing negative dual variable(s) as small as -2.85304549083e-14.
Allowing negative dual variable(s) as small as -2.86789906059e-14.
Allowing negative dual variable(s) as small as -1.15304575783e-13.
Allowing negative dual variable(s) as small as -5.83278931664e-10.
Allowing negative dual variable(s) as small as -3.24327966827e-14.
Allowing negative dual variable(s) as small as -2.85062500948e-14.
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 -5.01274953756e-10.
Allowing negative dual variable(s) as small as -4.84333523266e-10.
Allowing negative dual variable(s) as small as -5.96166518387e-11.
Allowing negative dual variable(s) as small as -5.9529602466e-11.
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 -5.44103969622e-12.
Allowing negative dual variable(s) as small as -2.90983117429e-12.
Allowing negative dual variable(s) as small as -3.02528192473e-12.
Allowing negative dual variable(s) as small as -3.02597200955e-12.
Solving took 4 GP solves and 2.47 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.7 seconds.
Max payload weight [lbf] = 9.228
Max take off weight [lbf] = 140.364
	

Standard Error