Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180124105526)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.0477976953037214e-13.
Allowing negative dual variable(s) as small as -9.414647880734428e-14.
Allowing negative dual variable(s) as small as -5.5496406081712024e-14.
Allowing negative dual variable(s) as small as -5.594266369590706e-14.
Solving took 4 GP solves and 54.8 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.1268186864431549e-13.
Allowing negative dual variable(s) as small as -9.155219984902097e-14.
Allowing negative dual variable(s) as small as -5.639629388487499e-14.
Allowing negative dual variable(s) as small as -5.3866633376031814e-14.
Solving took 4 GP solves and 78.7 seconds.
Allowing negative dual variable(s) as small as -5.972947830779063e-13.
Allowing negative dual variable(s) as small as -1.4369243642176066e-12.
Allowing negative dual variable(s) as small as -1.6874834862790067e-12.
Allowing negative dual variable(s) as small as -1.686859853189393e-12.
Allowing negative dual variable(s) as small as -1.3490573675528639e-12.
Allowing negative dual variable(s) as small as -2.2106632930479764e-12.
Allowing negative dual variable(s) as small as -2.272294765542915e-13.
Allowing negative dual variable(s) as small as -2.2566649070243638e-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 -1.7912045544715705e-12.
Allowing negative dual variable(s) as small as -2.0890494195624498e-13.
Allowing negative dual variable(s) as small as -2.1932369115296169e-13.
Allowing negative dual variable(s) as small as -2.2038816084590795e-13.
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 -2.287742296726882e-11.
Allowing negative dual variable(s) as small as -8.751167149842531e-12.
Allowing negative dual variable(s) as small as -8.175388839810334e-12.
Allowing negative dual variable(s) as small as -8.174399464501614e-12.
Solving took 4 GP solves and 59.5 seconds.
Max Speed [m/s]: 66.56
Beginning signomial solve.
Solving took 4 GP solves and 11.8 seconds.
Max payload weight [lbf] = 12.624
Max take off weight [lbf] = 145.409
Allowing negative dual variable(s) as small as -5.974439692968403e-13.
Allowing negative dual variable(s) as small as -1.4366988501657296e-12.
Allowing negative dual variable(s) as small as -1.6872466965245358e-12.
Allowing negative dual variable(s) as small as -1.6872822583557934e-12.
Allowing negative dual variable(s) as small as -1.344896416455299e-12.
Allowing negative dual variable(s) as small as -2.208836195546904e-12.
Allowing negative dual variable(s) as small as -2.2679189255747634e-13.
Allowing negative dual variable(s) as small as -2.250523985919406e-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 -1.790308786636663e-12.
Allowing negative dual variable(s) as small as -2.0293012062411186e-13.
Allowing negative dual variable(s) as small as -2.2213307582230613e-13.
Allowing negative dual variable(s) as small as -2.2226014431692143e-13.
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 -2.2877475235369124e-11.
Allowing negative dual variable(s) as small as -8.751244261941956e-12.
Allowing negative dual variable(s) as small as -8.175275243113355e-12.
Allowing negative dual variable(s) as small as -8.174472665995506e-12.
Solving took 4 GP solves and 118 seconds.
Max Speed [m/s]: 66.56
Beginning signomial solve.
Solving took 4 GP solves and 5.48 seconds.
Max payload weight [lbf] = 12.624
Max take off weight [lbf] = 145.409
	

Standard Error