Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428102421)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.102992681194074e-14.
Allowing negative dual variable(s) as small as -7.504630597510165e-14.
Allowing negative dual variable(s) as small as -1.5090099309000848e-13.
Allowing negative dual variable(s) as small as -1.4924042904262969e-13.
Solving took 4 GP solves and 6.56 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.128276275856436e-14.
Allowing negative dual variable(s) as small as -7.539628643637997e-14.
Allowing negative dual variable(s) as small as -1.5005921852329074e-13.
Allowing negative dual variable(s) as small as -1.489771847551502e-13.
Solving took 4 GP solves and 5.55 seconds.
Allowing negative dual variable(s) as small as -5.182815981941147e-13.
Allowing negative dual variable(s) as small as -1.4302985879011132e-12.
Allowing negative dual variable(s) as small as -4.450120827392823e-13.
Allowing negative dual variable(s) as small as -4.442158446638089e-13.
Allowing negative dual variable(s) as small as -1.2967603336619393e-12.
Allowing negative dual variable(s) as small as -1.0912152258180097e-12.
Allowing negative dual variable(s) as small as -1.0907444652347165e-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 -2.4741065189206137e-14.
Allowing negative dual variable(s) as small as -5.6960391505668125e-12.
Allowing negative dual variable(s) as small as -2.0879033542380764e-11.
Allowing negative dual variable(s) as small as -2.088079317958388e-11.
Solving took 4 GP solves and 6.15 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 10.4 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.186389512301659e-13.
Allowing negative dual variable(s) as small as -1.42993776541811e-12.
Allowing negative dual variable(s) as small as -4.443754392235988e-13.
Allowing negative dual variable(s) as small as -4.4523933151463524e-13.
Allowing negative dual variable(s) as small as -1.2969615615851526e-12.
Allowing negative dual variable(s) as small as -1.0912002638280294e-12.
Allowing negative dual variable(s) as small as -1.0913494500469634e-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 -2.4538602080197494e-14.
Allowing negative dual variable(s) as small as -5.696055323178633e-12.
Allowing negative dual variable(s) as small as -2.087917922032158e-11.
Allowing negative dual variable(s) as small as -2.0880753961323147e-11.
Solving took 4 GP solves and 9.41 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.32 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error