Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180424145228)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.192504412554477e-14.
Allowing negative dual variable(s) as small as -7.586856490271465e-14.
Allowing negative dual variable(s) as small as -1.5111219567320866e-13.
Allowing negative dual variable(s) as small as -1.502261856578535e-13.
Solving took 4 GP solves and 3.51 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.167914707282506e-14.
Allowing negative dual variable(s) as small as -7.780061317408382e-14.
Allowing negative dual variable(s) as small as -1.5036409617419366e-13.
Allowing negative dual variable(s) as small as -1.5009087722672732e-13.
Solving took 4 GP solves and 3.23 seconds.
Allowing negative dual variable(s) as small as -5.183284357279661e-13.
Allowing negative dual variable(s) as small as -1.4296584749384778e-12.
Allowing negative dual variable(s) as small as -4.445454421242445e-13.
Allowing negative dual variable(s) as small as -4.43759612389627e-13.
Allowing negative dual variable(s) as small as -1.2971992187013615e-12.
Allowing negative dual variable(s) as small as -1.0912069858814988e-12.
Allowing negative dual variable(s) as small as -1.0900964375962219e-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 -2.433819789652539e-14.
Allowing negative dual variable(s) as small as -5.696048081841027e-12.
Allowing negative dual variable(s) as small as -2.0878910114539636e-11.
Allowing negative dual variable(s) as small as -2.088075344201254e-11.
Solving took 4 GP solves and 3.42 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.11 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.15788800559136e-13.
Allowing negative dual variable(s) as small as -1.4300227668684329e-12.
Allowing negative dual variable(s) as small as -4.432842981572094e-13.
Allowing negative dual variable(s) as small as -4.441412515543419e-13.
Allowing negative dual variable(s) as small as -1.2965120513644401e-12.
Allowing negative dual variable(s) as small as -1.0909591372648686e-12.
Allowing negative dual variable(s) as small as -1.0907051086958552e-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
Allowing negative dual variable(s) as small as -1.0443035325380379e-15.
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 -2.5049209528549266e-14.
Allowing negative dual variable(s) as small as -5.696107112758261e-12.
Allowing negative dual variable(s) as small as -2.0878941801512797e-11.
Allowing negative dual variable(s) as small as -2.088093342364952e-11.
Solving took 4 GP solves and 2.95 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.17 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error