Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171018121412)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.40337217814e-14.
Allowing negative dual variable(s) as small as -1.19098958126e-12.
Allowing negative dual variable(s) as small as -1.13058000462e-12.
Allowing negative dual variable(s) as small as -1.14365721754e-12.
Solving took 4 GP solves and 2.12 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.16870745993e-14.
Allowing negative dual variable(s) as small as -1.18934029292e-12.
Allowing negative dual variable(s) as small as -1.14711235302e-12.
Allowing negative dual variable(s) as small as -1.15249953678e-12.
Solving took 4 GP solves and 1.57 seconds.
Allowing negative dual variable(s) as small as -1.57004183959e-12.
Allowing negative dual variable(s) as small as -3.96067813963e-12.
Allowing negative dual variable(s) as small as -1.78679120111e-12.
Allowing negative dual variable(s) as small as -2.08239328559e-12.
Allowing negative dual variable(s) as small as -2.08100117e-12.
Allowing negative dual variable(s) as small as -4.74035524375e-13.
Allowing negative dual variable(s) as small as -8.93840448705e-13.
Allowing negative dual variable(s) as small as -9.42251051489e-13.
Allowing negative dual variable(s) as small as -9.42389612527e-13.
MTOW [lbs] = 141.59
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 = 21.712
speed at top of climb [m/s] = 26.507
design loiter speed [m/s] = 25.048
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.32500216996e-13.
Allowing negative dual variable(s) as small as -9.32658898029e-14.
Allowing negative dual variable(s) as small as -1.18301527428e-13.
Allowing negative dual variable(s) as small as -1.19798485368e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.166
optimum loiter speed for min power, end of loiter [m/s] = 17.158
optimum cruise speed, inbound [m/s] = 35.697
optimum cruise speed, outbound [m/s] = 25.443
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.61861387395e-13.
Allowing negative dual variable(s) as small as -2.01617758465e-12.
Allowing negative dual variable(s) as small as -1.25482715001e-14.
Allowing negative dual variable(s) as small as -1.75128932284e-14.
Solving took 4 GP solves and 2.75 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000
Max Speed [m/s]: 73.83
Beginning signomial solve.
Solving took 4 GP solves and 2.11 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56960208719e-12.
Allowing negative dual variable(s) as small as -3.96027134697e-12.
Allowing negative dual variable(s) as small as -1.78696207137e-12.
Allowing negative dual variable(s) as small as -2.08209664787e-12.
Allowing negative dual variable(s) as small as -2.08121367362e-12.
Allowing negative dual variable(s) as small as -4.7270022098e-13.
Allowing negative dual variable(s) as small as -8.92441068961e-13.
Allowing negative dual variable(s) as small as -9.41775303576e-13.
Allowing negative dual variable(s) as small as -9.42861890993e-13.
MTOW [lbs] = 141.59
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 = 21.712
speed at top of climb [m/s] = 26.507
design loiter speed [m/s] = 25.048
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.3579640844e-13.
Allowing negative dual variable(s) as small as -9.38796566527e-14.
Allowing negative dual variable(s) as small as -1.2056816049e-13.
Allowing negative dual variable(s) as small as -1.2042320266e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.166
optimum loiter speed for min power, end of loiter [m/s] = 17.158
optimum cruise speed, inbound [m/s] = 35.697
optimum cruise speed, outbound [m/s] = 25.443
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.61205774788e-13.
Allowing negative dual variable(s) as small as -2.01690199396e-12.
Allowing negative dual variable(s) as small as -1.3252583525e-14.
Allowing negative dual variable(s) as small as -1.72641047758e-14.
Solving took 4 GP solves and 2.47 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000
Max Speed [m/s]: 73.83
Beginning signomial solve.
Solving took 4 GP solves and 1.88 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error