Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018120441)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.69732107114e-14.
Allowing negative dual variable(s) as small as -1.1855776777e-12.
Allowing negative dual variable(s) as small as -1.13600621965e-12.
Allowing negative dual variable(s) as small as -1.17015208287e-12.
Solving took 4 GP solves and 34.8 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.94933302412e-14.
Allowing negative dual variable(s) as small as -1.19666386175e-12.
Allowing negative dual variable(s) as small as -1.14396556464e-12.
Allowing negative dual variable(s) as small as -1.14327340997e-12.
Solving took 4 GP solves and 30.7 seconds.
Allowing negative dual variable(s) as small as -1.5698648978e-12.
Allowing negative dual variable(s) as small as -3.96119421986e-12.
Allowing negative dual variable(s) as small as -1.78705140963e-12.
Allowing negative dual variable(s) as small as -2.08226751813e-12.
Allowing negative dual variable(s) as small as -2.08046514044e-12.
Allowing negative dual variable(s) as small as -4.75364539398e-13.
Allowing negative dual variable(s) as small as -8.94327038641e-13.
Allowing negative dual variable(s) as small as -9.41880145926e-13.
Allowing negative dual variable(s) as small as -9.44626755289e-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 -2.35592361592e-13.
Allowing negative dual variable(s) as small as -9.1930477987e-14.
Allowing negative dual variable(s) as small as -1.19768344548e-13.
Allowing negative dual variable(s) as small as -1.20176763506e-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 -9.61410745538e-13.
Allowing negative dual variable(s) as small as -2.01746884974e-12.
Allowing negative dual variable(s) as small as -1.24523193961e-14.
Allowing negative dual variable(s) as small as -1.72829650761e-14.
Solving took 4 GP solves and 13.7 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 11.1 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56889865682e-12.
Allowing negative dual variable(s) as small as -3.96010221143e-12.
Allowing negative dual variable(s) as small as -1.78662987182e-12.
Allowing negative dual variable(s) as small as -2.08238287724e-12.
Allowing negative dual variable(s) as small as -2.08127178686e-12.
Allowing negative dual variable(s) as small as -4.73235166332e-13.
Allowing negative dual variable(s) as small as -8.93269291001e-13.
Allowing negative dual variable(s) as small as -9.40556335073e-13.
Allowing negative dual variable(s) as small as -9.44529068674e-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 -2.32509541134e-13.
Allowing negative dual variable(s) as small as -9.30087170475e-14.
Allowing negative dual variable(s) as small as -1.18649447906e-13.
Allowing negative dual variable(s) as small as -1.21298912754e-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 -9.61097659291e-13.
Allowing negative dual variable(s) as small as -2.01656715193e-12.
Allowing negative dual variable(s) as small as -1.29069371196e-14.
Allowing negative dual variable(s) as small as -1.75742971349e-14.
Solving took 4 GP solves and 12.1 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 7.05 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error