Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171016202209)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.77716171913e-14.
Allowing negative dual variable(s) as small as -1.17801384966e-12.
Allowing negative dual variable(s) as small as -1.13759045586e-12.
Allowing negative dual variable(s) as small as -1.13872323029e-12.
Solving took 4 GP solves and 2.77 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.78509807903e-14.
Allowing negative dual variable(s) as small as -1.18040256389e-12.
Allowing negative dual variable(s) as small as -1.14086691483e-12.
Allowing negative dual variable(s) as small as -1.14269531337e-12.
Solving took 4 GP solves and 1.88 seconds.
Allowing negative dual variable(s) as small as -1.56962116915e-12.
Allowing negative dual variable(s) as small as -3.96090365368e-12.
Allowing negative dual variable(s) as small as -1.78677732332e-12.
Allowing negative dual variable(s) as small as -2.08198909502e-12.
Allowing negative dual variable(s) as small as -2.08039054733e-12.
Allowing negative dual variable(s) as small as -4.73859233102e-13.
Allowing negative dual variable(s) as small as -8.92632430645e-13.
Allowing negative dual variable(s) as small as -9.42002552351e-13.
Allowing negative dual variable(s) as small as -9.44042045058e-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 -2.3144420408e-13.
Allowing negative dual variable(s) as small as -9.42069772886e-14.
Allowing negative dual variable(s) as small as -1.19311787013e-13.
Allowing negative dual variable(s) as small as -1.20692301639e-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 -9.60909352855e-13.
Allowing negative dual variable(s) as small as -2.01639579442e-12.
Allowing negative dual variable(s) as small as -1.28363729223e-14.
Allowing negative dual variable(s) as small as -1.74103687311e-14.
Solving took 4 GP solves and 20 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 11.8 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56932192935e-12.
Allowing negative dual variable(s) as small as -3.96024966293e-12.
Allowing negative dual variable(s) as small as -1.78695599984e-12.
Allowing negative dual variable(s) as small as -2.08253986972e-12.
Allowing negative dual variable(s) as small as -2.08142010572e-12.
Allowing negative dual variable(s) as small as -4.69487079421e-13.
Allowing negative dual variable(s) as small as -8.93504888133e-13.
Allowing negative dual variable(s) as small as -9.42736015121e-13.
Allowing negative dual variable(s) as small as -9.43989461252e-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 -2.34270502303e-13.
Allowing negative dual variable(s) as small as -9.29687099874e-14.
Allowing negative dual variable(s) as small as -1.19838384008e-13.
Allowing negative dual variable(s) as small as -1.21308236893e-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 -9.60686897863e-13.
Allowing negative dual variable(s) as small as -2.01631476232e-12.
Allowing negative dual variable(s) as small as -1.29339854756e-14.
Allowing negative dual variable(s) as small as -1.71998522975e-14.
Solving took 4 GP solves and 9.51 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 7.69 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error