Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171016202055)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.60867670152e-14.
Allowing negative dual variable(s) as small as -1.17364624963e-12.
Allowing negative dual variable(s) as small as -1.12875681024e-12.
Allowing negative dual variable(s) as small as -1.14209466537e-12.
Solving took 4 GP solves and 2.17 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.01437087896e-13.
Allowing negative dual variable(s) as small as -1.19715955899e-12.
Allowing negative dual variable(s) as small as -1.12336008551e-12.
Allowing negative dual variable(s) as small as -1.13328010171e-12.
Solving took 4 GP solves and 1.68 seconds.
Allowing negative dual variable(s) as small as -1.5693661648e-12.
Allowing negative dual variable(s) as small as -3.96067380282e-12.
Allowing negative dual variable(s) as small as -1.78682502822e-12.
Allowing negative dual variable(s) as small as -2.08208190272e-12.
Allowing negative dual variable(s) as small as -2.08052238632e-12.
Allowing negative dual variable(s) as small as -4.71060473614e-13.
Allowing negative dual variable(s) as small as -8.93816162577e-13.
Allowing negative dual variable(s) as small as -9.42071290769e-13.
Allowing negative dual variable(s) as small as -9.43198102087e-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 -2.40605929278e-13.
Allowing negative dual variable(s) as small as -9.17392247238e-14.
Allowing negative dual variable(s) as small as -1.20148465829e-13.
Allowing negative dual variable(s) as small as -1.20262632318e-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 -9.61676770635e-13.
Allowing negative dual variable(s) as small as -2.01678443637e-12.
Allowing negative dual variable(s) as small as -1.24501698382e-14.
Allowing negative dual variable(s) as small as -1.67940605706e-14.
Solving took 4 GP solves and 2.53 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 1.79 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56936009327e-12.
Allowing negative dual variable(s) as small as -3.96108493228e-12.
Allowing negative dual variable(s) as small as -1.7866281371e-12.
Allowing negative dual variable(s) as small as -2.08248088912e-12.
Allowing negative dual variable(s) as small as -2.08068111351e-12.
Allowing negative dual variable(s) as small as -4.75972993658e-13.
Allowing negative dual variable(s) as small as -8.9224081682e-13.
Allowing negative dual variable(s) as small as -9.4046005792e-13.
Allowing negative dual variable(s) as small as -9.42587262583e-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 -2.29838066981e-13.
Allowing negative dual variable(s) as small as -9.16620295291e-14.
Allowing negative dual variable(s) as small as -1.18937954104e-13.
Allowing negative dual variable(s) as small as -1.20013807919e-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 -9.60999286155e-13.
Allowing negative dual variable(s) as small as -2.01699973799e-12.
Allowing negative dual variable(s) as small as -1.2815828297e-14.
Allowing negative dual variable(s) as small as -1.74018127983e-14.
Solving took 4 GP solves and 2.54 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 1.66 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error