Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171018105752)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.70417322887e-14.
Allowing negative dual variable(s) as small as -1.18700752352e-12.
Allowing negative dual variable(s) as small as -1.13795734988e-12.
Allowing negative dual variable(s) as small as -1.13532707541e-12.
Solving took 4 GP solves and 12.5 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.73149512362e-14.
Allowing negative dual variable(s) as small as -1.16297596553e-12.
Allowing negative dual variable(s) as small as -1.13916341637e-12.
Allowing negative dual variable(s) as small as -1.13694340401e-12.
Solving took 4 GP solves and 15.8 seconds.
Allowing negative dual variable(s) as small as -1.57019796471e-12.
Allowing negative dual variable(s) as small as -3.96107105449e-12.
Allowing negative dual variable(s) as small as -1.78730294453e-12.
Allowing negative dual variable(s) as small as -2.08297355059e-12.
Allowing negative dual variable(s) as small as -2.08090229076e-12.
Allowing negative dual variable(s) as small as -4.68551629787e-13.
Allowing negative dual variable(s) as small as -8.92663438827e-13.
Allowing negative dual variable(s) as small as -9.42281842831e-13.
Allowing negative dual variable(s) as small as -9.42428318544e-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 -2.34065588092e-13.
Allowing negative dual variable(s) as small as -9.3277924447e-14.
Allowing negative dual variable(s) as small as -1.19918831809e-13.
Allowing negative dual variable(s) as small as -1.2081785225e-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 -9.6083069187e-13.
Allowing negative dual variable(s) as small as -2.01727714297e-12.
Allowing negative dual variable(s) as small as -1.28731224526e-14.
Allowing negative dual variable(s) as small as -1.81133148624e-14.
Solving took 4 GP solves and 2.89 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 2.67 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56962984277e-12.
Allowing negative dual variable(s) as small as -3.96080997861e-12.
Allowing negative dual variable(s) as small as -1.7870973798e-12.
Allowing negative dual variable(s) as small as -2.08266216772e-12.
Allowing negative dual variable(s) as small as -2.08118591805e-12.
Allowing negative dual variable(s) as small as -4.74043547471e-13.
Allowing negative dual variable(s) as small as -8.92942946147e-13.
Allowing negative dual variable(s) as small as -9.40872271586e-13.
Allowing negative dual variable(s) as small as -9.42665216719e-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 -2.31389993971e-13.
Allowing negative dual variable(s) as small as -9.22186589244e-14.
Allowing negative dual variable(s) as small as -1.20172751958e-13.
Allowing negative dual variable(s) as small as -1.19537409485e-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 -9.60674805621e-13.
Allowing negative dual variable(s) as small as -2.01724602674e-12.
Allowing negative dual variable(s) as small as -1.24429534351e-14.
Allowing negative dual variable(s) as small as -1.82272395762e-14.
Solving took 4 GP solves and 7.35 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 3.28 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error