Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171025135745)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.60746239509e-14.
Allowing negative dual variable(s) as small as -1.17544212211e-12.
Allowing negative dual variable(s) as small as -1.13401519078e-12.
Allowing negative dual variable(s) as small as -1.14676107152e-12.
Solving took 4 GP solves and 2.9 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.641853288e-14.
Allowing negative dual variable(s) as small as -1.17108579778e-12.
Allowing negative dual variable(s) as small as -1.1347537493e-12.
Allowing negative dual variable(s) as small as -1.14664831449e-12.
Solving took 4 GP solves and 3.23 seconds.
Allowing negative dual variable(s) as small as -1.56940606344e-12.
Allowing negative dual variable(s) as small as -3.96053329021e-12.
Allowing negative dual variable(s) as small as -1.78701411307e-12.
Allowing negative dual variable(s) as small as -2.08250951206e-12.
Allowing negative dual variable(s) as small as -2.08075223718e-12.
Allowing negative dual variable(s) as small as -4.72263504345e-13.
Allowing negative dual variable(s) as small as -8.92169042636e-13.
Allowing negative dual variable(s) as small as -9.40487596655e-13.
Allowing negative dual variable(s) as small as -9.42551375491e-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 -2.38329321556e-13.
Allowing negative dual variable(s) as small as -9.30038381378e-14.
Allowing negative dual variable(s) as small as -1.19231230791e-13.
Allowing negative dual variable(s) as small as -1.19818001007e-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 -9.61280156351e-13.
Allowing negative dual variable(s) as small as -2.01620264848e-12.
Allowing negative dual variable(s) as small as -1.29247866978e-14.
Allowing negative dual variable(s) as small as -1.7343430523e-14.
Solving took 4 GP solves and 3.56 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 2.3 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56955698438e-12.
Allowing negative dual variable(s) as small as -3.9602071622e-12.
Allowing negative dual variable(s) as small as -1.78685018171e-12.
Allowing negative dual variable(s) as small as -2.08236726473e-12.
Allowing negative dual variable(s) as small as -2.08093004633e-12.
Allowing negative dual variable(s) as small as -4.77057412671e-13.
Allowing negative dual variable(s) as small as -8.92114507267e-13.
Allowing negative dual variable(s) as small as -9.42305803699e-13.
Allowing negative dual variable(s) as small as -9.42792393634e-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 -2.34431614746e-13.
Allowing negative dual variable(s) as small as -9.17051807756e-14.
Allowing negative dual variable(s) as small as -1.19718471248e-13.
Allowing negative dual variable(s) as small as -1.20805492346e-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 -9.60497872932e-13.
Allowing negative dual variable(s) as small as -2.01671884638e-12.
Allowing negative dual variable(s) as small as -1.31153621759e-14.
Allowing negative dual variable(s) as small as -1.77151221858e-14.
Solving took 4 GP solves and 3.51 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 1.85 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error