Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171016202509)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.54887210969e-14.
Allowing negative dual variable(s) as small as -1.17742100791e-12.
Allowing negative dual variable(s) as small as -1.14131100404e-12.
Allowing negative dual variable(s) as small as -1.14081183736e-12.
Solving took 4 GP solves and 5.21 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.01646122075e-13.
Allowing negative dual variable(s) as small as -1.17227625177e-12.
Allowing negative dual variable(s) as small as -1.1354112095e-12.
Allowing negative dual variable(s) as small as -1.12470406252e-12.
Solving took 4 GP solves and 2.01 seconds.
Allowing negative dual variable(s) as small as -1.56934534812e-12.
Allowing negative dual variable(s) as small as -3.9608871738e-12.
Allowing negative dual variable(s) as small as -1.78670012813e-12.
Allowing negative dual variable(s) as small as -2.08236899946e-12.
Allowing negative dual variable(s) as small as -2.08074529828e-12.
Allowing negative dual variable(s) as small as -4.72235098248e-13.
Allowing negative dual variable(s) as small as -8.93242728048e-13.
Allowing negative dual variable(s) as small as -9.4073923998e-13.
Allowing negative dual variable(s) as small as -9.44143309541e-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 -2.28685343232e-13.
Allowing negative dual variable(s) as small as -9.27694336281e-14.
Allowing negative dual variable(s) as small as -1.19352986695e-13.
Allowing negative dual variable(s) as small as -1.20252115557e-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 -9.61398786492e-13.
Allowing negative dual variable(s) as small as -2.01783224596e-12.
Allowing negative dual variable(s) as small as -1.27258002355e-14.
Allowing negative dual variable(s) as small as -1.76552011693e-14.
Solving took 4 GP solves and 3.12 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 4.31 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56981459082e-12.
Allowing negative dual variable(s) as small as -3.96070242575e-12.
Allowing negative dual variable(s) as small as -1.78650670646e-12.
Allowing negative dual variable(s) as small as -2.08240716337e-12.
Allowing negative dual variable(s) as small as -2.08098815957e-12.
Allowing negative dual variable(s) as small as -4.72637554094e-13.
Allowing negative dual variable(s) as small as -8.93307563338e-13.
Allowing negative dual variable(s) as small as -9.41251200245e-13.
Allowing negative dual variable(s) as small as -9.43594594821e-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 -2.37099619452e-13.
Allowing negative dual variable(s) as small as -9.19345979553e-14.
Allowing negative dual variable(s) as small as -1.19538168426e-13.
Allowing negative dual variable(s) as small as -1.20402494398e-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 -9.61399790861e-13.
Allowing negative dual variable(s) as small as -2.01627488438e-12.
Allowing negative dual variable(s) as small as -1.32873863089e-14.
Allowing negative dual variable(s) as small as -1.76514913238e-14.
Solving took 4 GP solves and 22.8 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 5.68 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error