Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018091637)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.67195074031e-14.
Allowing negative dual variable(s) as small as -1.21197843428e-12.
Allowing negative dual variable(s) as small as -1.15194615999e-12.
Allowing negative dual variable(s) as small as -1.12502281796e-12.
Solving took 4 GP solves and 2.04 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.572984766e-14.
Allowing negative dual variable(s) as small as -1.20128126196e-12.
Allowing negative dual variable(s) as small as -1.14307174837e-12.
Allowing negative dual variable(s) as small as -1.14924302713e-12.
Solving took 4 GP solves and 1.69 seconds.
Allowing negative dual variable(s) as small as -1.56886829916e-12.
Allowing negative dual variable(s) as small as -3.96110401424e-12.
Allowing negative dual variable(s) as small as -1.78713901317e-12.
Allowing negative dual variable(s) as small as -2.08245139882e-12.
Allowing negative dual variable(s) as small as -2.0811347437e-12.
Allowing negative dual variable(s) as small as -4.70095533681e-13.
Allowing negative dual variable(s) as small as -8.92419601758e-13.
Allowing negative dual variable(s) as small as -9.41672412789e-13.
Allowing negative dual variable(s) as small as -9.42921088432e-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 -2.34192006066e-13.
Allowing negative dual variable(s) as small as -9.34480357678e-14.
Allowing negative dual variable(s) as small as -1.19161516592e-13.
Allowing negative dual variable(s) as small as -1.20696204767e-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 -9.6148660475e-13.
Allowing negative dual variable(s) as small as -2.01648257252e-12.
Allowing negative dual variable(s) as small as -1.29778170484e-14.
Allowing negative dual variable(s) as small as -1.8116413256e-14.
Solving took 4 GP solves and 2.62 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 2.04 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56942341067e-12.
Allowing negative dual variable(s) as small as -3.96040925749e-12.
Allowing negative dual variable(s) as small as -1.78703406239e-12.
Allowing negative dual variable(s) as small as -2.08269772956e-12.
Allowing negative dual variable(s) as small as -2.08094392412e-12.
Allowing negative dual variable(s) as small as -4.76670352495e-13.
Allowing negative dual variable(s) as small as -8.93899429304e-13.
Allowing negative dual variable(s) as small as -9.41172053487e-13.
Allowing negative dual variable(s) as small as -9.4385859805e-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 -2.32643548523e-13.
Allowing negative dual variable(s) as small as -9.30746365396e-14.
Allowing negative dual variable(s) as small as -1.20489338992e-13.
Allowing negative dual variable(s) as small as -1.20824140623e-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 -9.61597820811e-13.
Allowing negative dual variable(s) as small as -2.01692800724e-12.
Allowing negative dual variable(s) as small as -1.30405534436e-14.
Allowing negative dual variable(s) as small as -1.75970394931e-14.
Solving took 4 GP solves and 2.84 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