Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018121433)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.91047521826e-14.
Allowing negative dual variable(s) as small as -1.19023714495e-12.
Allowing negative dual variable(s) as small as -1.13900902599e-12.
Allowing negative dual variable(s) as small as -1.13200724836e-12.
Solving took 4 GP solves and 28.2 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.74801836473e-14.
Allowing negative dual variable(s) as small as -1.17701248054e-12.
Allowing negative dual variable(s) as small as -1.13590603937e-12.
Allowing negative dual variable(s) as small as -1.14101523369e-12.
Solving took 4 GP solves and 28.4 seconds.
Allowing negative dual variable(s) as small as -1.56937483842e-12.
Allowing negative dual variable(s) as small as -3.96051507562e-12.
Allowing negative dual variable(s) as small as -1.7869681429e-12.
Allowing negative dual variable(s) as small as -2.08257282946e-12.
Allowing negative dual variable(s) as small as -2.08129086882e-12.
Allowing negative dual variable(s) as small as -4.69997088123e-13.
Allowing negative dual variable(s) as small as -8.9279451887e-13.
Allowing negative dual variable(s) as small as -9.41162729348e-13.
Allowing negative dual variable(s) as small as -9.44275256945e-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 -2.36783249258e-13.
Allowing negative dual variable(s) as small as -9.17671971398e-14.
Allowing negative dual variable(s) as small as -1.1986960903e-13.
Allowing negative dual variable(s) as small as -1.19877090025e-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 -9.61822402492e-13.
Allowing negative dual variable(s) as small as -2.01712997195e-12.
Allowing negative dual variable(s) as small as -1.25289470787e-14.
Allowing negative dual variable(s) as small as -1.67865114424e-14.
Solving took 4 GP solves and 2.58 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 3.38 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.57000974721e-12.
Allowing negative dual variable(s) as small as -3.96081865223e-12.
Allowing negative dual variable(s) as small as -1.78660211625e-12.
Allowing negative dual variable(s) as small as -2.08244706201e-12.
Allowing negative dual variable(s) as small as -2.08077305386e-12.
Allowing negative dual variable(s) as small as -4.73323420389e-13.
Allowing negative dual variable(s) as small as -8.93349413542e-13.
Allowing negative dual variable(s) as small as -9.42264278755e-13.
Allowing negative dual variable(s) as small as -9.44950714898e-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 -2.34139097e-13.
Allowing negative dual variable(s) as small as -9.24780000841e-14.
Allowing negative dual variable(s) as small as -1.20604156002e-13.
Allowing negative dual variable(s) as small as -1.2022891363e-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 -9.61245455741e-13.
Allowing negative dual variable(s) as small as -2.01704779813e-12.
Allowing negative dual variable(s) as small as -1.24570813094e-14.
Allowing negative dual variable(s) as small as -1.70726006849e-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 2.01 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error