Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171115182637)

Standard Output

Allowing negative dual variable(s) as small as -1.21196455649e-13.
Allowing negative dual variable(s) as small as -8.14478692823e-14.
Allowing negative dual variable(s) as small as -2.049142106e-14.
Allowing negative dual variable(s) as small as -2.05495342964e-14.
Allowing negative dual variable(s) as small as -1.037345123e-12.
Allowing negative dual variable(s) as small as -1.64348742948e-12.
Allowing negative dual variable(s) as small as -1.46184518483e-12.
Allowing negative dual variable(s) as small as -1.4640255154e-12.
MTOW [lbs] = 132.53
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 = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.1265996816e-12.
Allowing negative dual variable(s) as small as -1.65844334793e-12.
Allowing negative dual variable(s) as small as -1.63563260158e-12.
Allowing negative dual variable(s) as small as -1.63483246038e-12.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.2544387639e-11.
Allowing negative dual variable(s) as small as -4.86404313812e-11.
Allowing negative dual variable(s) as small as -4.13813429939e-12.
Allowing negative dual variable(s) as small as -4.13943025279e-12.
Solving took 4 GP solves and 2.52 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 4.13 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21029054834e-13.
Allowing negative dual variable(s) as small as -8.14964415397e-14.
Allowing negative dual variable(s) as small as -2.06978531536e-14.
Allowing negative dual variable(s) as small as -2.06969857919e-14.
Allowing negative dual variable(s) as small as -1.04306602418e-12.
Allowing negative dual variable(s) as small as -1.64669840264e-12.
Allowing negative dual variable(s) as small as -1.46465435266e-12.
Allowing negative dual variable(s) as small as -1.46577801979e-12.
MTOW [lbs] = 132.53
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 = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.12236305319e-12.
Allowing negative dual variable(s) as small as -1.65165407393e-12.
Allowing negative dual variable(s) as small as -1.63697787964e-12.
Allowing negative dual variable(s) as small as -1.6358316611e-12.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.25444918836e-11.
Allowing negative dual variable(s) as small as -4.86406840432e-11.
Allowing negative dual variable(s) as small as -4.13829218711e-12.
Allowing negative dual variable(s) as small as -4.13938681893e-12.
Solving took 4 GP solves and 7.61 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 6.3 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
	

Standard Error