Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180428101942)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.123332313949902e-14.
Allowing negative dual variable(s) as small as -7.413991295890376e-14.
Allowing negative dual variable(s) as small as -1.518273354261801e-13.
Allowing negative dual variable(s) as small as -1.4950670909619213e-13.
Solving took 4 GP solves and 3.44 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.221777871211586e-14.
Allowing negative dual variable(s) as small as -7.471410642945209e-14.
Allowing negative dual variable(s) as small as -1.5029644195863057e-13.
Allowing negative dual variable(s) as small as -1.490149149907527e-13.
Solving took 4 GP solves and 3.4 seconds.
Allowing negative dual variable(s) as small as -5.162762578558855e-13.
Allowing negative dual variable(s) as small as -1.4295387790186354e-12.
Allowing negative dual variable(s) as small as -4.4376481656005495e-13.
Allowing negative dual variable(s) as small as -4.450086132923303e-13.
Allowing negative dual variable(s) as small as -1.296300415100371e-12.
Allowing negative dual variable(s) as small as -1.0914358609601105e-12.
Allowing negative dual variable(s) as small as -1.0903003760248664e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.4906021467552123e-14.
Allowing negative dual variable(s) as small as -5.696106223929532e-12.
Allowing negative dual variable(s) as small as -2.087905728669951e-11.
Allowing negative dual variable(s) as small as -2.088084704193254e-11.
Solving took 4 GP solves and 2.81 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.182260870428834e-13.
Allowing negative dual variable(s) as small as -1.4297382722183727e-12.
Allowing negative dual variable(s) as small as -4.44809120092593e-13.
Allowing negative dual variable(s) as small as -4.443286016897474e-13.
Allowing negative dual variable(s) as small as -1.296927300796502e-12.
Allowing negative dual variable(s) as small as -1.0908822673308394e-12.
Allowing negative dual variable(s) as small as -1.0897747548116454e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.485885761425782e-14.
Allowing negative dual variable(s) as small as -5.695906386357962e-12.
Allowing negative dual variable(s) as small as -2.0879042407162893e-11.
Allowing negative dual variable(s) as small as -2.0880836860252406e-11.
Solving took 4 GP solves and 2.85 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.09 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error