Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180420100305)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.993779249648725e-14.
Allowing negative dual variable(s) as small as -8.165560241857328e-14.
Allowing negative dual variable(s) as small as -1.5099249975336626e-13.
Allowing negative dual variable(s) as small as -1.5017891444313314e-13.
Solving took 4 GP solves and 2 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.891734141174389e-14.
Allowing negative dual variable(s) as small as -8.08689053222178e-14.
Allowing negative dual variable(s) as small as -1.5305942277499263e-13.
Allowing negative dual variable(s) as small as -1.4986623053658832e-13.
Solving took 4 GP solves and 1.5 seconds.
Allowing negative dual variable(s) as small as -5.236141381592674e-13.
Allowing negative dual variable(s) as small as -5.124355800800728e-13.
Allowing negative dual variable(s) as small as -5.150792986574615e-13.
Allowing negative dual variable(s) as small as -5.139326464398408e-13.
Allowing negative dual variable(s) as small as -2.352232991720271e-13.
Allowing negative dual variable(s) as small as -1.859038097073995e-14.
Allowing negative dual variable(s) as small as -1.2603038187716797e-12.
Allowing negative dual variable(s) as small as -1.2600053379135945e-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
Allowing negative dual variable(s) as small as -1.764864296371904e-14.
Allowing negative dual variable(s) as small as -1.142204820309134e-13.
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 -5.434135476564275e-11.
Allowing negative dual variable(s) as small as -6.44948768921938e-12.
Allowing negative dual variable(s) as small as -1.933934707199555e-11.
Allowing negative dual variable(s) as small as -1.9354543622604302e-11.
Solving took 4 GP solves and 3.15 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.07 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.22968821026204e-13.
Allowing negative dual variable(s) as small as -5.128779345664469e-13.
Allowing negative dual variable(s) as small as -5.153568544136178e-13.
Allowing negative dual variable(s) as small as -5.161357452543314e-13.
Allowing negative dual variable(s) as small as -2.402292774428272e-13.
Allowing negative dual variable(s) as small as -1.9418060909215384e-14.
Allowing negative dual variable(s) as small as -1.260251560226966e-12.
Allowing negative dual variable(s) as small as -1.2594413359434675e-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
Allowing negative dual variable(s) as small as -2.2159357682127734e-14.
Allowing negative dual variable(s) as small as -1.1436815036680592e-13.
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 -5.434128389016089e-11.
Allowing negative dual variable(s) as small as -6.449664200059448e-12.
Allowing negative dual variable(s) as small as -1.933932021647185e-11.
Allowing negative dual variable(s) as small as -1.9354580746417254e-11.
Solving took 4 GP solves and 2.09 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.26 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error