Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180420092045)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.97838357879943e-14.
Allowing negative dual variable(s) as small as -8.220117295176799e-14.
Allowing negative dual variable(s) as small as -1.5185335627831975e-13.
Allowing negative dual variable(s) as small as -1.4929507283212295e-13.
Solving took 4 GP solves and 2.55 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.950411162749305e-14.
Allowing negative dual variable(s) as small as -8.150554883790129e-14.
Allowing negative dual variable(s) as small as -1.5165256203597544e-13.
Allowing negative dual variable(s) as small as -1.5226405206125726e-13.
Solving took 4 GP solves and 8.23 seconds.
Allowing negative dual variable(s) as small as -5.237338340791098e-13.
Allowing negative dual variable(s) as small as -5.139846881441201e-13.
Allowing negative dual variable(s) as small as -5.13623865661117e-13.
Allowing negative dual variable(s) as small as -5.139291769928889e-13.
Allowing negative dual variable(s) as small as -2.4104026066784634e-13.
Allowing negative dual variable(s) as small as -1.8385249919705693e-14.
Allowing negative dual variable(s) as small as -1.259755212472402e-12.
Allowing negative dual variable(s) as small as -1.2606476192805749e-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 -1.9411989377049466e-14.
Allowing negative dual variable(s) as small as -1.1449825462750418e-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 -5.4341347547333855e-11.
Allowing negative dual variable(s) as small as -6.44975548289435e-12.
Allowing negative dual variable(s) as small as -1.9339119392212776e-11.
Allowing negative dual variable(s) as small as -1.9354660117771925e-11.
Solving took 4 GP solves and 2.15 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.86 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.239732259187946e-13.
Allowing negative dual variable(s) as small as -5.106540190702447e-13.
Allowing negative dual variable(s) as small as -5.136776420888722e-13.
Allowing negative dual variable(s) as small as -5.15039400017514e-13.
Allowing negative dual variable(s) as small as -2.3532478049537175e-13.
Allowing negative dual variable(s) as small as -1.958372700117117e-14.
Allowing negative dual variable(s) as small as -1.2599298774423895e-12.
Allowing negative dual variable(s) as small as -1.258728364594841e-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 -2.1412125544850724e-14.
Allowing negative dual variable(s) as small as -1.1434473159988023e-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 -5.4341215872462315e-11.
Allowing negative dual variable(s) as small as -6.4495575650170755e-12.
Allowing negative dual variable(s) as small as -1.933933168249216e-11.
Allowing negative dual variable(s) as small as -1.9354608310272256e-11.
Solving took 4 GP solves and 2.21 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 5.09 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error