Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180430090654)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.168001443456305e-14.
Allowing negative dual variable(s) as small as -7.66357463599654e-14.
Allowing negative dual variable(s) as small as -1.5024570129695825e-13.
Allowing negative dual variable(s) as small as -1.5007916784326447e-13.
Solving took 4 GP solves and 3 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.063354249768004e-14.
Allowing negative dual variable(s) as small as -7.534554577470765e-14.
Allowing negative dual variable(s) as small as -1.5139105247197193e-13.
Allowing negative dual variable(s) as small as -1.497708207454096e-13.
Solving took 4 GP solves and 2.87 seconds.
Allowing negative dual variable(s) as small as -5.173760725396548e-13.
Allowing negative dual variable(s) as small as -1.4292022426642959e-12.
Allowing negative dual variable(s) as small as -4.4327215509287754e-13.
Allowing negative dual variable(s) as small as -4.4316807168431893e-13.
Allowing negative dual variable(s) as small as -1.2962848025890872e-12.
Allowing negative dual variable(s) as small as -1.0908547285956582e-12.
Allowing negative dual variable(s) as small as -1.0911237191546519e-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] = 25.637
optimum cruise speed, outbound [m/s] = 36.269
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.4995791501609792e-14.
Allowing negative dual variable(s) as small as -5.695903911592388e-12.
Allowing negative dual variable(s) as small as -2.0878930279350085e-11.
Allowing negative dual variable(s) as small as -2.0880859609704485e-11.
Solving took 4 GP solves and 2.99 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.07 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.175634226750603e-13.
Allowing negative dual variable(s) as small as -1.431353299774507e-12.
Allowing negative dual variable(s) as small as -4.440527806570671e-13.
Allowing negative dual variable(s) as small as -4.442383960689966e-13.
Allowing negative dual variable(s) as small as -1.2969078935776146e-12.
Allowing negative dual variable(s) as small as -1.0904344918336029e-12.
Allowing negative dual variable(s) as small as -1.0903401662445966e-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] = 25.637
optimum cruise speed, outbound [m/s] = 36.269
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.518513449378194e-14.
Allowing negative dual variable(s) as small as -5.69591138038481e-12.
Allowing negative dual variable(s) as small as -2.087889202329231e-11.
Allowing negative dual variable(s) as small as -2.0880829841975633e-11.
Solving took 4 GP solves and 2.8 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.94 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error