Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20190508150212)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.966860256416794e-14.
Allowing negative dual variable(s) as small as -7.123034800882166e-14.
Allowing negative dual variable(s) as small as -1.5073619435979069e-13.
Allowing negative dual variable(s) as small as -1.5013467899449573e-13.
Solving took 4 GP solves and 1.62 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.380505069263464e-14.
Allowing negative dual variable(s) as small as -7.320142755840031e-14.
Allowing negative dual variable(s) as small as -1.5223716384737962e-13.
Allowing negative dual variable(s) as small as -1.4933887459989137e-13.
Solving took 4 GP solves and 2.17 seconds.
Allowing negative dual variable(s) as small as -5.195757019071934e-13.
Allowing negative dual variable(s) as small as -1.4280417126588674e-12.
Allowing negative dual variable(s) as small as -4.423857113966534e-13.
Allowing negative dual variable(s) as small as -4.4362256923502486e-13.
Allowing negative dual variable(s) as small as -1.2956045741460698e-12.
Allowing negative dual variable(s) as small as -1.0907540062138343e-12.
Allowing negative dual variable(s) as small as -1.0915283434054235e-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 -2.428842602878649e-14.
Allowing negative dual variable(s) as small as -5.695946820508021e-12.
Allowing negative dual variable(s) as small as -2.0878996062469868e-11.
Allowing negative dual variable(s) as small as -2.088077539400957e-11.
Solving took 4 GP solves and 1.53 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.99 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.182208828724555e-13.
Allowing negative dual variable(s) as small as -1.4289350952489954e-12.
Allowing negative dual variable(s) as small as -4.446720769379908e-13.
Allowing negative dual variable(s) as small as -4.4276908528484427e-13.
Allowing negative dual variable(s) as small as -1.2964630454262438e-12.
Allowing negative dual variable(s) as small as -1.092475177162655e-12.
Allowing negative dual variable(s) as small as -1.0914246936777339e-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 -1.1188966420050406e-16.
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 -2.4613689009872746e-14.
Allowing negative dual variable(s) as small as -5.695832026579602e-12.
Allowing negative dual variable(s) as small as -2.0879138379780995e-11.
Allowing negative dual variable(s) as small as -2.08808044844297e-11.
Solving took 4 GP solves and 1.63 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.48 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error

/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped.
  warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning)