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Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20190401143834)

Took 5.3 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.239567882151189e-14.
Allowing negative dual variable(s) as small as -7.984465952987074e-14.
Allowing negative dual variable(s) as small as -1.3164718880992465e-13.
Allowing negative dual variable(s) as small as -1.2665595568867039e-13.
Solving took 4 GP solves and 2.84 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.303868881231024e-14.
Allowing negative dual variable(s) as small as -7.689779802505514e-14.
Allowing negative dual variable(s) as small as -1.318002781566796e-13.
Allowing negative dual variable(s) as small as -1.2848055952474624e-13.
Solving took 4 GP solves and 2.65 seconds.
Allowing negative dual variable(s) as small as -7.890259626219809e-14.
Allowing negative dual variable(s) as small as -3.38600241595044e-13.
Allowing negative dual variable(s) as small as -1.0221441748559101e-12.
Allowing negative dual variable(s) as small as -1.0200985021968645e-12.
Allowing negative dual variable(s) as small as -2.777591524838474e-13.
Allowing negative dual variable(s) as small as -1.1531864601687508e-12.
Allowing negative dual variable(s) as small as -1.1158904475363357e-12.
Allowing negative dual variable(s) as small as -1.1154986981863624e-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 -1.2090846986806403e-12.
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 -6.145425215127482e-11.
Allowing negative dual variable(s) as small as -1.4545954918959036e-12.
Allowing negative dual variable(s) as small as -6.463173120715313e-12.
Allowing negative dual variable(s) as small as -6.468864609275126e-12.
Solving took 4 GP solves and 2.9 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.21 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -7.946681507275954e-14.
Allowing negative dual variable(s) as small as -3.38447585929158e-13.
Allowing negative dual variable(s) as small as -1.0207030533282424e-12.
Allowing negative dual variable(s) as small as -1.021184872773695e-12.
Allowing negative dual variable(s) as small as -2.8033922839371117e-13.
Allowing negative dual variable(s) as small as -1.1533613148741184e-12.
Allowing negative dual variable(s) as small as -1.1164494892815235e-12.
Allowing negative dual variable(s) as small as -1.1161345285504165e-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 -1.2090558046927435e-12.
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 -6.145427810796421e-11.
Allowing negative dual variable(s) as small as -1.454659110118587e-12.
Allowing negative dual variable(s) as small as -6.4632987955098575e-12.
Allowing negative dual variable(s) as small as -6.468896732642309e-12.
Solving took 4 GP solves and 2.91 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.22 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error

c:\anaconda2\lib\site-packages\pint\quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped.
  warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning)