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Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20190401143503)

Took 15 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.2056449428850016e-14.
Allowing negative dual variable(s) as small as -7.140902452684728e-14.
Allowing negative dual variable(s) as small as -1.5162914326904975e-13.
Allowing negative dual variable(s) as small as -1.4901751707596667e-13.
Solving took 4 GP solves and 1.91 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.1817924950903205e-14.
Allowing negative dual variable(s) as small as -7.365505774736825e-14.
Allowing negative dual variable(s) as small as -1.5116553842009495e-13.
Allowing negative dual variable(s) as small as -1.4841426698719573e-13.
Solving took 4 GP solves and 1.6 seconds.
Allowing negative dual variable(s) as small as -5.156066545941584e-13.
Allowing negative dual variable(s) as small as -1.4297660277939883e-12.
Allowing negative dual variable(s) as small as -4.461171015934795e-13.
Allowing negative dual variable(s) as small as -4.430796007870441e-13.
Allowing negative dual variable(s) as small as -1.2960959345706402e-12.
Allowing negative dual variable(s) as small as -1.0912547991973054e-12.
Allowing negative dual variable(s) as small as -1.092166721644583e-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 -2.543666188038117e-14.
Allowing negative dual variable(s) as small as -5.6959552859935236e-12.
Allowing negative dual variable(s) as small as -2.0878988586424726e-11.
Allowing negative dual variable(s) as small as -2.088072732274576e-11.
Solving took 4 GP solves and 2.58 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.93 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.177403644696099e-13.
Allowing negative dual variable(s) as small as -1.4296602096619537e-12.
Allowing negative dual variable(s) as small as -4.4327042036940156e-13.
Allowing negative dual variable(s) as small as -4.433259315206328e-13.
Allowing negative dual variable(s) as small as -1.2954514847993148e-12.
Allowing negative dual variable(s) as small as -1.0917835645968266e-12.
Allowing negative dual variable(s) as small as -1.0916731928156675e-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 -1.0495077029659683e-15.
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 -2.4602503304529543e-14.
Allowing negative dual variable(s) as small as -5.6959556658878004e-12.
Allowing negative dual variable(s) as small as -2.087902183320906e-11.
Allowing negative dual variable(s) as small as -2.0880824427449867e-11.
Solving took 4 GP solves and 1.51 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.19 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)