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Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20190312080634)

Took 1 min 44 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.090719512601538e-14.
Allowing negative dual variable(s) as small as -6.857188428188721e-14.
Allowing negative dual variable(s) as small as -1.5038144340895343e-13.
Allowing negative dual variable(s) as small as -1.4979857632102522e-13.
Solving took 4 GP solves and 13.1 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.061576158205128e-14.
Allowing negative dual variable(s) as small as -7.050696831933934e-14.
Allowing negative dual variable(s) as small as -1.5301822309243818e-13.
Allowing negative dual variable(s) as small as -1.4800920905555515e-13.
Solving took 4 GP solves and 15.9 seconds.
Allowing negative dual variable(s) as small as -5.19077836269588e-13.
Allowing negative dual variable(s) as small as -1.4308641077542816e-12.
Allowing negative dual variable(s) as small as -4.443893170114066e-13.
Allowing negative dual variable(s) as small as -4.426927574519013e-13.
Allowing negative dual variable(s) as small as -1.2958806120191846e-12.
Allowing negative dual variable(s) as small as -1.0905619940090872e-12.
Allowing negative dual variable(s) as small as -1.091577024082968e-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 -2.4780725389378952e-14.
Allowing negative dual variable(s) as small as -5.69602174126042e-12.
Allowing negative dual variable(s) as small as -2.0879140439632774e-11.
Allowing negative dual variable(s) as small as -2.088078384183973e-11.
Solving took 4 GP solves and 21.3 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 7.77 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.182885370880186e-13.
Allowing negative dual variable(s) as small as -1.428067733511007e-12.
Allowing negative dual variable(s) as small as -4.439244111198448e-13.
Allowing negative dual variable(s) as small as -4.4407012789182687e-13.
Allowing negative dual variable(s) as small as -1.2956917440007376e-12.
Allowing negative dual variable(s) as small as -1.0903196748235366e-12.
Allowing negative dual variable(s) as small as -1.0913212607904788e-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 -2.4976461256841383e-14.
Allowing negative dual variable(s) as small as -5.695862020678009e-12.
Allowing negative dual variable(s) as small as -2.0878945541877943e-11.
Allowing negative dual variable(s) as small as -2.0880710268928508e-11.
Solving took 4 GP solves and 11.8 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 7.59 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)