Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20190401143503)
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)