Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428152243)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.085255133652211e-14. Allowing negative dual variable(s) as small as -7.420973557881183e-14. Allowing negative dual variable(s) as small as -1.5152462617962215e-13. Allowing negative dual variable(s) as small as -1.4805344450419256e-13. Solving took 4 GP solves and 3.47 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.166396824241026e-14. Allowing negative dual variable(s) as small as -7.532993326342385e-14. Allowing negative dual variable(s) as small as -1.522454037838905e-13. Allowing negative dual variable(s) as small as -1.4957219490741025e-13. Solving took 4 GP solves and 3.41 seconds. Allowing negative dual variable(s) as small as -5.179953688205785e-13. Allowing negative dual variable(s) as small as -1.4293167344137103e-12. Allowing negative dual variable(s) as small as -4.445385032303406e-13. Allowing negative dual variable(s) as small as -4.450780022313694e-13. Allowing negative dual variable(s) as small as -1.2971360097147056e-12. Allowing negative dual variable(s) as small as -1.0914506061096563e-12. Allowing negative dual variable(s) as small as -1.0903196748235366e-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 -2.4830771589913643e-14. Allowing negative dual variable(s) as small as -5.696017586722632e-12. Allowing negative dual variable(s) as small as -2.087898621023261e-11. Allowing negative dual variable(s) as small as -2.088089343742107e-11. Solving took 4 GP solves and 3.36 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 2.34 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.18710074892681e-13. Allowing negative dual variable(s) as small as -1.429713986089709e-12. Allowing negative dual variable(s) as small as -4.443077850080357e-13. Allowing negative dual variable(s) as small as -4.434005246300998e-13. Allowing negative dual variable(s) as small as -1.2981976604820034e-12. Allowing negative dual variable(s) as small as -1.0898211586646278e-12. Allowing negative dual variable(s) as small as -1.0895535775684584e-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 -2.0027382530152238e-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 -2.4358659459673975e-14. Allowing negative dual variable(s) as small as -5.69604305530929e-12. Allowing negative dual variable(s) as small as -2.0878951690357758e-11. Allowing negative dual variable(s) as small as -2.0880936771679592e-11. Solving took 4 GP solves and 3.46 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 3.3 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417