Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180423170114)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.050126983263681e-14. Allowing negative dual variable(s) as small as -7.590672881918614e-14. Allowing negative dual variable(s) as small as -1.5105191403241847e-13. Allowing negative dual variable(s) as small as -1.4975260614891184e-13. Solving took 4 GP solves and 2.83 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.0065420559297635e-14. Allowing negative dual variable(s) as small as -7.408396812680351e-14. Allowing negative dual variable(s) as small as -1.5029123778820264e-13. Allowing negative dual variable(s) as small as -1.49964242412981e-13. Solving took 4 GP solves and 2.89 seconds. Allowing negative dual variable(s) as small as -5.183093537697303e-13. Allowing negative dual variable(s) as small as -1.4299846029519614e-12. Allowing negative dual variable(s) as small as -4.4411002653177434e-13. Allowing negative dual variable(s) as small as -4.4534341492319385e-13. Allowing negative dual variable(s) as small as -1.296652889226646e-12. Allowing negative dual variable(s) as small as -1.091077532142104e-12. Allowing negative dual variable(s) as small as -1.0907750397359806e-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 -2.6935918773229872e-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 -2.6323134905121117e-14. Allowing negative dual variable(s) as small as -5.695990546995736e-12. Allowing negative dual variable(s) as small as -2.0878980496915973e-11. Allowing negative dual variable(s) as small as -2.0880920619396563e-11. Solving took 4 GP solves and 3.02 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.81 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.155962462533026e-13. Allowing negative dual variable(s) as small as -1.429564799870775e-12. Allowing negative dual variable(s) as small as -4.45107492530461e-13. Allowing negative dual variable(s) as small as -4.447033019605584e-13. Allowing negative dual variable(s) as small as -1.296481043182307e-12. Allowing negative dual variable(s) as small as -1.0922071623856167e-12. Allowing negative dual variable(s) as small as -1.0929329273198785e-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 -1.7433970933566911e-16. 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 -2.4087889072699903e-14. Allowing negative dual variable(s) as small as -5.695981004904887e-12. Allowing negative dual variable(s) as small as -2.0878942246231564e-11. Allowing negative dual variable(s) as small as -2.088071071287965e-11. Solving took 4 GP solves and 2.77 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.71 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417