Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171115182727)
Standard Output
Allowing negative dual variable(s) as small as -1.21198190373e-13. Allowing negative dual variable(s) as small as -8.14348588563e-14. Allowing negative dual variable(s) as small as -2.07863240509e-14. Allowing negative dual variable(s) as small as -2.06709649397e-14. Allowing negative dual variable(s) as small as -1.04084254236e-12. Allowing negative dual variable(s) as small as -1.64693367451e-12. Allowing negative dual variable(s) as small as -1.46349490686e-12. Allowing negative dual variable(s) as small as -1.4643655212e-12. MTOW [lbs] = 132.53 Zero fuel weight [lbs] = 53.63 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 = 20.352 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.301 Allowing negative dual variable(s) as small as -1.12020722559e-12. Allowing negative dual variable(s) as small as -1.65538719885e-12. Allowing negative dual variable(s) as small as -1.63856948843e-12. Allowing negative dual variable(s) as small as -1.63844241993e-12. optimum loiter speed for min power, start of loiter [m/s] = 23.618 optimum loiter speed for min power, end of loiter [m/s] = 16.685 optimum cruise speed, inbound [m/s] = 31.024 optimum cruise speed, outbound [m/s] = 23.411 Beginning signomial solve. Allowing negative dual variable(s) as small as -1.25445656776e-11. Allowing negative dual variable(s) as small as -4.86405584922e-11. Allowing negative dual variable(s) as small as -4.13816859489e-12. Allowing negative dual variable(s) as small as -4.13935402382e-12. Solving took 4 GP solves and 3.52 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 2.13 seconds. Max payload weight [lbf] = 8.892 Max take off weight [lbf] = 140.364 Allowing negative dual variable(s) as small as -1.21185179947e-13. Allowing negative dual variable(s) as small as -8.15458811587e-14. Allowing negative dual variable(s) as small as -2.07438233257e-14. Allowing negative dual variable(s) as small as -2.07698441779e-14. Allowing negative dual variable(s) as small as -1.04775042808e-12. Allowing negative dual variable(s) as small as -1.64772145581e-12. Allowing negative dual variable(s) as small as -1.46369765266e-12. Allowing negative dual variable(s) as small as -1.46878321138e-12. MTOW [lbs] = 132.53 Zero fuel weight [lbs] = 53.63 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 = 20.352 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.301 Allowing negative dual variable(s) as small as -1.1214594791e-12. Allowing negative dual variable(s) as small as -1.65718610709e-12. Allowing negative dual variable(s) as small as -1.63720751366e-12. Allowing negative dual variable(s) as small as -1.63925318632e-12. optimum loiter speed for min power, start of loiter [m/s] = 23.618 optimum loiter speed for min power, end of loiter [m/s] = 16.685 optimum cruise speed, inbound [m/s] = 31.024 optimum cruise speed, outbound [m/s] = 23.411 Beginning signomial solve. Allowing negative dual variable(s) as small as -1.25444171048e-11. Allowing negative dual variable(s) as small as -4.86406774991e-11. Allowing negative dual variable(s) as small as -4.13813603127e-12. Allowing negative dual variable(s) as small as -4.13942781682e-12. Solving took 4 GP solves and 3.07 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 1.86 seconds. Max payload weight [lbf] = 8.892 Max take off weight [lbf] = 140.364