Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171205104026)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -8.17679257636e-13. Allowing negative dual variable(s) as small as -6.81579792605e-13. Allowing negative dual variable(s) as small as -1.19862713505e-12. Allowing negative dual variable(s) as small as -1.18537731714e-12. Solving took 4 GP solves and 1.91 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -8.17679257636e-13. Allowing negative dual variable(s) as small as -6.81579792605e-13. Allowing negative dual variable(s) as small as -1.19862713505e-12. Allowing negative dual variable(s) as small as -1.18537731714e-12. Solving took 4 GP solves and 2.11 seconds. Allowing negative dual variable(s) as small as -9.5725836112e-14. Allowing negative dual variable(s) as small as -7.33029739339e-13. Allowing negative dual variable(s) as small as -7.32822981984e-13. Allowing negative dual variable(s) as small as -5.95630889391e-10. Allowing negative dual variable(s) as small as -4.87301415582e-13. Allowing negative dual variable(s) as small as -3.64114391849e-14. 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 -1.90055490876e-14. 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 -8.88423020754e-12. Allowing negative dual variable(s) as small as -2.87609104575e-12. Allowing negative dual variable(s) as small as -4.72558199966e-12. Allowing negative dual variable(s) as small as -4.72780174951e-12. Solving took 4 GP solves and 3.02 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 2.84 seconds. Max payload weight [lbf] = 9.228 Max take off weight [lbf] = 140.364 Allowing negative dual variable(s) as small as -9.5725836112e-14. Allowing negative dual variable(s) as small as -7.33029739339e-13. Allowing negative dual variable(s) as small as -7.32822981984e-13. Allowing negative dual variable(s) as small as -5.95630889391e-10. Allowing negative dual variable(s) as small as -4.87301415582e-13. Allowing negative dual variable(s) as small as -3.64114391849e-14. 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 -1.90055490876e-14. 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 -8.88423020754e-12. Allowing negative dual variable(s) as small as -2.87609104575e-12. Allowing negative dual variable(s) as small as -4.72558199966e-12. Allowing negative dual variable(s) as small as -4.72780174951e-12. Solving took 4 GP solves and 2.94 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 2.96 seconds. Max payload weight [lbf] = 9.228 Max take off weight [lbf] = 140.364