Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171115183653)
Standard Output
Allowing negative dual variable(s) as small as -1.21116658369e-13. Allowing negative dual variable(s) as small as -8.15562894996e-14. Allowing negative dual variable(s) as small as -2.07681094544e-14. Allowing negative dual variable(s) as small as -2.06787711954e-14. Allowing negative dual variable(s) as small as -1.04394444478e-12. Allowing negative dual variable(s) as small as -1.6523199909e-12. Allowing negative dual variable(s) as small as -1.46156437647e-12. Allowing negative dual variable(s) as small as -1.46453964407e-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 -1.12470623093e-12. Allowing negative dual variable(s) as small as -1.6567528599e-12. Allowing negative dual variable(s) as small as -1.64171042212e-12. Allowing negative dual variable(s) as small as -1.63591644571e-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 -1.25444897575e-11. Allowing negative dual variable(s) as small as -4.86405767805e-11. Allowing negative dual variable(s) as small as -4.13816686217e-12. Allowing negative dual variable(s) as small as -4.13942155031e-12. Solving took 4 GP solves and 15.5 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 15.8 seconds. Max payload weight [lbf] = 8.892 Max take off weight [lbf] = 140.364 Allowing negative dual variable(s) as small as -1.21300539058e-13. Allowing negative dual variable(s) as small as -8.14912373692e-14. Allowing negative dual variable(s) as small as -2.06596892371e-14. Allowing negative dual variable(s) as small as -2.05885655746e-14. Allowing negative dual variable(s) as small as -1.04105634703e-12. Allowing negative dual variable(s) as small as -1.65249021064e-12. Allowing negative dual variable(s) as small as -1.46166455675e-12. Allowing negative dual variable(s) as small as -1.46543909819e-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 -1.12642512505e-12. Allowing negative dual variable(s) as small as -1.65428911889e-12. Allowing negative dual variable(s) as small as -1.6334162755e-12. Allowing negative dual variable(s) as small as -1.63950775699e-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 -1.25445300179e-11. Allowing negative dual variable(s) as small as -4.8640657348e-11. Allowing negative dual variable(s) as small as -4.1382402902e-12. Allowing negative dual variable(s) as small as -4.13928922846e-12. Solving took 4 GP solves and 11.5 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 19.5 seconds. Max payload weight [lbf] = 8.892 Max take off weight [lbf] = 140.364