Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171115191541)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -9.97426967408e-14. Allowing negative dual variable(s) as small as -1.9932605913e-12. Allowing negative dual variable(s) as small as -2.17647297754e-12. Allowing negative dual variable(s) as small as -2.1678505345e-12. Solving took 4 GP solves and 29.5 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.00262680103e-13. Allowing negative dual variable(s) as small as -2.05636722928e-12. Allowing negative dual variable(s) as small as -2.1628610361e-12. Allowing negative dual variable(s) as small as -2.16572029407e-12. Solving took 4 GP solves and 143 seconds. Allowing negative dual variable(s) as small as -1.2119211884e-13. Allowing negative dual variable(s) as small as -8.14079706424e-14. Allowing negative dual variable(s) as small as -2.06744343867e-14. Allowing negative dual variable(s) as small as -2.06362704702e-14. Allowing negative dual variable(s) as small as -1.04321347567e-12. Allowing negative dual variable(s) as small as -1.64886355437e-12. Allowing negative dual variable(s) as small as -1.46142906804e-12. Allowing negative dual variable(s) as small as -1.46553667639e-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 -1.12727730796e-12. Allowing negative dual variable(s) as small as -1.65648809773e-12. Allowing negative dual variable(s) as small as -1.64057764769e-12. Allowing negative dual variable(s) as small as -1.63821018383e-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 -1.25444896701e-11. Allowing negative dual variable(s) as small as -4.86405502145e-11. Allowing negative dual variable(s) as small as -4.13824285912e-12. Allowing negative dual variable(s) as small as -4.13948427358e-12. Solving took 4 GP solves and 21.6 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 2.81 seconds. Max payload weight [lbf] = 8.892 Max take off weight [lbf] = 140.364 Allowing negative dual variable(s) as small as -1.2114181186e-13. Allowing negative dual variable(s) as small as -8.15363401796e-14. Allowing negative dual variable(s) as small as -2.06388725554e-14. Allowing negative dual variable(s) as small as -2.06692302163e-14. Allowing negative dual variable(s) as small as -1.04364260289e-12. Allowing negative dual variable(s) as small as -1.64646638337e-12. Allowing negative dual variable(s) as small as -1.46147026772e-12. Allowing negative dual variable(s) as small as -1.46272013599e-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 -1.12306171307e-12. Allowing negative dual variable(s) as small as -1.65393371741e-12. Allowing negative dual variable(s) as small as -1.63849728056e-12. Allowing negative dual variable(s) as small as -1.63370901009e-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 -1.2544487946e-11. Allowing negative dual variable(s) as small as -4.86405684327e-11. Allowing negative dual variable(s) as small as -4.13816668948e-12. Allowing negative dual variable(s) as small as -4.13955771952e-12. Solving took 4 GP solves and 104 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 6.59 seconds. Max payload weight [lbf] = 8.892 Max take off weight [lbf] = 140.364