Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180110090622)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -2.9915566551741435e-13. Allowing negative dual variable(s) as small as -4.800053583775554e-13. Allowing negative dual variable(s) as small as -9.062824275762882e-14. Allowing negative dual variable(s) as small as -1.0795617871872665e-13. Solving took 4 GP solves and 2.68 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -2.9056314646003223e-13. Allowing negative dual variable(s) as small as -4.718736252434796e-13. Allowing negative dual variable(s) as small as -8.699638232023688e-14. Allowing negative dual variable(s) as small as -1.4872131304244363e-13. Solving took 4 GP solves and 2.8 seconds. MTOW [lbs] = 132.52 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 = 20.351 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] = 27.299 optimum loiter speed for min power, start of loiter [m/s] = 23.617 optimum loiter speed for min power, end of loiter [m/s] = 16.684 optimum cruise speed, inbound [m/s] = 31.019 optimum cruise speed, outbound [m/s] = 23.408 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.027304399061786e-12. Allowing negative dual variable(s) as small as -1.107190483904694e-12. Allowing negative dual variable(s) as small as -2.483434031665436e-12. Allowing negative dual variable(s) as small as -2.4819386855319764e-12. Solving took 4 GP solves and 2.31 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 1.59 seconds. Max payload weight [lbf] = 9.202 Max take off weight [lbf] = 140.328 MTOW [lbs] = 132.52 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 = 20.351 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] = 27.299 optimum loiter speed for min power, start of loiter [m/s] = 23.617 optimum loiter speed for min power, end of loiter [m/s] = 16.684 optimum cruise speed, inbound [m/s] = 31.019 optimum cruise speed, outbound [m/s] = 23.408 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.027411538704184e-12. Allowing negative dual variable(s) as small as -1.1072140989715051e-12. Allowing negative dual variable(s) as small as -2.4831202985828544e-12. Allowing negative dual variable(s) as small as -2.4819663291321526e-12. Solving took 4 GP solves and 2.31 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 1.6 seconds. Max payload weight [lbf] = 9.202 Max take off weight [lbf] = 140.328