Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180111113207)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -3.0299872853800647e-13. Allowing negative dual variable(s) as small as -4.4536423160490557e-13. Allowing negative dual variable(s) as small as -4.660182829907544e-14. Allowing negative dual variable(s) as small as -8.149275525226596e-14. Solving took 4 GP solves and 41.8 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -2.3534060984709004e-13. Allowing negative dual variable(s) as small as -5.112440418925113e-13. Allowing negative dual variable(s) as small as -9.358898205025223e-14. Allowing negative dual variable(s) as small as -7.952839775615672e-14. Solving took 4 GP solves and 16.9 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 -5.0273601589892405e-12. Allowing negative dual variable(s) as small as -1.1071861670327111e-12. Allowing negative dual variable(s) as small as -2.4833512552432796e-12. Allowing negative dual variable(s) as small as -2.482046452212021e-12. Solving took 4 GP solves and 6.08 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 4.54 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 -5.027359989185604e-12. Allowing negative dual variable(s) as small as -1.1072413620934149e-12. Allowing negative dual variable(s) as small as -2.4835058740337523e-12. Allowing negative dual variable(s) as small as -2.4821051056619263e-12. Solving took 4 GP solves and 5.65 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 4.43 seconds. Max payload weight [lbf] = 9.202 Max take off weight [lbf] = 140.328