Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171018121412)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -9.40337217814e-14. Allowing negative dual variable(s) as small as -1.19098958126e-12. Allowing negative dual variable(s) as small as -1.13058000462e-12. Allowing negative dual variable(s) as small as -1.14365721754e-12. Solving took 4 GP solves and 2.12 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -9.16870745993e-14. Allowing negative dual variable(s) as small as -1.18934029292e-12. Allowing negative dual variable(s) as small as -1.14711235302e-12. Allowing negative dual variable(s) as small as -1.15249953678e-12. Solving took 4 GP solves and 1.57 seconds. Allowing negative dual variable(s) as small as -1.57004183959e-12. Allowing negative dual variable(s) as small as -3.96067813963e-12. Allowing negative dual variable(s) as small as -1.78679120111e-12. Allowing negative dual variable(s) as small as -2.08239328559e-12. Allowing negative dual variable(s) as small as -2.08100117e-12. Allowing negative dual variable(s) as small as -4.74035524375e-13. Allowing negative dual variable(s) as small as -8.93840448705e-13. Allowing negative dual variable(s) as small as -9.42251051489e-13. Allowing negative dual variable(s) as small as -9.42389612527e-13. MTOW [lbs] = 141.59 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 = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.32500216996e-13. Allowing negative dual variable(s) as small as -9.32658898029e-14. Allowing negative dual variable(s) as small as -1.18301527428e-13. Allowing negative dual variable(s) as small as -1.19798485368e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -9.61861387395e-13. Allowing negative dual variable(s) as small as -2.01617758465e-12. Allowing negative dual variable(s) as small as -1.25482715001e-14. Allowing negative dual variable(s) as small as -1.75128932284e-14. Solving took 4 GP solves and 2.75 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Solving took 4 GP solves and 2.11 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -1.56960208719e-12. Allowing negative dual variable(s) as small as -3.96027134697e-12. Allowing negative dual variable(s) as small as -1.78696207137e-12. Allowing negative dual variable(s) as small as -2.08209664787e-12. Allowing negative dual variable(s) as small as -2.08121367362e-12. Allowing negative dual variable(s) as small as -4.7270022098e-13. Allowing negative dual variable(s) as small as -8.92441068961e-13. Allowing negative dual variable(s) as small as -9.41775303576e-13. Allowing negative dual variable(s) as small as -9.42861890993e-13. MTOW [lbs] = 141.59 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 = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.3579640844e-13. Allowing negative dual variable(s) as small as -9.38796566527e-14. Allowing negative dual variable(s) as small as -1.2056816049e-13. Allowing negative dual variable(s) as small as -1.2042320266e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -9.61205774788e-13. Allowing negative dual variable(s) as small as -2.01690199396e-12. Allowing negative dual variable(s) as small as -1.3252583525e-14. Allowing negative dual variable(s) as small as -1.72641047758e-14. Solving took 4 GP solves and 2.47 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Solving took 4 GP solves and 1.88 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531