Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171016093547)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.51571375379e-13. Allowing negative dual variable(s) as small as -3.58207821044e-13. Allowing negative dual variable(s) as small as -5.34050234591e-13. Allowing negative dual variable(s) as small as -5.18564358121e-13. Solving took 4 GP solves and 28.6 seconds. Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.54620585569e-13. Allowing negative dual variable(s) as small as -3.36492552572e-13. Allowing negative dual variable(s) as small as -5.37974179093e-13. Allowing negative dual variable(s) as small as -5.20328571896e-13. Solving took 4 GP solves and 33.1 seconds. Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000 Allowing negative dual variable(s) as small as -8.57169370205e-13. Allowing negative dual variable(s) as small as -7.72592927134e-13. Allowing negative dual variable(s) as small as -7.38496937214e-13. Allowing negative dual variable(s) as small as -7.40963713997e-13. Allowing negative dual variable(s) as small as -7.41314128139e-13. Allowing negative dual variable(s) as small as -1.5185025546e-12. Allowing negative dual variable(s) as small as -1.04814280085e-12. Allowing negative dual variable(s) as small as -1.06288523989e-12. Allowing negative dual variable(s) as small as -1.0624487401e-12. 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 = 21.769 speed at top of climb [m/s] = 26.550 design loiter speed [m/s] = 25.056 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 -1.47805834412e-12. Allowing negative dual variable(s) as small as -1.14467138025e-13. Allowing negative dual variable(s) as small as -6.11999600303e-15. Allowing negative dual variable(s) as small as -1.60893325572e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.207 optimum loiter speed for min power, end of loiter [m/s] = 17.178 optimum cruise speed, inbound [m/s] = 36.034 optimum cruise speed, outbound [m/s] = 25.521 Beginning signomial solve. Allowing negative dual variable(s) as small as -1.46245525947e-14. Allowing negative dual variable(s) as small as -1.08149416935e-12. Solving took 4 GP solves and 2.54 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 1078212.3036 but bound is 1000000.0000 Max Speed [m/s]: 74.35 Beginning signomial solve. Solving took 4 GP solves and 1.65 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351 Allowing negative dual variable(s) as small as -8.56747832401e-13. Allowing negative dual variable(s) as small as -7.72563436835e-13. Allowing negative dual variable(s) as small as -7.38706838754e-13. Allowing negative dual variable(s) as small as -7.41046113362e-13. Allowing negative dual variable(s) as small as -7.41023561956e-13. Allowing negative dual variable(s) as small as -1.51801596467e-12. Allowing negative dual variable(s) as small as -1.04915360254e-12. Allowing negative dual variable(s) as small as -1.06202037182e-12. Allowing negative dual variable(s) as small as -1.0609128593e-12. 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 = 21.769 speed at top of climb [m/s] = 26.550 design loiter speed [m/s] = 25.056 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 -1.47790590529e-12. Allowing negative dual variable(s) as small as -1.13437579642e-13. Allowing negative dual variable(s) as small as -5.82422565037e-15. Allowing negative dual variable(s) as small as -1.60928020042e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.207 optimum loiter speed for min power, end of loiter [m/s] = 17.178 optimum cruise speed, inbound [m/s] = 36.034 optimum cruise speed, outbound [m/s] = 25.521 Beginning signomial solve. Allowing negative dual variable(s) as small as -1.53877396563e-14. Allowing negative dual variable(s) as small as -1.08174079922e-12. Solving took 4 GP solves and 4.82 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 1078212.3036 but bound is 1000000.0000 Max Speed [m/s]: 74.35 Beginning signomial solve. Solving took 4 GP solves and 1.76 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351