Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171014225841)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.41836107232e-13. Allowing negative dual variable(s) as small as -3.27885288365e-13. Allowing negative dual variable(s) as small as -5.49356567181e-13. Allowing negative dual variable(s) as small as -5.34959663373e-13. Solving took 4 GP solves and 3.94 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 -5.4349233447e-13. Allowing negative dual variable(s) as small as -3.51075071792e-13. Allowing negative dual variable(s) as small as -5.23184794099e-13. Allowing negative dual variable(s) as small as -5.42363029488e-13. Solving took 4 GP solves and 2.26 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 -8.57051409009e-13. Allowing negative dual variable(s) as small as -7.7240124019e-13. Allowing negative dual variable(s) as small as -7.3824540231e-13. Allowing negative dual variable(s) as small as -7.408457528e-13. Allowing negative dual variable(s) as small as -7.41481528954e-13. Allowing negative dual variable(s) as small as -1.52242780015e-12. Allowing negative dual variable(s) as small as -1.048737811e-12. Allowing negative dual variable(s) as small as -1.06168611229e-12. Allowing negative dual variable(s) as small as -1.06121654433e-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 -1.47830966218e-12. Allowing negative dual variable(s) as small as -1.14118458606e-13. Allowing negative dual variable(s) as small as -6.22787411919e-15. Allowing negative dual variable(s) as small as -1.62398740289e-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 -1.53889734657e-14. Allowing negative dual variable(s) as small as -1.0815360907e-12. Solving took 4 GP solves and 3.29 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 6.36 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351 Allowing negative dual variable(s) as small as -8.57220544548e-13. Allowing negative dual variable(s) as small as -7.7215664418e-13. Allowing negative dual variable(s) as small as -7.38382445464e-13. Allowing negative dual variable(s) as small as -7.41271627414e-13. Allowing negative dual variable(s) as small as -7.40908202845e-13. Allowing negative dual variable(s) as small as -1.51644235363e-12. Allowing negative dual variable(s) as small as -1.04902263091e-12. Allowing negative dual variable(s) as small as -1.06085095136e-12. Allowing negative dual variable(s) as small as -1.06350431933e-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 -1.48135605345e-12. Allowing negative dual variable(s) as small as -1.14266885884e-13. Allowing negative dual variable(s) as small as -6.471819608e-15. Allowing negative dual variable(s) as small as -1.61040451807e-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 -1.54742659777e-14. Allowing negative dual variable(s) as small as -1.08131135963e-12. Solving took 4 GP solves and 4.45 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 1.56 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351