Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171011224113)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.55870020152e-13. Allowing negative dual variable(s) as small as -3.21922176416e-13. Allowing negative dual variable(s) as small as -5.20642990526e-13. Allowing negative dual variable(s) as small as -5.48804925116e-13. Solving took 4 GP solves and 2.04 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 -5.67190825557e-13. Allowing negative dual variable(s) as small as -3.38966701929e-13. Allowing negative dual variable(s) as small as -5.25873181806e-13. Allowing negative dual variable(s) as small as -5.4388655038e-13. Solving took 4 GP solves and 4.55 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 -8.5693691726e-13. Allowing negative dual variable(s) as small as -7.72083785794e-13. Allowing negative dual variable(s) as small as -7.38487396235e-13. Allowing negative dual variable(s) as small as -7.41046980723e-13. Allowing negative dual variable(s) as small as -7.40909937569e-13. Allowing negative dual variable(s) as small as -1.5175356631e-12. Allowing negative dual variable(s) as small as -1.0482085035e-12. Allowing negative dual variable(s) as small as -1.06272260957e-12. Allowing negative dual variable(s) as small as -1.06180710925e-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 -1.48263476149e-12. Allowing negative dual variable(s) as small as -1.14737863308e-13. Allowing negative dual variable(s) as small as -6.26495383349e-15. Allowing negative dual variable(s) as small as -1.6124645022e-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 -1.49485302033e-14. Allowing negative dual variable(s) as small as -1.08187436509e-12. Solving took 4 GP solves and 1.74 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 5.27 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351 Allowing negative dual variable(s) as small as -8.57045337477e-13. Allowing negative dual variable(s) as small as -7.72417720063e-13. Allowing negative dual variable(s) as small as -7.3815085988e-13. Allowing negative dual variable(s) as small as -7.41276831584e-13. Allowing negative dual variable(s) as small as -7.41431221973e-13. Allowing negative dual variable(s) as small as -1.51903056106e-12. Allowing negative dual variable(s) as small as -1.0468683212e-12. Allowing negative dual variable(s) as small as -1.06121979693e-12. Allowing negative dual variable(s) as small as -1.06332423335e-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 -1.48093061252e-12. Allowing negative dual variable(s) as small as -1.14652970278e-13. Allowing negative dual variable(s) as small as -5.35010404035e-15. Allowing negative dual variable(s) as small as -1.62330327132e-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 -1.47645186482e-14. Allowing negative dual variable(s) as small as -1.08032108788e-12. Solving took 4 GP solves and 7.34 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 21.6 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351