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Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171016200542)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -1.09517403826e-11. Allowing negative dual variable(s) as small as -1.59540956834e-12. Allowing negative dual variable(s) as small as -1.66419916042e-12. Allowing negative dual variable(s) as small as -1.6212964131e-12. Solving took 4 GP solves and 2.05 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.09517403826e-11. Allowing negative dual variable(s) as small as -1.59540956834e-12. Allowing negative dual variable(s) as small as -1.66419916042e-12. Allowing negative dual variable(s) as small as -1.6212964131e-12. Solving took 4 GP solves and 1.84 seconds. Allowing negative dual variable(s) as small as -7.7404610499e-12. Allowing negative dual variable(s) as small as -3.41817685268e-11. Allowing negative dual variable(s) as small as -2.09242762006e-11. Allowing negative dual variable(s) as small as -2.11255665739e-11. Allowing negative dual variable(s) as small as -2.14140580268e-11. Allowing negative dual variable(s) as small as -4.88766817817e-12. Allowing negative dual variable(s) as small as -1.04710206434e-11. Allowing negative dual variable(s) as small as -5.89423637936e-12. Allowing negative dual variable(s) as small as -1.10735253432e-11. 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 -2.7590570887e-12. Allowing negative dual variable(s) as small as -7.11731021341e-12. Allowing negative dual variable(s) as small as -1.34969088857e-11. Allowing negative dual variable(s) as small as -1.37367198779e-11. 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 -3.42429863041e-11. Allowing negative dual variable(s) as small as -3.57348868425e-11. Allowing negative dual variable(s) as small as -3.9752637683e-13. Allowing negative dual variable(s) as small as -5.67093765358e-11. Solving took 4 GP solves and 2.71 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 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.09963729631e-13. Allowing negative dual variable(s) as small as -1.80545283585e-11. Allowing negative dual variable(s) as small as -7.28730699916e-11. Allowing negative dual variable(s) as small as -1.42986642492e-11. Solving took 4 GP solves and 1.99 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -7.7404610499e-12. Allowing negative dual variable(s) as small as -3.41817685268e-11. Allowing negative dual variable(s) as small as -2.09242762006e-11. Allowing negative dual variable(s) as small as -2.11255665739e-11. Allowing negative dual variable(s) as small as -2.14140580268e-11. Allowing negative dual variable(s) as small as -4.88766817817e-12. Allowing negative dual variable(s) as small as -1.04710206434e-11. Allowing negative dual variable(s) as small as -5.89423637936e-12. Allowing negative dual variable(s) as small as -1.10735253432e-11. 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 -2.7590570887e-12. Allowing negative dual variable(s) as small as -7.11731021341e-12. Allowing negative dual variable(s) as small as -1.34969088857e-11. Allowing negative dual variable(s) as small as -1.37367198779e-11. 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 -3.42429863041e-11. Allowing negative dual variable(s) as small as -3.57348868425e-11. Allowing negative dual variable(s) as small as -3.9752637683e-13. Allowing negative dual variable(s) as small as -5.67093765358e-11. Solving took 4 GP solves and 1.99 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 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.09963729631e-13. Allowing negative dual variable(s) as small as -1.80545283585e-11. Allowing negative dual variable(s) as small as -7.28730699916e-11. Allowing negative dual variable(s) as small as -1.42986642492e-11. Solving took 4 GP solves and 1.95 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531