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- W2391588929 abstract "As the titl rotor aircraft is a hybrid aircraft,it uses both helicopter and airplane control strategies to control the aircraft.So it is a significant problem to make sure that when to fade out the helicopter control strategies.It is necessary to describe the conversion mode via unified mathematical model before the simulation analysis.Based on the complex aerodynamic of XV-15 tilt rotor aircraft,the mathematical model of the tilt rotor was established with the consideration of the influence of the rotor wake on the airframe aerodynamcs.And then make use of Matlab software,the simulaiton model of XV-15 was built and trim on helicopter mode,conversion mode and airplane mode respectively were finished.Based on the comparison of the trim result,the law of operating characteristics was given,and the suggestion of the time to fade out the cyclic pitch control was given." @default.
- W2391588929 created "2016-06-24" @default.
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- W2391588929 date "2010-01-01" @default.
- W2391588929 modified "2023-09-24" @default.
- W2391588929 title "Simulation Analysis and Trim of Tilt Rotor Aircraft" @default.
- W2391588929 hasPublicationYear "2010" @default.
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