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- W2357751966 abstract "The rotor of tiltrotor aircraft acts as common rotor in helicopter mode as well as propeller in fixed-wing airplane mode.In order to research the flight control method for tiltrotor airplane,a mathematics model is developed in this paper.In the model,the modified blade element analysis theory is used to model the rotor,and the modified momentum theory is used to calculate the induced velocity.The simulation is performed with Matlab/Simulink and the result shows that the model contains the basic properties of tiltrotor." @default.
- W2357751966 created "2016-06-24" @default.
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- W2357751966 date "2006-01-01" @default.
- W2357751966 modified "2023-09-22" @default.
- W2357751966 title "Modeling and Simulation for Tiltrotor Airplane" @default.
- W2357751966 hasPublicationYear "2006" @default.
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