V/STOL aircrafts have different flight modes, including conventional mode, hover and transition flight. And the control effectors include thrust engines, thrust vectors and aerodynamic actuators. The dynamic model of V/STOL aircrafts varies significantly due to jet-induced effect during hover and transition flight. In this paper, dynamic model of V/STOL aircraft propulsion system and jet-induced forces are built. The 6-DOF nonlinear equations of motion, for a V/STOL UAV are formulated and simulated. Simulations results validate the dynamic model built in this paper. And the dynamic model could be used for propulsion system and control system design.


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    Title :

    Dynamics modeling and analysis of thrust-vectored V/STOL aircraft


    Contributors:


    Publication date :

    2013-07-01


    Size :

    360148 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English