The design of a nonlinear adaptive dynamic surface controller for the longitudinal model of a hypothetical supersonic flight vehicle is considered in this work. The uncertain nonlinear functions in the strict feedback flight vehicle model are approximated by using radial basis function neural networks. A detailed stability analysis of the designed angle-of-attack controller shows that all the signals of the closed loop system are uniformly ultimately bounded. The performance of the designed controller is verified through numerical simulations of the flight vehicle model.


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    Title :

    Adaptive Dynamic Surface Control of a Supersonic Flight Vehicle



    Published in:

    Applied Mechanics and Materials ; 110-116 ; 3580-3586


    Publication date :

    2011-10-24


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Adaptive Dynamic Surface Control of a Supersonic Flight Vehicle

    Butt, W.A. / Yan, L. / Kendrick, A.S. | British Library Conference Proceedings | 2012




    Supersonic Flight

    Clarke, Basil | TIBKAT | 1965