This paper proposes a type-2 fuzzy adaptive sliding mode control scheme for tracking control of hypersonic aircraft with uncertainties. This method uses full-state feedback to linearize the nonlinear model of hypersonic aircraft. Combining the interval type-2 fuzzy approach and adaptive sliding mode control keeps the system stable in the existence of uncertain parameters. For rapid stabilization of the system, the adaptive laws are designed using a direct constructive Lyapunov analysis together with a well-established type-2 fuzzy logic control. Simulation test results indicate that the proposed control scheme provides enhancement of robustness to parametric uncertainty and improvement in tracking performance of the hypersonic aircraft.


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    Titel :

    Type-2 fuzzy adaptive sliding mode control of hypersonic flight


    Beteiligte:
    Jiao, Xin (Autor:in) / Fidan, Baris (Autor:in) / Jiang, Ju (Autor:in) / Kamel, Mohamed (Autor:in)


    Erscheinungsdatum :

    2019-06-01


    Format / Umfang :

    14 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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    Xu, H. / Leung, P. / Mirmirani, M. et al. | British Library Conference Proceedings | 2001



    Adaptive Sliding Mode Control of a Hypersonic Flight Vehicle (AAS 01-240)

    Xu, H. / Leung, P. / Mirmirani, M. et al. | British Library Conference Proceedings | 2001