Abstract A nonlinear controller is exploited and analyzed for the nonlinear longitudinal dynamics of a generic Hypersonic Vehicle in this paper. The vehicle model is nonlinear, multivariable and unstable. A combined nonlinear observer and back-stepping technique is adopted for designing a dynamic output-feedback controller that provides stable tracking of the velocity and altitude reference trajectories. The stability analysis of the closed-loop system and the convergence of the system outputs are verified based on the small-gain theorem. Numerical simulation results from the nonlinear model illustrate the effectiveness of the proposed control scheme.


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    Titel :

    Output feedback back-stepping control for a generic Hypersonic Vehicle via small-gain theorem


    Beteiligte:
    Zong, Qun (Autor:in) / Ji, Yuehui (Autor:in) / Zeng, Fanlin (Autor:in) / Liu, Helong (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2011-09-29


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch