In order to achieve good handling (or flying) qualities in longitudinal axis for all flight conditions, an adaptive backstepping flight control law is presented. With the backstepping technique, an adaptive controller is synthesized for the purpose of accomplishing desired responses under a wide range of flight envelope. The specification assignments for flying qualities are used for selecting essential parameters of the proposed adaptive controller for all flight conditions. In comparison with other conventional control methods, the proposed adaptive control law is much simpler and easier to construct and implement. Simulation results show that the proposed method is capable of giving desired closed-loop dynamic performance and robustness against uncertainties within the subsonic and supersonic flight conditions


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Longitudinal axis flight control law design by adaptive backstepping


    Beteiligte:
    Hann-Shing Ju, (Autor:in) / Ching-Chih Tsai, (Autor:in)


    Erscheinungsdatum :

    01.01.2007


    Format / Umfang :

    5877664 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Robust Backstepping Control for Longitudinal Flight Dynamics

    Li, Ming Suo ;Chen, Mou ;Mei, Rong | Trans Tech Publications | 2013



    Nonlinear Flight Control Design Using Constrained Adaptive Backstepping

    Lars Sonneveldt / Q. P. Chu / J. A. Mulder | AIAA | 2007


    Nonlinear Adaptive Flight Control with a Backstepping Design Approach

    Steinberg, M. / Page, A. / AIAA | British Library Conference Proceedings | 1998