Adaptive control algorithms are of interest in the flight control systems design not only for their capability to improve performance and reliability but also for handling aerodynamic parameter uncertainties, external disturbances and modeling inaccuracies. This paper addresses a nonlinear direct adaptive sliding mode controller to perform a flight path tracking for a transportation aircraft. The synthesis of the adaptation laws is based on the positivity and Lyapunov design principle. Simulation results for different flight conditions for transportation aircraft are provided to illustrate the effectiveness of the proposed controller.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Flight path tracking based-on direct adaptive sliding mode control


    Beteiligte:
    Bouadi, H. (Autor:in) / Wu, H. (Autor:in) / Mora-Camino, F. (Autor:in)


    Erscheinungsdatum :

    01.06.2011


    Format / Umfang :

    564266 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Flight Path Tracking Based-On Direct Adaptive Sliding Mode Control

    Bouadi, H. / Hongying, W. / Wu, H. et al. | British Library Conference Proceedings | 2011


    Flight path tracking based-on direct adaptive sliding mode control

    Bouadi, H. / Wu, H. / Mora-Camino, F. | Tema Archiv | 2011



    Nonlinear adaptive and sliding mode flight path control of F/A-18 model

    Singh, S.N. / Steinberg, M.L. / Page, A.B. | IEEE | 2003


    Nonlinear adaptive flight control using sliding mode online learning

    Kruger, T. / Schnetter, P. / Placzek, R. et al. | Tema Archiv | 2011