This paper describes an experimental study on an integrated servo control method. Conventional servo control schemes may experience performance degradation under the presence of physical constraints. An integrated scheme is proposed in this study to address this problem. In the proposed method, three controllers correspond to autopilot commands directly instead of four actuators. Various simulations and experiments show that the proposed integrated servo control method provides better performance than the conventional ones.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Experimental study on integrated servo control for canard-controlled missiles [Correspondence]


    Beteiligte:
    Sang Hwa Kim (Autor:in) / Min-Jea Tank (Autor:in) / Ha-Jun Lee (Autor:in)


    Erscheinungsdatum :

    01.06.2016


    Format / Umfang :

    1626439 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Aerodynamic predictions of pitch and roll control for canard-controlled missiles

    Landers, Michael / Hall, Les / Auman, Lamar | AIAA | 2000



    AIAA-2006-6569 Optimal Control Solution for Dual (Tail and Canard) Controlled Missiles

    Mracek, C. / Ridgely, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006