A new smooth second-order sliding mode control (SSOSM) is proposed and proved for a system driven by uncertain sufficiently smooth disturbances. The main target application of this technique, the missile interceptor guidance-control system against targets performing evasive maneuvers, is considered to demonstrate benefits of this design for a two-loop integration of guidance and flight control systems. The designed guidance-control system performance is verified via computer simulations using a miniature hypervelocity kinetic energy endo-atmospheric interceptor planar model.


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    Titel :

    Guidance and Control of Missile Interceptor using Second-Order Sliding Modes


    Beteiligte:
    Shtessel, Y.B. (Autor:in) / Shkolnikov, I.A. (Autor:in) / Levant, A. (Autor:in)


    Erscheinungsdatum :

    2009-01-01


    Format / Umfang :

    2002419 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch