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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    Title :

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


    Contributors:


    Publication date :

    2009-01-01


    Size :

    2002419 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English