New approaches are presented for the guidance of agile missiles. They are based an nonlinear discontinuous control techniques applied to the generation of guidance laws capable of taking advantage of the vehicle's post-stall. capabilities. Agility and maneuverability requirements imply a higher bandwidth and robustness for the guidance loop, which are addressed by a variable structure controller format. Formal stability considerations are presented, and the guidance structures are validated using nonlinear simulation.


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    Title :

    Nonlinear guidance techniques for agile missiles


    Additional title:

    Nichtlineare Regelungsmethoden für die Flugkörperlenkung


    Contributors:

    Published in:

    Control Engineering Practice ; 9 , 10 ; 1131-1144


    Publication date :

    2001


    Size :

    14 Seiten, 21 Bilder, 1 Tabelle, 19 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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