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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    Titel :

    Nonlinear guidance techniques for agile missiles


    Weitere Titelangaben:

    Nichtlineare Regelungsmethoden für die Flugkörperlenkung


    Beteiligte:
    Innocenti, M. (Autor:in)

    Erschienen in:

    Control Engineering Practice ; 9 , 10 ; 1131-1144


    Erscheinungsdatum :

    2001


    Format / Umfang :

    14 Seiten, 21 Bilder, 1 Tabelle, 19 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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