This paper investigates the use of preview control for optimal trajectory tracking for air-to-surface missiles. An off-line reference trajectory is obtained by solving a trajectory optimisation problem that incorporates the mission constraints. A trajectory following guidance scheme using a preview controller is used to generate the on-line control. An example of a terminal guidance trajectory with a bunt (climb and dive) manoeuvre and a look angle constraint is presented to demonstrate the method.


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    Titel :

    Optimal trajectory tracking using an output feedback preview controller


    Beteiligte:
    Farooq, A. (Autor:in) / MacBean, P. (Autor:in) / Limebeer, D.J.N. (Autor:in)

    Erscheinungsdatum :

    01.01.2006


    Format / Umfang :

    8 pages



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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