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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    Title :

    Optimal trajectory tracking using an output feedback preview controller


    Contributors:
    Farooq, A. (author) / MacBean, P. (author) / Limebeer, D.J.N. (author)

    Publication date :

    2006-01-01


    Size :

    8 pages



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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