Abstract Guidance law of a homing missile is implemented using an extended high gain observer without the model assumptions on target maneuvers. First, for a class of multi-input–multi-output nonlinear systems, extended high-gain observers are used for output feedback control with partial practical stabilization. Then the method is applied to the guidance law implementation of a homing missile with bearing only measurement. Simulation results show satisfactory performance.


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    Title :

    Guidance law implementation with performance recovery using an extended high-gain observer


    Contributors:
    Ma, Kemao (author) / Khalil, Hassan K. (author) / Yao, Yu (author)

    Published in:

    Publication date :

    2011-11-03


    Size :

    10 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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