The theory and design of optimal adaptive control laws for automatic control of aircraft in the azimuth radio guidance system (instrument landing system) are presented. The control laws are developed using Pontryagin maximum principle with state dynamics and cost function. (Author)


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    Title :

    Optimal-Adaptive Control Theory for Automatic Control of Aircraft


    Contributors:

    Publication date :

    1972


    Size :

    44 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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