An aircraft terminal area landing approach system based upon the Discrete Tracking Problem of Optimal Control Theory is presented. The control vector is made up of the aircraft's thrust and flight path. An example of the landing approach system will be presented.


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    Title :

    Aicraft terminal area guidance based on the discrete tracking problem of optimal control theory


    Additional title:

    Bordterminal fuer Gelaendelenkung basierend auf dem diskreten Nachfuehrproblem der optimalen Steuertheorie


    Contributors:

    Published in:

    Publication date :

    1984


    Size :

    4 Seiten, 7 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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