The guidance system is composed of a heading command subsystem and a glide slope command subsystem. The heading subsystem is responsive to certain input data and continuously develops command signals for use in directing the aircraft from a remote location to a terminal point. The glide slope command subsystem is responsive to certain other input data and continuously develops command signals for use in controlling the rate of descent of the aircraft at the terminal point.


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    Title :

    Terminal Guidance System


    Contributors:
    S. W. Gee (author)

    Publication date :

    1972


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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