Features of command type radioinertial guidance system in which ground-based radar continuously determines position of missile during powered flight and digital computer accepts data; this is done by reference to previously stored trajectory information for particular target, computing appropriate orders to maintain missile on proper flight path; corrective orders are transmitted by radio to missile and applied to missile's autopilot and control system.


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    Title :

    Missile guidance


    Additional title:

    Bell Laboratories Rec


    Contributors:
    Felch, E.P. (author)

    Published in:

    Publication date :

    1959


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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