This patent is on a laser attitude detection and guidance system which uses a number of ground base laser transmitter/detector stations and at least two retroreflecting arrays on the missile to track and determine attitude correction signals to be sent for correcting the attitude of the missile relative to a predetermined trajectory.


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    Title :

    Single Plane Corner Reflector Guidance System


    Contributors:
    R. G. Conard (author) / K. M. Pell (author)

    Publication date :

    1974


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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