A simplified guidance system for air-to-air missiles is described, where the pilot adjusts his helmet sight to compensate for missile errors and this information is fed to a computer which computes correction data from error information, aircraft position information and missile position information. Correction data is then sent via a radio link to the missile control system which changes the flight path accordingly. (Author)


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    Title :

    Simplified High Accuracy Guidance System


    Contributors:

    Publication date :

    1976


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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