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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    Titel :

    Simplified High Accuracy Guidance System


    Beteiligte:
    R. L. Schultz (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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