The attitude director indicator system utilizes cathode-ray tube image generation techniques to provide an attitude-director display with a high degree of flexibility. The display includes roll and pitch attitude, roll, pitch and yaw command, glide slope deviation, crab angle and radar altitude, and indications of failures. (Author)


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    Title :

    Attitude Director Indicator System for FAA All-Weather Landing System


    Publication date :

    1969


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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