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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    Titel :

    Attitude Director Indicator System for FAA All-Weather Landing System


    Erscheinungsdatum :

    1969


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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