Equipment was designed to be added or retrofitted to Boeing 707/720 airplanes to enable low approach and automatic landings to be made under conditions of low visibility as part of regular airline operations; major elements of system such as autopilot, yaw damper, approach and flare couplers and auto-throttle system are described in relation to their effects on performance and safety; details of monitoring and automatic test subsystems and test procedures used to evaluate system design.


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    Titel :

    Boeing/bendix automatic landing system for 707 aircraft


    Weitere Titelangaben:

    SAE-NASA -- Aerospace Vehicle Flight Control Conference -- Proc


    Beteiligte:
    Schoenman, R.L. (Autor:in) / Doniger, J. (Autor:in)

    Kongress:

    Proceedings of the SAE-NASA Aerospace Vehicle Flight Control Conference ; 1965 Landing



    Erscheinungsdatum :

    1965


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The Boeing/Bendix Automatic Landing System for the 707 Aircraft

    Doniger, J. / Schoenman, R. L. | SAE Technical Papers | 1965


    THE BOEING-BENDIX PRECISION APPROACH AND LANDING SYSTEM

    UTTERSTROM, J. / KESTEK, R. | AIAA | 1965


    Bell-Bendix instrument landing system

    Champlin, G.F. | Engineering Index Backfile | 1957


    Bell-Bendix instrument landing system

    Champlin, G.F. | Engineering Index Backfile | 1957