United States Air Force jet cargo transport must be capable of landing under conditions of limited visibility; landing function without dependence on ground base systems is accomplished through vertical navigation computer; two step programmed let-down to predetermined longitude and latitude is concept of system; in favorable terrain let-downs and approaches are planned to 200 ft altitude; computer outputs can be used by flight director for manual pilot control and by automatic flight control system for automatic modes; system is designed for future improvements.


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    Titel :

    Military and civil all weather landing systems for C-141


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Cannon, C.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :






    All-weather landing

    Philip Butterworth-Hayes | Online Contents | 2015