It was found that improvement could be obtained if work load of pilot were decreased by providing partial automatic control; one of demands placed on system was its ability to deal with maneuvers and atmospheric disturbances typical for terminal phase of approach near ground; results obtained including analog simulation work and flight testing; system characteristics and recommended piloting techniques were applied to automatic speed control, designed for experimental research aircraft of STOL capability.


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    Titel :

    Improvements in longitudinal stability and control during landing approach of STOL aircraft


    Weitere Titelangaben:

    Can Aeronautics Space J


    Beteiligte:
    Brenckmann, M. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :