Automatic system, designed to provide warning approach to stall condition and protection from entering full stall and possible pitch-up, senses aircraft pitch rate and angle of attack and actuates stick-shaker warning device followed by application of corrective pitch control force if warning is ignored and unsatisfactory conditions persist; techniques developed for evaluation of system performance consisted of flights with lowered system boundary limits, 1-g stall approaches, windup turns, and rapid pull-ups; performance data are presented for several stages of development including final system and preflight and inflight checkout procedures to verify system operation.


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    Titel :

    Automatic stall prevention control for supersonic fighter aircraft


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Cook, R.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :