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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    Title :

    Automatic stall prevention control for supersonic fighter aircraft


    Additional title:

    J Aircraft


    Contributors:
    Cook, R.H. (author)

    Published in:

    Publication date :

    1965


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English