Some fundamental information on control system effects on controllability of highly-maneuverable aircraft at high angles of attack and techniques for enhancing fighter aircraft departure/spin resistance using control system design is summarized. The discussion includes: (a) a brief review of pertinent high angle-of-attack phenomena including aerodynamics, inertia coupling, and kinematic coupling; (b) effects of conventional stability augmentation systems at high-alpha; (c) high-alpha control system concepts designed to enhance departure/spin resistance; and (d) the outlook for applications of these concepts to future fighters, particularly those designs which incorporate relaxed static stability.


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    Title :

    Control system techniques for improved departure/spin resistance for fighter aircraft


    Contributors:

    Conference:

    Aerospace Meeting ; 1979 ; Los Angeles, CA


    Publication date :

    1979-12-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English