The performance benefits to be gained from relaxed static stability (RSS) are illustrated for M = 0.9 and M = 2.0 flight conditions. The longitudinal, directional, and lateral control system structure is developed. The effect of static margin, bandwidth, and canard-wing interaction on canard rate requirements is analyzed. Control and maneuver limiter functions are developed and implemented about all three axes; simulation results strikingly demonstrate the concomitant improvement in energy management and improved resistance to departure and spin.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Control law development for a close-coupled canard, relaxed static stability fighter


    Contributors:
    Klein, R. W. (author) / Lapins, M. (author) / Martorella, R. P. (author) / Sturm, M. (author)

    Conference:

    Aerospace Sciences Meeting ; 1982 ; Orlando, FL


    Publication date :

    1982-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English