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.


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    Titel :

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


    Beteiligte:
    Klein, R. W. (Autor:in) / Lapins, M. (Autor:in) / Martorella, R. P. (Autor:in) / Sturm, M. (Autor:in)

    Kongress:

    Aerospace Sciences Meeting ; 1982 ; Orlando, FL


    Erscheinungsdatum :

    01.01.1982


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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

    KLEIN, R. / LAPINS, M. / MARTORELLA, R. et al. | AIAA | 1982



    Exploiting the close-coupled canard

    MARTIN, J. / FOSTER, N. | AIAA | 1987



    Exploiting the close-coupled canard

    Martin, J.D. / Foster, N.R. | Tema Archiv | 1987