The results of a study of the application of H infinity and mu synthesis techniques to the design of feedback control laws for the longitudinal dynamics of the High Angle of Attack Research Vehicle (HARV) are presented. The objective of this study is to develop methods for the design of feedback control laws which cause the closed loop longitudinal dynamics of the HARV to meet handling quality specifications over the entire flight envelope. Control law designs are based on models of the HARV linearized at various flight conditions. The control laws are evaluated by both linear and nonlinear simulations of typical maneuvers. The fixed gain control laws resulting from both the H infinity and mu synthesis techniques result in excellent performance even when the aircraft performs maneuvers in which the system states vary significantly from their equilibrium design values. Both the H infinity and mu synthesis control laws result in performance which compares favorably with an existing baseline longitudinal control law.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Feedback Control Laws for Highly Maneuverable Aircraft


    Beteiligte:
    W. L. Garrard (Autor:in) / G. J. Balas (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    41 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Feedback control laws for highly maneuverable aircraft

    Garrard, William L. / Balas, Gary J. | NTRS | 1995


    Feedback control laws for highly maneuverable aircraft

    Garrard, William L. / Balas, Gary J. | NTRS | 1992


    Feedback Control Laws for Highly Maneuverable Aircraft

    W. L. Garrard / G. J. Balas | NTIS | 1995


    HIGHLY MANEUVERABLE AIRCRAFT

    PIVEN PAVEL VLADISLAVOVICH | Europäisches Patentamt | 2019

    Freier Zugriff

    LQG controls for highly maneuverable aircraft

    STEIN, G. / HARTMANN, G. / GREENE, C. | AIAA | 1981