Dynamic inversion is a technique for control law design in which feedback is used to simultaneously cancel system dynamics and achieve desired dynamic response characteristics. However, dynamic inversion control laws lack robustness to modeling errors if improperly designed. This paper examines a simple linear example, control of roll rate about the body axis of high performance aircraft, to illustrate some robustness problems which may occur with a simple dynamic inversion control law. The paper demonstrates how structured singular value synthesis techniques can be used to enhance the robustness properties of the dynamic inversion controller.


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    Titel :

    Robust dynamic inversion control laws for aircraft control


    Beteiligte:
    Balas, Gary J. (Autor:in) / Garrard, William L. (Autor:in) / Reiner, Jakob (Autor:in)

    Kongress:

    AIAA Guidance, Navigation and Control Conference ; 1992 ; Hilton Head Island, SC, United States


    Erscheinungsdatum :

    1992-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Robust dynamic inversion control laws for aircraft control

    BALAS, GARY / GARRARD, WILLIAM / REINER, JAKOB | AIAA | 1992


    Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft

    Jacob Reiner / Gary J. Balas / William L. Garrard | AIAA | 1995




    Design of Robust Dynamic Inversion Control Laws using Multi-Objective Optimization

    Looye, Gertjan / Joos, Hans-Dieter | Deutsches Zentrum für Luft- und Raumfahrt (DLR) | 2001

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