Much research is being conducted in the area of decoupled mode control systems for control configured vehicles (CCV). One such mode is pitch pointing where decoupling of specified variables is the control objective. This paper describes the application of eigenstructure assignment to the design of such systems. The eigenvectors are chosen in an intuitively appealing way to obtain the desired mode decoupling. Then the eigenvalues are chosen to trade off the degree of decoupling versus the speed of the response. This simple design method is illustrated by designing a pitch pointing control law for the AFTI/F-16 aircraft.


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    Titel :

    A design methodology for pitch flight control systems using eigenstructure assignment


    Weitere Titelangaben:

    Ein Entwicklungsverfahren fuer Fluglage-Regelungssysteme unter Verwendung der Eigenstrukturverteilung


    Beteiligte:
    Sobel, K.M. (Autor:in) / Shapiro, E.Y. (Autor:in)


    Erscheinungsdatum :

    1983


    Format / Umfang :

    6 Seiten, 3 Bilder, 1 Tabelle, 7 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Eigenstructure assignment, eigensensitivity, and flight control design

    Sobel, K.M. / Shapiro, E.Y. | Tema Archiv | 1985


    Robust Flight Control Design with Eigenstructure Assignment

    Tokutake, H. / International Federation of Automatic Control | British Library Conference Proceedings | 2002


    Flight Control Design for a Tailless Aircraft Using Eigenstructure Assignment

    Clara Nieto-Wire / Kenneth Sobel | DOAJ | 2011

    Freier Zugriff


    Flight control examples of robust eigenstructure assignment

    Sobel, K.M. / Shapiro, E.Y. | Tema Archiv | 1987