The eigenstructure assignment flight control design methodology is extended to include dynamic compensator synthesis. Dynamic compensators may be designed via eigenstructure assignment by utilizing a composite system structure. The success of this design methodology depends upon proper choice of the desired eigenvectors. An example of the lateral dynamics of an L-1011 aircraft is presented to illustrate the design method.


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    Title :

    Dynamic output feedback flight control laws using eigenstructure assignment


    Additional title:

    Rueckgekoppelte, dynamische Ausgangs-Flugregelfunktion mit Eigenstruktur-Zuteilung


    Contributors:
    Sobel, K.M. (author) / Shapiro, E.Y. (author)

    Published in:

    Publication date :

    1986


    Size :

    6 Seiten, 3 Bilder, 10 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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