A new algorithm is proposed for assigning some of the eigenvalues to the desired places while guaranteeing the stability of the closed-loop system. For partial eigenstructure assignment, the null space approach is utilized, and additional feedback is used to stabilize the remaining eigenvalues. The quadratic type performance index is chosen to determine the additional feedback gain lying on the constrained vector space, and the problem in computing the additional feedback gain is formulated as the linear quadratic regulator problem with output feedback. To demonstrate the effectiveness of the proposed method, a design methodology is illustrated through application on the aircraft.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Partial eigenstructure assignment algorithm in flight control system design


    Contributors:
    Hee-Seob Kim (author) / Youdan Kim (author)


    Publication date :

    1999-10-01


    Size :

    254455 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English






    Robust Flight Control Design with Eigenstructure Assignment

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


    Eigenstructure assignment, eigensensitivity, and flight control design

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