• DocumentCode
    486602
  • Title

    Dynamic Output Feedback Flight Control Laws using Eigenstructure Assignment

  • Author

    Sobel, Kenneth M. ; Shapiro, Eliezer Y.

  • Author_Institution
    Lockheed California Company, Burbank, California
  • fYear
    1986
  • fDate
    18-20 June 1986
  • Firstpage
    605
  • Lastpage
    610
  • Abstract
    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.
  • Keywords
    Aerospace control; Control system synthesis; Damping; Design methodology; Eigenvalues and eigenfunctions; Interconnected systems; Military aircraft; Output feedback; Stability; Time invariant systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1986
  • Conference_Location
    Seattle, WA, USA
  • Type

    conf

  • Filename
    4789009
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=486602