• DocumentCode
    3067067
  • Title

    Eigenstructure assignment, eigensensitivity, and flight control design

  • Author

    Sobel, K.M. ; Shapiro, E.Y.

  • Author_Institution
    Lockheed California Company, Burbank, CA
  • fYear
    1985
  • fDate
    11-13 Dec. 1985
  • Firstpage
    658
  • Lastpage
    659
  • Abstract
    A sensitivity measure which describes changes in the damping of complex conjugate eigenvalues due to changes in the entries of the closed loop system matrix is introduced. An example is presented to illustrate the application of eigenstructure assignment with damping sensitivity reduction to the design of a flight control system.
  • Keywords
    Aerospace control; Aircraft; Closed loop systems; Damping; Design methodology; Digital signal processing; Eigenvalues and eigenfunctions; Equations; Output feedback; Uncertain systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1985 24th IEEE Conference on
  • Conference_Location
    Fort Lauderdale, FL, USA
  • Type

    conf

  • DOI
    10.1109/CDC.1985.268575
  • Filename
    4048375
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3067067