• DocumentCode
    3504590
  • Title

    A new tool for the analysis of modal control laws: the `pole attractors´

  • Author

    Magni, Jean-François ; Champetier, Calixte ; Menard, Philippe

  • Author_Institution
    CERT-DERA, Toulouse, France
  • fYear
    1989
  • fDate
    13-15 Dec 1989
  • Firstpage
    1349
  • Abstract
    In the design of modal control laws, particular attention must be devoted to the choice of the closed-loop eigenvalues. In the output feedback case, this choice becomes more and more crucial as the number of degrees of freedom appearing in the control design decreases. Then the assignment of right eigenvectors often induces weakly observable poles. The reluctance of the feedback to move away from these poles can be represented by attracting zones of the complex plane, called pole attractors. In this study the pole attractors are geometrically defined and their attractivity is quantified. The usefulness of such a concept for synthesizing modal control laws is illustrated for a realistic aircraft autopilot design
  • Keywords
    closed loop systems; control system synthesis; eigenvalues and eigenfunctions; feedback; poles and zeros; aircraft autopilot design; closed-loop eigenvalues; complex plane; control system synthesis; eigenvectors; feedback; modal control laws; pole attractors; Actuators; Aerodynamics; Aerospace control; Aircraft; Control design; Damping; Eigenvalues and eigenfunctions; Observability; Output feedback; Time factors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1989., Proceedings of the 28th IEEE Conference on
  • Conference_Location
    Tampa, FL
  • Type

    conf

  • DOI
    10.1109/CDC.1989.70359
  • Filename
    70359