• DocumentCode
    700647
  • Title

    Partial linearization by dynamic feedback for systems with perturbed input vector fields

  • Author

    Kremer, J.-P.

  • Author_Institution
    Dept. of Aeronaut., R. Inst. of Technol., Stockholm, Sweden
  • fYear
    1997
  • fDate
    1-7 July 1997
  • Firstpage
    1284
  • Lastpage
    1290
  • Abstract
    Input-output linearization and decoupling by feedback are considered for minimum phase systems with perturbation terms in the input vector fields. Perturbations inducing a reduction in relative degree are considered. The perturbed system may then be partially linearized by feedback. It is shown that a dynamic feedback can be used to achieve linear and decoupled input-output relations for the perturbed system that are of the same order as those obtained by static feedback for the unperturbed system. The dynamic feedback law is advantageous because it reduces the excursions at the plant input while maintaining control accuracy. Examples are presented.
  • Keywords
    feedback; linearisation techniques; nonlinear control systems; control accuracy; decoupled input-output relations; dynamic feedback law; input-output linearization; linear input-output relations; minimum phase systems; partially-linearized perturbed system; perturbed input vector fields; plant input; relative degree reduction; static feedback; unperturbed system; Aerodynamics; Aerospace control; Approximation methods; Heuristic algorithms; Manifolds; Nonlinear dynamical systems; Vehicle dynamics; Dynamic Feedback; Feedback Linearization; Perturbation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (ECC), 1997 European
  • Conference_Location
    Brussels
  • Print_ISBN
    978-3-9524269-0-6
  • Type

    conf

  • Filename
    7082277