• DocumentCode
    1729972
  • Title

    Sliding mode control design based on Ackermann´s formula

  • Author

    Ackermann, Jürgen ; Utkin, Vadim I.

  • Author_Institution
    Inst. for Robotics & Syst. Dynamics, German Aerosp. Res. Establ., Wessling, Germany
  • Volume
    4
  • fYear
    1994
  • Firstpage
    3622
  • Abstract
    The sliding mode control methods are developed to design systems which have the desired dynamic behavior and are robust with respect to perturbations. It is shown that the discontinuity plane for sliding mode control may be found in an explicit form using Ackermann´s formula. Two design procedures are derived: 1) static controllers are designed to enforce sliding modes with the desired dynamic properties after a finite time interval; and 2) dynamic controllers are designed that exhibit the desired dynamic properties during the entire control process
  • Keywords
    control system synthesis; dynamics; reduced order systems; state feedback; variable structure systems; Ackermann´s formula; design procedures; discontinuity plane; dynamic controllers; dynamics; finite time interval; reduced order systems; sliding mode control; state feedback; static controllers; Artificial intelligence; Control systems; Eigenvalues and eigenfunctions; Equations; Linear feedback control systems; Motion control; Nonlinear control systems; Sliding mode control; State feedback; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1994., Proceedings of the 33rd IEEE Conference on
  • Conference_Location
    Lake Buena Vista, FL
  • Print_ISBN
    0-7803-1968-0
  • Type

    conf

  • DOI
    10.1109/CDC.1994.411715
  • Filename
    411715