• DocumentCode
    3291845
  • Title

    On O(T2) state regulation with output feedback sliding mode control for sampled-data systems

  • Author

    Thang Nguyen ; Wu-Chung Su ; Gajic, Z.

  • Author_Institution
    Dept. of Electr. Eng., Rutgers Univ., Piscataway, NJ, USA
  • fYear
    2010
  • fDate
    June 30 2010-July 2 2010
  • Firstpage
    1823
  • Lastpage
    1828
  • Abstract
    This paper deals with the problem of output feedback sliding mode control for sampled-data systems in the presence of external disturbances. A discrete-time high gain output feedback control strategy is proposed to achieve a quasi sliding mode with an O(T3) boundary layer, where T is the sampling period. This new control strategy enables an O(T2) bound for state regulation, which outperforms the O(T) result induced by the one-step-ahead disturbance approximation method. The analysis of stability and robustness of the closed-loop system is carried out with the help of the singular perturbation technique. A numerical example of an aircraft attitude output feedback control problem is given to illustrate the efficacy of the new method.
  • Keywords
    aircraft control; approximation theory; attitude control; closed loop systems; discrete time systems; feedback; sampled data systems; singularly perturbed systems; stability; variable structure systems; aircraft attitude output feedback control problem; boundary layer; closed-loop system; discrete-time high gain output feedback control strategy; one-step-ahead disturbance approximation method; output feedback sliding mode control; sampled-data systems; singular perturbation technique; stability analysis; state regulation; Aerospace control; Aircraft; Approximation methods; Attitude control; Output feedback; Perturbation methods; Robust stability; Sampling methods; Sliding mode control; Stability analysis;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2010
  • Conference_Location
    Baltimore, MD
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4244-7426-4
  • Type

    conf

  • DOI
    10.1109/ACC.2010.5531437
  • Filename
    5531437