• DocumentCode
    2342778
  • Title

    On the feedback control of the wave equation

  • Author

    Alli, Hasan ; Singh, Tarunraj

  • Author_Institution
    Dept. of Mech. & Aerosp. Eng., State Univ. of New York, Buffalo, NY, USA
  • fYear
    1996
  • fDate
    15-18 Sep 1996
  • Firstpage
    291
  • Lastpage
    296
  • Abstract
    This paper addresses the problem of design of collocated and noncollocated controllers for a uniform bar without structural damping. The bar whose dynamics are described by the wave equation is required to perform a rest-to-rest maneuver. A time delay controller whose gains are determined using the root-locus technique is used to control the noncollocated system. The effect of sensor locations on the stability of the system is investigated when the actuator is located at one end of the bar. The critical gains which correspond to a pair of poles entering the right-half of the s-plane and the optimal gains which corresponding to locating the closed-loop poles at the left extreme of the root-locus for each vibration modes are determined. The gain which minimizes a quadratic cost, in the range of the critical gains, is selected as the optimum gain
  • Keywords
    closed loop systems; control system synthesis; delay systems; feedback; flexible structures; poles and zeros; root loci; wave equations; bar dynamics; closed-loop poles; collocated controller design; feedback control; noncollocated controller design; quadratic cost minimization; rest-to-rest maneuver; root-locus technique; sensor locations; stability; time delay controller; uniform bar; vibration modes; wave equation; Actuators; Aerospace engineering; Control systems; Delay effects; Feedback control; Open loop systems; Partial differential equations; Stability; Transfer functions; Vibration control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1996., Proceedings of the 1996 IEEE International Conference on
  • Conference_Location
    Dearborn, MI
  • Print_ISBN
    0-7803-2975-9
  • Type

    conf

  • DOI
    10.1109/CCA.1996.558717
  • Filename
    558717