• DocumentCode
    490401
  • Title

    Engine Throttle Control Using Anticipatory Band in the Sliding Phase Plane

  • Author

    Lee, B.J. ; Kim, Y.W. ; Cho, D.

  • Author_Institution
    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton NJ 08544
  • fYear
    1993
  • fDate
    2-4 June 1993
  • Firstpage
    1768
  • Lastpage
    1772
  • Abstract
    Drive-by-wire throttle control is investigated using the pneumatic cruise control hardware in a research automobile. The dynamics of this pneumatic system are difficult to model, and the solenoid valves used for controlling the pressure make accurate throttle control difficult. To this end, a dynamic switching control law is developed. This control law utilizes an anticipatory band in a phase plane, which is defined in the sense of sliding mode control. In contrast to the deadband frequently used in bang-bang control where the control direction is switched after the error crosses a desired value, the anticipatory band switches the control direction before the error reaches the desired value. Experimental results show stable and accurate tracking performance.
  • Keywords
    Automobiles; Engines; Error correction; Hardware; Pneumatic systems; Pressure control; Sliding mode control; Solenoids; Valves; Vehicle dynamics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1993
  • Conference_Location
    San Francisco, CA, USA
  • Print_ISBN
    0-7803-0860-3
  • Type

    conf

  • Filename
    4793181