• DocumentCode
    425327
  • Title

    Approximate model predictive control for gas turbine engines

  • Author

    Mu, Junxia ; Rees, David

  • Author_Institution
    Sch. of Electron., Univ. of Glamorgan, Wales, UK
  • Volume
    6
  • fYear
    2004
  • fDate
    June 30 2004-July 2 2004
  • Firstpage
    5704
  • Abstract
    A novel model predictive control strategy using instantaneous linearization of nonlinear models incorporating the generalized predictive control (GPC) called approximate model predictive control (AMPC) is used to control a shaft speed of a gas turbine engine. This method gives advantages over the nonlinear model predictive control (NMPC), which is computationally demanding and has local minimums. The performance of the model based control schemes is dependent on the accuracy of the process model, so firstly the paper examines the estimation of global nonlinear gas turbine models using NARMAX and neural network representations. The performance of the proposed methods is examined using a range of small and large random step tests. The results illustrate the improvements in control performance that can be achieved to that of gain-scheduling PID controllers.
  • Keywords
    aerospace engines; approximation theory; autoregressive moving average processes; gas turbines; neurocontrollers; nonlinear control systems; predictive control; random processes; shafts; statistical testing; three-term control; velocity control; NARMAX; approximate model predictive control; gain scheduling PID controllers; gas turbine engines; generalized predictive control; neural network; nonlinear gas turbine models; nonlinear model predictive control; process model; random step tests; shaft speed control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 2004. Proceedings of the 2004
  • Conference_Location
    Boston, MA, USA
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-8335-4
  • Type

    conf

  • Filename
    1384765