• DocumentCode
    620325
  • Title

    A novel nonlinear model predictive control method based on LMI and feedback linearization

  • Author

    Rui Pang ; Zhongke Shi

  • Author_Institution
    Sch. of Autom., Northwestern Polytech. Univ., Xi´an, China
  • fYear
    2013
  • fDate
    25-27 May 2013
  • Firstpage
    3503
  • Lastpage
    3508
  • Abstract
    Nonlinear model predictive control (NMPC) mainly deals with complex dynamic systems with different kinds of nonlinearities, which is much more difficult to solve than normal linear model predictive. The non-convex optimization method inside MPC is its main challenging problem. A LMI based NMPC method is proposed combined with nonlinear feedback linearization can efficiently convert complex non-convex optimization problem to convex. The method minimizes the upper bound of cost function instead of itself, which can stabilize the whole system and achieve the control performance. A high angle of attack (HAOA) aircraft controller design example is illustrated in the end to demonstrate the validity of proposed method.
  • Keywords
    aircraft control; control nonlinearities; control system synthesis; convex programming; feedback; large-scale systems; linear matrix inequalities; linearisation techniques; nonlinear control systems; predictive control; HAOA aircraft controller design; LMI based NMPC method; complex dynamic systems; convex optimization; cost function; high angle of attack aircraft controller design; nonlinear feedback linearization; nonlinear model predictive control method; nonlinearities; Aerospace control; Aircraft; Asymptotic stability; Cost function; Predictive control; Predictive models; LMI; NMPC; convex optimization; feedback linearization;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Decision Conference (CCDC), 2013 25th Chinese
  • Conference_Location
    Guiyang
  • Print_ISBN
    978-1-4673-5533-9
  • Type

    conf

  • DOI
    10.1109/CCDC.2013.6561554
  • Filename
    6561554