• DocumentCode
    2107775
  • Title

    Robust control approach for re-entry vehicle based on inversion model

  • Author

    Ma Wen-Tao ; Zhang Qing-Zhen ; Shi Bobo ; Gao Chen

  • Author_Institution
    Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
  • fYear
    2010
  • fDate
    29-31 July 2010
  • Firstpage
    2005
  • Lastpage
    2009
  • Abstract
    The classical linear control method based on small-perturbation theory couldn´t adapt to the complex flight environment and large airspace, strong coupling and nonlinear characteristics of re-entry vehicle. A new robust control method combining fuzzy sliding mode control and nonlinear dynamic inversion is presented. Dynamic inversion controller can approximately decouple the nonlinear plant into three separate one-order linear systems. To eliminate tracking errors caused by dynamic inversion and disturbances, the fuzzy sliding mode controller outputs the input signal needed by dynamic inversion controller. Nonlinear simulation of a control system using MATLAB/SIMULINK shows that the designed controller can provide the excellent tracking performance and robustness of control system.
  • Keywords
    aerospace control; nonlinear control systems; perturbation techniques; robust control; MATLAB; SIMULINK; classical linear control method; control system; coupling; fuzzy sliding mode control; nonlinear dynamic inversion; nonlinear plant; nonlinear simulation; re-entry vehicle; robust control; small-perturbation theory; tracking errors; Mathematical model; Niobium; Nonlinear dynamical systems; Sliding mode control; Vehicle dynamics; Vehicles; Control System; Fuzzy Sliding Mode Control; Nonlinear Dynamic Inversion; Re-entry Vehicle;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2010 29th Chinese
  • Conference_Location
    Beijing
  • Print_ISBN
    978-1-4244-6263-6
  • Type

    conf

  • Filename
    5573429