• DocumentCode
    596621
  • Title

    Self-regulation control scheme for reusable launch vehicle reentry attitude control

  • Author

    Jianshuang Song ; Zhang Ren ; Zhen Shen

  • Author_Institution
    Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
  • fYear
    2012
  • fDate
    18-20 Oct. 2012
  • Firstpage
    447
  • Lastpage
    451
  • Abstract
    Integrating sliding mode control and nonlinear dynamic inversion technique forms a new robust controller. Using nonlinear extended state observer to build the estimation of system disturbance, and based on the estimation, magnitude of the sliding mode item could be regulated to improve the control effect. Stability of This new controller is analyzed. This new control scheme is used in the reentry attitude control for reusable launch vehicle. Feasibility and validity of the new controller is demonstrated with simulation examples.
  • Keywords
    aircraft control; attitude control; control system synthesis; nonlinear control systems; observers; robust control; variable structure systems; control effect; controller stability; nonlinear dynamic inversion technique; nonlinear extended state observer; reentry attitude control; reusable launch vehicle; robust controller; self-regulation control scheme; sliding mode control; system disturbance; Conferences;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Advanced Computational Intelligence (ICACI), 2012 IEEE Fifth International Conference on
  • Conference_Location
    Nanjing
  • Print_ISBN
    978-1-4673-1743-6
  • Type

    conf

  • DOI
    10.1109/ICACI.2012.6463203
  • Filename
    6463203