• DocumentCode
    596750
  • Title

    Fuzzy Sliding Mode Control design for reusable launch vehicles

  • Author

    Jing Peng ; Xin Qu ; Zhang Ren

  • Author_Institution
    Sci. & Technol. on Aircraft Control Lab., Beihang Univ. (BUAA), Beijing, China
  • fYear
    2012
  • fDate
    18-20 Oct. 2012
  • Firstpage
    1053
  • Lastpage
    1056
  • Abstract
    This paper presents a Fuzzy Sliding Mode Control method for Reusable Launch Vehicles (RLV) in re-entry stage. RLV is a good measure to reduce transportation costs and improve launch vehicle performance effectively. The major contributions of this paper are as follows. Firstly, the non-linear mathematical model of reusable launch vehicle is introduced. And its characteristics are analyzed. Then, an attitude controller is designed by a combination of sliding mode control technology with fuzzy control technology. Finally, the simulations were performed based on the presented mathematical model and the designed controller.
  • Keywords
    attitude control; control system synthesis; fuzzy control; space vehicles; transportation; variable structure systems; attitude controller design; fuzzy sliding mode control design; launch vehicle performance improvement; nonlinear mathematical model; reentry stage; reusable launch vehicle; transportation cost reduction; Aerodynamics; Aerospace control; Fuzzy logic; Mathematical model; Niobium; Sliding mode control; Vehicles;
  • 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.2012.6463333
  • Filename
    6463333