• DocumentCode
    55536
  • Title

    Decoupling trajectory tracking for gliding reentry vehicles

  • Author

    Zixuan Liang ; Zhang Ren ; Xingyue Shao

  • Author_Institution
    Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
  • Volume
    2
  • Issue
    1
  • fYear
    2015
  • fDate
    January 10 2015
  • Firstpage
    115
  • Lastpage
    120
  • Abstract
    A decoupling trajectory tracking method for gliding reentry vehicles is presented to improve the reliability of the guidance system. Function relations between state variables and control variables are analyzed. To reduce the coupling between control channels, the multiple-input multiple-output (MIMO) tracking system is separated into a series of two single-input single-output (SISO) subsystems. Tracking laws for both velocity and altitude are designed based on the sliding mode control (SMC). The decoupling approach is verified by the Monte Carlo simulations, and compared with the linear quadratic regulator (LQR) approach in some specific conditions. Simulation results indicate that the decoupling approach owns a fast convergence speed and a strong anti-interference ability in the trajectory tracking.
  • Keywords
    MIMO systems; Monte Carlo methods; aircraft control; linear quadratic control; trajectory control; variable structure systems; LQR approach; MIMO tracking system; Monte Carlo simulations; SISO subsystems; SMC; antiinterference ability; control variables; convergence speed; decoupling trajectory tracking method; function relations; gliding reentry vehicles; guidance system reliability; linear quadratic regulator approach; multiple-input multiple-output tracking system; single-input single-output subsystems; sliding mode control; state variables; Aerodynamics; Earth; MIMO; Mathematical model; Trajectory; Uncertainty; Vehicles; Hypersonic; decoupling control; reentry vehicle; sliding mode control (SMC); trajectory tracking;
  • fLanguage
    English
  • Journal_Title
    Automatica Sinica, IEEE/CAA Journal of
  • Publisher
    ieee
  • ISSN
    2329-9266
  • Type

    jour

  • DOI
    10.1109/JAS.2015.7032913
  • Filename
    7032913