• DocumentCode
    1459978
  • Title

    Terminal Sliding Mode Control for Spacecraft Formation Flying

  • Author

    Hui, Liu ; Li, Junfeng

  • Author_Institution
    Tsinghua Univ., Beijing, China
  • Volume
    45
  • Issue
    3
  • fYear
    2009
  • fDate
    7/1/2009 12:00:00 AM
  • Firstpage
    835
  • Lastpage
    846
  • Abstract
    This paper considers the problem of relative motion control for spacecraft formation flying (SFF). Using terminal sliding mode technique, a relative position/velocity tracking control based on the nonlinear model is developed. The presented controller enables rapid formation reconfiguration with feasible fuel cost and strong robustness in the presence of uncertain but bounded disturbances. A nonlinear model with J2 disturbance and bounded uncertainties is used for dynamic simulation.
  • Keywords
    position control; space vehicles; variable structure systems; vehicle dynamics; velocity control; nonlinear model; position control; spacecraft formation flying; terminal sliding mode control; velocity tracking control; Aerodynamics; Costs; Radar tracking; Robust control; Satellites; Sliding mode control; Space technology; Space vehicles; Trajectory; Uncertainty;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2009.5259168
  • Filename
    5259168
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1459978