• DocumentCode
    1608042
  • Title

    Automatic Landing Control of UAV Based on Optical Guidance

  • Author

    Jian, Zhou ; Xin-min, Wang ; Xiao-yan, Wang

  • Author_Institution
    Sch. of Autom., Northwestern Polytech. Univ., Xi´´an, China
  • fYear
    2012
  • Firstpage
    152
  • Lastpage
    155
  • Abstract
    In this paper, the problem of landing for a UAV on the runway is discussed and a control method based on optical guidance is proposed. This method uses optical guidance to generate the guidance signal and then control the landing of the UAV along an ideal trajectory. In this paper, the design method of ideal trajectory and corresponding landing control method, which based on the small disturbance linearization model, are presented. The simulation results demonstrate that the control performance can satisfy the requirements of automatic landing of UAV and have the exact output tracking ability.
  • Keywords
    aircraft landing guidance; autonomous aerial vehicles; linearisation techniques; Optical Guidance; UAV; automatic landing control method; exact output tracking ability; guidance signal; small disturbance linearization model; Educational institutions; Integrated optics; Optical communication equipment; Optical feedback; Optical reflection; Optical variables measurement; Trajectory; UAV; automatic landing; optical guidance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Industrial Control and Electronics Engineering (ICICEE), 2012 International Conference on
  • Conference_Location
    Xi´an
  • Print_ISBN
    978-1-4673-1450-3
  • Type

    conf

  • DOI
    10.1109/ICICEE.2012.48
  • Filename
    6322337