• DocumentCode
    3496331
  • Title

    An overview of aerial refueling control systems applied to UAVs

  • Author

    Panday, A. ; Pedro, Jimoh O.

  • Author_Institution
    Sch. of Mech., Ind. & Aeronaut. Eng., Univ. of the Witwatersrand, Johannesburg, South Africa
  • fYear
    2013
  • fDate
    9-12 Sept. 2013
  • Firstpage
    1
  • Lastpage
    5
  • Abstract
    The development and extension of unmanned aerial vehicle (UAV) capabilities has ignited a renewed interest in aerial refueling. Two methods of aerial refueling still remain: boom-receptacle and probe-drogue. The receiver aircraft dynamics are complex, nonlinear and cross-coupled to that of the tanker, causing relative control to be a challenge. A survey of flight control systems as applied to the problem of UAV aerial refueling has been performed. Various techniques, both classical and novel, have been applied to this control problem. Trends indicate a focused research effort within specific aspects of aerial refueling. Even with much attention being given to this field, control system designs have by no means been exhausted.
  • Keywords
    aircraft control; autonomous aerial vehicles; control system synthesis; fuel systems; UAV; aerial refueling control system; boom-receptacle; control system design; flight control system; probe-drogue; receiver aircraft dynamics; tanker; unmanned aerial vehicle; Aerodynamics; Aerospace control; Aircraft; Atmospheric modeling; Control systems; Military aircraft; Receivers; aerial refueling; control systems; unmanned aerial vehicle (UAV); unmanned combat aerial vehicle (UCAV);
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    AFRICON, 2013
  • Conference_Location
    Pointe-Aux-Piments
  • ISSN
    2153-0025
  • Print_ISBN
    978-1-4673-5940-5
  • Type

    conf

  • DOI
    10.1109/AFRCON.2013.6757788
  • Filename
    6757788