• DocumentCode
    2121718
  • Title

    A height controller design for miniature UAVs based on GPS and barometer

  • Author

    Wang, Song ; Li, Juan ; Wang, Sihong

  • Author_Institution
    UAV Res. Inst., Beihang Univ., Beijing, China
  • fYear
    2012
  • fDate
    21-23 April 2012
  • Firstpage
    31
  • Lastpage
    34
  • Abstract
    With the limitations of airborne sensors configuration of conventional miniature UAVs, this paper proposes a practical real-time algorithm which can integrate barometric height and GPS altitude. This algorithm uses the GPS altitude to calibrate baro-altimeter on-line, without considering the motion model and maneuverability of carrier. Tests showed that the fusion algorithm has significantly improved measurement results of altitude information, combining short-term and dynamic performance of barometric height with long-term stability of GPS altitude. On this basis, the height controller was designed for miniature UAVs, and successfully applied to the flight control system of a small unmanned aerial vehicle for polar research, with the control error less than 10m during cruise stage.
  • Keywords
    Global Positioning System; aircraft control; autonomous aerial vehicles; barometers; stability; GPS altitude stability; baro-altimeter online calibration; barometric height; flight control system; height controller design; miniature UAV; polar research; real-time algorithm; unmanned aerial vehicle; Aerospace control; Atmospheric measurements; Atmospheric modeling; Global Positioning System; Heuristic algorithms; Mercury (metals); Unmanned aerial vehicles; GPS; barometric; data fusion; hight control; miniature UAVs;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Consumer Electronics, Communications and Networks (CECNet), 2012 2nd International Conference on
  • Conference_Location
    Yichang
  • Print_ISBN
    978-1-4577-1414-6
  • Type

    conf

  • DOI
    10.1109/CECNet.2012.6201800
  • Filename
    6201800