• DocumentCode
    2035942
  • Title

    Data Fusion Approach Based on High Precision Barometric Altimeter and GPS

  • Author

    Hao Zhenhai ; Huang Shengguo

  • Author_Institution
    Sch. of Civil Aviation, Nanjing Univ. of Aeronaut. & Astronaut., Nanjing
  • fYear
    2009
  • fDate
    23-24 May 2009
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    In order to ensure the precision flying and the capability of precision approach and landing for small aircraft, a data fusion algorithm of federal Kalman filtering (FKF) based on high precision barometric altimeter and GPS is presented. The model of the data fusion algorithm is analyzed in detail. An improved adaptive filter algorithm is developed to eliminate the oblivious error of GPS data. The preliminary experiment results are given and the results show that the adaptive algorithm is efficient in improving the vertical positioning accuracy. The safety and the reliability of small aircraft in the process of near-enter is improved, which satisfies the landing requirement of civil aviation.
  • Keywords
    Global Positioning System; adaptive Kalman filters; sensor fusion; GPS; adaptive filter algorithm; data fusion; federal Kalman filtering; high precision barometric altimeter; Adaptive filters; Aircraft; Atmosphere; Atmospheric measurements; Extraterrestrial measurements; Global Positioning System; Information filtering; Information filters; Kalman filters; Mathematical model;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Systems and Applications, 2009. ISA 2009. International Workshop on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4244-3893-8
  • Electronic_ISBN
    978-1-4244-3894-5
  • Type

    conf

  • DOI
    10.1109/IWISA.2009.5072799
  • Filename
    5072799