• DocumentCode
    2999423
  • Title

    A Fusion Estimation Method for Flight State Estimation

  • Author

    Runquan, WANG ; Zhongke, Shi

  • Author_Institution
    Coll. of Autom., Northwestern Polytech. Univ., Xi´´an, China
  • fYear
    2010
  • fDate
    25-27 June 2010
  • Firstpage
    57
  • Lastpage
    61
  • Abstract
    To get accurate estimation of flight state, a new fusion estimation method was presented. In the scheme, equipments of INS, GPS, wireless radio, and infrared equipments with different wavelength were considered. Firstly, three dimensional motion model of an aircraft was described, and then model simplification was discussed. By analysis of deferent equipment measurement errors, a new method for equivalent computational measurements and equivalent error were proposed. The new method was used for flight data processing. The experimental results show that fusion estimation outperforms any single measurement.
  • Keywords
    aircraft testing; inertial navigation; inertial systems; measurement errors; state estimation; GPS; INS; aircraft; flight data processing; flight state estimation; fusion estimation method; infrared equipments; measurement errors; three dimensional motion model; wireless radio; Aerodynamics; Aircraft; Measurement errors; Measurement uncertainty; Noise measurement; State estimation; flight state; fusion estimation; measurement errors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electrical and Control Engineering (ICECE), 2010 International Conference on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4244-6880-5
  • Type

    conf

  • DOI
    10.1109/iCECE.2010.22
  • Filename
    5630849