• DocumentCode
    2230533
  • Title

    The Accuracy Relative Position Algorithm For Multi-Aircrafts

  • Author

    Jiang, Tao ; Chen, Weidong

  • Author_Institution
    Dept. of Electron. Eng. & Inf. Sci., Univ. of Sci. & Technol. of China, Hefei, China
  • fYear
    2009
  • fDate
    26-28 Dec. 2009
  • Firstpage
    3864
  • Lastpage
    3867
  • Abstract
    For the applications of aircrafts work in collaboration, the initial relative position of multi-aircrafts is significant. A new method, achieved the relative position of aircrafts, is presented. Firstly, the multiple hypothesis is established, based on the error model of INS, to estimate the relative error covariance matrix between Inertial Navigation System(INS) information of multi-aircrafts, which is necessary for the least-square estimate method. Then the different least-square estimate results of the relative position between aircrafts can be obtained under each hypothesis. Finally, the weighted estimate results can be acquired according to the Bayes´s formula. Simulation results show the stabilization and the precision of this algorithm in the relative position.
  • Keywords
    aircraft navigation; covariance matrices; inertial navigation; least mean squares methods; Bayes´s formula; accuracy relative position algorithm; inertial navigation system information; least-square estimate method; multi-aircrafts; multiple hypothesis; Aerospace electronics; Aerospace engineering; Aircraft manufacture; Aircraft navigation; Aircraft propulsion; Collaborative work; Computer errors; Dead reckoning; Inertial navigation; Information science;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Information Science and Engineering (ICISE), 2009 1st International Conference on
  • Conference_Location
    Nanjing
  • Print_ISBN
    978-1-4244-4909-5
  • Type

    conf

  • DOI
    10.1109/ICISE.2009.1166
  • Filename
    5455442