• DocumentCode
    233747
  • Title

    Research on inertial information aided GPS tracking loop in high dynamic environment

  • Author

    Jin Lei ; Chen Shuai

  • Author_Institution
    Sch. of Autom., Nanjing Univ. Of Sci. & Technol., Nanjing, China
  • fYear
    2014
  • fDate
    28-30 July 2014
  • Firstpage
    728
  • Lastpage
    732
  • Abstract
    GPS signal will generate the doppler frequency offset and its higher derivative when the precision guided weapon, such as missile rocket and so on, are in flight. The common tracking loop cannot track the signal steady, so that the receiver is likely to lose lock the signal and even to lose the ability of positioning and navigation. In order to track the signal steady in high dynamic environment, a method of the inertial information aided GPS tracking loop is given. The method provides the dopplor frequency offset aid for the tracking loop with the predicted frequency. The experiment results show that the method can meet the dynamic requirement of 50g missile acceleration with respect to the satellite and overcome the dynamical stress effect markedly. GPS receiver has the better ability of tracking dynamically.
  • Keywords
    Doppler shift; Global Positioning System; missiles; satellite tracking; signal processing; Doppler frequency offset; GPS receiver; GPS signal generation; dynamical stress effect; high dynamic environment; inertial information aided GPS tracking loop; missile acceleration; missile rocket; precision guided weapon; satellite; Dopplor frequency offset; High dynamic; Inertial information aided; Tracking loop;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2014 33rd Chinese
  • Conference_Location
    Nanjing
  • Type

    conf

  • DOI
    10.1109/ChiCC.2014.6896716
  • Filename
    6896716