• DocumentCode
    3481124
  • Title

    Satellite navigation observation equations and theirs solution algorithm

  • Author

    Sun, Xigang ; Ji, Yuanfa

  • Author_Institution
    Guilin Univ. of Electron. Technol., Guilin, China
  • fYear
    2009
  • fDate
    5-7 Aug. 2009
  • Firstpage
    1695
  • Lastpage
    1698
  • Abstract
    The GPS positioning accuracy sometimes is poor for the big GDOP because of satellite distribution and the impact of systematic errors. To solve this problem, two sets of measurement equations were put forward in this paper: measurement equations subject to height constraint; hyperboloid measurement equations subject to height constraint, and Kalman filtering method was designed for solving these two different equations. Finally, these two methods were proved fast convergence and high precision through simulation tests comparing with general pseudo-range measurement equations.
  • Keywords
    Global Positioning System; Kalman filters; measurement errors; GPS positioning accuracy; Kalman filtering method; height constraint; hyperboloid measurement equations; satellite navigation observation equations; Differential equations; Error analysis; Extraterrestrial measurements; Filtering; Global Positioning System; Kalman filters; Nonlinear equations; Observatories; Satellite navigation systems; State estimation; Height constraint; Hyperboloid; Kalman filter; Measurement equations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Automation and Logistics, 2009. ICAL '09. IEEE International Conference on
  • Conference_Location
    Shenyang
  • Print_ISBN
    978-1-4244-4794-7
  • Electronic_ISBN
    978-1-4244-4795-4
  • Type

    conf

  • DOI
    10.1109/ICAL.2009.5262695
  • Filename
    5262695