• DocumentCode
    3350831
  • Title

    Real-time Onboard Orbit Determination Using GPS Navigation Solutions

  • Author

    Yu, Zejiang ; You, Zheng

  • Author_Institution
    Dept. of Precision Instrum. & Mechanology, Tsinghua Univ., Beijing, China
  • fYear
    2011
  • fDate
    21-23 Oct. 2011
  • Firstpage
    949
  • Lastpage
    952
  • Abstract
    Real-time onboard orbit determination utilizing GNSS is a promising approach with broader usage during the last decade. In this paper, we propose a novel real-time orbit determination algorithm based on reduced-dynamic technique using GPS navigation solutions. The proposed algorithm employs Extended Kalman Filter and introduces colored-noise whitening and self-adaptive method to enhance the robustness. Simulation results using real GPS navigation data collected from the CHAMP satellite show that the overall position and velocity errors of the estimated orbit are 10.860m and 0.0128m/s RMS respectively. Furthermore, prototype software of the algorithm has been developed and successfully demonstrated in DSP TMS320C6713.
  • Keywords
    Global Positioning System; Kalman filters; nonlinear filters; CHAMP satellite; DSP TMS320C6713; GNSS; GPS navigation solutions; colored-noise whitening; extended Kalman filter; global positioning system; prototype software; realtime onboard orbit determination; reduced-dynamic technique; self-adaptive method; velocity errors; Extraterrestrial measurements; Global Positioning System; Mathematical model; Orbits; Pollution measurement; Real time systems; GPS; colored-noise; real-time onboard orbit determination; selfadaptive filter;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation, Measurement, Computer, Communication and Control, 2011 First International Conference on
  • Conference_Location
    Beijing
  • Print_ISBN
    978-0-7695-4519-6
  • Type

    conf

  • DOI
    10.1109/IMCCC.2011.239
  • Filename
    6154265