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Volume 40 Issue 9
Sep.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(9): 1195-1199.
Qin Xianping, Ren Xia, Yang Yuanxet al. Real-time relative orbit determination for formation flying satellites using adaptive filtering[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(9): 1195-1199. doi: 10.13700/j.bh.1001-5965.2013.0589(in Chinese)
Citation: Qin Xianping, Ren Xia, Yang Yuanxet al. Real-time relative orbit determination for formation flying satellites using adaptive filtering[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(9): 1195-1199. doi: 10.13700/j.bh.1001-5965.2013.0589(in Chinese)
shu

Real-time relative orbit determination for formation flying satellites using adaptive filtering

doi: 10.13700/j.bh.1001-5965.2013.0589
  • 1.

    National Key Laboratory of Geo-information Engineering, Xi'an Institute of Surveying and Mapping, Xi'an 710054, China

  • 2. Institute of Navigation & Aerospace Targets Engineering, PLA Information Engineering University, Zhengzhou 450052, China

  • 3. National Key Laboratory of Geo-information Engineering, Xi'an Institute of Surveying and Mapping, Xi'an 710054, China

  • Received Date: 15 Oct 2013
  • Publish Date: 20 Sep 2014
    Abstract
  • A method of real-time relative orbit determination for formation flying satellites using adaptive filtering was proposed. Real-time relative orbit of two gravity recovery and climate experiment (GRACE) satellites was computed by using the global positioning system (GPS) data observed from December 9 to 10, 2005. The results of the real-time relative orbit determination were independently validated with the orbits of jet propulsion laboratory (JPL) which computed separately. The results of computation show that the information of relative dynamics and observation between formation flying satellites can be balanced finely by adaptive filtering through adaptive factor, and the relative orbit of formation flying satellites computed by adaptive filtering is better than that of Kalman filtering. The results of computation also show that the accuracy of relative orbit is improved for the shorter baseline of satellites based on the adaptive relative orbit determination. The accuracy of the baseline of GRACE satellites is better than 6 cm when using GPS single-frequency pseudoranges and broadcast ephemeris.

     

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