Integral Filter Method of Orbit Determination for Geostationary Satellite Based on Spaceborne GNSS

doi:10.3780/j.issn.1000.758X.2011.01.010

Abstract

Abstract: Spaceborne global navigation satellite system (GNSS) method is used to overcome the problem of poor satellite visibility when using GPS for orbit determination of geostationary orbit (GEO) satellite. For FENGYUN geostationary satellite, the visibility of GEO satellite relative to GNSS in the future was analyzed. Since the sampling interval of navigation receiver is a little longer, an integral filter method, combined with the orbit integral and Kalman filter methods, was proposed to determine the geostationary satellite orbit. After generating the necessary data by STK software and programming by MATLAB software, a simulation test was made. The simulation results show that the performance of the proposed method is good and that accuracy of orbit determination for GEO satellite is higher.

Key words: Integral filter method, Spaceborne global navigation satellite system, Orbit determination, Geotationary orbit, Satellite orbit

LIU Li, DONG Xu-Rong, ZHENG Kun, WANG Wei. Integral Filter Method of Orbit Determination for Geostationary Satellite Based on Spaceborne GNSS[J]. Chinese Space Science and Technology, 2011, 31(1): 70-75.

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