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]. , 2011, 31(1): 70-75.

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References

［1］余江林, 柳东升. 利用GPS 对地球静止轨道卫星定轨的可行性[J]. 中国空间科学技术, 2000, 20(4):36-47. YU JIANGLIN, LIU DONGSHENG. The feasibility of determining the orbit of geostationary satellite using GPS[J]. Chinese Space Science and Technology, 2000, 20(4):36-47. ［2］赵齐乐, 刘经南, 葛茂荣, 等. CHAMP卫星厘米级精密定轨[J]. 武汉大学学报(信息科学版), 2006, 31(10)：879-882. ZHAO QILE, LIU JINGNAN, GE MAORONG, et al. Precision orbit determination of champ satellite with cm-level accuracy[J]. Geomatics and Information Science of Wuhan University, 2006, 31(10):879-882. ［3］BALBACH O, et al. Tracking GPS above GPS satellite altitude：first results of the GPS experiment on the HEO mission equator-S[C]．Position Location and Navigation Symposium，IEEE，Palm Springs，CA，USA，1998:243-249.  ［4］MICHAEL C M, EDWARD P D, CARPENTER J R, et al. Results from the GPS flight experiment on the high earth orbit AMSAT OSCAR-40 spacecraft[C]. ION GPS 2002 Conference, Portland, OR, 2002:1-12. ［5］CHRISTIAN MEHLEN, DENIS LAURICHESSE. Real-time GEO orbit determination using TOPSTAR 3000 GPS receiver[C]. ION GPS 2000, Salt Lake City, 2000:1985-1994. ［6］秦红磊, 梁敏敏. 基于GNSS的高轨卫星定位技术研究[J]. 空间科学学报，2008, 28(4): 316-325.QIN HONGLEI，LIANG MINMIN. Research on positioning of high earth orbital satellite using GNSS[J]. Chinese Journal of Space Science，2008，28(4):316-325. ［7］LI QIAO, SAMSUNG LIM, CHRIS RIZOS, et al. A multiple GNSSbased orbit determination algorithm for geostationary satellites[C]. IGNSS Symposium 2009,Qld, Australia,2009.  ［8］TSAI MENGLUN, HUANG YUSHENG, CHIANG KAIWEI, et al. The impact of COMPASS/Beidou-2 onfutureGNSS: a perspective from Asia[C]. ION ITM 2008, Savannah, Georgia,2008. ［9］MITTNACHT M, GOTTZEIN E, HARTRAMPF M, et al. The MosaicGNSS receiver family orbit and attitude determination in various orbits[C]. 2nd ESA Workshop on Satellite Navigation User Equipment,Technologies. NAVITEC 2004, ESTEC, Noordwijk,2004. ［10］许其凤．空间大地测量学-卫星导航与精密定位[M]．北京：解放军出版社,2001. XU QIFENG. Space geodesy satellite navigtion and precise position[M]. Beijing: PLA Publishing Company, 2001.

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