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《Journal of Beijing University of Aeronautics and Astronautics》 2008-11
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Novel filter algorithm of space-borne GPS orbit determination

Wu Zhihua Ding Yangbin Shen Gongxun(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)  
When conventional EKF(extended Kalman filtering) algorithm was used in LEO(low earth orbit satellite) orbit determination by space-borne GPS(global positioning system).It is difficult to know the initial value of system noise variance.Therefore,the novel filter algorithm of orbit determination was proposed.In the new algorithm,the methods of linearization at the prior filtering estimate value was adopted during the linearization process of the nonlinear equations,and the disturbing equations were obtained,and then the disturbing equations were introduced in conventional EKF.Apply the EKF and the modified algorithm in LEO orbit determination based on space-borne GPS respectively,the results show the modified algorithm can restrain filter divergence of conventional EKF caused by the large deflection of system noise variance in a certain extent,and has better robustness to the selecting of initial value of system noise variance.
【CateGory Index】: P228.4
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【Citations】
Chinese Journal Full-text Database 2 Hits
1 SUN Hongxing 1 LI Deren 2 (1 School of Remote Sensing and Information Engineering, Wuhan University, 129 Luoyu Road, Wuhan 430079, China) (2 State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing, Wuhan University, 129 LuoyuRoad, Wuhan 430079, China);A New Linearization Method for the Kalman Filter in Nonlinear System[J];Editorial Board of Geomatics and Information Science of Wuhan University;2004-04
2 Zhang Yu Fang Jiancheng (Beijing University of Aeronautice and Astronautics, Beijing 100083);Simulation and Research on the Satellite Autonomous Celestial Navigation Based on the Perturbative Orbit[J];Chinese Space Science and Technology;2003-05
【Secondary Citations】
Chinese Journal Full-text Database 1 Hits
1 Yang Bo Fang Jiancheng Wu Xiaojie (Beijing University of Aeronautics and Astronautics,Beijing 100083);A Method of Autonomous Orbit Determination for Spacecraft Using Star Sensor[J];Chinese Space Science and Technology;2001-02
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