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基于视线测量和轨道预报高轨非合作目标相对导航方法
引用本文:张杨,王典军,朱志斌,高恩宇.基于视线测量和轨道预报高轨非合作目标相对导航方法[J].空间控制技术与应用,2016,42(3):21-26.
作者姓名:张杨  王典军  朱志斌  高恩宇
作者单位:中国空间技术研究院通信卫星事业部,北京;中国空间技术研究院通信卫星事业部,北京;北京控制工程研究所;中国空间技术研究院通信卫星事业部,北京
基金项目:国家自然科学基金资助项目(61203196,11502017)
摘    要:对于非合作目标,由于中远距离星上相对测量手段有限,大多情况仅能获得视线角信息.仅视线测量相对导航方法在GEO轨道条件下滤波精度低、可观测性差.提出一种基于星间视线方位测量和轨道预报信息结合的非合作目标相对导航方法.建立基于星间相对运动模型的状态方程和基于星间视线测量和轨道预报信息的观测方程,分别选取了扩展卡尔曼滤波和无迹卡尔曼滤波两种方法,仿真分析了轨道预报信息精度和滤波方法对导航精度的影响.

关 键 词:相对导航  视线测量  扩展卡尔曼滤波  无迹卡尔曼滤波

Relative Navigation Algorithm for GEO Noncooperative Satellites Based on Line of Sight Measurement and Orbit Prediction
ZHANG Yang,WANG Dianjun,ZHU Zhibin and GAO Enyu.Relative Navigation Algorithm for GEO Noncooperative Satellites Based on Line of Sight Measurement and Orbit Prediction[J].Aerospace Contrd and Application,2016,42(3):21-26.
Authors:ZHANG Yang  WANG Dianjun  ZHU Zhibin and GAO Enyu
Institution:Institute of Telecommunication Satellite, China Academy of Space Technology, Beijing 100094;Institute of Telecommunication Satellite, China Academy of Space Technology, Beijing 100094;Beijing Institute of Control Engineering, Beijing 100190;Institute of Telecommunication Satellite, China Academy of Space Technology, Beijing 100094
Abstract:For noncooperative objectives, with limited measuring method, only angle measurement information can be achieved for the mid long distance satellites. The line of sight measurement relative navigation algorithm has low precision and observability for GEO satellites. Based on the combination of line of sight inter satellite measurement and orbit forecast information of ground measurement, a method of relative navigation algorithm for GEO noncooperative satellites is presented. The system state equation based on the inter satellite relative motion model is established. The measurement equation is established based on LOS and orbit forecast information. EKF(extended Kalman filter) and UKF(unscented Kalman filter) methods are adopted. The effects of orbit forecast information measurement accuracy and filtering methods on the navigation accuracy are illuminated via the simulation and analysis.
Keywords:
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