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伴飞卫星自主相对导航衰减记忆滤波算法
引用本文:朱庆华,李英波.伴飞卫星自主相对导航衰减记忆滤波算法[J].上海航天,2006,23(5):20-23,41.
作者姓名:朱庆华  李英波
作者单位:上海航天控制工程研究所,上海,200233
摘    要:为实现伴飞卫星的自主相对导航,基于C-W方程提出了一种在伴飞卫星轨道系中建立简化的相对运动方程构成星上轨道递推、根据导航敏感器输出进行量测更新的导航滤波器,并利用衰减记忆滤波算法抑制系统模型误差对相对导航结果的影响。仿真结果表明,该滤波算法可实现伴飞星的自主相对导航。它不仅较C-W方程更简单,而且适于模型不准确时的相对导航,工程实现易。

关 键 词:自主相对导航  相对运动方程  伴飞卫星轨道系  滤波器  衰减记忆滤波
文章编号:1006-1630(2006)05-0020-04
收稿时间:2005-08-10
修稿时间:2005-08-102005-09-13

The Declining Memory Filtering Algorithm for Autonomous Relative Navigation of Tributary Satellite
ZHU Qing-hua,LI Ying-bo.The Declining Memory Filtering Algorithm for Autonomous Relative Navigation of Tributary Satellite[J].Aerospace Shanghai,2006,23(5):20-23,41.
Authors:ZHU Qing-hua  LI Ying-bo
Institution:Shanghai Aerospace .Control Engineering Institute, Shanghai 200233, China
Abstract:To implement the autonomous relative navigation of a tributary satellite,a navigation filter was put forward in this paper,which update was processed based on the output of relative navigation sensor when the onboard orbit propagation was realized by simplified relative motion equation in the tributary satellite coordinate system according to Clohessy-Wiltshire method.The declining memory filtering algorithm was applied to suppress the effect of system model error on the relative navigation.The simulation results showed that the autonomous relative navigation of the tributary satellite would be implemented by this algorithm.It was simpler than C-W method and more suitable to the relative navigation when the system model had error,which was easy to realize in engineering.
Keywords:Autonomous relative navigation  Relative motion equation  Tributary satellite coordinate system  Filter  Forgetting factor filter
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