航空学报 > 1996, Vol. 17 Issue (1): 42-50

航天器相对运动估计的一种并行推广卡尔曼滤波方法

陈根社1, 文传源1, 陈新海2   

  1. 1. 北京航空航天大学三系,北京, 100083;2. 西北工业大学航天学院, 西安, 710072
  • 收稿日期:1993-11-25 修回日期:1994-08-16 出版日期:1996-02-25 发布日期:1996-02-25

A PARALLEL EXTENDED KALMAN FILTER FOR SPACECRAFT RELATIVE MOTION ESTIMATION

Chen Genshe1, Wen Chuanyuan1, Chen Xinhai2   

  1. 1. College of Astronautics, Northwestern Polytechnical University, Xi'an, 710072;2. Department of Automatic Control, Beijing University of Aeronautics andAstronautics, Beijing, 100083
  • Received:1993-11-25 Revised:1994-08-16 Online:1996-02-25 Published:1996-02-25

摘要: 从并行的观点出发,研究应用推广卡尔曼滤波估计航天器交会对接寻的期相对位置和速率问题。推导出交会推广卡尔曼滤波公式;提出了基于奇异值分解(SVD)和Faddev算法的并行平方根算法;给出了其脉动阵列(Systolic)实现结构;并对阵列所需的处理单元数目和执行一次迭代所需的时间步进行了分析,说明了其实现的优越性。为航天器相对运动估计提供了一种新的有效方法

关键词: 交会对接, 卡尔曼滤波器, 脉动阵列

Abstract: A method of estimating the relative position and rate between a passive spacecraft and a target spacecraft during the home phase of a typical rendezvous and docking mission using a parallel extended Kalman filter (EKF) is proposed. The paper discusses the formulation of EKF for the problem. The proposed parallel square-root algorithm is designed based on the updated singular value decomposition and the Faddeev algorithm. A new systolic array acrchitecture is developed for its implementation. This architecture is more numerically stable than other square-root algorithms, and has higher efficiency and uses fewer time steps for a complete iteration.

Key words: rendezvous-docking, Kalman filters, systolic array

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