首页 | 本学科首页   官方微博 | 高级检索  
     

多星编队相对轨道的自主确定
引用本文:雪丹,曹喜滨,吴云华. 多星编队相对轨道的自主确定[J]. 宇航学报, 2006, 27(6): 1406-1408,1418
作者姓名:雪丹  曹喜滨  吴云华
作者单位:哈尔滨工业大学,卫星技术研究所,哈尔滨,150080
摘    要:编队飞行的相对轨道确定具有重要意义。针对编队应用中多颗环绕星相对中心星的自主定轨问题进行了研究,提出引入环绕星间相对测量信息的分布式滤波方案。设计了二级滤波器,利用环绕星间测量信息提高一级滤波得到的环绕星相对轨道的确定精度。仿真结果验证了这种导航方案的有效性。

关 键 词:编队飞行  相对轨道确定  分布式卡尔曼滤波器
文章编号:1000-1328(2006)06-1406-03
收稿时间:2005-04-11
修稿时间:2005-04-112005-08-02

Autonomous Determination of Relative Orbit for Multi-satellite Formation
XUE Dan,CAO Xi-bin,WU Yun-hua. Autonomous Determination of Relative Orbit for Multi-satellite Formation[J]. Journal of Astronautics, 2006, 27(6): 1406-1408,1418
Authors:XUE Dan  CAO Xi-bin  WU Yun-hua
Affiliation:Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150080, China
Abstract:Autonomous orbit determination for satellite formation flight is of great importance. The objective of this paper is to estimate the relative orbits for the multi-satellite formation, an approach of decentralized filter on the basis of augmenting the measurements between slave satellites is developed. The orbit states estimation was achieved through a two-level Kalman filter design, the first-level filter estimated the local states, and the precision of those estimations was enhanced in the second-level filter with the help of the measurements between slave satellites. The numerical simulation results verify the validity of this navigation approach.
Keywords:Formation flight   Relative orbit determination   Decentralized kalman filter
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号