首页 | 本学科首页   官方微博 | 高级检索  
     

卫星编队对空间非合作目标测距相对导航精度分析
引用本文:苏建敏,董云峰. 卫星编队对空间非合作目标测距相对导航精度分析[J]. 中国空间科学技术, 2011, 31(5): 48-56. DOI: 10.3780/j.issn.1000-758X.2011.05.007
作者姓名:苏建敏  董云峰
作者单位:(北京航空航天大学宇航学院,北京 100191)
摘    要:
针对单颗卫星对空间非合作目标测距不能估计全部相对运动状态的问题,提出利用编队中多颗卫星同时测距相对导航。建立了相对运动状态估计的系统模型;推导了系统可观测矩阵;通过计算系统可观测度和采用无迹卡尔曼滤波(UKF)对目标相对运动状态进行估计,研究了观测矢量方向和数量与相对导航精度的关系。结果表明双星测距能估计全部相对运动状态,观测矢量夹角越大,相对导航精度越高,在编队尺寸远小于目标距离的前提下,多于两颗的卫星测距并不能明显提高相对导航精度。

关 键 词:相对导航  测距  空间非合作目标  无迹卡尔曼滤波  编队飞行  卫星  
收稿时间:2010-11-25

Relative Guidance Accuracy Analysis for Non-cooperative Space Target by Range-only Measurement of Satellite Formation
Su Jianmin,Dong Yunfeng. Relative Guidance Accuracy Analysis for Non-cooperative Space Target by Range-only Measurement of Satellite Formation[J]. Chinese Space Science and Technology, 2011, 31(5): 48-56. DOI: 10.3780/j.issn.1000-758X.2011.05.007
Authors:Su Jianmin  Dong Yunfeng
Affiliation:(School of Astronautics, Beihang University, Beijing 100191)
Abstract:
Relative motion states of non-cooperative space target cannot be fully estimated by single satellite range-only measurement.To solve this problem,formation satellites range-only measurement was proposed.System model and measurement model were established.System observability matrix was derived,and the degree of observability was calculated.Relative motion states of non-cooperative space target were estimated through unscented Kalman filter(UKF).Analyses and simulations show that all relative motion states o...
Keywords:Relative guidance Range-only measurement Non-cooperative space targetUnscented Kalman filter Formation flight Satellite  
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《中国空间科学技术》浏览原始摘要信息
点击此处可从《中国空间科学技术》下载全文
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