首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于自适应滤波的脉冲星导航方法研究
引用本文:基于自适应滤波的脉冲星导航方法研究.基于自适应滤波的脉冲星导航方法研究[J].空间控制技术与应用,2015,41(6):8.
作者姓名:基于自适应滤波的脉冲星导航方法研究
摘    要:基于X射线脉冲星的自主导航技术能够为深空探测航天器提供高精度导航信息.脉冲星星表误差对导航性能存在不利影响,特别是方差不确定的星表误差,会引起较大定位误差.建立不确定项的导航模型,提出一种基于方差匹配的自适应滤波方法,通过估计不确定观测模型中的待估参数减小不确定项对观测的影响.通过数学仿真对比了自适应滤波方法和传统扩展卡尔曼滤波方法(EKF),验证了所提方法的有效性.

关 键 词:脉冲星导航  自适应卡尔曼滤波  自主导航  

Adaptive Filter of X-Ray Pulsar-Based Navigation
CHU Yong-Hui,LI Mao-Deng,HUANG Xiang-Yu,WANG Da-Yi.Adaptive Filter of X-Ray Pulsar-Based Navigation[J].Aerospace Contrd and Application,2015,41(6):8.
Authors:CHU Yong-Hui  LI Mao-Deng  HUANG Xiang-Yu  WANG Da-Yi
Abstract:High accuracy autonomous navigation information can be obtained autonomously by pulsar navigation, including the position, velocity, attitude and time. The precision of the pulsar navigation can be mainly affected by the pulsar’s position error system, especially the uncertainty variance affect. Firstly, the uncertainty model of the pulsar navigation is presented. Secondly, the adaptive filter can reduce the unacceptable effect uncertainty variance. Numerical simulation demonstrates the effectiveness of the proposed approach.
Keywords:pulsar navigation  adaptive filter  autonomous navigation  
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《空间控制技术与应用》浏览原始摘要信息
点击此处可从《空间控制技术与应用》下载免费的PDF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