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

常增益变采样率自适应滤波
引用本文:贾沛璋,郑在齐.常增益变采样率自适应滤波[J].航空学报,1991,12(9):542-547.
作者姓名:贾沛璋  郑在齐
作者单位:中国科学院系统科学所 (贾沛璋),北京电子工程总体研究所(郑在齐)
摘    要:作者曾给出一种跟踪飞机机动的自适应滤波,采用直角坐标系中的9维状态量,利用最优检测统计量探测目标机动,并用估计到的机动加速度修正目标的预报值。 本文将在文献1]的基础上,提出两种简化自适应滤波。其一,采用两套直角坐标系中的9维卡尔曼滤波,其中的一套滤波用于取代最优检测统计量,完成对目标机动的探测和估计的功能;其二,采用三通道解偶的常增益变采样率自适应滤波。

关 键 词:机动目标  变采样率  自适应滤波  

CONSTANT GAIN ADAPTIVE FILTER WITH VARIABLE SAMPLING RATE
Institute of Systems Science,Academia Sinica Jia Peizhang Beijing Institute of Electronic System Engineering Zheng Zaiqi.CONSTANT GAIN ADAPTIVE FILTER WITH VARIABLE SAMPLING RATE[J].Acta Aeronautica et Astronautica Sinica,1991,12(9):542-547.
Authors:Institute of Systems Science  Academia Sinica Jia Peizhang Beijing Institute of Electronic System Engineering Zheng Zaiqi
Institution:1. Institute of Systems Science, Academia Sinica;2. Beijing Institute of Electronic System Engineering
Abstract:Based on the previous paper of the author the two methods of simplified adaptive filter for tracking maneuvering target are presented in this paper. One is the two mode of Kalman filter, the other is the constant gain adaptive filter with variable sampling rate which is discussed in detail. Concerning the critical problem of how to change the sampling rate an adapive algorithm equivalent to the optimal test statisics is suggested, which is more reasonable in theory and is more applicable in engineering compared with the methods of cohen and Gardner. The simulation example given in the paper shows that the two methods have the performance comparable to the method suggested by the author previously.
Keywords:maneuvering target  variable sampling rate  adaptive filter  
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》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