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

自适应滤波方法研究
引用本文:张常云.自适应滤波方法研究[J].航空学报,1998,19(Z1):97-100.
作者姓名:张常云
作者单位:北京航空航天大学自动控制系, 北京, 100083
摘    要: 证明Sage-Husa的自适应卡尔曼滤波算法不能同时估计Q和R,并分析了该法导致滤波发散的原因。介绍了一种新的自适应卡尔曼滤波算法,该法当R(或Q)已知时可以准确地估计出Q(或R)。该法的独特之处在于当对Q(或R)进行修正估计时,只采用矩阵的乘运算和求逆运算,而不进行加减法运算,因此消除了滤波发散现象。数字仿真表明效果良好。

关 键 词:自适应滤波  惯性导航  组合导航  

APPROACH TO ADAPTIVE FILTERING ALGORITHM
Zhang Changyun.APPROACH TO ADAPTIVE FILTERING ALGORITHM[J].Acta Aeronautica et Astronautica Sinica,1998,19(Z1):97-100.
Authors:Zhang Changyun
Institution:Department of Automatic Control,Beijing University of Aeronautics and Astronautics, Beijing, 100083
Abstract:This paper proves that Sage Husa′s adaptive Kalman filtering algorithm cannot estimate Q and R simultaneously, and analyses the reason why Sage Husa′s algorithm may lead to filtering divergence. A new algorithm of adaptive Kalman filter is introduced which can estimate Q (or R) accurately when R (or Q)is known. The most particular feature of this algorithm is that only matrix multiplication and inversion are performed while no summation or reduction is carried out in the phase of updating and improving the estimation of Q(or R), hence resulting in no filtering divergence. Digital simulation shows that it is remarkable.
Keywords:adaptiv e filtering  inertial nav ig atio n  integ rat ed navigat ion
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