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

一种改进的强跟踪 UKF 算法及其在 SINS 大方位失准角初始对准中的应用郭泽,缪玲娟,赵洪松
引用本文:郭泽,缪玲娟,赵洪松.一种改进的强跟踪 UKF 算法及其在 SINS 大方位失准角初始对准中的应用郭泽,缪玲娟,赵洪松[J].航空学报,2014,35(1):203-214.
作者姓名:郭泽  缪玲娟  赵洪松
作者单位:北京理工大学 自动化学院, 北京 100081
基金项目:国家自然科学基金(61153002)
摘    要: 针对现有的强跟踪无迹卡尔曼滤波(UKF)算法存在理论依据不足和滤波性能欠佳等问题,从正交性原理出发,通过严谨的推导得到强跟踪UKF成立的充分条件,在此基础上提出一种改进的强跟踪UKF算法。该算法无需求解雅可比矩阵且计算量较小,渐消因子的作用位置以及求解公式均不同于原始的强跟踪滤波器。给出了该算法的流程和渐消因子的求解方法,证明了该算法满足强跟踪滤波器的充分条件,并分析了其渐消因子的作用机理。进行了捷联惯性导航系统(SINS)大方位失准角初始对准仿真,结果验证了所提强跟踪UKF算法的正确性和有效性。

关 键 词:大方位失准角  初始对准  强跟踪  卡尔曼滤波  无迹卡尔曼滤波  渐消因子  

An Improved Strong Tracking UKF Algorithm and Its Application in SINS Initial Alignment Under Large Azimuth Misalignment Angles
GUO Ze,MIAO Lingjuan,ZHAO Hongsong.An Improved Strong Tracking UKF Algorithm and Its Application in SINS Initial Alignment Under Large Azimuth Misalignment Angles[J].Acta Aeronautica et Astronautica Sinica,2014,35(1):203-214.
Authors:GUO Ze  MIAO Lingjuan  ZHAO Hongsong
Institution:School of Automation, Beijing Institute of Technology, Beijing 100081, China
Abstract:Against the lack of theoretical basis and poor filtering performance of the existing strong tracking unscented Kalman filter (UKF) algorithms, the sufficient condition of a strong tracking UKF is rigorously derived in this paper from the orthogonality principle, based on which an improved strong tracking UKF algorithm is proposed. This new algorithm requires less computation than the existing strong tracking UKF since it does not have to calculate the Jacobian matrix, and it is different from the original strong tracking filter in both the position and solution of the fading factor. This study presents the algorithm flow and the solution to the fading factor, and proves that the improved algorithm satisfies the sufficient condition of strong tracking UKF. Furthermore, the action mechanism of the fading factor is analyzed. The results of the strapdown inertial navigation system (SINS) initial alignment simulation under large azimuth misalignment angles verify the validity and effectiveness of the improved strong tracking UKF algorithm.
Keywords:large azimuth misalignment angle  initial alignment  strong tracking  Kalman filters  unscented Kalman filter  fading factor
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