首页 | 本学科首页   官方微博 | 高级检索  
     

联合高斯回归的平方根UKF方法
引用本文:李鹏,宋申民,陈兴林,段广仁. 联合高斯回归的平方根UKF方法[J]. 系统工程与电子技术, 2010, 32(6): 1281-1285. DOI: 10.3969/j.issn.1001-506X.2010.06.036
作者姓名:李鹏  宋申民  陈兴林  段广仁
作者单位:哈尔滨工业大学航天学院, 黑龙江 哈尔滨 150001
摘    要:针对传统的滤波方法容易受系统动态模型不确定性和噪声协方差不准确的限制这一问题,提出一种将高斯过程回归融入平方根不敏卡尔曼滤波(unscented Kalam filter,UKF)算法中的滤波算法。该算法用高斯过程对训练数据进行学习,得到动态系统的回归模型及系统噪声的协方差;采用标准的平方根UKF算法,状态方程和观测方程,相应的噪声协方差由高斯过程实时自适应调整。将应用于飞行器SINS/GPS组合导航,结果表明,该方法能够自适应系统噪声,收敛速度快,导航精度高。

关 键 词:平方根不敏卡尔曼滤波  高斯过程回归  组合导航

Square root unscented Kalman filter incorporating Gaussian process regression
LI Peng,SONG Shen-min,CHEN Xing-lin,DUAN Guang-ren. Square root unscented Kalman filter incorporating Gaussian process regression[J]. System Engineering and Electronics, 2010, 32(6): 1281-1285. DOI: 10.3969/j.issn.1001-506X.2010.06.036
Authors:LI Peng  SONG Shen-min  CHEN Xing-lin  DUAN Guang-ren
Affiliation:School of Astronautics, Harbin Inst. of Technology, Harbin 150001, China
Abstract:In classical filter algorithms, the predictive capabilities are limited by the uncertainty of system model and noise covariance. To solve this problem, Gaussian process regression and the square root unscented Kalman filter (UKF) are used in conjunction to derive a new filter algorithm. This new algorithm includes two parts. First, Gaussian process regression is used to learn training data, so the regression models and noise covariance of the dynamic system are gotten. Then the standard square root UKF filter is adopted, the state equation and observation equation are replaced by their regression models respectively, relevant noise covariance is adjusted by Gaussian kernel function adaptively and real timely. Applied in SINS/GPS integrated navigation of an aerial vehicle, this new algorithm shows its strong adaptability to system noise, good convergence rate and excellent navigation accuracy.
Keywords:square root unscented Kalman filter  Gaussian process regression  integrated navigation
本文献已被 万方数据 等数据库收录!
点击此处可从《系统工程与电子技术》浏览原始摘要信息
点击此处可从《系统工程与电子技术》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