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

一种非线性滤波器的误差分析及应用
引用本文:杨静,冀红霞,魏明坤.一种非线性滤波器的误差分析及应用[J].航空学报,2011,32(8):1469-1477.
作者姓名:杨静  冀红霞  魏明坤
作者单位:北京航空航天大学自动化科学与电气工程学院,北京,100191
基金项目:国家自然科学基金(60704006)~~
摘    要:针对一类具有未建模误差和扰动的非线性系统的状态估计问题,提出一种在线估计并补偿模型误差的非线性滤波算法,该算法利用非线性预测滤波(NPF)基于预测输出残差的方差最小的基本原则估计模型误差,冉利用扩展卡尔曼滤波(EKF)的思想对补偿后的模型进行状态估计;详细推导了状态估计误差及其方差阵的传播模型.以卫星姿态确定系统为例,...

关 键 词:非线性滤波  状态估计  误差补偿  误差分析  姿态控制
收稿时间:2010-10-09;

Error Analysis and Application of a Nonlinear Filter
YANG Jing,JI Hongxia,WEI Mingkun.Error Analysis and Application of a Nonlinear Filter[J].Acta Aeronautica et Astronautica Sinica,2011,32(8):1469-1477.
Authors:YANG Jing  JI Hongxia  WEI Mingkun
Institution:School of Automation Science and Electrical Engineering,Beihang University,Beijing 100191,China
Abstract:A nonlinear filtering algorithm with online model error estimation and compensation is proposed for a nonlinear system with uncertain model errors and disturbances. The model error is estimated by minimizing the variance of the predictive output residual based on the nonlinear predictive filter (NPF) principle, and then the system state is estimated by the extended Kalman filter (EKF) principle based on the compensated model. Detailed propagation formula of the state estimation error and its variance matrix are derived. Simulation results show the effectiveness of the proposed algorithm on a satellite attitude determination system with uncertain model errors. The simulation shows the robustness of the proposed algorithm for both the initial state error and uncertain model error, and the increasing filtering period may decrease the estimation accuracy. Compared with EKF and NPF, the proposed nonlinear filtering algorithm has the advantage of both improved estimation accuracy and faster convergence.
Keywords:nonlinear filtering  state estimation  error compensation  error analysis  attitude control
本文献已被 CNKI 万方数据 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