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组合导航系统中模糊自适应卡尔曼滤波器的设计
引用本文:缑娜,王睿,郭相科,冯晓林.组合导航系统中模糊自适应卡尔曼滤波器的设计[J].空军工程大学学报,2007,8(2):36-39.
作者姓名:缑娜  王睿  郭相科  冯晓林
作者单位:空军工程大学导弹学院 陕西三原713800(缑娜,王睿,郭相科),中国试飞院 陕西阎良710089(冯晓林)
基金项目:航空基金资助项目(619010803-1)
摘    要:为了解决常规卡尔曼滤波法存在的不足,给出了用模糊推理系统与卡尔曼法相结合的方法。该方法通过监视理论残差和实际残差的协方差一致程度,应用模糊系统不断调整滤波器的增益系数,对卡尔曼滤波器进行在线自适应控制,最终实现最优估计。通过对INS/GPS组合导航系统的计算机仿真,结果表明该方法是有效、实用的。

关 键 词:模糊推理系统  自适应卡尔曼滤波  组合导航
文章编号:1009-3516(2007)02-0036-04
收稿时间:2006-05-11
修稿时间:2006-05-11

The Design of Fuzzy Adaptive Kalman Filter on Integrated Navigation System
GOU N,WANG Rui,GUO Xiang-ke,FENG Xiao-lin.The Design of Fuzzy Adaptive Kalman Filter on Integrated Navigation System[J].Journal of Air Force Engineering University(Natural Science Edition),2007,8(2):36-39.
Authors:GOU N  WANG Rui  GUO Xiang-ke  FENG Xiao-lin
Affiliation:1. The Missile Institute, Air Force Engineering University, Sanyuan 713800, Shaanxi, China; 2. Chinese Flight Test Establishment, Yan Liang 710089 Shaanxi , China
Abstract:In order to resolve the shortcomings of the traditional Kalman filtering,a new method is presented in which the fuzzy reasoning system is combined with the traditional Kalman technology.By monitoring the covariance between abstract residual and actual residual,this algorithm modifies recursively the gain coefficient of the filter so as to adaptively control the Kalman filter.Finally the optimal estimate is achieved.The computer simulation results of the INS / GPS integrated navigation system indicate that the algorithm is effective and practical.
Keywords:fuzzy reasoning system  adaptive Kalman filter  integrated navigation
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