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降阶扩展卡尔曼滤波算法在船用INS/GPS组合导航系统中的应用
引用本文:徐金华,许江宁,张晓锋,朱涛.降阶扩展卡尔曼滤波算法在船用INS/GPS组合导航系统中的应用[J].中国惯性技术学报,2007,15(3):299-306.
作者姓名:徐金华  许江宁  张晓锋  朱涛
作者单位:1. 海军工程大学,导航工程系,武汉,430033
2. 海军工程大学,船舶与动力工程学院,武汉,430033
基金项目:国家自然科学基金;海军工程大学学校科研基金
摘    要:TNNS(真航向导航系统)由MS860接收机、INS及处理数据的PC/104架构的嵌入式工控机构成。针对TNNS推导了INS(惯性导航系统)的误差模型,提出了适合于TNNS的降阶扩展卡尔曼滤波算法组合GPS和INS。系统在东海作了三次海试,软件及滤波算法平台由C/C 编制。海上试验表明,组合滤波后,INS的位置误差由100m降低到40m以下;进行最优化滤波后的航向误差σ由原来的0.105°减小为0.034°,纵横摇的误差也大幅减小。整个海试结果表明,在TNNS中组合GPS/INS采用的降阶扩展卡尔曼滤波算法,大幅提高了系统精度和可靠性。

关 键 词:组合导航系统  误差模型  降阶扩展卡尔曼滤波
文章编号:1005-6734(2007)03-0299-08
修稿时间:2007-04-302007-05-17

Application of reduced-order extended Kalman filter in marine MS860 GPS/inertial navigation system
XU Jin-hua,XU Jiang-ning,ZHANG Xiao-feng,ZHU Tao.Application of reduced-order extended Kalman filter in marine MS860 GPS/inertial navigation system[J].Journal of Chinese Inertial Technology,2007,15(3):299-306.
Authors:XU Jin-hua  XU Jiang-ning  ZHANG Xiao-feng  ZHU Tao
Institution:l. Dept. of Navigation Eng., Naval Univ. of Engineering, Wuhan 430033, China; 2. Shipping and Dynamics Academy of Eng., Naval Univ. of Engineering, Wuhan 430033, China
Abstract:TNNS (True North Navigation System) consist of MS860 GPS, INS(inertial navigation system), and a PC/104 embedded computer system for processing data. An INS error model was developed for the actual TNNS.Based on the error model, a reduced-order EKF(Extended Kalman Filter) algorithm was designed for TNNS. The system tests have been conducted three times at East China Sea. TNNS software and the reduced-order EKF algorithm are programmed by C/C++ codes, and executed under real-time mode in the embedded computer. The test results show that the INS position errors in north and east are reduced from more than 100 m to 40 m after correction, and the heading error σ is reduced from 0.105° to 0.034° after optimal filter correction. The accuracy of roll and pitch is also increased greatly by the integration of MS860 GPS/INS. The whole tests validate the effect of the algorithm, and show that the TNNS performance is significantly improved by the reduced-order EKF.
Keywords:GPS/INS  GPS  INS  integrated navigation  error model  reduced-order extended Kalman filter
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