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GPS/SINS组合导航系统混合校正卡尔曼滤波方法
A New Composed Kalman Filtering Method for GPS/SINS Integrated Navigation System
【摘要】 利用卡尔曼滤波器将GPS伪距与SINS进行了深组合,在分析了导航误差产生原因的基础上,提出了输出校正与反馈校正相结合的混合校正卡尔曼滤波方法。与输出校正和反馈校正方案相比,这种校正方法提高了系统导航精度。仿真结果验证了混合校正卡尔曼滤波方法的有效性。
【Abstract】 The deep integration of pseudorange with strapdown inertial navigation system is completed in this paper. On the base of analyzing the production of navigation errors, a composed revising method is proposed by the combining output revising method with the backward revising method. Compared with these two revising methods, the composed revising method improves the integration system navigation accuracy. The simulation results show the efficiency of this revising Kalman filtering mechanism.
【关键词】 组合导航;
导航精度;
混合校正;
卡尔曼滤波;
GPS/SINS;
【Key words】 integrated navigation system; navigation accuracy; composed revising; Kalman filtering; GGPS/SINS;
【Key words】 integrated navigation system; navigation accuracy; composed revising; Kalman filtering; GGPS/SINS;
【基金】 国防科技预研基金项目(00J9.2.1HK0108);航天科技创新基金项目资助
- 【文献出处】 中国惯性技术学报 ,Journal of Chinese Inertial Technology , 编辑部邮箱 ,2003年03期
- 【分类号】V249
- 【被引频次】123
- 【下载频次】1642