Compensation Algorithm of Device Error for Rate Strapdown Inertial Navigation System

摘要：

Based on the character of Strapdown Inertial Navigation System(SINS)on certain ballistic missile,using established mathematical model of inertial measuring system,the compensation method of SINS between samplings is deduced,which supply reference in the design of software compensation algorithm.The experiment result shows that,after using the software designed by the Algorithm,the error of IMU is reduced and the SINS accuracy is improved effectively.

作者: Jie Wang Hongqiang Gu

作者单位: School of Mechanical Engineering Shijiazhuang,Hebei Province,China 050003

会议类型: 国际会议

会议名称: 第一届智能网络与智能系统国际会议(ICINIS 2008)(The First International Conference on Intelligent Networks and Intelligent Systems)

会议地点: 武汉

会议语种:英文

在线出版日期: 2008-11-01（万方平台首次上网日期，不代表论文的发表时间）