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SINS/GPS组合导航序贯滤波算法
引用本文:孙德波,杨功流,张玉堂. SINS/GPS组合导航序贯滤波算法[J]. 中国惯性技术学报, 2005, 13(1): 59-63,67
作者姓名:孙德波  杨功流  张玉堂
作者单位:1. 哈尔滨工业大学,哈尔滨,150001
2. 天津航海仪器研究所,天津,300131
3. 航天科工集团二院二部,北京,100854
基金项目:国家自然科学基金资助项目(60374024)
摘    要:针对SINS/GPS的速度、位置组合方式中,GPS接收机的位置测量误差相关的问题,提出了一种序贯形式的Kalman滤波算法。这种算法既具有计算量小的优点,又能克服由于GPS位置测量误差相关性带来的滤波性能变差的问题,实现对SINS/GPS组合系统信息的有效融合。通过仿真证明了该算法的有效性。

关 键 词:SINS GPS 组合导航 序贯滤波 计算简化 Kalman滤波
文章编号:1005-6734(2005)01-0059-05

Sequential Estimation for SINS/GPS Integrated Navigation
SUN De-bo,YANG Gong-liu,ZHANG Yu-tong. Sequential Estimation for SINS/GPS Integrated Navigation[J]. Journal of Chinese Inertial Technology, 2005, 13(1): 59-63,67
Authors:SUN De-bo  YANG Gong-liu  ZHANG Yu-tong
Affiliation:SUN De-bo1,YANG Gong-liu2,ZHANG Yu-tang3
Abstract:Based on the SINS/GPS integrated navigation, a sequential estimation method for integrated information processing is presented. The algorithm has smaller computation amount and better performance than that of Kalman filter in information processing. It can overcome the deficiency of Kalman filter whose performance in information processing will be corrupted when the position measurement noises of GPS receiver are not white noises. This algorithm can realize more effective information fusion for SINS/GPS system. Simulation shows that this algorithm is valid.
Keywords:SINS/GPS integrated navigation  sequential estimation  computation simplification  Kalman filter
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