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基于GPS及其与磁强计组合的姿态确定算法研究
引用本文:王建琦,曹喜滨,孙兆伟.基于GPS及其与磁强计组合的姿态确定算法研究[J].上海航天,2002,19(6):24-28.
作者姓名:王建琦  曹喜滨  孙兆伟
作者单位:哈尔滨工业大学,航天工程与力学系,黑龙江,哈尔滨,150001
摘    要:提出了一种组合敏感器定姿算法,针对卫星上同时装备有磁强计与全球卫星定位系统(GPS)的情况,利用两者的测量信息,在卡尔曼滤波算法的基础上,对两者信息融合定姿算法进行了设计和仿真,旨在提高卫星自主定姿精度和可靠性,结果表明,组合定姿算法使姿态确定的精度得到提高。

关 键 词:姿态确定  磁强计  全球卫星定位系统  卡尔曼滤波  飞行器
文章编号:1006-1630(2002)06-0024-05
修稿时间:2002年3月5日

The Research on Attitude Determination Algorithm Based on GPS and Integrated with Magnetometer
WANG Jian qi,CAO Xi bin,SUN Zhao wei.The Research on Attitude Determination Algorithm Based on GPS and Integrated with Magnetometer[J].Aerospace Shanghai,2002,19(6):24-28.
Authors:WANG Jian qi  CAO Xi bin  SUN Zhao wei
Abstract:A method of attitude determination using combined sensors is presented for satellite equipped magnetometer and globe positioning system (GPS) in this paper. Algorithms are designed and simulated for attitude determination using measuring information of both equipment based on Kalman filtering algorithm. The destination of the algorithm combined by both information is to improve the accuracy and reliability of autonomous attitude determination. The result shows that the precision of attitude determination of the system is improved.
Keywords:Attitude determination  Magnetometer  Globe positioning system  Kalman filtering
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