Attitude determination of extended Kalman filtering based on quaternion

被引：0
|
作者：
Li Jin-liang [1 ]
Liu Xiang-dong [1 ]
Zhang Yu-he [1 ]
Xiu Chun-bo [1 ]
机构：
[1] Beijing Inst Technol, Dept Automat Control, Beijing 100081, Peoples R China
来源：
PROCEEDINGS OF 2004 CHINESE CONTROL AND DECISION CONFERENCE | 2004年
关键词：
attitude quaternion; attitude determination; extended Kalman fiitering; satellite;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
An extended Kalman filtering technique for the large angular maneuvering and normal mode attitude determination of a satellite is presented by using gyro, sun sensors and infrared horizon scanners. The attitude quaternion representation is adapted to design an attitude estimator and integration linear error equations are established. The results of the simulation show that attitude determination is accurately achieved by using the attitude determination algorithm.
引用
收藏
页码：295 / 298
页数：4
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