Relative attitude determination for fly-around based on UKF

Yongqiang Jin*, Xiangdong Liu, Chaozhen Hou

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

1 引用 (Scopus)

摘要

To solve the problem of relative attitude determination of a deputy satellite with respect to chief satellite in fly-around, unscented Kalman filter (UKF) method of relative attitude determination is presented. The minimum representation of the attitude, modified Rodrigues parameter (MRP) is adopted as the attitude representation parameter. Combination of gyro, star tracker and laser rendezvous radar are employed as the attitude sensors. The state equation of relative attitude determination is obtained with consideration of relative attitude dynamic equation. Therefore, the UKF model is constructed. Simulations are done and the comparison with that of extended Kalman filter (EKF) shows that the UKF method has a faster convergence speed and a higher estimation precision.

源语言英语
主期刊名Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08
出版商Institute of Electrical and Electronics Engineers Inc.
6397-6401
页数5
ISBN(印刷版)9781424421145
DOI
出版状态已出版 - 2008
活动7th World Congress on Intelligent Control and Automation, WCICA'08 - Chongqing, 中国
期限: 25 6月 200827 6月 2008

出版系列

姓名Proceedings of the World Congress on Intelligent Control and Automation (WCICA)

会议

会议7th World Congress on Intelligent Control and Automation, WCICA'08
国家/地区中国
Chongqing
时期25/06/0827/06/08

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