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A constant-gain satellite attitude determination method based on projection

  • Fangfang Yin
  • , Hua Song*
  • , Shaoqiang Yuan
  • *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

摘要

Since the Extended Kalman Filter (EKF) algorithm requires computing Jacobi matrix and gain matrix on-line, a constant-gain Kalman filter algorithm based on projection is applied to satellite attitude determination system in this paper. Firstly, in order to avoid the calculation of Jacobi matrix, a projection method is used to obtain the time-invariant measurement matrix. Then, the gain matrix of EKF is replaced by the constant gain matrix, which is obtained when the filter get stable. So the real-time performance and stability have been improved greatly. The simulation results show that the method not only has the advantage of saving computation time, high stability, but also ensure high accuracy of attitude determination.

源语言英语
主期刊名Proceedings - 5th International Conference on Instrumentation and Measurement, Computer, Communication, and Control, IMCCC 2015
编辑Jun-Bao Li
出版商Institute of Electrical and Electronics Engineers Inc.
504-509
页数6
ISBN(电子版)9781467377232
DOI
出版状态已出版 - 11 2月 2016
活动5th International Conference on Instrumentation and Measurement, Computer, Communication, and Control, IMCCC 2015 - Qinhuangdao, 中国
期限: 18 9月 201520 9月 2015

出版系列

姓名Proceedings - 5th International Conference on Instrumentation and Measurement, Computer, Communication, and Control, IMCCC 2015

会议

会议5th International Conference on Instrumentation and Measurement, Computer, Communication, and Control, IMCCC 2015
国家/地区中国
Qinhuangdao
时期18/09/1520/09/15

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