Studies on optimized algorithm for SINS under high dynamic

Zhao Fei Zhang, Jian Jun Luo, Bai Chun Gong

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

As to improve the attitude solving accuracy of strapdown inertial navigation system (SINS) boarded on the spacecraft for high dynamic application, a novel optimized coning error compensation algorithm is developed. Based on the rotation vector concept, a general scheme of N measurement samples coning error compensation by utilizing the last P measurement samples is proposed. Then, an optimized compensation algorithm is given in fixed frequency environment. And the key coefficients of this algorithm can be acquired by a simple matrix calculus rather than a complicated derivation. Finally, the algorithm is verified and tested by physical experiment. The results show that the coning error compensation accuracy does can be improved.

源语言英语
主期刊名Information Technology and Intelligent Transportation System - Volume 1, Proceedings of the International Conference on Information Technology and Intelligent Transportation Systems, ITITS 2015
编辑Lakhmi C. Jain, Xiangmo Zhao, Valentina Emilia Balas
出版商Springer Verlag
67-75
页数9
ISBN(印刷版)9783319387871
DOI
出版状态已出版 - 2017
活动International Conference on Information Technology and Intelligent Transportation Systems, ITITS 2015 - Xi’an, 中国
期限: 12 12月 201513 12月 2015

出版系列

姓名Advances in Intelligent Systems and Computing
454
ISSN(印刷版)2194-5357

会议

会议International Conference on Information Technology and Intelligent Transportation Systems, ITITS 2015
国家/地区中国
Xi’an
时期12/12/1513/12/15

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