Initial attitude determination of aerial platform based on MIMU

Xiao Jing Du, Xiao Yang Lan, Jun Yi Zhai

科研成果: 书/报告/会议事项章节会议稿件同行评审

3 引用 (Scopus)

摘要

Aiming at the problem of initial attitude determination of aerial platform, a low computational attitude fusion algorithm is proposed based on MIMU. Attitude kinematic equations described by quaternions are developed and the filter structure used in this paper is designed. Real fly test results show that: at different initial deviation, the alignment precision of roll and pitch angles are within 1 °, attitude errors converge to 5 °or less within 12s, which meets the requirements of the aerial platform attitude fast self-determination. The filter algorithm has a small amount of calculation and is easy to be realized.

源语言英语
主期刊名Measurement Technology and its Application III
出版商Trans Tech Publications Ltd.
964-969
页数6
ISBN(印刷版)9783038351382
DOI
出版状态已出版 - 2014

出版系列

姓名Applied Mechanics and Materials
568-570
ISSN(印刷版)1660-9336
ISSN(电子版)1662-7482

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引用此

Du, X. J., Lan, X. Y., & Zhai, J. Y. (2014). Initial attitude determination of aerial platform based on MIMU. 在 Measurement Technology and its Application III (页码 964-969). (Applied Mechanics and Materials; 卷 568-570). Trans Tech Publications Ltd.. https://doi.org/10.4028/www.scientific.net/AMM.568-570.964