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Study on extended Kalman filtering for attitude estimation of micro flight vehicle

  • Beijing Institute of Technology

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

In this paper an extended Kalman filter for real-time estimation of micro flight vehicle body attitude by using MEMS gyros, accelerometers, and magnetometers is presented. The algorithm uses quaternions to represent rotation, which can avoid the singularity problem caused by using Euler angles. Attitude quaternion errors and drift bias of gyros were selected to construct a state vector. The state equation is established on the base of attitude quaternion error differential equation. The measurements of Kalman filter were obtained through iteration using acceleration and magnetic field vector. The algorithm can significantly reduce calculated amount and can converge quickly to rotation attitude.

源语言英语
主期刊名Proceedings - 3rd International Conference on Measuring Technology and Mechatronics Automation, ICMTMA 2011
457-460
页数4
DOI
出版状态已出版 - 2011
活动3rd International Conference on Measuring Technology and Mechatronics Automation, ICMTMA 2011 - Shanghai, 中国
期限: 6 1月 20117 1月 2011

丛书

姓名Proceedings - 3rd International Conference on Measuring Technology and Mechatronics Automation, ICMTMA 2011
3

会议

会议3rd International Conference on Measuring Technology and Mechatronics Automation, ICMTMA 2011
国家/地区中国
Shanghai
时期6/01/117/01/11

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