Research on guidance algorithm based on strap-down devices

Yongshan Liu, Xin Lu

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

This paper proposes a guidance algorithm based on strap-down devices to obtain more accurate guidance information for small missile system. This paper establishes a mathematic model of inertial devices to get the navigation information of the SINS. Then the calculation results of the navigation system are used to establish the mathematical model of the inertial line-of-sight angular velocity of the strap-down seeker. So, the extraction of guidance information can be realized. In order to reduce the influence of system noise, this paper designs extended Kalman filter and unscented Kalman filter to filter the guidance information separately and compares these two filter results with the data from the track generator. The simulation results show that the guidance algorithm is effective and can obtain the guidance information to meet the requirements.

源语言英语
主期刊名Proceedings of the 30th Chinese Control and Decision Conference, CCDC 2018
出版商Institute of Electrical and Electronics Engineers Inc.
1709-1714
页数6
ISBN(电子版)9781538612439
DOI
出版状态已出版 - 6 7月 2018
活动30th Chinese Control and Decision Conference, CCDC 2018 - Shenyang, 中国
期限: 9 6月 201811 6月 2018

出版系列

姓名Proceedings of the 30th Chinese Control and Decision Conference, CCDC 2018

会议

会议30th Chinese Control and Decision Conference, CCDC 2018
国家/地区中国
Shenyang
时期9/06/1811/06/18

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