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Adaptive sliding mode control for missile guidance law

  • Xiangyang Wu*
  • , Shihua Bi
  • , Zheng Zhu
  • , Weinan Wu
  • *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

The problem of missile interception is investigated in this paper. Sliding mode controllers are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.

源语言英语
主期刊名Proceedings of the 33rd Chinese Control Conference, CCC 2014
编辑Shengyuan Xu, Qianchuan Zhao
出版商IEEE Computer Society
960-965
页数6
ISBN(电子版)9789881563842
DOI
出版状态已出版 - 11 9月 2014
活动Proceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, 中国
期限: 28 7月 201430 7月 2014

出版系列

姓名Proceedings of the 33rd Chinese Control Conference, CCC 2014
ISSN(印刷版)1934-1768
ISSN(电子版)2161-2927

会议

会议Proceedings of the 33rd Chinese Control Conference, CCC 2014
国家/地区中国
Nanjing
时期28/07/1430/07/14

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