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A new angular acceleration guidance law with estimation approach based on sliding mode observer against high maneuvering target

  • Yuanyun Song*
  • , Wanchun Chen
  • , Xingliang Yin
  • *此作品的通讯作者
  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

A new type of guidance law is developed for intercepting high maneuvering target. The law takes angular acceleration of line-of-sight as a primary input in place of the acceleration of target. As the significant required input quantity of the angular acceleration guidance (AAG), the angular acceleration of line-of-sight is estimated by a developed estimation approach based on sliding mode observer (SMO). Simulation results demonstrates advantages of this AAG guidance with the estimation approach based on SMO by comparing with the conventional guidance techniques and extended Kalman filter.

源语言英语
主期刊名Mechanical and Aerospace Engineering
5249-5256
页数8
DOI
出版状态已出版 - 2012
活动2nd International Conference on Mechanical and Aerospace Engineering, ICMAE 2011 - Bangkok, 泰国
期限: 29 7月 201131 7月 2011

出版系列

姓名Applied Mechanics and Materials
110-116
ISSN(印刷版)1660-9336
ISSN(电子版)1662-7482

会议

会议2nd International Conference on Mechanical and Aerospace Engineering, ICMAE 2011
国家/地区泰国
Bangkok
时期29/07/1131/07/11

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