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Profile-tracking entry guidance using adaptive global sliding mode control theory

  • Yu Hu*
  • , Zhang Ren
  • , Zhen Shen
  • , Xin Qu
  • , Peng Jiang
  • *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

Profile-tracking guidance of Reusable Launch Vehicle (RLV) is a challenging task due to dramatic aerodynamic data perturbations. A novel adaptive global sliding mode control (AGSMC) scheme is developed so that the closed-loop system shows invariance property to parameter uncertainties all the time. The approach designs a global sliding mode surface based on optimization theory and uses adaptive technology to estimate the uncertain items of the system so as to alleviate the chattering. Numerical simulations for profile-tracking under the condition of aerodynamic data perturbations are presented to demonstrate the capability and effectiveness of the proposed algorithm.

源语言英语
主期刊名2011 International Conference on Electrical and Control Engineering, ICECE 2011 - Proceedings
751-754
页数4
DOI
出版状态已出版 - 2011
活动2nd Annual Conference on Electrical and Control Engineering, ICECE 2011 - Yichang, 中国
期限: 16 9月 201118 9月 2011

出版系列

姓名2011 International Conference on Electrical and Control Engineering, ICECE 2011 - Proceedings

会议

会议2nd Annual Conference on Electrical and Control Engineering, ICECE 2011
国家/地区中国
Yichang
时期16/09/1118/09/11

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