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Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle

  • Southeast University, Nanjing
  • Henan University of Science and Technology

科研成果: 书/报告/会议事项章节会议稿件同行评审

3 引用 (Scopus)

摘要

This paper presents a robust continuous terminal sliding mode attitude tracking control approach for a near-space hypersonic vehicle(NSHV) in the presence of parameter uncertainties and external disturbances. Firstly, a novel nonsingular terminal sliding surface is developed. Then, a continuous terminal sliding mode control law is proposed, which is chattering-free. Afterward, considering the presence of parameter uncertainties and external disturbances, a high order sliding mode disturbance observer is introduced to estimate the lumped disturbance to improve the control performance. Finally, numerical simulations applied to the NSHV illustrate the effectiveness of the proposed approach.

源语言英语
主期刊名Intelligence Science and Big Data Engineering - 4th International Conference, IScIDE 2013, Revised Selected Papers
出版商Springer Verlag
691-696
页数6
ISBN(印刷版)9783642420566
DOI
出版状态已出版 - 2013
已对外发布
活动4th International Conference on Intelligence Science and Big Data Engineering, IScIDE 2013 - Beijing, 中国
期限: 31 7月 20132 8月 2013

出版系列

姓名Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)
8261 LNCS
ISSN(印刷版)0302-9743
ISSN(电子版)1611-3349

会议

会议4th International Conference on Intelligence Science and Big Data Engineering, IScIDE 2013
国家/地区中国
Beijing
时期31/07/132/08/13

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