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Robust tracking control for the hypersonic flight vehicle via backstepping method

  • University of Science and Technology Beijing
  • Louisiana State University

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

2 引用 (Scopus)

摘要

The problem of output tracking control is addressed for the longitudinal dynamics of a generic hypersonic flight vehicle. For the altitude subsystem and velocity subsystem, the dynamics is transformed into block-triangular form where the backstepping scheme is used. This problem is challenging due to the nonlinear uncertain complex interactions between the altitude and velocity subsystems. A new design approach of robust controller is proposed by combining standard backstepping with signal compensation method. It is shown that semiglobal robust stability and semiglobal robust practical tracking property of the closed-loop system can be ensured and the tracking error can be made as small as desired.

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
页4306-4311
页数6
ISBN(电子版)9789881563842
DOI
出版状态已出版 - 11 9月 2014
已对外发布是
活动Proceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, 中国
期限: 28 7月 2014 → 30 7月 2014

丛书

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
市Nanjing
时期28/07/14 → 30/07/14

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