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Attitude tracking control of a 3-DOF helicopter with input and output constraints

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

A novel attitude tracking controller is proposed for the 3-DOF helicopter under input and output constraints. A barrier Lyapunov function is employed to address input constraint, and an auxiliary design system for output constraint. Combining the backstepping technique, a nonlinear disturbance observer is explored to tackle the unknown nonlinear functions. We proved that the presented method can control the system output errors converge to a neighbourhood of zero for any sufficient smooth and bounded time-varying trajectory, and simultaneously the input and output states remains in the prescribed set uniformly. Simulation results demonstrate the effectiveness of the proposed controller for the 3-DOF helicopter.

源语言英语
主期刊名Proceedings of the 35th Chinese Control Conference, CCC 2016
编辑Jie Chen, Qianchuan Zhao, Jie Chen
出版商IEEE Computer Society
10608-10612
页数5
ISBN(电子版)9789881563910
DOI
出版状态已出版 - 26 8月 2016
活动35th Chinese Control Conference, CCC 2016 - Chengdu, 中国
期限: 27 7月 201629 7月 2016

出版系列

姓名Chinese Control Conference, CCC
2016-August
ISSN(印刷版)1934-1768
ISSN(电子版)2161-2927

会议

会议35th Chinese Control Conference, CCC 2016
国家/地区中国
Chengdu
时期27/07/1629/07/16

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