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Fault-tolerant control for unmanned aerial vehicle with wing damaged

  • 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

The flight of unmanned aerial vehicle (UAV) is vulnerable to various disturbances and faults. In this paper, the small damage of the wing of an unmanned aerial vehicle is taken into consideration. The UAV control framework consists of force loop and torque loop, where the nonlinear disturbance observer (NDO) based dynamic inverse (DI) control and the extended state observer (ESO) based dynamic inverse control are employed respectively to control these two loops. The required force and moment are allocated to the steering gear and thrust vector of the UAV. The designed control law can not only make the UAV fly effectively in the presence of a fault, but also meet the demand of UAV for high maneuver flight. Finally, simulation results verify the effectiveness of the proposed method.

源语言英语
主期刊名Proceedings IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society
出版商Institute of Electrical and Electronics Engineers Inc.
3191-3196
页数6
ISBN(电子版)9781538611272
DOI
出版状态已出版 - 15 12月 2017
活动43rd Annual Conference of the IEEE Industrial Electronics Society, IECON 2017 - Beijing, 中国
期限: 29 10月 20171 11月 2017

出版系列

姓名Proceedings IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society
2017-January

会议

会议43rd Annual Conference of the IEEE Industrial Electronics Society, IECON 2017
国家/地区中国
Beijing
时期29/10/171/11/17

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