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Attitude control of small coaxial twin-rotor aircraft

  • Beijing Institute of Technology
  • Hong Kong Polytechnic University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

In this paper, the flight control of a small coaxial twin-rotor aircraft is studied, mainly for the hover control and trajectory tracking of the aircraft. In this paper, the PID algorithm is used to establish the mapping relationship between attitude angle and position, and the robust back-stepping control algorithm is selected to control the attitude of the aircraft to make it hover at the specified position. The simulation is verified in Matlab-Smulink, the stability error is less than 0.05m, and the trajectory tracking ability and anti-interference ability are verified. The results show that it has good hovering stability, anti-interference performance and certain maneuverability. The results show that it has good hovering stability, anti-interference performance and certain maneuverability.

源语言英语
主期刊名Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019
出版商Institute of Electrical and Electronics Engineers Inc.
558-562
页数5
ISBN(电子版)9781728137926
DOI
出版状态已出版 - 10月 2019
活动2019 IEEE International Conference on Unmanned Systems, ICUS 2019 - Beijing, 中国
期限: 17 10月 201919 10月 2019

丛书

姓名Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019

会议

会议2019 IEEE International Conference on Unmanned Systems, ICUS 2019
国家/地区中国
Beijing
时期17/10/1919/10/19

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