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Dynamics Modeling and Lateral Stability Control of Rotary Wing Aerial Recovery UAV

  • Guocheng Yan
  • , Honglun Wang*
  • , Yanxiang Wang
  • *此作品的通讯作者
  • 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 aerodynamic forces and moments acting on rotary wing air recovery UAV during wing rotation process represent strong nonlinearities, influencing the stability and safety of the air recovery process. In this paper, the dynamic modeling and lateral stability control of rotary wing UAV are studied. The dynamics model of the rotary wing UAV is established based on the Newton Euler method, and the additional forces and moments during wing rotation process are analyzed. Then the relationship between aerodynamic parameters and wing rotation angle is obtained through computational fluid dynamics, and dynamic response of UAV during wing rotation process are analyzed. The results show that the UAV cannot maintain a stable state during wing rotation process and lateral stability controllers based on active disturbance rejection control are designed and verified by simulation. The results of simulation show that the designed controllers can effectively solve the strong nonlinear and parameter time varying problems in the wing rotation process of rotary wing UAV, and ensure the stability of the wing rotation process of rotary wing UAV.

源语言英语
主期刊名Advances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 7
编辑Liang Yan, Haibin Duan, Yimin Deng
出版商Springer Science and Business Media Deutschland GmbH
497-506
页数10
ISBN(印刷版)9789819622238
DOI
出版状态已出版 - 2025
活动International Conference on Guidance, Navigation and Control, ICGNC 2024 - Changsha, 中国
期限: 9 8月 202411 8月 2024

出版系列

姓名Lecture Notes in Electrical Engineering
1343 LNEE
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议International Conference on Guidance, Navigation and Control, ICGNC 2024
国家/地区中国
Changsha
时期9/08/2411/08/24

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