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

  • Guocheng Yan
  • , Honglun Wang*
  • , Yanxiang Wang
  • *Corresponding author for this work
  • Beihang University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

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.

Original languageEnglish
Title of host publicationAdvances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 7
EditorsLiang Yan, Haibin Duan, Yimin Deng
PublisherSpringer Science and Business Media Deutschland GmbH
Pages497-506
Number of pages10
ISBN (Print)9789819622238
DOIs
StatePublished - 2025
EventInternational Conference on Guidance, Navigation and Control, ICGNC 2024 - Changsha, China
Duration: 9 Aug 202411 Aug 2024

Publication series

NameLecture Notes in Electrical Engineering
Volume1343 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Guidance, Navigation and Control, ICGNC 2024
Country/TerritoryChina
CityChangsha
Period9/08/2411/08/24

Keywords

  • Active Disturbance Rejection Control
  • Aerial Recovery
  • Rotating Variant Wing
  • UAV

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