Event-Triggered Trajectory Tracking Control for Quadrotor UAVs Subject to External Disturbances

IF 3.2 3区 计算机科学 Q2 AUTOMATION & CONTROL SYSTEMS
Peng Zhao, Zean Bao, Xinzhi Liu, Jingyao Zhang, Kaiquan Cai
{"title":"Event-Triggered Trajectory Tracking Control for Quadrotor UAVs Subject to External Disturbances","authors":"Peng Zhao,&nbsp;Zean Bao,&nbsp;Xinzhi Liu,&nbsp;Jingyao Zhang,&nbsp;Kaiquan Cai","doi":"10.1002/rnc.7933","DOIUrl":null,"url":null,"abstract":"<div>\n \n <p>This article investigates the trajectory tracking control problem for quadrotor UAVs using the dynamic event-triggered control approach. Unlike existing results, the dynamic event-triggered control strategy proposed in this work ensures that the trajectory tracking error of quadrotor UAVs converges to zero asymptotically for a class of external disturbances. Specifically, an event-triggered mechanism is introduced in the position loop to reduce the resource transmission consumption. To address the non-differentiable nature of the event-triggered signal, a fourth-order linear system model for the position loop is derived, ensuring the existence of a twice-differentiable acceleration reference which is essential for the attitude loop. Subsequently, based on the internal model principle, we develop a class of dynamic event-triggered control strategies with dynamic triggering mechanisms. Furthermore, to handle the challenges posed by the unknown parameters and external perturbations within the attitude-loop subsystem, a robust adaptive dynamic control law is implemented based on the attitude rotation matrix. Rigorous Lyapunov analysis demonstrates that the overall control approach ensures asymptotic stability of the closed-loop system. Finally, we verify the effectiveness and robustness of the controller through numerical simulations.</p>\n </div>","PeriodicalId":50291,"journal":{"name":"International Journal of Robust and Nonlinear Control","volume":"35 11","pages":"4669-4685"},"PeriodicalIF":3.2000,"publicationDate":"2025-03-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Robust and Nonlinear Control","FirstCategoryId":"94","ListUrlMain":"https://onlinelibrary.wiley.com/doi/10.1002/rnc.7933","RegionNum":3,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"AUTOMATION & CONTROL SYSTEMS","Score":null,"Total":0}
引用次数: 0

Abstract

This article investigates the trajectory tracking control problem for quadrotor UAVs using the dynamic event-triggered control approach. Unlike existing results, the dynamic event-triggered control strategy proposed in this work ensures that the trajectory tracking error of quadrotor UAVs converges to zero asymptotically for a class of external disturbances. Specifically, an event-triggered mechanism is introduced in the position loop to reduce the resource transmission consumption. To address the non-differentiable nature of the event-triggered signal, a fourth-order linear system model for the position loop is derived, ensuring the existence of a twice-differentiable acceleration reference which is essential for the attitude loop. Subsequently, based on the internal model principle, we develop a class of dynamic event-triggered control strategies with dynamic triggering mechanisms. Furthermore, to handle the challenges posed by the unknown parameters and external perturbations within the attitude-loop subsystem, a robust adaptive dynamic control law is implemented based on the attitude rotation matrix. Rigorous Lyapunov analysis demonstrates that the overall control approach ensures asymptotic stability of the closed-loop system. Finally, we verify the effectiveness and robustness of the controller through numerical simulations.

受外界干扰的四旋翼无人机事件触发轨迹跟踪控制
本文采用动态事件触发控制方法研究了四旋翼无人机的轨迹跟踪控制问题。与已有结果不同,本文提出的动态事件触发控制策略保证了四旋翼无人机在一类外部干扰下的轨迹跟踪误差渐近收敛于零。具体来说,在位置循环中引入了事件触发机制,以减少资源传输消耗。为了解决事件触发信号的不可微特性,推导了位置环的四阶线性系统模型,保证了姿态环所必需的二阶可微加速度参考的存在。随后,基于内模原理,我们开发了一类具有动态触发机制的动态事件触发控制策略。此外,为了应对姿态环子系统内部未知参数和外部扰动的挑战,基于姿态旋转矩阵实现了鲁棒自适应动态控制律。严格的李雅普诺夫分析表明,整体控制方法保证了闭环系统的渐近稳定。最后,通过数值仿真验证了该控制器的有效性和鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
International Journal of Robust and Nonlinear Control
International Journal of Robust and Nonlinear Control 工程技术-工程:电子与电气
CiteScore
6.70
自引率
20.50%
发文量
505
审稿时长
2.7 months
期刊介绍: Papers that do not include an element of robust or nonlinear control and estimation theory will not be considered by the journal, and all papers will be expected to include significant novel content. The focus of the journal is on model based control design approaches rather than heuristic or rule based methods. Papers on neural networks will have to be of exceptional novelty to be considered for the journal.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信