Adaptive reset control for group-bipartite formation of multi-UAVs subject to transmission delays

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2025-05-01 Epub Date: 2025-02-15 DOI:10.1016/j.ast.2025.110068
Zhen Tang , Xinhua Wang , Ziyang Zhen , Zhengen Zhao , Teng Cao , Geert Deconinck
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Abstract

Existing multi-UAV formation control methods face challenges in achieving stable and fast tracking under transmission delays and inaccessible information, particularly when addressing the design of various formation configurations and optimizing transient performance. To address these challenges, this paper proposes an adaptive reset control technique that integrates virtual leaders and state observers to achieve fast and accurate time-varying group-bipartite formation tracking in multi-UAV systems. Firstly, a state observer is designed to accurately estimate the position and velocity of each UAV. Then, a distributed adaptive group-bipartite time-varying formation tracking controller with a reset component is introduced. This controller enables each UAV to adjust its position and velocity according to neighboring UAVs, thus achieving the desired group-bipartite formation. The inclusion of reset component significantly enhances the transient performance of formation. Moreover, the sufficient conditions were derived for group-bipartite formation control by employing a novel Lyapunov-Krasovskii functional, which constructed with the matrix-valued polynomial, the Bessel-Legendre inequality, and the reciprocally convex matrix inequality. Finally, the effectiveness and advantages of the proposed control strategy are demonstrated through comprehensive simulations involving multiple fixed-wing UAVs.
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考虑传输延迟的多无人机群-二编队自适应复位控制
现有的多无人机编队控制方法面临着在传输延迟和信息不可访问情况下实现稳定和快速跟踪的挑战,特别是在处理各种编队配置的设计和优化瞬态性能时。为了解决这些问题,本文提出了一种集成虚拟领导者和状态观测器的自适应复位控制技术,以实现多无人机系统中快速准确的时变群-二部队形跟踪。首先,设计状态观测器来准确估计每架无人机的位置和速度;然后,提出了一种带有复位元件的分布式自适应群二部时变编队跟踪控制器。该控制器使每架无人机能够根据相邻无人机调整自己的位置和速度,从而实现理想的群-二部编队。复位元件的加入显著提高了地层的瞬态性能。利用由矩阵值多项式、Bessel-Legendre不等式和互凸矩阵不等式构造的Lyapunov-Krasovskii泛函,得到了群-二部形成控制的充分条件。最后,通过多架固定翼无人机的综合仿真,验证了所提控制策略的有效性和优越性。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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