具有外部干扰的多架无人飞行器编队容错控制

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Ziyuan Ma, Huajun Gong, Xinhua Wang
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引用次数: 0

摘要

本文的目的是构建一种事件触发的有限时间容错编队跟踪控制器,该控制器可在执行器故障和外部扰动时实现对多个无人飞行器(UAV)的时变编队控制。设计/方法/途径首先,本研究利用无人飞行器编队成员为每个跟随者制定了编队跟踪协议,定义了无人飞行器跟随者位置的跟踪误差。随后,本研究在有限时间内设计了基于反步法框架的多层事件触发控制器。然后,考虑到执行器故障,并增加了自适应思想以实现有限时间内的容错控制,随后证明事件触发闭环系统是一个有限时间稳定系统。此外,还分析了 Zeno 行为,以防止在有限时间内出现无限触发情况。最后,在外部干扰和执行器故障条件下进行了仿真,以证明编队跟踪控制器的性能。限时自适应控制与事件触发相结合,提高了系统稳定性,增强了对干扰的鲁棒性,并提高了计算效率。此外,所设计的编队跟踪控制器能有效控制领队和跟队的时变编队完成任务,并通过添加固定时间观测器,能有效补偿外部干扰,提高编队控制精度。原创性/价值设计了一种编队跟踪控制器,能同时处理编队飞行过程中的外部干扰和内部致动器故障,所提出的方法可应用于多种编队控制场景,且不依赖于特定类型的无人机或通信网络。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Formation fault-tolerant control for multiple UAVs with external disturbances

Purpose

The purpose of this paper is to construct an event-triggered finite-time fault-tolerant formation tracking controller, which can achieve a time-varying formation control for multiple unmanned aerial vehicles (UAVs) during actuator failures and external perturbations.

Design/methodology/approach

First, this study developed the formation tracking protocol for each follower using UAV formation members, defining the tracking inaccuracy of the UAV followers’ location. Subsequently, this study designed the multilayer event-triggered controller based on the backstepping method framework within finite time. Then, considering the actuator failures, and added self-adaptive thought for fault-tolerant control within finite time, the event-triggered closed-loop system is subsequently shown to be a finite-time stable system. Furthermore, the Zeno behavior is analyzed to prevent infinite triggering instances within a finite time. Finally, simulations are conducted with external disturbances and actuator failure conditions to demonstrate formation tracking controller performance.

Findings

It achieves improved performance in the presence of external disturbances and system failures. Combining limited-time adaptive control and event triggering improves system stability, increase robustness to disturbances and calculation efficiency. In addition, the designed formation tracking controller can effectively control the time-varying formation of the leader and followers to complete the task, and by adding a fixed-time observer, it can effectively compensate for external disturbances and improve formation control accuracy.

Originality/value

A formation-following controller is designed, which can handle both external disturbances and internal actuator failures during formation flight, and the proposed method can be applied to a variety of formation control scenarios and does not rely on a specific type of UAV or communication network.

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来源期刊
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
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