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Formation fault-tolerant control for multiple UAVs with external disturbances.

Authors :
Ma, Ziyuan
Gong, Huajun
Wang, Xinhua
Source :
Aircraft Engineering & Aerospace Technology. 2024, Vol. 96 Issue 3, p403-416. 14p.
Publication Year :
2024

Abstract

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. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
17488842
Volume :
96
Issue :
3
Database :
Academic Search Index
Journal :
Aircraft Engineering & Aerospace Technology
Publication Type :
Academic Journal
Accession number :
176581140
Full Text :
https://doi.org/10.1108/AEAT-05-2023-0148