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Full Length Article | Open Access

Distributed event-triggered collision avoidance coordinated control for QUAVs based on flexible virtual tubes

Hongzhen GUOaMou CHENa( )Mihai LUNGUbBaomin LIa
College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Faculty of Electrical Engineering, University of Craiova, Craiova 200008, Romania

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

In this paper, a distributed Event-Triggered (ET) collision avoidance coordinated control for Quadrotor Unmanned Aerial Vehicles (QUAVs) is proposed based on Virtual Tubes (VTs) with flexible boundaries in the presence of unknown external disturbances. Firstly, VTs are constructed for each QUAV, and the QUAV is restricted into the corresponding VT by the artificial potential field, which is distributed around the boundary of the VT. Thus, the collisions between QUAVs are avoided. Besides, the boundaries of the VTs are flexible by the modification signals, which are generated by the self-regulating auxiliary systems, to make the repulsive force smaller and give more buffer space for QUAVs without collision. Then, a novel ET mechanism is designed by introducing the concept of prediction to the traditional fixed threshold ET mechanism. Furthermore, a disturbance observer is proposed to deal with the adverse effects of the unknown external disturbance. On this basis, a distributed ET collision avoidance coordinated controller is proposed. Then, the proposed controller is quantized by the hysteresis uniform quantizer and then sent to the actuator only at the ET instants. The boundedness of the closed-loop signals is verified by the Lyapunov method. Finally, simulation and experimental results are performed to demonstrate the superiority of the proposed control method.

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Chinese Journal of Aeronautics

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Cite this article:
GUO H, CHEN M, LUNGU M, et al. Distributed event-triggered collision avoidance coordinated control for QUAVs based on flexible virtual tubes. Chinese Journal of Aeronautics, 2025, 38(2). https://doi.org/10.1016/j.cja.2024.11.010

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Received: 26 January 2024
Revised: 20 March 2024
Accepted: 09 October 2024
Published: 15 November 2024
© 2024 The Author(s). Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).