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Publishing Language: Chinese

A safety-evaluation-driven UAV swarm collision avoidance decision-making based on pigeon-inspired optimization

Yalan PENG, Haibin DUAN( ), Chen WEI
National Key Laboratory of Aircraft Integrated Flight Control,School of Automation Science and Electrical Engineering,Beihang University,Beijing 100191,China
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Abstract

This research proposes an adaptive avoidance decision-making mechanism that combines safety assessment with pigeon-inspired optimization (PIO) to enhance the collision avoidance capabilities and coordination efficiency of unmanned aerial vehicle (UAV) swarms operating in complicated environments. A multidimensional safety evaluation index system is constructed by analyzing both local conflict risks and the overall coordination level of the swarm. Principal component analysis is employed to derive a comprehensive safety score, based on which a three-stage avoidance control strategy is formulated. An artificial potential field function with adaptively tuned parameters is designed according to the safety score, enabling responsive and autonomous individual-level control. Furthermore, to improve global cooperative avoidance under high-risk scenarios, the improved PIO algorithm is embedded to jointly optimize the velocity direction and avoidance parameters of swarm members. The effectiveness and resilience of the suggested strategy in dynamic contexts are validated by simulation findings, which show that it dramatically lowers the likelihood of local conflicts while preserving swarm cohesion.

CLC number: V221+.3;TB553 Document code: A Article ID: 1001-5965(2026)10-3618-09

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Journal of Beijing University of Aeronautics and Astronautics
Pages 3618-3626

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Cite this article:
PENG Y, DUAN H, WEI C. A safety-evaluation-driven UAV swarm collision avoidance decision-making based on pigeon-inspired optimization. Journal of Beijing University of Aeronautics and Astronautics, 2026, 52(10): 3618-3626. https://doi.org/10.13700/j.bh.1001-5965.2025.0444

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Received: 04 July 2025
Accepted: 05 September 2025
Published: 28 September 2025
© Journal of Beijing University of Aeronautics and Astronautics