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Publishing Language: Chinese

Hierarchical control method for affine formation of fixed-wing UAV swarm

Ying AO1Hao CHEN1( )Huiming LI1Kun XIAO2Xiangke WANG1
College of Intelligence Science and Technology, National University of Defense Technology, Changsha 410073, China
Beijing Institute of Astronautical Systems Engineering, Beijing 100076, China
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Abstract

Affine formation control can generate and transform the overall formation by only using the configurations of a few key nodes, featuring high flexibility and good scalability. For the affine formation control problem of fixed-wing UAV swarms, an affine formation hierarchical control scheme is designed, incorporating leader cooperative path following, follower tracking, and collision avoidance. This scheme divides the swarm into a leader layer and a follower layer: multiple leaders cooperatively generate the reference configuration required for the swarm formation while following the preset path, followers only need to track the desired positions in the affine formation spanned by the leader positions. Meanwhile, collision avoidance control ensures that each UAV avoids environmental obstacles and prevents inter-UAV collisions. Compared with existing algorithms, this method achieves a higher obstacle avoidance success rate, guarantees inter-UAV safety, and enables faster convergence of follower tracking error. Furthermore, a software-in-the-loop simulation of six UAVs is completed on the XTDrone platform built based on ROS and Gazebo. In the simulation, UAVs can form the desired affine formation and fly safely without collisions throughout the process. The relevant codes have been-released as open source.

CLC number: V249 Document code: A Article ID: 1000-6893(2026)09-532494-18

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
AO Y, CHEN H, LI H, et al. Hierarchical control method for affine formation of fixed-wing UAV swarm. Acta Aeronautica et Astronautica Sinica, 2026, 47(9). https://doi.org/10.7527/S1000-6893.2025.32494

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Received: 30 June 2025
Revised: 11 August 2025
Accepted: 09 September 2025
Published: 25 September 2025
© 2026 The Journal of Acta Aeronautica et Astronautica Sinica