4.6 Article

Formation flight of fixed-wing UAV swarms: A group-based hierarchical approach

Journal

CHINESE JOURNAL OF AERONAUTICS
Volume 34, Issue 2, Pages 504-515

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.cja.2020.03.006

Keywords

Control input constraints; Coordinated path following; Formation control; Leader-following control; Unmanned aerial vehicles swarms

Funding

  1. National Natural Science Foundation of China [61973309, 61801494, 61702528]
  2. Hunan Provincial Innovation Foundation for Postgraduate, China [CX2017B014]

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This paper investigates the formation control problem of fixed-wing UAV swarms through a hierarchical group-based architecture and control laws, ensuring globally asymptotic stability of the swarm system. The theoretical proofs and numerical simulations validate the effectiveness of the proposed method in handling mission processes cooperatively among different groups.
This paper investigates a formation control problem of fixed-wing Unmanned Aerial Vehicle (UAV) swarms. A group-based hierarchical architecture is established among the UAVs, which decomposes all the UAVs into several distinct and non-overlapping groups. In each group, the UAVs form hierarchies with one UAV selected as the group leader. All group leaders execute coordinated path following to cooperatively handle the mission process among different groups, and the remaining followers track their direct leaders to achieve the inner-group coordination. More specifically, for a group leader, a virtual target moving along its desired path is assigned for the UAV, and an updating law is proposed to coordinate all the group leaders? virtual targets; for a follower UAV, the distributed leader-following formation control law is proposed to make the follower?s heading angle coincide with its direct leader, while keeping the desired relative position with respect to its direct leader. The proposed control law guarantees the globally asymptotic stability of the whole closed-loop swarm system under the control input constraints of fixed-wing UAVs. Theoretical proofs and numerical simulations are provided, which corroborate the effectiveness of the proposed method. ? 2020 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).

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