现代防御技术 ›› 2025, Vol. 53 ›› Issue (3): 112-119.DOI: 10.3969/j.issn.1009-086x.2025.03.013

• 指挥控制与通信 • 上一篇    

基于状态观测器的无人机群编队操纵控制

吴蜜1, 陈先桥2, 沈卫文1   

  1. 1.武汉交通职业学院 电子与信息工程学院,湖北 武汉 430000
    2.武汉理工大学 计算机与人工智能学院,湖北 武汉 430000
  • 收稿日期:2023-07-20 修回日期:2023-12-12 出版日期:2025-06-28 发布日期:2025-07-01
  • 作者简介:吴蜜(1981-),女,湖北武汉人。副教授,硕士,研究方向为计算机网络技术、人工智能。
  • 基金资助:
    国家自然科学基金(62001337);湖北省教育科学规划课题(2021GB171)

State Observer-Based Formation Maneuvering Control of Unmanned Aircraft Swarms

Mi WU1, Xianqiao CHEN2, Weiwen SHEN1   

  1. 1.School of Electronics and Information Engineering,Wuhan Technical College of Communications,Wuhan 430000,China
    2.School of Computer Science and Artificial Intelligence,Wuhan University of Technology,Wuhan 430000,China
  • Received:2023-07-20 Revised:2023-12-12 Online:2025-06-28 Published:2025-07-01

摘要:

针对具有领导-跟随结构的无人机群系统编队操纵控制问题,设计基于方向信息的分布式编队控制器,从而实现无人机群的平移和旋转操作。目前存在的基于方向信息的编队控制方法无法解决时变方向编队控制问题,因此设计了一种状态观测器。该观测器仅利用相邻无人机的相对方向以及领导者的位置和速度信息来估计无人机的期望位置和速度。结合估计的期望速度,设计了反演控制器来实现编队系统的操纵控制。使用Lyapunov方法证明了观测器的估计误差和控制器的稳定性。通过平移和旋转的仿真实验验证了所提控制方法的有效性。

关键词: 相对方向, 编队控制, 无人机群, 操纵控制, 反演控制

Abstract:

We address the problem of formation maneuvering control of unmanned aircraft swarm systems with leader-follower structure, and design distributed formation controllers based on bearing information, so as to realize the translation and rotation maneuver control of unmanned aircraft swarms. To overcome the limitations of existing formation control methods based on bearing information when handling time-varying bearing formation, we design a state observer. This observer estimates the desired positions and velocities of the UAVs using relative bearing information from neighboring UAVs and the position and velocity information of the leader. A backstepping controller is designed based on the desired velocities to achieve the maneuver control of the formation system. The estimation error of the observer and the stability of the controller are proven using the Lyapunov method. The effectiveness of the proposed control method is validated through simulations involving translation and rotation maneuvers.

Key words: relative bearing, formation control, UAVs, maneuver control, backstepping controls

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