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In this paper, a consensus sliding mode control method is proposed for multiple fixed-wing UAVs to achieve formation control. Relied on the kinematic model of fixed-wing UAVs, the outer loop of the formation controller is designed. Then the inner loop controller is constructed upon the aerodynamic properties of the studied UAV. Finally, a numerical simulation is conducted to assess the effectiveness of the proposed method to illustrate the capability to establish and maintain a predefined formation configuration.

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A Consensus Sliding Mode Formation Control of Multiple Fixed-Wing UAVs for Autonomous Aerial Refueling

  • 会议论文

  • 发表日期：

    2025年

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  • Tieli Niu,
  • Ban Wang,
  • Ni Li,
  • Youmin Zhang,
  • Lingxia Mu,
  • Jiangtao Huang,
  • Xin Du

摘要

In this paper, a consensus sliding mode control method is proposed for multiple fixed-wing UAVs to achieve formation control. Relied on the kinematic model of fixed-wing UAVs, the outer loop of the formation controller is designed. Then the inner loop controller is constructed upon the aerodynamic properties of the studied UAV. Finally, a numerical simulation is conducted to assess the effectiveness of the proposed method to illustrate the capability to establish and maintain a predefined formation configuration.