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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    Title :

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


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Niu, Tieli (author) / Wang, Ban (author) / Li, Ni (author) / Zhang, Youmin (author) / Mu, Lingxia (author) / Huang, Jiangtao (author) / Du, Xin (author)

    Conference:

    International Conference on Guidance, Navigation and Control ; 2024 ; Changsha, China August 09, 2024 - August 11, 2024



    Publication date :

    2025-03-06


    Size :

    11 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





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