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.
A Consensus Sliding Mode Formation Control of Multiple Fixed-Wing UAVs for Autonomous Aerial Refueling
Lect. Notes Electrical Eng.
International Conference on Guidance, Navigation and Control ; 2024 ; Changsha, China August 09, 2024 - August 11, 2024
2025-03-06
11 pages
Article/Chapter (Book)
Electronic Resource
English
Autonomous Aerial Refueling for UAVs Based on GPS/MV
Trans Tech Publications | 2012
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