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Formation Control of Fixed Wing UAV with a Novel Transition Function

Disha Zhu,Jianying Yang

IFAC-PapersOnLine（2022）

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Abstract
A variable structure controller is designed to achieve the formation of fixed wing aircraft under various trajectory conditions. A novel transition function is designed to improve the control performance. The effectiveness of the control law is proved by theory and simulation.
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Key words
Fixed-wing aircraft,formation control,transition function,sliding mode control
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