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Author/Affiliation: Kenji UchiyamaOpen AccessArticle
7 Pages, 1,204 KB 
Controller Design Using Backstepping Algorithm for Fixed-Wing UAV with Thrust Vectoring System
Abstract:
This paper describes the design method of a nonlinear flight controller for a fixed-wing UAV with a thrust vectoring system (TVS) using the backstepping method. The flight dynamics of the UAV exhibits strong nonlinear coupling behavior between its translational and rotational motion. The backstepping algorithm has been successfully applied to controller design for such a…
Read More(This article belongs to the SP8 (Special Issue on Multidisciplinary Sciences and Engineering 2019-20) & Section Aerospace Engineering (EAR))