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This article presents an approach and a systematic design methodology to path following control based on motion decoupling for high-performance ducted fan unmanned aerial vehicles (UAVs). The decoupling is performed according to the principle of regarding the attitude motion as a virtual input of the lateral longitudinal flight dynamics. This allows the attitude and flight controllers to be designed...
In this paper, a new actuator system of the ducted-fan Uninhabited Aerial Vehicle(DFUAV) is presented. The actuator system consists of four rotary cylinders which are symmetrically installed at bottom of inside duct. The force used for attitude stabilization is generated by the interaction between the surface of rotary cylinder and the downwash, which is known as Magnus effect. In this paper, the...
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