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Robust Model for the Design of Controller in Saucer UAV
Journal of Software
The saucer UAV (Unmanned Aerial Vehicle) features both helicopter and traditional fixed-wing airplane, is capable of hovering, takeoff and landing vertically. The configuration of the UAV in this paper which is comprised of a propeller and there pairs of control vanes enclosed in the duct is new-style aircraft. In order to research the attitude control of the saucer UAV, this paper mainly focuses on the dynamic analysis and control model design of the vehicle. The dynamics of all the componentsdoi:10.4304/jsw.5.7.753-760 fatcat:j4uoffanqrdwplevpj2z3dckpi