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Control Strategy for Transition Flight of a Fixed-wing UAV
2014
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN
We propose a control system for a small fixed-wing unmanned aerial vehicle (UAV) transitioning from level flight to hovering without switching the controller gains and dynamical model. The proposed system is divided into translational and rotational control systems. Nonlinear equations of motion are linearized using a dynamic inversion method in the flight control system design. A robust rotational motion controller is employed because the attitude of the UAV is significantly affected by
doi:10.2322/tastj.12.a99
fatcat:vr7h4ebhjvevfktnmiuhumeh2q