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Nonlinear controller design for an unmanned aerial vehicle with a slung-load
Author(s): 
Pages: 273-279
Year: Issue:  3
Journal: Control Theory & Applications

Keyword:  quadrotorunmanned aerial vehicle(UAV)anti-swing controlslung-loadenergy method;
Abstract: This article presents a novel nonlinear control strategy for a quadrotor unmanned aerial vehicle(UAV) with a slung-load.The dynamic model for a quadrotor UAV system with slung-load is firstly obtained.The load is considered as a mass point,with a rigid link connected to the centre of gravity of the quadrotor UAV.Then,a nonlinear control strategy for the considered system is designed via the energy-based methodology.The proposed control design is able to move the quadrotor UAV to its desired position while suppress the swing of the load.The Lyapunov-based stability analysis and the LaSalle Invariance Theorem are employed to prove the stability of the closed-loop system.The control performance of the proposed control strategy is compared with that of a linear-quadratic regulator(LQR) controller via numerical simulation of stabilization control and regulation control.
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