Trajectory Tracking Control Design for the System of a Quadrotor UAV With a Suspended Payload
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摘要
In this paper, we present a new control strategy based on partial feedback linearization for the system of a quadrotor UAV(unmanned aerial vehicle) with a suspended payload. An input-output stable based trajectory tracking control law is first proposed. To the end of stabilizing the internal system, a coupling term is then added to the input-output control law. And then the semi-global stability of the close-loop system is demonstrated by employing Lyapunov stability analysis. The simulation results show a good performance of the trajectory tracking ability of the proposed control design.
In this paper, we present a new control strategy based on partial feedback linearization for the system of a quadrotor UAV(unmanned aerial vehicle) with a suspended payload. An input-output stable based trajectory tracking control law is first proposed. To the end of stabilizing the internal system, a coupling term is then added to the input-output control law. And then the semi-global stability of the close-loop system is demonstrated by employing Lyapunov stability analysis. The simulation results show a good performance of the trajectory tracking ability of the proposed control design.
引文
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