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Global trajectory tracking of VTOL UAV based on disturbance rejection control

机译:基于干扰抑制控制的垂直起降无人机的全局轨迹跟踪

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In order to solve the trajectory tracking problem of the vertical take-off and landing unmanned aerial vehicles, the controller is proposed to make the system input-to-state stable with the consideration of model uncertainty and external disturbance. Firstly, with consideration of the dynamics of the servo system, the nonlinear error model is established completely by the modified Rodrigues parameters. Then, the hierarchical control method is used to design the translational and rotational controllers based on the time-scale property of the system, respectively. Thereafter, the disturbance observer which guarantees both the robust stability of the inner-loop and the disturbance rejection performance is designed. At last, the global stability of the closed-loop system is analyzed based on the singular perturbation theory. The global input-to-state stability of the system is obtained based on the Lyapunov stability theory. Simulation results show the effectiveness of the proposed method in this paper.
机译:为了解决垂直起降无人机的轨迹跟踪问题,提出了一种控制器,该模型考虑了模型的不确定性和外界干扰,使系统的输入状态稳定。首先,考虑到伺服系统的动力学特性,通过修改后的Rodrigues参数完全建立了非线性误差模型。然后,使用分层控制方法分别根据系统的时标属性设计平移和旋转控制器。此后,设计了一种既能保证内环的鲁棒稳定性又能抑制干扰的性能的干扰观测器。最后,基于奇异摄动理论,分析了闭环系统的整体稳定性。基于Lyapunov稳定性理论获得了系统的全局输入到状态稳定性。仿真结果表明了该方法的有效性。

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