本文已被:浏览 757次 下载 561次
中文摘要: 针对四旋翼无人机吊挂负载系统飞行中的摆角抑制问题,考虑过快位置机动容易引起吊挂大幅度摆动,提出了一种基于嵌套饱和的四旋翼无人机吊挂负载控制器。首先,利用扩张状态观测器估计干扰,设计具有强抗扰能力的垂直位置控制器;其次,基于简化模型通过构建李雅普诺夫函数,设计控制摆角收敛的抑摆控制器;最后,基于一种嵌套饱和控制方法,设计了限制机动速度的水平位置控制器。与已有控制方法的仿真对比表明,该控制器不但能保证四旋翼无人机吊挂负载系统稳定飞行,还能在大幅度位置机动指令下有效减小最大摆幅。
Abstract:Aiming at the problem of swing angle suppression in the flight of a quadrotor UAV with a suspended payload system, a quadrotor UAV with a suspended payload controller based on the nested saturation is proposed considering that too fast position maneuvers will easily cause the suspension to swing greatly. First, a vertical position controller with strong anti-disturbance capability is designed by using the extended state observer to estimate the disturbance. Second, an anti-swing controller is designed to control the convergence of the swing angle by constructing the Lyapunov function based on the simplified model. Finally, a horizontal position controller is designed to limit the maneuvering speed based on a nested saturation control method. The simulation comparison with the existing control method shows that the proposed controller can not only ensure the stable flight of a quadrotor UAV with a suspended payload system but also effectively reduce the maximum swing under the large-scale position maneuver commands.
keywords: quadrotor UAV suspended payload extended state observer anti-swing control nested saturation
文章编号:20230305 中图分类号:TP273 文献标志码:A
基金项目:
引用文本:
余志凯,黄子豪,傅瑾瑜,蒋宪鑫,辛颖.基于嵌套饱和的四旋翼无人机吊挂负载控制器设计[J].飞控与探测,2023,(3):37-43.
余志凯,黄子豪,傅瑾瑜,蒋宪鑫,辛颖.基于嵌套饱和的四旋翼无人机吊挂负载控制器设计[J].飞控与探测,2023,(3):37-43.

