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四旋翼无人机鲁棒嵌套饱和控制

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针对四旋翼无人机在执行任务中,动力系统受到输入饱和限制,传统嵌套饱和控制算法收敛条件严格、收敛速度慢、稳态精度不高、鲁棒性不强等问题,提出了一种四旋翼无人机鲁棒嵌套饱和控制算法.首先,设计了条件相对放松的嵌套饱和控制算法,降低了设计难度,并且给出了闭环系统的稳定性证明.其次,基于条件放松的嵌套饱和控制算法,引入自耦PD和补偿函数观测器,提升系统的响应速度,稳态精度以及鲁棒性,并利用Lyapunov稳定性原理证明了闭环系统的全局稳定性.最后,将所提算法与传统嵌套饱和控制算法和PD控制算法进行了仿真对比,结果表明:本文提出的算法在暂态性能、稳态性能和鲁棒性上都是最优.
Robust nested saturation control of quadrotor UAV
A robust nested saturation control algorithm for quadrotor UAV is proposed to address the problems during mission execution,such as power system constraints from input saturation,strict convergence conditions,slow convergence speed,low steady-state accuracy,and weak robustness of traditional nested saturation control algorithms.Firstly,a nested saturation control algorithm with relatively relaxed conditions was designed,the design difficulty was reduced and the stability of closed loop system is given.Secondly,based on condition relaxed nested saturation control algorithm,self-coupling PD and compensation function observer is introduced to improve the response speed,steady-state accuracy,and robustness of the system.The global stability of the closed loop system is demonstrated using the Lyapunov stability principle.Finally,the proposed algorithm is compared with traditional nested saturation control algorithm and PD control algorithm through simulation,and the results show that the algorithm proposed in this paper is optimal in terms of transient performance,steady-state performance,and robustness.

quadrotor UAVnested saturation controlinput constraintsrobustnessglobal stabilization

刘思成、郭玉英

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西南科技大学 信息工程学院,四川 绵阳 621010

四旋翼无人机 嵌套饱和控制 输入约束 鲁棒性 全局稳定

航空发动机高空模拟技术国防科技重点实验室创新基金项目

18zd9101

2024

兵器装备工程学报
重庆市(四川省)兵工学会 重庆理工大学

兵器装备工程学报

CSTPCD北大核心
影响因子:0.478
ISSN:2096-2304
年,卷(期):2024.45(7)
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