基于NESO-LFDC的四旋翼无人机滑模姿态控制  

Sliding mode attitude control of quadrotor UAV based on NESO-LFDC

作　　者：桂洋 郑柏超[1,2] 高鹏 GUI Yang;ZHENG Bochao;GAO Peng(School of Automation,Nanjing University of Information Science and Technology,Nanjing 210044,China;Jiangsu Collaborative Innovation Center on Atmospheric Environment and Equipment Technology,Nanjing 210044,China)

机构地区：[1]南京信息工程大学自动化学院,江苏南京210044 [2]江苏省大气环境与装备技术协同创新中心,江苏南京210044

出　　处：《系统工程与电子技术》2024年第3期1075-1083,共9页Systems Engineering and Electronics

基　　金：国家自然科学基金(61973169);江苏省自然科学基金(BK20201392);江苏高校“青蓝工程”项目(R2021Q04)资助课题。

摘　　要：针对四旋翼无人机姿态控制中存在空气动力学特性复杂,易受干扰的特性,提出一种基于非线性扩张状态观测器(nonlinear extended state observer,NESO)和低频干扰补偿器(low-frequency disturbance compensator,LFDC)的非奇异快速终端滑模控制方法。该方法内环设计了NESO和LFDC结合,以获得干扰补偿值并补偿总干扰的低频分量。在外环设计了跟踪微分器和可变切换增益的非奇异快速终端滑模控制器,用于补偿虚拟干扰估计值的误差和总干扰的高频分量。仿真结果表明,该控制方法可以更好地估计总干扰的低频和高频分量,减少虚拟干扰估计值的误差对四旋翼无人机姿态控制的影响,并提升响应速度。To deal with the complex aerodynamic characteristics and easy characteristics in the attitude control of quadrotor unmanned aerial vehicle,a nonsingular fast terminal sliding mode control scheme based on nonlinear extended state observer(NESO)and low-frequency disturbance compensator(LFDC)is proposed.In this method,NESO and LFDC are combined in the inner loop to obtain the disturbance compensation value and compensate the low-frequency component of the total disturbance.A non-singular fast terminal sliding mode controller with tracking differentiator and variable switching gain is designed in the outer ring to compensate the virtual disturbance estimation error and the high frequency component of the total disturbance.Simulation results show that the proposed control scheme can better estimate the low and high frequency components of the total disturbance,reduce the impact of the error of the virtual disturbance estimation on the attitude control of the quadrotor unmanned aerial vehicle,and improve the response speed.

关 键 词：四旋翼无人机 姿态控制 非线性扩张状态观测器 跟踪微分器 低频干扰补偿器 非奇异快速终端滑模控制 

分 类 号：TP273[自动化与计算机技术—检测技术与自动化装置]