Improved extended disturbance observer-based integral backstepping sliding mode control for quadrotor slung-load system

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2025-05-01 Epub Date: 2025-02-10 DOI:10.1016/j.ast.2025.110042
Xinyu Chen , Yunsheng Fan , Guofeng Wang , Dongdong Mu
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Abstract

Quadrotor slung-load (QSL) systems are commonly employed in aerial transportation tasks, where precise trajectory tracking and effective load swing suppression are critical challenges. These objectives are challenged by model uncertainties and unknown environmental disturbances, such as wind, which can compromise system stability and control accuracy. This paper addresses these challenges by developing a novel control strategy for QSL systems, where the system dynamics are divided into the attitude, position, and swing angle of the slung-load. Wind disturbances, including turbulence and wind shear, are modeled to simulate realistic outdoor scenarios. The integration backstepping control method forms the basis of the controller design, the sliding mode control is added to enhance the control accuracy and robustness while reducing steady-state error. An improved extended disturbance observer (IEDO) is incorporated to estimate and compensate for unknown disturbances and model uncertainties. The stability of the proposed controller and the convergence of the disturbance observer are rigorously analyzed using Lyapunov theory. Simulation results demonstrate the effectiveness of the proposed approach, achieving significant reductions in trajectory tracking errors and slung-load swing, even under complex and varying disturbance conditions.
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基于扩展扰动观测器的改进四旋翼悬挂系统积分反步滑模控制
四旋翼悬挂载荷(QSL)系统通常用于空中运输任务,其中精确的轨迹跟踪和有效的负载摆动抑制是关键挑战。这些目标受到模型不确定性和未知环境干扰(如风)的挑战,这些干扰会损害系统的稳定性和控制精度。本文通过开发一种新的QSL系统控制策略来解决这些挑战,其中系统动力学分为悬挂载荷的姿态,位置和摆动角度。风扰动,包括湍流和风切变,模拟真实的室外情景。以积分反演控制方法作为控制器设计的基础,加入滑模控制,提高控制精度和鲁棒性,同时减小稳态误差。采用改进的扩展扰动观测器(IEDO)对未知扰动和模型不确定性进行估计和补偿。利用李雅普诺夫理论对所提控制器的稳定性和扰动观测器的收敛性进行了严格的分析。仿真结果证明了该方法的有效性,即使在复杂多变的干扰条件下,也能显著降低轨迹跟踪误差和悬挂载荷摆动。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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