Observer-Based Finite-Time Nonsingular Terminal Sliding Control of Quadrotor Under External and Mismatched Disturbances

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2025-02-19 DOI:10.1109/TAES.2025.3543470
Zijian Zhang;Haowen Jia;Ranhao Zhang;Cheng Yu;Yangyang Dong
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Abstract

In this article, we propose an improved nonsingular terminal sliding mode control method, to achieve finite-time trajectory tracking of a quadrotor uncrewedaerial vehicle in the presence of external and mismatched disturbances. This method is combined with finite-time disturbance observers, which are employed to estimate these two types of disturbances, and it also ensures that disturbance estimation errors can converge to zero within a finite time. To counteract the effects of external disturbances, the control law incorporates their estimation. In addition, we modify the sliding mode surface to include the estimation of mismatched disturbances, which helps to mitigate their impact. Then, we demonstrate the stability of the system using a Lyapunov function, showing that the tracking error will converge to zero within a finite time. Finally, simulation results indicate that the proposed control method can effectively suppress both types of disturbances.
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基于观测器的四旋翼有限时间非奇异终端滑动控制
在本文中,我们提出了一种改进的非奇异末端滑模控制方法,以实现存在外部和不匹配干扰的四旋翼无人飞行器的有限时间轨迹跟踪。该方法结合有限时间干扰观测器对这两类干扰进行估计,同时保证了干扰估计误差在有限时间内收敛到零。为了抵消外部干扰的影响,控制律包含了外部干扰的估计。此外,我们修改了滑模表面以包括对不匹配干扰的估计,这有助于减轻它们的影响。然后,我们利用李雅普诺夫函数证明了系统的稳定性,表明跟踪误差将在有限时间内收敛到零。仿真结果表明,所提出的控制方法能有效抑制两种干扰。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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