基于动态表面的电静液执行器自适应自抗扰控制

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Xudong Han, Y. Fu, Yan Wang, Mingkang Wang, Deming Zhu
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引用次数: 0

摘要

电静液作动器的参数不确定性、扰动不确定性和非匹配扰动直接影响其控制精度和稳定性,对飞机方向舵的操纵性能产生负面影响,甚至导致方向舵颤振。针对这些问题,提出了一种基于动态表面的自适应自抗扰控制(DSAADRC)。通过建立一种由跟踪误差、参数估计误差和状态估计误差组合驱动的参数自适应律来估计未知参数,利用三个低阶eso在线估计和补偿不确定干扰,并采用动态曲面法获取反演方法中的虚拟控制信号的微分值来处理非匹配干扰。在本研究中,Lyapunov稳定性分析表明,该方法首先建立了具有非线性和不确定性的EHA动力学模型,然后针对不确定性和摄动设计了基于动态曲面的自适应自抗扰控制方法,可以在时变外部扰动下实现EHA的位置跟踪精度。与鲁棒控制(RC)和自适应鲁棒控制(ARC)等控制策略相比,仿真和实验对比表明,该方法在时变外部干扰下具有更强的抗扰性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Dynamic Surface-Based Adaptive Active Disturbance Rejection Control of Electrohydrostatic Actuators
The control accuracy and stability of the electrohydrostatic actuator (EHA) are directly impacted by parameter uncertainty, disturbance uncertainty, and non-matching disturbance, which negatively impacts aircraft rudder maneuvering performance and even results in rudder chatter. A dynamic surface-based adaptive active disturbance rejection control (DSAADRC) is proposed as a solution for these issues. It does this by developing a novel parametric adaptive law driven by the combination of tracking error, parameter estimation error, and state estimation error to estimate the unknown parameters, using three low-order ESOs to estimate and compensate the uncertain disturbances online, and employing a dynamic surface method to obtain the differential values of virtual control signals in the backstepping method to deal with non-matching disturbances. In this research, a Lyapunov stability analysis demonstrates that the method can achieve the position tracking accuracy of the EHA under time-varying external disturbances after first establishing an EHA dynamics model with nonlinearity and uncertainty, followed by the design of an adaptive active disturbance rejection control method based on dynamic surfaces for the uncertainties and perturbations. In contrast to control strategies like Robust Control (RC) and Adaptive Robust Control (ARC), simulation and experiment comparison shows that the method has stronger anti-disturbance under time-varying external disturbances.
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
0.00%
发文量
9
审稿时长
4-8 weeks
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