Output feedback active disturbance rejection control of an electro-hydraulic servo system based on command filter

被引:0
|
作者
Bai, Yanchun [1 ]
Yao, Jianyong [1 ]
Hu, Jian [1 ]
Feng, Guangbin [1 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Mech Engn, Nanjing 210094, Peoples R China
基金
国家重点研发计划; 中国国家自然科学基金;
关键词
Active disturbance rejection control; Extended state observer; Output feedback; Disturbance observer; Command filter; ROBUST-CONTROL; POSITION TRACKING; NONLINEAR CONTROL; MOTION CONTROL; OBSERVER; PERFORMANCE; SIMULATOR;
D O I
10.1016/j.cja.2024.07.041
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The output feedback active disturbance rejection control of a valve-controlled cylinder electro-hydraulic servo system is investigated in this paper. First, a comprehensive nonlinear mathematical model that encompasses both matched and mismatched disturbances is formulated. Due to the fact that only position information can be measured, a linear Extended State Observer (ESO) is introduced to estimate unknown states and matched disturbances, while a dedicated disturbance observer is constructed to estimate mismatched disturbances. Different from the traditional observer results, the design of the disturbance observer used in this study is carried out under the constraint of output feedback. Furthermore, an output feedback nonlinear controller is proposed leveraging the aforementioned observers to achieve accurate trajectory tracking. To mitigate the inherent differential explosion problem of the traditional backstepping framework, a finite-time stable command filter is incorporated. Simultaneously, considering transient filtering errors, a set of error compensation signals are designed to counter their negative impact effectively. Theoretical analysis affirms that the proposed control strategy ensures the boundedness of all signals within the closed-loop system. Additionally, under the specific condition of only time-invariant disturbances in the system, the conclusion of asymptotic stability is established. Finally, the algorithm's efficacy is validated through comparative experiments. (c) 2024 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).
引用
收藏
页数:12
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