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Full Length Article | Open Access

Precision motion control for electro-hydraulic axis systems under unknown time-variant parameters and disturbances

Xiaowei YANGYaowen GEWenxiang DENGJianyong YAO( )
School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China
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Abstract

This article focuses on asymptotic precision motion control for electro-hydraulic axis systems under unknown time-variant parameters, mismatched and matched disturbances. Different from the traditional adaptive results that are applied to dispose of unknown constant parameters only, the unique feature is that an adaptive-gain nonlinear term is introduced into the control design to handle unknown time-variant parameters. Concurrently both mismatched and matched disturbances existing in electro-hydraulic axis systems can also be addressed in this way. With skillful integration of the backstepping technique and the adaptive control, a synthesized controller framework is successfully developed for electro-hydraulic axis systems, in which the coupled interaction between parameter estimation and disturbance estimation is avoided. Accordingly, this designed controller has the capacity of low-computation costs and simpler parameter tuning when compared to the other ones that integrate the adaptive control and observer/estimator-based technique to dividually handle parameter uncertainties and disturbances. Also, a nonlinear filter is designed to eliminate the “explosion of complexity” issue existing in the classical back-stepping technique. The stability analysis uncovers that all the closed-loop signals are bounded and the asymptotic tracking performance is also assured. Finally, contrastive experiment results validate the superiority of the developed method as well.

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Chinese Journal of Aeronautics
Pages 463-471

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Cite this article:
YANG X, GE Y, DENG W, et al. Precision motion control for electro-hydraulic axis systems under unknown time-variant parameters and disturbances. Chinese Journal of Aeronautics, 2024, 37(1): 463-471. https://doi.org/10.1016/j.cja.2023.06.001

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Received: 17 January 2023
Revised: 28 February 2023
Accepted: 18 April 2023
Published: 08 June 2023
© 2023 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/).