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Publishing Language: Chinese

Composite adaptive tracking control of aerospace electro-hydrostatic actuator servo system

Zhenhua DOU1, Kai GUO1( ), Xiaoming HUANG2, Jie SUN1, Zheqing ZUO3, Shoujun ZHAO3
School of Mechanical Engineering, Shandong University, Jinan 250061, China
College of Mechanical and Electrical Engineering, Shandong University of Aeronautics, Binzhou 256600, China
Beijing Institute of Precision Mechatronics and Controls, Beijing 100076, China
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Abstract

In addressing challenges such as slow parameter convergence, suboptimal tracking performance, and rigorous persistent-excitation conditions encountered in the adaptive control methods within electro-hydrostatic actuator servo system, this study explores the development of a composite learning adaptive position tracking control algorithm. Leveraging the dynamics model of the electro-hydrostatic actuator servo system, the adaptive tracking controller is formulated through a combination of backstepping control and composite learning. Notably, parameter estimation is simultaneously guided by both tracking error and prediction error, ensuring convergence of both the tracking error and parameter estimation error under interval-excitation conditions, and the consistent stability of the controller is proved by the Lyapunov theory. The simulation and experimental findings indicate that, in contrast to traditional adaptive control, the proposed method eliminates the need for a cylinder acceleration signal and demonstrating superior trajectory tracking. Following the implementation of composite learning, the system's tracking error registers a significant 50% reduction and demonstrating heightened resilience.

CLC number: V37; TP273 Document code: A

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Acta Aeronautica et Astronautica Sinica
Article number: 630160

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Cite this article:
DOU Z, GUO K, HUANG X, et al. Composite adaptive tracking control of aerospace electro-hydrostatic actuator servo system. Acta Aeronautica et Astronautica Sinica, 2024, 45(15): 630160. https://doi.org/10.7527/S1000-6893.2024.30160

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Received: 15 January 2024
Revised: 06 March 2024
Accepted: 10 April 2024
Published: 11 May 2024
© 2024 The Journal of Acta Aeronautica et Astronautica Sinica