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Reliability and safety of an electro-hydraulic position servo system (EHPSS) can be greatly reduced for potential sensor and actuator faults. This paper proposes a novel reconfiguration control (RC) scheme that combines multi-model and adaptive control to compensate for the adverse effects. Such a design includes several fixed models, one adaptive model, and one reinitialized adaptive model. Each of the models has its own independent controller that is based on a complete parametrization of the corresponding fault. A proper switching mechanism is set up to select the most appropriate controller to control the current plant. The system output can track the reference model asymptotically using the proposed method. Simulation results validate robustness and effectiveness of the proposed scheme. The main contribution is a reconfiguration control method that can handle component faults and maintain the acceptable performance of the EHPSS.
Rocznik
Tom
Strony
185--196
Opis fizyczny
Bibliogr. 39 poz., rys., tab., wykr.
Twórcy
autor
- Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, 3888 Dongnanhu Road, Erdao District, Changchun 130033, China; College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, 29 Jiangjun Ave., Jiangning District, Nanjing 211100, China
autor
- College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, 29 Jiangjun Ave., Jiangning District, Nanjing 211100, China
autor
- College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, 29 Jiangjun Ave., Jiangning District, Nanjing 211100, China
autor
- Electronic Engineering Department, Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration, 33 Shuige Road, Jiangning District, Nanjing 211100, China
autor
- Electronic Engineering Department, Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration, 33 Shuige Road, Jiangning District, Nanjing 211100, China
Bibliografia
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- [35] Yu, X. and Jiang, J. (2011). Hybrid fault-tolerant flight control system design against partial actuator failures, IEEE Transactions on Control Systems Technology 20(4): 871–886.
- [36] Yu-Ying, G. and Jiang, B. (2009). Multiple model-based adaptive reconfiguration control for actuator fault, Acta Automatica Sinica 35(11): 1452–1458.
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- [39] Zhang, Z., Yang, Z., Xiong, S., Chen, S., Liu, S. and Zhang, X. (2021). Simple adaptive control-based reconfiguration design of cabin pressure control system, Complexity 2021(3): 1–16.
Typ dokumentu
Bibliografia
Identyfikator YADDA
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