Switching Anti-windup Control for Aircraft Engines

In this article, we propose a switching anti-windup scheme for the aircraft engine control. The linear engine model with asymmetric saturation is first transformed into a switched system, each subsystem of which is subject to symmetric saturation. A state-dependent switching logic is presented to or...

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Bibliographic Details
Published inIEEE transactions on industrial electronics (1982) Vol. 70; no. 2; pp. 1830 - 1840
Main Authors Wang, Ke, Wu, Fen, Sun, Xi-Ming
Format Journal Article
LanguageEnglish
Published New York IEEE 01.02.2023
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
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ISSN0278-0046
1557-9948
DOI10.1109/TIE.2022.3163464

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Summary:In this article, we propose a switching anti-windup scheme for the aircraft engine control. The linear engine model with asymmetric saturation is first transformed into a switched system, each subsystem of which is subject to symmetric saturation. A state-dependent switching logic is presented to orchestrate the switching among multiple anti-windup compensators. We then establish the sufficient condition to guarantee the regional stability and <inline-formula><tex-math notation="LaTeX">\mathcal {L}_{2}</tex-math></inline-formula> performance of the resulting closed-loop system. This condition is less conservative since the non-symmetric nature of the saturation nonlinearity can be fully exploited in the control design. Optimization algorithms are further developed for the anti-windup gain design. The theoretical aspect of the proposed method is analyzed rigorously, and the effectiveness is validated through experiments performed on a semi-physical test bed.
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ISSN:0278-0046
1557-9948
DOI:10.1109/TIE.2022.3163464