An anti-windup design with local sector and H2/H∞ optimization for flight environment simulation system

Flight Environment Simulation System (FESS) is an important ground test facility, which can simulate the flight environment to test the performance of the aircraft engine. Focusing on the anti-windup control of FESS in the presence of actuator (magnitude and rate) saturations, an anti-windup design...

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Published inAerospace science and technology Vol. 128; p. 107787
Main Authors Liu, Jiashuai, Wang, Xi, Liu, Xi, Pei, Xitong, Dan, Zhihong, Zhang, Song, Yang, Shubo, Zhang, Louyue
Format Journal Article
LanguageEnglish
Published Elsevier Masson SAS 01.09.2022
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ISSN1270-9638
1626-3219
DOI10.1016/j.ast.2022.107787

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Abstract Flight Environment Simulation System (FESS) is an important ground test facility, which can simulate the flight environment to test the performance of the aircraft engine. Focusing on the anti-windup control of FESS in the presence of actuator (magnitude and rate) saturations, an anti-windup design method with local sector and H2/H∞ optimization is proposed. Firstly, the saturation-type static nonlinearities are separated from the dynamic nonlinear model of the actuator, and then an anti-windup architecture with static compensator is constructed. Subsequently, the integrated H2 performance and H∞ performance are used to deal with the saturation nonlinearities to reduce the system performance degradation caused by the magnitude and rate saturations. Meanwhile, the internal stability of the closed-loop system is guaranteed via local sector condition. Finally, an optimization problem based on Linear Matrix Inequalities (LMI) is developed for anti-windup design, in which internal stability, H2 performance and H∞ performance are considered. The designed anti-windup controller is applied to FESS, and the numerical simulation results verify the effectiveness of the proposed method. Furthermore, some key issues in anti-windup design are discussed.
AbstractList Flight Environment Simulation System (FESS) is an important ground test facility, which can simulate the flight environment to test the performance of the aircraft engine. Focusing on the anti-windup control of FESS in the presence of actuator (magnitude and rate) saturations, an anti-windup design method with local sector and H2/H∞ optimization is proposed. Firstly, the saturation-type static nonlinearities are separated from the dynamic nonlinear model of the actuator, and then an anti-windup architecture with static compensator is constructed. Subsequently, the integrated H2 performance and H∞ performance are used to deal with the saturation nonlinearities to reduce the system performance degradation caused by the magnitude and rate saturations. Meanwhile, the internal stability of the closed-loop system is guaranteed via local sector condition. Finally, an optimization problem based on Linear Matrix Inequalities (LMI) is developed for anti-windup design, in which internal stability, H2 performance and H∞ performance are considered. The designed anti-windup controller is applied to FESS, and the numerical simulation results verify the effectiveness of the proposed method. Furthermore, some key issues in anti-windup design are discussed.
ArticleNumber 107787
Author Liu, Jiashuai
Liu, Xi
Dan, Zhihong
Zhang, Song
Pei, Xitong
Yang, Shubo
Zhang, Louyue
Wang, Xi
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Keywords LMI
H2/H
Flight environment simulation system
Local sector
Saturations
Anti-windup
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SubjectTerms Anti-windup
Flight environment simulation system
formula omitted
LMI
Local sector
Saturations
Title An anti-windup design with local sector and H2/H∞ optimization for flight environment simulation system
URI https://dx.doi.org/10.1016/j.ast.2022.107787
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