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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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)
Subjects
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Actuators
Aircraft control
aircraft engine control
Aircraft engines
Aircraft propulsion
Algorithms
Antiwindup compensators
asymmetric saturation
Control design
Control systems
Design optimization
Engine control
Engines
Feedback control
Fuels
Physical tests
Saturation
switched system
Switches
Switching
switching anti-windup
Online AccessGet full text
ISSN0278-0046
1557-9948
DOI10.1109/TIE.2022.3163464

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Abstract 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.
AbstractList 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 [Formula Omitted] 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.
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.
Author Sun, Xi-Ming
Wu, Fen
Wang, Ke
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Cites_doi 10.23943/princeton/9780691153896.001.0001
10.1016/j.isatra.2020.11.030
10.1109/ChiCC.2014.6895600
10.1016/j.conengprac.2006.08.001
10.1109/CDC40024.2019.9030005
10.1109/TSMC.2020.3048735
10.1007/978-1-4612-0017-8
10.1007/978-1-4614-1171-0
10.1109/TAC.2004.841128
10.1109/TIE.2016.2516498
10.1109/TIE.2021.3095784
10.1016/j.automatica.2007.06.003
10.1080/00207179.2014.942884
10.1002/rnc.3976
10.1109/LCSYS.2020.2986997
10.2514/4.867057
10.1016/S0005-1098(01)00209-6
10.1109/TITS.2021.3052940
10.1109/TAC.2006.884942
10.1109/TNNLS.2014.2344019
10.1109/37.793443
10.1109/TII.2020.3038939
10.1109/TAC.2008.2012009
10.1109/TNNLS.2018.2860944
10.2514/1.55922
10.1016/j.automatica.2009.09.022
10.1109/9.486637
10.2514/1.G002562
10.1016/j.conengprac.2008.11.002
10.1109/TCSI.2011.2143170
10.2514/1.30591
10.1109/TSMC.2019.2895097
10.2514/1.G001802
10.1016/j.automatica.2020.108872
10.1016/j.isatra.2019.02.008
10.1007/s00034-014-9786-5
10.1016/j.ast.2019.05.061
10.1109/TAC.2008.921036
10.1080/00207179.2017.1313451
10.1109/TIE.2021.3097602
10.1016/j.fss.2019.09.001
10.1109/TSMC.2018.2866996
10.1109/TNNLS.2019.2952108
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References ref13
ref35
ref12
ref34
ref15
ref37
ref14
ref36
ref31
ref30
ref11
ref33
ref10
ref32
ref2
ref1
ref17
ref16
ref38
ref19
ref18
ref24
ref23
ref26
ref25
ref20
Zhou (ref39) 1998; 104
ref42
ref41
ref22
ref44
ref21
ref43
ref28
ref27
ref29
ref8
ref7
ref9
ref4
ref3
ref6
ref5
ref40
References_xml – ident: ref34
  doi: 10.23943/princeton/9780691153896.001.0001
– ident: ref44
  doi: 10.1016/j.isatra.2020.11.030
– ident: ref21
  doi: 10.1109/ChiCC.2014.6895600
– ident: ref24
  doi: 10.1016/j.conengprac.2006.08.001
– ident: ref20
  doi: 10.1109/CDC40024.2019.9030005
– ident: ref8
  doi: 10.1109/TSMC.2020.3048735
– ident: ref30
  doi: 10.1007/978-1-4612-0017-8
– ident: ref4
  doi: 10.1007/978-1-4614-1171-0
– ident: ref13
  doi: 10.1109/TAC.2004.841128
– ident: ref10
  doi: 10.1109/TIE.2016.2516498
– ident: ref7
  doi: 10.1109/TIE.2021.3095784
– ident: ref14
  doi: 10.1016/j.automatica.2007.06.003
– ident: ref19
  doi: 10.1080/00207179.2014.942884
– ident: ref15
  doi: 10.1002/rnc.3976
– ident: ref22
  doi: 10.1109/LCSYS.2020.2986997
– ident: ref2
  doi: 10.2514/4.867057
– ident: ref27
  doi: 10.1016/S0005-1098(01)00209-6
– volume: 104
  volume-title: Essentials of Robust Control
  year: 1998
  ident: ref39
– ident: ref42
  doi: 10.1109/TITS.2021.3052940
– ident: ref11
  doi: 10.1109/TAC.2006.884942
– ident: ref23
  doi: 10.1109/TNNLS.2014.2344019
– ident: ref37
  doi: 10.1109/37.793443
– ident: ref9
  doi: 10.1109/TII.2020.3038939
– ident: ref32
  doi: 10.1109/TAC.2008.2012009
– ident: ref33
  doi: 10.1109/TNNLS.2018.2860944
– ident: ref1
  doi: 10.2514/1.55922
– ident: ref26
  doi: 10.1016/j.automatica.2009.09.022
– ident: ref40
  doi: 10.1109/9.486637
– ident: ref5
  doi: 10.2514/1.G002562
– ident: ref12
  doi: 10.1016/j.conengprac.2008.11.002
– ident: ref29
  doi: 10.1109/TCSI.2011.2143170
– ident: ref38
  doi: 10.2514/1.30591
– ident: ref36
  doi: 10.1109/TSMC.2019.2895097
– ident: ref3
  doi: 10.2514/1.G001802
– ident: ref31
  doi: 10.1016/j.automatica.2020.108872
– ident: ref18
  doi: 10.1016/j.isatra.2019.02.008
– ident: ref16
  doi: 10.1007/s00034-014-9786-5
– ident: ref6
  doi: 10.1016/j.ast.2019.05.061
– ident: ref28
  doi: 10.1109/TAC.2008.921036
– ident: ref17
  doi: 10.1080/00207179.2017.1313451
– ident: ref25
  doi: 10.1109/TIE.2021.3097602
– ident: ref41
  doi: 10.1016/j.fss.2019.09.001
– ident: ref43
  doi: 10.1109/TSMC.2018.2866996
– ident: ref35
  doi: 10.1109/TNNLS.2019.2952108
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Actuators
Aircraft control
aircraft engine control
Aircraft engines
Aircraft propulsion
Algorithms
Antiwindup compensators
asymmetric saturation
Control design
Control systems
Design optimization
Engine control
Engines
Feedback control
Fuels
Physical tests
Saturation
switched system
Switches
Switching
switching anti-windup
Title Switching Anti-windup Control for Aircraft Engines
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