Adaptive fault-tolerant tracking controller design against actuator stuck faults

Xiao Ni Zhang; Jian Liang Wang; Guang Hong Yang

doi:10.1109/CCDC.2012.6244655

Adaptive fault-tolerant tracking controller design against actuator stuck faults

Xiao Ni Zhang, Jian Liang Wang, Guang Hong Yang

Research output: Chapter in Book/Conference proceeding › Conference contribution › peer-review

6 Citations (Scopus)

Abstract

This paper studies the problem of adaptive fault-tolerant tracking control for linear continuous-time systems with actuator stuck faults. A design method of an adaptive fault-tolerant tracking controller is developed based on the online estimation of the functioning of the actuators that is used to monitor the health of the system. In the event of actuator stuck faults, a compensation controller is incorporated into the initial controller to improve control effect and reject the zero-frequency disturbance produced by the stuck-actuators. Finally, the design procedure and the advantage of the proposed method are illustrated via a numerical example of flight control of an F-16 aircraft.

Original language	English
Title of host publication	Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012
Pages	4098-4103
Number of pages	6
DOIs	https://doi.org/10.1109/CCDC.2012.6244655
Publication status	Published - 2012
Externally published	Yes
Event	2012 24th Chinese Control and Decision Conference, CCDC 2012 - Taiyuan, China Duration: 23 May 2012 → 25 May 2012

Publication series

Name	Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012

Conference

Conference	2012 24th Chinese Control and Decision Conference, CCDC 2012
Country/Territory	China
City	Taiyuan
Period	23/05/12 → 25/05/12

Keywords

actuator stuck fault
Adaptive fault-tolerant control
flight tracking control

ASJC Scopus subject areas

Information Systems and Management
Control and Systems Engineering

Access to Document

10.1109/CCDC.2012.6244655

Cite this

Zhang, X. N., Wang, J. L., & Yang, G. H. (2012). Adaptive fault-tolerant tracking controller design against actuator stuck faults. In Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012 (pp. 4098-4103). Article 6244655 (Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012). https://doi.org/10.1109/CCDC.2012.6244655

@inproceedings{ff680da136354005846ba8d72f9d3cf4,

title = "Adaptive fault-tolerant tracking controller design against actuator stuck faults",

abstract = "This paper studies the problem of adaptive fault-tolerant tracking control for linear continuous-time systems with actuator stuck faults. A design method of an adaptive fault-tolerant tracking controller is developed based on the online estimation of the functioning of the actuators that is used to monitor the health of the system. In the event of actuator stuck faults, a compensation controller is incorporated into the initial controller to improve control effect and reject the zero-frequency disturbance produced by the stuck-actuators. Finally, the design procedure and the advantage of the proposed method are illustrated via a numerical example of flight control of an F-16 aircraft.",

keywords = "actuator stuck fault, Adaptive fault-tolerant control, flight tracking control",

author = "Zhang, {Xiao Ni} and Wang, {Jian Liang} and Yang, {Guang Hong}",

year = "2012",

doi = "10.1109/CCDC.2012.6244655",

language = "English",

isbn = "9781457720727",

series = "Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012",

pages = "4098--4103",

booktitle = "Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012",

note = "2012 24th Chinese Control and Decision Conference, CCDC 2012 ; Conference date: 23-05-2012 Through 25-05-2012",

}

Zhang, XN, Wang, JL & Yang, GH 2012, Adaptive fault-tolerant tracking controller design against actuator stuck faults. in Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012., 6244655, Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012, pp. 4098-4103, 2012 24th Chinese Control and Decision Conference, CCDC 2012, Taiyuan, China, 23/05/12. https://doi.org/10.1109/CCDC.2012.6244655

Adaptive fault-tolerant tracking controller design against actuator stuck faults. / Zhang, Xiao Ni; Wang, Jian Liang; Yang, Guang Hong.
Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012. 2012. p. 4098-4103 6244655 (Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012).

Research output: Chapter in Book/Conference proceeding › Conference contribution › peer-review

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AU - Zhang, Xiao Ni

AU - Wang, Jian Liang

AU - Yang, Guang Hong

PY - 2012

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N2 - This paper studies the problem of adaptive fault-tolerant tracking control for linear continuous-time systems with actuator stuck faults. A design method of an adaptive fault-tolerant tracking controller is developed based on the online estimation of the functioning of the actuators that is used to monitor the health of the system. In the event of actuator stuck faults, a compensation controller is incorporated into the initial controller to improve control effect and reject the zero-frequency disturbance produced by the stuck-actuators. Finally, the design procedure and the advantage of the proposed method are illustrated via a numerical example of flight control of an F-16 aircraft.

AB - This paper studies the problem of adaptive fault-tolerant tracking control for linear continuous-time systems with actuator stuck faults. A design method of an adaptive fault-tolerant tracking controller is developed based on the online estimation of the functioning of the actuators that is used to monitor the health of the system. In the event of actuator stuck faults, a compensation controller is incorporated into the initial controller to improve control effect and reject the zero-frequency disturbance produced by the stuck-actuators. Finally, the design procedure and the advantage of the proposed method are illustrated via a numerical example of flight control of an F-16 aircraft.

KW - actuator stuck fault

KW - Adaptive fault-tolerant control

KW - flight tracking control

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U2 - 10.1109/CCDC.2012.6244655

DO - 10.1109/CCDC.2012.6244655

M3 - Conference contribution

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SN - 9781457720727

T3 - Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012

SP - 4098

EP - 4103

BT - Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012

T2 - 2012 24th Chinese Control and Decision Conference, CCDC 2012

Y2 - 23 May 2012 through 25 May 2012

ER -

Adaptive fault-tolerant tracking controller design against actuator stuck faults

Abstract

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Conference

Keywords

ASJC Scopus subject areas

Access to Document

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