Fault diagnosis and reconfigurable control for flight control systems with actuator failures

Kemin Zhou; Phalguna K. Rachinayani; Nike Liu; Zhang Ren; Jorge Aravena

doi:10.1109/CDC.2004.1429644

Fault diagnosis and reconfigurable control for flight control systems with actuator failures

Kemin Zhou^*
, Phalguna K. Rachinayani
, Nike Liu
, Zhang Ren
, Jorge Aravena

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Louisiana State University

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

25 Scopus citations

Abstract

In this paper we develop some fault diagnosis and reconfigurable control design techniques with possibly actuator failures for a special class of dynamic systems in which the full system states are reliably measurable and available for feedback and diagnosis. This class of dynamical systems is quite common in modern flight control systems. We have developed an analytic method for the detection and isolation of the actuator faults. We then further develop a robust reconfigurable state feedback controller design technique that guarantees stability and closed-loop performance under the actuator faults. A Boeing 747 model is used to demonstrate the design techniques.

Original language	English
Title of host publication	2004 43rd IEEE Conference on Decision and Control (CDC)
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	5266-5271
Number of pages	6
ISBN (Print)	0780386825
DOIs	https://doi.org/10.1109/CDC.2004.1429644
State	Published - 2004
Event	43rd IEEE Conference on Decision and Control, CDC 2004 - Nassau, Bahamas Duration: 14 Dec 2004 → 17 Dec 2004

Publication series

Name	Proceedings of the IEEE Conference on Decision and Control
Volume	5
ISSN (Print)	0743-1546
ISSN (Electronic)	2576-2370

Conference

Conference	43rd IEEE Conference on Decision and Control, CDC 2004
Country/Territory	Bahamas
City	Nassau
Period	14/12/04 → 17/12/04

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10.1109/CDC.2004.1429644

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Zhou, K., Rachinayani, P. K., Liu, N., Ren, Z., & Aravena, J. (2004). Fault diagnosis and reconfigurable control for flight control systems with actuator failures. In 2004 43rd IEEE Conference on Decision and Control (CDC) (pp. 5266-5271). Article FrC06.6 (Proceedings of the IEEE Conference on Decision and Control; Vol. 5). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CDC.2004.1429644

@inproceedings{2ae4f8cc0cdf44948e9973a29e5c9c26,

title = "Fault diagnosis and reconfigurable control for flight control systems with actuator failures",

abstract = "In this paper we develop some fault diagnosis and reconfigurable control design techniques with possibly actuator failures for a special class of dynamic systems in which the full system states are reliably measurable and available for feedback and diagnosis. This class of dynamical systems is quite common in modern flight control systems. We have developed an analytic method for the detection and isolation of the actuator faults. We then further develop a robust reconfigurable state feedback controller design technique that guarantees stability and closed-loop performance under the actuator faults. A Boeing 747 model is used to demonstrate the design techniques.",

author = "Kemin Zhou and Rachinayani, \{Phalguna K.\} and Nike Liu and Zhang Ren and Jorge Aravena",

year = "2004",

doi = "10.1109/CDC.2004.1429644",

language = "英语",

isbn = "0780386825",

series = "Proceedings of the IEEE Conference on Decision and Control",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "5266--5271",

booktitle = "2004 43rd IEEE Conference on Decision and Control (CDC)",

address = "美国",

note = "43rd IEEE Conference on Decision and Control, CDC 2004 ; Conference date: 14-12-2004 Through 17-12-2004",

}

Zhou, K, Rachinayani, PK, Liu, N, Ren, Z & Aravena, J 2004, Fault diagnosis and reconfigurable control for flight control systems with actuator failures. in 2004 43rd IEEE Conference on Decision and Control (CDC)., FrC06.6, Proceedings of the IEEE Conference on Decision and Control, vol. 5, Institute of Electrical and Electronics Engineers Inc., pp. 5266-5271, 43rd IEEE Conference on Decision and Control, CDC 2004, Nassau, Bahamas, 14/12/04. https://doi.org/10.1109/CDC.2004.1429644

Fault diagnosis and reconfigurable control for flight control systems with actuator failures. / Zhou, Kemin; Rachinayani, Phalguna K.; Liu, Nike et al.
2004 43rd IEEE Conference on Decision and Control (CDC). Institute of Electrical and Electronics Engineers Inc., 2004. p. 5266-5271 FrC06.6 (Proceedings of the IEEE Conference on Decision and Control; Vol. 5).

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

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T1 - Fault diagnosis and reconfigurable control for flight control systems with actuator failures

AU - Zhou, Kemin

AU - Rachinayani, Phalguna K.

AU - Liu, Nike

AU - Ren, Zhang

AU - Aravena, Jorge

PY - 2004

Y1 - 2004

N2 - In this paper we develop some fault diagnosis and reconfigurable control design techniques with possibly actuator failures for a special class of dynamic systems in which the full system states are reliably measurable and available for feedback and diagnosis. This class of dynamical systems is quite common in modern flight control systems. We have developed an analytic method for the detection and isolation of the actuator faults. We then further develop a robust reconfigurable state feedback controller design technique that guarantees stability and closed-loop performance under the actuator faults. A Boeing 747 model is used to demonstrate the design techniques.

AB - In this paper we develop some fault diagnosis and reconfigurable control design techniques with possibly actuator failures for a special class of dynamic systems in which the full system states are reliably measurable and available for feedback and diagnosis. This class of dynamical systems is quite common in modern flight control systems. We have developed an analytic method for the detection and isolation of the actuator faults. We then further develop a robust reconfigurable state feedback controller design technique that guarantees stability and closed-loop performance under the actuator faults. A Boeing 747 model is used to demonstrate the design techniques.

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U2 - 10.1109/CDC.2004.1429644

DO - 10.1109/CDC.2004.1429644

M3 - 会议稿件

AN - SCOPUS:14544298406

SN - 0780386825

T3 - Proceedings of the IEEE Conference on Decision and Control

SP - 5266

EP - 5271

BT - 2004 43rd IEEE Conference on Decision and Control (CDC)

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 43rd IEEE Conference on Decision and Control, CDC 2004

Y2 - 14 December 2004 through 17 December 2004

ER -

Zhou K, Rachinayani PK, Liu N, Ren Z, Aravena J. Fault diagnosis and reconfigurable control for flight control systems with actuator failures. In 2004 43rd IEEE Conference on Decision and Control (CDC). Institute of Electrical and Electronics Engineers Inc. 2004. p. 5266-5271. FrC06.6. (Proceedings of the IEEE Conference on Decision and Control). doi: 10.1109/CDC.2004.1429644

Fault diagnosis and reconfigurable control for flight control systems with actuator failures

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