Estimation of actuator fault parameters in a nonlinear boeing 747 model using a linear two-stage Kalman filter

Fikret Caliskan; Youmin Zhang; N. Eva Wu; J. Y. Shin

doi:10.3182/20090630-4-es-2003.00229

Estimation of actuator fault parameters in a nonlinear boeing 747 model using a linear two-stage Kalman filter

Fikret Caliskan^*, Youmin Zhang, N. Eva Wu, J. Y. Shin

^*Corresponding author for this work

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

2 Citations (Scopus)

Abstract

In this paper, an adaptive two-stage linear Kalman filtering algorithm (Wu, Zhang, and Zhou, 2000) is used to estimate the loss of control effectiveness and the magnitude of low degree of stuck faults in a closed-loop nonlinear B747 aircraft. Control effectiveness factors and stuck magnitudes are used to quantify faults entering control systems through actuators. Pseudo random excitation inputs are used to help distinguish partial loss and stuck faults. The partial loss and stuck faults in the stabilizer are identified successfully.

Original language	English
Title of host publication	SAFEPROCESS'09 - 7th IFAC International Symposium on Fault Detection, Supervision and Safety of Technical Systems, Proceedings
Publisher	IFAC Secretariat
Pages	1408-1413
Number of pages	6
ISBN (Print)	9783902661463
DOIs	https://doi.org/10.3182/20090630-4-es-2003.00229
Publication status	Published - 2009
Externally published	Yes

Publication series

Name	IFAC Proceedings Volumes (IFAC-PapersOnline)
ISSN (Print)	1474-6670

Keywords

Aircraft
Estimation
Fault detection
Fault identification
Fault isolation
Kalman filter

Access to Document

10.3182/20090630-4-es-2003.00229

Cite this

Caliskan, F., Zhang, Y., Eva Wu, N., & Shin, J. Y. (2009). Estimation of actuator fault parameters in a nonlinear boeing 747 model using a linear two-stage Kalman filter. In SAFEPROCESS'09 - 7th IFAC International Symposium on Fault Detection, Supervision and Safety of Technical Systems, Proceedings (pp. 1408-1413). (IFAC Proceedings Volumes (IFAC-PapersOnline)). IFAC Secretariat. https://doi.org/10.3182/20090630-4-es-2003.00229

Caliskan, Fikret ; Zhang, Youmin ; Eva Wu, N. et al. / Estimation of actuator fault parameters in a nonlinear boeing 747 model using a linear two-stage Kalman filter. SAFEPROCESS'09 - 7th IFAC International Symposium on Fault Detection, Supervision and Safety of Technical Systems, Proceedings. IFAC Secretariat, 2009. pp. 1408-1413 (IFAC Proceedings Volumes (IFAC-PapersOnline)).

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title = "Estimation of actuator fault parameters in a nonlinear boeing 747 model using a linear two-stage Kalman filter",

abstract = "In this paper, an adaptive two-stage linear Kalman filtering algorithm (Wu, Zhang, and Zhou, 2000) is used to estimate the loss of control effectiveness and the magnitude of low degree of stuck faults in a closed-loop nonlinear B747 aircraft. Control effectiveness factors and stuck magnitudes are used to quantify faults entering control systems through actuators. Pseudo random excitation inputs are used to help distinguish partial loss and stuck faults. The partial loss and stuck faults in the stabilizer are identified successfully.",

keywords = "Aircraft, Estimation, Fault detection, Fault identification, Fault isolation, Kalman filter",

author = "Fikret Caliskan and Youmin Zhang and {Eva Wu}, N. and Shin, {J. Y.}",

year = "2009",

doi = "10.3182/20090630-4-es-2003.00229",

language = "English",

isbn = "9783902661463",

series = "IFAC Proceedings Volumes (IFAC-PapersOnline)",

publisher = "IFAC Secretariat",

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}

Caliskan, F, Zhang, Y, Eva Wu, N & Shin, JY 2009, Estimation of actuator fault parameters in a nonlinear boeing 747 model using a linear two-stage Kalman filter. in SAFEPROCESS'09 - 7th IFAC International Symposium on Fault Detection, Supervision and Safety of Technical Systems, Proceedings. IFAC Proceedings Volumes (IFAC-PapersOnline), IFAC Secretariat, pp. 1408-1413. https://doi.org/10.3182/20090630-4-es-2003.00229

Estimation of actuator fault parameters in a nonlinear boeing 747 model using a linear two-stage Kalman filter. / Caliskan, Fikret; Zhang, Youmin; Eva Wu, N. et al.
SAFEPROCESS'09 - 7th IFAC International Symposium on Fault Detection, Supervision and Safety of Technical Systems, Proceedings. IFAC Secretariat, 2009. p. 1408-1413 (IFAC Proceedings Volumes (IFAC-PapersOnline)).

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

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AU - Zhang, Youmin

AU - Eva Wu, N.

AU - Shin, J. Y.

PY - 2009

Y1 - 2009

N2 - In this paper, an adaptive two-stage linear Kalman filtering algorithm (Wu, Zhang, and Zhou, 2000) is used to estimate the loss of control effectiveness and the magnitude of low degree of stuck faults in a closed-loop nonlinear B747 aircraft. Control effectiveness factors and stuck magnitudes are used to quantify faults entering control systems through actuators. Pseudo random excitation inputs are used to help distinguish partial loss and stuck faults. The partial loss and stuck faults in the stabilizer are identified successfully.

AB - In this paper, an adaptive two-stage linear Kalman filtering algorithm (Wu, Zhang, and Zhou, 2000) is used to estimate the loss of control effectiveness and the magnitude of low degree of stuck faults in a closed-loop nonlinear B747 aircraft. Control effectiveness factors and stuck magnitudes are used to quantify faults entering control systems through actuators. Pseudo random excitation inputs are used to help distinguish partial loss and stuck faults. The partial loss and stuck faults in the stabilizer are identified successfully.

KW - Aircraft

KW - Estimation

KW - Fault detection

KW - Fault identification

KW - Fault isolation

KW - Kalman filter

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U2 - 10.3182/20090630-4-es-2003.00229

DO - 10.3182/20090630-4-es-2003.00229

M3 - Conference contribution

AN - SCOPUS:79960922248

SN - 9783902661463

T3 - IFAC Proceedings Volumes (IFAC-PapersOnline)

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BT - SAFEPROCESS'09 - 7th IFAC International Symposium on Fault Detection, Supervision and Safety of Technical Systems, Proceedings

PB - IFAC Secretariat

ER -

Caliskan F, Zhang Y, Eva Wu N, Shin JY. Estimation of actuator fault parameters in a nonlinear boeing 747 model using a linear two-stage Kalman filter. In SAFEPROCESS'09 - 7th IFAC International Symposium on Fault Detection, Supervision and Safety of Technical Systems, Proceedings. IFAC Secretariat. 2009. p. 1408-1413. (IFAC Proceedings Volumes (IFAC-PapersOnline)). doi: 10.3182/20090630-4-es-2003.00229

Estimation of actuator fault parameters in a nonlinear boeing 747 model using a linear two-stage Kalman filter

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