Application of diagnostic techniques to an experimental aircraft fuel rig

P. J. Bennett, J. T. Pearson, A. Martin, R. Dixon, M. C. Walsh, M. Khella, R. M. Goodall

Research output: Chapter in Book/Report/Conference proceedingChapter

2 Citations (Scopus)

Abstract

An important issue for aerospace and defense systems providers is how to reduce the risks associated with installing a new fault detection tool (FDT) on a system. It is highly desirable that some degree of assessment, selection, and validation is carried out before the FDT is integrated with the system. This chapter describes an Advanced Diagnostic Test-bed (ADT), which has been designed to be used as part of a larger project for the assessment of various fault diagnostic tools and techniques. The project is in its early phases but the ADT has been successfully commissioned and some initial work has been started. The chapter also presents results from preliminary verification and validation work that has been used on a mathematical model of the ADT, and also some results from some initial diagnostic technique assessment that has been performed using real experimental data from the ADT and simulated data from mathematical models. © 2007

LanguageEnglish
Title of host publicationFault Detection, Supervision and Safety of Technical Processes 2006
Subtitle of host publicationA Proceedings Volume from the 6th IFAC Symposium SAFEPROCESS 2006
EditorsHong-Yue Zhang
PublisherElsevier Ltd
Pages324-329
Number of pages6
Volume1
ISBN (Print)9780080444857
DOIs
Publication statusPublished - 1 Dec 2007
Externally publishedYes
Event6th IFAC Symposium: SAFEPROCESS 2006 - Beijing, China
Duration: 30 Aug 20061 Sep 2006

Conference

Conference6th IFAC Symposium
CountryChina
CityBeijing
Period30/08/061/09/06

Fingerprint

Aircraft fuels
Fault detection
Mathematical models

Cite this

Bennett, P. J., Pearson, J. T., Martin, A., Dixon, R., Walsh, M. C., Khella, M., & Goodall, R. M. (2007). Application of diagnostic techniques to an experimental aircraft fuel rig. In H-Y. Zhang (Ed.), Fault Detection, Supervision and Safety of Technical Processes 2006: A Proceedings Volume from the 6th IFAC Symposium SAFEPROCESS 2006 (Vol. 1, pp. 324-329). Elsevier Ltd. https://doi.org/10.1016/B978-008044485-7/50055-5
Bennett, P. J. ; Pearson, J. T. ; Martin, A. ; Dixon, R. ; Walsh, M. C. ; Khella, M. ; Goodall, R. M. / Application of diagnostic techniques to an experimental aircraft fuel rig. Fault Detection, Supervision and Safety of Technical Processes 2006: A Proceedings Volume from the 6th IFAC Symposium SAFEPROCESS 2006 . editor / Hong-Yue Zhang. Vol. 1 Elsevier Ltd, 2007. pp. 324-329
@inbook{1fd0c9556d364634abce937cb11d8e9f,
title = "Application of diagnostic techniques to an experimental aircraft fuel rig",
abstract = "An important issue for aerospace and defense systems providers is how to reduce the risks associated with installing a new fault detection tool (FDT) on a system. It is highly desirable that some degree of assessment, selection, and validation is carried out before the FDT is integrated with the system. This chapter describes an Advanced Diagnostic Test-bed (ADT), which has been designed to be used as part of a larger project for the assessment of various fault diagnostic tools and techniques. The project is in its early phases but the ADT has been successfully commissioned and some initial work has been started. The chapter also presents results from preliminary verification and validation work that has been used on a mathematical model of the ADT, and also some results from some initial diagnostic technique assessment that has been performed using real experimental data from the ADT and simulated data from mathematical models. {\circledC} 2007",
keywords = "Aerospace, Fault Detection, Fault diagnosis, fault isolation, model cased",
author = "Bennett, {P. J.} and Pearson, {J. T.} and A. Martin and R. Dixon and Walsh, {M. C.} and M. Khella and Goodall, {R. M.}",
year = "2007",
month = "12",
day = "1",
doi = "10.1016/B978-008044485-7/50055-5",
language = "English",
isbn = "9780080444857",
volume = "1",
pages = "324--329",
editor = "Hong-Yue Zhang",
booktitle = "Fault Detection, Supervision and Safety of Technical Processes 2006",
publisher = "Elsevier Ltd",
address = "United Kingdom",

}

Bennett, PJ, Pearson, JT, Martin, A, Dixon, R, Walsh, MC, Khella, M & Goodall, RM 2007, Application of diagnostic techniques to an experimental aircraft fuel rig. in H-Y Zhang (ed.), Fault Detection, Supervision and Safety of Technical Processes 2006: A Proceedings Volume from the 6th IFAC Symposium SAFEPROCESS 2006 . vol. 1, Elsevier Ltd, pp. 324-329, 6th IFAC Symposium, Beijing, China, 30/08/06. https://doi.org/10.1016/B978-008044485-7/50055-5

Application of diagnostic techniques to an experimental aircraft fuel rig. / Bennett, P. J.; Pearson, J. T.; Martin, A.; Dixon, R.; Walsh, M. C.; Khella, M.; Goodall, R. M.

Fault Detection, Supervision and Safety of Technical Processes 2006: A Proceedings Volume from the 6th IFAC Symposium SAFEPROCESS 2006 . ed. / Hong-Yue Zhang. Vol. 1 Elsevier Ltd, 2007. p. 324-329.

Research output: Chapter in Book/Report/Conference proceedingChapter

TY - CHAP

T1 - Application of diagnostic techniques to an experimental aircraft fuel rig

AU - Bennett, P. J.

AU - Pearson, J. T.

AU - Martin, A.

AU - Dixon, R.

AU - Walsh, M. C.

AU - Khella, M.

AU - Goodall, R. M.

PY - 2007/12/1

Y1 - 2007/12/1

N2 - An important issue for aerospace and defense systems providers is how to reduce the risks associated with installing a new fault detection tool (FDT) on a system. It is highly desirable that some degree of assessment, selection, and validation is carried out before the FDT is integrated with the system. This chapter describes an Advanced Diagnostic Test-bed (ADT), which has been designed to be used as part of a larger project for the assessment of various fault diagnostic tools and techniques. The project is in its early phases but the ADT has been successfully commissioned and some initial work has been started. The chapter also presents results from preliminary verification and validation work that has been used on a mathematical model of the ADT, and also some results from some initial diagnostic technique assessment that has been performed using real experimental data from the ADT and simulated data from mathematical models. © 2007

AB - An important issue for aerospace and defense systems providers is how to reduce the risks associated with installing a new fault detection tool (FDT) on a system. It is highly desirable that some degree of assessment, selection, and validation is carried out before the FDT is integrated with the system. This chapter describes an Advanced Diagnostic Test-bed (ADT), which has been designed to be used as part of a larger project for the assessment of various fault diagnostic tools and techniques. The project is in its early phases but the ADT has been successfully commissioned and some initial work has been started. The chapter also presents results from preliminary verification and validation work that has been used on a mathematical model of the ADT, and also some results from some initial diagnostic technique assessment that has been performed using real experimental data from the ADT and simulated data from mathematical models. © 2007

KW - Aerospace

KW - Fault Detection

KW - Fault diagnosis

KW - fault isolation

KW - model cased

UR - http://www.scopus.com/inward/record.url?scp=84884079056&partnerID=8YFLogxK

U2 - 10.1016/B978-008044485-7/50055-5

DO - 10.1016/B978-008044485-7/50055-5

M3 - Chapter

SN - 9780080444857

VL - 1

SP - 324

EP - 329

BT - Fault Detection, Supervision and Safety of Technical Processes 2006

A2 - Zhang, Hong-Yue

PB - Elsevier Ltd

ER -

Bennett PJ, Pearson JT, Martin A, Dixon R, Walsh MC, Khella M et al. Application of diagnostic techniques to an experimental aircraft fuel rig. In Zhang H-Y, editor, Fault Detection, Supervision and Safety of Technical Processes 2006: A Proceedings Volume from the 6th IFAC Symposium SAFEPROCESS 2006 . Vol. 1. Elsevier Ltd. 2007. p. 324-329 https://doi.org/10.1016/B978-008044485-7/50055-5