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

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

An important issue for Aerospace and Defence 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 paper describes the initial phases of a project to investigate the processes behind the assessment and validation using an Experimental Aircraft Fuel Rig (referred to as the Advanced Diagnostic Test-bed ADT). This paper 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.

Original languageEnglish
Title of host publication6th IFAC Symposium on Fault Detection, Supervision and Safety of Technical Processes, SAFEPROCESS 2006
Pages324-329
Number of pages6
Volume6
EditionPART 1
Publication statusPublished - 1 Dec 2006
Event6th IFAC Symposium on Fault Detection, Supervision and Safety of Technical Processes, SAFEPROCESS 2006 - Beijing, China
Duration: 29 Aug 20061 Sep 2006

Conference

Conference6th IFAC Symposium on Fault Detection, Supervision and Safety of Technical Processes, SAFEPROCESS 2006
Country/TerritoryChina
CityBeijing
Period29/08/061/09/06

Keywords

  • Aerospace
  • Fault detection
  • Fault diagnosis
  • Fault isolation
  • Model based

ASJC Scopus subject areas

  • Control and Systems Engineering

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