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2017 | OriginalPaper | Chapter

8. Case Studies

Author : Andreas Varga

Published in: Solving Fault Diagnosis Problems

Publisher: Springer International Publishing

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Abstract

This chapter illustrates the formulation of typical fault monitoring problems in complex technological systems and the application of the linear synthesis techniques, described in this book, to address the challenges of practical applications. Two case studies, both related to flight control applications, are considered. The chosen examples address the monitoring of flight actuator faults and air data sensor faults, in the presence of uncertainties in the aircraft mass.

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previous chapter Computational Issues

next chapter System Theoretical Concepts

The European Flight Mechanics Action Group FM-AG(16) on Fault Tolerant Control was established in 2004 and concluded in 2008. It represented a collaboration involving thirteen European partners from industry, universities and research establishments under the auspices of the Group for Aeronautical Research and Technology in Europe (GARTEUR) program.

IMMUNE (Intelligent Monitoring and Management of Unexpected Events) was a ONERA-DLR Joint Research Project started in 2006 and concluded in 2009.

ADDSAFE (Advanced Fault Diagnosis for Safer Flight Guidance and Control) was a EU-funded project in the framework programme FP7, started in 2009 and finished in 2012, http://cordis.europa.eu/project/rcn/92071_en.html.

RECONFIGURE (Reconfiguration of Control in Flight for Integral Global Upset Recovery) was a EU-funded project in the framework programme FP7, started in 2013 and finished in 2016, http://cordis.europa.eu/project/rcn/104633_en.html.

Title: Case Studies
Author: Andreas Varga
Publisher: Springer International Publishing
Book: Solving Fault Diagnosis Problems
Print ISBN: 978-3-319-51558-8

Electronic ISBN: 978-3-319-51559-5

Copyright Year: 2017
DOI: https://doi.org/10.1007/978-3-319-51559-5_8