H ∞ ∕ H − LPV solutions for fault detection of aircraft actuator faults: Bridging the gap between theory and practice-Reference-Cited by-同舟云学术

H ∞ ∕ H − LPV solutions for fault detection of aircraft actuator faults: Bridging the gap between theory and practice

Published:2014-03-16 Issue:5 Volume:25 Page:649-672
ISSN:1049-8923
Container-title:International Journal of Robust and Nonlinear Control
language:en
Short-container-title:Int. J. Robust Nonlinear Control

Author:

Henry D.¹,Cieslak J.¹,Zolghadri A.¹,Efimov D.²

Affiliation:

1. Bordeaux University-UMR CNRS 5218; IMS lab. - 33405 Talence cedex Bordeaux France

2. INRIA-LNE, Parc Scientifique de la Haute Borne 40; avenue Halley Bat.A, Park Plaza 59650 Villeneuve d'Ascq France

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Mechanical Engineering,Aerospace Engineering,Biomedical Engineering,General Chemical Engineering,Control and Systems Engineering

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1002/rnc.3157/fullpdf

Reference62 articles.

1. A method for designing fault diagnosis filters for LPV polytopic systems;Grenaille;Journal of Control Science and Engineering - Robustness Issues in Fault Diagnosis and Fault Tolerant Control,2008

2. Structured fault detection filters for LPV systems modeled in a LFR manner;Henry;International Journal of Adaptive Control and Signal Processing,2012

3. FAR/JAR-25 Airworthiness standards: Transport category airplane, published by FAA, title 14, part 25, and Certification Specifications for Large Aeroplanes, published by EASA. CS-25

4. Caglayan A Rahnamai K Allen S Detection, identification and estimation of surface damage/actuator failure for high performance aircraft Proceedings of the American Control Conference 1988 2206 2212

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