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Detection and Isolation of Actuator/Surface Faults for a Large Transport Aircraft

Varga, A. (2010) Detection and Isolation of Actuator/Surface Faults for a Large Transport Aircraft. In: Lecture Notes in Control and Information Science, 399. Springer-Verlag. pp. 423-442.

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Abstract

We consider the problem of designing residual generators with least dynamical orders to solve actuator fault detection and isolation problems for a Boeing 747-100/200 aircraft. The main result of our analysis is the proof of feasibility of the complete isolation of all primary actuator/surface faults in the nominal case by using a minimal number of additional surface angle sensors. The analysis of the nominal case provides residual filter specifications which can be employed in a more realistic design, where robustness aspects with respect to external noise (gusts, measurements) and parametric/flight condition uncertainties are also considered.

Document Type:Book Section
Title:Detection and Isolation of Actuator/Surface Faults for a Large Transport Aircraft
Authors:
AuthorsInstitution or Email of Authors
Varga, A.DLR Oberpfaffenhofen
Date:2010
Refereed publication:Yes
Volume:399
Page Range:pp. 423-442
Editors:
EditorsEmail
Edwards, C.UNSPECIFIED
Lombaerts, T.UNSPECIFIED
Smaili, H.UNSPECIFIED
Publisher:Springer-Verlag
Series Name:Lecture Notes in Control and Information Science
Status:Published
Keywords:faul detection and isolation, FDI, actuator faults, numerical methods
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems & Cabin
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Robotics and Mechatronics > System Dynamics and Control (former Control Design Engineering)
Deposited By: Dr.-Ing. Andreas Varga
Deposited On:23 Dec 2011 14:48
Last Modified:12 Dec 2013 21:31

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