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Fault detection and isolation of actuator failures for a large transport aircraft

Varga, Andreas (2007) Fault detection and isolation of actuator failures for a large transport aircraft. In: Proceeding First CEAS European Air and Space Conference, Berlin, Germany. CEAS 2007, Berlin.

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Abstract

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 with 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:Conference or Workshop Item (Speech, Paper)
Title:Fault detection and isolation of actuator failures for a large transport aircraft
Authors:
AuthorsInstitution or Email of Authors
Varga, AndreasUNSPECIFIED
Date:2007
Journal or Publication Title:Proceeding First CEAS European Air and Space Conference, Berlin, Germany
Refereed publication:Yes
In ISI Web of Science:No
Status:Published
Keywords:-
Event Title:CEAS 2007
Event Location:Berlin
Event Type:international Conference
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: Monika Klauer
Deposited On:09 Jun 2008
Last Modified:12 Dec 2013 20:27

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