DocumentCode :
2549456
Title :
Process for diagnosis method selection of flight critical systems: Application to a Sensor Acquisition System
Author :
Martin, Rashad ; Terrasson, G. ; Briand, R. ; Guerineau, O. ; Gatti, Marc
fYear :
2012
fDate :
14-18 Oct. 2012
Firstpage :
1
Lastpage :
30
Abstract :
Save money: Reduce maintenance costs; Reduce V-model iterations number; Make the system more generic and then reduce installation delays and complexity; Increase performances: Make the system more Fault Tolerant; Prognosis ability through the measurement of wear-out and improve maintenance performances and costs; Parameters and aging compensation ability; Others SAS: Temperature, pressure, speed, torque; Others FCS: Engine control, auxiliary power unit, environment control systems.
Keywords :
aerospace instrumentation; fault tolerance; installation; sensors; V-model iterations number; aging compensation ability; auxiliary power unit; diagnosis method selection; engine control; environment control systems; fault tolerance; flight critical systems; installation delays; maintenance costs; maintenance performances; prognosis ability; sensor acquisition system; wear-out;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference (DASC), 2012 IEEE/AIAA 31st
Conference_Location :
Williamsburg, VA
ISSN :
2155-7195
Print_ISBN :
978-1-4673-1699-6
Type :
conf
DOI :
10.1109/DASC.2012.6383080
Filename :
6383080
Link To Document :
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