DocumentCode :
2924734
Title :
Redundancy design philosophy for catastrophic loss protection
Author :
Eagle, Kenneth H. ; Agarwala, Ajay S.
Author_Institution :
Boeing Helicopters, Philadelphia, PA, USA
fYear :
1992
fDate :
21-23 Jan 1992
Firstpage :
1
Lastpage :
4
Abstract :
To ensure high flight safety and mission reliability in flight-critical electronics of aerospace vehicles, a redundancy design technique named brick wall is discussed. Basically, the technique proposes triplex redundant, independent paths where each path can self-monitor its own health (by using a comparison scheme within each path). Upon a fault detection, the whole path is taken offline. The inherent high redundancy allows the achievement of stringent flight safety and mission reliability goals. The design also protects against hidden/unknown failure modes and sneak circuits. The design tradeoffs are made against higher maintenance rates, cost, and weight
Keywords :
aircraft; design engineering; reliability; safety; aerospace vehicles; brick wall; catastrophic loss protection; failure modes; fault detection; redundancy design; reliability; safety; sneak circuits; Aerospace control; Aerospace electronics; Aerospace safety; Automatic frequency control; Circuits; FCC; Helicopters; Maintenance; Protection; Redundancy;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability and Maintainability Symposium, 1992. Proceedings., Annual
Conference_Location :
Las Vegas, NV
Print_ISBN :
0-7803-0521-3
Type :
conf
DOI :
10.1109/ARMS.1992.187791
Filename :
187791
Link To Document :
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