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