DocumentCode
1747128
Title
Establishing ultra-reliability by fault injection experiments
Author
White, Allan L.
Author_Institution
NASA Langley Res. Center, Hampton, VA, USA
Volume
1
fYear
2001
fDate
2001
Abstract
A validation procedure combines field data, arguments-from-design, and fault injection experiments to demonstrate high reliability. This paper covers integrating these elements and deriving results that reduce the fault injection effort. A typical argument about the impossibility of demonstrating ultra reliability by experiment is presented to motivate the emphasis on reducing the experimental effort. An example is used to explain the integration of field data, fault injection, arguments-from-design, and performance monitoring. This validation procedure has stringent requirements, but it is shown that these requirements are common to other procedures. There is an extended analysis on number, type, and time of fault occurrence. These results are applied to a system with an extremely high reliability requirement. They reduce the experimental effort to a moderate level
Keywords
aerospace control; design of experiments; fault diagnosis; fault tolerance; probability; reliability theory; Markov model approach comparison; arguments-from-design; binomial sampling; fault injection experiments; fault tolerance; infeasibility argument; integration of field data; natural life experiment; performance monitoring; probability derivations; stringent requirements; ultrahigh reliability; validation procedure; Aerospace control; Aerospace electronics; Aircraft; Concrete; Counting circuits; Digital control; Government; Monitoring; NASA; Protection;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2001, IEEE Proceedings.
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-6599-2
Type
conf
DOI
10.1109/AERO.2001.931699
Filename
931699
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