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Software fault tolerance for real-time avionics systemsAvionics systems have very high reliability requirements and are therefore prime candidates for the inclusion of fault tolerance techniques. In order to provide tolerance to software faults, some form of state restoration is usually advocated as a means of recovery. State restoration can be very expensive for systems which utilize concurrent processes. The concurrency present in most avionics systems and the further difficulties introduced by timing constraints imply that providing tolerance for software faults may be inordinately expensive or complex. A straightforward pragmatic approach to software fault tolerance which is believed to be applicable to many real-time avionics systems is proposed. A classification system for software errors is presented together with approaches to recovery and continued service for each error type.
Document ID
19830013861
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, T.
(Newcastle upon Tyne Univ. Hampton, VA, United States)
Knight, J. C.
(NASA Langley Research Center)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Publication Information
Publication: AGARD Software for Avionics
Subject Category
Computer Programming And Software
Accession Number
83N22132
Funding Number(s)
CONTRACT_GRANT: NAS1-14101
CONTRACT_GRANT: NAS1-14472
Distribution Limits
Public
Copyright
Other
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