Reconfiguration in an integrated avionics design

This report covers the subject of F-22 avionics core processing fault tolerance and reconfiguration. Fault tolerance is defined as a survivable attribute of a system that allows it to deliver its expected service after faults have manifested themselves within the system. The report addresses all dim...

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Bibliographic Details
Published in15th DASC. AIAA/IEEE Digital Avionics Systems Conference pp. 471 - 478
Main Author Seeling, K.
Format Conference Proceeding
LanguageEnglish
Published IEEE 1996
Subjects
Aerospace electronics
Availability
Bandwidth
Computer architecture
Condition monitoring
Data processing
Fault tolerance
Fault tolerant systems
Liver
Signal processing
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Summary:This report covers the subject of F-22 avionics core processing fault tolerance and reconfiguration. Fault tolerance is defined as a survivable attribute of a system that allows it to deliver its expected service after faults have manifested themselves within the system. The report addresses all dimensions of the integrated avionics processing fault tolerance/reconfiguration implementation. This includes the preparation for failures, detection of failures, determination and implementation of a recovery scheme, and return to operations.
ISBN:0780333853
9780780333857
DOI:10.1109/DASC.1996.559202