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.
Reconfiguration in an integrated avionics design
1996-01-01
727102 byte
Conference paper
Electronic Resource
English
Reconfiguration in an Integrated Avionics Design
British Library Conference Proceedings | 1996
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