Theoretical tools are presented to analyze the relationship between the design choices for a class of NASA-inspired fault-tolerant, reconfigurable computer architectures and the tracking performance degradation of a digital flight control system implemented on such a platform while operating in a high-intensity radiated field (HIRF) environment. A HIRF experiment was conducted at the NASA Langley Research Center to validate the theory for a distributed Boeing 747 flight control system subject to HIRF upsets.
Tracking Performance of Distributed Recoverable Flight Control Systems Subject to High Intensity Radiated Fields
IEEE Transactions on Aerospace and Electronic Systems ; 49 , 1 ; 521-542
2013-01-01
8432522 byte
Article (Journal)
Electronic Resource
English
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