Tracking Performance of Distributed Recoverable Flight Control Systems Subject to High Intensity Radiated Fields

Tracking Performance of Distributed Recoverable Flight Control Systems Subject to High Intensity Radiated Fields

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 hi...

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Veröffentlicht in:IEEE transactions on aerospace and electronic systems 2013-01, Vol.49 (1), p.521-542
Hauptverfasser: Rui Wang, Gray, W. S., Gonzalez, O. R., Chavez-Fuentes, J. R.
Format: Artikel
Sprache:eng
Schlagworte:
Aerospace control
Atmospheric modeling
Computational modeling
Distributed computing
Joints
Markov processes
Switches
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Zusammenfassung: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.
ISSN:0018-9251
1557-9603
DOI:10.1109/TAES.2013.6404118