Tracking performance of distributed recoverable flight control systems subject to high intensity radiated fields

Rui Wang; W. Steven Gray; Oscar R. Gonzalez; Jorge R. Chávez-Fuentes

Tracking performance of distributed recoverable flight control systems subject to high intensity radiated fields

Rui Wang, W. Steven Gray, Oscar R. Gonzalez, Jorge R. Chávez-Fuentes

Sección de Matemáticas

Old Dominion University

Producción científica: Contribución a una revista › Artículo › revisión exhaustiva

14 Citas (Scopus)

Resumen

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. © 1965-2011 IEEE.

Idioma original	Español
Páginas (desde-hasta)	521-542
Número de páginas	22
Publicación	IEEE Transactions on Aerospace and Electronic Systems
Volumen	49
Estado	Publicada - 21 ene. 2013

Citar esto

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N2 - 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. © 1965-2011 IEEE.

AB - 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. © 1965-2011 IEEE.

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