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

Research output: Contribution to journal › Article › peer-review

14 Scopus citations

Abstract

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.

Original language	Spanish
Pages (from-to)	521-542
Number of pages	22
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	49
State	Published - 21 Jan 2013

Cite this

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title = "Tracking performance of distributed recoverable flight control systems subject to high intensity radiated fields",

abstract = "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. {\textcopyright} 1965-2011 IEEE.",

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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.

M3 - Artículo

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JO - IEEE Transactions on Aerospace and Electronic Systems

JF - IEEE Transactions on Aerospace and Electronic Systems

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