TY - JOUR
T1 - Tracking performance of distributed recoverable flight control systems subject to high intensity radiated fields
AU - Wang, Rui
AU - Steven Gray, W.
AU - Gonzalez, Oscar R.
AU - Chavez-Fuentes, Jorge R.
PY - 2013
Y1 - 2013
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.
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.
UR - http://www.scopus.com/inward/record.url?scp=84872362381&partnerID=8YFLogxK
U2 - 10.1109/TAES.2013.6404118
DO - 10.1109/TAES.2013.6404118
M3 - Article
AN - SCOPUS:84872362381
SN - 0018-9251
VL - 49
SP - 521
EP - 542
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 1
M1 - 6404118
ER -