DocumentCode :
3269050
Title :
Characterization of a recoverable flight control computer system
Author :
Malekpour, Mahyar ; Torres, Wilfredo
Author_Institution :
NASA Langley Res. Center, Hampton, VA, USA
Volume :
2
fYear :
1999
fDate :
1999
Firstpage :
1519
Abstract :
The design and development of a closed-loop system to study and evaluate the performance of the Honeywell Recoverable Computer System (RCS) in electromagnetic environments (EME) is presented. The development of a Windows-based software package to handle the time-critical communication of data and commands between the RCS and flight simulation code in real-time, while meeting the stringent hard deadlines is also submitted. The performance results of the RCS and characteristics of its upset recovery scheme while exercising flight control laws under ideal conditions as well as in the presence of electromagnetic fields are also discussed
Keywords :
aerospace simulation; aircraft control; closed loop systems; electromagnetic interference; fault tolerant computing; Honeywell Recoverable Computer System; Windows-based software package; electromagnetic environments; flight control laws; flight simulation code; recoverable flight control computer system; time-critical communication; upset recovery scheme; Aerospace control; Aerospace electronics; Aerospace simulation; Aircraft; Computer architecture; Electromagnetic fields; Electromagnetic radiation; NASA; Protection; Prototypes;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications, 1999. Proceedings of the 1999 IEEE International Conference on
Conference_Location :
Kohala Coast, HI
Print_ISBN :
0-7803-5446-X
Type :
conf
DOI :
10.1109/CCA.1999.801197
Filename :
801197
Link To Document :
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