Characterization of a recoverable flight control computer system
Malekpour, M.
Torres, W.
NASA Langley Res. Center, Hampton, VA;
This paper appears in: Control Applications, 1999. Proceedings of the 1999 IEEE International Conference on
Publication Date: 1999
Volume: 2,
On page(s): 1519-1524 vol. 2
Meeting Date: 08/22/1999 - 08/27/1999
Location: Kohala Coast, HI, USA
ISBN: 0-7803-5446-X
References Cited: 6
INSPEC Accession Number: 6468565
Digital Object Identifier: 10.1109/CCA.1999.801197
Current Version Published: 2002-08-06
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
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