DocumentCode
3341926
Title
The Space Shuttle launch computer control system at NASA Kennedy Space Center
Author
Furht, Borko ; Luken, Robert
Author_Institution
MODCOMP, AEG Co., Fort Lauderdale, FL, USA
fYear
1991
fDate
12-14 Jun 1991
Firstpage
184
Lastpage
192
Abstract
This paper illustrates how a complex application, the data acquisition and Space Shuttle Launch Control System at NASA Kennedy Space Center, which requires both intensive communications and high processing power, can be mapped into an advanced open system architecture. This is achieved by employing a symmetric, tightly-coupled multiprocessor system which includes a high bandwidth common memory bus, an efficient interrupt distribution scheme, dedicated high-performance I/O processors, and runs a multiprocessor real-time UNIX operating system. The authors concentrate on the Data Acquisition System. First, the communication and processing requirements for the system is specified. Then, on the basis of the model of the system, the multiprocessor architecture is defined to meet these requirements
Keywords
computer interfaces; data acquisition; multiprocessing systems; parallel architectures; real-time systems; space vehicles; NASA Kennedy Space Center; Space Shuttle Launch Control System; communication requirements analysis; data acquisition; data acquisition processor; dedicated I/O processor; dedicated high-performance I/O processors; high bandwidth common memory bus; interrupt distribution scheme; open system architecture; processing requirements; tightly-coupled multiprocessor system; Application software; Bandwidth; Communication system control; Computer architecture; Control systems; Data acquisition; Multiprocessing systems; NASA; Open systems; Space shuttles;
fLanguage
English
Publisher
ieee
Conference_Titel
Real Time Systems, 1991. Proceedings., Euromicro '91 Workshop on
Conference_Location
Paris-Orsay
Print_ISBN
0-8186-2210-5
Type
conf
DOI
10.1109/EMWRT.1991.144103
Filename
144103
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