DocumentCode :
1095169
Title :
32-bit processing unit for embedded space flight applications
Author :
Stachetti, Vincent ; Gaisler, Jiri ; Goller, Gerhard ; Le Gargasson, Christophe
Author_Institution :
MATRA MHS, Nantes, France
Volume :
43
Issue :
3
fYear :
1996
fDate :
6/1/1996 12:00:00 AM
Firstpage :
873
Lastpage :
878
Abstract :
This paper describes the concurrent error-detection methods as well as the design and layout hardening techniques employed in the ERC 32, a 32-bit modular fault-tolerant processing core for embedded space flight applications. The core consists of three devices: an Integer Unit (IU), a Floating Point Unit (FPU), and a Memory Controller (MEC)
Keywords :
aerospace computing; error detection; fault tolerant computing; radiation hardening (electronics); real-time systems; space vehicle electronics; special purpose computers; 32 bit; ERC 32; Floating Point Unit; Integer Unit; Memory Controller; concurrent error-detection; design; embedded space flight applications; layout; modular fault-tolerant processing unit; radiation hardening; Application software; CMOS logic circuits; Computer errors; Error correction; Fault tolerance; Radiation hardening; Registers; Single event upset; Space technology; Space vehicles;
fLanguage :
English
Journal_Title :
Nuclear Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9499
Type :
jour
DOI :
10.1109/23.510727
Filename :
510727
Link To Document :
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