DocumentCode :
2200232
Title :
32-bit processing unit for embedded space flight applications
Author :
Stachetti, Vincent ; Gaisler, Jiri ; Goller, Gerhard ; Le Gargasson, Chstophe
Author_Institution :
MATRA MHS, Nantes, France
fYear :
1995
fDate :
18-22 Sep 1995
Firstpage :
212
Lastpage :
217
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); special purpose computers; 32 bit; ERC 32 processing unit; Floating Point Unit; Integer Unit; Memory Controller; concurrent error-detection; design; embedded space flight applications; layout; modular fault-tolerant processing; radiation hardening; Application software; CMOS logic circuits; Circuit testing; Computer errors; Error correction; Fault tolerance; Radiation hardening; Registers; Space technology; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Radiation and its Effects on Components and Systems, 1995. RADECS 95., Third European Conference on
Conference_Location :
Arcachon
Print_ISBN :
0-7803-3093-5
Type :
conf
DOI :
10.1109/RADECS.1995.509779
Filename :
509779
Link To Document :
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