DocumentCode
1804830
Title
A fault-tolerant solid state mass memory for highly reliable instrumentation
Author
Cardarilli, G.C. ; Ottavi, M. ; Pontarelli, S. ; Re, M. ; Salsano, A.
Author_Institution
Dept. of Electron. Eng., Univ. of Rome Tor Veroata, Italy
Volume
3
fYear
2004
fDate
18-20 May 2004
Firstpage
1651
Abstract
Often, in space missions, a large amount of data from on board instrumentation must be stored in highly reliable mass memories. In this paper the implementation of a prototype of a Solid State Mass Memory (SSMM) for high reliability demanding applications is presented. A description of the SSMM architecture is given together with an in depth description of the prototype. The SSMM has been implemented by using a fast prototyping methodology. By using this technique, a flexible re-programmable test bed useful for the testing of both the conventional and faulty (using the fault-injection approach) functionality of the system has been obtained.
Keywords
DRAM chips; avionics; error detection; fault tolerant computing; memory architecture; space vehicle electronics; COTS components; SDRAM modules; design methodology; fast prototyping; fault-injection approach; fault-tolerant solid state mass memory; flexible re-programmable test bed; highly reliable instrumentation; low hardware redundancy; memory kernel unit; on board instrumentation; routing system; space missions; system control unit; Design methodology; Fault tolerance; Fault tolerant systems; Hardware; Instruments; Prototypes; Redundancy; Satellites; Solid state circuits; Space technology;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation and Measurement Technology Conference, 2004. IMTC 04. Proceedings of the 21st IEEE
ISSN
1091-5281
Print_ISBN
0-7803-8248-X
Type
conf
DOI
10.1109/IMTC.2004.1351398
Filename
1351398
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