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
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;
Conference_Titel :
Instrumentation and Measurement Technology Conference, 2004. IMTC 04. Proceedings of the 21st IEEE
Print_ISBN :
0-7803-8248-X
DOI :
10.1109/IMTC.2004.1351398