• 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