• DocumentCode
    2714946
  • Title

    State model for scheduling Built-in Self-Test and scrubbing in FPGA to maximize the system availability in space applications

  • Author

    Agarwal, Ankit ; Bhatia, Gaurav ; Chakraverty, Shampa

  • Author_Institution
    Comput. Eng. Dept., Netaji Subhas Inst. of Technol., New Delhi, India
  • fYear
    2011
  • fDate
    28-30 Jan. 2011
  • Firstpage
    1
  • Lastpage
    7
  • Abstract
    Reconfigurable Field Programmable Gate Arrays (rFPGAs) are employed extensively in spacecraft electronic systems to implement low-power adaptable systems that provide high density functionality. A challenge that must be tackled during system design is their high susceptibility to radiation induced Single Event Upsets (SEUs). A burst of energized particles may cause extensive damage to circuits. Even if their presence is transient, SEU faults may cause a permanent failure when they afflict the configuration memory - SRAM. There are two ways in which timely detection of faults and timely action to circumvent them can be undertaken - (i) Online error detecting/correcting circuits that demand a high premium in terms of FPGA area for extending error-security and Fault Tolerance, thus increasing cost and redundancy, and (ii) Built-in Self-Test (BIST) that allows efficient and very high-coverage fault detection but the fault testing is performed off-line. In general, Reliability and Availability (R&A) is a crucial quality parameter. In this paper, we present a state model that schedules Self-tests judiciously to optimize availability while ensuring a high degree of reliability. The aim of system design is to determine an optimal value of the mean time to self testing λT so that faults are detected on time and are reconfigured to boost system availability.
  • Keywords
    SRAM chips; avionics; built-in self test; fault tolerance; field programmable gate arrays; integrated circuit design; integrated circuit reliability; integrated circuit testing; low-power electronics; space vehicle electronics; space vehicles; BIST; SEU fault; SRAM; built-in self-test; circuit damage; configuration memory; error-security; fault detection; fault testing; fault tolerance; high density functionality; low-power adaptable system; online error correcting circuit; online error detecting circuit; quality parameter; rFPGA; radiation susceptibility; reconfigurable field programmable gate array; reliability-and-availability; scheduling; single event upsets; space application; spacecraft electronic system; state model; system availability; system design; transient fault; Automatic testing; Availability; Built-in self-test; Circuit faults; Field programmable gate arrays; Maintenance engineering; Noise measurement; Built-in Self-Test (BIST); Fault Tolerance (FT); Field Programmable Gate Arrays (FPGA); Single Event Upsets (SEUs); Triple Modular Redundancy (TMR);
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Electronics (IICPE), 2010 India International Conference on
  • Conference_Location
    New Delhi
  • Print_ISBN
    978-1-4244-7883-5
  • Type

    conf

  • DOI
    10.1109/IICPE.2011.5728146
  • Filename
    5728146