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Availability Analysis of Xilinx FPGA on Orbit Nozomu Nishinaga National Institute of Information and Communications Technology Masayoshi Yoneda – PowerPoint PPT presentation

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Title: No. 1


1
Availability Analysis of Xilinx FPGA on Orbit
  • Nozomu Nishinaga
  • National Institute of Information and
    Communications Technology
  • Masayoshi Yoneda
  • NEC TOSHIBA Space Systems, Ltd.

2
Outline
  • Motivation
  • Heavy Ion test results of Virtex II pro
  • Availability analysis
  • Conclusion

3
Motivation
  • Very high availability or low non-availability is
    required for the consumer communications
    equipment.
  • typical non-availability value for terrestrial
    network equipment is 10E-6
  • If the SEU can be defined as an accidental
    failure and the failure can be fixed without any
    loss of the original device function.
  • the rebooting process also can be defined as a
    repairing
  • Does equimpment with S-RAM type FPGAs meet the
    non-availability criteria?

4
Radiation test of Virtex II Pro
  • Virtex II pro (XC2VP7-5FG456 and XC2VP4)
  • Test carried out in November 2003 and February
    2004 at TIARA in Takasaki, Japan
  • Heavy Ions (N, Ne, and Kr)
  • Result compared with that of Virtex II. (Gary
    Swift, Candice Yui, and Carl Carmichael,
    Single-Event Upset Susceptibility Testing of the
    Xilinx Virtex II FPGA, MAPLD2002, paper P29)

5
Devices Under Testing
XC2VP4 XC2VP7 XC2VP100
Configuration Memory 3.01 Mbit 4.49 Mbit 34.29 Mbit
DCM (Digital Clock Manager) 4 unit 4 unit 12 unit
Block RAM 28 unit 44 unit 7992 kbit
F/F 6016 unit 9856 unit 9856 unit
Multiplier 28 unit 44 unit 44 unit
Rocket I/O 4 Block 8 Block 8 Block
6
Radiation test result (1)
  • Block RAM region

0.000001
0.0000001
1E-08
Cross Section cm2/bit
1E-09
1E-10
1E-11
0
10
20
30
40
50
60
70
LETMev cm2/mg
7
Radiation test result (2)
  • Configuration Memory region

8
SEU frequency analysis (CREAM 96)
XC2VP4
Solar MAX Flare Peak (1 week)
Conf. Memory 0.33 times/day 163.4 times/day
DCM 0.00 times/day 0.11 times/day
Block RAM 0.04 times/day 21.87 times/day
Multiplier 0.00 times/day 0.46 times/day
XC2VP7
Solar MAX Flare Peak (1 week)
Conf. Memory 0.49 times/day 243.8 times/day
DCM 0.00 times/day 0.11 times/day
Block RAM 0.07 times/day 34.4 times/day
Multiplier 0.00 times/day 0.72 times/day
9
Mean Time Before Failure Analysis
XC2VP4 XC2VP4 XC2VP7 XC2VP7 XC2VP100 (Simulated) XC2VP100 (Simulated)
Solar MAX (Sec.) Flare Peak (1 week) (Sec.) Solar MAX (Sec.) Flare Peak (1 week) (Sec.) Solar MAX (Sec.) Flare Peak (1 week) (Sec.)
Conf. Memory 2.64E05 5.29E02 1.77E05 3.55E02 2.32E04 4.64E01
DCM 4.14E08 8.09E05 4.14E08 8.09E05 1.38E08 2. 70E05
Block RAM 2.02E06 3.95E03 1.28E06 2.51E03 1.27E05 2.49E02
Multipliers 7.89E07 1.89E05 5.02E07 1.21E05 4.98E06 1.19E04

SYSTEM 2.3267E05 4.6495E02 1.5501E05 3.0972E02 1.95E04 3.90E01
  • If the SEU can be considered as A Failure, the
    MTTR is roughly proportional to the size.
  • System MTBF -gt Harmonic Mean of all functional
    blocks
  • Assumption 1 All the SEUs can be detected.
  • Assumption 2 All the gates are used.
  • Assumption 3 All the SEUs must be repaired as
    soon as quickly

10
Mean Time To Repair (MTTR)
XC2VP4 XC2VP7 XC2VP100
Configuration data (bit) 3,006,560 4,485,472 34,292,832
MTTR (s) (10Mbyte/s) 0.037582 0.056068 0.42866
MTTR (s) (50Mbyte/s) 0.007516 0.011214 0.085732
  • REBOOT Repair
  • The effects of SEU are volatile.
  • By loading the correct configuration data, the
    operation mode will go to the normal mode.
  • Rebooting time -gt Repair time
  • The maximum data rate for loading is fixed 50M
    byte/Sec. for XC2VP series.
  • The larger gate size or configuration size, the
    longer MTTR becomes necessary.

11
Triple Module Redundancy
  • Case 1 One out of Three system failure is
    acceptable.
  • Loose regulation
  • Acceptable when the MTBF is quite large compared
    with MTTR
  • Case 2 NO failure is acceptable
  • Tight configuration
  • The output is always guaranteed.

12
Non-Availability Alalysis
Case 1 XC2VP4 XC2VP4 XC2VP7 XC2VP7 XC2VP100 (Simulated) XC2VP100 (Simulated)
Case 1 Solar MAX Flare Peak Solar MAX Flare Peak Solar MAX Flare Peak
10Mbyte/s 7.83E-14 1.96E-08 3.93E-13 9.83E-08 1.45E-09 3.53E-04
50Mbyte/s 3.13E-15 7.84E-10 1.57E-14 3.93E-09 5.79E-11 1.44E-05
Case 2 XC2VP4 XC2VP4 XC2VP7 XC2VP7 XC2VP100 (Simulated) XC2VP100 (Simulated)
Case 2 Solar MAX Flare Peak Solar MAX Flare Peak Solar MAX Flare Peak
10Mbyte/s 4.85E-07 2.42E-04 1.09E-06 5.43E-04 6.59E-05 3.23E-02
50Mbyte/s 9.69E-08 4.85E-05 2.17E-07 1.09E-04 1.32E-05 6.57E-03
  • MTBF is proportional to the area of the die and
    MTTR is also proportional. -gt Large FPGA has
    disadvantage.
  • Large size FPGA does not meet the criteria 10e-6
  • How to mitigate? divide small FPGAs
  • Much larger down load rate will be needed (50 M
    Byte/S is too slow)

13
Dividing
  • The Non-Availability depends on the size
  • A Large size FPGA is split up to several (D)
    small FPGAs
  • Sc-gt Configuration data size bits
  • R -gt Configuration rate bps

14
Interstage VOTER
  • The availability is varying With or Without the
    interstage Voter.
  • The performance with interstage voters is
    superior to tat without the voters.

15
Non-Availability Analysis with dividing
  • Area or gate loss due to the division is not
    taking into account in this figure. -gt next issue

16
Conclusion
  • Non availability analysis for Vertex II pro
  • Large scaled FPGA do not meet a non availability
    criteria for communication equipment (10e-6).
  • Need much faster or wider Interface for
    configuration to enhance its availability.
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