DocumentCode :
871694
Title :
Low Power Error Correction Architecture for Space
Author :
Maier, R.J.
Author_Institution :
Air Force Weapons Lab Kirtland AFB NM 87117
Volume :
30
Issue :
6
fYear :
1983
Firstpage :
4333
Lastpage :
4338
Abstract :
Massively redundant fault-tolerant methods, such as triple modular redundancy require enormously more weight and power than the nonfault-tolerant system and solve only one reliability problem. This paper will show that three reliability problems, random bit flips, error bursts and hard failures can be solved for less than 25 percent more power and 50-100 percent more parts using error detection codes and powered-down spares with repeated execution on detection of error.
Keywords :
Circuit faults; Costs; Error correction; Error correction codes; Fault tolerance; Fault tolerant systems; Power system reliability; Redundancy; Single event upset; Space vehicles;
fLanguage :
English
Journal_Title :
Nuclear Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9499
Type :
jour
DOI :
10.1109/TNS.1983.4333133
Filename :
4333133
Link To Document :
بازگشت