DocumentCode
2351235
Title
A Double or Triple Module Redundancy Model Exploiting Dynamic Reconfigurations
Author
Shinohara, Kouji ; Watanabe, Minoru
Author_Institution
Shizuoka Univ., Shizuoka
fYear
2008
fDate
22-25 June 2008
Firstpage
114
Lastpage
121
Abstract
Majority voting is a commonly used approach to increase system reliability. Standard triple-module-redundancy (TMR) methods are frequently used in space applications. Using these methods, triple modules and voting circuits are implemented onto an application specific integrated circuit (ASIC) or an FPGA. When a single event upset occurs, the voting circuit neglects the failure value of a module receiving the single event upset and takes a correct value of the other two modules not receiving it. However, the triple-module implementation requires a large implementation area on VLSIs. Therefore, to reduce the area of TMR implementation, this paper presents a novel double or triple module redundancy (DTMR) method for dynamically reconfigurable devices using a design example of a state machine. Furthermore, this paper presents experimental results of the method using a highly reliable optically reconfigurable gate array.
Keywords
application specific integrated circuits; avionics; field programmable gate arrays; space vehicle electronics; ASIC; FPGA; application specific integrated circuit; double-triple module redundancy; dynamic reconfigurations; module redundancy model; reconfigurable gate arrays; space applications; state machine; system reliability; triple-module implementation; triple-module-redundancy methods; voting circuits; Application specific integrated circuits; Field programmable gate arrays; Holographic optical components; Holography; Optical arrays; Redundancy; Single event upset; Vertical cavity surface emitting lasers; Very large scale integration; Voting;
fLanguage
English
Publisher
ieee
Conference_Titel
Adaptive Hardware and Systems, 2008. AHS '08. NASA/ESA Conference on
Conference_Location
Noordwijk
Print_ISBN
978-0-7695-3166-3
Type
conf
DOI
10.1109/AHS.2008.67
Filename
4584263
Link To Document