Name
Abstract | ||
|---|---|---|
This paper describes the implementation of aCPU which can operate successfully in hostileenvironments such as an orbiting space vehicle.The design goal is to reduce sensitivity to theeffects of radiation which can cause malfunctions inelectronic circuit or a complete failure of thesystem.Moreover, to test performance and collect data,special hardware structures are integrated onsilicon to collect data on detected errors. |
Year | DOI | Venue |
|---|---|---|
2004 | 10.1109/DELTA.2004.10082 | DELTA |
Keywords | DocType | ISBN |
complete failure,space vehicles,special hardware structure,slow control,seu protected cpu,malfunctions inelectronic circuit,integrated onsilicon,orbiting space vehicle,design goal | Conference | 0-7695-2081-2 |
Citations | PageRank | References |
1 | 0.43 | 2 |
Authors | ||
7 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| Andrea S. Brogna | 1 | 1 | 1.11 |
| Franco Bigongiari | 2 | 12 | 6.29 |
| Fabrizio Bertuccelli | 3 | 1 | 0.77 |
| Walter Errico | 4 | 1 | 0.43 |
| Simone Giovannetti | 5 | 2 | 0.81 |
| Egidio Pescari | 6 | 1 | 0.43 |
| Roberto Saletti | 7 | 86 | 20.89 |