Design of ultrareliable computer for air- and rocket-borne data-acquisition systems

Citation
Aa. Avakyan et al., Design of ultrareliable computer for air- and rocket-borne data-acquisition systems, MEAS TECH R, 43(7), 2000, pp. 572-577
Citations number
4
Categorie Soggetti
Instrumentation & Measurement
Journal title
MEASUREMENT TECHNIQUES
ISSN journal
05431972 → ACNP
Volume
43
Issue
7
Year of publication
2000
Pages
572 - 577
Database
ISI
SICI code
0543-1972(200007)43:7<572:DOUCFA>2.0.ZU;2-T
Abstract
A fail-safe computer with a systolic processor as the majority element is p roposed. The processor consists of arrays of monobit processors. High relia bility is achieved by triple redundancy.