Pedar, A and Sarma, VVS (1980) Fault-tolerant computing concepts for aerospace applications - A survey. Indian Academy of Sciences, Proceedings (Engineering Sciences), 3. pp. 89-128.
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Abstract
Fault-tolerant computing systems for aerospace applications are discussed with a view toward fault classification, figures of merit, fault-tolerant architectures, coverage estimation, and automated methods of reliability evaluation. The combined performance and reliability of a system are examined, and the configuration optimization of a gracefully degradable computing system is analyzed. Current research in the design, analysis and validation of FTC systems is surveyed with attention to fault-tolerant software techniques. It is noted that the present hardware technology is equipped with all the capabilities necessary to build the required fault-tolerance into digital computing systems
Item Type: | Article |
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Additional Information: | Copyright for this article belongs to Indian Academy of Sciences |
Uncontrolled Keywords: | Computation;Aerospace;Reliability;Aircraft components; Aerial surveys;Digital computers;Optimization;Computer programs;Construction;Degradation;Architecture; Classification;Figure of merit;Design engineering; Automation;Airborne/spaceborne computers;Computer design; Computer systems performance;Digital systems |
Subjects: | MATHEMATICAL AND COMPUTER SCIENCES > Computer Operations and Hardware ASTRONAUTICS > Spacecraft Design, Testing and Performance |
Depositing User: | Ms. Alphones Mary |
Date Deposited: | 13 Dec 2005 |
Last Modified: | 24 May 2010 04:09 |
URI: | http://nal-ir.nal.res.in/id/eprint/897 |
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