Pedar, A and Sarma, VVS (1983) Architecture optimization of aerospace computing systems. IEEE Transactions on computers, C32 (10). pp. 911-922.
Full text not available from this repository.Abstract
Simultaneous consideration of both performance and reliability issues is important in the choice of computer architectures for real-time aerospace applications.One of the requirements for such a fault-tolerant computer system is the characteristic of graceful degradation.A shared and replicated resources computing system represents such an architecture.In this paper, a combinatorial models used for the evaluation of the instruction execution rate of a degradable, replicated resources computing system such as a modular multi processor system. Next a method is presented to evaluate the computation reliability of such a system utilizing a reliability graph model and the instruction execution rate.Finally, this computation reliability measure, Which simultaneously describes both performance and reliability, is applied as a constraint in an architecture optimization model for such computing systems.
Item Type: | Article |
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Uncontrolled Keywords: | Architecture;Aerospace computing system |
Subjects: | MATHEMATICAL AND COMPUTER SCIENCES > Computer Operations and Hardware MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software |
Depositing User: | M/S ICAST NAL |
Date Deposited: | 06 Aug 2008 |
Last Modified: | 24 May 2010 04:26 |
URI: | http://nal-ir.nal.res.in/id/eprint/4865 |
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