Pedar, A. ; Sarma, V. V. S. (1983) Architecture optimization of aerospace computing systems IEEE Transactions on Computers, 32 (10). pp. 911-922. ISSN 0018-9340
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Official URL: http://www.computer.org/portal/web/csdl/doi/10.110...
Related URL: http://dx.doi.org/10.1109/TC.1983.1676135
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 model is used for the evaluation of the instruction execution rate of a degradable, replicated resources computing system such as a modular multiprocessor 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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Source: | Copyright of this article belongs to IEEE. |
ID Code: | 61399 |
Deposited On: | 15 Sep 2011 03:36 |
Last Modified: | 15 Sep 2011 03:36 |
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