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Issue No.10 - October (1983 vol.32)
pp: 911-922
A. Pedar , Systems Engineering Division, National Aeronautical Laboratory
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.
shared resources computing system, Architecture optimization, computation reliability, fault-tolerant computing, replicated resources computing system
A. Pedar, V.V.S. Sarma, "Architecture Optimization of Aerospace Computing Systems", IEEE Transactions on Computers, vol.32, no. 10, pp. 911-922, October 1983, doi:10.1109/TC.1983.1676135
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