A new approach to the organization of a reliable aerospace computer system is described in this paper. The organization is based on the use of a multithreading design in which a multiplicity of paths are available, any of which can perform the minimum data processing functions. The combination of all of the multithreading paths comprises a total data processing system which is capable of handling more than the minimum task for which the highest reliability is required. This approach utilizes active redundancy to provide a higher capability for more extensive data processing tasks during that period in which no failures have occurred. Optimum utilization of system weight is achieved through use of a minimum of inactive redundant hardware.
Multithreading Design of a Reliable Aerospace Computer
IEEE Transactions on Aerospace and Electronic Systems ; AES-2 , 6 ; 147-158
1966-11-01
1746160 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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