NASA NTRS · 19730043019
Highly reliable processor system for space application.
Abstract
Description of a redundant processor organization which can be implemented with off-the-shelf processors for fault-tolerant operation. Reconfiguration can be performed automatically in a transientless manner. To support this system configuration and redundancy management concept, an operating system referred to as a synchronous executive has been designed. This system is directed at real-time closed-loop space applications where minimum response time, no degradation of software solution, and system simplicity are of importance. The system is based on a multicomputer organization with each machine solving the same problem based on a common set of inputs. Processor status is fed to a higher-level device which selects a controlling processor for controlling outputs and monitoring computers for fault detection.
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Tsou, H. S. E., Daly, T. E., Swearingen, C. N.. 1973-04-01. Highly reliable processor system for space application.. https://ntrs.nasa.gov/citations/19730043019
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