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Highly reliable processor system for space application.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.
Document ID
19730043019
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tsou, H. S. E.
Daly, T. E.
(TRW Systems Group Redondo Beach, Calif., United States)
Swearingen, C. N.
(NASA Marshall Space Flight Center Astrionics Laboratory, Huntsville, Ala., United States)
Date Acquired
August 7, 2013
Publication Date
April 1, 1973
Subject Category
Computers
Report/Patent Number
AIAA PAPER 73-424
Report Number: AIAA PAPER 73-424
Meeting Information
Meeting: Computer Network Systems Conference
Location: Huntsville, AL
Start Date: April 16, 1973
End Date: April 18, 1973
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
73A27821
Distribution Limits
Public
Copyright
Other

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