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Advanced information processing systemDesign and performance details of the advanced information processing system (AIPS) for fault and damage tolerant data processing on aircraft and spacecraft are presented. AIPS comprises several computers distributed throughout the vehicle and linked by a damage tolerant data bus. Most I/O functions are available to all the computers, which run in a TDMA mode. Each computer performs separate specific tasks in normal operation and assumes other tasks in degraded modes. Redundant software assures that all fault monitoring, logging and reporting are automated, together with control functions. Redundant duplex links and damage-spread limitation provide the fault tolerance. Details of an advanced design of a laboratory-scale proof-of-concept system are described, including functional operations.
Document ID
19850035681
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lala, J. H.
(Charles Stark Draper Laboratory, Inc. Cambridge, MA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Computer Systems
Report/Patent Number
AIAA PAPER 84-2644
Meeting Information
Meeting: Digital Avionics Systems Conference
Location: Baltimore, MD
Start Date: December 3, 1984
End Date: December 6, 1984
Accession Number
85A17832
Funding Number(s)
CONTRACT_GRANT: NAS9-16023
CONTRACT_GRANT: NASA TASK 84-18
Distribution Limits
Public
Copyright
Other

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