DocumentCode
1711553
Title
System control for fault-tolerant avionics architectures
Author
Benning, Stephen L.
Author_Institution
Wright Lab., Wright-Patterson AFB, OH, USA
fYear
1992
Firstpage
219
Lastpage
224
Abstract
The real-time, multitasking and multiple processor configurations required for avionics systems have been examined in detail with respect to implementation in Ada to understand the problems associated with these configurations. A key element in this architecture is the software, specifically the operating system which runs as the core software element in the system. The author examines such a real-time operating system, the Ada Avionics Real-Time Software (AARTS) Operating System (AOS), developed for the Wright Laboratory (WL). Development concerns, integration issues, and testing results are discussed. The AARTS Program met its program objectives. It was demonstrated that Ada could indeed support fault-tolerant operation of an operational flight program on a distributed network of VHSIC (very high speed integrated circuit) processors
Keywords
Ada; aerospace computing; aircraft instrumentation; fault tolerant computing; microprocessor chips; multiprocessing systems; operating systems (computers); real-time systems; Ada; VHSIC; Wright Laboratory; distributed network; fault-tolerant avionics architectures; multiple processor configurations; multitasking; operational flight program; real-time; software development; system control; testing; very high speed integrated circuit; Aerospace electronics; Circuit testing; Computer architecture; Control systems; Fault tolerant systems; Multitasking; Operating systems; Real time systems; Software systems; Very high speed integrated circuits;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1992. Proceedings., IEEE/AIAA 11th
Conference_Location
Seattle, WA
Print_ISBN
0-7803-0820-4
Type
conf
DOI
10.1109/DASC.1992.282153
Filename
282153
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