DocumentCode :
2593059
Title :
Modular Avionics System Architecture (MASA)-the impact of fault tolerance
Author :
Brock, Larry D. ; Schor, Andrei L.
Author_Institution :
Charles Stark Draper Lab. Inc., Cambridge, MA, USA
fYear :
1990
fDate :
15-18 Oct 1990
Firstpage :
310
Lastpage :
315
Abstract :
The Air Force Modular Avionics System Architecture (MASA) program is defining how the advantages of modular avionics can be applied to upgrades of current aircraft. Life cycle cost (LCC) studies performed for the MASA program showed significant savings when a modular architecture was used to integrate at least two or three avionics functions. These studies also showed no significant LCC penalty for the modular implementation of a single function. Other advantages not quantified in the LCC analysis include increased competition, reduced time lag for technology insertion, and more effective implementation of integrated systems and fault tolerance. Some of the more interesting results were for fault-tolerant modular systems which could provide a high probability of full operational capability for a 30-day combat surge with no line maintenance
Keywords :
aerospace computing; computer architecture; fault tolerant computing; military computing; military systems; probability; Air Force; Modular Avionics System Architecture; avionics functions; combat surge; fault tolerance; life cycle cost; modular architecture; modular avionics; operational capability; probability; reduced time lag; technology insertion; Aerospace electronics; Cost function; Fault tolerance; Fault tolerant systems; Helicopters; Information analysis; Laboratories; Measurement standards; Military aircraft; Surges;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
Conference_Location :
Virginia Beach, VA
Type :
conf
DOI :
10.1109/DASC.1990.111306
Filename :
111306
Link To Document :
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