DocumentCode
2653760
Title
Developing a stable architecture for interfacing aircraft to commercial personal computers
Author
Christenson, D.W.
Author_Institution
Software Eng. Div., Ogden Air Logistics Center, Hill AFB, UT
fYear
2000
fDate
2000
Firstpage
559
Lastpage
563
Abstract
The focus of this paper is the concept of utilizing commercial PC products and interfacing them to military and commercial aircraft. The problem of the life cycle of the different products is examined from multiple viewpoints. Existing products are described, architecture for each implementation is derived and their strengths and weaknesses are explored. Finally, an attempt to define the root causes for the problem of implementation of interface architectures in this environment are presented. A new developmental architecture is introduced. This architecture is designed to maintain the strengths of the traditional architectures and eliminate some of the weaknesses and inefficiencies. A series of hardware/software co-development projects is described to demonstrate the new architecture. The relative performance of the architecture has been evaluated and refined by multiple implementations. These are described and future implementations examined
Keywords
aircraft computers; computer interfaces; microcomputer applications; military aircraft; military avionics; commercial PC products; commercial aircraft; commercial personal computers; developmental architecture; hardware/software co-development projects; interface architectures; military aircraft; product life cycle; stable architecture; Aircraft propulsion; Computer architecture; Computer interfaces; Costs; Embedded computing; Microcomputers; Military aircraft; Military standards; Personal communication networks; Weapons;
fLanguage
English
Publisher
ieee
Conference_Titel
AUTOTESTCON Proceedings, 2000 IEEE
Conference_Location
Anaheim, CA
ISSN
1080-7725
Print_ISBN
0-7803-5868-6
Type
conf
DOI
10.1109/AUTEST.2000.885640
Filename
885640
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