DocumentCode
2270494
Title
Developing a stable architecture for interfacing aircraft to commercial personal computers
Author
Silver, Lynn ; Christenson, D.W.
Author_Institution
Software Eng. Div., Ogden Air Logistics Center, Hill AFB, UT, USA
fYear
2003
fDate
22-25 Sept. 2003
Firstpage
95
Lastpage
99
Abstract
The intent of this paper is to introduce an entirely new and exciting adventure in software and hardware in which the concept of commercial PC products are utilized to interface with military and commercial aircraft. The life cycle problem 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 is 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 are 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 testing; computer interfaces; hardware-software codesign; microcomputers; military aircraft; commercial PC/aircraft interface; hardware/software co-development; military aircraft; stable interface architecture; Aircraft propulsion; Computer architecture; Computer interfaces; Costs; Hardware; Microcomputers; Military aircraft; Military standards; Personal communication networks; Weapons;
fLanguage
English
Publisher
ieee
Conference_Titel
AUTOTESTCON 2003. IEEE Systems Readiness Technology Conference. Proceedings
ISSN
1080-7725
Print_ISBN
0-7803-7837-7
Type
conf
DOI
10.1109/AUTEST.2003.1243560
Filename
1243560
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