DocumentCode
2568014
Title
A versatile input interface for avionic computers
Author
Canu, Antoine ; Faura, David ; Toillon, Patrice ; Gatti, Marc ; Benabes, Philippe
Author_Institution
Comput. Competence Center, Thales Avionics, Meudon-la-Foret, France
fYear
2011
fDate
16-20 Oct. 2011
Abstract
During the last decades, the Integrated Modular Avionics (IMA) concept has allowed important cost- savings in the development of avionic equipment thanks to an important reduction of the number of different modules. However, modularity in avionics is still limited by hardware concerns: current avionic computers have to interface with a lot of different inputs or outputs, from environment sensing to inter- computer communications, and the applications which can be hosted on the computer directly depends on these inputs and outputs. In this paper, we propose a new concept of input interface, named versatile input interface, which could facilitate the design and reuse of avionic equipment by allowing more flexibility in the development of Input/Output boards. The versatile input interface is meant to be used in avionic environment, and therefore will comply with avionic environmental procedures such as DO160-F [1].
Keywords
aerospace computing; avionics; user interfaces; IMA concept; avionic computers; avionic environment procedure; avionic equipment; input-output boards; integrated modular avionic concept; intercomputer communications; versatile input interface; Aerospace electronics; Aircraft; Aircraft manufacture; Computers; Fluctuations; Impedance; Noise;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference (DASC), 2011 IEEE/AIAA 30th
Conference_Location
Seattle, WA
ISSN
2155-7195
Print_ISBN
978-1-61284-797-9
Type
conf
DOI
10.1109/DASC.2011.6096114
Filename
6096114
Link To Document