Design and implementation of low cost aircraft control bus system upon I2C

Ke Gao*, Bo Mo, Jin Lin

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Citations (Scopus)

Abstract

With the development of microelectronic technology, the quantity of electronic devices in aircraft is expanding at an exponential rate. But the traditional control buses on aircraft are not portable or scalable. It is an important problem to modern aircraft design to connect numbers of digital electronic devices within one bus. In this paper, we propose a new design of aircraft control bus which has characteristics like high-speed, small-size, highly-reliability, more-scalable etc. The following test of the prototype validates the design. This new aircraft control bus is very suitable for aircraft systems which require compact size, flexible configurations and highly reliability.

Original languageEnglish
Title of host publicationPractical Applications of Intelligent Systems
Subtitle of host publicationProceedings of the Sixth International Conference on Intelligent Systems and Knowledge Engineering, Shanghai, China, Dec 2011 (ISKE2011)
EditorsYinglin Wang, Tianrui Li
Pages513-521
Number of pages9
DOIs
Publication statusPublished - 2011

Publication series

NameAdvances in Intelligent and Soft Computing
Volume124
ISSN (Print)1867-5662

Keywords

  • I2C SOC FPGA Control Bus IP Core

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