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

  • Ke Gao*
  • , Bo Mo
  • , Jin Lin
  • *此作品的通讯作者
  • Beijing Institute of Technology

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

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.

源语言英语
主期刊名Practical Applications of Intelligent Systems
主期刊副标题Proceedings of the Sixth International Conference on Intelligent Systems and Knowledge Engineering, Shanghai, China, Dec 2011 (ISKE2011)
编辑Yinglin Wang, Tianrui Li
513-521
页数9
DOI
出版状态已出版 - 2011

出版系列

姓名Advances in Intelligent and Soft Computing
124
ISSN(印刷版)1867-5662

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