Small aircraft avionics using hybrid data bus technology

Chin E. Lin, S. F. Tai, C. C. Li, H. T. Lin, T. P. Chen

研究成果: Article

4 引文 斯高帕斯(Scopus)

摘要

This paper presents a recent study of avionics system design and implementation for small aircraft. Avionics systems is one of the most important systems to all kinds of aircraft. For digital avionics system integration, a hybrid data bus is proposed in this development. The proposed hybrid data bus (HDB) adopts some characteristics from time trigger protocol (TTP) in conjunction with the controller area node (CAN) to simplify the data bus structure and enhance system reliability in the applications. The proposed hybrid data bus system is designed and fabricated for test as a preliminary solution. In addition to data bus system, a virtual flight instrument with geodetic information system (GIS) is integrated into cockpit display together with mobile communication surveillance for low altitude flight The overall system integration will bring in a new era of digital avionics for small aircrafts.

原文English
文章編號1684279
頁(從 - 到)17-21
頁數5
期刊IEEE Aerospace and Electronic Systems Magazine
21
發行號7
DOIs
出版狀態Published - 2006 七月 1

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science
  • Electrical and Electronic Engineering

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    Lin, C. E., Tai, S. F., Li, C. C., Lin, H. T., & Chen, T. P. (2006). Small aircraft avionics using hybrid data bus technology. IEEE Aerospace and Electronic Systems Magazine, 21(7), 17-21. [1684279]. https://doi.org/10.1109/MAES.2006.1684279