Small aircraft avionics using hybrid data bus technology

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

doi:10.1109/MAES.2006.1684279

Small aircraft avionics using hybrid data bus technology

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

Research output: Contribution to journal › Article › peer-review

5 Citations (Scopus)

Abstract

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.

Original language	English
Article number	1684279
Pages (from-to)	17-21
Number of pages	5
Journal	IEEE Aerospace and Electronic Systems Magazine
Volume	21
Issue number	7
DOIs	https://doi.org/10.1109/MAES.2006.1684279
Publication status	Published - 2006 Jul 1

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Space and Planetary Science
Electrical and Electronic Engineering

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10.1109/MAES.2006.1684279

Cite this

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title = "Small aircraft avionics using hybrid data bus technology",

abstract = "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.",

author = "Lin, {Chin E.} and Tai, {S. F.} and Li, {C. C.} and Lin, {H. T.} and Chen, {T. P.}",

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AU - Lin, Chin E.

AU - Tai, S. F.

AU - Li, C. C.

AU - Lin, H. T.

AU - Chen, T. P.

PY - 2006/7/1

Y1 - 2006/7/1

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AB - 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.

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Small aircraft avionics using hybrid data bus technology

Abstract

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