Construction of hybrid data transfer interface system with implementation of small aircraft flight instruments

Chin-E. Lin, S. F. Tai, C. C. Li, T. P. Chen, Hui-Tang Lin, P. K. Chang

Research output: Contribution to journalArticle

Abstract

This paper presents a digital avionics system implementation for small aircraft. Avionics system is one of the most important systems to all kinds of aircraft. For digital avionics system integration, a hybrid data bus technology for small aircraft is developed in Avionics Laboratory. The proposed hybrid data transfer interface (HDTI) 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 transfer interface 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 design will bring in new era of digital avionics for small aircrafts.

Original languageEnglish
Pages (from-to)49-56
Number of pages8
JournalHangkong Taikong ji Minhang Xuekan/Journal of Aeronautics, Astronautics and Aviation
Volume38 A
Issue number1
Publication statusPublished - 2006 Mar 1

Fingerprint

flight instruments
avionics
Digital avionics
Data transfer
aircraft
flight
Aircraft
Avionics
cockpits
mobile communication
systems integration
information systems
low altitude
surveillance
Information systems
systems engineering
Systems analysis
controllers
information system
Controllers

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

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abstract = "This paper presents a digital avionics system implementation for small aircraft. Avionics system is one of the most important systems to all kinds of aircraft. For digital avionics system integration, a hybrid data bus technology for small aircraft is developed in Avionics Laboratory. The proposed hybrid data transfer interface (HDTI) 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 transfer interface 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 design will bring in new era of digital avionics for small aircrafts.",
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Construction of hybrid data transfer interface system with implementation of small aircraft flight instruments. / Lin, Chin-E.; Tai, S. F.; Li, C. C.; Chen, T. P.; Lin, Hui-Tang; Chang, P. K.

In: Hangkong Taikong ji Minhang Xuekan/Journal of Aeronautics, Astronautics and Aviation, Vol. 38 A, No. 1, 01.03.2006, p. 49-56.

Research output: Contribution to journalArticle

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