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 language | English |
|---|---|
| Pages (from-to) | 49-56 |
| Number of pages | 8 |
| Journal | Hangkong Taikong ji Minhang Xuekan/Journal of Aeronautics, Astronautics and Aviation |
| Volume | 38 A |
| Issue number | 1 |
| Publication status | Published - 2006 Mar 1 |
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All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science
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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 journal › Article
TY - JOUR
T1 - Construction of hybrid data transfer interface system with implementation of small aircraft flight instruments
AU - Lin, Chin-E.
AU - Tai, S. F.
AU - Li, C. C.
AU - Chen, T. P.
AU - Lin, Hui-Tang
AU - Chang, P. K.
PY - 2006/3/1
Y1 - 2006/3/1
N2 - 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.
AB - 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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UR - http://www.scopus.com/inward/citedby.url?scp=33745968799&partnerID=8YFLogxK
M3 - Article
AN - SCOPUS:33745968799
VL - 38 A
SP - 49
EP - 56
JO - Zhongguo Hangkong Taikong Xuehui Huikan/Transactions of the Aeronautical and Astronautical Society of the Republic of China
JF - Zhongguo Hangkong Taikong Xuehui Huikan/Transactions of the Aeronautical and Astronautical Society of the Republic of China
SN - 1022-0666
IS - 1
ER -