This paper covers mainly five sections of ARINC 629 physical layer technology. The first three will give an introduction with an historical overview, leading from aeronautical data bus systems in general to the ARINC 629 development. The impact of new avionic architectures such as IMA (integrated modular avionic), ACR (avionic computing resource) and RDC (remote data concentrator), which are creating new data bus requirements will be discussed-considering the ARINC 629 solution in particular. European activities in this area are also mentioned here. In the fourth section, the current status of the B 777 technology is mentioned briefly and the European view on ARINC 629 CP technology is covered in more detail. The fifth section covers physical layer development with a special view on current mode coupling methods. Also, possible alternatives to the present solution will be investigated from technical and economical viewpoints, and the problem areas and advantages of individual solutions will be shown. This will lead to directions for probable solutions in the near future.
ARINC 629 data bus physical layer technology
1997
8 Seiten, 3 Quellen
Aufsatz (Konferenz)
Englisch
ARINC 629 data bus physical layer technology
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