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Erschienen in:
2012 | OriginalPaper | Buchkapitel
Design of New Aircraft Sensor Bus System
verfasst von : Ke Gao, Bo Mo, Hongying Wang
Erschienen in: Practical Applications of Intelligent Systems
Verlag: Springer Berlin Heidelberg
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Traditional aircraft sensor system requires a lot of cables and volume for each sensor’s connection. It can not meet the rapid development of modern information technology requirements of aircraft. Future aircraft sensor system requires less cables and more speed. This paper proposed a new design of digital aircraft sensor bus. It combines the I2C with SOC technology. It’s also designed to be a modular structure in order to increase or decrease additional functional module when additional features in need. In this paper, a fully functional prototype of aircraft sensor bus and an upper PC system was designed. Corresponding test software based on LabWindows\CVI is written in order to actually test the efficiency of the prototype. The following test result verified the original design.