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Design of New Aircraft Sensor Bus System

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Practical Applications of Intelligent Systems

Part of the book series: Advances in Intelligent and Soft Computing ((AINSC,volume 124))

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Abstract

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.

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References

  1. NI Company Measurement Studio LabWindows\CVI Instrument Driver Developers Guide (2001)

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  2. TI Company P82B96_Developer Reference Manual (2005)

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  3. TI Company P82B96 Dual bidirectional bus buffer Reference Manual (2007)

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  4. AME Company “AME8510 Reference Manual” (2006)

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  5. NI Company “LabWindows\CVI programmer Reference Manual” (2001), http://www.ni.com/pdf/manuals/323643a.pdf

  6. “LabWindows\CVI 8.5”, NI instruments Corporation (2008)

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Author information

Authors and Affiliations

  1. School of Aerospace Engineering, Beijing Institute of Technology, No.5, Zhongguancun Nandajie Haidian District, Beijing, 100081, P.R. China

    Ke Gao, Bo Mo & Hongying Wang

Authors
  1. Ke Gao
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  2. Bo Mo
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  3. Hongying Wang
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Editor information

Editors and Affiliations

  1. Department of Computer Science and Engineering, Shanghai Jiao Tong University, 800 Dongchuan Road, 200240, Shanghai, China

    Yinglin Wang

  2. School of Information Science and Technology, Southwest Jiaotong University, 610031, Chengdu, Sichuan Province, China

    Tianrui Li

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© 2011 Springer-Verlag Berlin Heidelberg

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Cite this paper

Gao, K., Mo, B., Wang, H. (2011). Design of New Aircraft Sensor Bus System. In: Wang, Y., Li, T. (eds) Practical Applications of Intelligent Systems. Advances in Intelligent and Soft Computing, vol 124. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-25658-5_30

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  • DOI: https://doi.org/10.1007/978-3-642-25658-5_30

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-25657-8

  • Online ISBN: 978-3-642-25658-5

  • eBook Packages: EngineeringEngineering (R0)

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