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Information Technology Journal

Year: 2012 | Volume: 11 | Issue: 4 | Page No.: 563-565
DOI: 10.3923/itj.2012.563.565

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Research Article

The Design for Airborne Electronic Equipment Fault Diagnostic System Base on IPC

Cheng Weng
Aviation automation institute, Civil Aviation University of China, Tianjin, China

With the rapid development of science and technology, modern aviation equipment increases its functionality, while, its structure becomes more and more complex, the speed and reliability requirements are increasing also. The study introduces the design for airborne electronic equipment fault diagnostic system based on IPC, containing the design about the hardware and software, as well as function and task.
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How to cite this article

Cheng Weng, 2012. The Design for Airborne Electronic Equipment Fault Diagnostic System Base on IPC. Information Technology Journal, 11: 563-565.

DOI: 10.3923/itj.2012.563.565

URL: https://scialert.net/abstract/?doi=itj.2012.563.565

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References


  1. Lord, D.H. and D. Gleason, 1981. Design and evaluation methodology for built-in test. IEEE Trans. Reliab., 30: 222-226.
    CrossRefDirect Link

  2. Shao, J.J. and L.R. Lamberson, 1988. Impact of BIT design parameterson systems RAM. Reliab. Eng. Syst. Saf., 23: 219-246.

  3. Chen, P. and H.C. Xu, 2002. Avionics BIT review. China Shipping, 6: 108-110.

Keywords


  • IPC
  • diagnostic system
  • Airborne electronic equipment
  • BIT

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