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A Design of New Airborne Integrated Alarm System

Received: 12 March 2019     Published: 15 June 2019
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Abstract

Aiming at the fault alarm requirement of a certain type of aircraft, a new type of airborne integrated alarm system is designed. The system adopts modular design idea, and the acquisition part is composed of multi-slice shift register 54HC165 cascade, which can reduce the number of control pins; the main control part uses the heterogeneous processing scheme of DSP and FPGA, which not only ensures the real-time processing of information, but also enriches the interactive ability of the interface; the output part uses a single FPGA to control the alarm lamp box, giving full play to the system advantages of centralized alarm and hierarchical processing. potential. Ground debugging experiments show that the system can accurately judge the aircraft warning information, and quickly notify the pilot according to the degree of emergency. The scheme is simple to implement, and the interface is scalable, so it has high practical value with strong portability and expansibility.

Published in Journal of Electrical and Electronic Engineering (Volume 7, Issue 2)
DOI 10.11648/j.jeee.20190702.16
Page(s) 64-68
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2019. Published by Science Publishing Group

Keywords

Airborne, Alarm System, Modular Design, Hierarchical Process

References
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  • APA Style

    Jianhua Li, Jintao Xie, Xun Li, Chaogang Hu. (2019). A Design of New Airborne Integrated Alarm System. Journal of Electrical and Electronic Engineering, 7(2), 64-68. https://doi.org/10.11648/j.jeee.20190702.16

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    ACS Style

    Jianhua Li; Jintao Xie; Xun Li; Chaogang Hu. A Design of New Airborne Integrated Alarm System. J. Electr. Electron. Eng. 2019, 7(2), 64-68. doi: 10.11648/j.jeee.20190702.16

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    AMA Style

    Jianhua Li, Jintao Xie, Xun Li, Chaogang Hu. A Design of New Airborne Integrated Alarm System. J Electr Electron Eng. 2019;7(2):64-68. doi: 10.11648/j.jeee.20190702.16

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  • @article{10.11648/j.jeee.20190702.16,
      author = {Jianhua Li and Jintao Xie and Xun Li and Chaogang Hu},
      title = {A Design of New Airborne Integrated Alarm System},
      journal = {Journal of Electrical and Electronic Engineering},
      volume = {7},
      number = {2},
      pages = {64-68},
      doi = {10.11648/j.jeee.20190702.16},
      url = {https://doi.org/10.11648/j.jeee.20190702.16},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.jeee.20190702.16},
      abstract = {Aiming at the fault alarm requirement of a certain type of aircraft, a new type of airborne integrated alarm system is designed. The system adopts modular design idea, and the acquisition part is composed of multi-slice shift register 54HC165 cascade, which can reduce the number of control pins; the main control part uses the heterogeneous processing scheme of DSP and FPGA, which not only ensures the real-time processing of information, but also enriches the interactive ability of the interface; the output part uses a single FPGA to control the alarm lamp box, giving full play to the system advantages of centralized alarm and hierarchical processing. potential. Ground debugging experiments show that the system can accurately judge the aircraft warning information, and quickly notify the pilot according to the degree of emergency. The scheme is simple to implement, and the interface is scalable, so it has high practical value with strong portability and expansibility.},
     year = {2019}
    }
    

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  • TY  - JOUR
    T1  - A Design of New Airborne Integrated Alarm System
    AU  - Jianhua Li
    AU  - Jintao Xie
    AU  - Xun Li
    AU  - Chaogang Hu
    Y1  - 2019/06/15
    PY  - 2019
    N1  - https://doi.org/10.11648/j.jeee.20190702.16
    DO  - 10.11648/j.jeee.20190702.16
    T2  - Journal of Electrical and Electronic Engineering
    JF  - Journal of Electrical and Electronic Engineering
    JO  - Journal of Electrical and Electronic Engineering
    SP  - 64
    EP  - 68
    PB  - Science Publishing Group
    SN  - 2329-1605
    UR  - https://doi.org/10.11648/j.jeee.20190702.16
    AB  - Aiming at the fault alarm requirement of a certain type of aircraft, a new type of airborne integrated alarm system is designed. The system adopts modular design idea, and the acquisition part is composed of multi-slice shift register 54HC165 cascade, which can reduce the number of control pins; the main control part uses the heterogeneous processing scheme of DSP and FPGA, which not only ensures the real-time processing of information, but also enriches the interactive ability of the interface; the output part uses a single FPGA to control the alarm lamp box, giving full play to the system advantages of centralized alarm and hierarchical processing. potential. Ground debugging experiments show that the system can accurately judge the aircraft warning information, and quickly notify the pilot according to the degree of emergency. The scheme is simple to implement, and the interface is scalable, so it has high practical value with strong portability and expansibility.
    VL  - 7
    IS  - 2
    ER  - 

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Author Information
  • Jiangxi Hongdu Aviation Industry Group Co., Ltd, Nanchang, China

  • Jiangxi Hongdu Aviation Industry Group Co., Ltd, Nanchang, China

  • Jiangxi Hongdu Aviation Industry Group Co., Ltd, Nanchang, China

  • Jiangxi Hongdu Aviation Industry Group Co., Ltd, Nanchang, China

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