舱内低功耗无线传感网络系统设计
DOI:
作者:
作者单位:

1.中北大学 电子测试技术国家重点实验室,山西太原 030051; 2.中北大学 仪器科学与动态测试教育部重点实验室,山西太原 030051

作者简介:

通讯作者:

中图分类号:

TN98

基金项目:

微纳传感器信号无线引出及测量仪器研制(2018YFB0003)


Design of Low-power Wireless Sensor Network System in Cabin
Author:
Affiliation:

1.National Key Laboratory for Electronic Measurement Technology,North University of China,Taiyuan 030051,China; 2.Key Laboratory of Instrument Science & Dynamic Measurement of Ministry of Education,North University of China,Taiyuan 030051,China

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    在火箭参数测量系统中,传统的传感网络使用电缆进行连接,随着测试点的增加,大量缆线的使用不仅带来了多余的负载和功耗,而且还占用了大量的舱内空间,为火箭舱内其他设备的布局和安装造成巨大的困扰。针对上述问题,提出了一种基于CC1310的无线传感网络(WSN)设计方案,实现测试系统无缆化。该设计选用通信频段低于1GHz(Sub-GHz)的超低功耗射频芯片CC1310作为传感网络控制器,使用低功耗的K型热电偶AD8495实现温度数据的采集,使用锂电池为传感器节点供电。软件设计实现了传感器节点周期性休眠和唤醒侦听机制,主节点轮询访问传感器节点获取状态和数据的功能,完成了传感器节点低功耗设计并且数据的可靠性可以得到保证。经试验测试,该系统设计合理,具有功耗低、数据传输稳定可靠等显著特点,且系统在组网后工作状态平均能耗为88μA,可实现火箭舱内环境参数的进行长期测量。

    Abstract:

    In the launch vehicle parameter measurement system, the traditional sensor network is connected by cables. With the increase of test points, the use of a large number of cables not only brings excess load and power consumption, but also takes up a lot of cabin space , causing huge trouble for the layout and installation of other equipment in the rocket cabin. In response to the above problems, we propose a CC1310-based wireless sensor network (WSN) design scheme to realize the cableless test system. In this design, the ultra-low-power RF chip CC1310 with a communication frequency band below 1GHz (Sub-GHz) is selected as the sensor network controller, the low-power K-type thermocouple AD8495 is used to collect temperature data, and the lithium battery is used for power supply. The software design implements the periodic sleep and wake-up listening mechanism of sensor nodes, and the master node polls and accesses sensor nodes to obtain the function of status and data. The node low power consumption design is completed and the reliability of the data can be guaranteed. The experimental test shows that the system has a reasonable design, low power consumption, stable and reliable data transmission, and the average energy consumption of the system in working state is 88μA, which can realize long-term measurement of environmental parameters in the rocket cabin.

    参考文献
    相似文献
    引证文献
引用本文

马游春,李晋芳,李超杰,叶思楠.舱内低功耗无线传感网络系统设计[J].电子测量技术,2022,45(11):109-113

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2024-04-25
  • 出版日期: