卫星系统网络节点的智能化设计

董立珉; 刘源; 徐国栋; 李鹏飞

doi:10.3788/OPE.20132104.1086

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卫星系统网络节点的智能化设计

信息科学 | 更新时间：2020-08-12

- 卫星系统网络节点的智能化设计
- Intelligent Design of Satellite Network Nodes
- 光学精密工程 2013年21卷第4期页码：1086-1095
- 作者机构：
  
  哈尔滨工业大学航天学院卫星技术研究所
- 作者简介：
- 基金信息：
  
  国家自然科学基金资助项目(No.91023049);中国博士后科学基金资助项目(2015M582113)
- DOI：10.3788/OPE.20132104.1086
  中图分类号： TP273;V474.1
- 收稿日期：2012-08-23，
  
  修回日期：2012-11-02，
  
  网络出版日期：2013-04-20，
  
  纸质出版日期：2013-04-15
- 稿件说明：
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董立珉刘源徐国栋李鹏飞. 卫星系统网络节点的智能化设计[J]. 光学精密工程, 2013,21(4): 1086-1095

DONG Li-Min LIU Yuan XU Guo-dong LI Peng-Fei. Intelligent Design of Satellite Network Nodes[J]. Editorial Office of Optics and Precision Engineering, 2013,21(4): 1086-1095
董立珉刘源徐国栋李鹏飞. 卫星系统网络节点的智能化设计[J]. 光学精密工程, 2013,21(4): 1086-1095 DOI： 10.3788/OPE.20132104.1086.

DONG Li-Min LIU Yuan XU Guo-dong LI Peng-Fei. Intelligent Design of Satellite Network Nodes[J]. Editorial Office of Optics and Precision Engineering, 2013,21(4): 1086-1095 DOI： 10.3788/OPE.20132104.1086.

摘要

为了提高卫星系统的控制精度，解决系统故障检测与故障处理问题，进行了卫星节点智能化设计。以嵌入式SOC处理器为基础，建立了智能化网络节点的体系结构，将其划分为自诊断及上位机辅助单元、智能电源管理单元、标准化接口单元和基本功能单元等4个部分。采用过采样技术和数据融合处理技术提高了自诊断及上位机辅助单元的数据采集精度，采用直接冗余检测和知识检测方法实现了数据纠错功能，采用自断电/加电技术实现了智能电源管理功能，基于标准无线接口设计实现了接口标准化功能。最后，在太阳矢量测量仪原理样机上对所设计的智能化网络节点进行了功能验证。结果表明：智能化太阳矢量测量仪测量精度可达0.01，高于传统太阳敏感器的采集精度0.1；实现了状态自检、测量数据校验及标准接口功能，提高了卫星系统的可靠性。设计的网络节点可进行自主故障检测及处理，具备自断电/加电功能，能够针对空间环境带来的翻转及锁定进行自主处理，支持单机设备的即插即用，可实现卫星系统的快速测试、快速集成和快速装配。

Abstract

The intelligent design of a satellite network node was implemented to improve the control accuracy of a satellite system and to solve the problems of fault detection and trouble processing. The system structure of the intelligent network node was established based on an embedded SOC processor. The node was divided into four parts: the diagnosis and On Board Computer(OBC) auxiliary unit

intelligent power management unit

standardization interface unit and the basic function unit. Then

oversampling technology and data fusion processing technology were used to improve the accuracy of the data collection in the diagnosis and OBC auxiliary unit

and the testing error correction method based on redundant detection or direct knowledge was used correct the data errors. In the intelligent power management unit

the self on/off circuit technology was implemented to improve the reliability. Moreover

the wireless standard interface design was adopted in the standardization interface unit. Finally

an experiment was perfornced on a principle prototype of the sun vector measuring instrument to validate the design of intelligent network node. The experimental results show that the accuracy of the sun vector measuring instrument has reached 0.01

far higher than the traditional accuracy of 0.1 . It realizes the state self-inspection calibration

measurement data auto-calibration and the standard interface function and improves the reliability of the system. The network node can finish the fault detection and treatment by itself and can realize the self on/off circuit function. It deals with the space environment from the flip and locking autotono-mously and allows the plug for the single equipment. Furthermore

the node supports quick test

rapid integration and rapid assembly of the satellite systems.

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references

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