微纳卫星高性能综合电子系统设计

冯田雨; 陈健

doi:10.37188/OPE.20202809.2056

您当前的位置：

首页 >

文章列表页 >

微纳卫星高性能综合电子系统设计

微纳技术与精密机械 | 更新时间：2020-09-28

- 微纳卫星高性能综合电子系统设计
- Design and implementation of high performance reconfigurable integrated electronic system for micro/nano-satellite
- 光学精密工程 2020年28卷第9期页码：2056-2064
- 作者机构：
  
  哈尔滨工业大学航天学院卫星技术研究所, 黑龙江哈尔滨 150001
- 作者简介：
  
  [ "冯田雨(1991-), 男, 河南许昌人, 博士研究生, 2014年于哈尔滨工业大学获得学士学位, 2016年于哈尔滨工程大学获得硕士学位, 主要从事航天器系统工程及软件控制方面的研究。E-mail:rainyuoko@163.com" ]
- 基金信息：
  
  国家重点研发计划资助项目(2016YFB0500901)
- DOI：10.37188/OPE.20202809.2056
  中图分类号： TP394.1;TH691.9
- 收稿日期：2020-03-24，
  
  修回日期：2020-05-26，
  
  录用日期：2020-5-26，
  
  纸质出版日期：2020-09-25
- 稿件说明：
移动端阅览
冯田雨, 陈健. 微纳卫星高性能综合电子系统设计[J]. 光学精密工程, 2020,28(9):2056-2064.

Tian-yu FENG, Jian CHEN. Design and implementation of high performance reconfigurable integrated electronic system for micro/nano-satellite[J]. Optics and precision engineering, 2020, 28(9): 2056-2064.
冯田雨, 陈健. 微纳卫星高性能综合电子系统设计[J]. 光学精密工程, 2020,28(9):2056-2064. DOI： 10.37188/OPE.20202809.2056.

Tian-yu FENG, Jian CHEN. Design and implementation of high performance reconfigurable integrated electronic system for micro/nano-satellite[J]. Optics and precision engineering, 2020, 28(9): 2056-2064. DOI： 10.37188/OPE.20202809.2056.

摘要

为了提高卫星星上资源利用率及集成度，实现对卫星星上资源的充分利用，综合考虑体积、质量及功耗等多方面限制及要求，提出一套基于可重构系统的微纳卫星综合电子系统方案。该方案提出利用分布式专用模块及通用中心处理器提高卫星系统功能集成度，在不降低整星系统可靠性的基础上减少电路设计冗余。首先，通过选用双高性能CPU冷备份，配合外部电路设计，实现了高可靠性高性能计算功能；其次，通过标准化系统总线，将电源及热控，姿态轨道控制，载荷管理等功能模块中的专用电路与计算处理控制功能解耦，将其中的计算控制功能通过综合电子CPU软件重构的方式实现；最后设计并研制了一台功能样机，重量约为0.2 kg，功耗小于2 W，系统计算能力大于220 DMIPS，具备双CPU冷备份功能，满足微纳卫星低功耗较高可靠性的要求，同时该样机可通过通用系统总线扩展不同功能，实现在各种微纳卫星中的应用。

Abstract

To improve the level of integration and maximize the use of on-board resources by considering the size

mass

and power consumption

a set of integrated electronic system based on reconfigurable software is proposed. By using a distributed functional module and a generic processor

high level of integration

less redundancy

and high function density are achieved without reducing reliability. First

a high computing capability is realized using a high-performance processor with a cold backup processor and an external circuit design. The standardized communication bus among the systems helps in decoupling the dedicated circuits and the general computing and control circuits in the electric power system

altitude and orbit control system

and other systems. Computing and control are achieved using reconfigurable modular software that runs in the main processor. Finally

a test prototype is designed and tested. The prototype consumes less than 2 W of power

achieves computing capability of more than 220 Dhrystone million instructions per second

and fits in a single CubeSat sized printed circuit board that weighs less than 0.2 kg

which satisfies the requirements of high reliability

low power consumption

and ability for expansion needed by micro/nanosatellites. By adding different functions through the system bus

this system can also satisfy other satellite requirements.

关键词

Keywords

references

石荣 , 张伟 . 研发微纳电子侦察卫星面临的挑战与思考 . 航天电子对抗 , 2015 . 31 ( 4 ): 1 - 5 . http://www.cqvip.com/QK/91418X/201504/665919280.html http://www.cqvip.com/QK/91418X/201504/665919280.html .

R SHI , W ZHANG . Challenge and pondering on the development of micro-nano electronic reconnaissance satellite . Aerospace Electronic Warfare , 2015 . 31 ( 4 ): 1 - 5 . http://www.cqvip.com/QK/91418X/201504/665919280.html http://www.cqvip.com/QK/91418X/201504/665919280.html .

张科科 , 朱振才 , 夏磊 . 小卫星模块化设计技术分析 . 航天器工程 , 2015 . 24 ( 6 ): 107 - 115 . DOI: 10.3969/j.issn.1673-8748.2015.06.016 http://doi.org/10.3969/j.issn.1673-8748.2015.06.016 .

K K ZHANG , ZH C ZHU , L XIA . Analysis of small satellite modular design technology . Spacecraft Engineering , 2015 . 24 ( 6 ): 107 - 115 . DOI: 10.3969/j.issn.1673-8748.2015.06.016 http://doi.org/10.3969/j.issn.1673-8748.2015.06.016 .

宫颖 , 潘腾 , 杜洁 . 低轨遥感卫星长寿命设计研究 . 质量与可靠性 , 2018 . ( 5 ): 27 - 30 .

Y GONG , T PAN , J DU . Research on long-life design of LEO remote sensing satellite . Quality and Reliability , 2018 . ( 5 ): 27 - 30 .

张景楠 , 李华旺 , 朱野 . 微小卫星星务分系统的硬件设计与实现 . 电子设计工程 , 2014 . 22 ( 15 ): 177 - 179 .

J N ZHANG , H W LI , Y ZHU . The hardware design and realization of micro satellite's house keeping system . Electronic Design Engineering , 2014 . 22 ( 15 ): 177 - 179 .

T NARUMI , S TAKANO , S KIMURA . Development of high-performance compact on-board computer for micro/nano-satellites with software resource sharing framework . SICE Journal of Control, Measurement, and System Integration , 2017 . 10 ( 1 ): 10 - 15 .

王连国.高性能一体化空间综合电子技术研究[D].北京: 中国科学院大学(中国科学院国家空间科学中心), 2019.

WANG L G. Research on High Performance Integrated Aerospace Electronic Technology [D]. Beijing: University of Chinese Academy of Sciences (National Center for Space Science, Chinese Academy of Sciences), 2019. (in Chinese)

陈雯雯 , 刘洋 , 高海云 , 等 . 微纳卫星陀螺阵列系统信息融合 . 光学精密工程 , 2019 . 27 ( 1 ): 172 - 180 . http://ope.lightpublishing.cn/thesisDetails?columnId=1424903&Fpath=&index=-1&l=zh http://ope.lightpublishing.cn/thesisDetails?columnId=1424903&Fpath=&index=-1&l=zh .

W W CHEN , Y LIU , H Y GAO , 等 . Signal fusion of silicon micro-gyroscope array of micro/nano satellite . Opt. Precision Eng. , 2019 . 27 ( 1 ): 172 - 180 . http://ope.lightpublishing.cn/thesisDetails?columnId=1424903&Fpath=&index=-1&l=zh http://ope.lightpublishing.cn/thesisDetails?columnId=1424903&Fpath=&index=-1&l=zh .

赵琳 , 王艺鹏 , 郝勇 . 在轨飞轮故障诊断混合框架设计 . 光学精密工程 , 2018 . 26 ( 7 ): 1728 - 1740 . http://ope.lightpublishing.cn/thesisDetails?columnId=1420615&Fpath=&index=-1&l=zh http://ope.lightpublishing.cn/thesisDetails?columnId=1420615&Fpath=&index=-1&l=zh .

L ZHAO , Y P WANG , Y HAO . Design of hybrid frame for on-orbit flywheel fault diagnosis . Opt. Precision Eng. , 2018 . 26 ( 7 ): 1728 - 1740 . http://ope.lightpublishing.cn/thesisDetails?columnId=1420615&Fpath=&index=-1&l=zh http://ope.lightpublishing.cn/thesisDetails?columnId=1420615&Fpath=&index=-1&l=zh .

袁春柱 , 李志刚 , 李军予 , 等 . 微纳卫星COTS器件应用研究 . 计算机测量与控制 , 2017 . 25 ( 2 ): 156 - 159+163 . http://www.cnki.com.cn/Article/CJFDTOTAL-JZCK201702043.htm http://www.cnki.com.cn/Article/CJFDTOTAL-JZCK201702043.htm .

CH ZH YUAN , ZH G LI , J Y LI , 等 . Study on COTS component for micro/nano satellite application . Computer Measurement and Control , 2017 . 25 ( 2 ): 156 - 159+163 . http://www.cnki.com.cn/Article/CJFDTOTAL-JZCK201702043.htm http://www.cnki.com.cn/Article/CJFDTOTAL-JZCK201702043.htm .

宋丹 , 杜刚 , 田贺祥 . 容错设计在微纳卫星上的应用 . 中国航天 , 2007 . ( 12 ): 16 - 18 . http://www.cnki.com.cn/Article/CJFDTotal-ZGHT200712006.htm http://www.cnki.com.cn/Article/CJFDTotal-ZGHT200712006.htm .

D SONG , G DU , H X TIAN . Application of fault-tolerant design on micro and nano satellites . Aerospace China , 2007 . ( 12 ): 16 - 18 . http://www.cnki.com.cn/Article/CJFDTotal-ZGHT200712006.htm http://www.cnki.com.cn/Article/CJFDTotal-ZGHT200712006.htm .

刘凯俊 , 彭攀 , 王新元 . 基于COTS器件的高费效比商业卫星计算机研究 . 计算机测量与控制 , 2018 . 26 ( 11 ): 213 - 217 . http://www.cqvip.com/QK/97801A/201811/7000933741.html http://www.cqvip.com/QK/97801A/201811/7000933741.html .

K J LIU , P PENG , X Y WANG . Research on cost-effective commercial satellite computer based on COTS devices . Computer Measurement and Control , 2018 . 26 ( 11 ): 213 - 217 . http://www.cqvip.com/QK/97801A/201811/7000933741.html http://www.cqvip.com/QK/97801A/201811/7000933741.html .

黄佳 , 陈夏 , 李宗德 . 基于软件定义的微纳卫星综合电子设计与实现 . 现代电子技术 , 2019 . 42 ( 2 ): 30 - 32+40 .

J HUANG , X CHEN , Z D LI . Design and realization of micro/nano-satellite synthesized electronic system based on software definition . Modern Electronics Technique , 2019 . 42 ( 2 ): 30 - 32+40 .

浏览量

576

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

九自由度超冗余机械臂的设计和测试