摘要
随着微小卫星技术的提高,高功能密度、低成本并且能够快速研制的微小卫星已经成为现代航天领域的研究热点之一。但传统的微小卫星电子系统集成度较低,板间连线复杂,可靠性较低,质量、体积、功耗和性能等多方面需求相互制约,逐渐不能满足微小卫星发展的需求。微小卫星星载综合电子系统的提出,实现了其在体积、质量有限的情况下,可靠性、功耗和性能等方面的全面提高。在微小卫星综合电子系统发展历程和研究现状的基础上,分析了微小卫星综合电子系统在通用化和柔性化设计中应用的关键技术,并总结其目前的挑战和未来的发展趋势。
With the improvement of microsatellite technology,microsatellites with high functional density,low cost and rapid development have become research hotspots in the modern aerospace field.However,the traditional electronic system in the microsatellite is low in integration.The wiring between boards is complicated and the reliability is low.Due to the mutual constraints on quality,volume,power consumption,and performance,it is gradually unable to meet the development requirements of microsatellites.The proposed onboard integrated electronic system for microsatellites has achieved an overall improvement in reliability,power consumption and performance under the condition of limited size and quality.This article describes the development history and research status of the integrated electronic system of microsatellites.Then,it analyzes the key technologies applied in the general and flexible design of the integrated electronic system of micro-satellites.Finally,it summarizes current challenges and future development trend.
作者
彭宇
孙树志
姚博文
崔秀海
刘连胜
Peng Yu;Sun Shuzhi;Yao Bowen;Cui Xiuhai;Liu Liansheng(Harbin Institute of Technology,Harbin 150080,China)
出处
《电子测量与仪器学报》
CSCD
北大核心
2021年第8期1-11,共11页
Journal of Electronic Measurement and Instrumentation
关键词
微小卫星
星载综合电子系统
通用化
柔性化
microsatellite
onboard integrated electronic system
universal
flexible