航天器工程2025，Vol.34Issue(1)：75-80,6.DOI:10.3969/j.issn.1673-8748.2025.01.013
亚太6E卫星智能化综合电子分系统设计与验证
Design and Verification of Intelligent Integrated Electronic Subsystem for APSTAR-6E Satellite
成艳 1乐浪 1潘宇倩 1徐楠 1熊晓将 1宫江雷 1刘士暄 1王珏1
作者信息
- 1. 中国空间技术研究院通信与导航卫星总体部,北京 100094
- 折叠
摘要
Abstract
In response to the problems of low integration level of satellite integrated electronic sub-system,large number of devices,large volume,high functional coupling between various de-vices,and low level of autonomous intelligence in orbit in the past.A highly reliable,integrated hardware design and satellite autonomous task management and planning method is proposed in this paper.Through the in orbit verification of the APSTAR-6E satellite,the results show that the integrated electronic subsystem has the advantages of high modularity of hardware,good sta-bility of system,high degree of software autonomy and high in orbit application efficiency.It can quickly and flexibly respond to future market mission requirements and provide reference for the design of integrated electronic subsystem for light weight and fully autonomous satellites in orbit.关键词
亚太6E卫星/综合电子分系统/高集成/小型化/全自主飞行Key words
APSTAR-6E satellite/integrated electronic subsystem/high-integration/miniaturiza-tion/fully autonomous flight分类
航空航天引用本文复制引用
成艳,乐浪,潘宇倩,徐楠,熊晓将,宫江雷,刘士暄,王珏..亚太6E卫星智能化综合电子分系统设计与验证[J].航天器工程,2025,34(1):75-80,6.
