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

作　　者：成艳[1] 乐浪[1] 潘宇倩[1] 徐楠[1] 熊晓将[1] 宫江雷[1] 刘士暄 王珏[1] CHENG Yan;LE Lang;PAN Yuqian;XU Nan;XIONG Xiaojiang;GONG Jianglei;LIU Shixuan;WANG Jue(Institute of Telecommunication and Navigation Satellites,China Academy of Space Technology,Beijing 100094,China)

机构地区：[1]中国空间技术研究院通信与导航卫星总体部,北京100094

出　　处：《航天器工程》2025年第1期75-80,共6页Spacecraft Engineering

摘　　要：针对以往卫星综合电子分系统集成化程度不高,设备数量多、体积庞大、各设备间功能耦合度高以及在轨自主智能化水平不高的问题,文章提出了一种高可靠、高集成化的硬件设计和卫星全自主任务管理与规划设计方法。经亚太6E卫星在轨验证,结果表明:综合电子分系统硬件模块化程度高、系统稳定性好、软件自主程度高,卫星在轨应用效能高等优点,能快速灵活响应未来市场任务需求,可以为轻小型化、在轨全自主运行卫星综合电子分系统设计提供参考。In response to the problems of low integration level of satellite integrated electronic subsystem,large number of devices,large volume,high functional coupling between various devices,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 stability 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 

分 类 号：V57[航空宇航科学与技术—航空宇航推进理论与工程]