亚太6E卫星全自主飞行设计与实现  

Design and Implementation of Fully Autonomous Flight for APSTAR-6E Satellite

作　　者：安然[1] 王珏[1] 王敏[1] 魏强[1] 彭坤[1] 侯卫国[1] 成艳[1] 安秀枝 AN Ran;WANG Jue;WANG Min;WEI Qiang;PENG Kun;HOU Weiguo;CHENG Yan;AN Xiuzhi(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38-43,共6页Spacecraft Engineering

摘　　要：亚太6E卫星全自主飞行设计遵循高性能、高效率、高性价比的设计理念,构建飞行任务管理架构,将卫星自火箭起飞后的所有飞行任务划分为不同的飞行阶段,设计数十个程控事件,并进行程控功能、循环判定功能设计。全自主飞行设计减少了卫星对地面测控系统的依赖,具备更强自主飞行能力,首次实现了我国卫星全寿命周期自主飞行。文章介绍的全自主飞行设计,对全电推进卫星及自主运行卫星具有借鉴意义。The fully autonomous flight design of APSTAR-6E satellite follows the design concept of high performance,high efficiency and high cost-effectiveness,constructs a flight task management architecture.All flight tasks of the satellite after takeoff of the rocket are divided into different flight stages and dozens of programmable events are designed.In addition,programmable functions and cycle judgment functions are designed.The fully autonomous flight design reduces the satellite dependence on ground TT&C(telemetry,tracking and command)systems,providing stronger autonomous flight capabilities and achieving China’s first autonomous flight throughout satellite entire lifecycle.The fully autonomous flight design introduced in this paper has the reference significance for all-electric propulsion satellites and autonomous operation satellites.

关 键 词：亚太6E卫星 全自主飞行 全电推进 自主变轨 

分 类 号：V474.2[航空宇航科学与技术—飞行器设计]