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亚太6E卫星全自主飞行设计与实现

安然 王珏 王敏 魏强 彭坤 侯卫国 成艳 安秀枝

航天器工程2025,Vol.34Issue(1):38-43,6.
航天器工程2025,Vol.34Issue(1):38-43,6.DOI:10.3969/j.issn.1673-8748.2025.01.007

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

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
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摘要

Abstract

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 manage-ment architecture.All flight tasks of the satellite after takeoff of the rocket are divided into dif-ferent 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,provi-ding 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

Key words

APSTAR-6E satellite/fully autonomous flight/all-electric propulsion/autonomous orbit transfer

引用本文复制引用

安然,王珏,王敏,魏强,彭坤,侯卫国,成艳,安秀枝..亚太6E卫星全自主飞行设计与实现[J].航天器工程,2025,34(1):38-43,6.

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OA北大核心

1673-8748

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