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基于在轨可维修性的载人航天器配电系统设计

杜占超 陈丹 任亮 姜文彩 王志莹

航天器工程2018,Vol.27Issue(6):56-62,7.
航天器工程2018,Vol.27Issue(6):56-62,7.DOI:10.3969/j.issn.1673-8748.2018.06.008

基于在轨可维修性的载人航天器配电系统设计

Design of Manned Spacecraft Power Distribution System Based on In-orbit Maintainability

杜占超 1陈丹 1任亮 2姜文彩 1王志莹1

作者信息

  • 1. 中国空间技术研究院载人航天总体部,北京 100094
  • 2. 北京卫星制造厂有限公司,北京 100094
  • 折叠

摘要

Abstract

Distribution power system is the transmission network of electrical power on manned spacecraft, and it has high failure severity.On the basis of fault mode analysis, the reasonable design of the telemetry point and control point can realize its in-orbit maintenance, which can improve the reliability and lifetime of the manned spacecraft significantly.A fundamental unit of manned spacecraft distribution system is taken as an example to achieve in-orbit maintenance.The topology of the fundamental unit is designed in detail, including fault diagnosis, fault isolation and system reconstruction, maintenance process and security design, and the reliability of the designed is analyzed.The design proposed in the paper can optimize the design of manned spacecraft from the point of view of systems engineering and can plan the platform resources in advance, so as to realize the balance between the maintainability of power distribution system and the use of platform resources.The topology and design in the paper can be used for reference in the design of the in-orbit maintainability for manned spacecraft power distribution system.

关键词

载人航天器配电系统/在轨可维修性/基本单元拓扑结构/配电器

Key words

manned spacecraft power distribution system/in-orbit maintainability/topology of fundamental unit/distributor

分类

航空航天

引用本文复制引用

杜占超,陈丹,任亮,姜文彩,王志莹..基于在轨可维修性的载人航天器配电系统设计[J].航天器工程,2018,27(6):56-62,7.

基金项目

国家重大科技专项工程 ()

航天器工程

OA北大核心CSCDCSTPCD

1673-8748

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