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面向批量化平板卫星布局优化设计

罗卓伟 曹强 刘正山 帅智康 彭也伦 朱艳阳

航天器工程2026,Vol.35Issue(1):52-62,11.
航天器工程2026,Vol.35Issue(1):52-62,11.DOI:10.3969/j.issn.1673-8748.2026.01.007

面向批量化平板卫星布局优化设计

Layout Optimization Design for Mass Produced Flat-panel Satellites

罗卓伟 1曹强 1刘正山 2帅智康 3彭也伦 3朱艳阳3

作者信息

  • 1. 中国星网易联供应链有限公司,河北雄安新区 071708
  • 2. 中国航天科技集团商业卫星有限公司,北京 100090
  • 3. 湖南大学,长沙 410082
  • 折叠

摘要

Abstract

To meet the requirements of low-cost and high-efficiency constellation deployment,flat-panel satellite configurations have gradually emerged as the mainstream architecture for next-gen-eration mass-produced satellites owing to their compact form structural advantages that facilitate stacked launch.To address the challenges of layout design for flat-panel satellites under mass production conditions,a system modeling and optimization method focused on assembly consis-tency and multi-objective optimization is proposed.First,the modular design characteristics are analyzed to identify key influencing factors such as geometry,thermal control,power supply,and interface constraints.Subsequently,a two-dimensional layout modeling framework that sup-ports optimization is established,incorporating layout region modeling,parameter modeling,wiring topology modeling,and thermal priority modeling.On this basis,a multi-objective heu-ristic optimization procedure is implemented to generate and evaluate typical motherboard layout schemes.Finally,simulation experiments are conducted to verify the effectiveness of the pro-posed model in terms of wiring length reduction,thermal control path optimization,and system-level coordination enhancement.The results demonstrate that the proposed method enables intel-ligent layout design with high reusability and strong constraint adaptability,thereby providing feasible support for the batch assembly and automated design of flat-panel satellites.

关键词

平板卫星/模块布局/批量制造

Key words

flat-panel satellite/module layout/mass production

分类

航空航天

引用本文复制引用

罗卓伟,曹强,刘正山,帅智康,彭也伦,朱艳阳..面向批量化平板卫星布局优化设计[J].航天器工程,2026,35(1):52-62,11.

航天器工程

1673-8748

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