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多板式星载SAR天线展开机构装配误差建模与分析

余精汉 侯鹏 马海龙 刘俊杰

航天器环境工程2025,Vol.42Issue(6):650-659,10.
航天器环境工程2025,Vol.42Issue(6):650-659,10.DOI:10.12126/see.2025030

多板式星载SAR天线展开机构装配误差建模与分析

Modeling and analysis of assembly errors in a multi-panel SAR antenna deployment mechanism

余精汉 1侯鹏 2马海龙 3刘俊杰1

作者信息

  • 1. 上海卫星装备研究所
  • 2. 上海卫星装备研究所||上海交通大学 机械与动力工程学院:上海 200240
  • 3. 上海卫星装备研究所||南京航空航天大学 航天学院,南京 211106
  • 折叠

摘要

Abstract

To address the challenge of controlling assembly accuracy due to the coupled transmission of multiple errors in multi-panel synthetic aperture radar(SAR)antenna deployment mechanisms,a modular error modeling approach was proposed.The complex deployment structure was decomposed into functional modules—hinges,rods,and panels—based on series-parallel mechanism principles.Parametric assembly error models for each module were established using the closed-loop vector method.By linearly superimposing the error-transfer functions of the modules,the pose errors of the antenna panels were mapped to global geometric-tolerance sources,enabling the prediction of geometric accuracy in statically indeterminate rod systems.Partial differential methods were further employed to quantify the sensitivity coefficients of individual error sources.Assembly and adjustment tests on a 22 m×3 m antenna yielded a pointing accuracy better than 0.012°.The results demonstrate that the method provides a systematic theoretical tool for the digital assembly,adjustment,and tolerance optimization of SAR antennas,effectively enhancing on-orbit deployment accuracy and imaging performance.

关键词

SAR天线机构/串并联耦合/闭环矢量法/装配误差建模/灵敏度分析

Key words

SAR antenna mechanism/series-parallel coupling/closed-loop vector method/assembly error modeling/sensitivity analysis

分类

机械制造

引用本文复制引用

余精汉,侯鹏,马海龙,刘俊杰..多板式星载SAR天线展开机构装配误差建模与分析[J].航天器环境工程,2025,42(6):650-659,10.

基金项目

国防基础科学研究计划项目 ()

航天器环境工程

1673-1379

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