| 注册
首页|期刊导航|中国空间科学技术|基于分割法的抛物面固面天线热变形抑制

基于分割法的抛物面固面天线热变形抑制

楼春钢 李昊 潘殿坤

中国空间科学技术2024,Vol.44Issue(2):59-67,9.
中国空间科学技术2024,Vol.44Issue(2):59-67,9.DOI:10.16708/j.cnki.1000-758X.2024.0022

基于分割法的抛物面固面天线热变形抑制

Thermal deformation suppression of parabolic solid antenna based on the segmentation method

楼春钢 1李昊 2潘殿坤1

作者信息

  • 1. 宁波大学冲击与安全工程教育部重点实验室,宁波 315211
  • 2. 上海卫星工程研究所,上海 201109
  • 折叠

摘要

Abstract

To meet the demands of large-aperture,high surface accuracy of deployable antennas for high-resolution microwave remote sensing spacecraft in the future,a novel method called segmented method was proposed,which can effectively reduce the surface error caused by thermal deformation of the solid partial feed antenna in orbit.A parabolic solid partial feed antenna with a 5m aperture was employed,and then the effect of thermal deformation on the electrical performance of the antenna,especially the main beam efficiency,was analyzed with the finite element method.The influence of the support method with six points on the thermal deformation of the continuous solid surface antenna was investigated.Under the uniform temperature field with a difference of 200℃,the surface errors of cells with different shapes were analyzed,and then a hexagon shape was adopted as a segmented cell and the relationship between the surface error and the size was studied.The surface error and electrical performance of the antenna after being segmented by single cells with different sizes and arrangements were investigated,the effect of the splits among the segmented cells on the electrical performance of the antenna was verified,and the final segmented configuration was determined.The results show that the surface error decreases from 500 pm to 5 pm and the main beam efficiency decreases from 6.72%to 1.77%through the final segmented configuration.

关键词

空间可展开天线/高形面精度/热变形/分割法/主波束效率

Key words

space deployable antenna/high surface accuracy/thermal deformation/segmented method/main beam efficiency

分类

航空航天

引用本文复制引用

楼春钢,李昊,潘殿坤..基于分割法的抛物面固面天线热变形抑制[J].中国空间科学技术,2024,44(2):59-67,9.

基金项目

中国博士后科学基金(2020M681805) (2020M681805)

中国空间科学技术

OA北大核心CSTPCD

1000-758X

访问量5
|
下载量0
段落导航相关论文