Mechanism design and dynamic analysis of large-scale two-dimensional deployable planar antenna

SHI Chuang; LIU Ming-li; GUO Hong-wei; LIU Rong-qiang; MA Xiao-fei

doi:10.37188/OPE.20212912.2868

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Mechanism design and dynamic analysis of large-scale two-dimensional deployable planar antenna

Micro\/Nano Technology and Fine Mechanics | 更新时间：2026-09-12

- Mechanism design and dynamic analysis of large-scale two-dimensional deployable planar antenna
- Optics and Precision Engineering Vol. 29, Issue 12, Pages: 2868-2876(2021)
- 作者机构：
  
  1.哈尔滨工业大学机器人技术与系统国家重点实验室，黑龙江哈尔滨 150001
  2.西安空间无线电技术研究所，陕西西安 710100
- 作者简介：
- 基金信息：
- DOI：10.37188/OPE.20212912.2868
  CLC： TP394.1;TH691.9
- Received：10 May 2021，
  
  Revised：2021-06-28，
  
  Published：15 December 2021
- 稿件说明：
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史创,刘名利,郭宏伟等.大型二维多折展开平面天线机构设计及动力学特性分析[J].光学精密工程,2021,29(12):2868-2876.

SHI Chuang,LIU Ming-li,GUO Hong-wei,et al.Mechanism design and dynamic analysis of large-scale two-dimensional deployable planar antenna[J].Optics and Precision Engineering,2021,29(12):2868-2876.
史创,刘名利,郭宏伟等.大型二维多折展开平面天线机构设计及动力学特性分析[J].光学精密工程,2021,29(12):2868-2876. DOI： 10.37188/OPE.20212912.2868.

SHI Chuang,LIU Ming-li,GUO Hong-wei,et al.Mechanism design and dynamic analysis of large-scale two-dimensional deployable planar antenna[J].Optics and Precision Engineering,2021,29(12):2868-2876. DOI： 10.37188/OPE.20212912.2868.

摘要

随着空间对地观测范围和观测精度要求的不断提升，对大型平面可展开天线机构的需求越来越迫切。本文提出了一种全新的空间大型二维多折展开相控阵天线机构，对其进行了构型优选、结构设计及动力学特性分析。首先，建立了综合评价指标，优选出综合性能最优的天线整体构型方案。其次，对天线机构各部件进行了详细的结构设计，进行样机的研制与展开原理实验验证。最后，建立了天线机构的有限元模型，通过仿真得出了天线机构展开态前5阶振动频率及其对应的振型，并以系统频率变形比作为优化目标对各杆件截面参数进行优化。本文所设计的二维多折展开平面天线机构折展比达到17.6，提高了传统平面天线机构的折叠比；分子振动基频达到1.333 9 Hz，实现了大型平面天线机构的高刚度支撑，为我国大型平面相控阵天线机构的研制提供了可行方案。

Abstract

The improvement of the space-to-earth observation range and observation accuracy has created demand for large-scale planar deployable antenna mechanisms. A new space large-scale two-dimensional multi-folding and unfolding planar antenna mechanism， which has been optimized for configuration， structure design， and dynamic characteristics analysis， is proposed in this study. First， a comprehensive evaluation index is established， and the overall configuration of the antenna with the best comprehensive performance is selected. Second， the structure of each part of the antenna mechanism is designed in detail and the prototype is developed. Additionally， the experimental verification of the deployment principle is carried out. Finally， the finite element model of the antenna mechanism is established， and the first five vibration frequencies of the antenna mechanism in the unfolded state and the corresponding mode shapes are obtained through simulation. Further， the cross-section parameters of each member are optimized with the system specific frequency as the optimization target. The folding ratio of the two-dimensional multi-folding and unfolding planar antenna mechanism designed in this study is greater than 17.6， which is an improvement over the folding ratio of the traditional planar antenna mechanism. The vibration fundamental frequency is 1.333 9 Hz， which helps in realizing the high rigidity support of the large planar antenna mechanism and provides a feasible scheme for the development of large planar phased array antenna mechanism in China.

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references

殷康程，永强，霍银龙，等 . 星载双反射面偏置天线可展开双轴指向机构设计［J］. 光学精密工程， 2021 ， 29 （ 3 ）： 582 - 591 . doi: 10.37188/OPE.2020.0548 http://dx.doi.org/10.37188/OPE.2020.0548

YIN K CH ， YONG Q ， HUO Y L ， et al . Design of deployable biaxial pointing mechanism for spaceborne dual-reflector offset antenna ［J］. Opt. Precision Eng. ， 2021 ， 29 （ 3 ）： 582 - 591 . （in Chinese） . doi: 10.37188/OPE.2020.0548 http://dx.doi.org/10.37188/OPE.2020.0548

杨慧，范硕硕，刘荣强 . 光学薄膜折展机构单元胞豆荚蜂窝杆优化［J］. 光学精密工程， 2020 ， 28 （ 10 ）： 2244 - 2251 . doi: 10.37188/ope.20202810.2244 http://dx.doi.org/10.37188/ope.20202810.2244

YANG H ， FAN SH SH ， LIU R Q . Optimization of single lenticular honeycomb boom for optical film deployable mechanism ［J］. Opt. Precision Eng. ， 2020 ， 28 （ 10 ）： 2244 - 2251 . （in Chinese） . doi: 10.37188/ope.20202810.2244 http://dx.doi.org/10.37188/ope.20202810.2244

姜鑫，陈武雄，聂海涛，等 . 航空遥感影像的实时舰船目标检测［J］. 光学精密工程， 2020 ， 28 （ 10 ）： 2360 - 2369 . doi: 10.37188/OPE.20202810.2360 http://dx.doi.org/10.37188/OPE.20202810.2360

JIANG X ， CHEN W X ， NIE H T ， et al . Real-time ship target detection based on aerial remote sensing images ［J］. Opt. Precision Eng. ， 2020 ， 28 （ 10 ）： 2360 - 2369 . （in Chinese） . doi: 10.37188/OPE.20202810.2360 http://dx.doi.org/10.37188/OPE.20202810.2360

GRALEWSKI M R ， ADAMS L ， HEDGEPETH J M . Deployable extendable support structure for the RADARSAT synthetic aperture radar antenna ［C］. 43th International Astronautical Congress ， Washington ， 1992 ： 18 .

SRIVASTAVA S K ， HAWKINS R K ， BANIK B T ， et al . RADARSAT-1 image quality and calibration-a continuing success ［J］. Advances in Space Research ， 2001 ， 28 （ 1 ）： 99 - 108 . doi: 10.1016/s0273-1177(01)00305-2 http://dx.doi.org/10.1016/s0273-1177(01)00305-2

GIMENO M ， SAN-MIGUEL-AYANZ J . Evaluation of RADARSAT-1 data for identification of burnt areas in Southern Europe ［J］. Remote Sensing of Environment ， 2004 ， 92 （ 3 ）： 370 - 375 . doi: 10.1016/j.rse.2004.03.018 http://dx.doi.org/10.1016/j.rse.2004.03.018

THOMAS W D R . RADARSAT-2 extendible support structure ［J］. Canadian Journal of Remote Sensing ， 2004 ， 30 （ 3 ）： 282 - 286 . doi: 10.5589/m04-005 http://dx.doi.org/10.5589/m04-005

CHIU S . Moving target parameter estimation for RADARSAT-2 Moving Object Detection EXperiment （MODEX）［J］. International Journal of Remote Sensing ， 2010 ， 31 （ 15 ）： 4007 - 4032 . doi: 10.1080/01431160903032901 http://dx.doi.org/10.1080/01431160903032901

TADONO T ， SHIMADA M ， WATANABE M ， et al . Overview of ALOS research and science program ［C］. Remote Sensing. Proc SPIE 5570 ，. doi: 10.1117/12.565485 http://dx.doi.org/10.1117/12.565485

Sensors ， Systems ， and Next-Generation Satellites VIII ， Maspalomas ， Canary Islands ， Spain . 2004 ， 5570 ： 10 - 21 . doi: 10.1117/12.565485 http://dx.doi.org/10.1117/12.565485

IGARASHI T . Alos mission requirement and sensor specifications ［J］. Advances in Space Research ， 2001 ， 28 （ 1 ）： 127 - 131 . doi: 10.1016/s0273-1177(01)00316-7 http://dx.doi.org/10.1016/s0273-1177(01)00316-7

MIKULAS M M ， PAPPA R S ， WARREN J ， et al . Telescoping solar array concept for achieving high packaging efficiency ［C］. 2nd AIAA Spacecraft Structures Conference . 5 - 9 January 2015， Kissimmee， Florida. Reston ， Virginia： AIAA ， 2015 . doi: 10.2514/6.2015-1398 http://dx.doi.org/10.2514/6.2015-1398

JODOI D ， KUROSE T . A 100-meter-class plate space structure construction method using a deployable truss ［J］. Mechanical Engineering Letters ， 2017 ， 3 ： 17 - 82 . doi: 10.1299/mel.17-00082 http://dx.doi.org/10.1299/mel.17-00082

SHEN Y ， MONTMINY S ， ZHENG W P ， et al . Large SAR membrane antenna deployable structure design and dynamic simulation ［C］. 48th AIAA/ASME/ASCE/AHS/ASC Structures， Structural Dynamics， and Materials Conference . 23 April 2007-26 April 2007， Honolulu， Hawaii. Reston ， Virginia： AIAA ， 2007.

HORI K ， KATSUMI T ， SAWAI S ， et al . HAN-based green propellant， SHP163 - its R&D and test in space ［J］. Propellants ， Explosives， Pyrotechnics， 2019 ， 44 （ 9 ）： 1080 - 1083 . doi: 10.1002/prep.201900237 http://dx.doi.org/10.1002/prep.201900237

崔岳，唐勇 . 实践二十号卫星在轨核心试验全部完成［J］. 国际太空， 2020 （ 7 ）： 38 - 41 .

CUI Y ， TANG Y . Practicing the completion of the core test of No.20 satellite in orbit ［J］. Space International ， 2020 （ 7 ）： 38 - 41 . （in Chinese）

WANG Y ， DENG Z Q ， LIU R Q ， et al . Topology structure synthesis and analysis of spatial pyramid deployable truss structures for satellite SAR antenna ［J］. Chinese Journal of Mechanical Engineering ， 2014 ， 27 （ 4 ）： 683 - 692 . doi: 10.3901/cjme.2014.0422.081 http://dx.doi.org/10.3901/cjme.2014.0422.081

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