两级可重复展收立方星伞状天线机构设计与样机验证

doi:10.3901/JME.2022.07.044

机械工程学报 ›› 2022, Vol. 58 ›› Issue (7): 44-52.doi: 10.3901/JME.2022.07.044

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两级可重复展收立方星伞状天线机构设计与样机验证

张树新, 韩晓童, 于亦奇

西安电子科技大学电子装备结构设计教育部重点实验室西安 710071

收稿日期:2021-04-09 修回日期:2021-07-25 出版日期:2022-05-20 发布日期:2022-05-20
通讯作者: 张树新(通信作者),男,1987年出生,博士,教授,博士研究生导师。主要研究方向为有效载荷技术。E-mail:sxzhang@xidian.edu.cn
作者简介:韩晓童,男,1996年出生,硕士研究生。主要研究方向为机构设计。于亦奇,男,1997年出生,硕士研究生。主要研究方向为机构设计。
基金资助:
国家自然科学基金资助项目(51705388)。

Two-step Repeatable Deploying and Furling Mechanism Design and Prototype Verification of a Deployable Umbrella Antenna for CubeSat

ZHANG Shuxin, HAN Xiaotong, YU Yiqi

Key Laboratory of Electronic Equipment Structure Design (Ministry of Education), Xidian University, Xi'an 710071

Received:2021-04-09 Revised:2021-07-25 Online:2022-05-20 Published:2022-05-20

摘要/Abstract

摘要： 针对现有RainCube立方星伞状天线展开冲击大、同步性差、难以重复展收的问题，提出了一种两级可重复展收立方星伞状天线展收机构创新方案，实现了对伞状天线主面根肋、尖肋和副面的重复展收。该展收机构由根肋、尖肋、电机、丝杠丝母、拉索、弹簧、扭簧等组成。通过电机与丝杠丝母相结合、拉索与扭簧相结合、拉索与弹簧相结合分别实现对天线主面根肋、尖肋和副面的同步可控展开及收拢。在对天线关键机构部件运动学分析的基础上，完成了天线展开与收拢过程的轨迹仿真。设计并制作了两级可重复展收立方星伞状天线原理样机，通过原理样机试验验证了所提展收机构创新方案的可行性。

关键词: 立方星, 伞状天线, 展收机构, 样机验证

Abstract: In order to solve the problems of large impact, poor synchronization and unrepeatable deployment of the RainCube antenna for CubeSat applications, a two-step repeatable deploying and furling mechanism is proposed for deployable umbrella antennas. With the proposed mechanism, both the repeatable deploying and furling operations on the root ribs, tip ribs and sub-reflector of the umbrella antenna can be easily performed separately. The mechanism is mainly composed of root ribs, tip ribs, motors, lead screws, cables, a helical spring, and torsion springs. Through the combination of lead screws and motors, the combination of cables and torsion springs, the combination of cables and the helical spring, the synchronous repeatable deploying and furling of the root ribs, tip ribs and sub-reflector can be realized, respectively. Based on the kinematics analysis of the key components of the antenna, the simulation of the deploying and furling trajectory is accomplished. An experimental prototype of the deployable umbrella antenna is fabricated. The feasibility and effectiveness of the proposed repeatable deploying and furling mechanism is verified through experiments.

Key words: CubeSat, umbrella antennas, deploying and furling mechanism, prototype verification

中图分类号:

V414

张树新, 韩晓童, 于亦奇. 两级可重复展收立方星伞状天线机构设计与样机验证[J]. 机械工程学报, 2022, 58(7): 44-52.

ZHANG Shuxin, HAN Xiaotong, YU Yiqi. Two-step Repeatable Deploying and Furling Mechanism Design and Prototype Verification of a Deployable Umbrella Antenna for CubeSat[J]. Journal of Mechanical Engineering, 2022, 58(7): 44-52.

参考文献

[1] POGHOSYAN A,GOLKAR A. CubeSat evolution:Analyzing CubeSat capabilities for conducting science missions[J]. Progress in Aerospace Sciences,2017,88:59-83.
[2] NAG S,RIOS J L,GERHARDT D,PHAM C. CubeSat constellation design for air traffic monitoring[J]. Acta Astronautica,2016,128:180-193.
[3] 陈传志,董家宇,陈金宝,等. 空间大型星载抛物面天线研究进展与展望[J]. 航空学报,2020,41(1):133-153. CHEN Chuanzhi,DONG Jiayu,CHEN Jinbao,et al. Research progress and prospect of large spaceborne parabolic antenna[J]. Acta Aeronautica et Astronautica Sinica,2020,41(1):133-153.
[4] 张骞,李萌,江超,等. 抛物面式固体反射面天线结构的展开设计[J]. 机械工程学报,2020,56(5):21-28. ZHANG Qian,LI Meng,JIANG Chao,et al. Deployment design of the parabolic solid reflector antenna structure[J]. Journal of Mechanical Engineering,2020,56(5):21-28.
[5] FREELAND R E,BILYEU G D,VEAL G R,et al. Large inflatable deployable antenna flight experiment results[J]. Acta Astronautica,1997,41(4):267-277.
[6] 刘荣强,史创,郭宏伟,等. 空间可展开天线机构研究与展望[J]. 机械工程学报,2020,56(5):1-12. LIU Rongqiang,SHI Chuang,GUO Hongwei,et al. Review of space deployable antenna mechanisms[J]. Journal of Mechanical Engineering,2020,56(5):1-12.
[7] 田大可,刘荣强,杨谢柳,等. 模块化构架式空间可展天线支撑桁架展开精度测量与分析[J]. 机械工程学报,2020,56(5):63-71. TIAN Dake,LIU Rongqiang,YANG Xieliu,et al. Deployment accuracy measurement and analysis of truss structure for modular space deployable truss antenna[J]. Journal of Mechanical Engineering,2020,56(5):63-71.
[8] 刘文兰,许允斗,郭金伟,等. 被动输入过约束四面体可展天线机构动力学分析[J]. 机械工程学报,2020,56(5):181-191. LIU Wenlan,XU Yundou,GUO Jinwei,et al. Dynamics of passive-input overconstrained deployable antenna mechanisms composed of 3RR-3RRR tetrahedron units[J]. Journal of Mechanical Engineering,2020,56(5):181-191.
[9] 秦波,吕胜男,刘全,等. 可展收抛物柱面天线机构的设计及分析[J]. 机械工程学报,2020,56(5):100-107. QIN Bo,LÜ Shengnan,LIU Quan,et al. Structural design and analysis of a deployable parabolic-cylinder antenna[J]. Journal of Mechanical Engineering,2020,56(5):100-107.
[10] 吴新燕,关富玲. 双圈六面体环形桁架式可展开天线结构设计[J]. 机械工程学报,2020,56(5):218-225. WU Xinyan,GUAN Fuling. Design of deployable antenna of double-loop hexahedron truss[J]. Journal of Mechanical Engineering,2020,56(5):218-225.
[11] 师甜,王波,华岳,等. 星载高精度伞状天线展开过程运动及受力分析[J]. 空间电子技术,2019,16(2):58-61. SHI Tian,WANG Bo,HUA Yue,et al. Force and dynamic analysis of deployable mechanism of high precision space umbrella antenna[J]. Space Electronic Technology,2019,16(2):58-61.
[12] 马小飞,李洋,肖勇,等. 大型空间可展开天线反射器研究现状与展望[J]. 空间电子技术,2018,15(2):16-26. MA Xiaofei,LI Yang,XIAO Yong,et al. Development and tendency of large space deployable antenna reflector[J]. Space Electronic Technology,2018,15(2):16-26.
[13] 陈国辉,华岳,王波,等. "嫦娥4号"中继星伞状可展开天线设计与验证[J]. 深空探测学报,2018,5(6):524-530. CHEN Guohui,HUA Yue,WANG Bo,et al. Design and verification for umbrella-type deployable antenna of Chang'e-4 lunar relay satellite[J]. Journal of Deep Space Exploration,2018,5(6):524-530.
[14] GAO Yongxin,GE Yimin,MA Lingxi,et al. Optimization design of configuration and layout for Queqiao relay satellite[J]. Advances in Astronautics Science and Technology,2019,2:33-38.
[15] DOMINOCIELO G,LANGAN D. Articulated folding rib reflector for concentrating radiator. US:2019/0214737 A1[P]. 2019-07-11.
[16] SAUDER J,CHAHAT N,HODGES R,et al. Designing,building,and testing a mesh Ka band parabolic deployable antenna (KaPDA) for CubeSats[C]//The 54th AIAA Aerospace Sciences Meeting. 2016:1-7.
[17] CHAHAT N,HODGES R,SAUDER J,et al. CubeSat deployable Ka-band mesh reflector antenna development for earth science missions[J]. IEEE Transactions on Antennas and Propagation,2016,64(6):2083-2093.
[18] PERAL E,TANELLI S,STATHAM S,et al. RainCube:the first ever radar measurements from a CubeSat in space[J]. Journal of Applied Remote Sensing,2019,13(3):032504.
[19] CHAHAT N,SAUDER J,HODGES R E,et al. The deep-space network telecommunication CubeSat antenna:Using the deployable Ka-band mesh reflector antenna[J]. IEEE Antennas and Propagation Magazine,2017,59(2):31-38.
[20] 段宝岩. 空间太阳能发电卫星的几个理论与关键技术问题[J]. 中国科学:技术科学,2018,48(11):1207-1218. DUAN Baoyan. The main aspects of the theory and key technologies about space solar power satellite[J]. Scientia Sinica Technologica,2018,48:1207-1218.

两级可重复展收立方星伞状天线机构设计与样机验证

Two-step Repeatable Deploying and Furling Mechanism Design and Prototype Verification of a Deployable Umbrella Antenna for CubeSat

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