Mechanism Design and Kinematics Analysis for a Solid Surface Deployable Antenna

doi:10.3901/JME.2025.03.237

Abstract

Abstract: The solid surface deployable antenna has the characteristics of high reliability, high accuracy and good thermal stability. In view of the problems that the shape accuracy, linkage drive and locking stiffness of the solid surface deployable antenna structure are affected by the excessive number of rotating pairs and the presence of spherical joints, universal joints and other high pairs in the deployment mechanism of the solid surface deployable antenna, the two deployment methods of the solid surface deployable antenna rotating around the orthogonal double axis in two steps and rotating around the single axis in one time are compared. A deployable mechanism for deployable antenna on solid surface is proposed, which rotates around a single axis and deploys once. The parametric model for calculating the position of the rotation axis is constructed, and the kinematic model of the deployment mechanism is established. The numerical simulation software is used to simulate the established model, and the influence of the position of the rotation axis on the antenna storage rate and the gap between adjacent panels is analyzed. The finite element model of the antenna structure is established, and the antenna structure is optimized. The results show that the design of rotating around a single axis reduces the number of rotating pairs and does not use high pairs such as spherical joints and universal joints, which not only improves the deployment reliability of the mechanism, but also facilitates the linkage, driving, locking and stiffening of the mechanism. At the same time, the optimized structure has better mechanical performance, which is expected to provide reference for the theoretical research and engineering application of deployable antennas on solid surfaces.

Key words: deployable antennas, deployable mechanism, solid surface deployable antenna, configuration synthesis, kinematics analysis, mechanism design

CLC Number:

V443
TH112

FAN Xiaodong, SHI Chuang, WANG Zhiyi, LIU Tianming, GUO Hongwei, LIU Rongqiang. Mechanism Design and Kinematics Analysis for a Solid Surface Deployable Antenna[J]. Journal of Mechanical Engineering, 2025, 61(3): 237-250.

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URL: http://www.cjmenet.com.cn/EN/10.3901/JME.2025.03.237

http://www.cjmenet.com.cn/EN/Y2025/V61/I3/237

References

[1] MA X，LI T，MA J，et al. Recent advances in space-deployable structures in China[J]. Engineering，2022，17:207-219.
[2] 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.
[3] ZHANG X，NIE R，CHEN Y，et al. Deployable structures:structural design and static/dynamic analysis[J]. Journal of Elasticity，2021，146:199-235.
[4] MUKESH C，SATISH K，SOMNATH C，et al. A review on developments of deployable membrane-based reflector antennas[J]. Advances in Space Research，2021，68(9):3749-3764.
[5] YUAN S. Review of root-mean-square error calculation methods for large deployable mesh reflectors[J]. International Journal of Aerospace Engineering，2022(1):5352146.
[6] KARDASHEV N S，KHARTOV V V，ABRAMOV V V，et al. “RadioAstron” —A telescope with a size of 300000 km:Main parameters and first observational results[J]. Astronomy Reports，2013，57:153-194.
[7] SAYAPIN S N，SHKAPOV P M. Kinematics of deployment of petal-type large space antenna reflectors with axisymmetric petal packaging[J]. Journal of Machinery Manufacture and Reliability，2016，45(5):387-397.
[8] WU Z，LI H，LI Q. Novel thermally stable segmented solid paraboloid antenna for high surface accuracy[J]. AIAA Journal，2021，59(11):4669-4685.
[9] 王建东，郭宏伟，刘荣强，等. 可展开固体反射面机构设计及运动学分析[J]. 光学精密工程，2018，26(12):2940-2948. WANG Jiandong，GUO Hongwei，LIU Rongqiang，et al. Mechanism design and kinematic analysis of deployable solid reflector mechanism[J]. Optics and Precision Engineering，2018，26(12):2940-2948.
[10] HUANG H，GUAN F，PAN L，et al. Design and deploying study of a new petal-type deployable solid surface antenna[J]. Acta Astronautica，2018，148:99-110.
[11] HUANG H，CHENG Q，ZHENG L. Structural dynamic improvement for petal-type deployable solid-surface reflector based on numerical parameter study[J]. Applied Sciences，2020，10(18):6560.
[12] HUANG H，CHENG Q，ZHENG L，et al. Development for petal-type deployable solid-surface reflector by uniaxial rotation mechanism[J]. Acta Astronautica，2021，178:511-521.
[13] TAN G，DUAN X，YANG D，et al. Parametric design optimization approach to petal-type solid surface deployable reflectors[J]. Acta Astronautica，2022，197:280-297.
[14] TAN G，DUAN X，NIU D，et al. Visual synthesis of uniaxial synchronous deployment mechanisms for solid-surface deployable antennas[J]. Mechanism and Machine Theory，2022，178:105073.
[15] 徐彦，成强，黄河，等. 绕单轴旋转的固面可展开天线展开过程研究[J]. 工程设计学报，2020，27(3):301-306. XU Yan，CHENG Qiang，HUANG He，et al. Study of deploying process of solid-surface deployable antenna rotating along a single axis[J]. Chinese Journal of Engineering Design，2020，27(3):301-306.
[16] 王志岗. 基于刚性折纸的固面天线结构设计与分析[D]. 西安:西安电子科技大学，2020. WANG Zhigang. Structure design and analysis of solid surface antenna based on rigid origami[D]. Xi’an:Xidian University，2020.
[17] BUJAKAS V I. New design of petal type deployable space mirror[J]. Multibody Mechatronic Systems，2015，25:391-398.
[18] 潘亮来，关富玲，黄河. 星载刚性可展开抛物面的设计与展开分析[J]. 空间结构，2018，24(2):67-71. PAN Lianglai，GUAN Fuling，HUANG He. Design and unfolding analysis of rigid deployable parabolic reflector for space borne platform[J]. Spatial Structures，2018，24(2):67-71.
[19] MOROZOV E V，LOPATIN A V. Design，analysis，manufacture and testing of the spacecraft mirror antenna with the composite high precision and size-stable solid surface reflector[J]. Composite Structures，2022，301:116185.
[20] LEE J Y，YOON S，KIM S，et al. Performance of solid surface deployable antenna for panel misalignment[C]// 2016 URSI Asia-Pacific Radio Science Conference. 2016:877-879.
[21] LEE J Y，LEE K，YOON S，et al. Effects on performance of deployable solid antenna for panel misalignment[J]. The Journal of Korean Institute of Electromagnetic Engineering and Science 2017，28:603-609.
[22] JO S J，LEE J Y，YOON S，et al. Performance degradation of deployable antenna from panel misalignment with random surface errors[C]// 2018 International Symposium on Antennas and Propagation (ISAP)，2018:1-2.
[23] JO S J，LEE J Y，YOON S，et al. Panel misalignment effects on the radiation pattern from a solid surface deployable antenna[J]. Journal of Electromagnetic Engineering and Science，2019，19(4):253-258.
[24] LEE S A，JO S J，KIM S J，et al. Analysis of cross-polarized field by panel misalignment errors in a deployable reflector antenna[J]. Journal of Electromagnetic Engineering and Science，2023，23(1):18-26.
[25] 史创，李伟杰，郭宏伟，等. 空间大型结构体在轨组装单元及对接接口研究[J]. 机械工程学报，2022，58(1):52-60. SHI Chuang，LI Weijie，GUO Hongwei，et al. Research on in-orbit assembly unit and docking interface of large space structure[J]. Journal of Mechanical Engineering，2022，58(1):52-60.
[26] 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. Journal of Mechanical Engineering，2020，56(5):63-71.
[27] XIAO H，WU S，XIE D，et al. Shape memory polymer composite booms with applications in reel-type solar arrays[J]. Chinese Journal of Mechanical Engineering，2023，36:67.
[28] ZHAO P，LIU J，WU C，et al. Novel surface design of deployable reflector antenna based on polar scissor structures[J]. Chinese Journal of Mechanical Engineering，2020，33:68