1.西安交通大学机械工程学院现代设计及转子轴承系统教育部重点实验室,710049,西安
2.中国空间技术研究院西安分院,710000,西安
收稿:2026-02-02,
修回:2026-04-16,
录用:2026-04-24,
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张进华, 蒋金波, 朱佳龙, 等. 大型可展开网状天线展开过程仿真建模与竖向索预拉力优化调控[J/OL]. 西安交通大学学报, 2026.
ZHANG Jinhua, JIANG Jinbo, ZHU Jialong, et al. Multi-Objective Assembly Performance Oriented Optimization of Vertical Cable Pretension in Large Deployable Mesh Antenna[J/OL]. JOURNAL OF XI’AN JIAOTONG UNIVERSITY, 2026.
为解决传统形面调节方法难以兼顾天线多方面性能要求的问题,本文提出了一种面向多目标装配性能的预拉力优化方法。研究基于拉格朗日方程构建了系统动力学模型,通过结构简化及力学等效建立了仿真简化模型,通过天线展开过程仿真及模态振频仿真揭示了竖向索预拉力对多目标装配性能的影响。研究搭建了原理样机并进行展开实验,验证了仿真模型的可靠性,同时测试了样机的低阶模态与形面精度,对仿真模型进行了标定。利用参数相关性仿真分析的样本建立了代理模型。最后基于代理模型,在预设形面精度及样本范围约束条件下,以突变力矩峰值、形面精度及一阶固有频率为优化目标,优化索拉力配置。优化后天线形面精度达较基准提升16.5%,满足样机设计要求;展开突变力矩峰值降低8%;一阶固有频率降低11.3%,有效避开共振带,实现了天线装配的形性一体化协同调控。
To solve the problem that traditional surface adjustment methods struggle to balance multiple antenna performance requirements
a pretension optimization method for multi-objective assembly performance is proposed. Based on Lagrange equations
a system dynamic model is constructed
and a simplified simulation model is established through structural simplification and mechanical equivalence. Through antenna deployment and modal vibration simulations
the impact of vertical cable pretension on multi-objective assembly performance is revealed. A principle prototype was built and deployment experiments were conducted to verify the reliability of the simulation model. Low-order modes and surface accuracy were tested to calibrate the simulation model. A surrogate model is established using samples from parameter correlation simulation analysis. Finally
based on the surrogate model
cable tension configuration is optimized with peak abrupt torque
surface accuracy
and first-order natural frequency as optimization objectives
under constraints of preset surface accuracy and sample range. After optimization
antenna surface accuracy is improved by 16.5% compared to the baseline
meeting prototype design requirements. Peak deployment abrupt torque is reduced by 8%
and first-order natural frequency is decreased by 11.3%
effectively avoiding the resonance band. Thereby
the integrated collaborative regulation of shape and properties in antenna assembly is achieved.
YOU, G. Application of Flexible Reflector Space-Borne Deployable Antenna . In: Xu, Z., Parizi, R.M., Loyola-González, O., Zhang, X. (eds) Cyber Security Intelligence and Analytics. CSIA 2021 . Advances in Intelligent Systems and Computing, vol 1342 . Springer , Cham .
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 [J ] . 航空学报 , 2021 , 42 ( 01 ): 133 - 153 .
CHEN C , DONG J , CHEN J , et al . Research progress of large spaceborne parabolic antennas [J ] . Acta Aeronautica et Astronautica Sinica , 2021 , 42 ( 01 ): 133 - 153 .
刘荣强 , 田大可 , 邓宗全 . 空间可展开天线结构的研究现状与展望 [J ] . 机械设计 , 2010 , 27 ( 09 ): 1 - 10 .
LIU R , TIAN D , DENG Z . Research status and prospects of space deployable antenna structures [J ] . Journal of Machine Design , 2010 , 27 ( 09 ): 1 - 10 .
杜雪林 , 杜敬利 , 保宏 , 等 . 考虑桁架柔性的可展开天线动力学分析 [J ] . 机械工程学报 , 2020 , 56 ( 07 ): 119 - 126 .
DU X , DU J , BAO H , et al . Dynamic analysis of deployable antenna considering truss flexibility [J ] . Journal of Mechanical Engineering , 2020 , 56 ( 07 ): 119 - 126 .
冯涛 , 冀有志 , 肖勇 , 等 . 星载环形天线结构及其应用综述 [J ] . 空间电子技术 , 2015 , 12 ( 02 ): 22 - 28 .
FENG T , JI Y , XIAO Y , et al . Review of spaceborne hoop antenna structures and their applications [J ] . Space Electronic Technology , 2015 , 12 ( 02 ): 22 - 28 .
L. Dwight Gilger , Mark W. Thomson , John C. Gereau . Mi-cro fold reflector [P ] . United States Patent 6323827B1 .
魏聚周 . 计及桁架柔性的环形天线找形方法研究 [D ] . 天津大学 , 2014 .
WEI J . Research on form-finding method of hoop antenna considering truss flexibility [D ] . Tianjin University , 2014 .
牛治永 , 李晓岚 , 王三民 , 等 . 空间桁架可展天线反射器的形面精度优化调整 [J ] . 机械设计与制造 , 2011 ,( 06 ): 123 - 125 .
NIU Z , LI X , WANG S , et al . Surface accuracy optimization adjustment of space truss deployable antenna reflector [J ] . Machinery Design & Manufacture , 2011 , ( 06 ): 123 - 125 .
韩若宇 , 何柏岩 , 聂锐 , 等 . 考虑在轨热效应的网状天线索网优化设计 [J ] . 中国空间科学技术 , 2022 , 42 ( 04 ): 111 - 119 .
HAN R , HE B , NIE R , et al . Optimization design of mesh antenna cable-net considering on-orbit thermal effects [J ] . Chinese Space Science and Technology , 2022 , 42 ( 04 ): 111 - 119 .
李团结 , 杨丽 , 李洋 , 等 . 绳索-金属丝网组合结构力热匹配设计 [J ] . 西安电子科技大学学报 , 2018 , 45 ( 02 ): 48 - 53 .
LI T , YANG L , LI Y , et al . Thermal-mechanical matching design of cable-metal mesh composite structure [J ] . Journal of Xidian University , 2018 , 45 ( 02 ): 48 - 53 .
苏冠龙 , 马小飞 , 范叶森 , 等 . 基于多神经网络的可展开网状天线型面调整方法 [J ] . 中国空间科学技术(中英文) , 2024 , 44 ( 02 ): 51 - 58 .
SU G , MA X , FAN Y , et al . Surface adjustment method for deployable mesh antennas based on multiple neural networks [J ] . Chinese Space Science and Technology , 2024 , 44 ( 02 ): 51 - 58 .
杨东武 , 杜敬利 , 李团结 . 周边桁架式索网天线型面的快速调整方法 [J ] . 中国机械工程 , 2010 , 21 ( 01 ): 35 - 37 .
YANG D , DU J , LI T . Rapid surface adjustment method for perimeter truss cable-net antenna [J ] . China Mechanical Engineering , 2010 , 21 ( 01 ): 35 - 37 .
袭安 , 彭湘涛 . 星载环形网架天线的振动特性分析 [J ] . 电子产品可靠性与环境试验 , 2020 , 38 ( S1 ): 31 - 34 .
XI A , PENG X . Vibration characteristics analysis of spaceborne hoop-truss antenna [J ] . Electronic Product Reliability and Environmental Testing , 2020 , 38 ( S1 ): 31 - 34 .
杨军刚 , 肖勇 , 赵治华 , 等 . 大型环形桁架天线分布式驱动展开方法与数值分析 [J ] . 中国科学:物理学 力学 天文学 , 2017 , 47 ( 10 ): 27 - 36 .
YANG J , XIAO Y , ZHAO Z , et al . Distributed drive deployment method and numerical analysis of large hoop-truss antenna [J ] . Scientia Sinica: Physica , Mechanica & Astronomica, 2017 , 47 ( 10 ): 27 - 36 .
任伟峰 , 何柏岩 , 聂锐 . 环形桁架天线展开动力学分析 [J ] . 中国机械工程 , 2019 , 30 ( 24 ): 2945 - 2952 .
REN W , HE B , NIE R . Deployment dynamics analysis of hoop-truss antenna [J ] . China Mechanical Engineering , 2019 , 30 ( 24 ): 2945 - 2952 .
ZHANG Yiqun , RU Wenrui , YANG Guigeng , LI Na , Deployment analysis considering the cable-net tension effect for deployable antennas , Aerospace Science and Technology , Volume 48 , 2016 , Pages 193 - 202 , ISSN 1270 - 9638 .
GOLDSTEIN H , POOLE C P , SAFKO J L . Classical Mechanics . San Francisco : Addison Wesley , 2002
齐晓志 . 环形桁架式可展开天线机构设计及展开动力学研究 [D ] . 哈尔滨工业大学 , 2016 .
QI X . Mechanism design and deployment dynamics research of hoop-truss deployable antenna [D ] . Harbin Institute of Technology , 2016 .
SHABANA A A . Dynamics of multibody systems [M ] . Cambridge University Press , 2020 .
董富祥 , 周志成 , 曲广吉 . 星载大型天线反射器桁架展开动力学建模仿真 [J ] . 航天器工程 , 2012 , 21 ( 04 ): 26 - 31 .
DONG F , ZHOU Z , QU G . Dynamic modeling and simulation of truss deployment for large spaceborne antenna reflector [J ] . Spacecraft Engineering , 2012 , 21 ( 04 ): 26 - 31 .
YANG , Z , HE K , LIU L et al . Active Vibration Control of Beam-Pointing-Sensitive Modes in Large Space Deployable Antennas . Adv. Astronaut . ( 2025 ).
JIANG X , BAI Z . Dynamics Modelling and Simulation for Deployment Characteristics of Mesh Reflector Antennas . Applied Sciences . 2020 ; 10 ( 21 ): 7884 .
邓汉卿 . 空间可展开索网天线的机构构型综合与形面设计方法研究 [D ] . 西安电子科技大学 , 2016 .
DENG H . Research on mechanism configuration synthesis and surface design method for space deployable cable-net antenna [D ] . Xidian University , 2016 .
HE B , JIA L , LI K , et al . Deployment Dynamic Modeling and Driving Schemes for a Ring-Truss Deployable Antenna . Chin. J. Mech. Eng . 37 , 79 ( 2024 ).
PENG Y , ZHAO Z , ZHOU M , et al . Flexible multibody model and the dynamics of the deployment of mesh antennas [J ] . Journal of guidance, control, and dynamics , 2017 , 40 ( 6 ): 1499 - 1510 .
师甜 , 肖勇 . 一种大型可展开天线结构频率调整技术研究 [J ] . 现代电子技术 , 2013 , 36 ( 11 ): 75 - 78+81 .
SHI T , XIAO Y . Research on frequency adjustment technology for large deployable antenna structure [J ] . Modern Electronics Technique , 2013 , 36 ( 11 ): 75 - 78+81 .
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