空间大型结构体在轨组装单元及对接接口研究

doi:10.3901/JME.2022.01.052

机械工程学报 ›› 2022, Vol. 58 ›› Issue (1): 52-60.doi: 10.3901/JME.2022.01.052

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空间大型结构体在轨组装单元及对接接口研究

史创¹, 李伟杰², 郭宏伟¹, 陶磊¹, 刘荣强¹, 邓宗全¹

1. 哈尔滨工业大学机器人国家重点实验室哈尔滨 150001;
2. 北京空间飞行器总体设计部北京 100094

收稿日期:2021-01-20 修回日期:2021-07-26 出版日期:2022-01-05 发布日期:2022-03-19
通讯作者: 李伟杰(通信作者),男,1981年出生,博士,研究员。主要研究方向为在轨服务航天器机械系统技术。E-mail:lwjhit@outlook.com
作者简介:史创,男,1990年出生,博士,讲师。主要研究方向为空间大型可展开机构。E-mail:ty12shichuang@126.com
基金资助:
国家自然科学基金（52005123）、中国博士后科学基金（2021M690827）和黑龙江省博士后专向经费（LBH-Z20135）资助项目。

Research on In-orbit Assembly Unit and Docking Interface of Large Space Structure

SHI Chuang¹, LI Weijie², GUO Hongwei¹, TAO Lei¹, LIU Rongqiang¹, DENG Zongquan¹

1. State Key Laboratory of Robotics, Harbin Institute of Technology, Harbin 150001;
2. Beijing Institute of Spacecraft System Engineering, Beijing 100094

Received:2021-01-20 Revised:2021-07-26 Online:2022-01-05 Published:2022-03-19

摘要/Abstract

摘要： 近年来，在轨服务技术日趋成熟，因此在空间技术研究领域在轨组装受到了较高的关注度。研究了一种大折展比高刚度索杆张拉式六棱柱组装单元及三爪式对接接口机构，并对其运动学及动力学特性进行了研究。首先，提出并设计了一种新型的空间结构组装单元和一种结构为三爪式的对接接口，进行在轨组装时可应用该接口。接着，分析了空间结构组装单元的运动学特性，验证了组装单元具有良好的展开与锁定功能。最终，通过对大型结构体模型进行有限元分析，发现了结构体的基频受到多个参数的影响，通过进一步的分析得到了具体的影响关系和灵敏度，为在轨组装空间大型结构体的设计奠定了基础。

关键词: 在轨组装, 六棱柱单元, 结构设计, 对接接口, 运动学, 动力学

Abstract: In recent years, in-orbit service technology is becoming more and more mature, so in-orbit assembly has received great attention in the space technology research field. In this paper, a kind of cable-strut tension hexagonal prism assembly unit with large deployment ratio and high stiffness and a kind of three-claw-type docking interface mechanism are studied, and their kinematic and dynamic characteristics are studied. Firstly, a new space structure assembly unit and a three-claw docking interface are proposed and designed, the interface can be used for in-orbit assembly. Then, the kinematic characteristics of the spatial structure assembly unit are analyzed, and the good deployment and locking functions of the assembly unit are verified. Finally, according to the finite element analysis of the large structure model, it is found that the fundamental frequency of the structure is affected by many parameters, and the specific influence rules and sensitivity are also shown under the further analysis, which lays a foundation for the design of the space large structure in-orbit assembly.

Key words: in-orbit assembly, hexagonal prism unit, structure design, docking interface, kinematics, dynamics

中图分类号:

TG156

史创, 李伟杰, 郭宏伟, 陶磊, 刘荣强, 邓宗全. 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, TAO Lei, LIU Rongqiang, DENG Zongquan. Research on In-orbit Assembly Unit and Docking Interface of Large Space Structure[J]. Journal of Mechanical Engineering, 2022, 58(1): 52-60.

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空间大型结构体在轨组装单元及对接接口研究

Research on In-orbit Assembly Unit and Docking Interface of Large Space Structure

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