一种新型张力-杆系结构展开过程动力学研究

doi:10.3901/JME.2022.19.095

机械工程学报 ›› 2022, Vol. 58 ›› Issue (19): 95-103.doi: 10.3901/JME.2022.19.095

扫码分享

一种新型张力-杆系结构展开过程动力学研究

张大羽^1,2, 马小飞¹, 王辉¹, 罗建军², 王坤³, 李洋¹, 吴迪⁴

1. 中国空间技术研究院西安分院西安 710100;
2. 西北工业大学航天学院西安 710072;
3. 北京理工大学宇航学院北京 100081;
4. 南京航空航天大学航天学院南京 210000

收稿日期:2022-03-07 修回日期:2022-06-30 出版日期:2022-10-05 发布日期:2023-01-05
通讯作者: 马小飞(通信作者)，男，1980年出生，博士，研究员，博士研究生导师。主要研究方向为空间可展开结构与机构、空间新材料与工艺。E-mail：Maxf041600@sina.com
作者简介:张大羽，男，1987年出生，博士后。主要研究方向为空间可展开结构动力学。E-mail：zhangdayu504@foxmail.com
基金资助:
国家自然科学基金(11290154,U20B2033)和中国博士后科学基金(2020M683601)资助项目。

Deployment Dynamics Simulation of a Novel Tension/Rod Structural System

ZHANG Dayu^1,2, MA Xiaofei¹, WANG Hui¹, LUO Jianjun², WANG Kun³, LI Yang¹, WU Di⁴

1. China Academy of Space Technology (Xi'an), Xi'an 710100;
2. School of Astronautics, Northwestern Polytechnical University, Xi'an 710072;
3. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081;
4. College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210000

Received:2022-03-07 Revised:2022-06-30 Online:2022-10-05 Published:2023-01-05

摘要/Abstract

摘要： 针对新型张力-杆系结构展开过程复杂导致动力学分析困难的问题，采用多柔体动力学方法，提出了张力-杆系结构的全新多体系统模型，实现了结构的展开过程仿真，研究了不同的绳索加载方式对桁架展开动力学行为的影响，总结了绳索力光滑加载方式的优势，揭示了桁架壁厚和绳索张紧力大小对张力-杆系结构展开过程的影响机理，结果表明杆件壁过薄及绳索张紧力过大均对结构展开过程中桁架受力产生显著影响。在此基础上，提出了张力-杆系结构的理论驱动力矩，给出了力矩与桁架杆件展开角度之间的关系，可以为电机选型提供参考。新型张力-杆系结构动力学分析为实际工程应用提供一种新的建模与仿真方法。

关键词: 新型张力-杆系结构, 展开过程仿真, 多柔体动力学, 绳索张紧力, 驱动力矩

Abstract: Concerning solving the problem that the complex deployment dynamics analysis of the novel tension/rod system structure, a multi-body model of the novel tension/rod structural system is proposed using the multi-flexible body dynamics. First, its deplorable process is simulated, and the effect of different cable loading methods on the hoop’s deployment dynamics behavior is studied; the advantages of the smooth loading method of the cable forces are summarized. Then, the effect of the hoop thickness and the magnitude of the cable tension force on the deployment dynamics of the tension-rod system structural system is analyzed. The results show that rod’s thickness and the excessive tensioning force of the cables can significantly affect the hoop’s strength during the structure deployment. On this basis, the theoretical driving moment of the tension/rod structural system is proposed. The relationship between the moment and the deplorable angle of the hoop’s rod is given, providing a reference for motor selection. The structural dynamics analysis of the novel tension/rod system provides a new modeling and simulation method for practical engineering applications.

Key words: novel tension/rod structural system, deployment dynamics simulation, multi-flexible body dynamics, cable tensioning force, driving moment

中图分类号:

O313

张大羽, 马小飞, 王辉, 罗建军, 王坤, 李洋, 吴迪. 一种新型张力-杆系结构展开过程动力学研究[J]. 机械工程学报, 2022, 58(19): 95-103.

ZHANG Dayu, MA Xiaofei, WANG Hui, LUO Jianjun, WANG Kun, LI Yang, WU Di. Deployment Dynamics Simulation of a Novel Tension/Rod Structural System[J]. Journal of Mechanical Engineering, 2022, 58(19): 95-103.

参考文献

[1] 胡海岩，田强，张伟，等. 大型网架式可展开空间结构的非线性动力学与控制[J]. 力学进展，2013，43(4):390-414. HU Haiyan，TIAN Qiang，ZHANG Wei，et al. Nonlinear dynamics and control of large deployable space structures composed of trusses and meshes[J]. Advances in Mechanics，2013，43(4):390-414.
[2] 段宝岩. 大型空间可展开天线的研究现状与发展趋势[J].电子机械工程，2017，33(01):1-14. DUAN Baoyan. The state-of-art and development trend of large space-borne deployable antenna[J]. Electro- Mechanical Engineering，2017，33(01):1-14.
[3] MA X，LI T J，MA Y J，et al. Recent advances of space deployable structures in China[J]. Engineering，2022 (accepted).
[4] 侯欣宾，王立. 空间太阳能电站技术发展现状及展望[J]. 中国航天，2015(2):12-15. HOU Xinbin，WANG Li. Status and prospect of space solar power station technology[J]. Aerospace China，2015(2):12-15.
[5] 肖洪，成正爱，郭宏伟，等. 空间太阳能电站大折展比体展开桁架机构[J]. 机械工程学报，2020，56(13):128-137. XIAO Hong，CHENG Zhengai，GUO Hongwei，et al. Large folding ratio 3D deployable truss mechanism for space solar power station[J]. Journal of Mechanical Engineering，2020，56(13):128-137.
[6] HASANZADE V，SEDIGHY S H，SHAHRAVI M. Compact deployable umbrella antenna design with optimum communication properties[J]. Journal of Spacecraft and Rockets，2017，54(3):781-785.
[7] 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，2018，2:16-26. MA Xiaofei，LI Yang，XIAO Yong，et al. Development and tendency of large space deployable antenna reflector [J]. Space Electronic Technology，2018，2:16-26.
[8] 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，2019，56(5):1-12. LIU Rongqiang，SHI Chuang，GUO Hongwei，et al. Review of space deployable antenna mechanisms[J]. Journal of Mechanical Engineering，2019，56(5):1-12.
[9] 田强，刘铖，李培，等.多柔体系统动力学研究进展与挑战[J]. 动力学与控制学报，2017，15(05):385-405. TIAN Qiang，LIU Cheng，LI Pei，et al. Advances and challenges in dynamics of flexible multibody system[J]. Journal of Dynamics and Control，2017，15(05):385-405.
[10] 周志成，董富祥. 空间大型天线多体动力学分析[M].北京:中国宇航出版社，2014. ZHOU Zhicheng，DONG Fuxiang. Multi-body dynamics analysis of large antennas in space [M]. Beijing:China Astronautic Publishing House，2014.
[11] LI P，LIU C，TIAN Q，et al. Dynamics of a deployable mesh reflector of satellite antenna: form-finding and modal analysis[J]. ASME Journal of Computational and Nonlinear Dynamics，2016，11(4):041017.
[12] 荣吉利，崔硕，石文静，等. 大型空间电站在轨展开与组装动力学与控制[J]. 宇航学报，2021, 42(03):295-304. RONG Jili，CUI Shuo，SHI Wenjing，et al. On-orbit deployment and assembly dynamics and control of large space power station[J]. Journal of Astronautics，2021，42(03):295-304.
[13] 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 Xuelin，DU Jingli，BAO Hong，et al. Dynamic analysis of deployable antennas considering truss flexibility[J]. Journal of Mechanical Engineering，2020，56(07):119-126.
[14] PENG Y，ZHAO Z H，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.
[15] 彭云，杨军刚，肖勇，等. 重力对大型环形可展天线展开动力学的影响研究[J]. 工程力学，2018，35(4): 226-256. PENG Yun，YANG Jungang，XIAO Yong, et al. Gravity effect on deployment dynamics of astromesh[J]. Engineering Mechanics，2018，35(4):226-256.
[16] 马小飞，杨军刚，胡建峰，等. 大型椭圆环形可展开天线展开过程动力学数值仿真[J]. 中国科学:物理学力学天文学，2019，49(2):024516. MA Xiaofei，YANG Jungang，HU Jianfeng，et al. Deployment dynamical numerical simulation on large elliptical truss antenna[J]. Scientia Sinica Physica，Mechanica & Astronomica，2019，49:024516.
[17] SIMO J C. A finite strain beam formulation. the three-dimensional dynamic problem. Part I[J]. Computer Methods in Applied Mechanics and Engineering, 1985，49:55-70.
[18] BAUCHAU O A，HAN S L，MIKKOLA A，et al. Comparison of the absolute nodal coordinate and geometrically exact formulations for beams[J]. Multibody System Dynamics，2014，32(1):67-85.
[19] SHABANA A A. Computational continuum mechanics[M]. New York City，New York:Cambridge University Press，2012.

一种新型张力-杆系结构展开过程动力学研究

Deployment Dynamics Simulation of a Novel Tension/Rod Structural System

PDF

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 3

编辑推荐

Metrics

本文评价

[1]	何玉林;黄伟;李成武;杜静;侯海臣. 大型风力发电机传动链多柔体动力学建模与仿真分析[J]. , 2014, 50(1): 152-156.
[2]	于苏洋;王挺;王志东;王越超;姚辰;李小凡. 一种采用单节变形履带机构的新型轮椅机器人[J]. , 2013, 49(13): 40-47.
[3]	张永顺;王楠;马壮. 肠道胶囊机器人的转向随动力学模型[J]. , 2012, 48(1): 84-90.