Rigid-Flexible-Thermal Coupling Dynamic Modeling and Hybrid Control of Membrane Antenna Spacecraft

CHEN Cheng; LIU Xiang

doi:10.21656/1000-0887.450094

Volume 46 Issue 3

Mar. 2025

Turn off MathJax

Article Contents

Article Navigation > Applied Mathematics and Mechanics > 2025 > 46(3): 283-297

CHEN Cheng, LIU Xiang. Rigid-Flexible-Thermal Coupling Dynamic Modeling and Hybrid Control of Membrane Antenna Spacecraft[J]. Applied Mathematics and Mechanics, 2025, 46(3): 283-297. doi: 10.21656/1000-0887.450094

Citation:

PDF( 3995 KB)

Rigid-Flexible-Thermal Coupling Dynamic Modeling and Hybrid Control of Membrane Antenna Spacecraft

doi: 10.21656/1000-0887.450094

CHEN Cheng¹,
LIU Xiang^{1,2
,
,}

1. Department of Engineering Mechanics, Shanghai Jiao Tong University, Shanghai 200240, P.R.China;
2. Chongqing Research Institute, Shanghai Jiao Tong University, Chongqing 401122, P.R.China

Funds:

The National Science Foundation of China(12102252

12172214)

Received Date: 2024-04-11
Rev Recd Date: 2024-05-09

Available Online: 2025-04-02

Publish Date: 2025-03-01

Abstract

Abstract

Large space membrane antenna has a great prospect in the fields of deep space exploration, space-based early warning and earth observation. Due to the large-size and high-flexibility of the membrane structure, the membrane antenna spacecraft poses challenging dynamic and control issues. Meanwhile, to maintain the working performance of the antenna, the pointing accuracy and surface accuracy must be kept strictly. Therefore, accurate dynamic modeling and effective active control of large membrane antenna are of great significance and practical interest, and attract a lot of attentions in recent years. The rigid-flexible-coupling dynamics and hybrid control of membrane antenna spacecraft were studied. First, based on the nonlinear finite method the nonlinear dynamic model for the membrane antenna structure was established, and the nonlinear dynamic model order reduction was also studied. Then, in view of the thermal flux, the rigid-flexible-thermal coupling dynamic model for the spacecraft was established by means of the hybrid coordinate method. With the component synthesis vibration suppression method and the cable-actuator-based nonlinear vibration control method, a hybrid control system was designed to control the attitude motion meanwhile reduce the nonlinear vibration.
- membrane antenna,
- rigid-flexible-thermal coupling dynamic modeling,
- nonlinear vibration,
- hybrid control

FullText(HTML)

References(17)

References

[2]MODI V J. Attitude dynamics of satellites with flexible appendages: a brief review[J]. Journal of Spacecraft and Rockets,1974,11(11): 743-751.

董召勇, 徐融, 郭海波. 一种空间碎片天基测量定位技术与参数优化[J]. 航天器工程, 2023,32(5):40-48.

(DONG Zhaoyong, XU Rong, GUO Haibo. Space-based position technology for space debris and parameters optimization design[J]. Spacecraft Engineering,2023,32(5): 40-48. (in Chinese))

[3]PREUMONT A. Vibration Control of Active Structures: an Introduction[M]. Berlin: Springer, 2018.

[4]关晓东, 杨雷. 带有大型柔性附件的变结构航天器动力学与控制仿真技术研究[C]//全国第十二届空间及运动体控制技术学术会议论文集.桂林, 2006. (GUAN Xiaodong, YANG Lei. Study on dynamics and control simulation technology of variable structure spacecraft with large flexible appendage[C]//Proceedings of the 12th National Conference on Space and Motion Control Technology. Guilin, 2006. (in Chinese))

[5]蒋建平, 李东旭. 带太阳帆板航天器刚柔耦合动力学研究[J]. 航空学报, 2006,27(3): 418-422.(JIANG Jianping, LI Dongxu. Research on rigid-flexible coupling dynamics of spacecraft with solar panel[J]. Acta Aeronautica et Astronautica Sinica,2006,27(3): 418-422. (in Chinese))

[6]和兴锁, 邓峰岩, 张烈霞, 等. 大型空间刚柔耦合组合体的动力学建模[J]. 机械科学与技术, 2004,23(5): 543-545.(HE Xingsuo, DENG Fengyan, ZHANG Liexia, et al. Dynamics modeling of large coupled rigid-flexible space platform system[J]. Mechanical Science and Technology,2004,23(5): 543-545. (in Chinese))

[7]HU Q, SHI P, GAO H. Adaptive variable structure and commanding shaped vibration control of flexible spacecraft[J]. Journal of Guidance, Control, and Dynamics,2007,30(3): 804-815.

[8]DA FONSECA I M, RADE D A, GOES L C S, et al. Attitude and vibration control of a satellite containing flexible solar arrays by using reaction wheels, and piezoelectric transducers as sensors and actuators[J]. Acta Astronautica,2017,139: 357-366.

[9]LIU X, CAI G, PENG F, et al. Active control of large-amplitude vibration of a membrane structure[J]. Nonlinear Dynamics,2018,93(2): 629-642.

[10]〖JP3〗LIU X, CAI G, PENG F, et al. Nonlinear vibration control of a membrane antenna structure[J]. Proceedings of the Institution of Mechanical Engineers (Part G): Journal of Aerospace Engineering,2019,233(9): 3273-3285.〖JP〗

[11]LIU X, LV L, CAI G. Nonlinear model order reduction and vibration control of a membrane antenna structure[J]. Advances in Space Research,2023,71(12): 5369-5385.

[12]LIU X, CAI G P. Thermal analysis and rigid-flexible coupling dynamics of a satellite with membrane antenna[J/OL]. International Journal of Aerospace Engineering,2022[2024-04-11]. https://doi.org/10.1155/2022/3256825.

[13]谢超, 张恩杰, 严飙, 等. 空间可展薄膜阵列天线构型设计与验证[J/OL]. 机械工程学报, 2023: 1-9[2024-04-11].http://kns.cnki.net/KCMS/detail/detail.aspx?filename=JXXB20231018006&dbname=CJFD&dbcode=CJFQ.(XIE Chao, ZHANG Enjie, YAN Biao, et al. Configuration design and verification of space deployable thin film array antenna[J/OL]. China Industrial Economics,2023: 1-9[2024-04-11]. http://kns.cnki.net/KCMS/detail/detail.aspx?filename=JXXB20231018006&dbname=CJFD&dbcode=CJFQ.(in Chinese))

[14]LIU S W, SINGH T. Fuel/time optimal control of spacecraft maneuvers[J]. Journal of Guidance, Control, and Dynamics,1997,20(2): 394-397.

[15]胡庆雷. 挠性航天器姿态机动的主动振动控制[D]. 哈尔滨: 哈尔滨工业大学, 2006.(HU Qinglei. Active vibration control of flexible spacecraft attitude maneuver[D]. Harbin: Harbin Institute of Technology, 2006. (in Chinese))

[16]陕晋军, 刘暾. 挠性结构的分力合成主动振动抑制方法研究[J]. 上海航天, 2001,18(6): 28-37.(SHAN Jinjun, LIU Dun. Study on component synthesis active vibration suppression methods for flexible structures[J]. Aerospace Shanghai,2001,18(6): 28-37. (in Chinese))

[17]唐颖卓, 卢光宇, 蔡国平. 基于绳索作动器的大型太空望远镜桁架结构的振动主动控制[J]. 应用数学和力学, 2022,43(2):123-131. (TANG Yingzhuo, LU Guangyu, CAI Guoping. Active vibration control of truss structures for large space telescopes based on cable actuators[J]. Applied Mathematics and Mechanics,2022,43(2): 123-131. (in Chinese))

Relative Articles

Supplements(0)

Cited By

Proportional views