Mechanism design and dynamic analysis of large-scale two-dimensional deployable planar antenna

被引:0
作者
Shi C. [1 ]
Liu M.-L. [1 ]
Guo H.-W. [1 ]
Liu R.-Q. [1 ]
Ma X.-F. [2 ]
机构
[1] State Key Laboratory of Robotics and Systems, Harbin Institute of Technology, Harbin
[2] Xi'an Institute of Space Radio Technology, Xi'an
来源
Guangxue Jingmi Gongcheng/Optics and Precision Engineering | 2021年 / 29卷 / 12期
关键词
Configuration design; Dynamic analysis; Planar antenna; Structure design; Two-dimensional expansion;
D O I
10.37188/OPE.20212912.2868
中图分类号
学科分类号
摘要
The improvement of the space-to-earth observation range and observation accuracy has created demand for large-scale planar deployable antenna mechanisms. A new space large-scale two-dimensional multi-folding and unfolding planar antenna mechanism, which has been optimized for configuration, structure design, and dynamic characteristics analysis, is proposed in this study. First, a comprehensive evaluation index is established, and the overall configuration of the antenna with the best comprehensive performance is selected. Second, the structure of each part of the antenna mechanism is designed in detail and the prototype is developed. Additionally, the experimental verification of the deployment principle is carried out. Finally, the finite element model of the antenna mechanism is established, and the first five vibration frequencies of the antenna mechanism in the unfolded state and the corresponding mode shapes are obtained through simulation. Further, the cross-section parameters of each member are optimized with the system specific frequency as the optimization target. The folding ratio of the two-dimensional multi-folding and unfolding planar antenna mechanism designed in this study is greater than 17.6, which is an improvement over the folding ratio of the traditional planar antenna mechanism. The vibration fundamental frequency is 1.333 9 Hz, which helps in realizing the high rigidity support of the large planar antenna mechanism and provides a feasible scheme for the development of large planar phased array antenna mechanism in China. © 2021, Science Press. All right reserved.
引用
收藏
页码:2868 / 2876
页数:8
相关论文
共 16 条
[1]  
YIN K CH, YONG Q, HUO Y L, Et al., Design of deployable biaxial pointing mechanism for spaceborne dual-reflector offset antenna, Opt. Precision Eng, 29, 3, pp. 582-591, (2021)
[2]  
YANG H, FAN SH SH, LIU R Q., Optimization of single lenticular honeycomb boom for optical film deployable mechanism, Opt. Precision Eng, 28, 10, pp. 2244-2251, (2020)
[3]  
JIANG X, CHEN W X, NIE H T, Et al., Real-time ship target detection based on aerial remote sensing images, Opt. Precision Eng, 28, 10, pp. 2360-2369, (2020)
[4]  
GRALEWSKI M R, ADAMS L, HEDGEPETH J M., Deployable extendable support structure for the RADARSAT synthetic aperture radar antenna, 43th International Astronautical Congress, (1992)
[5]  
SRIVASTAVA S K, HAWKINS R K, BANIK B T, Et al., RADARSAT-1 image quality and calibration-a continuing success, Advances in Space Research, 28, 1, pp. 99-108, (2001)
[6]  
GIMENO M, SAN-MIGUEL-AYANZ J., Evaluation of RADARSAT-1 data for identification of burnt areas in Southern Europe, Remote Sensing of Environment, 92, 3, pp. 370-375, (2004)
[7]  
THOMAS W D R., RADARSAT-2 extendible support structure, Canadian Journal of Remote Sensing, 30, 3, pp. 282-286, (2004)
[8]  
CHIU S., Moving target parameter estimation for RADARSAT-2 Moving Object Detection EXperiment (MODEX), International Journal of Remote Sensing, 31, 15, pp. 4007-4032, (2010)
[9]  
TADONO T, SHIMADA M, WATANABE M, Et al., Overview of ALOS research and science program, Remote Sensing. Proc SPIE5570,. Sensors, Systems, and Next-Generation Satellites VIII, 5570, pp. 10-21, (2004)
[10]  
IGARASHI T., Alos mission requirement and sensor specifications, Advances in Space Research, 28, 1, pp. 127-131, (2001)