[1] 陈务军,张淑杰. 空间可展开结构体系与分析导论[M]. 北京:中国宇航出版社,2006. CHEN Wujun,ZHANG Shujie. Deployable space structures and analysis theory[M]. Beijing:China Astronautic Publishing House,2006. [2] LOPEZ B C,LOU M C,GAMA E. Deployment simulations of a fold-up synthetic aperture radar array[C]//1999 American Institute of Aeronautics and Astronautics,AIAA-99-1445. [3] TAKAMATSU K A. ONODA J. New deployable truss concepts for large antenna structures or solar concentrators[J]. Journal of Spacecraft,1991,28:330-338. [4] 张祎贝,高冀峰,陈务军,等. 织物复合材料空间可展桁架模态试验与分析[J]. 振动与冲击,2018,37(17):155-160. ZHANG Yibei,GAO Jifeng,CHEN Wujun,et al. Modal tests and analysis of a weave composite space deployable truss[J]. Journal of Vibration and Shock,2018,37(17):155-160. [5] 李天,晁进涛,樊嘉. 等腰三角形空间桁架自由扭转理论分析和试验研究[J]. 工程力学,2018,35(5):223-238. LI Tian,CHAO Jintao,FAN Jia. Theoretical and experimental study on free torsion of isosceles triangular space truss[J]. Engineering Mechanics,2018,35(5):223-238. [6] 熊波,罗锡林,谭惠丰. 考虑接头作用的全复合材料桁架结构多尺度分析[J]. 工程力学,2015,32(8):229-235. XIONG Bo,LUO Xilin,TAN Huifeng. Multi-scale analysis of all-composite truss considering joint effects[J]. Engineering Mechanics,2015,32(8):229-235. [7] 游斌弟,王兴贵,陈军. 卫星太阳阵展开锁紧过程冲击振动[J]. 机械工程学报,2012,38(21):67-76. YOU Bindi,WANG Xinggui,CHEN Jun. Vibration and impact for deployable solar array of satellite with locking hinges[J]. Journal of Mechanical Engineering,2012,48(21):67-76. [8] Guerci J,Jaska E. ISAT-Innovative space-based-radar antenna technology[C]//6th IEEE Phased Array Systems and Technology Symposium,Array 2003,October 14-17,2003,Boston,MA,Institute of Electrical and Electronics Engineers Inc. 2003:45-51. [9] MURPHEY T,CLIFF E,LANE S. Matching space antenna deformation electronic compensation strategies to support structure architectures[J]. IEEE Transactions on Aerospace and Electronic Systems,2010,46(3):1422-1436. [10] LANE S A,MURPHEY T W. Overview of the innovative space-based radar antenna technology program[J]. Journal of Spacecraft and Rockets,2011,48(1):135-166. [11] 王新栋,胡伟鹏,邓子辰. 空间太阳能电站太阳能接收器二维展开过程的保结构分析[J]. 动力学与控制学报,2015,13(6):406-409. WANG Xindong,HU Weipeng,DENG Zichen. Structure preserving analysis of 2D deploying process for solar power receiver of solar power satellite[J]. Journal of Dynamics and Control,2015,13(6):406-409. [12] 卫剑征,苗常青,杜星文. 充气太阳帆板展开动力学数值模拟预报[J]. 宇航学报,2007,28(2):322-327. WEI Jianzheng,MIAO Changqing,DU Xingwen. Simulation prediction of deployment dynamics of inflatable solar array[J]. Journal of Astronautics,2007,28(2):322-327. [13] 卫剑征,谭惠丰,苗常青,等. 空间折叠薄膜管的充气展开动力学实验研究[J]. 力学学报,2011,43(1):202-207. WEI Jianzheng,TAN Huifeng,MIAO Changqing,et al. Experimental study of inflatable deployment dynamics of folded membrane booms[J]. Chinese Journal of Theoretical and Applied Mechanics,2011,43(1):202-207. [14] 刘宇艳,孟秋影,谭惠丰,等. 空间充气展开结构用刚化材料和刚化技术的研究现状[J]. 材料工程,2008(2):76-80. LIU Yuyan,MENG Qiuying,TAN Huifeng,et al. The situation of the rigidizable materials and rigidization technology used in space inflatable structures[J]. Journal of Materials Engineering,2008(2):76-80. [15] WEI Jianzheng,TAN Huifeng,WANG Weizhi,et al. Deployable dynamic analysis and on-orbit experiment for inflatable gravity-gradient boom[J]. Advances in Space Research,2015,55:639-646. [16] Sun He,LIU Yuyan,TAN Huifeng,et al. A new method to improve the stability,tensile strength,and heat resistant properties of shape-memory epoxy resins:Two-stages curing[J]. Journal of Applied Polymer Science,2014,131(4):1001-1007. [17] ZHAO Haojiang,LIU Rongqiang,GUO Hongwei,et al. Model analysis and active vibration control for space deployable truss type mast[C]//2011 IEEE International Conference on Mechatronics and Automation,August 7-10,Beijing,China:Beijing,IEEE Computer Society,2011:371-375. |