Citation: | HU Ming, LI Wenjuan, CHEN Wenhua, TIAN Fangfei, ZHANG Yang. Motion simulation and function test on repeated fold-unfold mechanism of fan-shaped solar array[J]. Chinese Journal of Space Science, 2016, 36(1): 92-98. doi: 10.11728/cjss2016.01.092 |
[1] |
MA Xingrui, YU Dengyun, SUN Jing, et al. The researching evolvement of spacecraft deployment and driving mechanism[J]. J. Astron., 2006, 27(6):1123-1131 (马兴瑞, 于登云, 孙京, 等. 空间飞行器展开与驱动机构研究进 展[J]. 宇航学报, 2006, 27(6):1123-1131)
|
[2] |
CHEN Liemin. Spacecraft Structures and Mechan-isms[M].Beijing: China Science and Technology Press, 2005:354-374 (陈烈民. 航天器结构与机构[M]. 北京: 中国科学技术出版社, 2005:354-374)
|
[3] |
LI Junlan, YAN Shaoze, WU Xiaoyan, et al. Effectsof gravity potential on frequency of deployable panel structures[J]. J. Tsinghua. Univ. (Sci. Technol.), 2012, 52(1):25-30 (李君兰, 阎绍泽, 吴小燕, 等. 太阳翼可展结构频率的重力势影 响[J]. 清华大学学报(自然科学版), 2012, 52(1):25-30)
|
[4] |
LI Dongxu. Structural Dynamics of Flexible Spacecraft[M]. Beijing: Science Press, 2010:218-244 (李东旭. 挠性航天器 结构动力学[M]. 北京: 科学出版社, 2010:218-244)
|
[5] |
AN Yuan, GU Song, JIN Guang. Analysis and simulation of deployment motion of satellite solar array[J]. Chin. J. Opt. Appl. Opt., 2009, 2(1):29-35 (安源, 谷松, 金光. 卫星太阳翼展开运动的分析及仿真[J]. 中国光学与应用光学, 2009, 2(1):29-35)
|
[6] |
REN Shouzhi, SHANG Hongjun, PU Hailing. Dynamic simulation for deployment of a 2-dimension solar array[J]. Spacecr. Eng., 2012, 21(4):32-36 (任守志, 商红军, 濮海玲. 一种二维展开太阳翼的展开动力学仿真分析[J]. 航天器工程, 2012, 21(4):32-36)
|
[7] |
SPENCE B, WHITE S, WILDER N, et al. Next gene-ration ultra-flex technology maturation for NASA's new millennium program space technology 8[C]//IEEE Aerospace Conference. Big Sky, MT: IEEE, 2005:1-13
|
[8] |
NARAYANA B L, KUMAR H N S, NAGESH G, et al. Deployment simulation for the side panels of a spacecraft solar array[C]//13th National Conference on Mechanismsand Machines (NaCoMM07). Bangalore, India: IISc, 2007:1-8
|
[9] |
ZHANG Z J, YUAN G Z, ZOU Y J. Study on latch-up impact loads during solar wing deployment[J]. Spacecr. Eng., 2012, 21(3):31-36
|
[10] |
JONES P A, SPENCE B R. Spacecraft solar array technology trends[C]//IEEE Aerospace Conference Proceedings. Snowmass at Aspen: IEEE, 1998:141-152
|
[11] |
WHITE S F, DOUGLAS M V, TAKEDA R S, et al. Solar Arrays: US0126775[P]. 2009-05-21
|
[12] |
CHEN Tianzhi, WANG Xian, CHAI Hongyou. Method of modifying maximum impact load on solar array deployment and locking process[J]. Spacecr. Eng., 2011, 20(6):55-62 (陈天智, 王晛, 柴洪友. 太阳翼展开锁定最大冲击载荷修正方 法[J]. 航天器工程, 2011, 20(6):55-62)
|
[13] |
YOU Bindi, WANG Xinggui, CHEN Jun. Vibration and impact for deployable solar array of satellite with locking hinges[J]. J. Mech. Eng., 2012, 48(21):67-75 (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, 48(21):67-75)
|
[14] |
YUAN Jiajun. Design and Analysis of Satellite Structures[M]. Beijing: China Astronautic Publishing Com-pany, 2009:210-267 (袁家军. 卫星结构设计与分析[M]. 北京: 中 国宇航出版社, 2009:210-267)
|