[1] Rong Siyuan, Liu Jiafu, Cui Naigang. A review of solar sail spacecraft research and its key technology[J]. Aerospace Shanghai, 2011, 2: 53-62. (in Chinese) 荣思远, 刘家夫, 崔乃刚. 太阳帆航天器研究及其关键技术综述[J]. 上海航天, 2011, 2: 53-62.
[2]
[3]
[4] Johnson Les, Whorton Mark, Heaton Andy, et al. Nano sail-D: A solar sail demonstration mission[J]. Acta Astronautica, 2011, 68(5/6): 571-575.
[5] Johnson L, Young R, Montgomery E, et al. Status of solar sail technology within NASA[J]. Advances in Space Research, 2011, 48(11): 1687-1694.
[6]
[7]
[8] Qian Hang, Zheng Jianhua, Yu Xizheng, et al. Dynamics and control of displaced orbits for solar sail spacecraft[J]. Chin J Space Sci, 2013, 33(4): 458-464. (in Chinese) 钱航, 郑建华, 于锡峥, 等. 太阳帆航天器悬浮轨道动力学与控制[J]. 空间科学学报, 2013, 33(4): 458-464.
[9] Ma Xin, Yang Xuan, Zheng Jianhua, et al. Simulation and analysis for the flexible structure of solar sail spacecraft[J]. Aerospace Control and Application, 2014, 40(3): 36-40. (in Chinese) 马鑫, 杨萱, 郑建华, 等. 太阳帆柔性结构动力学仿真计算[J]. 空间控制技术与应用, 2014, 40(3): 36-40.
[10]
[11]
[12] Wie B. Dynamic modeling and attitude control of solar sail spacecraft:Part 1[J]. AIAA Paper, 2002, 4572: 5-8.
[13]
[14] Heiligers J, McInnes C R, Biggs J D, et al. Displaced geostationary orbits using hybrid low-thrust propulsion[J].Acta Astron, 2012, 71: 51-67.
[15] Cui Hutao, Luo Junhong, Cui Pingyuan, et al. Attitude control of solar sail spacecraft with control boom[J]. Journal of Astronautics, 2008, 29(2): 170-176. (in Chinese) 崔祜涛, 骆军红, 崔平远, 等. 基于控制杆的太阳帆姿态控制研究[J]. 宇航学报, 2008, 29(2): 170-176.
[16]
[17] 张震亚. 太阳帆推进技术发展历程与研究要点[J]. 科技创业家, 2013(13): 5-8.
[18]
[19] Tsuda Y, Mori O, Funase R, et al. Flight status of IKAROS deep space solar sail demonstrator[J]. Acta Astronautica, 2011, 69(9): 833-840.
[20]
[21] Hu Jie, Yang Xuan. Dynamic modeling of solar sail spacecraft deployment mechanism[J]. Mmcrocomputer Information, 2012, 28(4): 155-156. (in Chinese) 胡洁, 杨萱. 太阳帆航天器展开机构柔性动力学建模[J]. 微计算机信息, 2012, 28(4): 155-156.