[1] 张洪华, 关轶峰, 胡锦昌, 王泽国.分区四元数姿态控制.自动化学报, 2015, 41(7): 1341-1349 doi: 10.16383/j.aas.2015.c140624

Zhang Hong-Hua, Guan Yi-Feng, Hu Jin-Chang, Wang Ze-Guo. A novel attitude control strategy based on quaternion partition. Acta Automatica Sinica, 2015, 41(7): 1341-1349 doi: 10.16383/j.aas.2015.c140624
[2] 段晨阳, 汤国建, 张世杰.单轴飞轮故障时的小卫星姿态控制方法研究.航天控制, 2007, 25(3): 48-52 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=htkz200703011

Duan Chen-Yang, Tang Guo-Jian, Zhang Shi-Jie. Attitude control method of small satallite in the case of single reaction wheel failure. Aerospace Control, 2007, 25(3): 48-52 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=htkz200703011
[3] 黄静, 李传江, 马广富, 刘刚.基于广义逆的欠驱动航天器姿态机动控制.自动化学报, 2013, 39(3): 285-292 doi: 10.3724/SP.J.1004.2013.00285

Huang Jing, Li Chuan-Jiang, Ma Guang-Fu, Liu Gang. Generalised inversion based maneuver attitude control for underactuated spacecraft. Acta Automatica Sinica, 2013, 39(3): 285-292 doi: 10.3724/SP.J.1004.2013.00285
[4] 李世华, 田玉平.带两控制器刚体飞行器的姿态镇定.自动化学报, 2003, 29(2): 168-174 http://www.aas.net.cn/article/id/14096

Li Shi-Hua, Tian Yu-Ping. Attitude stabilization of a rigid spacecraft with two controls. Acta Automatica Sinica, 2003, 29(2): 168-174 http://www.aas.net.cn/article/id/14096
[5] 张洪华, 王芳, 胡锦昌, 王泽国.欠驱动挠性航天器的全姿态控制.宇航学报, 2015, 36(4): 419-429 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201504008

Zhang Hong-Hua, Wang Fang, Hu Jin-Chang, Wang Ze-Guo. All-attitude control for underactuated flexible spacecraft. Journal of Astronautics, 2015, 36(4): 419-429 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201504008
[6] 张佳为, 许诺, 伍少雄.欠驱动航天器飞轮控制方法.宇航学报, 2016, 37(5): 552-561 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201605007

Zhang Jia-Wei, Xu Nuo, Wu Shao-Xiong. Control method of underactuated spacecraft using flywheels. Journal of Astronautics, 2016, 37(5): 552-561 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201605007
[7] 段晨阳.冗余配置航天器推力动态分配方法研究[博士学位论文].哈尔滨工业大学, 2015

Duan Chen-Yang. Thrust dynamic allocation of spacecraft with redundant thrusters[Ph. D. dissertation]. Harbin Institute of Technology, 2015
[8] 郭朝礼, 张笃周, 王淑一.欠驱动航天器滑模速率阻尼控制.空间控制技术与应用, 2013, 39(4): 12-17 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=kjkzjsyyy201304003

Guo Chao-Li, Zhang Du-Zhou, Wang Shu-Yi. Sliding model control for rate damping of underactuated spacecraft. Aerospace Control and Application, 2013, 39(4): 12-17 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=kjkzjsyyy201304003
[9] 金磊, 徐世杰.带有两个飞轮的欠驱动航天器姿态稳定控制研究.中国空间科学技术, 2009, 2: 8-16 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zgkjkxjs200902002

Jin Lei, Xu Shi-Jie. Attitute stablization of an underactuated spacecraft with two reaction wheels. Chinese Space Science and Technology. 2009, 2: 8-16 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zgkjkxjs200902002
[10] 戈新生, 胡兵.基于欧拉四元数的欠驱动航天器姿态稳定性滑模控制.北京信息科技大学学报:自然科学版, 2012, 27(1): 5-11 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=bjjxgyxyxb201201002

Ge Xin-Sheng, Hu Bing. Control of attitude stabilization of underactuated spacecraft based on Euler$'$s quaternion. Journal of Beijing Information Science and Technology University, 2012, 27(1): 5-11 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=bjjxgyxyxb201201002
[11] Krishnan H, McClamroch N H, Reyhanoglu M. Attitude stabilization of a rigid spacecraft using two momentum wheel actuators, Journal of Guidance. Control, and Dynamics, 1995, 18(2): 256-263 doi: 10.2514/3.21378
[12] Horri N M, Hodgart S. Attitude stabilization of an underactuated satellite using two wheels. Aerospace Conference, Proceedings 2003 IEEE, 2003, 6: 2629-2635
[13] Horri N M, Palmer P, Hodgart S. Practical implementation of attitude-control algorithms for an underactuated satellite. Journal of Guidance, Control, and Dynamics, 2012, 35(1): 40-45 doi: 10.2514/1.54075
[14] 张洪华, 王芳.欠驱动挠性航天器的单轴指向控制.宇航学报, 2011, 32(7): 1491-1501 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201107009

Zhang Hong-Hua, Wang Fang. Single axis pointing control of underactuated flexiable spacecraft. Journal of Astronautics, 2011, 32(7): 1491-1501 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201107009
[15] 宋道喆, 耿云海, 易涛.零角动量欠驱动航天器逆最优稳定控制律设计.宇航学报, 2016, 37(6): 729-736 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201606013

Song Dao-Zhe, Geng Yun-Hai, Yi Tao. Inverse optimal stabilization of an underactuated spacecraft in a zero angular momentum mode. Journal of Astronautics, 2016, 37(6): 729-736 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201606013