Citation: | HUANG Yong, LI Xiaojiang, WANG Zhiheng, LI Zhaoming. Finite-time Control of Satellites Formation[-1.5mm] Based on Terminal Sliding Mode[J]. Chinese Journal of Space Science, 2014, 34(1): 109-115. doi: 10.11728/cjss2014.01.109 |
[1] |
Zhang Yukun, Dai Jinhai. Satellite formation flying with J2 perturbation[J]. J. Natl. Univ. Def. Tech., 2002, 24(2):6-10. In Chinese (张玉锟, 戴金海. 考虑J2项摄动的卫星编队飞行[J]. 国防科技大学学报, 2002, 24(2):6-10)
|
[2] |
Yeh H H, Nelson E, Sparks A. Nonlinear tracking control for satellite formations[J]. J. Guid. Cont. Dyn., 2002, 25(2):376-386
|
[3] |
Liu Hui, Li Junfeng. Coordinated control of spacecraft formation flying[J]. J. Tsinghua Univ.: Sci. Tech., 2006, 46(11):1922-1925. In Chinese (刘辉, 李俊峰. 卫星编队飞行的协同控制[J]. 清华大学学报: 自然科学版, 2006, 46(11):1922-1925)
|
[4] |
Liu Hui, Li Junfeng. Autonomous formation control for spacecraft formation flying[J]. J. Astron., 2007, 28(5): 1138-1141. In Chinese (刘辉, 李俊峰. 卫星编队自主队形 控制[J]. 宇航学报, 2007, 28(5):1138-1141)
|
[5] |
Liu Hui, Li Junfeng, Hexi Baoyin. Sliding mode control for low-thrust Earth-orbiting spacecraft formation maneuvering[J]. Aeros. Sci. Tech., 2006, 10(7):636-643
|
[6] |
Liu Hui, Li Junfeng. Terminal sliding mode control for spacecraft formation flying[J]. IEEE Trans. Aeros. Elect. Syst., 2009, 45(3):835-846
|
[7] |
Hu Min, Zeng Guoqiang. Finit-time control for electromagnetic formations of fractionated spacecraft based on terminal sliding mode technique[J]. Aeros. Contr., 2011, 29(6):22-27. In Chinese (胡敏, 曾国强. 基于终端滑模的集 群航天器电磁编队有限时间控制[J]. 航天控制, 2011, 29(6):22-27)
|
[8] |
Hu Min, Zeng Guoqiang. Finit-time control for satellite formation flight[J]. Aeros. Contr. appl., 2012, 38(1):23-28. In Chinese (胡敏, 曾国强. 卫星编队飞行有限时 间控制方法[J]. 空间控制技术与应用, 2012, 38(1):23-28)
|
[9] |
Sail M, Ebrahimi B, Vali M. Fault tolerant control of satellite formation flying using second order sliding mode control[C]//Proceedings of the 2011 IEEE International Conference on Systems, Man and Cybernetics. Stoughton: The Print House Inc., 2011: 2015-2020
|
[10] |
Wu Y Q, Yu X H, Man Z H. Terminal sliding mode control design for uncertain dynamic systems[J]. Syst. Contr. Lett., 1998, 34(5):281-287
|
[11] |
Gao Youtao, Lu Yuping, Xu Bo. A Four-impulse control method for reconfiguration of LEO spacecraft formation flying[J]. J. Astron., 2009, 30(3):1000-1005. In Chinese (高有涛, 陆宇平, 徐波. 卫星编队飞行的探测目标指向动力 学与控制方法研究[J]. 宇航学报, 2009, 30(3):1000-1005)
|
[12] |
Meng Yunhe, Han Hongwei, Dai Jinhai. A Four-impulse control method for reconfiguration of LEO spacecraft formation flying[J]. J. Astron., 2008, 29(3):505-510. In Chinese (孟云鹤, 韩宏伟, 戴金海. 近地轨道航天器编队构型的一种四 冲量控制方法[J]. 宇航学报, 2008, 29(3):505-510)
|