Citation: | Li Baojun, Shi Peng, Zhang Hao, et al. Satellites formation reconfiguration with multiple impulses[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(8): 950-952. (in Chinese) |
[1] Kapila V, Sparks A G, Buffington J M, et al. Spacecraft formation flying: dynamics and control [J]. Journal of Guidance, Control and Dynamics, 2000, 23(3): 561-564 [2] 林来兴.分布式空间系统和航天器编队飞行辨析[J].航天器工程,2008, 17(4):24-29 Lin Laixing. Study on distributed space systems and spacecraft formation flying [J]. Spacecraft Engineering, 2008, 17(4):24-29(in Chinese) [3] Ichimura Y, Ichikawa A. Optimal impulsive relative orbit transfer along a circular orbit [J]. Journal of Guidance, Control and Dynamics, 2008,31(4):1014-1027 [4] 孟云鹤,韩宏伟,戴金海. 近地轨道航天器编队构形重构的一种四冲量控制方法[J].宇航学报, 2008, 29(2):505-510 Meng Yunhe, Han Hongwei, Dai Jinhai. A four-impulses control method for reconfiguration of LEO spacecraft formation flying[J]. Journal of Astronautics, 2008, 29(2):505-510(in Chinese) [5] Vaddi S S, Alfriend K T,Vadali S R. et al. Formation establishment and reconfiguration using impulsive control [J]. Journal of Guidance, Control and Dynamics,2005, 28(2):262-268 [6] Lawden D F. Optimal trajectories for space navigation[M]. London: Butterworths, 1963 [7] Carter T E. New form for the optimal rendezvous equations near a keplerian orbit[J]. Journal of Guidance, Control, and Dynamics, 1990, 13(1): 183-186 [8] 崔海英,李俊峰,高云峰.基于Lawden方程的理想编队队形设计[J].清华大学学报(自然科学版),2006,46(2):271-275 Cui Haiying, Li Junfeng, Gao Yunfeng. Ideal relative trajectories design based on Lawden-s equations[J]. Journal Of Tsinghua University(Science & Technology), 2006, 46(2):271-275(in Chinese) [9] Yamanak K, Ankersen F.New state transition matrix for relative motion on an arbitrary elliptical orbit[J]. Journal Of Guidance, Control, and Dynamics, 2002, 25(1):60-66
|