Citation: | Liu Tao, Zhao Yushan, Shi Peng, et al. Combined simulation system design for trajectory planning of spacecraft proximity guidance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (4): 513-518. (in Chinese) |
[1] |
余力凡.虚拟现实技术在航天控制领域的应用[J].航天控制,2004,22(3):79-83 Yu Lifan.Application of virtual reality technology in aerospace control field[J].Aerospace Control,2004,22(3):79-83(in Chinese)
|
[2] |
张汉清,李言俊.月球探测器可视化仿真系统的开发[J].空间科学学报,2008,28(3):236-241 Zhang Hanqing,Li Yanjun.Design of a moon exploration probe simulation and visualization system[J].Chin J Space Sci,2008,28(3):236-241(in Chinese)
|
[3] |
夏丰领,赵育善.基于HLA 的地空导弹仿真系统设计[J].系统仿真学报,2007,19(2):296-299 Xia Fengling,Zhao Yushan.Surface-to-air missile simulation system design based on HLA[J].Journal of System Simulation,2007,19(2):296-299(in Chinese)
|
[4] |
周剑勇,王跃峰,罗汝斌.导弹攻防对抗仿真可视化系统的设计与实现[J].宇航学报,2009,21(18):5779-5782 Zhou Jianyong,Wang Yuefeng,Luo Rubin.Design and realization of missile attack and defense visual simulation system[J].Journal of System Simulation,2009,21(18):5779-5782(in Chinese)
|
[5] |
崔海英,李俊峰,高云峰.卫星编队飞行中Lawden 方程的误差分析[J].工程力学,2006,23(12):188-192 Cui Haiying,Li Junfeng,Gao Yunfeng.Error analysis of lawden’s equations in satellite formation flying[J].Engineering Mechanics,2006,23(12):188-192(in Chinese)
|
[6] |
李保军,师鹏,张皓,等.卫星编队队形重构中的模型选择[J].宇航学报, 2010,31(9):2101-2107 Li Baojun,Shi Peng,Zhang Hao,et al.Model selection for satellite formation flight reconfiguration[J].Journal of Astronautics,2010,31(9):2101-2107(in Chinese)
|
[7] |
Clohessy W H,Wiltshire R S.Terminal guidance system for satellite rendezvous [J].Journal of the Aerospace Sciences,1960,27(9):653-674
|
[8] |
朱彦伟.航天器近距离相对运动轨迹规划与控制研究. 长沙:国防科学技术大学航天与材料工程学院,2009 Zhu Yanwei.Trajectory planning and control for spacecraft proximity relative motion. Changsha:College of Aerospace and Material Engineering,National University of Defense Technology,2009(in Chinese)
|
[9] |
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
|
[10] |
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
|
[11] |
刘维.精通Matlab与C/C+ +混合程序设计[M].2版.北京:清华大学出版社,2008:177-198 Liu Wei.Master the matlab and C/C+ + hybrid program design[M].2 ed.Beijing:Tsinghua University Press,2008:177-198(in Chinese)
|