Method of early warning for a single satellite based on missile dynamic characteristics

被引：0
|
作者：
Qiang S. [1 ]
Shen Z. [1 ]
Yi D.-Y. [1 ]
机构：
[1] College of Science, National University of Defense Technology
来源：
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2011年 / 33卷 / 10期
关键词：
Cutting plane; Early warning database; Integral trajectory; Missile thrust acceleration;
D O I：
10.3969/j.issn.1001-506X.2011.10.18
中图分类号：
学科分类号：
摘要：
It is very important to research early warning of a single satellite, because it is a necessary process and an important part of the early warning system. The early warning of a single satellite belongs to the condition of incomplete surveys and needs to estimate the missile trajectory as well as the point of descent parameter based on early warning database. Considering the missile dynamic characteristic, a method suitable for early warning of a single satellite is established to solve the deficiency existing in the method with ballistic trajectory as characteristics. Finally, the simulation comparation is carried on, and the results show that the proposed method is confirmed more reliability and feasibility.
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收藏
页码：2234 / 2238
页数：4
相关论文
共 10 条
  • [1] Sharma J., Stokes G.H., Braun C., Et al., Toward operational space-based space surveillance, Lincoln Laboratory Journal, 13, 2, pp. 309-334, (2002)
  • [2] Jasinski M., Russia strategic defense, Physics and Society, 34, 7, pp. 10-15, (2005)
  • [3] Taff L.G., Belkin B., Schweiter G.A., Statistical initial orbit determination, Journal of Spacecraft and Rockets, 29, 1, pp. 117-122, (1992)
  • [4] Beaulieu M.R., Alfriend K.T., Jerardi T., Launch detection satellite system engineering error analysis, Journal of Spacecraft and Rockets, 35, 4, pp. 487-495, (1998)
  • [5] Danis N.J., Space-based tactical ballistic missile launch parameter estimation, IEEE Trans. on Aerospace and Electronic Systems, 29, 2, pp. 412-424, (1993)
  • [6] Li Y.L., Yi D.Y., Wu Y., A new method of estimating trajectory measured by a single satellite, Journal of Ballistics, 15, 3, pp. 38-44, (2003)
  • [7] Qiang S., Shen Z., Yi D.Y., Space-based tactical ballistic missile type identification, Proc. of the 23rd International Symposium on Ballistics, pp. 713-720, (2007)
  • [8] Wafolmieph K., Tactical Ballistic Missile Design and Experiment, (1970)
  • [9] Qian X.F., Lin R.X., Zhao Y.N., The Missile Flight Mechanics, (2000)
  • [10] Kanzow C., Yamashita N., Fukushima M., Levenberg-Marquardt methods for constrained nonlinear equations with strong local convergence properties, Journal of Computational and Applied Mathematics, 172, 2, pp. 375-397, (2004)
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