| 反导仿真弹道计算方法 |
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| 引用本文： | 高付申,刘兴,冯燕来. 反导仿真弹道计算方法[J]. 弹道学报, 2009, 21(2) |
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| 作者姓名： | 高付申 刘兴 冯燕来 |
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| 作者单位： | 1. 南京莱斯大型电子系统工程有限公司,南京,210007
2. 中国电子科技集团公司,第二十八研究所,南京,210007 |
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| 摘 要： | 在分析发射坐标系下来袭导弹的发动机推力、重力和空气动力的基础上,建立了反导仿真过程所需的相关参考坐标系下弹道导弹各飞行段(主动段、被动段和再入段)较为精确的弹道计算模型,研究了导弹来袭仿真、预警探测仿真和来袭导弹弹道预报等过程之间的信息流传递.该研究成果已应用于仿真试验并得到了试验验证,结果表明该方法对反导仿真系统的构建具有重要的指导意义.
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| 关 键 词： | 弹道导弹 反导 弹道计算 仿真 |
Ballistic Computation of Ballistic Missile Defense Simulation |
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| GAO Fu-shen,LIU Xing,FENG Yan-lai. Ballistic Computation of Ballistic Missile Defense Simulation[J]. Journal of Ballistics, 2009, 21(2) |
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| Authors: | GAO Fu-shen LIU Xing FENG Yan-lai |
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| Affiliation: | GAO Fu-shen1,LIU Xing2,FENG Yan-lai2(1.Nanjing Large-scale Electronics System Engineering Co.Ltd,Nanjing 210007,China,2.The 28th Research Institute,China Electronics Technology Group Corporation,China) |
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| Abstract: | Based on the analysis of the motor thrust,gravity,and aerodynamic force of coming missile under the launching coordinate system,the accurate ballistic calculation model of every flight phase(cactive phase,passive phase,and reentrant) needed in simulation process under correlative reference coordinate systems was built.The active section ballistic trajectory computing method can be used for both coming missile and antimissile.The transmission of information flow among coming missile simulation,detecting simu... |
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| Keywords: | ballistic missile antimissile ballistic computation simulation |
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