| 固体弹道式导弹射程能力仿真评定的一种方法 |
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| 引用本文： | 唐胜景,钱杏芳,张振泰,曹国敏. 固体弹道式导弹射程能力仿真评定的一种方法[J]. 弹道学报, 1994, 0(4) |
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| 作者姓名： | 唐胜景 钱杏芳 张振泰 曹国敏 |
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| 作者单位： | 北京理工大学，航天工业总公司二院 |
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| 摘 要： | 通过对影响某固体弹道式导弹射程的各种干扰因素的研究和分析，确定了各随机干扰因素的统计概型，并利用蒙特卡洛方法，进行计算机数字仿真、统计分析，评定出导弹飞行的最大射程．
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| 关 键 词： | 导弹弹道，弹道式导弹，蒙特卡洛法，弹道仿真 |
A METHOD OF EMULATING EVALUATION OF RANGE ABILITY OF A SOLID BALLISTIC MISSILE |
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| Tang Shengjing,Qian Xingfang,Zhang Zhentai,Cao Gucmin. A METHOD OF EMULATING EVALUATION OF RANGE ABILITY OF A SOLID BALLISTIC MISSILE[J]. Journal of Ballistics, 1994, 0(4) |
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| Authors: | Tang Shengjing Qian Xingfang Zhang Zhentai Cao Gucmin |
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| Abstract: | in this paper,several disturbance factors affecting the range of a solid ballistic missile are discussed and analyzed.And the statistical models of all the random factors are studied. Through the mathematical simulation and statistical analysis of a computer,the maximum range of a solid ballistic missile is evaluted by means of Monte Carlo's method. |
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| Keywords: | missiles trajectory ballistic missiles monte carlo's method trajectory simulation |
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