| 基于制导火箭的脱靶量精度分析 |
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| 引用本文： | 郭涛涛,王根,苏宗锋,赵军伟.基于制导火箭的脱靶量精度分析[J].弹箭与制导学报,2010,30(3). |
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| 作者姓名： | 郭涛涛 王根 苏宗锋 赵军伟 |
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| 作者单位： | 中国兵器工业第203研究所,西安,710065 |
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| 摘 要： | 为了提高制导火箭命中精度,基于制导火箭的控制模型,运用蒙特卡罗方法进行弹道仿真计算,得到了关于制导火箭的脱靶量数据,在此基础上分析了误差因素对火箭脱靶量精度的影响,给出改进方案,使脱靶量满足设计要求.本方法在导弹研制过程中有一定的实用性和经济性.
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| 关 键 词： | 制导火箭 误差分析 蒙特卡罗法 脱靶量 精度评估 |
Accuracy Assessment of Miss Distance Based on a Guidance Rocket |
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| GUO Taotao,WANG Gen,SU Zongfeng,ZHAO Junwei.Accuracy Assessment of Miss Distance Based on a Guidance Rocket[J].Journal of Projectiles Rockets Missiles and Guidance,2010,30(3). |
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| Authors: | GUO Taotao WANG Gen SU Zongfeng ZHAO Junwei |
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| Affiliation: | GUO Taotao,WANG Gen,SU Zongfeng,ZHAO Junwei(No.203 Research Institute of China Ordnance Industries,Xi'an 710065,China) |
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| Abstract: | Based on the control mode of guidance rocket,its trajectory was simulated and computed with the Monte Carlo method and the data were given.Then the influence of error factor on rocket miss distance was analyzed,and an improvement scheme was given. |
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| Keywords: | guidance rocket error analysis Monte Carlo method off-axis value miss distance accuracy assessment |
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