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[an error occurred while processing this directive]After-launching Interception Probability Analysis of Helicopter-borne Long-range Air-to-ground Missile
Received date: 2011-09-08
Online published: 2025-05-29
直升机载远程空地导弹主要特点就是采用发射后截获技术,因此,发射后截获概率是影响其毁伤概率的重要因素。影响截获概率的误差源很多,文中通过对各种误差源的定量分析,指出了影响截获概率的主要误差源,提供了一种发射后截获概率的近似估算方法,在武器系统初步方案设计时,可用该方法进行发射后截获概率的计算。
关键词: 直升机载远程空地导弹; 发射后截获; 截获概率; 误差源
薛晓东 , 刘代军 , 杨亚丽 . 直升机载远程空地导弹发射后截获概率分析[J]. 弹箭与制导学报, 2012 , 32(3) : 227 -229 . DOI: 10.15892/j.cnki.djzdxb.2012.03.065
Adoption of after-launching interception technique is a major feature of helicopter-borne long-range air-to-ground missile. With quantitative analysis, the major error source that affects the interception probability was found. It provides a method of estimating the interception probability approximately. The method can be used for calculating the interception probability during preliminary scheme design phase of the weapon system.
| [1] | 李峰, 王新龙, 王起飞. 空空导弹目标截获概率研究[J]. 电光与控制, 2010. 17 (8): 15- 20. |
| [2] | 姜继庆. 发射后不管导弹的中制导:现有寻的导弹的改进[J]. 航空兵器, 1987 (6): 42- 47. |
| [3] | 闵华侨, 金钊, 张伟. 发射后不管技术在防空导弹中的应用与发展. 飞航导弹, 2006 (11): 38– 40. |
| [4] | 沈亮. 一种雷达导引头截获概率计算方法[C] // 1999年制导与引信信息网会议文集, 北京: 航天系统第一信息网, 1999: 32- 39. |
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