A Convenient Solution Method for Kill Probability of Antiaircraft Rocket Weapon

WANG Bao-hua;PEI Yi-xuan;HUO Yong-mou;XUN Pan-pan

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  • Sponsored by: China Association for Science and Technology (CAST)

    Editor-In-Chief: Xu Yida

    ISSN 1000-1093

    　

  • Hosted By: China Ordnance Society

    Published By: Acta Armamentarii

    CN 11-2176/TJ

Acta Armamentarii, a Chinese monthly journal, was first published in 1979. The journal is supervised by China Association for Science and Technology, sponsored by China Ordnance Society，and edited and published by Editorial Board of Acta Armamentarii. The Journal is included in all important domestic databases，and also collected by Engineering Index (EI, USA), Chemical Abstracts (CA, USA), Science Abstracts (SA, UK）, Abstract Journal (AJ, Russia), and Current Bibliography on Science and Technology(CBST).Acta Armamentarii has been selected into the journal Of Ordnance Science and Technology (Weapons Industry) Field Of High Quality Scientific and Technological Periodical Classification Catalogue (2022 edition), ranking T1, and the journal of Automotive Engineering Field of High Quality Scientific and technological Periodical classification Catalogue, ranking T2.
Acta Armamentarii ›› 2016, Vol. 37 ›› Issue (4) : 751-755. DOI: 10.3969/j.issn.1000-1093.2016.04.025
Research Notes

A Convenient Solution Method for Kill Probability of Antiaircraft Rocket Weapon

  • WANG Bao-hua, PEI Yi-xuan, HUO Yong-mou, XUN Pan-pan
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Abstract

A convenient solution method for kill probability of antiaircraft rocket weapon is proposed to calculate the kill capability of antiaircraft rocket weapon. On the assumption that the kill capability parameters of fragment warhead and the firing accuracy parameters of antiaircraft rocket weapon are known, a damage capability model of rocket projectile fragment is established according to the damage mechanism of antiaircraft gun AHEAD projectile against aircraft target. The kill barrage size of rocket projectile fragment is translated into an additional size of target in elevation and azimuth directions, and the hit probability of antiaircraft rocket weapon is calculated. A kill probability model of antiaircraft rocket weapon against the aircraft target is established. The kill probability to the aircraft target is computed to show the feasibility of the proposed method by And taking an antiaircraft rocket weapon for example.

Key words

ordnance science and technology / antiaircraft rocket weapon / kill probability / fragment warhead / hit probability

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WANG Bao-hua, PEI Yi-xuan, HUO Yong-mou, XUN Pan-pan. A Convenient Solution Method for Kill Probability of Antiaircraft Rocket Weapon. Acta Armamentarii. 2016, 37(4): 751-755 https://doi.org/10.3969/j.issn.1000-1093.2016.04.025

References

［1］ 肖元星．地面防空武器系统效费分析[M]．北京：国防工业出版社，2006：1-2，218-219.
XIAO Yuan-xing. Effectiveness-cost analysis of land-based air defense weapon system [M]. Beijing: National Defense Industry Press, 2006: 1-2, 218-219. (in Chinese)
[2］ 张学锋．火箭武器防空反导效能研究与系统仿真[D]．南京：南京理工大学, 2006.
ZHANG Xue-feng. Simulation research on damage probability of multiple launch rocket system intercepting aircraft [D]. Nanjing:Nanjing University of Scienceand Technology, 2006. (in Chinese)
[3］ 李铁鹏，乔相信，于锋，等．定向驱动预制破片战斗部数值模拟与试验[J]．弹箭与制导学报，2013，33(1)：89-92.
LI Tie-peng, QIAO Xiang-xin, YU Feng, et al. Numerical simulation and experiment of directional driving preformed fragment warhead [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013, 33(1): 89-92. (in Chinese)
[4］ 石志彬，高敏，杨锁昌，等．瞄准式战斗部杀伤装置结构设计研究[J]．兵工学报，2011，28(3)：373-377.
SHI Zhi-bin, GAO Min, YANG Suo-chang, et al. Research on the structural design of gimbaled warhead killing device [J]. Acta Armamentarii, 2011, 28(3): 373-377.(in Chinese)
[5］ 胡健，马大为，姚建勇，等．基于混沌神经网络的防空火箭炮交流伺服系统状态预测研究[J]．兵工学报，2015，36(2)：220-226.
HU Jian, MA Da-wei, YAO Jian-yong, et al. State forecasting research of air-defense rocket launcher AC servo system based on chaotic neural network [J]. Acta Armamentarii, 2015, 36(2): 220-226. (in Chinese)
[6］ 杨勇，吕席卷．防空火箭弹对无人机毁伤概率评估模型[J]．弹箭与制导学报，2014，34(6)：87-90.
YANG Yon, LYU Xi-juan. Damage probability assessment model of air defense rocket for UAV [J]. Journal of Projectiles, Rockets, Missiles and Guiolance, 2014, 34(6): 87-90. (in Chinese)
[7］ Zhang X F, Zhang Y X. Simulation research on damage efficiency of multiple launch rockets intercepting aircraft [J]. World Journal of Modeling and Simulation, 2008, 4(4): 312-318.
[8］ 李魁武．现代自行高炮武器系统总体技术[M]．北京：国防工业出版社，2012: 358-359, 388.
LI Kui-wu.Overall technology of modern antiaircraft weapon system[M]. Beijing: National Defense Industry Press, 2012: 358-359, 388. (in Chinese)
[9］ 王金云，王孟军，纪政．某型火箭弹对巡航导弹毁伤概率仿真分析[J]．指挥控制与仿真，2012，34(1)：92-95.
WANG Jin-yun, WANG Meng-jun, JI Zheng. Simulation analysis on damage probability of rocket intercepting cruise missile [J]. Command Control & Simulation, 2012, 34(1): 92-95. (in Chinese)

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