[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

Journal of Projectiles, Rockets, Missiles and Guidance >

2024 , Vol. 44 >Issue 6: 62 - 68

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2024.06.008

Exploration for Interception and Damage Assessment of Anti-missile Defense Based on Hardware-in-the-loop Systems

  • MA Qing 1, 2 ,
  • QIN Jingui 1, 2 ,
  • CHEN Gong 1, 2
Expand
  • 1 Chengdu Innovation Center for Intelligent Unmanned Aerial System,Chengdu 610072, Sichuan,China
  • 2 Chengdu Fluid Innovation Center,Chengdu 610072, Sichuan,China

Received date: 2024-08-29

  Online published: 2025-02-10

Fold

Abstract

At present, scholars carry out anti-missile damage assessment work basically simplifies the assessment model and assumes the derivation conditions, which has the problem of insufficient credibility. It is an effective means to enhance the credibility by injecting external fitted attitude information into the semi-physical system to reproduce the flight process of the missile, so as to carry out the damage assessment under the real ballistic rendezvous conditions. In this paper, firstly, the equations of motion of the missile model in the relative coordinate system of the target are given through the ballistic fitting of the semi-physical simulation system, and then according to the empirical formulas of the probability of the distribution of the guidance error, the probability of the distribution of the fuse activation zone and the probability of the destruction of the combat unit, combined with the semi-physical projectile-eye rendezvous conditions, the method of the determination of the integrated probability of the destruction is given. Finally, this paper carries out simulation calculations for specific examples, and analyzes the parameter characteristics and damage classifications of the simulation results. The results show that the relationship between the distance of the meeting and the azimuth angle of the fragmentation incident and the damage result, and the established damage evaluation table can predict the interception result of the interceptor to a certain extent, which can provide support and reference for the subsequent military operational decision-making.

Key words： hardware-in-the-loop simulation; target relative coordinate system; missile-target engagement; fragmentation warhead

Cite this article

MA Qing , QIN Jingui , CHEN Gong . Exploration for Interception and Damage Assessment of Anti-missile Defense Based on Hardware-in-the-loop Systems[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2024 , 44(6) : 62 -68 . DOI: 10.15892/j.cnki.djzdxb.2024.06.008

[an error occurred while processing this directive]

References

Publishing order | Descend order by publishing year | Descend order by cited within
[1]
魏庆栋, 王忠, 江光德, 等. 导弹打击目标的毁伤效果评估方法研究综述[J]. 战术导弹技术, 2023(3):76-88.

WEI Q D, WANG Z, JIANG G D, et al. Review on damage effect evaluation method of missile attacking target[J]. Tactical Missile Technology, 2023(3):76-88.

[2]
CONLEY K A, GAMACHE R M, DROTAR J T. Battle damage assessment system:US12287162[P].2009-08-04.

[3]
倪小清, 龙建国, 沈医文. 基于轨迹法和雷达回波变化的空中目标打击效果评估研究[J]. 战术导弹技术, 2012(1):77-82.

NI X Q, LONG J G, SHEN Y W. Research on air targets hitting effect evaluation based on the trajectory change and radar echo change[J]. Tactical Missile Technology, 2012(1):77-82.

[4]
周智超. 中远程舰空弹对目标拦截效果的实时评估[J]. 弹箭与制导学报, 2012, 32(4):61-63.

ZHOU Z C. The research on damage effect real-time assessment of aerial target interception by medium-range or long-range ship-to-air missile[J]. Journal of Projectiles,Rockets,Missiles and Guidance, 2012, 32(4):61-63.

[5]
LI J, YANG W, ZHANG Y G, et al. Aircraft vulnerability modeling and computation methods based on product structure and CATIA[J]. Chinese Journal of Aeronautics, 2013, 26(2):334-342.

[6]
刘一鸣, 王德荣, 熊自明, 等. 基于改进模糊层次分析法的某拦截系统防护效能评估研究[J]. 兵器装备工程学报, 2019, 40(7):113-117.

LIU Y M, WANG D R, XIONG Z M, et al. Research on protection effectiveness evaluation of an interception system based on improved fuzzy analytic hierarchy process[J]. Journal of Ordnance Equipment Engineering, 2019, 40(7):113-117.

[7]
王光源, 毛世超, 李建华. 基于马尔可夫链的舰艇反导毁伤决策研究[J]. 电光与控制, 2019, 26(1):87-91.

WANG G Y, MAO S C, LI J H. Warship anti-missile decision-making based on Markov chain[J]. Electronics Optics & Control, 2019, 26(1):87-91.

[8]
易亮, 陈敏. 水面舰船目标毁伤效果评估指标研究[J]. 舰船科学技术, 2010(7):5.

YI L, CHEN M. Study on criteria of damage effect assessment of surface warship[J]. Ship Science and Technology, 2010(7):5.

[9]
曹菲, 曹海, 朱晓菲, 等. 武器电子系统质量评估[M]. 西安: 西安电子科技大学出版社, 2014.

CAO F, CAO H, ZHU X F, et al. Quality assessment of weapon electronic systems[M]. Xi'an: Xidian University Press, 2014.

[10]
胡晓伟, 胡国平, 王宇晨. 基于贝叶斯网络的TBM拦截效果评估[J]. 弹箭与制导学报, 2012, 32(5):167-170.

HU X W, HU G P, WANG Y C. TBM intercepting effect assessment based on Bayesian networks[J]. Journal of Projectiles,Rockets,Missiles and Guidance, 2012, 32(5):167-170.

[11]
余丽山, 李彦彬, 赵永龙, 等. 基于BP神经网络的飞机抗毁伤能力评估[J]. 弹箭与制导学报, 2018, 38(1):23-26.

YU L S, LI Y B, ZHAO Y L, et al. Assessment of aircraft anti damage capability based on BP neural network[J]. Journal of Projectiles,Rockets,Missiles and Guidance, 2018, 38(1):23-26.

[12]
XU Y, YU Q, WANG Y, et al. Ground target detection and damage assessment by patrol missiles based on YOLO-VGGNet[J]. Applied Sciences, 2022, 12(19):9484.

[13]
张欣, 刘满国, 岳超, 等. 一种新型姿态注入弹道模拟半实物仿真方法[C]// 中国仿真学会.第三十四届中国仿真大会暨第二十一届亚洲仿真会议论文集. 西安: 西安现代控制技术研究所,2022:5-14.

ZHANG X, LIU M G, YUE C, et al. A new attitude injection hardware-in-the-loop simulation method for trajectory simulation[C]// CSF.Proceeding of the 34th China Simulation Conference and the 21st Asian Simulation Conference. Xi'an: Xi'an Modern Control Technology Research Institute,2022:5-14.

[14]
李云, 刘兴堂, 王学智. 地空导弹拦截目标仿真的目标毁伤判别研究[J]. 弹箭与制导学报, 2007, 27(4):160-162.

LI Y, LIU X T, WANG X Z. Research on the estimation methods of damaging target in the simulation of surface-to-air missile on intercepting target[J]. Journal of Projectiles,Rockets,Missiles and Guidance, 2007, 27(4):160-162.

[15]
郑平泰, 杨涛, 王宝敏. 拦截弹单发杀伤概率仿真计算研究[J]. 系统仿真学报, 2006, 18(7):1763-1765.

ZHENG P T, YANG T, WANG B M. Calculation research on kill probability of one missile[J]. Journal of System Simulation, 2006, 18(7):1763-1765.

[16]
陈远富. 杀伤战斗部作用下典型飞机目标易损性研究[D]. 南京: 南京理工大学, 2016.

CHEN Y F. Study on the vulnerability of typical aircraft targets under the action of killing warhead[D]. Nanjing: Nanjing University of Science and Technology, 2016.

[17]
MOTT N F. Fragmentation of shell cases[J]. Royal Society of London, 1947, 189(1018):300-308.

[18]
GURNEY R W. The initial velocities of fragments from bombs,shell,grenades[EB/OL].(1943-07-11)[2024-08-15]. https://www.researchgate.net/publication/235106871_The_Initial_Velocities_of_Fragments_from_Bombs_Shell_Grenades.

[19]
王秦英. 制导火箭弹战斗部破片威力设计研究[D]. 太原: 中北大学, 2017.

WANG Q Y. Research on the design of fragment power of guided rocket warhead[D]. Taiyuan: North University of China, 2017.

[20]
王泽, 童幼堂, 鞠巍. 舰空导弹单发毁伤概率的一种仿真计算方法[J]. 战术导弹技术, 2010(4):96-99.

WANG Z, TONG Y T, J W. A method of calculating the kill probability of single ship-to-air missile based on simulation[J]. Tactical Missile Technology, 2010(4):96-99.

Options
Outlines

/

〈 〉

[an error occurred while processing this directive]