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In order to study the issue of whether target maneuver can get rid of the missile attack,mathematical models of target machines with different maneuvering styles and the simulation model of defensive confrontation are established. The influence of different maneuvering modes, overloads, navigational agility and other parameters on missile guidance and control system and fuze warhead coordination is analysed.The Monte Carlo simulation is carried out in combination with specific parameters and algorithms. The kill probability of air defense missile intercepting maneuvering target in whole airspace is calculated from guidance control and fuze-warhead system.The simulation results show that the different movement characteristics of target have siginificant influence on missile miss distance.
[1]金振中,袁刚.防空导弹对机动目标杀伤效果分析[J].宇航学报,2007(5):1419-1421.
[2]冷述振,才晓峰.舰空导弹拦截机动目标仿真试验分析[J].上海航天,2014,31(3):69-72.
[3]陈战辉,吴达.目标机动导致导弹脱靶判别建模与仿真[J].弹箭与制导学报,2012,32(6):1-2.
[4]肖业伦.航空航天器运动的建模——飞行动力学的理论基础[M].北京:北京航空航天大学出版社,2003.
[5]帅鹏,周波华.防空导弹对过失速机动目标拦截研究[J].空天防御,2018,1(4):65-70.
[6] Yuan P J,Hsu S C. Solutions of generalized proportional navigation with mancuvering and nonmancuvering targets[J]. IEEE Transactions on Aerospace and Electronic Systems,1995,31(1):469-474.
[7]郑平泰,杨涛.导弹破片战斗部对空中目标的杀伤概率计算[J].弹道学报,2006(1):45-47.
Basic Information:
DOI:10.16358/j.issn.1009-1300.20220563
China Classification Code:TJ761.13
Citation Information:
[1]Zhang Kai.Research on influence of target maneuver on air defense missile miss distance[J].Tactical Missile Technology,2022,No.213(03):29-33+65.DOI:10.16358/j.issn.1009-1300.20220563.
2022-06-09
2022-06-09
2022-06-09