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《Tactical Missile Technology》 2009-04
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Study of Single Kill Probability of Air Defense Missile Based on Simulation and Calculation

Wang Miao,Song Han, Zhang Liqun (Unit 92941 Element 93,Huludao Liaoning 125001,China)  
Single kill probability of air defense missile is a key index to evaluat the combat effectiveness of missile weapon system.The detonating probability model of fuze and the conditional probability model of warhead are introduced.The mathematical model of kill probability is established.Related simulation is carried out by an example and the result is analyzed.
【Key Words】: single kill probability detonating probability of fuze conditional kill probability of warhead
【CateGory Index】: TJ761.13
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【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 LI Min-yong1,CHEN Hong-quan2 (1.Institute of Weaponry Engineering, Naval University of Engineering, Wuhan 430033, China; 2.Naval Factory No.705, Zhanjiang 524001, China);Research on Network Anti-Ship Cruise Missiles[J];Intelligence Command Control and Simulation Technigues;2004-03
2 PAN Han-Jin, ZHANG Duo-lin, WANG Hong (Missile Institute of Air Force Engineering University, Sanyuan 713800, China);Application of Grey Hierarchical Theory in Effective Evaluation for Anti-Air Missile Weapon System[J];Intelligence Command Control and Simulation Technigues;2004-05
3 WANG Jian-fei,WU Wen-jun,PENG Xiao-long,XIONG Ping (The Air Defense Command Academy,Zhengzhou 450052,China);Analysis on Effectiveness of Air-Attack Firepower of US Carrier Fighting Group[J];Intelligence Command Control and Simulation Technigues;2005-01
4 ZHAO Guo-hua, YAO Yi (Naval Submarine Academy, Qingdao 266071, China);Application of Fuzzy-AHP to the Analysis of Submarine Cruise Missile Hit Probability[J];Intelligence Command Control and Simulation Technigues;2005-06
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6 ZHU Chuan-wei, WANG Feng, ZHAO Guo-gang (Dalian Naval Academy, Dalian 116018, China);The Operational Effectiveness Model of Ship-to-Air Missile Weapon System[J];Command Control & Simulation;2006-02
7 SHI Ying,HUANG Zi-cai,HONG Jun (Artillery Academy, Hefei 230031, China);The Assessment of Joint Fire-Attacks of the Three Services[J];Command Control & Simulation;2006-04
8 WU Yin-hua, ZHANG Xing-pu (Laboratory of Naval Campaigns & Tactics of NCC,Nanjing 710016, China);Research on the Integrated Battle Ability of Air-to-Ship Missile System[J];Command Control & Simulation;2006-04
9 YANG Juan,LUO Xiao-ming,MIN Hua-qiao(The Academy of Equipment Command & Technology,Beijing 101416,China);Research on the Combat Capability Evaluation Method for Missile Combat System[J];Command Control & Simulation;2009-03
10 SI Guang-yu,PAN Feng(Jiangsu Automation Research Institute of CSIC,Lianyungang 222006,China);Research on Efficiency Evaluation Model Applied in Submarine Air Defense Missile Weapon System[J];Command Control & Simulation;2010-06
China Proceedings of conference Full-text Database 6 Hits
1 Zhou Yuan Cao Zhi-xin (Navy Arms-Command Academy,Guangdong,Guangzhou,510430);Evaluating on Influenced Factor Anti-missile Efficacy of Ship-to-air Missile[A];[C];2008
2 Cai Yuan-li Zhi Qiang Lu Cang-hai (School of Electronic & Information Engineering,Xi'an Jiaotong University,Shanxi,Xi'an,710049);On the Evaluation of Operation Effectiveness for PAC-3 Anti-TBM System[A];[C];2009
3 Yuanli CAI,Qian WEI,Qiang ZHI School of Electronic & Information Engineering,Xi’an Jiaotong University,Xi’an,China;Analytic Hierarchy Process Based Performance Evaluation for Flight Trajectories[A];[C];2011
4 Kungang YUAN,Dengdi LIU,Zhiwei ZHANG,Jinhui ZHU,Daogang JIANG The 5088th Mailbox of Air Force Command College,Beijing,China;Simulation Evaluation of Air-to-Air Missile Terminal Kill Efficiency[A];[C];2011
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6 WANG Zhe-kun~(1,2) HUANG Zhi-ying~2 (1.Ordnance Engineering College,Shijiazhuang,Hebei,050003; 2.63880 troops,People' s Liberation Army,Luoyang,Henan,471003,China);The Object Interference Efficiency Analysis of Electronic War Based on Queuing Theory[A];[C];2010
【Co-references】
Chinese Journal Full-text Database 1 Hits
1 GAO Shang (Department of Electronics and Information, East China Shipbuilding Institute, Zhenjiang 212003, China);Simulation on missile ideal trajectory under on proportion guide method[J];Computer Engineering and Design;2003-08
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