To study the change law of kill probability for single Air-Defense Missile(ADM) in killing scope,the factors affecting kill probability were analyzed according to kill principle of single ADM,and the mathematical model of kill probability for ADM was established.The kill probability for single ADM was calculated.The calculation methods of guidance error,priming distribution of fuze,priming probability of fuze and damage probability of warhead were respectively determined.Taking certain type ADM for instance,the change of kill probability in killing scope was analyzed;the relating table of kill probability and trajectory error was obtained by Matalab simulation.The result shows that the kill probability of single ADM gradually decreases with the increase of trajectory error.The study result offers decision strategy for controlling ADM to hit target effectively.
Key words
anti-air missile /
kill probability /
combat effectiveness
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References
[1] 张望根,郭长栋.寻的防空导弹总体设计[M].北京:中国宇航 出版社,1991. ZHANG Wang-gen,GUO Chang-dong.Macrodesignabout homingantiaircraftmissileweaponsystem[M].Beijing:China AstronauticPublishingHouse,1991.(inChinese)
[2] 谢邦荣,杨剑影.导弹单发杀伤概率影响因素分析[J].火力与 指挥控制,2000,29(2):60-64. XIEBang-rong,YANGJian-ying.Analysisoftheinfluencing factorsuponkillprobabilityforsinglemissile[J].FireControl andCommandControl,2004,29(2):60-64.(inChinese)
[3] 陈瑞源,蒋武涛.防空导弹武器指挥控制通信系统[M].北京: 中国宇航出版社,1995. CHENRui-yuan,JIANG Wu-tao.Antiaircraftmissileweapon commandcontrolandcommunicationsystem [M].Beijing: ChinaAstronauticPublishingHouse,1995.(inChinese)
[4] ГАОБо,ГОРЕВАГ.Методикиоценкиогневыхвозможностей корабельных ЗОС на этапе подготовки боевых действий. СовремнноесостояниеипутиповышенияэффективностиПВО силфлота[M].СПБ:ВСОК,2007.
[5] ГАОБО,ГОРЕВ А Г.Оптимизацияпараметровбарражирования СРЛДНвинтересахПВОприкрываемыхобъектов.Материалы11- ой Всероссийской ВПК 《Актуальные проблемы защиты и безопасности》[M].СПб:ВМАим.Н.Г.Кузнецова,2008.
[6] MANIONJ.Ballisticvulnerabilityassessmentfordesignof aircraft,AIAA0324976[R].2003.
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Footnotes
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