上海航天
上海航天
상해항천
AEROSPACE SHANGHAI
2012年
2期
55-60
,共6页
黄仁全%李为民%王刚%邓思思
黃仁全%李為民%王剛%鄧思思
황인전%리위민%왕강%산사사
弹道导弹%导弹防御%防卫区%灵敏度分析
彈道導彈%導彈防禦%防衛區%靈敏度分析
탄도도탄%도탄방어%방위구%령민도분석
Ballistic missile%Missile defense%Defended footprint%Sensitivity analysis
根据拦截弹发射时刻至拦截弹命中目标,拦截弹和弹道导弹飞行时间相等条件,基于合理假设分别建立了防卫区前置半径、后置半径、侧界半径和防卫区面积模型。在分析防御系统防卫区主要影响因素的基础上,用定量方法对某防卫区主要参数进行了灵敏度分析。研究结果对导弹防御系统的部署和使用有一定的参考价值。
根據攔截彈髮射時刻至攔截彈命中目標,攔截彈和彈道導彈飛行時間相等條件,基于閤理假設分彆建立瞭防衛區前置半徑、後置半徑、側界半徑和防衛區麵積模型。在分析防禦繫統防衛區主要影響因素的基礎上,用定量方法對某防衛區主要參數進行瞭靈敏度分析。研究結果對導彈防禦繫統的部署和使用有一定的參攷價值。
근거란절탄발사시각지란절탄명중목표,란절탄화탄도도탄비행시간상등조건,기우합리가설분별건립료방위구전치반경、후치반경、측계반경화방위구면적모형。재분석방어계통방위구주요영향인소적기출상,용정량방법대모방위구주요삼수진행료령민도분석。연구결과대도탄방어계통적부서화사용유일정적삼고개치。
According to the condition that the flight time of interceptor after launch to the time of the threat between interceptor launch and intercept were equal,the calculating models of the forward-edge footprint radius,the back-edge footprint radius,the side-edge footprint edge and the defended footprint area were established based on the reasonable assumption in this paper.Based on the analysis on the major factors effecting the defended footprint,the sensibility was analyzed by using the quantitative method.The study was valuable to the deployment and use of ballistic missile defense system.
