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出 处:《北京航空航天大学学报》2013年第11期1449-1454,共6页Journal of Beijing University of Aeronautics and Astronautics
摘 要:针对巡航导弹初始设计阶段需要频繁进行人机对话的特点,引入拦截弹拦截性能修正因子的概念,综合运用导弹分析方法中的估计方法与检验方法,以突防效率为评价指标采用新思路建立了巡航导弹群突防舰载反导系统快速分析模型,为初始设计阶段提高巡航导弹作战性能提供快速、可靠的数学工具.基于所建立的快速分析模型,对影响巡航导弹突防典型舰载反导系统的主要因素进行灵敏度分析,分析结果可为巡航导弹设计指明方向.Aim at the characteristics of frequent human-computer dialogue of cruise missile in the initial design phase, the interceptor performance correction factor was introduced, a fast analytical model of cruise missiles penetration ship-based anti-missile system with penetration efficiency as evaluation index was estab lished with new ideas by the integrated use of estimation method and simulation method of missile analytical methods, which provided fast and reliable mathematical tools for the improvement of cruise missile operational performance in the initial design phase. Based on the establishment of fast analytical model, sensitivity analy sis of the main factors that affect cruise missiles penetration typical ship-based anti-missile system were con ducted. Results can set the direction for cruise missile design.
关 键 词:巡航导弹 拦截性能修正因子 突防效率 灵敏度分析
分 类 号:TJ761.6[兵器科学与技术—武器系统与运用工程]
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