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作 者:韩波[1] 张凯[1] 蒋涛 HAN Bo;ZHANG Kai;JIANG Tao(Unit 92941 of PLA, Huludao 125001, Liaoning, China;Shanghai Institute of Mechanical and Electrical Engineering, Shanghai 201109, China)
机构地区:[1]中国人民解放军92941部队 [2]上海机电工程研究所
出 处:《上海航天》2019年第1期29-33,共5页Aerospace Shanghai
摘 要:针对舰空导弹飞行试验中导弹引战配合性能难以直接观测,以及靶标与典型作战对象差异较大的问题,提出了一种基于视景仿真的引战配合效率评估方法,实现了导弹对典型目标的引战配合效率评估。基于某型舰空导弹引战系统的工作原理,建立了引信启动模型、战斗部毁伤模型和目标毁伤效果评估模型,实现了对典型目标引战配合及毁伤的定量分析。仿真模型经过靶试飞行试验数据检验,仿真结果与实际靶试结果基本吻合,仿真模型得到了有效验证。所提供的毁伤评估手段可为导弹性能鉴定及导弹对防空体系贡献度提供参考依据,对后续靶场开展相关舰空导弹试验鉴定具有借鉴意义。Aiming at the difficulty with direct observation of fuze-warhead coordination and great difference between drones and opponent targets in the flight test of the ship-to-air missile, a damage evaluation method based on the fuze-warhead coordination simulation is proposed, solving the problem mentioned above. The method, based on one ship-to-air missile fuze-warhead system, realizes a quantitative analysis on damage evaluation by establishing the fuze working model, the warhead damage model and the damage evaluation model. Simulation models are verified by missile flight test data, and the simulation result fits the flight test result well. The damage evaluation method can provide the reference for missile performance evaluation and contribution degree of the missile to the anti-air system. It can also be used for the range to conduct the test evaluation of ship-to-air missiles.
分 类 号:V19[航空宇航科学与技术—人机与环境工程]
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