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毁伤高超声速目标的顺轨定角引战配合研究

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为降低拦截器导引头的气动加热影响以及高相对速度对成像质量的影响,文中提出顺轨毁伤临近空间高超声速变轨飞行器的后向定角探测体制,通过约束弹目交会参数,结合高爆大飞散破片战斗部,构建后向定角的引战配合模型,实现低速拦截器有效毁伤高超声速临近空间飞行器HTV-2的目的,为防空反临系统提供一种新的前沿毁伤策略.
Study on Fuze-warhead Coordination of Backward Fixing Angle Along Orbit Destroying the Hypersonic Vehicle
Aiming at reducing the influences of aerodynamic heating of the interceptor on the infrared seeker and high relative velocity on the imaging quality,a method of destroying hypersonic variable trajectory vehicle by low-speed interceptor along or-bit is proposed. By constraining the parameters of interceptor-target rendezvous and combining a high explosive fragment war-head,a mathematical model of fuze-warhead coordination with the backward fixed angle is constructed. Through simulation,it is able to intercept a hypersonic near-space vehicle,such as HTV-2,with a low velocity interceptor. The work provides a novel damage method for air defense and anti-aircraft system.

imaging qualityalong orbithypersonic variable trajectory vehiclebackward fixed anglefuze-warhead coordination

刘清成、李佩绮、张芳洲、高小五、赵立程

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上海工程技术大学航空运输学院,上海 201620

北京理工大学材料学院,北京 100081

陕西寰宇聚能信息科技有限公司,陕西 西安 710100

上海工程技术大学城市轨道交通学院,上海 201620

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成像质量 顺轨 高超声速变轨飞行 后向定角 引战配合

2024

弹箭与制导学报
中国兵工学会 中国兵器工业第203研究所

弹箭与制导学报

CSTPCD北大核心
影响因子:0.311
ISSN:1673-9728
年,卷(期):2024.44(4)
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