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反舰可见光弹对水面目标的边缘检测算法 被引量:1
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作者 刘宗昂 杨莘元 张维义 《系统仿真学报》 CAS CSCD 北大核心 2009年第7期1991-1995,共5页
针对反舰导弹通过可见光锁定水面目标问题进行研究是十分必要的。利用目标梯度变化以及目标边缘灰度变化均方值,通过该均方值对目标运动造成的偏差和边缘模糊的综合分析,运用极值估计对断裂的边缘进行补偿。并通过Simulink和导弹逼近仿... 针对反舰导弹通过可见光锁定水面目标问题进行研究是十分必要的。利用目标梯度变化以及目标边缘灰度变化均方值,通过该均方值对目标运动造成的偏差和边缘模糊的综合分析,运用极值估计对断裂的边缘进行补偿。并通过Simulink和导弹逼近仿真实验,验证了对目标边缘的有效检测。 展开更多
关键词 反舰弹 边缘检测 梯度 灰度变化 SIMULINK 逼近
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反舰导弹喷管流场及红外辐射特征研究
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作者 桑学仪 吉亚平 +3 位作者 李建 赵亚南 朱春艳 宋敏敏 《红外》 CAS 2022年第1期35-42,共8页
为了评估反舰导弹喷管和尾流在超音速飞行状态下的流场特性和红外辐射特性,以“雄风3”反舰弹的尾喷管为研究对象,建立了相应的二维仿真计算模型。流场计算结果表明,凝相颗粒对尾喷流的流场特性有显著影响。相比于纯气相,加入凝相颗粒... 为了评估反舰导弹喷管和尾流在超音速飞行状态下的流场特性和红外辐射特性,以“雄风3”反舰弹的尾喷管为研究对象,建立了相应的二维仿真计算模型。流场计算结果表明,凝相颗粒对尾喷流的流场特性有显著影响。相比于纯气相,加入凝相颗粒后喷流轴向高温区长度明显增加,马赫数下降更快。红外辐射特征计算结果表明,喷管及尾流的红外辐射特征表现出强对称性,最大辐射强度出现在偏航角60°时,辐射强度达到103.68 W/sr。 展开更多
关键词 反舰弹 喷管 流场特性 红外辐射特征 凝相颗粒
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反舰弹斜穿甲和爆炸成型自锻弹丸形成过程的数值分析
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作者 柏劲松 李平 《爆轰波与冲击波》 2000年第4期146-155,共10页
采用流体动力学有限元方法,对亚音速钢质柱形反舰弹贯穿20mm厚钢质靶板的过程和爆炸成型自锻弹丸形成过程进行了数值模拟。在给定的破坏准则条件下,给出了弹体斜穿甲过程的三维图形分析结果,同时对斜穿甲后弹体剩余速度与近似方法计... 采用流体动力学有限元方法,对亚音速钢质柱形反舰弹贯穿20mm厚钢质靶板的过程和爆炸成型自锻弹丸形成过程进行了数值模拟。在给定的破坏准则条件下,给出了弹体斜穿甲过程的三维图形分析结果,同时对斜穿甲后弹体剩余速度与近似方法计算的弹体剩余速度进行了比较。给出了爆炸成型自锻弹丸形过程的数值结果,以及弹丸形成后的速度和长径比等。 展开更多
关键词 有限元法 侵彻 贯穿 爆炸成型 自锻 反舰弹 斜穿甲 数值分析
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Discussion of the target-missile control scheme with supersonic speed at minimum altitude
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作者 史震 于秀萍 赵万生 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2006年第1期16-19,共4页
An antiship missile with supersonic speed at minimum altitude is an effective weapon to break through a defense line. The former Soviet Union was a leader in this field since it had developed several kinds of antiship... An antiship missile with supersonic speed at minimum altitude is an effective weapon to break through a defense line. The former Soviet Union was a leader in this field since it had developed several kinds of antiship missiles which obtained supersonic speed at minimum altitudes. To counter this kind of missile, many countries have been developing corresponding antimissiles. For the purpose of verifing the antimissile missile′s effectiveness in intercepting antiship missiles, a target-missile is needed. A target-missle is cheaper and can imitate the main characteristics of antiship missiles with supersonic speed at minimum altitude. In this paper, the control scheme of a target missile flying with supersonic speed at minimum altitude is studied. To counter the problem of hedgehopping over the sea, a control scheme utilizing a SINS+altimeter was proposed. In this scheme, both the quick response ability of altitude control and the anti-jamming problem were considered. A simulation experiment shows that when an integrated altitude control system is used, the anti-disturbance ability of the integrated altitude is good and the response speed of altitude control system can be dramatically improved. 展开更多
关键词 SUPERSONIC minimum altitude target missile integrated altitude
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Numerical simulation of three interior double-layer bulkhead structures
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作者 许俊祥 《Journal of Measurement Science and Instrumentation》 CAS CSCD 2017年第2期195-198,共4页
When anti-ship missiles penetrate into the ship armor, fragments and shock waves caused by explosion will severely destroy the personnel and equipment on the ships. In this study, three double-layer bulkheads with dif... When anti-ship missiles penetrate into the ship armor, fragments and shock waves caused by explosion will severely destroy the personnel and equipment on the ships. In this study, three double-layer bulkheads with different interior sandwich structures were investigated, including X and hexagonal combined sandwich structure, cross-type honeycomb sandwich struc-ture and cell growth type honeycomb sandwich structure. The penetration processes of three different bulkhead structures were simulated by software ANSYS/LS-DYNA. The simulation shows that the double-layer bulkhead with cross-type honeycomb sandwich structure is the most suitable. Finally, the dynamic response characteristics of the cross-type sandwich bulkhead structure are analyzed. 展开更多
关键词 cross-type sandwich structure forging fragments dynamic response ship armor anti-ship missile
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