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Elements of Dynamics Analysis of the Warship Launcher of Anti-Aircraft Short Range Homing Missiles

机译:防空航空归巢导弹战舰发射器动力学分析的要素

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The paper presents a physical and mathematical model of a short range missile launcher based onboard a warship. The conducted numerical simulation allowed for developing an analysis of the anti-aircraft assembly dynamics. The selected responses of the system are demonstrated in the form of physical values characterizing the launcher motion.
机译:本文介绍了基于战舰的短程导弹发射器的物理和数学模型。进行了对抗飞机组装动力学的分析的进行了数值模拟。系统的选择响应以表征发射器运动的物理值的形式进行说明。

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