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Elements of dynamics analysis of the warship launcher of anti-aircraft short range homing missiles

机译:防空短程寻的导弹的舰载发射器动力学分析要素

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摘要

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:本文提出了一种基于舰船的短程导弹发射器的物理和数学模型。进行的数值模拟可以对防空总成动力学进行分析。系统选择的响应以表征发射器运动的物理值的形式展示。

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