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High-low Modulated Dynamic Simulation of Rigid-flexible Coupled Rocket Launcher
Author(s): 
Pages: 44-48
Year: Issue:  9
Journal: Ordnance Industry Automation

Keyword:  高低调炮随动装置刚柔耦合动力学仿真;
Abstract: 为准确描述火箭炮高低调炮中的动力学特性,对其进行刚柔耦合的动力学仿真分析.以刚柔多体动力学理论为基础,利用SolidWorks、ANSYS和ADAMS软件构建火箭炮高低随动装置刚柔耦合动力学模型,通过对模型进行检验及参数设置,并结合实际工况进行仿真对比,确定了起落架应力集中区域.仿真结果表明:该研究能准确反映火箭炮高低调炮时的动态性能,可为进行调炮的运动精度及可靠性分析提供数据支持,为高低随动装置的设计优化提供参考.
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