| 基于模态综合法的发射过程刚柔耦合动力学研究 |
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| 引用本文： | 张涛,刘相新,郑斌. 基于模态综合法的发射过程刚柔耦合动力学研究[J]. 导弹与航天运载技术, 2009, 0(6) |
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| 作者姓名： | 张涛 刘相新 郑斌 |
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| 作者单位： | 北京航天发射技术研究所,北京,100076 |
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| 摘 要： | 基于模态综合法方法,利用ADAMS和ANSYS建立了导弹发射系统的刚柔耦合模型,通过对发射过程动力学仿真分析,获得了导弹的发射姿态和发射系统的动力学特性,分析结果通过试验进行了验证.
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| 关 键 词： | 倾斜发射 发射车 发射动力学 刚柔耦合 |
Rigid-flexible Coupling Dynamic Analysis During Launching Based on Component Model Synthesis |
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| Zhang Tao,Liu Xiangxin,Zheng Bin. Rigid-flexible Coupling Dynamic Analysis During Launching Based on Component Model Synthesis[J]. Missiles and Space Vehicles, 2009, 0(6) |
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| Authors: | Zhang Tao Liu Xiangxin Zheng Bin |
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| Abstract: | Based on the method of component model synthesis,a rigid-flexible coupling model of missile launcher is built by the ADAMS and ANSYS.The dynamic characteristics of missile attitude and launching system have been obtained through the dynamic analysis of the launching process.Its results have been proved by tests. |
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| Keywords: | Oblique launching Missile launcher Dynamic analysis of launching Rigid-flexible coupling |
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