| 多管火箭炮刚柔耦合多体发射动力学仿真研究 |
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| 引用本文： | 冯勇,马大为,薛畅,陈兵. 多管火箭炮刚柔耦合多体发射动力学仿真研究[J]. 兵工学报, 2006, 27(3): 545-548 |
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| 作者姓名： | 冯勇 马大为 薛畅 陈兵 |
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| 作者单位： | 南京理工大学,机械工程学院,江苏,南京,210094;南京理工大学,机械工程学院,江苏,南京,210094;南京理工大学,机械工程学院,江苏,南京,210094;南京理工大学,机械工程学院,江苏,南京,210094 |
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| 摘 要： | 以多刚体动力学和柔性多体动力学理论为基础，建立了刚柔耦合多体系统动力学方程；应用ADAMS、ANSYS软件，通过建立ADAMS模型，并在模型中引入柔性定向管，对某火箭炮系统进行了发射动力学仿真和分析，得到了全炮的受力及振动情况，为今后更精确的研究火箭炮的发射过程动力学特性提供了理论参考。
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| 关 键 词： | 振动与波 刚柔耦合多体动力学 拉格朗日方程 多管火箭炮 发射动力学 |
| 文章编号： | 1000-1093（2006）03-0545-04 |
| 收稿时间： | 2004-03-14 |
| 修稿时间： | 2004-03-14 |
Simulation Studies of Coupled Rigid and Flexible Multi-body Dynamics for Multiple Launch Rocket Systems |
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| FENG Yong,MA Da-wei,XUE Chang,CHEN Bing. Simulation Studies of Coupled Rigid and Flexible Multi-body Dynamics for Multiple Launch Rocket Systems[J]. Acta Armamentarii, 2006, 27(3): 545-548 |
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| Authors: | FENG Yong MA Da-wei XUE Chang CHEN Bing |
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| Affiliation: | School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu,China |
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| Abstract: | Coupled rigid and flexible multi-body system dynamics was proposed using rigid multi-body dynamics and flexible body dynamics theories. An ADAMS simulation model was established with the ADAMS and ANSYS software. In this model, flexible launch tubes are referred to. Launching dynamics simulation and analysis of a multiple launch rocket system were performed. Simulation results of the force and the vibration in the whole multiple launch rocket system were obtained. It can be used as a theoretical foundation for investigating dynamic characteristics under the launching process of a MLRS. Additionally, it is of more importance to analyze the initial disturbance and dispersion for MLRS accurately. |
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| Keywords: | vibration and wave coupled rigid and flexible multi-body dynamics Lagrange equation multiple launch rocket system launch dynamics |
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