| 基于ADAMS的导弹级间分离动力学仿真 |
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| 引用本文： | 王竞男,刘莉. 基于ADAMS的导弹级间分离动力学仿真[J]. 系统仿真学报, 2006, 18(12): 3512-3514,3519 |
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| 作者姓名： | 王竞男 刘莉 |
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| 作者单位： | 北京理工大学,机电工程学院,北京,100081 |
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| 摘 要： | 利用ADAMS软件对两级套接式导弹进行动力学仿真，解决了导弹飞行过租中气动力在ADAMS中如何表达的问题；计算了套接形式下两级弹体的级间作用力；通过仿真，确定两级弹体分离迅速、平稳，并且将仿真结果与弹道动力学解算结果相比较，验证了ADAMS动力学仿真所得结果的正确性。
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| 关 键 词： | 级间分离 动力学仿真 气动力 |
| 文章编号： | 1004-731X（2006）12-3512-03 |
| 收稿时间： | 2005-09-05 |
| 修稿时间： | 2005-09-052006-03-21 |
Dynamic Simulation of Stage Separation of Missile Based on ADAMS |
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| WANG Jing-nan,LIU Li. Dynamic Simulation of Stage Separation of Missile Based on ADAMS[J]. Journal of System Simulation, 2006, 18(12): 3512-3514,3519 |
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| Authors: | WANG Jing-nan LIU Li |
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| Affiliation: | School of Mechotronics Engineering, Beijing Institute of Technology, Beijing 100081, China |
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| Abstract: | Using ADAMS software, dynamic simulation was done to the two-stage missile with sleeve joint. The aerodynamic forces on the missile in the course of separation were described accurately in ADAMS software. The forces between two stages were calculated. The separation was proved to be rapid and successful. The results were compared with the data which was got through the ballistic simulation, and the two results are similar. So the dynamic simulation means using ADAMS software is correct. |
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| Keywords: | ADAMS |
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