| 多管火箭随机发射与飞行动力学仿真 |
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| 引用本文： | 芮筱亭,王国平,陈卫东,贠来峰.多管火箭随机发射与飞行动力学仿真[J].南京理工大学学报(自然科学版),2003,27(5):616-620. |
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| 作者姓名： | 芮筱亭 王国平 陈卫东 贠来峰 |
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| 作者单位： | 南京理工大学动力工程学院,南京,210094 |
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| 摘 要： | 该文从武器全系统弹、炮、药、环境一体化的角度，在多管火箭发射与飞行动力学的理论研究的基础上，形成了多管火箭随机发射与飞行动力学数值仿真系统。对某多管火箭振动特性、动力响应及射击密集度等进行了数值仿真，仿真结果得到了一系列试验验证。由仿真系统仿真得出的某多管火箭武器密集度试验方案减少了试验用弹量82．5％。
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| 关 键 词： | 多管火箭发射 火箭 发射动力学 飞行动力学 仿真 |
| 修稿时间： | 2003年5月9日 |
Simulation of Random Launch and Flight Dynamics of MLRS |
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| RuiXiaoting WangGuoping ChengWeidong YunLaifeng.Simulation of Random Launch and Flight Dynamics of MLRS[J].Journal of Nanjing University of Science and Technology(Nature Science),2003,27(5):616-620. |
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| Authors: | RuiXiaoting WangGuoping ChengWeidong YunLaifeng |
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| Abstract: | By studying the theory of launch and flight dynamics of Multiple Launch Rocket System (MLRS) from the point of whole system including launching device, rockets, propellant and environment, the simulation system of random launch and flight dynamics of MLRS is established. The simulated results of vibration characteristics, response, and dispersion of MLRS in launching process are verified by series of tests. A new method acquired from the simulation system has reduced the number of rockets used in dispersion test for one MLRS by 82.5 %. |
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| Keywords: | multiple launch rocket system rockets launch dynamics flight dynamics simulation |
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