| 多管火箭／发射装置系统全弹道模拟技术研究 |
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| 引用本文： | 宋廷伦 方远乔. 多管火箭／发射装置系统全弹道模拟技术研究[J]. 兵工学报, 1995, 16(4): 6-9 |
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| 作者姓名： | 宋廷伦 方远乔 |
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| 作者单位： | 北京理工大学 |
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| 摘 要： | 建立了多管火箭／发射装置系统7自由的全弹道模拟多体动力学随机非线性时变系统模型。编制了仿真软件对系统的密集进行了仿真计算；分析了系统的主要参量对密集度影响的敏感程度；并对缠角这一敏感参数对密集度的影响规律进行了实弹射击验证性实验，取得了预期的结果。
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| 关 键 词： | 火箭 发射装置 弹道模拟 火箭炮 |
GLOBAL-TRAJECTORY SIMULATION OF A MULTIPLE-ROCKET/LAUNCHER SYSTEM |
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| Sang Tinglun,Fang Yuanqiao. GLOBAL-TRAJECTORY SIMULATION OF A MULTIPLE-ROCKET/LAUNCHER SYSTEM[J]. Acta Armamentarii, 1995, 16(4): 6-9 |
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| Authors: | Sang Tinglun Fang Yuanqiao |
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| Affiliation: | Beijing Institute of Technology |
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| Abstract: | A 7-degree-of-freedom nonlineer,random,and time dependent model has been established for a multiple-rocket/launcher system.A simulation software has been developed and the rocket dispersion simulated.On the basis of digital simulation,ef-fects of some sensitive parameters on the weapon system performance were analyzed.Firing tests were carried out by changing the guiding angle of the launching tube,yielding satisfactory results. |
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| Keywords: | multiple-rocket launcher simulation dispersion |
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