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火箭爆破器爆炸带落点位置受风影响动力学仿真研究

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针对火箭爆破器作战运用过程爆炸带受风影响偏移问题,建立受风影响动力学模型和不同环境风发射角修正模型,分析研究风速、风向与火箭爆破器发射角之间的影响关系,并结合相关数据对模型进行仿真验证.该模型可为实战条件下,合理运用火箭爆破器、提升作战运用效能提供支持.
Dynamic simulation study on the impact of wind on the location of the explosion belt of rocket explosive device
In this paper,aiming at the problem that the explosion belt is offset by wind during the operation of rocket explo-sive device,the dynamic model affected by wind and launching angle in different environments are established.The relation-ship between wind speed,wind direction and launching angle of rocket explosive device is analyzed and studied,and the model is simulated and verified by combining the relevant data.The model can provide method support for rational use of rocket explosive device and improvement of operational efficiency under actual combat conditions.

rocket explosive deviceexplosion beltlocation of landing pointDynamic simulation

涂建刚、陈实、张凯凯

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陆军工程大学训练基地, 江苏 徐州 221004

火箭爆破器 爆炸带 落点位置 动力学仿真

2024

指挥控制与仿真
中国船舶重工集团公司 第七一六研究所

指挥控制与仿真

CSTPCD
影响因子:0.309
ISSN:1673-3819
年,卷(期):2024.46(1)
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