火箭爆破器爆炸帶落點(diǎn)位置受風(fēng)影響動(dòng)力學(xué)仿真研究

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摘 要：針對(duì)火箭爆破器作戰(zhàn)運(yùn)用過程爆炸帶受風(fēng)影響偏移問題，建立受風(fēng)影響動(dòng)力學(xué)模型和不同環(huán)境風(fēng)發(fā)射角修正模型，分析研究風(fēng)速、風(fēng)向與火箭爆破器發(fā)射角之間的影響關(guān)系，并結(jié)合相關(guān)數(shù)據(jù)對(duì)模型進(jìn)行仿真驗(yàn)證。該模型可為實(shí)戰(zhàn)條件下，合理運(yùn)用火箭爆破器、提升作戰(zhàn)運(yùn)用效能提供支持。

關(guān)鍵詞：火箭爆破器;爆炸帶；落點(diǎn)位置;動(dòng)力學(xué)仿真

中圖分類號(hào)：TJ518    文獻(xiàn)標(biāo)志碼：A    DOI：10.3969/j.issn.1673-3819.2024.01.014

Dynamic simulation study on the impact of wind on the location

of the explosion belt of rocket explosive device

TU Jiangang， CHEN Shi， ZHANG Kaikai

（Army Engineering University of PLA， Xuzhou 221004， China）

Abstract： In this paper， aiming at the problem that the explosion belt is offset by wind during the operation of rocket explosive device， the dynamic model affected by wind and launching angle in different environments are established. The relationship 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.

Key words：rocket explosive device; explosion belt; location of landing point; Dynamic simulation

收稿日期：  2023-08-21修回日期：  2023-09-19

作者簡(jiǎn)介：  涂建剛（1979—），男，副教授，研究方向?yàn)楣こ萄b備保障。（剩余5695字）