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多管火箭炮发射间隔仿真研究

Simulation Investigation for Launching Intervals of Multi-Rocket Launch System

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【作者】 陈效全徐美丽

【Author】 CHEN Xiao-quan,XU Mei-li (No.203 Research Institute of China Ordnance Industries,Xi’an 710065,China)

【机构】 中国兵器工业第203研究所中国兵器工业第203研究所 陕西西安 710065陕西西安 710065

【摘要】 文中利用ADAMS软件,对多管火箭炮齐射过程中不同的发射间隔进行了仿真研究。对火箭弹和定向器束的初始扰动角及扰动角速度绘制了仿真曲线,并对仿真曲线进行了统计计算。通过对不同发射间隔计算结果的比较分析,以减小火箭炮初始扰动为出发点,并考虑到多管火箭炮的技术精度指标和快速反应能力,得出了较优的发射间隔范围。

【Abstract】 Tins paper were described an simulation investigation that is carried out by adapting ADAMS software to simulate varied launch intervals during MRLS’ ripple fire. According to the initial perturbation angle of rocket and diectional device and tubulence angular velocity, curves were drawn, as well as it statistic and calculated. Taking reduction of the Rocket’s initial tubulence as a starting point,though the comparing and analyzing the calculate results of varied launched intervals, a better lauch interval range is obtained in consideration of the MRLS’ accuracy and the ability of quick response.

  • 【文献出处】 弹箭与制导学报 ,Journal of Projectiles.Rockets.Missiles and Guidance , 编辑部邮箱 ,2003年02期
  • 【分类号】TJ393
  • 【被引频次】21
  • 【下载频次】233
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