节点文献

旋转弹弹道修正引信修正能力仿真研究

Study on Correcting Ability of Trajectory Correction Fuze for Spin Stabilized Projectiles

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 李虎全李世义罗会浦肖洪兵王琴郑倩

【Author】 LI Hu-quan1, LI Shi-yi1, LUO Hui-fu1, XIAO Hong-bing1, WANG Qing1, ZHENG Qian2 (1. School of Aerospace Science and Engineering, Beijing Institute of Technology, Beijing 100081, China; 2. Ordnance Engineering College Information and Administration Branch, Shijiazhuang 050035, China)

【机构】 北京理工大学宇航科学技术学院军械学院信息与管理学院

【摘要】 首先分析了舵修正引信可行性,之后通过舵修正时全弹受力分析,给出了合并舵后对应的全弹受力表达式。在研究舵工作时弹丸攻角方程的基础上,推导出舵工作时动力平衡攻角的表达式,结合该表达式和修正力分析,提出了修正力计算公式。并对某旋转稳定弹修正力能力进行了计算仿真,结果表明所选用的舵修正某弹,修正能力足够。

【Abstract】 Firstly, the correcting feasibility of the fuze was analyzed. Then, the force expression was given through the force analysis while the projectile canard was functioning. By researching the equation of attack angle, the expression of the yaw of repose while the projectile canard was functioning was derived. Based on the expression and the analysis of the correction force, the calculation formula of the correction force was given. According to this, the correcting ability for a spin stabilized projectile was emulated. Finally, the result shows that the correcting ability is enough by using the selected canard.

  • 【文献出处】 系统仿真学报 ,Journal of System Simulation , 编辑部邮箱 ,2009年09期
  • 【分类号】TJ430.1
  • 【被引频次】15
  • 【下载频次】310
节点文献中: 

本文链接的文献网络图示:

本文的引文网络