首页> 外文学位 >Introduction of control pins in the vicinity of missile fins for roll and yaw control.
【24h】

Introduction of control pins in the vicinity of missile fins for roll and yaw control.

机译:在导弹鳍附近引入控制销,以进行侧倾和偏航控制。

获取原文
获取原文并翻译 | 示例

摘要

A recent study performed by the United States Army Research Laboratory has shown placement of diametrically opposed pins in the vicinity of missile fins is capable of producing a roll torque. To perform a follow up investigation on the project, an opposing pin model was created to determine whether a yaw moment instead of roll torque could be imposed on the projectile. A Matlab code was written to estimate the roll torque and fin normal force generated by the two pin configurations. The code was calibrated and verified by results from Computational Fluid Dynamics and spark range test data. The effect of the pin length, radius, and placement on the roll torque and normal force were investigated. Finally, trajectory simulations were performed in PRODAS to predict the roll and yaw performances of the projectile as it reaches a downrange distance of 100 m.
机译:美国陆军研究实验室最近进行的一项研究表明,将直径相对的销钉放置在导弹鳍片附近能够产生侧倾扭矩。为了对该项目进行后续调查,创建了一个反向销模型来确定是否可以在弹丸上施加偏航力矩而不是侧倾扭矩。编写了Matlab代码,以估算由两个销配置产生的侧倾扭矩和翅片法向力。该代码已通过计算流体动力学和火花范围测试数据的结果进行了校准和验证。研究了销钉长度,半径和位置对轧制扭矩和法向力的影响。最后,在PRODAS中进行了轨迹模拟,以预测弹丸到达下限距离100 m时的侧倾和偏航性能。

著录项

  • 作者

    Pei, Jing.;

  • 作者单位

    The University of Alabama in Huntsville.;

  • 授予单位 The University of Alabama in Huntsville.;
  • 学科 Engineering Aerospace.
  • 学位 M.S.E.
  • 年度 2006
  • 页码 113 p.
  • 总页数 113
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号