## 留言板

 引用本文: 芦艳龙, 童中翔, 王超哲, 等 . 航空拖曳诱饵空气动力及动态特性[J]. 北京航空航天大学学报, 2011, 37(4): 395-398.
Lu Yanlong, Tong Zhongxiang, Wang Chaozhe, et al. Aerodynamic and dynamic characteristics of aeronautic towed decoy[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(4): 395-398. (in Chinese)
 Citation: Lu Yanlong, Tong Zhongxiang, Wang Chaozhe, et al. Aerodynamic and dynamic characteristics of aeronautic towed decoy[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(4): 395-398. (in Chinese)

## 航空拖曳诱饵空气动力及动态特性

###### 作者简介:芦艳龙(1982-),男,山西汾阳人,博士生,lyl_key@163.com.
• 中图分类号: TP 391.9

## Aerodynamic and dynamic characteristics of aeronautic towed decoy

• 摘要: 航空拖曳式诱饵与被保护载机的相对空间位置及投放使用方法是诱饵能否成功干扰导弹的关键因素.针对传统有限段法的不足,提出改进的拖缆有限段法,将拖曳式诱饵的动态运动特性问题转变为拖曳线与拖曳飞机航迹轴系的夹角动态计算问题.通过分析拖曳飞机的速度矢量与拖曳线的几何关系,建立了拖曳式诱饵对拖曳载机的动态跟随模型.仿真计算了拖曳飞机机动飞行时,拖曳式诱饵的动态运动特性,结果证明算法简单有效,较好地模拟了其动态跟随特性.

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##### 出版历程
• 收稿日期:  2010-01-18
• 刊出日期:  2011-04-30

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