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兵工学报 ›› 2006, Vol. 27 ›› Issue (1): 27-31.

• 论文 • 上一篇    下一篇

利用导引头测角信息进行遭遇段剩余飞行时间估计的算法

刘剑锋,庄志洪   

  1. 南京理工大学电子工程与光电技术学院,江苏南京210094
  • 收稿日期:2005-05-19 上线日期:2014-12-25
  • 通讯作者: 刘剑锋

The Algorithm of Time-to-go Using Angle Information Provided by Seeker During Missile-target Encounter

LIU Jian-feng, ZHUANG Zhi-hong   

  1. School of Electronic Engineering and Optoelectronic Techniques, Nanjing Ijniversity of Science and Technology, Nanjing 210094, Jiangsu, China
  • Received:2005-05-19 Online:2014-12-25
  • Contact: LIU Jian-feng

摘要: 反战术弹道导弹的导弹性能很大程度上取决于导弹引信和战斗部,为了提高反战术弹道导弹的毁伤概率,一个简洁而有效的延时估计算法是至关重要的。研究了两种利用导引头角度信息进行的剩余飞行时间估计算法,通过仿真对两种算法进行了分析。根据仿真结果,算法1对导引头角度噪声过于敏感,估计误差太大。算法2相对于算法1具有良好的性能,通过GHK滤波使估计值稳态误差较小,可以满足精确炸点控制要求。

关键词: 信息处理技术 , 反战术弹道导弹(ATBM) , 剩余飞行时间 , GHK滤波 , 仿真

Abstract: The missile performance of anti-tactical ballistic missile (ATBM) depends on missile fuze and warhead to a great extent. In order to improve the kill probability, a simple but effective time de?lay algorithm is very important. The paper does some researches on two time-to-go algorithms, which are deduced using angle information provided by the seeker fuze and are analyzed through simulation. The simulation results show that the algorithm I is too sensitive to the noise of angle and the estima?tion error is too big. Algorithm 2 has better performance than algorithm I. GHK filter can make the steady estimation error very small. It can satisfy the request of accurate burst time control.

Key words: information processing technique , ATBM , time-to-go , GHK filter , simulation

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