| 目标末端逃逸的变结构制导律研究 |
| |
| 引用本文： | 郭晓楠,贾晓洪,王湛.目标末端逃逸的变结构制导律研究[J].航空兵器,2006(1):8-11. |
| |
| 作者姓名： | 郭晓楠 贾晓洪 王湛 |
| |
| 作者单位： | 1. 中国空空导弹研究院,河南,洛阳,471009
2. 西北工业大学,西安,710072 |
| |
| 摘 要： | 在变结构控制理论的基础上。以零化视线角速度为滑动面设计了一种应对弹道末端目标机动逃选的变结构制导律，分析和推导了该制导律对目标机动的鲁棒性，并得出弹道收敛的条件。仿真结果表明，该制导律算法对目标的不同的末端逃逸方式具有强的鲁棒性，保证了较高的制导精度。
|
| 关 键 词： | 变结构控制 制导规律 末端逃逸 鲁棒性 |
| 文章编号： | 1673-5048（2006）01-0008-04 |
| 收稿时间： | 2005-04-19 |
| 修稿时间： | 2005-04-19 |
Study on a Variable Structure Guidance Law Against the Escape Maneuvering Target at Endgame |
| |
| GUO Xiao-nan,JIA Xiao-hong,WANG Zhan.Study on a Variable Structure Guidance Law Against the Escape Maneuvering Target at Endgame[J].Aero Weaponry,2006(1):8-11. |
| |
| Authors: | GUO Xiao-nan JIA Xiao-hong WANG Zhan |
| |
| Abstract: | For the case of the escape maneuver of the target in the endgame phase of the missile,a guidance law of variable structure,which is based on the slip plane of zeroing LOS(Line of Sight)anglar(velocity,is presented) in this paper.Based on this guidance law,the robust conditions of the ballistic convergence have been deduced and established.The simulation results show that the algorithm has strong robustness to the different kinds of the escape maneuvering way of the target. |
| |
| Keywords: | variable structure control guidance law escape maneuver at endgame robustness |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
