首页 | 官方网站   微博 | 高级检索  
     

微分几何制导律捕获条件分析
引用本文:叶继坤,雷虎民,李炯,王飞.微分几何制导律捕获条件分析[J].系统工程与电子技术,2010,32(11):2403-2406.
作者姓名:叶继坤  雷虎民  李炯  王飞
作者单位:空军工程大学导弹学院, 陕西 三原 713800
基金项目:航空科学基金(20090196005)资助课题 
摘    要:基于Frenet坐标系的传统微分几何制导律推导过程较为复杂,工程应用中存在很大的局限性。首先在时域中推导了微分几何制导指令,其次为方便对导弹捕获目标条件的研究,建立了相对速度坐标系。基于此坐标系将弹目相对运动轨迹区域进行了分割,根据分割的不同区域给出导弹捕获目标的充分条件,并对其进行了证明推导。最后仿真结果表明,当弹目相对运动初始信息位于不同的区域时,根据给定的充分条件,导弹能够捕获目标,并且具有较高的制导精度。

关 键 词:制导  微分几何  相对速度  比例导引  捕获

Capture condition analysis of differential geometric guidance laws
YE Ji-kun,LEI Hu-min,LI Jiong,WANG Fei.Capture condition analysis of differential geometric guidance laws[J].System Engineering and Electronics,2010,32(11):2403-2406.
Authors:YE Ji-kun  LEI Hu-min  LI Jiong  WANG Fei
Affiliation:Missile Inst., Air Force Engineering Univ., Sanyuan 713800, China
Abstract:Based on the Frenet coordinate system, it is complicated to derive the differentric geometric guidance law, which has heavier limitation in employing the project. The differential geometric guidance law is firstly derived and the relative velocity coordinate system is built to analyze the capture condition for convenience. The relative motion area between missile and target is partioned into subsets, then the sufficient condition for capture is obtained, also the course is derived and proved. Simulation results show that the missile can capture the target and has a higher guidance precision when the initional information satisfies the sufficient condition for capture in different subsets of the relative velocity space.
Keywords:guidance  differentry geometirc  relative velocity  proportional guidance  capture
本文献已被 万方数据 等数据库收录!
点击此处可从《系统工程与电子技术》浏览原始摘要信息
点击此处可从《系统工程与电子技术》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司    京ICP备09084417号-23

京公网安备 11010802026262号