一种基于滑模非奇异的反舰导弹导引律的设计与仿真
作者:
作者单位:

(1.海军航空工程学院7系,山东 烟台 264001;2. 海军航空工程学院控制工程系,山东 烟台 264001)

作者简介:

通讯作者:

中图分类号:

TJ765.2+2

基金项目:


Design and Simulation of Anti-Ship Missiles Guidance Law Based on the Non-Singular Sliding Mode
Author:
Affiliation:

(1.Naval Aeronautical and Astronautical University,No.7 Department, Yantai Shandong 264001, China;2.Naval Aeronautical and Astronautical University, Department of Control Engineering, Yantai Shandong 264001, China)

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    提出了一种反舰导弹滑模非奇异导引律。根据反舰导弹弹道的运动学分析方法,建立了弹目相对运动的数学模型。在非奇异理论的基础上,推导出具有带落角约束的滑模非奇异导引律。通过仿真,表明了该导引律能同时满足脱靶和落角的性能指标,具有优良的鲁棒性,脱靶量更小,精度更高。相比传统的比例导引律,具有更强的实用性和有效性。

    Abstract:

    A kind of anti-ship missiles guidance law based on the non-singular sliding mode was proposed in this paper. Based on the kinematics analysis method of anti-ship ballistic missile, the mathematics model of missile target relative motion was established. On the basis of the non-singular theory, guidance law based on the non-singular sliding mode which had the angle constraint was deduced. It was showed that the guidance law could meet performance index of missing target and falling angle at the same time by simulation. The guidance law had excellent robustness. The distance of missing target was smaller, the precision was higher. Compared with the traditional proportional guidance law, it had stronger practicability and effectiveness.

    参考文献
    相似文献
    引证文献
引用本文

周源,雷军委,薛于廷.一种基于滑模非奇异的反舰导弹导引律的设计与仿真[J].海军航空大学学报,2014,29(4):301-305
ZHOU Yuan, LEI Jun-wei, XUE Yu-ting. Design and Simulation of Anti-Ship Missiles Guidance Law Based on the Non-Singular Sliding Mode[J]. JOURNAL OF NAVAL AVIATION UNIVERSITY,2014,29(4):301-305

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2015-04-08
  • 出版日期: