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弹箭与制导学报 >

2011 , Vol. 31 >Issue 5: 57 - 60

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.05.024

导弹与制导技术

图像制导导弹落角约束的制导律设计

  • 卢莺 ,
  • 张安 ,
  • 何海峰
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  • 1 西北工业大学电子信息学院,西安 710072
    2 骊山微电子公司,西安 710065

卢莺(1976-),女,陕西汉中人,工程师,博士研究生,研究方向:导弹制导与控制。

收稿日期: 2011-02-17

  网络出版日期: 2025-05-30

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A Design of Guidance Law of Inage Guiding Missile with Terminal Angle Constraint

  • LU Ying ,
  • ZHANG An ,
  • HE Haifeng
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  • 1 School of Electronics and Information, Northwestern Polytechnical University, Xi'an 710072, China
    2 Lishan Microelectronic Corporation, Xi'an 710065, China

Received date: 2011-02-17

  Online published: 2025-05-30

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摘要

针对某些图像制导导弹限制终端攻击角的作战要求,提出一种落角约束最优导引律。该导引律形式简单,易于工程实现。仿真结果证明,能满足脱靶量小的要求,对于某些机动的目标,该制导律都能够以期望的终端攻击角度命中目标,对于目标的机动具有较好的鲁棒性。

关键词： 图像制导; 制导律; 落角约束; 变结构控制

本文引用格式

卢莺 , 张安 , 何海峰 . 图像制导导弹落角约束的制导律设计[J]. 弹箭与制导学报, 2011 , 31(5) : 57 -60 . DOI: 10.15892/j.cnki.djzdxb.2011.05.024

Abstract

According to the requirements of image guiding missile with terminal attack angle constrain, a new terminal guidance law was deduced based on the optimal control theory. The guidance law is simple and convenient to be realized in engineering. The simulation result shows that the guidance law can be used to hit the varying accelerated targets with expected terminal attack angle. The law shows better robustness for maneuvering target.

Key words： image guidance; guidance law; terminal angle constraint; variable structure control

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参考文献

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吴鹏, 杨明. 带终端攻击角度约束的变结构制导律[J]. 固体火箭技术, 2008, 31(2): 116-120.
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