机载空地导弹雷达前斜成像制导系统设计方法

陈士超; 陈笑; 陈韵; 魏靖彪; 卢福刚; 王彦华; 赵康

doi:10.12382/bgxb.2025.0273

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机载空地导弹雷达前斜成像制导系统设计方法

更新时间：2026-02-10

- 机载空地导弹雷达前斜成像制导系统设计方法
- Design Method of Airborne Forward-squint Imaging Guidance System for Airborne Air-to-ground Missile
- 兵工学报 2025年46卷第S2期页码：250273
- 作者机构：
  
  1. 西北工业大学电子信息学院, 陕西西安 710072
  2. 中国兵器工业第二○三研究所, 陕西西安 710065
  3. 陆军航空兵研究所, 北京, 101121
  4. 北京理工大学信息与电子学院, 北京, 100081
- 作者简介：
  
  * 邮箱: chenshichao@nwpu.edu.cn
- 基金信息：
  
  国家自然科学基金项目(62471393);国家自然科学基金项目(62271408);中央高校基本科研业务费资助项目(G2024KY05104)
- DOI：10.12382/bgxb.2025.0273
  中图分类号：
- 收稿：2025-04-14，
  
  网络首发：2026-02-03，
  
  纸质出版：2025
- 稿件说明：
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陈士超, 陈笑, 陈韵, 等. 机载空地导弹雷达前斜成像制导系统设计方法[J]. 兵工学报, 2025,46(S2):250273.

Shichao CHEN, Xiao CHEN, Yun CHEN, et al. Design Method of Airborne Forward-squint Imaging Guidance System for Airborne Air-to-ground Missile[J]. Acta Armamentarii, 2025, 46(S2): 250273.
陈士超, 陈笑, 陈韵, 等. 机载空地导弹雷达前斜成像制导系统设计方法[J]. 兵工学报, 2025,46(S2):250273. DOI： 10.12382/bgxb.2025.0273.

Shichao CHEN, Xiao CHEN, Yun CHEN, et al. Design Method of Airborne Forward-squint Imaging Guidance System for Airborne Air-to-ground Missile[J]. Acta Armamentarii, 2025, 46(S2): 250273. DOI： 10.12382/bgxb.2025.0273.

摘要

针对雷达制导空地导弹对地高概率目标截获难题

提出一种在前倾角固定条件下的机载空地导弹雷达前斜成像制导系统设计方法。建立机载空地导弹前斜成像制导系统总体构型

并结合导弹本体特性设计了多约束条件下的成像制导系统参数;设计三通道制导控制系统

在此基础上构建了预置前倾角度下导引头聚束模式成像的导弹飞行轨迹;分析评估系统相关参数是否满足成像制导系统的约束条件;采用后向投影算法进行成像处理

聚焦结果验证了系统设计的有效性

所提成像制导系统设计方法可为雷达制导空地导弹的精确打击提供技术支撑。

Abstract

To address the challenge of achieving high target acquisition probability for radar-guided air-to-ground missiles against ground targets

a design method for an airborne forward-squint imaging guidance system with a preset forward-tilt angle is proposed.The overall configuration of the airborne air-to-ground missile forward-squint imaging guidance system is established

and the parameters of the imaging guidance system under multiple constraints are designed according to the characteristics of the missile body.A three-channel guidance and control system is designed

upon which a missile flight trajectory imaged in the seeker spotlight mode at a preset forward-tilt angle is constructed.Subsequently

the system-related parameters are analyzed and evaluated to verify compliance with the constraints of the imaging guidance system.Finally

the backward projection algorithm is employed for imaging processing

and the focusing results validate the effectiveness of the system design.The proposed design method for the imaging guidance system can provide technical support for precision strikes of radar-guided air-to-ground missiles.

关键词

Keywords

references

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