一种图像寻的空地导弹的制导控制方法  

A Guidance Control Method for Imaging Air-to-Ground Missiles

作　　者：邹汝平[1] 陈士超 陈韵 王玄 Zou Ruping;Chen Shichao;Chen Yun;Wang Xuan(Xi'an Modern Control Technology Research Institute,Xi'an 710065,China)

机构地区：[1]西安现代控制技术研究所,西安710065

出　　处：《战术导弹技术》2021年第1期93-98,114,共7页Tactical Missile Technology

摘　　要：鉴于图像寻的空地导弹可实现威胁目标要害部位的精确打击,提出了一种适用于图像寻的空地导弹的制导控制方法。在图像寻的制导特性详细分析的基础上,确定制导控制系统组成,给出了目标指向计算方法。通过倾斜稳定控制、姿态控制、高度控制、比例导引控制、重力补偿控制、环境适应性补偿控制、落角约束控制等控制方案的设计与有机组合,实现图像寻的空地导弹制导控制方案设计。飞行实验数据表明,采用本文所述方法可实现图像寻的空地导弹的稳定控制,飞行所得弹道和弹体姿态结果与理论设计相吻合。Precise attacking of the vital regions of the threating targets can be achieved by using the imaging air-to-ground missiles(AGMs), a guidance control method suitable for AGMs with imaging seekers is proposed. Components of the guidance control system are determined on the basis of the guidance property analysis of the imaging seekers, and the calculation method of target pointing is given. Missile body control is realized by fusing tilt stability control, attitude control, height control, proportional guidance control, gravity compensation control, environmental adoption compensation control, and terminal angular constraint control together. Results of the trajectories and the altitudes obtained from flight experiment and theoretical design fit each other.

关 键 词：图像 要害部位 空地导弹 制导控制 

分 类 号：TJ762.2[兵器科学与技术—武器系统与运用工程]