一种适用于系列化空地导弹的飞行控制器设计方法  

A Design Method of Flight Controller for Serialized Air-to-ground Missiles

作　　者：邹汝平 陈士超 张琨 李鹏 黄超凡 ZOU Ruping;CHEN Shichao;ZHANG Kun;LI Peng;HUANG Chaofan(No.203 Research Institute of China Ordnance Industries,Xi'an 710065,Shaanxi,China)

机构地区：[1]中国兵器工业第203研究所,陕西西安710065

出　　处：《兵工学报》2022年第S01期121-127,共7页Acta Armamentarii

基　　金：国防基础科研计划项目(JCKY2019208D002)。

摘　　要：为避免空地导弹系列化发展带来的飞行控制器冗余设计问题,提出一种适用于多种类型空地导弹的飞行控制器设计方法,指出系列化空地导弹飞行控制器与普通导弹飞行控制器设计的区别。通过多回路普适性限流电阻的确定,使得飞行控制器可有效执行多类型导弹点火功能。通过弹型识别电路判定导弹种类,继而选择对应导弹种类的控制模型,实现威胁目标的高效毁伤。通过系列化空地导弹的闭环飞行试验数据验证了所提方法的有效性。实测数据表明:新方法可提高空地导弹飞行控制器的普适性,显著提升系列化空地导弹研制的效率,降低研制成本。A design method of flight controller suitable for various types of air-to-ground missiles is proposed to avoid the redundancy design of flight controller caused by the development of serialized air-to-ground missiles.The differences between the traditional flight controller and the flight controller suitable for serialized air-to-ground missiles are analyzed.Through the determination of multi-loop universal current-limiting resistance,the flight controller can effectively perform various types of missile ignition functions.The type of missile is judged by circuit code recognition,and then the corresponding missile control model is selected to achieve the efficient damage to the threatening target.The proposed method was verified through the closed-loop flight test of a serialized air-to-ground missile.The test data demonstrates that the proposed method can improve the universality of the flight controller,thus improving thedevelopmental efficiency of the serialized air-to-ground missile and reducing the developmental cost.

关 键 词：空地导弹 飞行控制器 限流电阻 系列化 

分 类 号：TJ762.2[兵器科学与技术—武器系统与运用工程]