空天防御2025，Vol.8Issue(6)：1-15,15.
偏转弹头导弹关键技术研究综述
A Comprehensive Review of Key Technologies for Deflectable-Nose Missiles
摘要
Abstract
Conventional air-to-air missiles with aerodynamic control surfaces have limitations in terminal interception against high-speed,highly maneuverable targets.At the same time,the presence of exposed fins also constrains the loading efficiency on fighter jets.As a feasible and efficient control approach,nose deflection control technology has gradually demonstrated considerable engineering potential.It is expected to provide valuable reference information for the development of next-generation missile control technologies.This paper first systematically reviewed the historical development and current research status of nose deflection control.Then,it provided a comprehensive analysis of research endeavors related to aerodynamic characteristics,configuration optimization,dynamic modeling,and control system design,as well as the mechanism design and simulation of nose-deflection-based missiles.Finally,this paper summarized the significant research progress and anticipated the future trends in the development of nose deflection control technology.关键词
偏转弹头控制/气动特性/动力学建模/偏转机构Key words
deflection nose control/aerodynamic characteristics/dynamics modeling/deflection mechanism分类
军事科技引用本文复制引用
王健磊,张知朴,孔晓俊,张顺家,龚春林..偏转弹头导弹关键技术研究综述[J].空天防御,2025,8(6):1-15,15.基金项目
中国航天科技集团有限公司第八研究院产学研合作基金项目(SAST2023-003) （SAST2023-003）
