摘要
当下高速飞行武器技术的飞速发展为防空反导任务带来严峻挑战,亦对应用于空空导弹的目标轨迹预测技术与空空导弹制导技术提出全新要求。在此背景下,本文提出空空导弹目标预测与制导任务的新需求,以两种典型空空导弹为例介绍第四代空空导弹的特性,阐述了空空导弹制导系统工作方式,详细综述了高速目标轨迹预测方法、制导算法以及制导控制一体化方法的研究现状,并对比分析了各方法的优势与缺陷。最后,对仍需进一步研究的问题进行展望。
The rapid development of high-speed flight weapon technology brings severe challenges to air defense and anti-missile missions,and also puts forward new requirements for target trajectory prediction technology and air-to-air missile guidance technology.Under this background,this paper analyzes the new requirements of air-to-air missile target prediction and guidance technology,introduces the characteristics of the fourth-generation air-to-air missiles by taking two typical air-to-air missiles as examples,expounds the working principle of air-to-air missile guidance system,summarizes the research status of high-speed target trajectory prediction method,terminal guidance algorithm and integrated guidance and control method in detail,and compares and analyzes the advantages and disadvantages of each method.Finally,the problems that still need to be further researched are prospected.
作者
纪毅
王伟
张宏岩
范军芳
豆登辉
裴培
Ji Yi;Wang Wei;Zhang Hongyan;Fan Junfang;Dou Denghui;Pei Pei(School of Automation,Beijing Information Science and Technology University,Beijing 100192,China;Beijing Key Laboratory of High Dynamic Navigation Technology,Beijing Information Science and Technology University,Beijing 100192,China;School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China;Beijing Key Laboratory of UAV Autonomous Control,Beijing Institute of Technologym,Beijing 100081,China;Xi’an Modern Control Technology Research Institute,Xi’an 710065,China)
出处
《航空兵器》
CSCD
北大核心
2022年第6期15-25,共11页
Aero Weaponry
基金
国家自然科学基金项目(61903043)
北京市自然科学基金项目(4214072)。
关键词
导航、制导与控制
空空导弹
高机动目标
目标轨迹预测
制导算法
制导控制一体化
navigation
guidance and control
air-to-air missile
high maneuvering target
target trajectory prediction
guidance algorithm
integrated guidance and control
