反临近空间高超声速飞行器若干研究进展  

Some Achievements on Interception of Near Space Hypersonic Vehicles

作　　者：赵良玉[1] 雍恩米[2] 王波兰 ZHAO Liang-yu;YONG En-mi;WANG Bo-lan(School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China;China Aerodynamics Research and Development Center,Mianyang 621000,China;Shanghai Electromechanical Engineering Institute,Shanghai 201109,China)

机构地区：[1]北京理工大学宇航学院飞控系,北京100081 [2]中国空气动力研究与发展中心,绵阳621000 [3]上海机电工程研究所,上海201109

出　　处：《宇航学报》2020年第10期1239-1250,共12页Journal of Astronautics

基　　金：国家自然科学基金重点项目(11532002)。

摘　　要：为了支撑我国反临近空间高超声速飞行器相关领域的基础研究和工程研制,在分析典型临近空间高超声速目标飞行特性和作战任务剖面的基础上,综述了目标预警探测、轨迹跟踪预测、制导控制方法、拦截攻击策略四个方面的若干研究成果,讨论了每个方面存在的技术难题和可行的解决方案,并建议从天/临/空/地/海体系预警、红外多模复合敏感、可攻击区轨迹预测、直/气复合等先进控制、协同拦截防御等方面给予重点研究。In order to support the fundamental research and engineering development on interception of near space hypersonic vehicles in China,following the introduction of the flight characteristics and mission profiles of the typical near space hypersonic targets,the research achievements including target early warning and detection,trajectory tracking and prediction,guidance and control methods,and interception strategies are reviewed.Some key technical issues and feasible solutions in each aspect are discussed.It is suggested that the research should focus on early warning with space/near space/air/ground/sea system,infrared multi-mode seeker,direct/aerodynamic force control,collaborative interception and defense and so on.

关 键 词：高超声速飞行器 临近空间 拦截 轨迹预测 制导控制 

分 类 号：TJ762.5[兵器科学与技术—武器系统与运用工程]