高速飞行器编队通信保持控制与协同制导技术研究综述  

Research Progress of Formation Communication Holding Control and Collaborative Guidance for Hypersonic Glide Vehicles

作　　者：李曦 赵长见[1] 高峰[1] 王辰琳 黄建友 LI Xi;ZHAO Changjian;GAO Feng;WANG Chenlin;HUANG Jianyou(China Academy of Launch Vehicle Technology,Beijing,100076)

机构地区：[1]中国运载火箭技术研究院,北京100076

出　　处：《导弹与航天运载技术（中英文）》2024年第1期71-76,共6页Missiles and Space Vehicles

基　　金：国家自然科学基金(12272258)。

摘　　要：在高速武器平台网络化的背景下,对于高速滑翔飞行器(以下简称“高速飞行器”)的研究不再局限于多约束下的制导方法,而是亟须破解多飞行器协同制导控制技术难题。通过总结部分军事大国研制高速飞行器的发展历程,分析了目前多飞行器协同作战的发展现状与趋势,进而引出研究多飞行器协同制导控制技术的必要性。随后分别对编队通信保持控制技术、带飞行时间约束的协同制导控制技术以及带飞行角度约束的协同制导控制技术的研究现状进行了梳理,为多高速飞行器协同作战探索解决思路,最后对多飞行器协同制导控制技术的未来发展方向进行了展望。Under the background of networked hypersonic weapon platforms,the research on hypersonic glide vehicles is no longer limited to the guidance methods under multiple constraint,but urgently needs to break through the technical difficulties of multiple vehicles cooperative guidance and control.Firstly,in order to lead to the necessity of research on multiple vehicles cooperative guidance and control,the development process of hypersonic glide vehicles of major military powers is summarized,and the development status and trend of multiple vehicles are analyzed.Secondly,to explore ideas for multiple hypersonic vehicles cooperative operations,the research status of formation communication maintenance control,collaborative guidance control with flight time constraint,and collaborative guidance control with flight angle constraint are summarized.Finally,the future development direction of multiple vehicles collaborative guidance and control is prospected.

关 键 词：高速飞行器 协同制导控制 编队通信保持 飞行角度约束 飞行时间约束 

分 类 号：V44[航空宇航科学与技术—飞行器设计]