摘要
为适应临近空间高超声速机动目标实现大范围机动的要求,满足未来军事技术发展的需求,对近年来高超声速飞行器制导控制技术主要面临的四个科学问题进行了论述,包括侧窗喷流致冷多场耦合条件下侧喷干扰效应机理与分析方法、非弹道式机动目标跟踪与轨迹预测方法、大空域宽马赫非弹道式机动目标多约束中制导控制机理及方法,以及高超声速机动目标高精度末制导控制机理与方法。在此基础上,对四者之间的关系进行梳理,并对四个问题的国内外研究现状及发展趋势进行阐述,以期对未来临近空间高超声速飞行器控制技术发展提供借鉴。
In order to satisfy the need of military technology development in the future,to achieve largescale maneuver of hypersonic aircraft in near space,firstly,four scientific problems are introduced with respect to guidance and control technology of hypersonic aircraft,including principle and analysis methods of lateral jet interference effects in the condition of side window jet cooling multi-field coupling,tracking and trajectory prediction for non-ballistic maneuvering target,principle and analysis methods of multi-constraint midcourse guidance control for non-ballistic maneuvering target with large space and Mach number,and principle and analysis methods of terminal guidance control with high precision for hypersonic maneuvering target. The scientific problems above is described respectively,as well as the relationship among them. The research status and development trends are summarized,to give reference to the future development of near space hypersonic vehicles’ control technology.
作者
秦雷
Qin Lei(Beijing Institute of Electronic System Engineering, Beijing 100854, China)
出处
《战术导弹技术》
北大核心
2017年第1期85-92,97,共9页
Tactical Missile Technology
关键词
侧窗喷流致冷
轨迹预测
临近空间
多约束中制导
目标跟踪
高超声速
side window jet cooling
trajectory prediction
near space
multi-constraint midcourse guidance
target tracking
hypersonic
