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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 meet the requirements of large-scale maneuver of hypersonic maneuvering targets in the near space and meet the requirements of the future development of military technology, four scientific problems confronting the hypersonic guidance and control technology in recent years are mainly discussed, including side-window jet cooling The mechanism and method of lateral spray interference effect under multi-field coupling conditions, the method of non-ballistic maneuvering target tracking and trajectory prediction, the guidance control mechanism and method of multi-constraint maneuvering target with wide space Mach number and the high-precision maneuvering target hypersonic Terminal guidance control mechanism and method. On this basis, the relationship between the four is sorted out, and the status quo and development trend of the four issues at home and abroad are expatiated, with a view to provide reference for the development of the control technology of space hypersonic vehicles in the near future.