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通过对国内外高超声速飞行器制导控制技术研究成果的回顾,介绍了高超声速飞行器独特的动力学特性,并分别从动力学建模及特性分析、轨迹优化与制导、稳定控制等方面分析了当前达到的技术水平、关键控制问题及存在的难点。在此基础上,结合高超声速飞行器面临的技术难点和未来发展需求,对制导控制技术后续发展方向提出了思考与建议。
Through reviewing the research achievements of guidance and control technology for hypersonic vehicle at home and abroad, the unique dynamic characteristics of hypersonic vehicle are introduced. The current kinematic characteristics of hypersonic vehicle are analyzed from the aspect of dynamics modeling and characteristics analysis, trajectory optimization and guidance, and stability control. The technical level, the key control problems and the existing difficulties. On this basis, considering the technical difficulties and future development needs of hypersonic vehicles, some suggestions and suggestions on the future development of guidance and control technology are put forward.