1.国防科技大学 机电工程与自动化学院， 湖南 长沙 410073，panliang.2000@gmail.com
谢愈
1.国防科技大学 机电工程与自动化学院， 湖南 长沙 410073
彭双春
1.国防科技大学 机电工程与自动化学院， 湖南 长沙 410073
徐明亮
2.北京跟踪与通信技术研究所， 北京 100094
袁天保
3.火箭军装备研究院， 北京 100094
阐明高超声速飞行器滑翔制导的基本问题，分析滑翔制导过程面临的复杂多约束、机动任务要求、参数扰动等研究难点；分别就国内外标准轨迹制导方法和预测-校正制导方法相关研究现状展开综述，指出了这两类方法中存在的问题。在此基础上，提出高超声速飞行器滑翔制导研究中亟待解决的关键问题，并指出未来滑翔制导方法的研究热点。
国家自然科学基金资助项目（11502289）
1.College of Mechatronic Engineering and Automation, National University of Defense Technology, Changsha 410073, China,panliang.2000@gmail.com
XIE Yu
1.College of Mechatronic Engineering and Automation, National University of Defense Technology, Changsha 410073, China
PENG Shuangchun
1.College of Mechatronic Engineering and Automation, National University of Defense Technology, Changsha 410073, China
XU Mingliang
2.Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094, China
YUAN Tianbao
3.Equipment Academy of the Rocket Force, Beijing 100094, China
The basic problem of gliding guidance for hypersonic vehicles was proposed, and the difficulties of complicated multiple constraints, maneuver requirements, and parameter perturbation in the course of gliding guidance were analyzed. The corresponding research status at home and abroad was surveyed, and the problems were also pointed out. On this basis, the key problems required to be solved at present in the research of gliding guidance for hypersonic vehicles were presented, and the research hotspots in the methods of future gliding guidance were also pointed out.