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高超声速飞行器滑翔制导方法综述
引用本文:潘亮,谢愈,彭双春,徐明亮,袁天保.高超声速飞行器滑翔制导方法综述[J].国防科技大学学报,2017,39(3):15-22.
作者姓名:潘亮  谢愈  彭双春  徐明亮  袁天保
作者单位:国防科学技术大学 机电工程与自动化学院,国防科学技术大学 机电工程与自动化学院,国防科学技术大学 航天科学与工程学院,北京跟踪与通信技术研究所,二炮装备研究院
基金项目:国家自然科学基金资助项目(11502289)
摘    要: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。

关 键 词:高超声速飞行器  滑翔制导  标准轨迹制导  预测-校正制导  综述
收稿时间:2015/10/10 0:00:00
修稿时间:2016/1/15 0:00:00

A survey of gliding guidance methods for hypersonic vehicles
PAN Liang,XIE Yu,PENG Shuangchun,XU Mingliang and YUAN Tianbao.A survey of gliding guidance methods for hypersonic vehicles[J].Journal of National University of Defense Technology,2017,39(3):15-22.
Authors:PAN Liang  XIE Yu  PENG Shuangchun  XU Mingliang and YUAN Tianbao
Institution:1.College of Mechatronic Engineering and Automation, National University of Defense Technology, Changsha 410073, China,1.College of Mechatronic Engineering and Automation, National University of Defense Technology, Changsha 410073, China,1.College of Mechatronic Engineering and Automation, National University of Defense Technology, Changsha 410073, China,2.Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094, China and 3.Equipment Academy of the Rocket Force, Beijing 100094, China
Abstract:Gliding guidance is one of the key factors in scheme design for hypersonic vehicles. Firstly, the basic problem of gliding guidance for hypersonic vehicles is proposed, and the difficulties of complicated multiple constraints, maneuver requirements, and parameter perturbation in the course of gliding guidance are analyzed; Then, the gliding guidance methods are divided into two categories: the standard trajectory guidance and predictor-corrector guidance. The corresponding research status at home and abroad is surveyed, and the problems are also pointed out. Based on which, the key problems which required to be solved at present in the research of gliding guidance for hypersonic vehicles are presented, and the research hotspots in the future are also proposed. This work can provide a good reference for the research on gliding guidance for hypersonic vehicles.
Keywords:hypersonic vehicle  gliding guidance  standard trajectory guidance  predictor-corrector guidance  survey
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