| 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.[点击复制] |
| PAN Liang,XIE Yu,PENG Shuangchun,XU Mingliang,YUAN Tianbao.A survey of gliding guidance methods for hypersonic vehicles[J].Journal of National University of Defense Technology,2017,39(3):15-22[点击复制] |
|
| |
|
|
| 本文已被：浏览 2773次 下载 3765次 |
| 高超声速飞行器滑翔制导方法综述 |
| 潘亮1, 谢愈1, 彭双春1, 徐明亮2, 袁天保3 |
| (1.国防科技大学 机电工程与自动化学院， 湖南 长沙 410073;2.北京跟踪与通信技术研究所， 北京 100094;3.火箭军装备研究院， 北京 100094) |
| 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 |
| DOI：10.11887/j.cn.201703003 |
| 投稿日期：2016-01-10 |
| 基金项目:国家自然科学基金资助项目（11502289） |
|
| A survey of gliding guidance methods for hypersonic vehicles |
| PAN Liang1, XIE Yu1, PENG Shuangchun1, XU Mingliang2, YUAN Tianbao3 |
| (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;3.Equipment Academy of the Rocket Force, Beijing 100094, China) |
| Abstract: |
| 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. |
| Key words: hypersonic vehicle gliding guidance standard trajectory guidance predictor corrector guidance survey |
|
|
|
|
|
