摘要
结合高超声速飞行器发展状况,对其姿态控制问题的研究进展进行归纳总结。首先,对高超声速飞行器现有的姿态动力学模型进行分类,总结了当前高超声速飞行器模型的几类常用的构型,以及使用较多的动力学模型。其次,详细分析了目前高超声速飞行器姿态控制系统设计所面临的主要控制问题以及相应的对策。最后,对高超声速飞行器姿态控制设计进行展望。
The research on attitude control problem for hypersonic vehicle according to the development of hypersonic vehicle is reviewed and summarized.Firstly,the existing attitude dynamics models of hypersonic vehicles are classified and summarized several common configurations of current hypersonic vehicles models,as well as the models used in more attitude control designs.Secondly,the main control problems and solutions are elaborated to obtain the desired attitude performance of hypersonic vehicles.Finally,the future of attitude control of hypersonic aircraft is forecasted.
作者
郭建国
鲁宁波
周军
Guo Jianguo;Lu Ningbo;Zhou Jun(Institute of Precision Guidance and Control,Northwestern Polytechnical University,Xi’an 710072,China)
出处
《战术导弹技术》
北大核心
2020年第4期92-99,134,共9页
Tactical Missile Technology
基金
国家自然科学基金(61973254)。
