高速飞行器俯冲段制导控制一体化综述  

Overview of Integrated Guidance and Control for Hypersonic Vehicles in Dive Phase

作　　者：郭建国[1] 梁乐成 周敏[1] 蒋瑞民[1] Guo Jianguo;Liang Lecheng;Zhou Min;Jiang Ruimin(Institute of Precision Guidance and Control,Northwestern Polytechnical University,Xi’an 710072,China)

机构地区：[1]西北工业大学精确制导与控制研究所,西安710072

出　　处：《航空兵器》2023年第1期1-10,共10页Aero Weaponry

基　　金：国家自然科学基金项目(61973254,62003270,62103331)。

摘　　要：本文从模型构建和方法设计两个方面对高速飞行器俯冲段制导控制一体化问题进行综述。首先,对俯冲段制导控制一体化模型构建进行总结,依据系统集成度提升程度的不同,分别对分通道制导控制一体化模型、全状态耦合高阶一体化模型,以及集成度提升低阶一体化模型构建进行了介绍,并对飞行器系统和设计模型特性进行了分析,指出了面临的主要设计问题。其次,针对俯冲段制导控制一体化设计难点,从快时变强不确定性鲁棒控制、高阶非匹配不确定性控制,以及考虑多约束控制方面对设计方法进行综述,总结并评述了国内外相关理论的发展现状和不足。最后,对俯冲段制导控制一体化的发展趋势进行了展望。The integrated guidance and control(IGC)problem for hypersonic vehicles in dive phase is reviewed from the perspective of model construction and method design in this paper.Firstly,this paper summarizes model construction of IGC in dive phase.In the sequence of integration improving degree,it introduces IGC model of individual channels,coupling full state high-order IGC model,improved integrated low-order IGC model,and analyzes and summarizes the characters of hypersonic vehicles system and design models,then points out typical problems of system faced in method design.Secondly,with respect to design difficulties of IGC system in dive phase,this paper reviews design methods from views of robust control under strong uncertainties,control methods under high-order mismatched uncertainties and control methods with multiple constraints.It points out the current development and existing problems of related theories at home and abroad.Finally,the IGC for hypersonic vehicles in dive phase is forecasted.

关 键 词：高速飞行器 制导控制一体化 俯冲段 不确定性 多约束控制 鲁棒控制 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程] V249[航空宇航科学与技术—飞行器设计]