高超声速飞行器控制技术研究进展与展望  

Research Progress and Prospect of the Hypersonic Flight Vehicle Control Technology

作　　者：张远 黄旭 路坤锋[1,2] 白文艳 黄万伟 ZHANG Yuan;HUANG Xu;LU Kunfeng;BAI Wenyan;HUANG Wanwei(Beijing Aerospace Automatic control Institute,Beijing 100854,China;National Key Laboratory of Science and Technology on Aerospace Intelligent Control,Beijing 100854,China)

机构地区：[1]北京航天自动控制研究所,北京100854 [2]宇航智能控制技术国家级重点实验室,北京100854

出　　处：《宇航学报》2022年第7期866-879,共14页Journal of Astronautics

基　　金：国家自然科学基金(61773341,U21B2028)。

摘　　要：针对一类包含可变构型在内的高超声速飞行器的难点,分析了工程应用需求,综述了几类典型的非线性控制方法的研究进展。首先针对高超声速飞行器的几类常见研究模型,总结了模型来源及特点;其次,以实际工程需求为出发点,分析了此类飞行器的控制难点及对于控制系统能力提出的需求;再者,总结了高超声速飞行器几种典型非线性控制及智能控制研究的基本情况和进展,并给出了各类控制方案的框架;最后,面向未来任务形式多样化、环境复杂化的飞行器控制,讨论了可以进一步研究的问题和方向。Aiming at the difficulties of a class of hypersonic flight vehicle(HFV) involving variable configurations, the engineering application requirements are analyzed, and the research progress of several typical nonlinear control methods is summarized. Firstly, the sources and characteristics of several common research models of hypersonic flight vehicle are summarized. Secondly, based on the actual engineering requirements, the control difficulties and needs for the control system capability of such vehicle are analyzed. Furthermore, the current status of several typical nonlinear control methods and intelligent control methods for hypersonic flight vehicle are summarized, and the frameworks of various control schemes are given. Finally, some problems and directions for further research are discussed for the HFV control with diversified mission forms and complicated environment in the future.

关 键 词：高超声速飞行器 高超声速变外形飞行器 非线性控制 容错控制 智能控制 

分 类 号：V249[航空宇航科学与技术—飞行器设计]