基于自适应控制的近空间高超声速飞行器研究进展
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  • 英文篇名:Research Progress of Adaptive Control for Hypersonic Vehicle in Near Space
  • 作者:甄子洋 ; 朱平 ; 江驹 ; 陶钢
  • 英文作者:ZHEN Zi-yang;ZHU Ping;JIANG Ju;TAO Gang;College of Automation Engineering,Nanjing University of Aeronautics and Astronautics;Department of Electrical and Computer Engineering,University of Virginia;
  • 关键词:高超声速飞行器 ; 自适应控制 ; 飞行控制 ; 研究进展
  • 英文关键词:Hypersonic vehicle;;Adaptive control;;Flight control;;Research progress
  • 中文刊名:YHXB
  • 英文刊名:Journal of Astronautics
  • 机构:南京航空航天大学自动化学院;美国弗吉尼亚大学电气与计算机工程系;
  • 出版日期:2018-04-30
  • 出版单位:宇航学报
  • 年:2018
  • 期:v.39
  • 基金:国家自然科学基金(61741313,61673209,61533008,61533009);; 航空基金(2016ZA52009);; 院高效联合创新基金(CALT201603)
  • 语种:中文;
  • 页:YHXB201804001
  • 页数:13
  • CN:04
  • ISSN:11-2053/V
  • 分类号:5-17
摘要
综述了高超声速飞行器数学建模与自适应控制技术。在概述典型数学模型基础上,着重概述了模型参考自适应控制、浸入-不变集非线性自适应控制、自适应动态面反步控制、自适应滑模控制、自适应模糊滑模控制和神经网络自适应控制等多种自适应控制技术在高超声速飞行器中的应用与研究。对高超声速飞行器自适应容错控制技术现状,自适应控制在高超声速飞行器飞行测试中的应用情况进行概述。总结了高超声速飞行器的当前研制项目和技术现状,重点展望了若干种鲁棒非线性自适应控制技术。与已有综述相区别,重点概述自适应控制在解决高超声速飞行器鲁棒、稳定、切换、协调等关键控制问题的研究进展。
        The mathematical dynamic model and the adaptive control techniques of the hypersonic vehicles are summarized. Based on the descriptions of the generally used mathematical models,the applications of the model reference adaptive control,immersion and invariance nonlinear adaptive control,adaptive dynamic surface back-stepping control,adaptive sliding mode control,adaptive fuzzy slide model control and neural network adaptive control in the hypersonic vehicles are summarized. Moreover,the fault tolerant control techniques of the hypersonic vehicles are summarized,and the flight tests of the hypersonic vehicles based on the adaptive control methods are introduced. Finally,the current projects and research achievements are concluded,and the future development direction on the robust nonlinear adaptive control techniques is prospected. Different from the previous review work,this paper is emphasized on the research progress of solving the robustness,stability,switching and coordination problems of the hypersonic vehicles based on the adaptive control techniques.
引文
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