高超声速飞行器模型及控制若干问题综述  

A Survey of Models and Control Problems of Hypersonic Vehicles

作　　者：张超凡[1] 宗群[1] 董琦[1] 田栢苓[1] 叶林奇[1] ZHANG Chaofan ZONG Qun DONG Qi TIAN Bailing YE Linqi(School of Electrical and Information Engineering, Tianjin University, Tianjin 300072, Chin)

机构地区：[1]天津大学电气自动化与信息工程学院,天津300072

出　　处：《信息与控制》2017年第1期90-102,共13页Information and Control

基　　金：国家自然科学基金资助项目(61673294;61273092)

摘　　要：高超声速技术是21世纪航空航天领域的战略制高点,具有显著的军事和民用价值.高超声速飞行器已成为当今世界军事强国研究的热点,对高超声速飞行器的模型及控制问题进行研究,具有前瞻性、战略性和先导性.本文针对高超声速飞行器模型及控制若干问题展开综述.首先,介绍了高超声速飞行器控制中的难点问题;然后,对国内外几种典型高超声速飞行器模型进行了介绍;在此基础上,重点针对控制器设计中的干扰/不确定问题、弹性问题、非最小相位问题以及再入控制问题等进行了综述.最后,分别针对弹性和再入高超声速飞行器进行了控制方法的仿真与分析,并给出了结论和展望.As one of the most important directions in the aerospace field in the 21 st century,the hypersonic vehicle（HSV） has critical value in both military and civilian affairs.In recent years,HSV research has become a hot spot in military planning,strategy,and focus,especially with respect to the study of HSV model and control problems.This paper reviews some typical HSV model and control problems.First,we summarize the more difficult control problems of the HSV and then introduce typical HSV models.We then give a detailed overview of problems relating to disturbance / uncertainties,flexibility,and non-minimumphase and reentry control.In addition,we present a simulation and analysis of a typical flexible and reentry HSV and discuss the future prospects of hypersonic flight control.

关 键 词：高超声速飞行器 非最小相位 再入控制 模型 弹性 

分 类 号：V448.2[航空宇航科学与技术—飞行器设计]