Modified robust optimal adaptive control for flight environment simulation system with heat transfer uncertainty  

作　　者：Meiyin ZHU Xi WANG Xitong PEI Song ZHANG Zhihong DAN Nannan GU Shubo YANG Keqiang MIAO Huairong CHEN Jiashuai LIU 

机构地区：[1]School of Energy and Power Engineering,Beihang University,Beijing 100083,China [2]Collaborative Innovation Center for Advanced Aero Engine,Bejing 100083,China [3]Science and Technology on Altitude Simulation Laboratory,AECC(Aero Engine Corporation of China)Sichuan Gas Turbine Establishment,Mianyang 621000,China

出　　处：《Chinese Journal of Aeronautics》2021年第2期420-431,共12页中国航空学报（英文版）

基　　金：funded by China Scholarship Council (CSC)and National Science and Technology Major Project,China(No. 2017-V-0015-0067)。

摘　　要：To solve the rapid transient control problem of Flight Environment Simulation System(FESS) of Altitude Ground Test Facilities(AGTF) with large heat transfer uncertainty and disturbance, a new adaptive control structure of modified robust optimal adaptive control is presented.The mathematic modeling of FESS is given and the influence of heat transfer is analyzed through energy view. To consider the influence of heat transfer in controller design, we introduce a matched uncertainty that represents heat transfer influence in the linearized system of FESS. Based on this linear system, we deduce the design of modified robust optimal adaptive control law in a general way. Meanwhile, the robust stability of the modified robust optimal adaptive control law is proved through using Lyapunov stability theory. Then, a typical aero-engine test condition with Mach Dash and Zoom-Climb is used to verify the effectiveness of the devised adaptive controller. The simulation results show that the designed controller has servo tracking and disturbance rejection performance under heat transfer uncertainty and disturbance;the relative steady-state and dynamic errors of pressure and temperature are both smaller than 1% and 0.2% respectively. Furthermore,the influence of the modification parameter c is analyzed through simulation. Finally, comparing with the standard ideal model reference adaptive controller, the modified robust optimal adaptive controller obviously provides better control performance than the ideal model reference adaptive controller does.

关 键 词：Altitude ground test facilities Flight environment simulation system Heat transfer Model reference adaptive control Optimal control modification UNCERTAINTY 

分 类 号：V216.8[航空宇航科学与技术—航空宇航推进理论与工程]