LMI-BASED AERO-ENGINE CONTROLLER DESIGN

作     者：范训礼 谢振华 张新家 戴冠中 

作者机构：西北工业大学 陕西 西安 71 0 0 72 

出 版 物：《Chinese Journal of Aeronautics》 (中国航空学报（英文版）)

年 卷 期：2000年第13卷第1期

页      面：34-38页

核心收录：

学科分类：082502[工学-航空宇航推进理论与工程] 08[工学] 0825[工学-航空宇航科学与技术] 

基　　金：National Natural Science Foundation of China! ( 6 98740 3 2 ) The Youth Teacher Foundation of NPU 

主　　题：Control system analysis Control system synthesis Matrix algebra Riccati equations Turbojet engines 

摘      要：The problem of analysis and synthesis of robust control is addressed in this work. The approach transferring the robust control design into Linear Matrix Inequality (LMI) is provided. The LMI standard structure of robust controller is also given and the controller is obtained through solving three LMIs. As an example, a robust control law is designed to the twin-spool turbojet engine system using the given approach. The result shows that LMI approach is feasible.