New Stability Condition of T-S Fuzzy Systems and Design of Robust Flight Control Principle
作者机构：the School of Aeronautics and AstronauticsZhejiang University the National Key Laboratory of Science and Technology on Aircraft ControlXi'An Flight Automatic Control Research Institute
基 金：supported by the Aviation Science Foundation under Grant No.20110776001 Zhejiang Provincial Natural Science Foundation under Grants No. Y1100696 and No.R1090052 the Fundamental Research Funds for the Central Universities under Grant No.2011QNA4021 National Natural Science Foundation of China under Grant No.61070003 and No.61071128
出 版 物：《Journal of Electronic Science and Technology》 (电子科技学刊（英文版）)
年 卷 期：2013年第11卷第1期
页 码：96-100页
摘 要：Unlike the previous research works analyzing the stability of the T-S （Takagi-Sugeno） fuzzy model, an extension on the stability condition of T-S fuzzy systems with a different strategy is provided. In the strategy a new variable, which is relative to the grade of fuzzy membership function, is introduced to the stability analysis and a new stability conclusion is deduced. The definition of stability condition in this paper is different from previous works, though they are similar in form. With the proposed method, the simulation in flight control law shows a better effectiveness.
主 题 词：Flight control linear matrix inequalities stability Takgagi-Sugeno (T-S) fuzzy control.
学科分类：08[工学] 081105[081105] 0811[工学-水利类]
D O I：10.3969/j.issn.1674-862X.2013.01.017
馆 藏 号：203156488...
