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New Stability Condition of T-S Fuzzy Systems and Design of Robust Flight Control Principle

Chun-Ning Yang Ya-Zhou Yue Hui Li

电子科技学刊2013，Vol.11Issue(1)：96-100,5.

电子科技学刊2013，Vol.11Issue(1)：96-100,5.DOI:10.3969/j.issn.1674-862X.2013.01.017

New Stability Condition of T-S Fuzzy Systems and Design of Robust Flight Control Principle

Chun-Ning Yang ¹Ya-Zhou Yue ²Hui Li¹

作者信息

1. School of Aeronautics and Astronautics, Zhejiang University, Hangzhou, 310027, China
2. National Key Laboratory of Science and Technology on Aircraft Control, Xi'An Flight Automatic Control Research Institute, Xi'an 710065, China
折叠

摘要

关键词

Flight control/linear matrix inequalities/stability/Takgagi-Sugeno (T-S) fuzzy control

Key words

Flight control/linear matrix inequalities/stability/Takgagi-Sugeno (T-S) fuzzy control

引用本文复制引用

Chun-Ning Yang,Ya-Zhou Yue,Hui Li..New Stability Condition of T-S Fuzzy Systems and Design of Robust Flight Control Principle[J].电子科技学刊,2013,11(1):96-100,5.

基金项目

This work was 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, and National Natural Science Foundation of China under Grant No.61070003 and No.61071128. （）

电子科技学刊

ISSN：1674-862X

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