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High Speed Aircraft Robust Fuzzy Controller Design Based on H∞ Performance

Chun-Ning Yang Zhen-Yang Chai Quan-Jun Liu Hui Ge

电子科技学刊2017，Vol.15Issue(1)：83-89,7.

电子科技学刊2017，Vol.15Issue(1)：83-89,7.DOI:10.11989/JEST.1674-862X.5102615

High Speed Aircraft Robust Fuzzy Controller Design Based on H∞ Performance

Chun-Ning Yang ¹Zhen-Yang Chai ¹Quan-Jun Liu ²Hui Ge³

作者信息

1. School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China
2. Science and Technology on Space Physics Laboratory, Nanjing 210000, China
3. Institute of Spaceflight Control Technology, Shanghai 200000, China
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摘要

关键词

Fuzzy control/high-speed vehicle (HSV)/large flight envelop (LFE)/nonlinear system with uncertainty/robust H∞ control

Key words

Fuzzy control/high-speed vehicle (HSV)/large flight envelop (LFE)/nonlinear system with uncertainty/robust H∞ control

引用本文复制引用

Chun-Ning Yang,Zhen-Yang Chai,Quan-Jun Liu,Hui Ge..High Speed Aircraft Robust Fuzzy Controller Design Based on H∞ Performance[J].电子科技学刊,2017,15(1):83-89,7.

基金项目

This work was supported by the Shanghai Aerospace Science and Technology Innovation Fund under Grant No. SAST2015085. （）

电子科技学刊

OACSCD

ISSN：1674-862X

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