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Aircraft Electric Anti-skid Braking System Based on Fuzzy-PID Controller with Parameter Self-adjustment Feature

Wei Xiaohui Yin Qiaozhi Nie Hong Zhang Ming Tao Zhouliang

南京航空航天大学学报（英文版）2014，Vol.31Issue(1)：111-118,8.

Aircraft Electric Anti-skid Braking System Based on Fuzzy-PID Controller with Parameter Self-adjustment Feature

Wei Xiaohui ¹Yin Qiaozhi ¹Nie Hong ¹Zhang Ming ¹Tao Zhouliang¹

作者信息

1. State Key Laboratory of Mechanics and Control of Mechanical Structure, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, P.R.China
折叠

摘要

关键词

electric braking system/slip rate/anti-skid braking/fuzzy-PID controller

Key words

electric braking system/slip rate/anti-skid braking/fuzzy-PID controller

分类

航空航天

引用本文复制引用

Wei Xiaohui,Yin Qiaozhi,Nie Hong,Zhang Ming,Tao Zhouliang..Aircraft Electric Anti-skid Braking System Based on Fuzzy-PID Controller with Parameter Self-adjustment Feature[J].南京航空航天大学学报（英文版）,2014,31(1):111-118,8.

基金项目

Supported by the National Natural Science Foundation of China (51105197,51305198,11372129) （51105197,51305198,11372129）

the Project Funded by the Priority Academic Program Department of Jiangsu Higher Education Instructions. （）

南京航空航天大学学报（英文版）

OACSCD

ISSN：1005-1120

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