跳到主要导航 跳到搜索 跳到主要内容

Research on aircraft taxiing lateral control based on fuzzy controller

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

Aircraft anti-skid braking system is modeled, and the traditional anti-skid braking control algorithm is analyzed. A lateral fuzzy controller is designed, based on the original structure of the controller, whose key variable is the reference velocity, Two more inputs of aircraft drift angel and its derivation are introduced to compensate the reference velocities of two wheel braking control loops respectively. The simulation results demonstrate the performance of the lateral fuzzy controller on this principle.

源语言英语
主期刊名Proceedings of 2011 International Conference on Fluid Power and Mechatronics, FPM 2011
页582-587
页数6
DOI
出版状态已出版 - 2011
活动2011 International Conference on Fluid Power and Mechatronics, FPM 2011 - Beijing, 中国
期限: 17 8月 2011 → 20 8月 2011

丛书

姓名Proceedings of 2011 International Conference on Fluid Power and Mechatronics, FPM 2011

会议

会议2011 International Conference on Fluid Power and Mechatronics, FPM 2011
国家/地区中国
市Beijing
时期17/08/11 → 20/08/11

学术指纹

探究 'Research on aircraft taxiing lateral control based on fuzzy controller' 的科研主题。它们共同构成独一无二的学术指纹。

引用此