论文:2015,Vol:33,Issue(1):45-49
引用本文:
李玉忍, 张智慧, 徐健龙. 飞机防滑刹车模糊滑模变结构控制研究[J]. 西北工业大学学报
Li Yuren, Zhang Zhihui, Xu Jianlong. Study on Fuzzy Sliding-Mode Variable Structure Control for Aircraft Anti-Skid Braking[J]. Northwestern polytechnical university

飞机防滑刹车模糊滑模变结构控制研究
李玉忍, 张智慧, 徐健龙
西北工业大学自动化学院, 陕西西安 710072
摘要:
滑模变结构控制具有好的快速性和强的鲁棒性,非常适合工作环境复杂的飞机刹车系统,但其固有的抖振问题亟待解决。针对飞机防滑刹车系统的高度非线性,设计了一个模糊滑模变结构控制器。在滑模变结构控制基础之上,通过模糊逻辑的调节作用实现附加控制,柔滑控制信号,削弱抖振,提高控制品质。仿真结果表明,飞机防滑刹车系统能够很好地跟踪最佳滑移率,控制方法合理有效。
关键词:    飞机    刹车    模糊控制    滑模控制    变结构控制    滑移率   
Study on Fuzzy Sliding-Mode Variable Structure Control for Aircraft Anti-Skid Braking
Li Yuren, Zhang Zhihui, Xu Jianlong
Department of Automatic Control, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:
Sliding-mode variable structure control has good rapidity and strong robustness, which is very suitable for the complex working environment of aircraft braking system, but its inherent chattering problem needs to be solved urgently. In order to deal with the high nonlinearity of aircraft braking system, we design a fuzzy sliding-mode variable structure controller. Based on sliding-mode variable structure control, additional control is realized through adjustment with fuzzy logic, which can make the control signal smooth, weaken the chattering and improve the quality of control. The simulation results and their analysis indicate preliminarily that the anti-skid braking system can track the optimal slip ratio well and the control method is reasonable and effective.
Key words:    aircraft    braking    fuzzy control    sliding mode control    variable structure control    slip ratio   
收稿日期: 2014-04-28     修回日期:
DOI:
基金项目: 教育部博士点基金(20116102120033)资助
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作者简介: 李玉忍(1962-),西北工业大学教授、博士生导师,主要从事飞机电力系统、电力电子与电力传动等研究。
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