首页 | 本学科首页   官方微博 | 高级检索  
     检索      

三余度直接驱动阀驱动控制系统
引用本文:郭宏,蔚永强,邢伟.三余度直接驱动阀驱动控制系统[J].北京航空航天大学学报,2007,33(11):1286-1290.
作者姓名:郭宏  蔚永强  邢伟
作者单位:北京航空航天大学,自动化科学与电气工程学院,北京,100083;北京航空航天大学,自动化科学与电气工程学院,北京,100083;北京航空航天大学,自动化科学与电气工程学院,北京,100083
基金项目:教育部跨世纪优秀人才培养计划
摘    要:设计了一种新型的电气三余度直接驱动阀(DDV,Direct-Drive-Valve)驱动控制系统,介绍了系统结构,分析了三余度永磁无刷直流力矩电机、位置传感器以及交叉通道数据链(CCDL,Cross Channel Data Link)模块的方案设计,探讨了基于新型变结构PID算法的位置伺服控制策略和基于CCDL的余度管理策略.实验结果表明,系统具有良好的动静态性能以及冗余工作特性,其角度范围为-10° ~10°,定位精度不大于4′,三通道工作时频宽不小于20Hz,两通道工作时频宽不小于15Hz,可满足航空DDV式作动器的要求.

关 键 词:余度  直接驱动阀  无刷直流电机  交叉通道数据链  变结构
文章编号:1001-5965(2007)11-1286-05
收稿时间:2007-01-22
修稿时间:2007年1月22日

Triplex-redundancy control system for direct-drive-valve
Guo Hong,Yu Yongqiang,Xing Wei.Triplex-redundancy control system for direct-drive-valve[J].Journal of Beijing University of Aeronautics and Astronautics,2007,33(11):1286-1290.
Authors:Guo Hong  Yu Yongqiang  Xing Wei
Institution:School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:The design and implementation of a triplex-redundancy control system for direct-drive-valve (DDV) were presented. The total structure of the system was built up. The schemes of triplex-redundancy brushless DC motor, transducer and cross channel data link (CCDL) were analyzed. Meanwhile, the strategies of servo control based on variable-structure PID and redundancy management based on CCDL were researched. Experiment results suggest that the proposed system possesses well steady and dynamic performance, and maintains good operation characteristics after first or second electrical failure. Main characteristics of the system are that the range of angle is from -10° to 10°, the precision is less than 4′, and the bandwidth is up to 20Hz for dual redundancy and 15Hz for single redundancy. The system satisfies the DDV actuator of airplane.
Keywords:redundancy  direct-drive-valve  brushless DC motor  cross channel data link  variable structure
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《北京航空航天大学学报》浏览原始摘要信息
点击此处可从《北京航空航天大学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号