DESIGN OF DUAL REDUNDANCY ELECTRO-MECHANICAL ACTUATOR CONTROL SYSTEM

摘要：

In order to improve the stability and reliability of the aircrafts actuator, it is an effective way to use the redundancy technology.This paper describes a kind of dual redundancy electro-mechanical actuator control system.Both of the electric channels of control system are completely independent, which are composed of motor, control unit, drive unit, and power supply, etc.So entire electric dual redundancy is realized.The control system uses EPOS positioning controller that is a small-sized full digital smart motion controller, with two channels communicating with each other and the host PC via the Controller Area Network(CAN)bus.Besides these, this paper mainly describes the method of redundancy management and fault detection and diagnosis.

关键词： Dual redundancy electro-mechanical actuator Redundancy management Fault detection and diagnosis CAN bus

作者: ZUNYI DENG YIMIN MO YI NING XUEQIN GAO

作者单位: Research Institute of Robotics,Henan University of Technology,Zhengzhou,China and School of Mechanic School of Mechanical and Electronic Engineering,Wuhan University of Technology,Wuhan,China Research Institute of Robotics,Henan University of Technology,Zhengzhou,China Henan Institute of Science and technology,Xinxiang,China

会议类型: 国际会议

会议名称: 3rd International Conference on Mechanical and Electrical Technology(ICMET2011) (2011第三届机械与电气技术国际会议)

会议地点: 大连

会议语种:英文

页码: 659-662

在线出版日期: 2011-08-26（万方平台首次上网日期，不代表论文的发表时间）