测控技术2017，Vol.36Issue(4)：61-65,69,6.
基于滑模变结构控制的EHA系统仿真研究
Simulation Research on EHA System Based on Sliding Mode Variable Structure Control
摘要
Abstract
The multi-electric aircraft telex power actuation system uses electricity to replace the secondary energy,such as hydraulic energy and pneumatic energy,etc.in the aircraft energy system.A typical power telex actuation system mainly includes electrical hydrostatic actuator(EHA) and electromechanical actuator(EMA).According to the operating characteristics of the aircraft system,the EHA is taken as the research object to analyze its working principle and structure characteristics.Simulink linearization simulation models of driving motor,hydraulic pump,actuator,piston rod load in EHA system are established.At the same time,in order to solve the problem of low control accuracy of the drive motor,as well as the problems of poor control accuracy and narrow bandwidth existed in EHA of traditional PID control,the sliding mode control mechanism is used to improve and optimize the traditional PID control,and make simulation and comparison.The simulation results show that the control quality of EHA system with sliding mode variable structure control is improved obviously.关键词
功率电传/EHA/电机控制/滑模变结构控制Key words
PBW(power-by-wire)/EHA/motor control/sliding mode variable structure control分类
信息技术与安全科学引用本文复制引用
杨钟鼎,周洁敏,郑罡,刘亚..基于滑模变结构控制的EHA系统仿真研究[J].测控技术,2017,36(4):61-65,69,6.基金项目
国防基础预研基金(APSC-NJZX-D201303-J03) （APSC-NJZX-D201303-J03）
南京航空航天大学民航/飞行学院创新基金(MH15Z01) （MH15Z01）
国家自然科学基金(81671667,81471644,81101039,81230032) （81671667,81471644,81101039,81230032）
中国博士后科学基金(2016T90445,2014T71014,2015M570436) （2016T90445,2014T71014,2015M570436）
