摘要
分析了一种新型飞机电动静液作动系统的工作原理,推导了其详细的数学模型。为了克服电动静液作动系统工作时外界大干扰的影响,设计了一种基于线性反馈的滑模变结构控制器,采用数字仿真对系统进行研究,结果表明所设计的控制算法提高了系统的鲁棒性,使系统具有良好的动态特性。
The principle of characteristics of the a new aircraft electro-hydrostatic actuator ( EHA ) system mathematical model was constructed. In order to overcome the huge disturbance when EHA works, a sliding mode controller with linearization feedback was designed. The simulation results show that the sliding mode controller can improve the robust of the system, and verify the perfect dynamic performances.
出处
《机床与液压》
北大核心
2008年第12期71-74,共4页
Machine Tool & Hydraulics
关键词
电动静液作动器
线性反馈
滑模变结构控制
Electro-hydrostatic actuator (EHA)
Linearization feedback
Sliding mode control