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飞机主动侧杆摩擦补偿研究
引用本文:陈悦,孙永荣,王欢,袁洋,刘闯,赵伟.飞机主动侧杆摩擦补偿研究[J].机械与电子,2018,0(12):29-34.
作者姓名:陈悦  孙永荣  王欢  袁洋  刘闯  赵伟
作者单位:(南京航空航天大学自动化学院,江苏 南京 211106)
摘    要:针对飞机主动侧杆系统中存在非线性摩擦因素,导致在飞机主动侧杆伺服系统中位置跟踪不精确,侧杆跟随性能下降的现象,在三环控制的基础上研究了Stribeck摩擦补偿方法。对Stribeck摩擦模型开展研究,并通过实验辨识其参数,将摩擦模型引入到飞机主动侧杆伺服系统中设计摩擦补偿方法,通过前馈补偿的方式在三环控制的基础上实现摩擦补偿。通过仿真和实验,对侧杆伺服系统摩擦补偿的可行性进行了验证。实验结果表明,所研究的摩擦补偿方法,提高了系统的稳态跟踪精度,具有较好的动态响应性能。

关 键 词:飞机主动侧杆  伺服系统  摩擦补偿  Stribeck模型  参数辨识

Research on Friction Compensation of Aircraft Active Side-stick
CHEN Yue,SUN Yongrong,WANG Huan,YUAN Yang,LIU Chuang,ZHAO Wei.Research on Friction Compensation of Aircraft Active Side-stick[J].Machinery & Electronics,2018,0(12):29-34.
Authors:CHEN Yue  SUN Yongrong  WANG Huan  YUAN Yang  LIU Chuang  ZHAO Wei
Affiliation:(College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China)
Abstract:For the phenomenon that the non-linear friction factor exists in the aircraft active side-stick system, which leads to inaccurate position tracking in the aircraft active side-stick servo system, the paper puts forward the method which adds the Stribeck friction compensation based on the three-loop control. The paper firstly researches the Stribeck friction model and identifies its parameters through experiments. Then the paper introduces the Stribeck friction model into the aircraft active side-stick servo system, designs the friction compensation method, and achieves the friction compensation on the basis of the three-loop control through the feed-forward compensation. Finally, the paper verifies the feasibility of friction compensation in the aircraft active side-stick servo system through simulation and experiments. The experimental results show that the friction compensation method in this paper improves the steady-state tracking accuracy and achieves better dynamic response performance.
Keywords:aircraft active side-stick  servo system  friction compensation  Stribeck friction model  parameter identification
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