Study of the Dynamic Properties of the Miniature Electro-Hydrostatic Actuator

被引:1
|
作者
An, Yiqiang [1 ]
Mao, Jiazhe [1 ]
Tong, Chengwei [1 ]
Zhou, Xiaoyun [1 ]
Ruan, Jian [1 ]
Li, Sheng [1 ]
机构
[1] Zhejiang Univ Technol, Coll Mech Engn, Hangzhou 310023, Peoples R China
关键词
miniature electro-hydrostatic actuator; micro two-dimensional pump; joint simulation; dynamic properties; PUMP;
D O I
10.3390/machines12020114
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
The electro-hydrostatic actuator (EHA) is a new type of high-performance servo actuator that originated in the field of aerospace, and it is gradually becoming a common basic component for various types of large equipment. A miniature EHA, mainly composed of a micro two-dimensional (2D) piston pump and a brushless DC motor, is designed in this article by simplifying the system structure. This paper analyzes the structure and working principle of this EHA and establishes the mathematical models of the brushless DC motor, micro two-dimensional pump, and hydraulic cylinder. Field-oriented control (FOC) is used to drive the brushless DC motor, and the models of the controller are established in Simulink. Furthermore, the models of the mechanical and hydraulic systems of the miniature EHA are established in AMESim. In addition to this, a prototype of this miniature EHA was fabricated in this paper and an experimental platform was built for experiments. In the joint simulation environment, the rise time of the EHA system at 6000 r/min is 0.158 s and the frequency response amplitude attenuation to -3 dB has a bandwidth of 20 Hz. On the other hand, the constructed miniature EHA prototype was dynamically characterized to obtain a rise time of 0.242 s at 6000 r/min and a bandwidth of 13 Hz. In this paper, the feasibility of the design scheme of the miniature EHA system is verified, and its excellent dynamic properties are verified with simulation and experiment.
引用
收藏
页数:17
相关论文
共 50 条
  • [1] Electro-hydrostatic actuator
    Holt, D
    AEROSPACE ENGINEERING, 1997, 17 (11) : 18 - 18
  • [2] Electro-hydrostatic actuator
    Aerosp Eng (Warrendale PA), 11 (18):
  • [3] Electro-Hydrostatic Actuator Modeling
    Song, Yu
    Habibi, S. R.
    MECHATRONICS AND COMPUTATIONAL MECHANICS, 2013, 307 : 131 - 135
  • [4] The Study on the Dynamic Capability of an Electro-Hydrostatic Actuator to Drive a Large Inertia Load
    Zhao Shoujun
    He Jun
    Zhang Yuqiang
    2016 IEEE/CSAA INTERNATIONAL CONFERENCE ON AIRCRAFT UTILITY SYSTEMS (AUS), 2016, : 836 - 841
  • [5] Analysis of the dynamic performance of an electro-hydrostatic actuator and improvement methods
    Li, Zhihui
    Shang, Yaoxing
    Jiao, Zongxia
    Lin, Yan
    Wu, Shuai
    Li, Xiaobin
    CHINESE JOURNAL OF AERONAUTICS, 2018, 31 (12) : 2312 - 2320
  • [6] Analysis of the dynamic performance of an electro-hydrostatic actuator and improvement methods
    Zhihui LI
    Yaoxing SHANG
    Zongxia JIAO
    Yan LIN
    Shuai WU
    Xiaobin LI
    Chinese Journal of Aeronautics, 2018, 31 (12) : 2312 - 2320
  • [7] Analysis of the dynamic performance of an electro-hydrostatic actuator and improvement methods
    Zhihui LI
    Yaoxing SHANG
    Zongxia JIAO
    Yan LIN
    Shuai WU
    Xiaobin LI
    Chinese Journal of Aeronautics, 2018, (12) : 2312 - 2320
  • [8] Study on Nonlinear PID Control for Electro-hydrostatic Actuator
    Fan, Jizhong
    Ling, Dongyao
    Tang, Zhiyong
    Pei, Zhongcai
    2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2014, : 1317 - 1320
  • [9] Test Research of Electro-Hydrostatic Actuator
    Yin, Lisheng
    Xing, Keli
    ADVANCES IN MATERIALS, MACHINERY, ELECTRONICS III, 2019, 2073
  • [10] Modelling and control of an electro-hydrostatic actuator
    Pachter, M
    Houpis, CH
    Kang, K
    INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 1997, 7 (06) : 591 - 608