Parametric Vibration Analysis of a Six-Degree-of-Freedom Electro-Hydraulic Stewart Platform

被引:2
|
作者
Yuan, Xiaoming [1 ]
Tang, Yue [1 ]
Wang, Weiqi [1 ]
Zhang, Lijie [1 ]
机构
[1] Yanshan Univ, Hebei Prov Key Lab Heavy Machinery Fluid Power Tr, Qinhuangdao 066004, Hebei, Peoples R China
基金
中国国家自然科学基金;
关键词
SYSTEM; DESIGN; VALVES; PUMP;
D O I
10.1155/2021/9994786
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Electro-hydraulic Stewart 6-DOF platform is a 6-DOF parallel mechanism combined with the electro-hydraulic servo control system, which is widely used in the field of construction machinery. In actual working conditions, the flow and pressure pulsation of the hydraulic oil output from the hydraulic leg of the electro-hydraulic Stewart platform are inevitable, so the equivalent stiffness of the platform leg will change, and the stiffness parameters of the transmission system will change, resulting in vibration, which will affect the accuracy of the platform. This paper considering the fluid unit equivalent stiffness cyclical fluctuations and leg, on the basis of the relationship between hydraulic stiffness, constructs the electric hydraulic Stewart platform machine vibration dynamics equation, fluid coupling parameters of vibration parameters using the method of the multiscale approximate analytic formula of the main resonance and combination resonance are derived, and the system parameters vibration time-domain response and frequency response under two different poses are discussed. Results show that the system first to six order natural frequency and the first to the sixth order natural frequency and frequency of hydraulic oil equivalent stiffness of the combination of frequency will have an effect on the parameters of the system vibration. In the main resonance, the dominant frequency is mainly the first to sixth order natural frequency of the system; in the combined resonance, the dominant frequency is the combined frequency. Through the parameter vibration analysis of two different positions of the platform, it is concluded that when the platform is in an asymmetric position, each leg of the system is more involved in vibration. This study can provide the reference for the subsequent dynamic optimization and reliability analysis of the electro-hydraulic Stewart platform.
引用
收藏
页数:27
相关论文
共 50 条
  • [41] Application of sensitivity analysis for the design of six-degree-of-freedom measurement system
    Kim, JA
    Bae, EW
    Kim, SH
    Kwak, YK
    OPTICAL ENGINEERING, 2001, 40 (12) : 2837 - 2844
  • [42] Mars Exploration Rover six-degree-of-freedom entry trajectory analysis
    Desai, Prasun N.
    Schoenenberger, Mark
    Cheatwood, F. M.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (05) : 1019 - 1025
  • [43] An Integral Variable Structure Controller with Fuzzy Tuning Design for Electro-hydraulic Driving Stewart Platform
    Wu, Bo
    Dong, Yanlang
    Wu, Shenglin
    Xu, Dongguang
    Zhao, Keding
    ISSCAA 2006: 1ST INTERNATIONAL SYMPOSIUM ON SYSTEMS AND CONTROL IN AEROSPACE AND ASTRONAUTICS, VOLS 1AND 2, 2006, : 941 - +
  • [44] ANALYSIS AND EXPERIMENTS ON AN ELECTRO-HYDRAULIC TORSIONAL SERVO VIBRATION DAMPER
    OKADA, Y
    NAKADA, T
    BULLETIN OF THE JSME-JAPAN SOCIETY OF MECHANICAL ENGINEERS, 1976, 19 (131): : 477 - 484
  • [45] Six-degree-of-freedom sensor fish design and instrumentation
    Deng, Zhiqun
    Carlson, Thomas J.
    Duncan, Joanne P.
    Richmond, Marshall C.
    SENSORS, 2007, 7 (12) : 3399 - 3415
  • [46] Six-degree-of-freedom ground-motion measurement
    Nigbor, Robert L.
    Bulletin of the Seismological Society of America, 1994, 84 (05)
  • [47] On the trilaterable six-degree-of-freedom parallel and serial manipulators
    Porta, JA
    Ros, L
    Thomas, F
    2005 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND AUTOMATION (ICRA), VOLS 1-4, 2005, : 960 - 967
  • [48] Six-degree-of-freedom magnetic actuation for wireless microrobotics
    Diller, Eric
    Giltinan, Joshua
    Lum, Guo Zhan
    Ye, Zhou
    Sitti, Metin
    INTERNATIONAL JOURNAL OF ROBOTICS RESEARCH, 2016, 35 (1-3): : 114 - 128
  • [50] Nonlinear six-degree-of-freedom control for flexible spacecraft
    Yamashita, T
    Uo, M
    Hashimoto, T
    AUTOMATIC CONTROL IN AEROSPACE 2001, 2002, : 327 - 332