JZUS - Journal of Zhejiang University SCIENCE

Journal of Zhejiang University SCIENCE A

Accepted manuscript available online (unedited version)

Track-position and vibration control simulation for strut of the Stewart platform

Author(s): Zhao-dong Xu¹, Chen-hui Weng^1;2
Affiliation(s): 1. MOE Key Laboratory of C&PC Structures, Southeast University, Nanjing 210096, China;2. Guangzhou Design Institute, Guangzhou 510630, China
Corresponding email(s): xuzhdgyq@seu.edu.cn
Key Words: Stewart platform, Track-positioning control, Vibration control

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Zhao-dong Xu, Chen-hui Weng. Track-position and vibration control simulation for strut of the Stewart platform[J]. Journal of Zhejiang University Science A,in press.Frontiers of Information Technology & Electronic Engineering,in press.https://doi.org/10.1631/jzus.A1200278

@article{title="Track-position and vibration control simulation for strut of the Stewart platform",
author="Zhao-dong Xu, Chen-hui Weng",
journal="Journal of Zhejiang University Science A",
year="in press",
publisher="Zhejiang University Press & Springer",
doi="https://doi.org/10.1631/jzus.A1200278"
}

%0 Journal Article
%T Track-position and vibration control simulation for strut of the Stewart platform
%A Zhao-dong Xu
%A Chen-hui Weng
%J Journal of Zhejiang University SCIENCE A
%P 281-291
%@ 1673-565X
%D in press
%I Zhejiang University Press & Springer
doi="https://doi.org/10.1631/jzus.A1200278"

TY - JOUR
T1 - Track-position and vibration control simulation for strut of the Stewart platform
A1 - Zhao-dong Xu
A1 - Chen-hui Weng
J0 - Journal of Zhejiang University Science A
SP - 281
EP - 291
%@ 1673-565X
Y1 - in press
PB - Zhejiang University Press & Springer
ER -
doi="https://doi.org/10.1631/jzus.A1200278"

Abstract
Chinese Summary
Academic Network
Reviewer Comment

Abstract: Vibrations inherently generated by on-board disturbance sources degrade the performance of the instruments in an on-orbit spacecraft, which have stringent accuracy requirements. The stewart platform enables both track-positioning and vibration control. The strut of the stewart platform is designed as a piezoelectric (PZT) element in series with a voice coil motor (VCM) element and a viscoelastic element. The track-positioning system uses a VCM as the main positioning control driver and a PZT as the positioning compensator. The vibration control system uses the characteristics of struts including active and passive control elements to attenuate the vibration. Simulation results indicate that the stewart platform with the designed struts has good performance in tracking and vibration attenuation with different interference waves.

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References

[1] Anderson,E.H, Fumo,J.P, Erwin,R.S, 2000, Satellite Ultraquiet Isolation Technology Experiment (SUITE) , ():299-313.

[2] Bandyopadhyay,S, Ghosal,A, 2009, An algebraic formulation of static isotropy and design of statically isotropic 6-6 Stewart platform manipulators Mechanism and Machine Theory, 44(7):1360-1370.

[3] Fraguela,L, Fridman,L, Alexandrov,V.V, 2012, Output integral sliding mode control to stabilize position of a Stewart platform Journal of the Franklin Institute, 349(4):1526-1542.

[4] Grewal,K.S, Dixon,R, Pearson,J, 2012, LQG controller design applied to a pneumatic Stewart-Gough platform International Journal of Automation and Computing, 9(1):45-53.

[5] Huang,X.H, Horowitz,R, Li,Y.F, 2005, Track-following control with active vibration damping and compensation of a dual-stage servo system Microsystem Technologies, 11(12):1276-1286.

[6] Li,Y, Horowitz,R, 2002, Design and testing of track-following controllers for dual-stage servo systems with PZT actuated suspensions Microsystem Technologies, 8(2-3):194-205.

[7] Li,Y, Ang,K.H, Chong,G.C.Y, 2006, PID control system analysis and design IEEE Control Systems Magazine, 26(1):32-41.

[8] Liu,Y.J, Li,T, Sun,L.N, 2009, Design of a control system for a macro-micro dual-drive high acceleration high precision positioning stage for IC packaging Science in China Series E: Technological Sciences, 52(7):1858-1865.

[9] Masterson,R.A, Miller,D.W, Grogan,R.L, 1999, Development of Empirical and Analytical Reaction Wheel Disturbance Models , ():12-15.

[10] Mukherjee,P.B, Dasgupta,B, Mallik,A.K, 2007, Dynamic stability index and vibration analysis of a flexible Stewart platform Journal of Sound and Vibration, 307(3-5):495-512.

[11] Mura,A, 2012, Multi-dofs MEMS displacement sensors based on the Stewart platform theory Microsystem Technologies, 18(5):575-579.

[12] Neat,G.W, Melody,J.W, Lurie,B.J, 1998, Vibration attenuation approach for space borne optical interferometers IEEE Transactions on Control System Technology, 6(6):689-700.

[13] Preumont,A, Horodinca,M, Romanescu,I, de Marneffe,B, Avraam,M, Deraemaeker,A, Bossens,F, Abu Hanieh,A, 2007, A six-axis single-stage active vibration isolator based on Stewart platform Journal of Sound and Vibration, 300(3-5):644-661.

[14] Stewart,D, 1965, A platform with six degrees of freedom Proceedings of the Institution of Mechanical Engineers, 180():371-386.

[15] Sullivan,L.A, Erwin,R.S, Denoyer,K.K, 2000, Experiences with smart structures for on-orbit vibration isolation SPIE, 3991():122-130.

[16] Wang,Z.L, He,J.J, Gu,H, 2011, Forward kinematics analysis of a six degree-of-freedom Stewart platform based on independent component analysis and Nelder-Mead algorithm IEEE Transactions on Systems, Man, and Cybernetics A, 41(3):589-597.

[17] Xu,Z.D, Wang,D.X, Wu,K.Y, 2011, Simulation of stochastic wind field for large complex structures based on modified Fourier spectrum Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 12(3):238-246.

[18] Zhang,Z, Cui,L, Huang,H, 2011, A Real-time Linux Based Controller for Active Vibration Isolation Stewart Platform and the Experiment , 30th Chinese Control Conference, Beijing, p. 2429-2434.

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References