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General Information
Editor-in-chief
Prof. T. Hikmet Karakoc
Anadolu University, Faculty of Aeronautics and Astronautics, Turkey

IJET 2013 Vol.5(2): 210-212 ISSN: 1793-8236
DOI: 10.7763/IJET.2013.V5.544

A New Command Shaper Design for Residual Vibration Reduction in Flexible Systems Using Artificial Mode Constraints

Seong-Wook Hong, Yong-Kyu Seo, and William Singhose
Abstract—Positioning systems often exhibit vibration resulting from changes in speed and direction. Command shaping efficiently reduces residual vibration by generating appropriately shaped reference commands for positioning systems. However, the presence of command shapers increases the rise time of the systems. This paper proposes a new command-shaper design method for a single-mode system. In addition to suppressing the dominant single mode, this method also constrains vibration at an artificial high mode. This approach can shorten the command shaper duration, or the rise time of the system. The artificial mode frequencies are design variables used to adjust the rise time of the system. The proposed design scheme is illustrated with a simulation example.

Index Terms—Artificial mode constraint, command shaping, natural frequency, residual vibration

S. W. Hong is with the Department of Mechatronics, Kumoh National Institute of Technology, Gumi, Gyeongbuk 730-701, Korea (e-mail: swhong@ kumoh.ac.kr).
Y. K. Seo is with the Top Engineering Co., Ltd., Paju, Gyeonggi 413-813, Korea (e-mail: ykseo@topengnet.com).
W. Singhose is with the School of Mechanical Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332, USA (e-mail: singhose@gatech.edu).

[PDF]

Cite: Seong-Wook Hong,Yong-Kyu Seo, and William Singhose, "A New Command Shaper Design for Residual Vibration Reduction in Flexible Systems Using Artificial Mode Constraints," International Journal of Engineering and Technology  vol. 5, no. 2, pp. 210-212, 2013.

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