Robust Optimal Influence-Coefficient Control of Multiple-Plane Active Rotor Balancing Systems

[+] Author and Article Information
Stephen W. Dyer

BalaDyne Corporation, 1665 Highland Drive, Ann Arbor, MI 48108-2254e-mail: sdyer@baladyne.com

Jianjun Shi

Industrial and Operations Engineering Department, The University of Michigan, Ann Arbor, MI 48109-2117e-mail: shihang@umich.edu

Jun Ni

Department of Mechanical Engineering, The University of Michigan, Ann Arbor, MI 48109-2136e-mail: junni@umich.edu

Kwang-Keun Shin

General Motors Corporation, P.O. Box 9055, Warren, MI 48090-9055e-mail: kwang-keun.shin@gm.com

J. Dyn. Sys., Meas., Control 124(1), 41-46 (Sep 17, 2001) (6 pages) doi:10.1115/1.1435622 History: Received September 17, 2001
Copyright © 2002 by ASME
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Experimental flexible rotor test stand with active balancing devices installed in two axial planes
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Predicted mode shapes of flexible rotor test rig for first two critical speeds
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Predicted forced response deflected shape of rotor at 3100 rpm due to 245 g-mm unbalance at drive-end active balancing plane
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Comparitive results of single-plane and dual-plane active balancing
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Optimal control results with and without control effort penalty
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Optimal control results for inaccurate influence matrix estimate




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