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27 June 2002 Vibration suppression of a rotationally periodic structure using an adaptive/PPF control law
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Abstract
A jet turbine engine compressor disk is modeled as a rotationally periodic structure. An adaptive parameter estimator was used to eliminate the inter-blade coupling forces. The individual blade vibrations were then suppressed using a positive position feedback method. The resulting control law was tested on a simulated four and eight bladed system.
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Mark J. Keller and Gregory S. Agnes "Vibration suppression of a rotationally periodic structure using an adaptive/PPF control law", Proc. SPIE 4697, Smart Structures and Materials 2002: Damping and Isolation, (27 June 2002); doi: 10.1117/12.472657; https://doi.org/10.1117/12.472657
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