论文信息 - Adaptive active control of sound fields in elastic cylinders via vibrational inputs

Adaptive active control of sound fields in elastic cylinders via vibrational inputs

A model of an aircraft fuselage is used to evaluate an active noise control system using vibrational force inputs as secondary control sources. The cylindrical shell is unstiffened, undamped, and contains no interior acoustic damping. A control system based on the filtered-x version of the least mean squares algorithm is configured, using one control source and one error sensor.

D. S. Mandic | J. D. Jones | James D. Jones | D. Mandić

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