A common source of noise is operational excitations of mechanical devices,
which cause vibrations and thus sound radiation from their surfaces. Plate
and shell structures in automotive, aviation and space applications vibrati
ng in resonance show particularly high noise levels. Classical methods of n
oise reduction such as passive damping or anti-noise are not efficient enou
gh in certain cases.
Therefore, the use of structural control for reduction of sound radiation i
s presented here. Control forces are generated by piezo-electric actuators
directly attached to the panel surface.
The Finite Element Method supplies a numerical description of the noise rad
iating structure and the effects of the attached piezo actuators. Technical
expenditures are kept low by minimizing the number of sensors and actuator
s used in the control system. To achieve a high control performance, a meth
od is derived to find suitable locations for these elements.
The rapid development of the capability of digital signal processors opens
the possibility to use structural control with complete state feedback as a
method for active noise control of plate structures. The instantaneous sta
te of vibration is measured and these signals are transmitted to a real-tim
e computer. Control outputs are computed on the basis of a modal state obse
rver considering 10 modes in connection with a linear quadratic controller.
The developed active noise control achieves good results for the reduction
of the sound pressure levels at resonance frequencies. In a frequency rang
e of 0-650 Hz attenuations up to 17 dB have been measured. Through the use
of commercially available components such as digital signal processors and
piezo-electric actuators a wide spectrum of future applications is opened.
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