System for computationally efficient active control of tonal sound or vibration
AssigneeSikorsky Aircraft Corporation
InventorsWilliam Arthur Welsh, Douglas G. MacMartin, Alan M. Finn
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AssigneeSikorsky Aircraft Corporation
InventorsWilliam Arthur Welsh, Douglas G. MacMartin, Alan M. Finn
Estimating the term…
A noise or vibration control system reduces a sampling rate and reduces a control rate to improve computation efficiency. The present invention permits the use of a sample frequency (fs) that is less than twice the frequency of interest (fd). The sensed signals are filtered to extract a particular frequency range with a lower bound given by (2n−1)*fs/2 and an upper bound given by (2n+1)*fs/2, where n is an integer chosen so that the frequency of interest (fd) is within the extracted frequency range. The control commands are also calculated at a reduced rate, which is dependent upon the bandwidth of the tone, rather than the absolute frequency of the tone. Rather than updating the control signals directly on the sampled sensor data yk as it enters the computer, the control computations are done on the harmonic components ak and bk, or equivalently on the magnitude and phase.
A method for controlling a physical variable at a frequency of interest (fd) including the steps of:
A method for computing control commands at a reduced rate in a noise or vibration control system including the steps of:
A method for analyzing a physical variable having a first frequency of interest f1 and a second frequency of interest f2 including the steps of:
An apparatus for sensing physical variables at a reduced rate comprising:
Dependencies are inferred from the claim text.