DocumentCode :
2412530
Title :
Two methods for reducing controller dimensionality in acoustics applications
Author :
Nowlin, William C.
Author_Institution :
SRI Int., Menlo Park, CA, USA
fYear :
1992
fDate :
1992
Firstpage :
1373
Abstract :
The author examines the finite-dimensional linear problem where local control affects a remote, unmeasurable variable, under the assumption that the mapping from the local space to the remote space is rank-deficient. Such is the case in the acoustic radiating and scattering problems when transducers are located on the radiating body, but control of the far field is desired. Drawing upon the acoustics problem for motivation, it is shown that the rank-deficient mapping allows for control of only a subspace of the local space, and two frequency-domain methods are presented to construct filters acting on the transducer arrays: each reduces the controller dimension so that only the propagating subspace is controlled. The constructions are of interest because the filters can be made frequency-independent, and can thus be easily implemented in fast digital hardware
Keywords :
acoustic field; acoustic intensity; acoustic variables control; control system synthesis; filtering and prediction theory; frequency-domain synthesis; state-space methods; transfer functions; acoustic radiating problems; acoustic scattering problems; controller dimensionality; far field control; filters; finite-dimensional linear problem; frequency-domain methods; local control; propagating subspace; rank-deficient mapping; transducer arrays; transfer functions; Acoustic propagation; Acoustic scattering; Acoustic transducers; Actuators; Admittance; Digital filters; Extraterrestrial measurements; Filters; Frequency; Frequency measurement; Hardware; Kernel; Surface waves;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1992., Proceedings of the 31st IEEE Conference on
Conference_Location :
Tucson, AZ
Print_ISBN :
0-7803-0872-7
Type :
conf
DOI :
10.1109/CDC.1992.371486
Filename :
371486
Link To Document :
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