DocumentCode :
488433
Title :
Collocated versus Non-collocated Multivariable Control for Flexible Structure
Author :
Balas, Gary J. ; Doyle, John C.
Author_Institution :
Dept. of Aerospace Engineering and Mechanics, University of Minnesota, Minneapolis, MN 55455
fYear :
1990
fDate :
23-25 May 1990
Firstpage :
1923
Lastpage :
1928
Abstract :
Future space structures have many closely spaced, lightly damped natural frequencies throughout the frequency domain. To achieve desired performance objectives, a number of these modes must actively be controlled. For control, a combination of collocated and noncollocated sensors and actuators will be employed. The control designs will be formulated based on models which have inaccuracies due to unmodeled dynamics, and variations in damping levels, natural frequencies and mode shapes. Therefore, along with achieving the performance objectives, the control design must be robust to a variety of uncertainty. This paper focuses on the benefits and limitations associated with multivariable control design using noncollocated versus collocated sensors and actuators. We address the question of whether performance is restricted due to the noncollocation of the sensors and actuators or the uncertainty associated with modeling of the flexible structures. Control laws are formulated based on models of the system and evaluated analytically and experimentally. Results of implementation of these control laws on the Caltech flexible structure are presented.
Keywords :
Accelerometers; Actuators; Aluminum; Control design; Flexible structures; Frequency; Robust control; Space technology; Uncertainty; Vibration control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1990
Conference_Location :
San Diego, CA, USA
Type :
conf
Filename :
4791064
Link To Document :
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