DocumentCode :
783129
Title :
Active damping control of vibrational systems
Author :
Song, Y.D. ; Mitchell, T.L.
Author_Institution :
Dept. of Electr. Eng., North Carolina A&T State Univ., Greensboro, NC, USA
Volume :
32
Issue :
2
fYear :
1996
fDate :
4/1/1996 12:00:00 AM
Firstpage :
569
Lastpage :
577
Abstract :
The problem of vibration suppression in large flexible space structure (LFSS) is investigated. Based on the structure property of LFSS, an active damping strategy is proposed to effectively attenuate the critical vibrations of the structure subject to modeling uncertainty and external disturbance. Control algorithms are derived with the aim of suppressing both the vibrating magnitude and vibrating rate to an acceptable level. It is shown that the strategy exhibits robust and adaptive properties and is truly model-independent. The novelty of the proposed approach lies in the fact that it is fairly easy to set up the strategy and the overall computation involved is much less than any other strategies available to date. A two-bay truss is used to verify the validity of the proposed approach.
Keywords :
aerospace control; damping; flexible structures; vibration control; active damping control; critical vibrations; external disturbance; large flexible space structure; model-independent strategy; modeling uncertainty; two-bay truss; vibrating magnitude; vibrating rate; vibration suppression; vibrational systems; Actuators; Agriculture; Control systems; Damping; Flexible structures; Fuels; Modal analysis; NASA; Robustness; Uncertainty; Vibration control; Weight control;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.489501
Filename :
489501
Link To Document :
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