DocumentCode :
486830
Title :
Vibration Suppression of Planar Truss Structures Utilizing Uniform Damping Control
Author :
Andersen, G.C. ; Silverberg, L.M.
Author_Institution :
NASA Langley Research Center, Hampton, Virginia 23665-5225
fYear :
1986
fDate :
18-20 June 1986
Firstpage :
2040
Lastpage :
2047
Abstract :
A variety of methods has been devised for vibrational control of a structure using both passive and active controls. Presented in this paper is a relatively new method for vibration suppression, uniform damping control. This method consists of implementing a control law which tends to dampen each vibrational mode of the structure at the same desireable exponential rate. The unique aspects of this method are that the control law is not explicitly dependent on the structural stiffness, the control forces are directly proportional to the distribution of the structural mass, and the control law is natural and decentralized. The control law was applied to a flexible planar truss structure and the various aspects of implementation of the control law examined are: actuator/sensor number, placement, and the impact of the actuator/sensor number and placement on the necessary control "power" requirements such as peak power loads, total power requirements, etc. Also examined are the effects of using a limited number of active members in terms of the vibrational performance when compared with the "ideal" distributed control law.
Keywords :
Actuators; Damping; Distributed control; Force control; Optimal control; Proportional control; Sensor phenomena and characterization; Space vehicles; Vibration control; Weight control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1986
Conference_Location :
Seattle, WA, USA
Type :
conf
Filename :
4789264
Link To Document :
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