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A new approach for vibration control in large space structuresAn approach for augmenting vibration damping characteristics in space structures with large panels is presented. It is based on generation of bending moments rather than forces. The moments are generated using bimetallic strips, suitably mounted at selected stations on both sides of the large panels, under the influence of differential solar heating, giving rise to thermal gradients and stresses. The collocated angular velocity sensors are utilized in conjunction with mini-servos to regulate the control moments by flipping the bimetallic strips. A simple computation of the rate of dissipation of vibrational energy is undertaken to assess the effectiveness of the proposed approach.
Document ID
19870013310
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kumar, K.
(Auburn Univ. AL, United States)
Cochran, J. E., Jr.
(Auburn Univ. AL, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA. Marshall Space Flight Center Structural Dynamics and Control Interaction of Flexible Structures
Subject Category
Structural Mechanics
Accession Number
87N22743
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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