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A design procedure for active control of beam vibrationsThe transverse vibrations of beams is discussed and a methodology for the design of an active damping device is given. The Bernoulli-Euler equation is used to derive a transcendental transfer function, which relates a torque applied at one end of the beam to the rotational position and velocity at that point. The active damping device consists of a wire, a linear actuator and a short torque arm attached to one end of the beam. The action of the actuator varies a tension in the wire and creates a torque which opposes the rotation of the beam and thus damps vibration. A design procedure for such an active damper is given. This procedure shows the relationships and trade-offs between the actuator stroke, power required, stress levels in the wire and beam and the geometry of the beam and wire. It is shown that by consideration of the frequency response at the beam natural frequencies, the aforementioned relationships can be greatly simplified. Similarly, a simple way of estimating the effective damping ratios and eigenvalue locations of actively controlled beams is presented.
Document ID
19830027808
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dickerson, S. L.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Jarocki, G.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
August 11, 2013
Publication Date
July 1, 1983
Publication Information
Publication: JPL Proc. of the Workshop on Appl. of Distributed System Theory to the Control of Large Space Struct.
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
83N36079
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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