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Stabilization of large space structures by linear reluctance actuatorsApplication of magnetic forces are considered for stabilization of vibrations of flexible space structures. Three electromagnetic phenomena are studied, such as: (1) magnetic body force; (2) reluctance torque; and (3) magnetostriction, and their application is analyzed for stabilization of a beam. The magnetic body force actuator uses the force that exists between poles of magnets. The reluctance actuator is configured in such a way that the reluctance of the magnetic circuit will be minimum when the beam is straight. Any bending of the beam increases the reluctance and hence generates a restoring torque that reduces bending. The gain of the actuator is controlled by varying the magnetizing current. Since the energy density of a magnetic device is much higher compared to piezoelectric or thermal actuators, it is expected that the reluctance actuator will be more effective in controlling the structural vibrations.
Document ID
19910012996
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Biswas, Saroj K.
(Temple Univ. Philadelphia, PA, United States)
Sendaula, Henry M.
(Temple Univ. Philadelphia, PA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Publication Information
Publication: NASA. Langley Research Center, Fourth NASA Workshop on Computational Control of Flexible Aerospace Systems, Part 1
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N22309
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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