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NASA NTRS · 19910012996

Stabilization of large space structures by linear reluctance actuators

Abstract

Application 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.

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BibTeXRIS

Biswas, Saroj K., Sendaula, Henry M.. 1991-03-01. Stabilization of large space structures by linear reluctance actuators. https://ntrs.nasa.gov/citations/19910012996

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