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NASA NTRS · 19860048516

Stiffness control of large space structures

Abstract

A method of using internal force producing dual element/actuators for vibration suppression of large space structures is proposed. This technique is applied to a vibrating string as well as a low order system. Response feedback control for the vibrating string and selected modal control are used for achieving the modal damping. The actuators used in this method may be electrically powered and are suitable for structures with extremely low rigidity.

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BibTeXRIS

Chen, J.-C., Fanson, J. L.. 1985-01-01. Stiffness control of large space structures. https://ntrs.nasa.gov/citations/19860048516

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