Search NASA⌕ Search

NASA NTRS · 19860054767

Vibration control of flexible beams using an active hinge

Abstract

The use of an active hinge to attenuate the transverse vibrations of a flexible beam is examined. A slender aluminum beam is suspended vertically, cantilevered at the top. An active hinge is placed at the node of the second vibration mode. The active hinge consists of a torque motor, strain gauge, and tachometer. A control law is implemented using both beam-bending strain and the relative angular velocity measured at this hinge, thereby configuring the hinge to act as an active damper. Results from implementing this control law show little improvement in the first mode damping ratio, 130 percent increase in the second mode damping ratio, and 180 percent increase in the third mode damping ratio. The merits of using a motor with a gearbox are discussed.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Cudney, H. H., Jr., Inman, D. J., Horner, G. C.. 1985-01-01. Vibration control of flexible beams using an active hinge. https://ntrs.nasa.gov/citations/19860054767

Cite the original work for its findings. Save a collection to share your selection of sources.