Minimizing Residual Vibrations in Flexible Systems

Item

Title
en_US Minimizing Residual Vibrations in Flexible Systems
Creator
en_US Rappole, B. Whitney, Jr.
Date
2004-10-20T19:55:29Z
Date Available
2004-10-20T19:55:29Z
Date Issued
en_US 1992-06-01
Identifier
en_US AITR-1371
Abstract
en_US Residual vibrations degrade the performance of many systems. Due to the lightweight and flexible nature of space structures, controlling residual vibrations is especially difficult. Also, systems such as the Space Shuttle remote Manipulator System have frequencies that vary significantly based upon configuration and loading. Recently, a technique of minimizing vibrations in flexible structures by command input shaping was developed. This document presents research completed in developing a simple, closed- form method of calculating input shaping sequences for two-mode systems and a system to adapt the command input shaping technique to known changes in system frequency about the workspace. The new techniques were tested on a three-link, flexible manipulator.
Extent
en_US 122 p.
20616630 bytes
7330468 bytes
Format
application/postscript
application/pdf
Language
en_US
Relation
en_US AITR-1371
Subject
en_US input shaping
en_US vibration suppression
en_US robots
en_US spacesstructures
en_US adaptive