Shaping Inputs to Reduce Vibration in Flexible Space Structures

Future NASA plans to launch large space strucutres solicit the need for effective vibration control schemes which can solve the unique problems associated with unwanted residual vibration in flexible spacecraft. In this work, a unique method of input command shaping called impulse shaping is e...

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Bibliographic Details
Main Author: Chang, Kenneth W.
Language:en_US
Published: 2004
Subjects:
Online Access:http://hdl.handle.net/1721.1/6802