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Active vibration damping of the Space Shuttle remote manipulator systemThe feasibility of providing active damping augmentation of the Space Shuttle Remote Manipulator System (RMS) following normal payload handling operations is investigated. The approach used in the analysis is described, and the results for both linear and nonlinear performance analysis of candidate laws are presented, demonstrating that significant improvement in the RMS dynamic response can be achieved through active control using measured RMS tip acceleration data for feedback.
Document ID
19920001855
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Scott, Michael A. (NASA Langley Research Center Hampton, VA, United States)
Gilbert, Michael G. (NASA Langley Research Center Hampton, VA, United States)
Demeo, Martha E. (Draper, Charles Stark Lab., Inc., Cambridge MA , United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:104149
NASA-TM-104149
Meeting Information
Meeting: AIAA Guidance, Navigation, and Control Conference
Location: New Orleans, LA
Country: United States
Start Date: August 12, 1991
End Date: August 14, 1991
Accession Number
92N11073
Funding Number(s)
PROJECT: RTOP 590-14-41-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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