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Hardware interface unit for control of shuttle RMS vibrationsVibration of the Shuttle Remote Manipulator System (RMS) increases the time for task completion and reduces task safety for manipulator-assisted operations. If the dynamics of the manipulator and the payload can be physically isolated, performance should improve. Rockwell has developed a self contained hardware unit which interfaces between a manipulator arm and payload. The End Point Control Unit (EPCU) is built and is being tested at Rockwell and at the Langley/Marshall Coupled, Multibody Spacecraft Control Research Facility in NASA's Marshall Space Flight Center in Huntsville, Alabama.
Document ID
19950017286
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lindsay, Thomas S.
(Rockwell International Corp. Downey, CA, United States)
Hansen, Joseph M.
(Rockwell International Corp. Downey, CA, United States)
Manouchehri, Davoud
(Rockwell International Corp. Downey, CA, United States)
Forouhar, Kamran
(Rockwell International Corp. Downey, CA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1994
Publication Information
Publication: JPL, Third International Symposium on Artificial Intelligence, Robotics, and Automation for Space 1994
Subject Category
Mechanical Engineering
Accession Number
95N23706
Funding Number(s)
CONTRACT_GRANT: NAS1-19243
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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