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Certification of a hybrid parameter model of the fully flexible Shuttle Remote Manipulator SystemThe development of high fidelity models of mechanical systems with flexible components is in flux. Many working models of these devices assume the elastic motion is small and can be superimposed on the overall rigid body motion. A drawback associated with this type of modeling technique is that it is required to regenerate the linear modal model of the device if the elastic motion is sufficiently far from the base rigid motion. An advantage to this type of modeling is that it uses NASTRAN modal data which is the NASA standard means of modal information exchange. A disadvantage to the linear modeling is that it fails to accurately represent large motion of the system, unless constant modal updates are performed. In this study, which is a continuation of a project started last year, the drawback of the currently used modal snapshot modeling technique is addressed in a rigorous fashion by novel and easily applied means.
Document ID
19950026000
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barhorst, Alan A.
(Texas Technological Univ. Lubbock, TX, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1995
Publication Information
Publication: NASA. Johnson Space Center, National Aeronautics and Space Administration (NASA)(American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1994, Volume 1 10 p (SEE N95-32418
Subject Category
Mechanical Engineering
Accession Number
95N32421
Funding Number(s)
CONTRACT_GRANT: NGT-44-005-803
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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