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An application of the Observer/Kalman Filter Identification (OKID) technique to Hubble flight dataThe objective of the current research is to identify vibration parameters, including frequencies, damping ratio and uncertainty characteristics, of the Hubble Space Telescope from flight data using an advanced system identification technique. The Observer/Kalman Filter Identification (OKID) technique is used to identify the vibration parameters. The OKID was recently developed by the researchers in the Spacecraft Dynamics Branch at NASA Langley Research Center.
Document ID
19930009636
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Juang, Jer-Nan
(NASA Langley Research Center Hampton, VA, United States)
Horta, Lucas G.
(NASA Langley Research Center Hampton, VA, United States)
Belvin, W. Keith
(NASA Langley Research Center Hampton, VA, United States)
Sharkey, John
(NASA Marshall Space Flight Center Huntsville, AL., United States)
Bauer, Frank H.
(NASA Goddard Space Flight Center Greenbelt, MD., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: The Fifth NASA(DOD Controls-Structures Interaction Technology Conference, Part 1
Subject Category
Astronomy
Accession Number
93N18825
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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