An application of the Observer/Kalman Filter Identification (OKID) technique to Hubble flight data

Details An application of the Observer/Kalman Filter Identification (OKID) technique to Hubble flight data An application of the Observer/Kalman Filter Identification (OKID) technique to Hubble flight data

Feb 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993csit.nasa...97j&link_type=abstract

In its The Fifth NASA/DOD Controls-Structures Interaction Technology Conference, Part 1 p 97-112 (SEE N93-18818 06-18)

Physics

Damping, Hubble Space Telescope, Kalman Filters, System Identification, Controllers, Identifying, Vibration

Scientific paper

The 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.

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