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.
Application of the Observer/Kalman Filter Identification (OKID) Technique to Hubble Flight Data
1993
17 pages
Report
No indication
English
Observer/Kalman-Filter Time-Varying System Identification
Online Contents | 2010
|Bilinear Observer/Kalman Filter Identification (AAS 14-307)
British Library Conference Proceedings | 2014
|