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An adaptive tracking observer for failure-detection systemsThe design problem of adaptive observers applied to linear, constant and variable parameters, multi-input, multi-output systems, is considered. It is shown that, in order to keep the observer's (or Kalman filter) false-alarm rate (FAR) under a certain specified value, it is necessary to have an acceptable proper matching between the observer (or KF) model and the system parameters. An adaptive observer algorithm is introduced in order to maintain desired system-observer model matching, despite initial mismatching and/or system parameter variations. Only a properly designed adaptive observer is able to detect abrupt changes in the system (actuator, sensor failures, etc.) with adequate reliability and FAR. Conditions for convergence for the adaptive process were obtained, leading to a simple adaptive law (algorithm) with the possibility of an a priori choice of fixed adaptive gains. Simulation results show good tracking performance with small observer output errors and accurate and fast parameter identification, in both deterministic and stochastic cases.
Document ID
19820016331
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sidar, M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1982
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-84240
NAS 1.15:84240
A-8901
Report Number: NASA-TM-84240
Report Number: NAS 1.15:84240
Report Number: A-8901
Accession Number
82N24207
Funding Number(s)
PROJECT: RTOP 505-34-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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