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Minimal time change detection algorithm for reconfigurable control system and application to aerospaceSystem parameters should be tracked on-line to build a reconfigurable control system even though there exists an abrupt change. For this purpose, a new performance index that we are studying is the speed of adaptation- how quickly does the system determine that a change has occurred? In this paper, a new, robust algorithm that is optimized to minimize the time delay in detecting a change for fixed false alarm probability is proposed. Simulation results for the aircraft lateral motion with a known or unknown change in control gain matrices, in the presence of doublet input, indicate that the algorithm works fairly well. One of its distinguishing properties is that detection delay of this algorithm is superior to that of Whiteness Test.
Document ID
19960003225
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kim, Sungwan
(California Univ. Los Angeles, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NIPS-95-05569
NAS 1.26:199529
NASA-CR-199529
Report Number: NIPS-95-05569
Report Number: NAS 1.26:199529
Report Number: NASA-CR-199529
Accession Number
96N13234
Funding Number(s)
CONTRACT_GRANT: NCC2-374
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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