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Parameter estimation using an a posteriori criterionA procedure for estimating noise statistics as well as system model parameters, based on a maximum likelihood criterion, has been successfully applied to a number of aircraft parameter-identification problems. In the present investigation, an a posteriori criterion is examined for use in such an application, when it is desired to model process noise. The criteria lead to identical results when there is no process noise.
Document ID
19740017469
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bach, R. E., Jr. (Northeastern Univ. Boston, MA, United States)
Date Acquired
August 7, 2013
Publication Date
April 1, 1974
Publication Information
Publication: NASA. Flight Res. Center Parameter Estimation Tech. and Appl. in Aircraft Flight Testing
Subject Category
Aircraft
Accession Number
74N25582
Funding Number(s)
CONTRACT_GRANT: NAS2-7397
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19740017456Collected WorksParameter estimation techniques and application in aircraft flight testing
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