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Efficient computation of parameter confidence intervalsAn important step in system identification of aircraft is the estimation of stability and control derivatives from flight data along with an assessment of parameter accuracy. When the maximum likelihood estimation technique is used, parameter accuracy is commonly assessed by the Cramer-Rao lower bound. It is known, however, that in some cases the lower bound can be substantially different from the parameter variance. Under these circumstances the Cramer-Rao bounds may be misleading as an accuracy measure. This paper discusses the confidence interval estimation problem based on likelihood ratios, which offers a more general estimate of the error bounds. Four approaches are considered for computing confidence intervals of maximum likelihood parameter estimates. Each approach is applied to real flight data and compared.
Document ID
19870062349
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murphy, Patrick C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Systems Analysis
Report/Patent Number
AIAA PAPER 87-2624
Accession Number
87A49623
Distribution Limits
Public
Copyright
Other

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