NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Improvements in aircraft extraction programsFlight data from an F-8 Corsair and a Cessna 172 was analyzed to demonstrate specific improvements in the LRC parameter extraction computer program. The Cramer-Rao bounds were shown to provide a satisfactory relative measure of goodness of parameter estimates. It was not used as an absolute measure due to an inherent uncertainty within a multiplicative factor, traced in turn to the uncertainty in the noise bandwidth in the statistical theory of parameter estimation. The measure was also derived on an entirely nonstatistical basis, yielding thereby also an interpretation of the significance of off-diagonal terms in the dispersion matrix. The distinction between coefficients as linear and non-linear was shown to be important in its implication to a recommended order of parameter iteration. Techniques of improving convergence generally, were developed, and tested out on flight data. In particular, an easily implemented modification incorporating a gradient search was shown to improve initial estimates and thus remove a common cause for lack of convergence.
Document ID
19770006100
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Balakrishnan, A. V.
(Optimization Software, Inc. Los Angeles, CA, United States)
Maine, R. E.
(Optimization Software, Inc. Los Angeles, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-145090
Report Number: NASA-CR-145090
Accession Number
77N13043
Funding Number(s)
CONTRACT_GRANT: NAS1-13824
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available