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Important factors in the maximum likelihood analysis of flight test maneuversThe information presented is based on the experience in the past 12 years at the NASA Dryden Flight Research Center of estimating stability and control derivatives from over 3500 maneuvers from 32 aircraft. The overall approach to the analysis of dynamic flight test data is outlined. General requirements for data and instrumentation are discussed and several examples of the types of problems that may be encountered are presented.
Document ID
19790013942
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Iliff, K. W. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Maine, R. E. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Montgomery, T. D. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1979
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TP-1459
H-1076
Report Number: NASA-TP-1459
Report Number: H-1076
Accession Number
79N22113
Funding Number(s)
PROJECT: RTOP 505-06-64
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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