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More than you want to know about maximum likelihood estimationThe maximum likelihood estimator has been used to extract stability and control derivatives from flight data for many years. Most of the literature on aircraft estimation concentrates on new developments and applications, assuming familiarity with basic estimation concepts. Some of these basic concepts are presented. The maximum likelihood estimator is briefly discussed and the aircraft equations of motion that the estimator uses. The basic concepts of minimization and estimation are examined for a simple computed aircraft example. The cost functions that are to be minimized during estimation are defined and discussed. Graphic representations of the cost functions are given to help illustrate the minimization process. Finally, the basic concepts are generalized, and estimation from flight data is discussed. Some of the major conclusions for the computed example are also developed for the analysis of flight data.
Document ID
19850007443
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Iliff, K. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Maine, R. E.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 84-2070-CP
NAS 1.15:85905
H-1252
NASA-TM-85905
Report Number: AIAA PAPER 84-2070-CP
Report Number: NAS 1.15:85905
Report Number: H-1252
Report Number: NASA-TM-85905
Meeting Information
Meeting: AIAA Atmospheric Flight Mech. Conf.,
Location: Seattle, WA
Country: United States
Start Date: August 21, 1984
End Date: August 23, 1984
Accession Number
85N15752
Funding Number(s)
PROJECT: RTOP 505-43-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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