Initial evaluation of the modified step-wise regression procedure to estimate aircraft stability and control parameters from flight test data

dc.contributor.authorHoff, J. C.en_UK
dc.date1993en_UK
dc.date.accessioned2005-11-23T12:21:33Z
dc.date.available2005-11-23T12:21:33Z
dc.date.issued1993en_UK
dc.description.abstractThis report presents the initial results of research in progress in the College of Aeronautics at the Cranfield Institute of Technology. The object of the research is to investigate the use of the Modified Stepwise Regression procedure to estimate aircraft stability and control parameters from flight test data. The Stepwise Regression Method for parameter identification is a procedure that inserts independent variables into a regression model. Each time a new variable is added to the model a regression is performed and the fit is examined when the new variable, or any other previously included variable, may be rejected from the model if non-significant to the fit. The iterative process continues until a satisfactory fit (or model) is obtained.en_UK
dc.description.sponsorshipThe Universityen_UK
dc.format.extent1963 bytes
dc.format.extent1518327 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/220
dc.language.isoen_UKen_UK
dc.relation.ispartofseriesCollege of Aeronautics Report;9313en_UK
dc.relation.ispartofseriesCU/CoA/R;9313en_UK
dc.titleInitial evaluation of the modified step-wise regression procedure to estimate aircraft stability and control parameters from flight test dataen_UK
dc.typeTechnical Reporten_UK

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