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Determination of stability and control parameters of a general aviation airplane from flight dataValues for the stability and control parameters for a general aviation airplane were determined from flight data. Lateral and longitudinal transient maneuvers were analyzed by the equation error and output error methods. There was a good agreement between the parameters extracted from flight data and those predicted by wind tunnel.
Document ID
19830018573
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Abbasy, I. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-84635
NAS 1.15:84635
Accession Number
83N26844
Funding Number(s)
PROJECT: RTOP 505-34-03-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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