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Evaluation of a nonlinear parameter extraction mathematical model including the term C(subm(sub delta e squared))Shuttle flight test data were used to determine values for the short-period parameters. The best identified, as judged by its estimated standard deviation, was the elevon effectiveness parameter C (sub m (sub sigma e squared)). However, the scatter about the preflight prediction of C (sub m (sub sigma e squared)) was large. Other investigators have suggested that adding nonlinear terms to the mathematical model used to identify C (sub m (sub sigma e)) could reduce the scatter. The results of this investigation show that C (sub m (sub sigma e squared)) is the only identifiable nonlinear parameter applicable and that the changes in C (sub m (sub sigma e)) values when C (sub m (sub sigma e squared)) is included are in the order of ten percent for the data estimated.
Document ID
19870003133
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Suit, W. T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1986
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:87731
NASA-TM-87731
Report Number: NAS 1.15:87731
Report Number: NASA-TM-87731
Accession Number
87N12566
Funding Number(s)
PROJECT: RTOP 506-46-21-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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