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Mathematical modeling of the aerodynamic characteristics in flight dynamicsBasic concepts involved in the mathematical modeling of the aerodynamic response of an aircraft to arbitrary maneuvers are reviewed. The original formulation of an aerodynamic response in terms of nonlinear functionals is shown to be compatible with a derivation based on the use of nonlinear functional expansions. Extensions of the analysis through its natural connection with ideas from bifurcation theory are indicated.
Document ID
19840009073
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tobak, M. (NASA Ames Research Center Moffett Field, CA, United States)
Chapman, G. T. (NASA Ames Research Center Moffett Field, CA, United States)
Schiff, L. B. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:85880
A-9603
NASA-TM-85880
Report Number: NAS 1.15:85880
Report Number: A-9603
Report Number: NASA-TM-85880
Meeting Information
Meeting: Berkeley-Ames Conf. on Nonlinear Probl. in Control and Fluid Dyn.
Location: Berkeley, CA
Country: United States
Start Date: May 31, 1983
End Date: June 10, 1983
Accession Number
84N17141
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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