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A model for unsteady effects in lateral dynamics for use in parameter estimationA mathematical model for the unsteady aerodynamic effects for use in lateral aircraft dynamics has been developed. The approach is to derive approximations to the force and moment coefficients based on Weissinger's arrangement for the trailing vortex pattern for a sideslipped wing. The main thrust of the modeling is for application to estimation of the lateral stability and control derivatives.
Document ID
19790061305
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Wells, W. R. (Wright State University Dayton, Ohio, United States)
Banda, S. S. (Wright State Univ. Dayton, OH, United States)
Quam, D. L. (Dayton, University Dayton, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 79-1638
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference for Future Space Systems
Location: Boulder, CO
Start Date: August 6, 1979
End Date: August 8, 1979
Accession Number
79A45318
Funding Number(s)
CONTRACT_GRANT: NSG-1417
Distribution Limits
Public
Copyright
Other

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