The relationship of unsteadiness in downwash to the quality of parameter estimatesThis paper investigates the relative importance of including unsteady effects in the lift and downwash in the longitudinal dynamics and parameter extraction algorithm. A simple vortex system has been used to model unsteady aerodynamic effects into the longitudinal equations of motion of an aircraft. Computer-generated data and flight data were used to demonstrate that inclusion of unsteady aerodynamics in the parameter-extraction algorithm produced aerodynamic parameters that were different from those extracted when unsteady aerodynamics were left out of the algorithm. The differences between derivatives associated with the two extraction algorithms (with and without unsteady aerodynamics) were related to acceleration derivatives which usually cannot be extracted individually.
Document ID
19790061306
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Wells, W. R. (Wright State University Dayton, Ohio, United States)
Keskar, D. A. (SDC Integrated Services, Inc. Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 79-1639Report Number: AIAA PAPER 79-1639
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference for Future Space Systems