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Algorithms for real-time flutter identificationThe work reported here addresses the important algorithm issues necessary to achieve a real-time flutter monitoring system; namely, the guidelines for choosing appropriate model forms, reduction of the parameter convergence transient, handling multiple modes, the effect of overparameterization, and estimate accuracy predictions, both online and for experiment design. An approach for efficiently computing continuous-time flutter parameter Cramer-Rao estimate error bounds has been developed. This enables a convincing comparison of theoretical and simulation results, as well as off-line studies in preparation for a flight test. Theoretical predictions, simulation and flight test results from the NASA/Dryden Drones for Aerodynamic and Structural Test (DAST) Program are compared.
Document ID
19830060485
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Walker, R. A.
(Integrated Systems, Inc. Palo Alto, CA, United States)
Gupta, N. K.
(Integrated Systems, Inc. Palo Alto, CA, United States)
Gilyard, G. B.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 83-2223
Report Number: AIAA PAPER 83-2223
Meeting Information
Meeting: Guidance and Control Conference
Location: Gatlinburg, TN
Start Date: August 15, 1983
End Date: August 17, 1983
Accession Number
83A41703
Distribution Limits
Public
Copyright
Other

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