Adaptive Modal Identification for Flutter Suppression ControlIn this paper, we will develop an adaptive modal identification method for identifying the frequencies and damping of a flutter mode based on model-reference adaptive control (MRAC) and least-squares methods. The least-squares parameter estimation will achieve parameter convergence in the presence of persistent excitation whereas the MRAC parameter estimation does not guarantee parameter convergence. Two adaptive flutter suppression control approaches are developed: one based on MRAC and the other based on the least-squares method. The MRAC flutter suppression control is designed as an integral part of the parameter estimation where the feedback signal is used to estimate the modal information. On the other hand, the separation principle of control and estimation is applied to the least-squares method. The least-squares modal identification is used to perform parameter estimation.
Document ID
20160008950
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Nguyen, Nhan T. (NASA Ames Research Center Moffett Field, CA United States)
Drew, Michael (SGT, Inc. Moffett Field, CA, United States)
Swei, Sean S. (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
July 12, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Design, Testing And PerformanceStructural Mechanics
Report/Patent Number
ARC-E-DAA-TN28797Report Number: ARC-E-DAA-TN28797
Meeting Information
Meeting: AIAA SciTech 2016
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics