M-MRAC for Nonlinear Systems with Bounded DisturbancesThis paper presents design and performance analysis of a modified reference model MRAC (M-MRAC) architecture for a class of multi-input multi-output uncertain nonlinear systems in the presence of bounded disturbances. M-MRAC incorporates an error feedback in the reference model definition, which allows for fast adaptation without generating high frequency oscillations in the control signal, which closely follows the certainty equivalent control signal. The benefits of the method are demonstrated via a simulation example of an aircraft's wing rock motion.
Document ID
20120010637
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Stepanyan, Vahram (NASA Ames Research Center Moffett Field, CA, United States)
Krishnakumar, Kalmanje (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 26, 2013
Publication Date
December 12, 2011
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN4164Report Number: ARC-E-DAA-TN4164
Meeting Information
Meeting: 50th IEEE Conference on Decision and Control
Location: Orlando, FL
Country: United States
Start Date: December 12, 2012
Sponsors: Institute of Electrical and Electronics Engineers