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Optimal Control Modification for Time-Scale Separated SystemsRecently a new optimal control modification has been introduced that can achieve robust adaptation with a large adaptive gain without incurring high-frequency oscillations as with the standard model-reference adaptive control. This modification is based on an optimal control formulation to minimize the L2 norm of the tracking error. The optimal control modification adaptive law results in a stable adaptation in the presence of a large adaptive gain. This study examines the optimal control modification adaptive law in the context of a system with a time scale separation resulting from a fast plant with a slow actuator. A singular perturbation analysis is performed to derive a modification to the adaptive law by transforming the original system into a reduced-order system in slow time. A model matching conditions in the transformed time coordinate results in an increase in the actuator command that effectively compensate for the slow actuator dynamics. Simulations demonstrate effectiveness of the method.
Document ID
20140006576
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Nguyen, Nhan T.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
June 3, 2014
Publication Date
March 30, 2012
Subject Category
Cybernetics, Artificial Intelligence And Robotics
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN4802
Report Number: ARC-E-DAA-TN4802
Meeting Information
Meeting: American Control Conference
Location: Montreal, Canada
Country: Canada
Start Date: March 30, 2012
Sponsors: American Automatic Control Council
Funding Number(s)
WBS: WBS 561581.02.08.01.46.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Adaptive Control
Flight Control
Optimal Control
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