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Performance Optimizing Multi-Objective Adaptive Control with Time-Varying Model Reference ModificationThis paper presents a new adaptive control approach that involves a performance optimization objective. The problem is cast as a multi-objective optimal control. The control synthesis involves the design of a performance optimizing controller from a subset of control inputs. The effect of the performance optimizing controller is to introduce an uncertainty into the system that can degrade tracking of the reference model. An adaptive controller from the remaining control inputs is designed to reduce the effect of the uncertainty while maintaining a notion of performance optimization in the adaptive control system.
Document ID
20170000383
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Nguyen, Nhan T.
(NASA Ames Research Center Moffett Field, CA United States)
Hashemi, Kelley E.
(Universities Space Research Association Moffett Field, CA, United States)
Yucelen, Tansel
(University of South Florida FL, United States)
Arabi, Ehsan
(University of South Florida FL, United States)
Date Acquired
January 12, 2017
Publication Date
January 9, 2017
Subject Category
Cybernetics, Artificial Intelligence And Robotics
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN38208
Meeting Information
Meeting: AIAA SciTech Forum
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNH15CO48B
WBS: WBS 081876.02.01.02.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Adaptive Control
Flight Control
Optimal Control
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