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Performance Optimizing Adaptive Control with Time-Varying Reference Model ModificationThis paper presents a new adaptive control approach that involves a performance optimization objective. The control synthesis involves the design of a performance optimizing adaptive controller from a subset of control inputs. The resulting effect of the performance optimizing adaptive controller is to modify the initial reference model into a time-varying reference model which satisfies the performance optimization requirement obtained from an optimal control problem. The time-varying reference model modification is accomplished by the real-time solutions of the time-varying Riccati and Sylvester equations coupled with the least-squares parameter estimation of the sensitivities of the performance metric. The effectiveness of the proposed method is demonstrated by an application of maneuver load alleviation control for a flexible aircraft.
Document ID
20170009885
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)
Date Acquired
October 11, 2017
Publication Date
June 21, 2017
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN42886
Report Number: ARC-E-DAA-TN42886
Meeting Information
Meeting: Eighteenth Yale Workshop on Adaptive and Learning Systems
Location: New Haven, CT
Country: United States
Start Date: June 21, 2017
End Date: June 23, 2017
Sponsors: Yale Univ. Observatory
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
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