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Adjustment of Adaptive Gain with Bounded Linear Stability Analysis to Improve Time-Delay Margin for Metrics-Driven Adaptive ControlThis paper presents the application of Bounded Linear Stability Analysis (BLSA) method for metrics driven adaptive control. The bounded linear stability analysis method is used for analyzing stability of adaptive control models, without linearizing the adaptive laws. Metrics-driven adaptive control introduces a notion that adaptation should be driven by some stability metrics to achieve robustness. By the application of bounded linear stability analysis method the adaptive gain is adjusted during the adaptation in order to meet certain phase margin requirements. Analysis of metrics-driven adaptive control is evaluated for a linear damaged twin-engine generic transport model of aircraft. The analysis shows that the system with the adjusted adaptive gain becomes more robust to unmodeled dynamics or time delay.
Document ID
20100021411
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Bakhtiari-Nejad, Maryam
(NASA Ames Research Center Moffett Field, CA, United States)
Nguyen, Nhan T.
(NASA Ames Research Center Moffett Field, CA, United States)
Krishnakumar, Kalmanje Srinvas
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 24, 2013
Publication Date
June 4, 2009
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN528
Report Number: ARC-E-DAA-TN528
Meeting Information
Meeting: AIAA Infotech Aerospace Conference
Location: Seattle, WA
Country: United States
Start Date: June 4, 2009
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 457280.02.07.01.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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