NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Bounded Linear Stability Margin Analysis of Nonlinear Hybrid Adaptive ControlThis paper presents a bounded linear stability analysis for a hybrid adaptive control that blends both direct and indirect adaptive control. Stability and convergence of nonlinear adaptive control are analyzed using an approximate linear equivalent system. A stability margin analysis shows that a large adaptive gain can lead to a reduced phase margin. This method can enable metrics-driven adaptive control whereby the adaptive gain is adjusted to meet stability margin requirements.
Document ID
20090019073
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Nguyen, Nhan T.
(NASA Ames Research Center Moffett Field, CA, United States)
Boskovic, Jovan D.
(Scientific Systems Co., Inc. Woburn, MA, United States)
Date Acquired
August 24, 2013
Publication Date
June 11, 2008
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN119
Report Number: ARC-E-DAA-TN119
Meeting Information
Meeting: American Control Conference
Location: Seattle, WA
Country: United States
Start Date: June 11, 2008
End Date: June 13, 2008
Sponsors: Agency of Industrial Science and Technology, American Inst. of Chemical Engineers, Institute of Electrical and Electronics Engineers, Italian Space Agency, Society for Computer Simulation International, American Society of Civil Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 457280.02.07.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available