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L1 Adaptive Control Augmentation System with Application to the X-29 Lateral/Directional Dynamics: A Multi-Input Multi-Output ApproachThis paper presents an L(sub 1) adaptive control augmentation system design for multi-input multi-output nonlinear systems in the presence of unmatched uncertainties which may exhibit significant cross-coupling effects. A piecewise continuous adaptive law is adopted and extended for applicability to multi-input multi-output systems that explicitly compensates for dynamic cross-coupling. In addition, explicit use of high-fidelity actuator models are added to the L1 architecture to reduce uncertainties in the system. The L(sub 1) multi-input multi-output adaptive control architecture is applied to the X-29 lateral/directional dynamics and results are evaluated against a similar single-input single-output design approach.
Document ID
20100037212
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Griffin, Brian Joseph
(NASA Dryden Flight Research Center Edwards, CA, United States)
Burken, John J.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Xargay, Enric
(Illinois Univ. at Urbana-Champaign Urbana, IL, United States)
Date Acquired
August 25, 2013
Publication Date
August 2, 2010
Subject Category
Aircraft Stability And Control
Report/Patent Number
DFRC-E-DAA-TN1776
DFRC-E-DAA-TN1927
Meeting Information
Meeting: AIAA Guidance, Navigation, and Control Conference
Location: Toronto, Ontario, Canada
Country: Canada
Start Date: August 2, 2010
End Date: August 5, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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