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Adaptive Flight Control Research at NASAA broad overview of current adaptive flight control research efforts at NASA is presented, as well as some more detailed discussion of selected specific approaches. The stated objective of the Integrated Resilient Aircraft Control Project, one of NASA s Aviation Safety programs, is to advance the state-of-the-art of adaptive controls as a design option to provide enhanced stability and maneuverability margins for safe landing in the presence of adverse conditions such as actuator or sensor failures. Under this project, a number of adaptive control approaches are being pursued, including neural networks and multiple models. Validation of all the adaptive control approaches will use not only traditional methods such as simulation, wind tunnel testing and manned flight tests, but will be augmented with recently developed capabilities in unmanned flight testing.
Document ID
20080022957
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Motter, Mark A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
June 2, 2008
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: 14th Yale Workshop on Adaptive and Learning Systems
Location: New Haven, CT
Country: United States
Start Date: June 2, 2008
End Date: June 5, 2008
Funding Number(s)
WBS: WBS 561581.02.08.07.14.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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