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Flight Test Approach to Adaptive Control ResearchThe National Aeronautics and Space Administration s Dryden Flight Research Center completed flight testing of adaptive controls research on a full-scale F-18 testbed. The validation of adaptive controls has the potential to enhance safety in the presence of adverse conditions such as structural damage or control surface failures. This paper describes the research interface architecture, risk mitigations, flight test approach and lessons learned of adaptive controls research.
Document ID
20110024034
Acquisition Source
Armstrong Flight Research Center
Document Type
Other
Authors
Pavlock, Kate Maureen
(NASA Dryden Flight Research Center Edwards, CA, United States)
Less, James L.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Larson, David Nils
(NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Aircraft Stability And Control
Report/Patent Number
DFRC-E-DAA-TN4220
Report Number: DFRC-E-DAA-TN4220
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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