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Assessment of the State of the Art of Flight Control Technologies as Applicable to Adverse ConditionsLiterature from academia, industry, and other Government agencies was surveyed to assess the state of the art in current Integrated Resilient Aircraft Control (IRAC) aircraft technologies. Over 100 papers from 25 conferences from the time period 2004 to 2009 were reviewed. An assessment of the general state of the art in adaptive flight control is summarized first, followed by an assessment of the state of the art as applicable to 13 identified adverse conditions. Specific areas addressed in the general assessment include flight control when compensating for damage or reduced performance, retrofit software upgrades to flight controllers, flight control through engine response, and finally test and validation of new adaptive controllers. The state-of-the-art assessment applicable to the adverse conditions include technologies not specifically related to flight control, but may serve as inputs to a future flight control algorithm. This study illustrates existing gaps and opportunities for additional research by the NASA IRAC Project
Document ID
20100036846
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Reveley, Mary s.
(NASA Glenn Research Center Cleveland, OH, United States)
Briggs, Jeffrey L.
(NASA Glenn Research Center Cleveland, OH, United States)
Leone, Karen M.
(ASRC Aerospace Corp. Cleveland, OH, United States)
Kurtoglu, Tolga
(Stinger Ghaffarian Technologies, Inc. (SGT, Inc.) Greenbelt, MD, United States)
Withrow, Colleen A.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
September 1, 2010
Subject Category
Air Transportation And Safety
Report/Patent Number
E-17212
NASA/TM-2010-216226
Funding Number(s)
WBS: WBS 645846.02.07.03.16
Distribution Limits
Public
Copyright
Public Use Permitted.
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