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Restructurable controls for aircraftFuture aircraft with highly sophisticated controls are likely to have multiple interdependent failure modes which will be difficult for the pilot to recognize. Such failures may lead to unanticipated sequences of events from which the pilot cannot intuitively recover. Advances in the state-of-the-art in failure detection, failure identification, and control system technology suggest it may be feasible to detect and identify potentially catastrophic failures in flight controls and to restructure the controls in real time to execute a safe landing. Two accidents are reviewed, one in which the pilot successfully restructured the controls and one in which he did not, but for which a solution existed. The problem requirements and potential theoretical techniques which apply are also discussed.
Document ID
19830060510
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Howell, W. E.
(NASA Langley Research Center Hampton, VA, United States)
Bundick, W. T.
(NASA Langley Research Center Hampton, VA, United States)
Hueschen, R. M.
(NASA Langley Research Center Hampton, VA, United States)
Ostroff, A. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 83-2255
Report Number: AIAA PAPER 83-2255
Meeting Information
Meeting: Guidance and Control Conference
Location: Gatlinburg, TN
Start Date: August 15, 1983
End Date: August 17, 1983
Accession Number
83A41728
Distribution Limits
Public
Copyright
Other

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