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Restructurable ControlsRestructurable control system theory, robust reconfiguration for high reliability and survivability for advanced aircraft, restructurable controls problem definition and research, experimentation, system identification methods applied to aircraft, a self-repairing digital flight control system, and state-of-the-art theory application are addressed.
Document ID
19830025625
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Montoya, R. J. (Research Triangle Inst. Research Triangle Park, N.C., United States)
Howell, W. E. (NASA Langley Research Center Hampton, VA, United States)
Bundick, W. T. (NASA Langley Research Center Hampton, VA, United States)
Ostroff, A. J. (NASA Langley Research Center Hampton, VA, United States)
Hueschen, R. M. (NASA Langley Research Center Hampton, VA, United States)
Belcastro, C. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CP-2277
L-15638
NAS 1.55:2277
Accession Number
83N33896
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19830025626WorkOn Restructurable Control System Theory19830025627WorkRobust Reconfiguration for High Reliability and Survivability for Advanced Aircraft19830025628WorkRestructurable Controls Problem Definition and Future Research19830025629WorkExperimental Experience at Calspan19830025630WorkA Review of System Identification Methods Applied to Aircraft19830025631WorkSelf-repairing Digital Flight Control System19830025632WorkState-of-the-art Theory Application
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