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Requirement analysis of an intelligent, redundant, actuation systemThe reliability and fault tolerance requirements of integrated, critical, digital fly-by-wire control systems for advanced military and civil aircraft requires redundant, reconfigurable implementations of the actuation system. An effective way for controlling the actuators and implementing the required fault detection and reconfiguration strategies is by means of dedicated microprocessors. This paper describes a laboratory implementation of a flexible intelligent redundant actuation system capable of demonstrating the concept and analyzing a variety of configurations and technical issues.
Document ID
19870029492
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
De Feo, P.
(SPARTA, Inc. Laguna Hills, CA, United States)
Shih, K. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Instrumentation
Accession Number
87A16766
Distribution Limits
Public
Copyright
Other

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