Title: Architecture Analysis And Development Of Distributed FBW Flight Control System
Abstract: As the most important supported technique in an aviation vehicle,the flight control has developed from damper,augment stability system,control augment stability system to fly by wire.And now the integrated control is the most trend of the flight control in a new generation aircraft platform.This paper discusses the inherent requests of the flight control system architecture development in manifold points of view,and also analyzes the status,development and challenge of the distributed flight control system architecture.
Publication Year: 2009
Publication Date: 2009-01-01
Language: en
Type: article
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Cited By Count: 1
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