分布式电传飞行控制系统结构发展及分析  

Architecture Analysis And Development Of Distributed FBW Flight Control System

作　　者：占正勇[1] 刘林[1] 

机构地区：[1]西安飞行自动控制研究所飞控部,陕西西安710065

出　　处：《飞行力学》2009年第6期1-4,9,共5页Flight Dynamics

基　　金：航空基金资助项目(2006ZC18003)

摘　　要：飞行控制作为各类航空飞行器最主要的支撑技术,经历了从阻尼器、增稳系统、控制增稳到电传技术的发展历程。新一代飞机平台的发展主流正在向综合控制体制迈进,从多个角度阐述了飞行控制系统结构发展的内在要求,并对分布式飞行控制系统结构演进的现状、发展和面临的挑战进行了系统分析。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.

关 键 词：飞行控制 系统结构 分布式系统 容错 重构 

分 类 号：V249[航空宇航科学与技术—飞行器设计]