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电传飞控系统供电方案设计与分析 被引量:2

Design and Analysis on the Redundancy Power Supply Scheme for FBW System
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摘要 针对某直升机电传飞行控制系统,提出了一种能够给电传飞控系统提供可靠供电的供电网络,能实现多余度的供电和供电逻辑重构,有效防止了当系统正常运作时,由于部分电源突然故障并且剩余电源无法供给电传飞控系统,使供电系统过载工作,从而出现飞控系统下电的危险。实验室验证和可靠性计算表明,该方案可极大的提高电传飞控系统供电的可靠性,能够保证飞行安全。 To the fly-by-wire control system of a helicopter,a fault isolatable and reconfigurable power supply scheme is proposed in this paper. This power supply scheme could prevent the power supply system from overloading and appearing the power failure of the whole system when the partial power was failed suddenly and the remaining part could not supply the whole flight control system in the normal operation process of the power supply system. The results of laboratory and flight test show that the scheme could improve the reliability of power supply for fly-by-wire control system obviously and ensure the flight safety.
作者 王胜利 李波 WANG Sheng-li;LI Bo(China Helicopter Research and Development Institute, Jingdezhen Jiangxi 333001, China)
出处 《机械研究与应用》 2018年第2期141-143,共3页 Mechanical Research & Application
关键词 电传飞行控制系统 供电方案 多余度 可重构 fly-by-wire control system pouter supply scheme redundancy reconfiguration
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  • 1杨士斌,徐敏.智能蒙皮飞行器的飞行控制研究[J].飞行力学,2007,25(1):39-42. 被引量:10
  • 2Florance J B. Contributions of the NASA Langley Research Center to the DARPA/AFRL/N-ASA/Northrop Grumman Smart Wing Program[ R]. AIAA 2003-1961,2003.
  • 3Johannes Schweiger,Mzal Suleman. MDO Concepts for an European Research Project on Active Aeroelastic Aircraft [ R ]. AIAA 2002-5403,2002.
  • 4North Atlantic Treaty Organization Working Group. Integrated Vehicle Management Systems [ R ]. FRANCE: AGARD-AR-343, 1998.
  • 5Hall I K, Stigall P D. Distibuted Flight Control System Using Fiber Distributed Data Interface (FDDI) [ J ]. Aerospace and Electronic System Magazine, IEEE, 1992, 7 (6) :21-32.
  • 6Ahlstrom K,Torin J. Future Architecture of Flight Control System [ J ]. Aerospace and Electronic System Magazine, IEEE ,2002,17 (12) :21-27.
  • 7Lanny Fields. Airplane Digital Distributed Fly-by-Wire Flight Control System Architectures [ R ]. SAE549 : System Architectures, 2005.
  • 8贾忠.容错计算机在飞行控制系统中的应用技术--机载计算机发展趋势文集[M].北京:电子工业出版社,1997.
  • 9Andrew S.Tanenbaum.分布式操作系统[M].北京:电子工业出版社,1999.
  • 10隋学礼,刘同利,王智鹏.多电源互补供电装置:中国,2009-20312354.4[P].2009-10-13.

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