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多余度飞行控制系统仿真平台设计 被引量:7

Simulation Platform Design For the Multi-Redundant Flight Control System
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摘要 为验证飞行控制系统的余度配置方式,设计了多余度飞控系统仿真的软硬件平台。该平台基于Simulink图形化的建模方法和Vxworks嵌入式实时操作系统,利用实时仿真工具(RTW)可自动生成运行在Vxworks及相应硬件平台下的代码。还设计了三余度飞控计算机的余度管理算法和表决算法以验证该平台的功能。本仿真平台的建模方法直观明了,同时可利用Simulink外部模式进行实时监控和在线调参,从而提高了平台的升级和维护能力。 In order to validate the redundancy allocation scheme of the flight control system, a simulation platform for multi-redundant flight control system has been designed in this paper. This platform was based on the graphical modeling method of Simulink and the embedded real-time operating system ——Vxworks, where the executable code could be compiled for Vxworks and the relative hardware platform by utilizing the real-time simulation tool (RTW). This paper also proposed the algorithms of triple-redundant management and voting to verify the the functionality of the platform. The modeling method of the proposed platform was straightforward. Besides, real-time monitoring and online debugging could be achieved via the external mode of Simulink, leading to the enhancement of the capability of upgrading and maintenance of the proposed platform.
出处 《系统仿真学报》 CAS CSCD 北大核心 2010年第A01期207-211,共5页 Journal of System Simulation
关键词 多余度 飞控系统 Simulink VXWORKS RTW Multi-Redundant flight control system Simulink Vxworks RTW
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参考文献6

  • 1Yeh Y C. Triple-triple Redundant 777 Primary Flight Computer [C]// IEEE Aerospace Applications Conference Proceedings (ISBN0-7803- 3196-6),Aspen, CO, 1996, 1: 293-307.
  • 2Briere D, Traverse E AIRBUS A320/A330/A340 electrical flight controls-A family of fault-tolerant systems [C] //The Twenty-third International on Symposium on Fault-tolerant Computing. Piscataway: IEEE (ISBN: 0-8186-3680-7), Toulouse, 1993:616-623.
  • 3齐劲松.余度飞行控制计算机系统研究与实现[D].西北工业大学,2005.
  • 4马秋瑜,吴成富,陈怀民,邓宏德,段晓军.基于PC104的三余度飞控计算机同步算法的设计与实现[J].测控技术,2007,26(3):62-64. 被引量:6
  • 5顾颖彦.反射内存网实时通信技术的研究[J].计算机工程,2002,28(7):143-144. 被引量:83
  • 6Malekpour M, Torres W. Characterization of A Recoverable Flight Control Computer System [C] //IEEE International Conference on control Applications (ISBN 0-7803-5446-X), Kohala Coast, HI, 1999, 2: 1519-1524.

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共引文献88

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  • 1朱雨童,王江云.飞行模拟器发动机系统建模方法研究[J].系统仿真学报,2006,18(z2):126-129. 被引量:2
  • 2崔勇,黄金泉.航空发动机双余度智能位置控制器设计[J].推进技术,2005,26(6):535-539. 被引量:7
  • 3郭军,郝克刚.双变迁Petri网的电路模拟技术研究[J].系统仿真学报,2007,19(A01):285-288. 被引量:2
  • 4吴跃.基于EDA的电路故障仿真研究[D].北京:北京航空航天大学,2004
  • 5Kenffield J A C. Professor Emeritus. Aerodyrmmic Loading and Sta- bility of an Aircraft with Outboard Horizontal Stabilizers [ Z ], AIAA,2007 (65) :2 -9.
  • 6KristinA Ahlstrom, JAn Torin. Future Architecture for flight control systems[C]. Proceedings of the 20th D/g/tAl Avionics Systems Con- ference. 2001,10( 1 ) :14 - 18.
  • 7Eva N Wu,Oguz A Aydin. Reliability - Based Modeling & Analysis of Fault - Tolerant Flight Control Systems[Z]. AIAA ,2005 : 1 - 11.
  • 8Lokl, Nghs, Trecatj. Power System Fault Diagnosis Using Petri Nets [J]. Transmission and Distribution on IEE Proceedings-Generator (S1350-2360), 1997, 144(3): 231-236.
  • 9Cheng jiali, Fu lingding. Fuzzy Dynamic Petri Nets [C]// Sixth Intemational Conference on Fuzzy Systems and Knowledge Discovery ($978-0-7695-3735-1), Tianjin, China. USA: 1EEE Computer Society, 2009, 7: 34-38.
  • 10Celso F Silva, Camilo Quintns, Antonio Colmenar, Manuel A Castro, Enrique Mandado. A Method based on Petri nets and a Matrix Model to Implement Reconfigurable Logic Controllers [J]. IEEE Transactions on Industrial Electronics (S0278-0046), 2009. 57(10): 3544-3556.

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