电子与自动控制

基于余度和容错技术的高可靠机载智能配电系统设计

展开
  • 北京航空航天大学 自动化科学与电气工程学院, 北京 100191
徐金全(1986- ) 男,博士研究生。主要研究方向:机载电气系统设计。 Tel: 010-82339498 E-mail: xujinquan_buaa@163.com 郭宏(1967- ) 男,博士,教授,博士生导师。主要研究方向:机载电气系统设计、特种电机设计及其驱动控制。 Tel: 010-82339498 E-mail: guohong@buaa.edu.cn

收稿日期: 2011-03-01

  修回日期: 2011-04-23

  网络出版日期: 2011-11-24

Design of Intelligent Airborne Power Distribution Systems with High Reliability Based on Redundancy and Fault-tolerant Technology

Expand
  • School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China

Received date: 2011-03-01

  Revised date: 2011-04-23

  Online published: 2011-11-24

摘要

针对大型无人机(UAV)用常规配电系统占用航空总线资源多和可靠性低的问题,通过研究多电/全电飞机技术发展趋势和大型无人机供电系统技术特点,提出一种适用于大型无人机体系结构和指标要求的机载智能配电系统;建立系统的马尔可夫模型,计算和分析不同余度结构的供电处理机(PSP)和电气负载管理中心(ELMC)对系统可靠性的影响,进而实现机载智能配电系统余度结构的优化配置;提出一种适用于大型无人机机载配电系统的、基于总线形式的PSP与ELMC相互监控方法,有效解决了三余度系统的二次故障容错问题;在此基础上,采用高速数字信号处理器(DSP)、大规模现场可编程门阵列(FPGA)和实时软件进行系统设计,完成了原理样机的研制。理论分析和实验结果表明,所设计的机载配电系统具有高可靠性、容错性和智能化的特点。

本文引用格式

徐金全, 郭宏, 张秦岭, 钱浩 . 基于余度和容错技术的高可靠机载智能配电系统设计[J]. 航空学报, 2011 , 32(11) : 2117 -2123 . DOI: CNKI:11-1929/V.20110526.1756.019

Abstract

An intelligent airborne power distribution system for large-scale unmanned aerial vehicles (UAVs) is presented to deal with the excessive avionics bus resource occupancy and low reliability of traditional power distribution systems in keeping with the development of aircraft electric technology and the electrical system characteristics of UAVs. In order to realize the optimal allocation of intelligent airborne power distribution system redundancy structure, the approach establishes a Markov model to analyze the impact of different redundancy power supply processors (PSPs) and electrical load management centers (ELMCs) on system reliability. At the same time, a mutual monitoring approach between the PSP and the ELMC is put forward to solve the fault monitoring problem for the dual redundant system. On this basis, a prototype is developed with a high speed digital signal processor (DSP), huge field-programmable gate arrays (FPGAs) and real-time software. Theoretical analysis and experimental results demonstrate that the designed airborne power distribution system has the characteristics of high reliability, fault tolerance and intelligence.

参考文献

[1] Izquierdo D, Azcona R, del Cerro F, et al. Electrical power distribution system (HV270DC), for application in more electric aircraft[J]. 2010 Twenty-Fifth Annual IEEE Applied Power Electronics Conference and Exposition (APEC). 2010: 1300-1305.

[2] Rosero J A, Ortega J A, Aldabas E, et al. Moving towards a more electric aircraft[J]. IEEE Aerospace and Electronic System Magazine, 2007, 22(3): 3-9.

[3] Howse M. All electric aircraft[J]. IEE Power Engineer, 2003, 17(4): 35-37.

[4] Maldonado M A, Shah N M, Cleek K J. Power management and distribution system for a more-electric aircraft (MADMEL) program status[J]. IEEE Aerospace and Electronic Systems Magazine, 1999, 12(12): 3-8.

[5] Avery C R, Burrow S G, Mellor P H. Electrical generation and distribution for the more electric aircraft//42nd International Universities Power Engineering Conference. 2007: 1007-1012.

[6] Jones R I. The more electric aircraft: the past and the future?[J]. IEE Colloquium on Electrical Machines and Systems for the More Electric Aircraft. 1999: 1-4.

[7] Izquierdo D, Barrado A, Sanz M, et al. Modeling methods for Solid State Power Controllers (SSPC) //Compatibility and Power Electronics. 2009: 265-270.

[8] Cotton I, Husband M. Higher voltage aircraft power systems[J]. IEEE Aerospace and Electronics Systems Magazine, 2008, 23(2): 25-32.

[9] Zhang Q L, Xu J Q, Guo H. The study of an intelligent three-redundant electrical load management center based on DSP and FPGA//International Conference on Electrical Machines and Systems. 2010: 1907-1911.

[10] 王宏伦, 王英勋. 无人机飞行控制与管理[J]. 航空学报, 2008, 29(S1): S1-S7. Wang Honglun, Wang Yingxun. Flight control and management system of unmanned aerial vehicles[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(S1): S1-S7. (in Chinese)

[11] Fu D F, Xing Y, Yang S H. Electrical power distribution system based on 1553B bus for advanced aircraft//International Conference on Electrical Machines and Systems. 2005: 2373-2375.

[12] 谢拴勤, 濮孟勇. 先进飞机电气系统处理机的研究及实现[J]. 计算机测量与控制, 2008, 16(11): 1584-1587. Xie Shuanqin, Pu Mengyong. Research and implement of power system processor in advanced aircraft[J]. Computer Measurement & Control, 2008, 16(11): 1584-1587. (in Chinese)

[13] 王少萍. 工程可靠性[M]. 北京: 北京航空航天大学出版社, 2000: 88-101. Wang Shaoping. Reliability engineering [M]. Beijing: Beihang University Press, 2000: 88-101. (in Chinese)

[14] 岳小杰, 王少萍, 石健. 机载机电系统可靠性的计算机辅助分析方法[J]. 航空学报, 2007, 28(3): 708-713. Yue Xiaojie, Wang Shaoping, Shi Jian. Computer assistant analysis for reliability of airborne electromechanical systems[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(3): 708-713. (in Chinese)

[15] Weber P, Poure P, Theilliol D, et al. Design of hardware fault tolerant control architecture for wind energy conversion system with DFIG based on reliability analysis// IEEE International Symposium on Industrial Electronics. 2008: 2323-2328.

[16] Chan P, Lyu M R. Developing aerospace applications with a reliable web services paradigm//2008 IEEE Aerospace Conference. 2008: 1-13.
文章导航

/