航空学报 > 2012, Vol. 33 Issue (12): 2279-2290

综合化飞机环境监视系统研究及其数字仿真测试

肖刚1, 敬忠良1, 李元祥1, 刁海南1, 于超鹏2   

  1. 1. 上海交通大学 航空航天学院, 上海 200240;
    2. 中航工业雷达与电子设备研究院, 江苏 无锡 214063
  • 收稿日期:2011-11-18 修回日期:2012-02-05 出版日期:2012-12-25 发布日期:2012-12-24
  • 通讯作者: 肖刚 E-mail:xiaogang@sjtu.edu.cn
  • 作者简介:肖刚 男, 博士, 副教授, 硕士生导师。主要研究方向: 航空电子综合、 信息融合等。Tel: 021-34206192 E-mail: xiaogang@sjtu.edu.cn
  • 基金资助:

    航空科学基金(20095557010,20102057006);上海市大飞机创新工程、上海市高新技术产业化项目以及上海市科技攻关计划项目(10111100302)

Study on Integrated Aircraft Environment Surveillance System and Its Digital Simulation Test

XIAO Gang1, JING Zhongliang1, LI Yuanxiang1, DIAO Hainan1, YU Chaopeng2   

  1. 1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China;
    2. AVIC Radar and Avionics Institute, Wuxi 214063, China
  • Received:2011-11-18 Revised:2012-02-05 Online:2012-12-25 Published:2012-12-24
  • Supported by:

    Aeronautical Science Foundation of China (20095557010, 20102057006); Shanghai Civil Aircraft Innovation Project, Shanghai High-tech Industrialization Project, Shanghai Science and Technology Research Project (10111100302)

摘要:

综合模块化航空电子(IMA)技术日益成为飞机航电系统开发的主流构型。基于美国航空无线电技术委员会(RTCA)对飞机环境监视系统(AESS)的定义,分析了AESS的发展过程及技术趋势,以空客A380、Boeing787飞机的AESS为例进行现状分析,依据ARINC768规范开展了综合飞机环境监视系统(IAESS)方案及架构设计,实现了由综合飞机环境监视系统处理单元(IAESSPU)对T3CAS(TCAS、TAWS和ATCRBS)和WXR数据综合与处理的统一,开展了基于高级体系结构(HLA)的IAESS数字仿真系统设计、测试用例和性能分析,验证了IAESS具有高可靠性、低功耗、低总量等优点,未来IAESS发展也将进一步使得系统具备多功能特点。

关键词: 飞机环境监视系统, 飞机计算机仿真, 航空电子, 数字仿真测试, ARINC768

Abstract:

Integrated modular avionics (IMA) technology is becoming the main trend of modern avionics. Based on the definition of Radio Technical Commission for Aeronautics (RTCA), this paper introduces the development process and technology tendency of aircraft environment surveillance system (AESS). With Airbus A380, Boeing787 AESS as examples, it also analyzes the status quo for AESS. According to ARINC768 standards, the prototype and framework of a so-called integrated aircraft environment surveillance system (IAESS) is designed, which realizes the data synthesis and the information processing consistency for T3CAS (TCAS, TAWS and ATCRBS) and WXR by the integrated aircraft environment surveiuance system processing unit (IAESSPU). Then a digital simulation for the IAESS is performed based on high level architecture (HLA). The test examples and simulation performance are analyzed too. The results verify the high reliability, low power consumption and low volume of the IAESS. Future development of IAESS is also discussed.

Key words: aircraft environment surveillance system, aircraft computer simulation, avionics, digital simulation test, ARINC768

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