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基于虚拟仪器技术的飞行参数检测设备设计 被引量:2

Design of flight data recorder system testing device based on virtual instrument
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摘要 本文介绍基于虚拟仪器技术飞行参数记录系统检测设备的功能需求,分析硬件和软件的设计方案,讨论直流信号生成与检测模块、12位并行码生成与检测模块等设计问题。采用虚拟仪器技术,在PC总线结构基础上可对飞机飞行参数系统整体和各分部件的性能进行全面检测。检测系统具有硬件可靠性高、软件可移植和可扩充的特点,性价比优良。 In this paper, a flight data recorder system testing device is introduced which is based on virtual instrument. Its design scheme, including its function, hardware and software, as well as the direct current signal generator and modularized testing, bring about twelve bits collateral code and modularized testing of question to be designed are discussed. The hardware of this device has good reliability, and the maintainability and extensibility of software are very well, all of these advantages make this device has high performance to price ratio.
作者 孔韬 蒋绍先
出处 《国外电子测量技术》 2006年第8期36-38,共3页 Foreign Electronic Measurement Technology
关键词 飞行参数采集记录系统 虚拟仪器 模块化设计 串行通讯 flight data register system, virtual instrument, modularized design, serial communication.
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参考文献3

  • 1刘君化 贾惠芹 丁晖 阎晓艳.虚拟仪器图形化编程语言[M].西安:西安电子科技大学出版社,2001..
  • 2William Buchanan.PC接口通信与Windows 编程[M].北京:中国电力出版社,2001.
  • 3Harold Goldberg.What is Virtual Instrumentation?[J].IEEE Instrumentation & Measurement Magazine,2000,3(4).

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