标准空速管角度测试装置测控系统设计
Measurement and Control System Design for the Standard Pitot Tube Angle Test Device
  
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中文摘要:
      随着航空技术的发展,现有攻角、侧滑角传感器的测试方法无法满足机载系统大量测试的需求。针对这一现状,基于labview语言设计了一套标准空速管角度测试装置测控系统,并详细阐述了系统的工作原理、硬件结构和软件设计。经实验验证,该测控系统可靠性好、自动化程度高,为机载系统的相关性能评价提供了重要依据。
英文摘要:
With the development of aviation technology, the existing testing methods of angle of attack and sideslip sensors cannot meet the needs of a large number of airborne system testing. In view of this situation, based on LabVIEW language, a set of measurement and control system of standard airspeed tube angle test device is designed, and the working principle, hardware structure and software design of the system are described in detail. The experimental results show that the measurement and control system have good reliability and high automation, which provides an important basis for the performance evaluation of airborne systems.
作者单位
孔祥雪,李亚晋,张鹏 航空工业北京长城计量测试技术研究所, 北京100095 
中文关键词:  标准空速管  攻角  侧滑角  测控系统
英文关键词:standard pitot tube  angle of attack  angle of sideslip  control system
基金项目:
DOI:10.11823/j.issn.1674-5795.2019.03.10
引用本文:孔祥雪,李亚晋,张鹏.标准空速管角度测试装置测控系统设计[J].计测技术,2019,39(3):.
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