直升机试飞测试参数实时显示
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  • 英文篇名:Display Test Parameters of Helicopter Flight Test in Real-time
  • 作者:任远
  • 英文作者:REN Yuan;China Helicopter Research and Development Institute;
  • 关键词:直升机 ; 试飞测试 ; 实时显示
  • 英文关键词:flight test;;Real-time display;;real-time display
  • 中文刊名:SZJT
  • 英文刊名:Digital Technology & Application
  • 机构:中国直升机设计研究所;
  • 出版日期:2019-03-25
  • 出版单位:数字技术与应用
  • 年:2019
  • 期:v.37;No.345
  • 语种:中文;
  • 页:SZJT201903085
  • 页数:2
  • CN:03
  • ISSN:12-1369/TN
  • 分类号:170+173
摘要
显示系统对直升机而言是一个很重要的界面,飞行员可以从这个界面获得相关数据以及一些至关重要的信息,如指示空速、气压高度、横滚角、俯仰角等重要的飞行参数。座舱显示系统主要用于试飞时,在座舱内为飞行员提供操纵量、飞行过载、侧滑角等实测飞行参数,为飞行员完成预定科目提供实况数据。
        The display system is an important interface for helicopters. From this interface, pilots can obtain relevant data as well as some vital information such as airspeed, barometric altitude, roll angle, pitch angle and other important flight parameters. The cockpit display system is mainly used for flight test, and provides pilots with measured flight parameters such as maneuvering amount, flight overload and side slip angle in the cockpit, and provides live data for the pilot to complete the scheduled subject.
引文
[1]王化翔,张淑英.传感器原理及应用[M].天津:天津大学出版社,2007.