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A method and apparatus for automatically triggering of a rescue system for an aircraft

机译:一种自动触发飞机的救援系统的方法和装置

摘要

A process for the triggering of a rescue system and / or a warning signal for an aircraft, wherein the current distance (h) of the aircraft above the ground (2) as well as the vertical rate of descent rate (v) are determined, and a signal (6, 6.1, 6.2) is generated when a predetermined minimum level above the ground (mh) is not reached in the case of simultaneous exceeding a maximum vertical rate of descent rate, characterized in that the height of the aircraft above the ground (h) on the basis of satellite navigation and initial geographical data is determined by measuring the current altitude above sea level is detected and thereof, the height of the base, located beneath the aircraft above sea level (2) is subtracted.
机译:用于触发飞机的救援系统和/或警告信号的过程,其中确定飞机在地面(2)上方的当前距离(h)以及垂直下降率(v),在同时超过最大垂直下降率的情况下,如果没有达到地面以上最低预定高度(mh)时,会产生信号(6、6.1、6.2),其特征在于飞机的高度超过在卫星导航的基础上确定地面(h),并通过测量检测到的当前海拔高度确定初始地理数据,并减去位于飞机海拔(2)下方的底座高度。

著录项

  • 公开/公告号DE102011105059B4

    专利类型

  • 公开/公告日2017-03-30

    原文格式PDF

  • 申请/专利权人 MARTIN WEIDENTHALER;

    申请/专利号DE201110105059

  • 发明设计人 GLEICH PATENTINHABER;

    申请日2011-06-20

  • 分类号B64D45/04;B64D17/54;B64D45/00;B64D25/00;

  • 国家 DE

  • 入库时间 2022-08-21 13:23:09

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