首页> 外国专利> SYSTEM AND METHOD FOR ADJUSTING THE CORRELATION BETWEEN A PERSPECTIVE OF AN ONBOARD VISUAL DISPLAY AND A CURRENT ORIENTATION OF AN INFLIGHT AIRCRAFT

SYSTEM AND METHOD FOR ADJUSTING THE CORRELATION BETWEEN A PERSPECTIVE OF AN ONBOARD VISUAL DISPLAY AND A CURRENT ORIENTATION OF AN INFLIGHT AIRCRAFT

机译:用于调节机载视觉显示器的视角与飞行飞机的当前方向之间的相关性的系统和方法

摘要

Methods are provided for adjusting any correlation between a perspective of an onboard visual display and a current orientation of an inflight aircraft. The method comprises determining the current orientation of the inflight aircraft and determining the perspective of the visual display. The visual display is shown to a pilot of the inflight aircraft on a display element located onboard the inflight aircraft. The current orientation of the aircraft is compared with the perspective of the visual display to determine if the perspective of the visual display needs to transition to reflect the current orientation of the aircraft. If the display does need to be changed, a rate of transition of the visual display's perspective is selected based on current aircraft performance parameters. The perspective of the visual display is then transitioned to reflect the current orientation of the aircraft at the selected rate.
机译:提供了用于调节机载视觉显示器的视角与飞行中飞机的当前方向之间的任何相关性的方法。该方法包括确定飞行中的飞机的当前方向以及确定视觉显示器的视角。在机上飞机上的显示元件上向机上飞机的飞行员显示视觉显示。将飞机的当前方位与视觉显示器的视角进行比较,以确定视觉显示器的视角是否需要转变以反映飞机的当前方位。如果确实需要更改显示,则根据当前的飞机性能参数选择视觉显示的视角的转换率。然后,转换视觉显示的透视图以反映选定速率下飞机的当前方向。

著录项

  • 公开/公告号US2019311646A1

    专利类型

  • 公开/公告日2019-10-10

    原文格式PDF

  • 申请/专利权人 HONEYWELL INTERNATIONAL INC.;

    申请/专利号US201916417215

  • 发明设计人 GANG HE;

    申请日2019-05-20

  • 分类号G09B9/32;H04B7/185;G01C23;G01S19/26;

  • 国家 US

  • 入库时间 2022-08-21 12:06:54

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