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METHOD FOR VIEWING THE ATTITUDE OF AN AIRCRAFT, ASSOCIATED COMPUTER PROGRAM PRODUCT AND VIEWING SYSTEM

机译:用于查看飞机的姿态的方法,相关的计算机程序产品和查看系统

摘要

The present invention relates to a method for displaying the attitude of an aircraft, comprising the formation of a pitch scale (E) defining a low border and a high border, and comprising: - for displaying the zero attitude of the 'aircraft, a zero scale between the lower border and the upper border; - to visualize the negative bases of the aircraft, parallel straight graduations forming at least two groups converging towards each other with the approach of the gradation zero from the lower border; and to display the positive plates of the aircraft, curved graduations whose curvature increases with the distance from the zero graduation to the upper border.
机译:本发明涉及一种用于显示飞机的姿态的方法,其包括形成限定低边界和高边界的俯仰标度(E),并且包括:-用于显示飞机的零姿态,零。在下边框和上边框之间缩放; -为了使飞机的负基座可视化,形成平行的直线刻度,至少形成两个组,并从下边界趋近于零灰度;为了显示飞机的正极板,弯曲了的刻度,其曲率随着从零刻度到上边界的距离而增加。

著录项

  • 公开/公告号EP3521765A1

    专利类型

  • 公开/公告日2019-08-07

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号EP20150005144

  • 发明设计人 MENNECHET FLORENT;SERVANTIE XAVIER;

    申请日2019-02-01

  • 分类号G01C23;

  • 国家 EP

  • 入库时间 2022-08-21 12:26:41

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