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

机译:观看飞机态度的方法,相关的计算机程序产品和观看系统

摘要

The present invention relates to a visualization method of the attitude of an aircraft, comprising the formation of a pitch scale (E) defining a lower border and an upper border, and including:to visualize the nil pitch angle of the aircraft, a zero graduation on the lower border and the upper border;to visualize the negative pitch angles of the aircraft, straight parallel graduations forming at least two groups converging toward one another with the approach of the zero graduation from the lower border; andto visualize the positive pitch angles of the aircraft, curved graduations, the curvature of which increases moving away from the zero graduation toward the upper border.
机译:本发明涉及一种飞机姿态的可视化方法,包括形成限定较低边界和上边界的间距(e),并且包括:以可视化飞机的零螺距角度,零刻度 在较低的边界和上边界;为了可视化飞机的负桨距角,直行刻度形成至少两个群体朝着彼此聚集的彼此会聚; 并且可视化飞机的正俯仰角,弯曲刻度,曲率的曲率随着向上边界的零刻度移动而增加。

著录项

  • 公开/公告号EP3521765B1

    专利类型

  • 公开/公告日2021-10-13

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号EP20190155144

  • 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 2022-08-24 21:39:47

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