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Brief description of the evaluation and signalling lateral of the margins of maneuver on either side of the trajectory of the flight plan of a 371

机译:在371型飞机的飞行计划轨迹的任一侧上的机动余量的评估和横向信号的简要说明

摘要

The parts of the flight plan of an aircraft corresponding to the lateral trajectory at low altitude may comprise the freedom of lateral deployment limited either by the risk of collision with the ground, or by the risk of penetration into a forbidden overfly zone. The method makes it possible to the signal to the attention of the crew, on the navigation screen, so that it redoubling attention. It uses for this purpose a detection method similar to that of the taws systems alarm of risk of collision with the ground protection envelopes tied to the aircraft, according to the monitoring the integrity of the spaces necessary for the aircraft to perform flat turns that are as tight as is permitted, while taking account of the local wind.
机译:飞机的飞行计划中与低海拔处的侧向轨迹相对应的部分可以包括侧向展开的自由度,该自由度受到与地面碰撞的风险或渗透到禁止飞越区域的风险的限制。该方法使得有可能在导航屏幕上向乘员发出信号,从而使注意力加倍。为此,它根据监视飞机执行平面转弯所需空间的完整性,使用一种类似于飞行系统的警报系统的检测方法,该警报系统具有与绑扎在飞机上的地面保护层相撞的危险。在考虑当地风向的情况下,尽量允许收紧。

著录项

  • 公开/公告号FR2871879B1

    专利类型

  • 公开/公告日2006-09-01

    原文格式PDF

  • 申请/专利权人 THALES SOCIETE ANONYME;

    申请/专利号FR20040006654

  • 发明设计人 BITAR ELIAS;MARTY NICOLAS;

    申请日2004-06-18

  • 分类号G01C21/20;B64D45/04;G01C5/00;G01C23/00;

  • 国家 FR

  • 入库时间 2022-08-21 21:17:25

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