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system for controlling an aircraft to control the aircraft, at least in ungenauem approach and the subsequent landing

机译:用于控制飞机以至少在非定距进近和随后着陆中控制飞机的系统

摘要

- system for piloting an aircraft, at least for piloting the aircraft during a non-precision approach, in view of a landing. - the control system (1) comprises information sources (2) which supply at least an indication of the actual position of the aircraft and of information making it possible to characterize a virtual approach path, and an information processing unit (3) which comprises a landing aid multimode receiver (5) which includes a function (6) of assisted approach mode, capable of determining the lateral and vertical deviations between the actual position of the aircraft and the position that it would have if it was on the approach axis, and which transmits the lateral and vertical deviations thus determined to a user device (4).
机译:-鉴于着陆,用于驾驶飞机的系统,至少用于在非精确进场期间驾驶飞机的系统。 -控制系统(1)包括信息源(2)和信息处理单元(3),信息源至少提供飞机的实际位置的指示以及使得能够表征虚拟进场路径的信息。着陆辅助多模式接收器(5),包括辅助进近模式功能(6),能够确定飞机的实际位置与飞机在进近轴上的位置之间的横向和垂直偏差,以及将如此确定的横向和纵向偏差传送给用户设备(4)。

著录项

  • 公开/公告号DE602004015180D1

    专利类型

  • 公开/公告日2008-09-04

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号DE20046015180T

  • 发明设计人 PEYRUCAIN ERIC;TATHAM GILLES;

    申请日2004-02-26

  • 分类号G05D1/06;

  • 国家 DE

  • 入库时间 2022-08-21 19:48:09

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