公开(公告)号：US20190113593A1

公开(公告)日：2019-04-18

申请号：US16143714

申请日：2018-09-27

Applicant: Airbus Operations S.A.S.

Inventor： Jerôme Bazile ,  Patrice Rouquette ,  Sylvain Raynaud ,  Nicolas Marconnet ,  Guillaume Discours ,  Kevin Etchebarne

IPC: G01S1/02 ,  G01S1/18 ,  G01S1/16 ,  G01S13/91 ,  G08G5/02

Abstract: The system for aiding the landing of an aircraft on a landing runway of an airport equipped with an Instrument Landing System (“ILS”) corresponding to an axis of a predetermined approach, includes: an ILS signals receiver and a processing unit. The processing unit is configured to, when the ILS signals receiver) has not yet captured a Glide signal corresponding to a Glide axis of the approach as a function of items of information relating to the predetermined approach, acquired from a database, determine a protection volume in which there is no risk of the ILS signals receiver detecting a replica of the Glide signal; and when a current position of the aircraft is above the protection volume, inhibit the capture of the Glide signal by the ILS signals receiver and instruct the emission of an alert item of information in the cockpit of the aircraft.

公开(公告)号：US20180174473A1

公开(公告)日：2018-06-21

申请号：US15840522

申请日：2017-12-13

Applicant: Airbus Operations (S.A.S.)

Inventor： Esteban Quiroz-Hernandez ,  Christophe Bouchet ,  Jean-Pierre Demortier ,  Sylvain Raynaud ,  François Cusset ,  Marc Vie ,  Alexandre Grattard

IPC: G08G5/02 ,  G01C21/20 ,  G05D1/06 ,  G05B19/05

CPC classification number: G08G5/025 ,  G01C21/20 ,  G01C23/00 ,  G05B17/02 ,  G05B19/0423 ,  G05B19/056 ,  G05B2219/1187 ,  G05D1/0653 ,  G08G5/0021

Abstract: A method and device for adjusting performance variables of an aircraft. The device which is intended for adjusting performance variables, the performance variables being generated by at least one performance module, includes an auxiliary data input unit for entering into a flight management system correction data intended to be used for adjusting at least one associated performance variable, and a correction unit for carrying out a correction, the correction including adjusting the associated performance variable on the basis of the input correction data.

公开(公告)号：US09922568B2

公开(公告)日：2018-03-20

申请号：US15351852

申请日：2016-11-15

Applicant: Airbus Operations S.A.S.

Inventor： Sylvain Raynaud ,  Jean-Claude Mere ,  Simon Sellem

IPC: G05D1/02 ,  G08G5/00 ,  G05D1/10

CPC classification number: G08G5/0039 ,  G05D1/0077 ,  G05D1/101 ,  G08G5/003

Abstract: A flight management unit includes two guidance subsystems each including a flight management system, each of the flight management systems being configured at least to extract a flight plan from at least one navigation database, to construct a flight trajectory, and to compute guidance commands for the aircraft. The flight management unit also includes at least one monitoring unit configured to compute a guidance command from a validated flight trajectory and a consolidated flight plan and to monitor the guidance command, as well as guidance commands computed by the two flight management systems so as to be able to detect and to identify a defective flight management system.