The vision system for an aircraft according to the invention comprises a display management system, on a display, capable of dynamically displaying synthetic information coming from a synthetic environment generating assembly on the display. The management assembly can control the display, on a first region of the display, of relief lines representative of the terrain situated facing the aircraft, without displaying synthetic surface representations of the terrain in the intermediate areas situated between the relief lines of the first region of the display. The generating assembly includes means for determining the position of the crest lines of the terrain from topographical data present in at least one database, and means for computing the position of the relief lines from the position of the crest lines of the terrain.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft vision system with relief lines and associated method


    Contributors:

    Publication date :

    2018-07-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G06T Bilddatenverarbeitung oder Bilddatenerzeugung allgemein , IMAGE DATA PROCESSING OR GENERATION, IN GENERAL



    Aircraft vision system, and associated vision method

    BAUDSON OLIVIER / TURPIN ARNAUD | European Patent Office | 2015

    Free access

    Vision system for an aircraft approaching a landing runway and associated vision method

    BAUDSON OLIVIER / TURPIN ARNAUD | European Patent Office | 2016

    Free access

    Aircraft compression relief rod

    NANDALOCHANA CHATHURA B / WENTLAND MARK E / BRUHNS JOEL A et al. | European Patent Office | 2020

    Free access

    Aircraft enhanced vision system, related aircraft, and vision process

    LEFLOUR GÉRARD / LAGARDE JÉRÔME / SOUDAIS PAUL et al. | European Patent Office | 2020

    Free access

    Aircraft pressure relief device and pressure relief control method

    ZHANG HUI / GAO FEI / RUI PENG et al. | European Patent Office | 2024

    Free access