公开(公告)号：US10036651B2

公开(公告)日：2018-07-31

申请号：US15176682

申请日：2016-06-08

Applicant: THALES

Inventor： Sylvain Lissajoux ,  Bruno Aymeric ,  Didier Poisson

IPC: B64D43/02 ,  G01C23/00

CPC classification number: G01C23/005 ,  B64D43/02

Abstract: This electronic device for aiding with the piloting of an aircraft includes: an acquisition module, configured to acquire a current value of the roll angle of the aircraft; a computing module configured to compute a roll angle limit corresponding to a beginning of stalling of the aircraft; and a display module, configured to display, on a screen, a first symbol indicating a current orientation of the aircraft. The computing module is configured to compute at least one roll margin, each roll margin depending on a corresponding roll angle limit and the current value of the roll angle, and the display module is configured, when the display condition is verified, to display, on the screen, at least one second symbol positioned relative to the first symbol, the deviation between each second symbol and the first symbol representing a respective roll margin.

公开(公告)号：US20160133136A1

公开(公告)日：2016-05-12

申请号：US14934108

申请日：2015-11-05

Applicant: THALES

Inventor： Xavier Servantie ,  Emmanuel Monvoisin ,  Didier Poisson

IPC: G08G5/00 ,  G01C23/00 ,  G06T11/60 ,  G06F17/30 ,  G06T15/00

CPC classification number: G08G5/0047 ,  G01C23/00 ,  G06F16/29 ,  G06T11/60 ,  G06T15/00 ,  G06T2215/16

Abstract: The general field of the invention is that of methods of representing a cartographic image in a geolocated synthetic vision system for vehicles, said system including a cartographic database, geolocation means, graphic generation means enabling generation of a two-dimensional or three-dimensional synthetic view of said terrain, and a display device. In the method in accordance with the invention, the angular position of each point of the synthetic view is known with an angular error depending on the distance of said vehicle and the accuracy of geolocation of said vehicle, if said angular error is less than or equal to a predetermined angular tolerance, the point is represented in a standard representation mode and if said angular error is greater than a predetermined angular tolerance, the point is represented in an uncertainty representation mode different from the standard representation mode. The applications are preferably aeronautical.

Abstract translation: 本发明的一般领域是在用于车辆的地理位置合成视觉系统中表示制图图像的方法，所述系统包括制图数据库，地理位置装置，能够产生二维或三维合成视图的图形生成装置 的所述地形，以及显示装置。 在根据本发明的方法中，如果所述角度误差小于或等于，所述合成视点的每个点的角位置是取决于所述车辆的距离和所述车辆的地理定位的精度的角度误差而已知的 该点以标准表示模式表示，并且如果所述角度误差大于预定角度公差，则该点以不同于标准表示模式的不确定性表示模式表示。 这些应用优选是航空的。

公开(公告)号：US10854094B2

公开(公告)日：2020-12-01

申请号：US15919630

申请日：2018-03-13

Applicant: THALES

Inventor： Benoit Dacre-Wright ,  Didier Poisson ,  Guy Deker ,  Vincent Savarit

IPC: G08G5/00 ,  G05D1/02 ,  G05D1/08 ,  G05D1/04 ,  G05D1/06 ,  G01C21/00 ,  G05D1/00

Abstract: A method is provided for adjusting a flight plan rejoining trajectory of an aircraft, the method being implemented in a flight management system of the aircraft. In a first step, the rejoining trajectory comprises a guidance setpoint holding point to be reached situated in the extension of a guidance setpoint, and set manually or automatically, the guidance setpoint no longer being necessarily maintained when this setpoint holding point is passed. This first step can be preceded by a step of rejoining a guidance setpoint or a step of searching for the intersection of the current guidance setpoint trajectory with a segment of the flight plan.

公开(公告)号：US10249097B2

公开(公告)日：2019-04-02

申请号：US15640933

申请日：2017-07-03

Applicant: THALES

Inventor： Romain Sacheau ,  Didier Poisson ,  Emmanuel Monvoisin ,  Frédéric Scarfone ,  Patrice Malot

IPC: G06T19/00 ,  B64D43/00 ,  G01C23/00 ,  G06T19/20 ,  G06F3/147

Abstract: A method for managing a symbology in an on-board viewing system for an aircraft, the graphical representation comprising the piloting and navigation symbology overlaid on a representation of the exterior landscape, the symbology comprises a first angular attitude scale comprising a first symbol called an aircraft mockup, a second speed scale, a third altitude scale and a second symbol called the speed vector. When the angular lateral distance between the position of the first symbol and the position of the second symbol is such that the second symbol is not overlaid on the lateral scales, the various scales are represented in the nominal position; when the angular lateral distance between the position of the first symbol and the position of the second symbol is such that the second symbol is overlaid on one of the scales, the various scales move and/or their size decreases.

公开(公告)号：US09719793B2

公开(公告)日：2017-08-01

申请号：US14958812

申请日：2015-12-03

Applicant: THALES

Inventor： Xavier Servantie ,  Didier Poisson

IPC: G01C21/36 ,  G01C21/00 ,  G01C23/00 ,  G06F3/01 ,  G08G5/00 ,  G02B27/01 ,  G09B29/00

CPC classification number: G01C21/3635 ,  G01C21/00 ,  G01C23/00 ,  G02B27/01 ,  G02B2027/014 ,  G06F3/012 ,  G08G5/0021 ,  G08G5/0052 ,  G08G5/0086 ,  G09B29/007

Abstract: The general field of the invention is that of synthetic vision systems for a vehicle, said vehicle having a particular navigation direction. The system in accordance with the invention includes at least: a cartographic database representative of the terrain travelled over by the vehicle, means for geolocation of said vehicle, electronic means for computing a representation of the principal parameters of said vehicle; graphic generator means for generating a three-dimensional synthetic representation of said terrain; and a display device displaying said three-dimensional synthetic representation in a particular field of view (FOV) and in a particular display direction, means for modifying the display direction to a direction different from the particular navigation direction of the vehicle, said modification means being manual or automatic, the display direction then being a function of a piloting or navigation parameter.