公开(公告)号：US20160085367A1

公开(公告)日：2016-03-24

申请号：US14862384

申请日：2015-09-23

Applicant: THALES

Inventor： Michael MANCEAU ,  Didier POISSON ,  Jean-Noël PERBET

IPC: G06F3/041 ,  G06F3/0484 ,  B64C19/00 ,  G06F3/0488

CPC classification number: G06F3/0416 ,  B64C19/00 ,  G06F3/016 ,  G06F3/0412 ,  G06F3/04847 ,  G06F3/0488 ,  G06F3/04883 ,  G06F2203/04808

Abstract: A data input system and a method implementing the system, including physical controls, an environment sensor and a touchscreen displaying virtual commands, the method defining and displaying at least one virtual control on the touchscreen and assigning a datum to be input to one of the controls. The datum to be input is assigned to both a first of the physical controls and a first of the virtual controls. The topology of the virtual controls is adapted to environmental conditions.

Abstract translation: 数据输入系统和实现该系统的方法，包括物理控制，环境传感器和显示虚拟命令的触摸屏，所述方法定义并显示在触摸屏上的至少一个虚拟控件并且将要输入的数据分配给控件之一 。 要输入的数据被分配给第一个物理控件和第一个虚拟控件。 虚拟控件的拓扑结构适用于环境条件。

公开(公告)号：US20160363459A1

公开(公告)日：2016-12-15

申请号：US15176682

申请日：2016-06-08

Applicant: THALES

Inventor： Sylvain LISSAJOUX ,  Bruno AYMERIC ,  Didier POISSON

IPC: G01C23/00 ,  B64D43/02

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.

Abstract translation: 用于辅助飞机驾驶的该电子设备包括：获取模块，被配置为获取飞行器的滚动角度的当前值; 计算模块，被配置为计算对应于飞行器停止开始的滚转角度限制; 以及显示模块，被配置为在屏幕上显示指示飞行器的当前方向的第一符号。 计算模块被配置为计算至少一个滚动边缘，每个滚动边距取决于相应的滚动角度限制和滚动角度的当前值，并且当显示条件被验证时，显示模块被配置为显示在 所述屏幕，相对于所述第一符号定位的至少一个第二符号，每个第二符号与所述第一符号之间的偏差表示相应的卷边距。

公开(公告)号：US20230192312A1

公开(公告)日：2023-06-22

申请号：US17924969

申请日：2021-05-12

Applicant: THALES

Inventor： Frédéric BERGER ,  Thierry GANILLE ,  Didier POISSON ,  Pierre-Yves DUMAS

IPC: B64D43/02 ,  B64D45/08 ,  G01C23/00

CPC classification number: B64D43/02 ,  B64D45/08 ,  G01C23/005

Abstract: Disclosed is a method of guiding the pilot of an aircraft for the alignment maneuver, including: determining at a first instant an occurrence close to the alignment maneuver and triggering the display of a first symbol on the screen; updating the position of the first symbol on the horizon according to the updated value of the aircraft heading; when the alignment maneuver is to begin, moving a second symbol on the screen from the position of the first symbol, the direction of the displacement with respect to the horizon being determined depending on the direction of the crosswind with respect to the runway and the value of the displacement being determined depending on the difference between the current dynamic sideslip of the aircraft and a current dynamic sideslip setpoint value calculated for the aircraft.

公开(公告)号：US20180276999A1

公开(公告)日：2018-09-27

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

CPC classification number: G08G5/0039 ,  G01C21/00 ,  G08G5/0021 ,  G08G5/0052

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：US20180033207A1

公开(公告)日：2018-02-01

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

CPC classification number: G06T19/006 ,  B64D43/00 ,  G01C23/005 ,  G06F3/147 ,  G06T19/003 ,  G06T19/20 ,  G06T2219/2004 ,  G06T2219/2016 ,  G09G2340/14 ,  G09G2354/00 ,  G09G2380/12

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：US20160161278A1

公开(公告)日：2016-06-09

申请号：US14958812

申请日：2015-12-03

Applicant: THALES

Inventor： Xavier SERVANTIE ,  Didier POISSON

IPC: G01C21/36

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.

Abstract translation: 本发明的一般领域是用于车辆的合成视觉系统的一般领域，所述车辆具有特定的导航方向。 根据本发明的系统至少包括：代表车辆行驶的地形的地图数据库，所述车辆的地理定位装置，用于计算所述车辆的主要参数的表示的电子装置; 用于产生所述地形的三维合成表示的图形发生器装置; 以及在特定视场（FOV）和特定显示方向上显示所述三维合成表示的显示装置，用于将显示方向修改为与车辆的特定导航方向不同的方向的装置，所述修改装置是 手动或自动，显示方向然后是导航或导航参数的功能。