公开(公告)号：US10055999B2

公开(公告)日：2018-08-21

申请号：US15319489

申请日：2015-06-05

Applicant: THALES

Inventor： Sylvain Lissajoux ,  Eric Guillouet ,  Christophe Garnavault ,  Joël Bosson

IPC: G01C23/00 ,  G08G5/00 ,  G05D1/02

CPC classification number: G08G5/0039 ,  G01C23/005 ,  G05D1/0061 ,  G05D1/0202 ,  G08G5/0052 ,  G08G5/045

Abstract: This method makes it possible to generate a resulting setpoint trajectory of an aircraft, a guiding system controlling the trajectory of the aircraft relative to the resulting setpoint trajectory.The generating method is implemented by an electronic device and comprises selecting at least one mode from among several operating modes, acquiring a setpoint trajectory prepared by a flight management system, obtaining an alternative setpoint trajectory from an element from among a module for computing a trajectory and an external generating system, and generating the resulting setpoint trajectory, which includes one or several segments of the alternative setpoint trajectory for the period of time corresponding to the selection of another mode.

公开(公告)号：US20180075632A1

公开(公告)日：2018-03-15

申请号：US15652801

申请日：2017-07-18

Applicant: THALES

Inventor： Luc Baron ,  Christophe Garnavault ,  Bruno Aymeric ,  Yannick Le Roux

IPC: G06T11/60 ,  G09G5/14 ,  G09G5/00 ,  B64D43/00

CPC classification number: G06T11/60 ,  B64D43/00 ,  G01C23/00 ,  G06F3/14 ,  G06F3/147 ,  G08G5/0021 ,  G09G5/005 ,  G09G5/14 ,  G09G2340/0442 ,  G09G2340/12 ,  G09G2354/00 ,  G09G2380/12

Abstract: The present invention relates to a system (14) for displaying avionic data on at least one display space of an aircraft cockpit, comprising a processing module (23) configured to receive a message to be displayed indicating an event and to associate the content of this message with one of the display formats, a display module (25) configured to display the received message superimposed on at least one current display format, displayed in a respective display space and an acquisition module (27) configured to acquire a display control command relative to the received message. The display module (25) is further configured to display the display format associated with said message on at least one display space in case of acquisition of the display control command relative to said message.

公开(公告)号：US20160101873A1

公开(公告)日：2016-04-14

申请号：US14878489

申请日：2015-10-08

Applicant: THALES

Inventor： Joel Bosson ,  Christophe Garnavault ,  Eric Guillouet

IPC: B64D45/00 ,  G01C21/00 ,  B64C13/04

CPC classification number: B64D45/00 ,  B64C13/04 ,  B64C13/12 ,  B64D45/0005 ,  G01C21/00 ,  G01C23/00

Abstract: The present invention relates to an aid system (30) for piloting an aircraft, the aircraft including at least two piloting units each having at least one piloting member that can be actuated by a pilot to command at least one control surface of the aircraft.The piloting aid system (30) includes a module (32) for detecting actions performed on at least one piloting unit and a feedback module (34) indicating, via a man-machine interface (24A, 24B) separate from the piloting members, the movement of said piloting member and/or the force exerted on said piloting member.

Abstract translation: 本发明涉及一种用于飞行飞行器的辅助系统（30），该飞行器包括至少两个引导单元，每个引导单元具有至少一个可由飞行员致动以便指挥飞行器的至少一个控制表面的引导构件。 引导辅助系统（30）包括用于检测对至少一个引导单元执行的动作的模块（32）和反馈模块（34），所述反馈模块（34）经由与引导构件分离的人机界面（24A，24B） 所述导向构件的运动和/或施加在所述导向构件上的力。

公开(公告)号：US20150360789A1

公开(公告)日：2015-12-17

申请号：US14729509

申请日：2015-06-03

Applicant: THALES

Inventor： Sylvain LISSAJOUX ,  Matthieu Claybrough ,  Christophe Garnavault

IPC: B64D31/06 ,  B64D33/04 ,  B64C25/44

CPC classification number: B64D31/06 ,  B64C25/44 ,  B64D33/04 ,  G01C23/00

Abstract: A method and device for controlling at least one actuator control system of an aircraft, an associated computer program product and aircraft are disclosed. In one aspect, the method includes determining a variation in thrust of the aircraft for controlling a variable relating to the aircraft relative to a set point, calculating a first control command signal to be sent to an engine control system in order to obtain the variation in thrust, and transmitting the first control command signal to the engine control system. The controlled variable can be an acceleration along a direction taken by a speed vector among the air speed vector and the ground speed vector and the set point can be an acceleration set point along the direction.

Abstract translation: 公开了一种用于控制飞机，相关联的计算机程序产品和飞行器的至少一个致动器控制系统的方法和装置。 一方面，该方法包括确定用于控制与飞行器相对于设定点的变量的飞行器的推力变化，计算要发送到发动机控制系统的第一控制命令信号，以获得 推力，并将第一控制命令信号发送到发动机控制系统。 控制变量可以是沿着空气速度矢量和地面速度矢量之间的速度矢量所采取的方向的加速度，并且设定点可以是沿该方向的加速度设定点。

公开(公告)号：US10453234B2

公开(公告)日：2019-10-22

申请号：US15652801

申请日：2017-07-18

Applicant: THALES

Inventor： Luc Baron ,  Christophe Garnavault ,  Bruno Aymeric ,  Yannick Le Roux

IPC: G09G5/00 ,  G06F3/14 ,  G06F3/147 ,  G08G5/00 ,  G06T11/60 ,  B64D43/00 ,  G09G5/14 ,  G01C23/00

Abstract: The present invention relates to a system (14) for displaying avionic data on at least one display space of an aircraft cockpit, comprising a processing module (23) configured to receive a message to be displayed indicating an event and to associate the content of this message with one of the display formats, a display module (25) configured to display the received message superimposed on at least one current display format, displayed in a respective display space and an acquisition module (27) configured to acquire a display control command relative to the received message. The display module (25) is further configured to display the display format associated with said message on at least one display space in case of acquisition of the display control command relative to said message.

公开(公告)号：US10173786B2

公开(公告)日：2019-01-08

申请号：US14878489

申请日：2015-10-08

Applicant: THALES

Inventor： Joel Bosson ,  Christophe Garnavault ,  Eric Guillouet

IPC: B64D45/00 ,  G01C21/00 ,  B64C13/04 ,  B64C13/12 ,  G01C23/00

Abstract: The present invention relates to an aid system (30) for piloting an aircraft, the aircraft including at least two piloting units each having at least one piloting member that can be actuated by a pilot to command at least one control surface of the aircraft.The piloting aid system (30) includes a module (32) for detecting actions performed on at least one piloting unit and a feedback module (34) indicating, via a man-machine interface (24A, 24B) separate from the piloting members, the movement of said piloting member and/or the force exerted on said piloting member.

公开(公告)号：US09856032B2

公开(公告)日：2018-01-02

申请号：US14729509

申请日：2015-06-03

Applicant: THALES

Inventor： Sylvain Lissajoux ,  Matthieu Claybrough ,  Christophe Garnavault

IPC: B64D31/06 ,  B64D33/04 ,  B64C25/44 ,  G01C23/00

CPC classification number: B64D31/06 ,  B64C25/44 ,  B64D33/04 ,  G01C23/00

Abstract: A method and device for controlling at least one actuator control system of an aircraft, an associated computer program product and aircraft are disclosed. In one aspect, the method includes determining a variation in thrust of the aircraft for controlling a variable relating to the aircraft relative to a set point, calculating a first control command signal to be sent to an engine control system in order to obtain the variation in thrust, and transmitting the first control command signal to the engine control system. The controlled variable can be an acceleration along a direction taken by a speed vector among the air speed vector and the ground speed vector and the set point can be an acceleration set point along the direction.