公开(公告)号：US09604718B2

公开(公告)日：2017-03-28

申请号：US14740023

申请日：2015-06-15

Applicant: THALES

Inventor： Sylvain Lissajoux ,  Eric Guillouet ,  Thibaut Debard

IPC: G05D1/00 ,  G05B19/18 ,  B64C13/22 ,  B64C13/04 ,  B64C13/18 ,  B64D31/04 ,  B64D31/06 ,  B64D31/00

CPC classification number: B64C13/22 ,  B64C13/04 ,  B64C13/18 ,  B64D31/00 ,  B64D31/04 ,  B64D31/06 ,  G05D1/0061

Abstract: A method and device for generating at least one set point from a flight control set point, a motor control set point and an aircraft guidance set point, a related computer program product and an aircraft are disclosed. In one aspect, the method includes acquiring a mechanical property relative to at least one corresponding primary control member and computing at least one set point from among one or more primary set points and one or more secondary set points. The method also includes generating at least one of the computed set point(s) and switching, based on the mechanical property acquired for the corresponding primary control member, between a first mode in which one or more primary set points are generated and a second mode in which one or more secondary set points are generated.

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：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：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：US20150360767A1

公开(公告)日：2015-12-17

申请号：US14740023

申请日：2015-06-15

Applicant: THALES

Inventor： Sylvain LISSAJOUX ,  Eric Guillouet ,  Thibaut Debard

IPC: B64C13/22 ,  B64C13/04 ,  B64D31/04 ,  B64C13/18 ,  B64D31/06

CPC classification number: B64C13/22 ,  B64C13/04 ,  B64C13/18 ,  B64D31/00 ,  B64D31/04 ,  B64D31/06 ,  G05D1/0061

Abstract: A method and device for generating at least one set point from a flight control set point, a motor control set point and an aircraft guidance set point, a related computer program product and an aircraft are disclosed. In one aspect, the method includes acquiring a mechanical property relative to at least one corresponding primary control member and computing at least one set point from among one or more primary set points and one or more secondary set points. The method also includes generating at least one of the computed set point(s) and switching, based on the mechanical property acquired for the corresponding primary control member, between a first mode in which one or more primary set points are generated and a second mode in which one or more secondary set points are generated.

Abstract translation: 公开了一种用于从飞行控制设定点，马达控制设定点和飞行器引导设定点，相关的计算机程序产品和飞行器产生至少一个设定点的方法和装置。 在一个方面，该方法包括相对于至少一个对应的主控制构件获取机械性能，并从一个或多个主要设定点和一个或多个辅助设定点计算至少一个设定点。 该方法还包括基于在对应的主控制构件获取的机械特性，在其中产生一个或多个主要设定点的第一模式和第二模式之间产生所计算的设定点和切换中的至少一个 其中生成一个或多个次要设定点。