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：US09472107B2

公开(公告)日：2016-10-18

申请号：US14737362

申请日：2015-06-11

Applicant: THALES

Inventor： Sylvain Lissajoux ,  Bruno Aymeric ,  Thibaut Debard

IPC: G01D7/02 ,  G08G5/00 ,  G01C23/00 ,  G05D1/02 ,  G05D99/00

CPC classification number: G08G5/0047 ,  G01C23/00 ,  G05D1/0202 ,  G05D1/0607 ,  G08G5/0021

Abstract: A method and device for determining a control set point of an aircraft, an associated computer program and an aircraft are disclosed. In one aspect, the method includes calculating a performance scale in the form of slope values of the aircraft, the performance scale including a slope characteristic value, the slope characteristic value being associated with a corresponding performance characteristic value. The method also includes acquiring a guidance set point and displaying the acquired guidance set point, in the form of a slope value with respect to the performance scale. The method further includes determining a slope characteristic value associated with a guidance set point displayed in the form of a slope value, and calculating an aircraft control set point, the control set point being calculated relative to the performance characteristic value corresponding to the determined slope characteristic value.

Abstract translation: 公开了一种用于确定飞行器，相关联的计算机程序和飞机的控制设定点的方法和装置。 一方面，该方法包括以飞机的斜率值的形式计算性能量表，该性能量表包括斜率特征值，斜率特征值与相应的性能特征值相关联。 该方法还包括以相对于性能量表的斜率值的形式获取引导设定点并显示所获取的引导设定点。 该方法还包括确定与以斜率值形式显示的引导设定点相关联的斜率特征值，以及计算飞行器控制设定点，控制设定点是相对于与所确定的斜率特性对应的性能特征值计算的 值。

公开(公告)号：US20150364045A1

公开(公告)日：2015-12-17

申请号：US14737362

申请日：2015-06-11

Applicant: THALES

Inventor： Sylvain LISSAJOUX ,  Bruno Aymeric ,  Thibaut Debard

IPC: G08G5/00

CPC classification number: G08G5/0047 ,  G01C23/00 ,  G05D1/0202 ,  G05D1/0607 ,  G08G5/0021

Abstract: A method and device for determining a control set point of an aircraft, an associated computer program and an aircraft are disclosed. In one aspect, the method includes calculating a performance scale in the form of slope values of the aircraft, the performance scale including a slope characteristic value, the slope characteristic value being associated with a corresponding performance characteristic value. The method also includes acquiring a guidance set point and displaying the acquired guidance set point, in the form of a slope value with respect to the performance scale. The method further includes determining a slope characteristic value associated with a guidance set point displayed in the form of a slope value, and calculating an aircraft control set point, the control set point being calculated relative to the performance characteristic value corresponding to the determined slope characteristic value.

Abstract translation: 公开了一种用于确定飞行器，相关联的计算机程序和飞机的控制设定点的方法和装置。 一方面，该方法包括以飞机的斜率值的形式计算性能量表，该性能量表包括斜率特征值，斜率特征值与相应的性能特征值相关联。 该方法还包括以相对于性能量表的斜率值的形式获取引导设定点并显示所获取的引导设定点。 该方法还包括确定与以斜率值形式显示的引导设定点相关联的斜率特征值，以及计算飞行器控制设定点，控制设定点是相对于与所确定的斜率特性对应的性能特征值计算的 值。

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。