公开(公告)号：US20170291691A1

公开(公告)日：2017-10-12

申请号：US15484616

申请日：2017-04-11

Applicant: DASSAULT AVIATION

Inventor： Jérôme BARRAL ,  Patrick DARSES

IPC: B64C13/18 ,  B64D43/02 ,  G05D1/10

CPC classification number: B64C13/18 ,  B64D43/02 ,  B64D45/00 ,  G01C23/00 ,  G05D1/101 ,  G08G5/003

Abstract: An assistance method for assisting flying of an aircraft with restriction of possibilities of adjusting the flying parameters depending on the context, and corresponding device are provided. The assistance method for assisting flying of an aircraft includes the steps of: configuring at least one flying mode, the configuration comprising selecting a flying mode selected from among an available flying mode and entering at least one flying setpoint associated with the selected flying mode, presenting the or each configured flying mode, engaging at least one configured flying mode, and flying of the aircraft by an automatic pilot system of the aircraft based on the flying setpoint of the or each engaged flying mode. The method also includes a step for collecting at least one avionics parameter representative of a flying context, and a step for restricting configuration possibilities of the flying modes based on the or each collected avionics parameter.

公开(公告)号：US20190352008A1

公开(公告)日：2019-11-21

申请号：US16413768

申请日：2019-05-16

Applicant: DASSAULT AVIATION

Inventor： François-Xavier D'ARBONNEAU ,  Patrick DARSES ,  Bruno FERRY ,  François SALMON-LEGAGNEUR ,  Jean-Christophe DENJEAN

IPC: B64D11/00

Abstract: A device for waking up a crew member resting on an aircraft includes a processing unit configured to detect current development parameters of the aircraft and/or to detect a state of consciousness of at least one other active crewmember. The processing unit is also configured to activate an apparatus for waking up the resting crew member, when at least one predetermined condition for waking up the resting crew member on one or several current parameters of the aircraft and/or on a parameter representative of the state of consciousness of the at least one other active crew member is satisfied.

公开(公告)号：US20160343261A1

公开(公告)日：2016-11-24

申请号：US15158807

申请日：2016-05-19

Applicant: DASSAULT AVIATION

Inventor： Arnaud BRANTHOMME ,  Igor FAIN ,  Patrick DARSES

IPC: G08G5/00 ,  G09G5/377 ,  B64D43/00 ,  G06T15/20

CPC classification number: G08G5/0086 ,  B64D43/00 ,  G01C23/00 ,  G06T15/20 ,  G08G5/0047 ,  G08G5/0078 ,  G08G5/0091 ,  G09G5/377 ,  G09G2340/04 ,  G09G2354/00 ,  G09G2380/12

Abstract: A system for displaying information related to a flight of an aircraft and an associated method are provided. The display system comprises a display device, a man-machine interface, a module for dynamically generating synthesis images, each comprising a synthetic depiction of the environment and a curve representative of a trajectory, said module being configured to generate a first synthesis image centered around a first central point of interest, to command the display thereof, and to detect an action to modify the central point of interest by an operator via said man-machine interface. The generating module is also configured to determine, as a function of said modification action, a second central point of interest, situated along said curve whatever said modification action is, to generate a second synthesis image centered around said second central point of interest, and to command the display thereof.

Abstract translation: 提供了一种用于显示与飞机的飞行有关的信息的系统和相关的方法。 显示系统包括显示装置，人机接口，用于动态产生合成图像的模块，每个模块包括对环境的合成描述和表示轨迹的曲线，所述模块被配置为产生以中心为中心的第一合成图像 第一中心点，用于指示其显示，并且通过所述人机界面检测操作者修改所述中心点的动作。 生成模块还被配置为根据所述修改动作来确定不管所述修改动作是沿着所述曲线定位的第二中心点，以产生以所述第二中心点为中心的第二合成图像，以及 命令其显示。

公开(公告)号：US20160343260A1

公开(公告)日：2016-11-24

申请号：US15158802

申请日：2016-05-19

Applicant: DASSAULT AVIATION

Inventor： Arnaud BRANTHOMME ,  Igor FAIN ,  Patrick DARSES

IPC: G08G5/00 ,  G09G5/377 ,  B64D43/00 ,  G06T15/20

CPC classification number: G08G5/0086 ,  B64D43/00 ,  G01C23/00 ,  G06T15/205 ,  G08G5/0047 ,  G08G5/0078 ,  G08G5/0091 ,  G09G5/377 ,  G09G2340/04 ,  G09G2380/12

Abstract: A system for displaying information related to a flight of an aircraft and an associated method are provided. The display system comprises a dynamic synthesis image generating module, configured to generate at least two successive transition synthesis images between an image according to a first type of perspective and an image according to a second type of perspective, or between an image according to a second type of perspective and an image according to a first type of perspective, respectively, and to command the display thereof at successive transition moments. Each transition image is centered around an intermediate central point of interest, seen from an intermediate point of view situated at an intermediate observation distance from the intermediate central point of interest, which is an increasing function, a decreasing function, respectively, of the transition moment at which the image is displayed, and seen from an intermediate opening angle, which is a decreasing function, an increasing function, respectively, of the transition moment at which this image is displayed.

Abstract translation: 提供了一种用于显示与飞机的飞行有关的信息的系统和相关的方法。 显示系统包括动态合成图像生成模块，其被配置为根据第一类型的透视图像和根据第二类型的图像的图像之间或在根据第二类型的图像之间的图像之间或在根据第二类型的图像之间产生至少两个连续的过渡合成图像 分别根据第一类型的透视图和透视图的类型，并且在连续的过渡时刻命令其显示。 每个转换图像围绕中间的中心点居中，从位于距离中间中心点的中间观察距离的中间视点看，该中间观察距离分别是递增函数，递减函数，递减函数 在该图像显示时，从作为递减函数的中间开放角度看，分别显示该图像的过渡时刻的递增函数。