公开(公告)号：US20140327699A1

公开(公告)日：2014-11-06

申请号：US14269504

申请日：2014-05-05

Applicant: DASSAULT AVIATION

Inventor： Sebastien DUPONT DE DINECHIN ,  Fabrice Vallete

IPC: B64D45/00 ,  G06T13/00 ,  G06T19/00

CPC classification number: B64D45/00 ,  G01C23/00 ,  G06F3/147 ,  G06T13/00 ,  G06T19/006 ,  G09G5/14 ,  G09G2340/12 ,  G09G2340/125 ,  G09G2354/00 ,  G09G2358/00 ,  G09G2380/12

Abstract: A device is provided for assisting in the piloting of a vehicle, in particular an aircraft. The device includes a surface displaying images and a display management unit for images designed to be displayed on the display surface superimposed on a view of the outside landscape. The management unit is capable of commanding the display of piloting information images on the display surface. The management unit is capable of commanding the display, for at least one of the piloting information images, of an animation intended to attract a user's attention to that piloting information image, the animation comprising the display of an alert image and the shrinkage of the alert image.

Abstract translation: 提供了一种用于辅助驾驶车辆，特别是飞机的装置。 该装置包括显示图像的表面和用于被设计为显示在叠加在外部景观的显示表面上的图像的显示管理单元。 管理单元能够命令在显示面上显示引导信息图像。 管理单元能够命令用于至少一个驾驶信息图像的旨在吸引用户注意该导航信息图像的动画，该动画包括警报图像的显示和警报的收缩 图片。

公开(公告)号：US20150052994A1

公开(公告)日：2015-02-26

申请号：US14388775

申请日：2013-03-26

Applicant: DASSAULT AVIATION

Inventor： Sebastien DUPONT DE DINECHIN

IPC: G01P13/02

CPC classification number: G01P13/025 ,  B64F5/60 ,  G01P21/025

Abstract: A method for determining a state of credibility of measurements of an incidence sensor of an aircraft is provided. This method includes at least one coherence test between incidence measurements from said incidence sensor, and the measurements of a flight characteristic of the aircraft, distinct from the incidence. The coherence test includes determining an incidence value from said incidence sensor, determining said flight characteristic of the aircraft, determining a value of at least one indicator of the coherence of the incidence value with the value of said flight characteristic, and activating a low state of credibility, in which the measurements of said incidence sensor are deemed unreliable, or an intermediate state of credibility, in which the measurements from said incidence sensor are deemed coherent with said flight characteristic, based on the value of said coherence indicator.

Abstract translation: 提供了一种用于确定飞行器的入射传感器的测量的可信度状态的方法。 该方法包括来自所述入射传感器的入射测量值与飞行器的飞行特征的测量值之间的至少一个相干性测试，与入射不同。 相干测试包括确定来自所述入射传感器的入射值，确定飞行器的飞行特性，确定入射值的一致性的至少一个指示符与所述飞行特性的值的值，以及激活低 基于所述相干指示器的值，将所述入射传感器的测量值视为不可靠的可信度或可信度的中间状态，其中来自所述入射传感器的测量值与所述飞行特性相一致。