公开(公告)号：US20100060730A1

公开(公告)日：2010-03-11

申请号：US12540605

申请日：2009-08-13

Applicant: Sandra POUSSIN ,  David Bideau ,  Laurent Coloma ,  Stephane Gauthier

Inventor： Sandra POUSSIN ,  David Bideau ,  Laurent Coloma ,  Stephane Gauthier

IPC: H04N7/18

CPC classification number: G02B27/01 ,  G02B2027/014

Abstract: The invention relates to a method for adjustment of a harmonization compensation applied to alleviate a discrepancy of conformity between a video image transmitted by a video transducer (1) and projected by a head-up display device (5, 6), of an aircraft, and an external scene ahead of the aircraft. At least one equipment item of the aircraft—preferably the said HUD device—equipped with at least one control element accessible in the cockpit, is programmed to be able to function according to a nominal mode and according to a maintenance mode, in which at least one of its control elements, known as a redirected control element, is used to define the applied harmonization compensation. An operator activates the maintenance mode and starts an adjustment operation, in which he modifies in real time the applied harmonization compensation, by manipulating at least one redirected control element, until the video image is matched with the external scene.

Abstract translation: 本发明涉及一种用于调整用于减轻由视频传感器（1）传输的视频图像并由飞机的平视显示设备（5,6）投影的视频图像之间的一致性差异）的调谐补偿的方法， 和飞机前的外部场景。 飞机的至少一个设备项目 - 优选地，所述HUD设备 - 配备有在驾驶舱中可访问的至少一个控制元件被编程为能够根据标称模式并且根据维护模式来运行，其中至少 被称为重定向控制元件的控制元件之一被用于定义所应用的协调补偿。 操作员激活维护模式并开始调整操作，其中他通过操纵至少一个重定向的控制元件实时修改应用的协调补偿，直到视频图像与外部场景匹配。

公开(公告)号：US08537214B2

公开(公告)日：2013-09-17

申请号：US12540605

申请日：2009-08-13

Applicant: Sandra Poussin ,  David Bideau ,  Laurent Coloma ,  Stephane Gauthier

Inventor： Sandra Poussin ,  David Bideau ,  Laurent Coloma ,  Stephane Gauthier

IPC: H04N7/00

CPC classification number: G02B27/01 ,  G02B2027/014

Abstract: The invention relates to a method for adjustment of a harmonization compensation applied to alleviate a discrepancy of conformity between a video image transmitted by a video transducer (1) and projected by a head-up display device (5, 6), of an aircraft, and an external scene ahead of the aircraft. At least one equipment item of the aircraft—preferably the said HUD device—equipped with at least one control element accessible in the cockpit, is programmed to be able to function according to a nominal mode and according to a maintenance mode, in which at least one of its control elements, known as a redirected control element, is used to define the applied harmonization compensation. An operator activates the maintenance mode and starts an adjustment operation, in which he modifies in real time the applied harmonization compensation, by manipulating at least one redirected control element, until the video image is matched with the external scene.

Abstract translation: 本发明涉及一种用于调整用于减轻由视频传感器（1）传输的视频图像并由飞机的平视显示设备（5,6）投影的视频图像之间的一致性差异）的调谐补偿的方法， 和飞机前的外部场景。 飞机的至少一个设备项目 - 优选地，所述HUD设备 - 配备有在驾驶舱中可访问的至少一个控制元件被编程为能够根据标称模式并且根据维护模式来运行，其中至少 被称为重定向控制元件的控制元件之一被用于定义所应用的协调补偿。 操作员激活维护模式并开始调整操作，其中他通过操纵至少一个重定向的控制元件实时修改应用的协调补偿，直到视频图像与外部场景匹配。

公开(公告)号：US08416151B2

公开(公告)日：2013-04-09

申请号：US12706352

申请日：2010-02-16

Applicant: Sandra Poussin ,  David Bideau ,  Laurent Coloma ,  Stephane Gauthier

Inventor： Sandra Poussin ,  David Bideau ,  Laurent Coloma ,  Stephane Gauthier

IPC: G09G5/00 ,  G06K9/40 ,  G06K9/36

CPC classification number: G02B27/01 ,  G02B2027/0138 ,  G02B2027/014

Abstract: A set of equipment items for an aircraft including a video transducer and at least two head-up display devices, wherein the video transducer and/or each HUD device is/are capable of defining the image to be projected by the HUD device on the basis of the display field of the HUD device and of one or more HUD/transducer errors, each HUD/transducer error being defined as being the difference between the HUD error of the corresponding HUD support around a direction and the transducer error around this same direction, the HUD error of an HUD support around a direction being the angular difference around this direction between the line of sight of the HUD support and a measuring reference line, and the transducer error around a direction being the angular difference around this direction between the line of sight of the transducer support and a measuring reference line.

Abstract translation: 一种用于包括视频传感器和至少两个平视显示设备的飞行器的设备项目，其中视频换能器和/或每个HUD设备能够基于HUD设备来定义要投影的图像 的HUD设备的显示区域和一个或多个HUD /换能器错误，每个HUD /换能器误差被定义为相对于方向的相应HUD支持的HUD误差与围绕该相同方向的换能器误差之间的差异， HUD支持的HUD误差是围绕该方向在HUD支撑的视线与测量参考线之间的角度差的方向，以及围绕该方向的换能器误差，该方向是该方向之间的角度差 传感器支架的视线和测量参考线。

公开(公告)号：US20100265162A1

公开(公告)日：2010-10-21

申请号：US12706352

申请日：2010-02-16

Applicant: Sandra Poussin ,  David Bideau ,  Laurent Coloma ,  Stéphane Gauthier

Inventor： Sandra Poussin ,  David Bideau ,  Laurent Coloma ,  Stéphane Gauthier

IPC: G09G5/00

CPC classification number: G02B27/01 ,  G02B2027/0138 ,  G02B2027/014

Abstract: The invention relates to a set of equipment items for an aircraft comprising a video transducer (1) and at least two head-up display devices (2, 3), characterized in that the video transducer (1) and/or each HUD device (2, 3) is/are capable of defining the image to be projected by the said HUD device on the basis of the display field of the said HUD device and of one or more HUD/transducer errors, each HUD/transducer error being defined as being the difference between the HUD error of the corresponding HUD support around a direction and the transducer error around this same direction, the HUD error of an HUD support around a direction being the angular difference around this direction between the line of sight of the said HUD support and a measuring reference line, and the transducer error around a direction being the angular difference around this direction between the line of sight of the transducer support and a measuring reference line.

Abstract translation: 本发明涉及一种用于飞行器的设备项目，其包括视频换能器（1）和至少两个平视显示设备（2,3），其特征在于，视频换能器（1）和/或每个HUD设备 2，3）能够基于所述HUD设备的显示区域和一个或多个HUD /换能器错误来定义由所述HUD设备投影的图像，每个HUD /换能器误差被定义为 作为相对于方向上的对应HUD支持的HUD误差与在该相同方向周围的换能器误差之间的差异，HUD支持的HUD误差围绕该方向在该方向之间的角度差在所述HUD的视线之间 支撑和测量参考线，以及围绕传感器支撑的视线与测量参考线之间的该方向周围的角度差的方向的换能器误差。