公开(公告)号：US09536432B2

公开(公告)日：2017-01-03

申请号：US12815333

申请日：2010-06-14

Applicant: Eric Laurent ,  Nicolas Marty ,  Laurent Flotte

Inventor： Eric Laurent ,  Nicolas Marty ,  Laurent Flotte

IPC: G08G5/04 ,  G08G5/00 ,  G05D1/00 ,  G05F7/00 ,  G01W1/10 ,  G08B23/00 ,  G01C23/00 ,  G01C21/00

CPC classification number: G08G5/0021 ,  G08G5/0086 ,  G08G5/045

Abstract: A method of displaying, for a system for anti-collision monitoring of an aircraft, the limits of flight margins in relation to obstructions located in a flight zone, and a device for displaying the limits of operational flight margins and the limits of alert zones, is provided. The operational flight margins in the flight zones not initially envisaged, and the limits of the alert zones around the trajectory of the aircraft, are presented.

Abstract translation: 一种用于对于飞机的防碰撞监控系统显示与位于飞行区域中的障碍物相关的飞行边界限制的方法，以及用于显示操作飞行边界限制和警报区域限制的装置， 被提供。 最初设想的飞行区域的作战飞行距离，以及飞机轨迹周围的警戒区域的限制。

公开(公告)号：US20100318295A1

公开(公告)日：2010-12-16

申请号：US12815333

申请日：2010-06-14

Applicant: Laurent Flotte ,  Nicolas Marty ,  Eric Laurent

Inventor： Laurent Flotte ,  Nicolas Marty ,  Eric Laurent

IPC: G08G5/04 ,  G08B23/00

CPC classification number: G08G5/0021 ,  G08G5/0086 ,  G08G5/045

Abstract: A method of displaying, for a system for anti-collision monitoring of an aircraft, the limits of flight margins in relation to obstructions located in a flight zone, and a device for displaying the limits of operational flight margins and the limits of alert zones, is provided. The operational flight margins in the flight zones not initially envisaged, and the limits of the alert zones around the trajectory of the aircraft, are presented.

Abstract translation: 一种用于对于飞机的防碰撞监控系统显示与位于飞行区域中的障碍物相关的飞行边界限制的方法，以及用于显示操作飞行边界限制和警报区域限制的装置， 被提供。 最初设想的飞行区域的作战飞行距离，以及飞机轨迹周围的警戒区域的限制。

公开(公告)号：US08249799B2

公开(公告)日：2012-08-21

申请号：US12479957

申请日：2009-06-08

Applicant: Laurent Flotte ,  Nicolas Marty ,  Fabien Vittoz

Inventor： Laurent Flotte ,  Nicolas Marty ,  Fabien Vittoz

IPC: G06G7/78

CPC classification number: G08G5/045 ,  G08G5/0021

Abstract: The invention relates to a method of presenting zones at risk for an aircraft comprising a system of databases, a processor, an anticollision device and a viewing device, wherein to display on the viewing device the zones at risk in relation to the obstacles, the processor carries out the steps of: acquiring obstacle data, the data corresponding to obstacles situated in the aircraft's close displacement zone; calculating the risk of collision with each of the obstacles of the displacement zone; calculating the limits of the zones at risk of collision in the close displacement zone, these limits representing the positions from which the anticollision device might possibly produce collision alerts in relation to the obstacles if the aircraft were to steer towards the obstacle while maintaining the instantaneous flight parameters; and displaying the limits of zones at risk.

Abstract translation: 本发明涉及一种呈现处于危险中的飞机区域的方法，包括数据库系统，处理器，防撞设备和观察设备，其中在观察设备上显示与障碍物相关的危险区域，处理器 执行以下步骤：获取障碍物数据，对应于位于飞机紧邻位移区的障碍物的数据; 计算与位移区的每个障碍物碰撞的风险; 计算在紧密位移区域有碰撞风险的区域的极限，这些极限值代表防撞装置如果飞机在保持瞬时飞行的同时转向障碍物时可能产生碰撞警报的位置 参数; 并显示有风险的区域的限制。

公开(公告)号：US20100106419A1

公开(公告)日：2010-04-29

申请号：US12479957

申请日：2009-06-08

Applicant: Laurent Flotte ,  Nicolas Marty ,  Fabien Vittoz

Inventor： Laurent Flotte ,  Nicolas Marty ,  Fabien Vittoz

IPC: G06F17/00 ,  G06F19/00 ,  G01C21/00

CPC classification number: G08G5/045 ,  G08G5/0021

Abstract: The invention relates to a method of presenting zones at risk for an aircraft comprising a system of databases, a processor, an anticollision device and a viewing device, wherein to display on the viewing device the zones at risk in relation to the obstacles, the processor carries out the steps of: acquiring obstacle data, the data corresponding to obstacles situated in the aircraft's close displacement zone; calculating the risk of collision with each of the obstacles of the displacement zone; calculating the limits of the zones at risk of collision in the close displacement zone, these limits representing the positions from which the anticollision device might possibly produce collision alerts in relation to the obstacles if the aircraft were to steer towards the obstacle while maintaining the instantaneous flight parameters; and displaying the limits of zones at risk.

Abstract translation: 本发明涉及一种呈现处于危险中的飞机区域的方法，包括数据库系统，处理器，防撞设备和观察设备，其中在观察设备上显示与障碍物相关的危险区域，处理器 执行以下步骤：获取障碍物数据，对应于位于飞机紧邻位移区的障碍物的数据; 计算与位移区的每个障碍物碰撞的风险; 计算在紧密位移区域有碰撞风险的区域的极限，这些极限值代表防撞装置如果飞机在保持瞬时飞行的同时转向障碍物时可能产生碰撞警报的位置 参数; 并显示有风险的区域的限制。

公开(公告)号：US08576093B2

公开(公告)日：2013-11-05

申请号：US12870663

申请日：2010-08-27

Applicant: Laurent Flotte ,  Gabrielle DeBrito ,  Christian Nouvel ,  Nicolas Marty

Inventor： Laurent Flotte ,  Gabrielle DeBrito ,  Christian Nouvel ,  Nicolas Marty

IPC: G08G5/04

CPC classification number: G01C23/00 ,  G08G5/0021 ,  G08G5/0086 ,  G08G5/045

Abstract: The invention relates to an aircraft navigational aid system with 3D display including an anti-collision device, with means of storing data representing obstructions, means for calculating a representation of the obstructions in a three-dimensional space and a device for displaying the obstructions data in three dimensions. The system includes means for augmenting the display of the representation of the area of hazardous obstructions with at least two indicator objects for the said area of hazardous obstructions disposed together in such a manner as to form a third object targeting the localization of the point in the area of hazardous obstructions closest to the aircraft. The invention also relates to the method of display of the indicator objects in a three-dimensional display.

Abstract translation: 本发明涉及一种具有3D显示器的飞行器导航辅助系统，其包括防冲突装置，具有存储表示障碍物的数据的装置，用于计算三维空间中的障碍物的表示的装置和用于显示障碍物数据的装置 三维。 该系统包括用于增加危险障碍物区域的表示的显示的装置，其中至少两个用于所述危险障碍物区域的指示物体一起放置在一起，以便形成针对该点在 最接近飞机的危险障碍物区域。 本发明还涉及在三维显示器中显示指示物体的方法。

公开(公告)号：US08145365B2

公开(公告)日：2012-03-27

申请号：US12487919

申请日：2009-06-19

Applicant: Laurent Flotte ,  Nicolas Marty ,  Aurélie Sallier

Inventor： Laurent Flotte ,  Nicolas Marty ,  Aurélie Sallier

IPC: G05D1/00

CPC classification number: G05D1/0646

Abstract: The invention relates to a calculation method for an aircraft navigation aid system making it possible to maintain a vertical safety margin with an obstruction profile, the aircraft comprising a navigation system, an automatic piloting system, a database system and a display device, characterized in that the method comprises the following steps: calculation of an obstruction altitude profile, calculation of a vertical safety margin with respect to the obstruction profile, of a plurality of vertical safety trajectories and of the respective flight setpoints for the aircraft to execute the trajectories, selection of the flight setpoints making it possible to maintain the aircraft as close as possible to the obstruction profile while maintaining between the aircraft and the obstruction profile at least the vertical safety margin, filtering of the flight set point values so that the variation of the values of the setpoints does not exceed a variation difference in a duration predefined in the system.

Abstract translation: 本发明涉及一种用于航空器导航辅助系统的计算方法，使得可以保持具有障碍物轮廓的垂直安全裕度，飞行器包括导航系统，自动驾驶系统，数据库系统和显示装置，其特征在于： 该方法包括以下步骤：计算障碍物高度剖面，计算多个垂直安全轨迹中相对于障碍物轮廓的垂直安全边界以及飞行器执行轨迹的相应飞行设定点，选择 飞行设定点使得有可能使飞机尽可能靠近障碍物轮廓，同时在至少垂直安全裕度之间保持飞机和障碍物轮廓之间，同时过滤飞行设定点值，使得飞行设置点值的变化 设定值不超过预定义的持续时间的变化差异 系统。

公开(公告)号：US20110210871A1

公开(公告)日：2011-09-01

申请号：US12870663

申请日：2010-08-27

Applicant: Laurent Flotte ,  Gabrielle De Brito ,  Christian Nouvel ,  Nicolas Marty

Inventor： Laurent Flotte ,  Gabrielle De Brito ,  Christian Nouvel ,  Nicolas Marty

IPC: G08G5/04

CPC classification number: G01C23/00 ,  G08G5/0021 ,  G08G5/0086 ,  G08G5/045

Abstract: The invention relates to an aircraft navigational aid system with 3D display including an anti-collision device, with means of storing data representing obstructions, means for calculating a representation of the obstructions in a three-dimensional space and a device for displaying the obstructions data in three dimensions. The system includes means for augmenting the display of the representation of the area of hazardous obstructions with at least two indicator objects for the said area of hazardous obstructions disposed together in such a manner as to form a third object targeting the localization of the point in the area of hazardous obstructions closest to the aircraft. The invention also relates to the method of display of the indicator objects in a three-dimensional display.

Abstract translation: 本发明涉及一种具有3D显示器的飞行器导航辅助系统，其包括防冲突装置，具有存储表示障碍物的数据的装置，用于计算三维空间中的障碍物的表示的装置和用于显示障碍物数据的装置 三维。 该系统包括用于增加危险障碍物区域的表示的显示的装置，其中至少两个用于所述危险障碍物区域的指示物体一起放置在一起，以便形成针对该点在 最接近飞机的危险障碍物区域。 本发明还涉及在三维显示器中显示指示物体的方法。

公开(公告)号：US09047764B2

公开(公告)日：2015-06-02

申请号：US12900747

申请日：2010-10-08

Applicant: Stéphane Fleury ,  Laurent Flotte ,  Nicolas Marty ,  Erick Rakotoarisoa

Inventor： Stéphane Fleury ,  Laurent Flotte ,  Nicolas Marty ,  Erick Rakotoarisoa

IPC: G08B23/00 ,  G01C5/00 ,  G05D1/00 ,  G08G5/00

CPC classification number: G08G5/0086 ,  G08G5/0052

Abstract: The invention relates to a method of alert calculation for an aircraft obstruction proximity warning system including a step for detecting a hazardous flight situation capable of triggering an alert as a function of a data signal representing the change in height below the aircraft, including, prior to the step of detection, a step for converting the data signal representing the change in height as a function of information representative of the vertical profile of the obstructions below the aircraft.

Abstract translation: 本发明涉及一种用于飞机障碍物接近警报系统的警报计算方法，该系统包括用于检测能够触发警报的危险飞行状况的步骤，该危险飞行情况是表示飞机下方的高度变化的数据信号的函数，包括： 检测步骤，用于将表示高度变化的数据信号变换为表示飞机下方的障碍物的垂直剖面的信息的函数的步骤。

公开(公告)号：US08498755B2

公开(公告)日：2013-07-30

申请号：US12973763

申请日：2010-12-20

Applicant: Gabrielle De Brito ,  Laurent Flotte ,  Gilles Francois ,  Fabien Guilley ,  Nicolas Marty

Inventor： Gabrielle De Brito ,  Laurent Flotte ,  Gilles Francois ,  Fabien Guilley ,  Nicolas Marty

IPC: G05D1/00

CPC classification number: G05D1/0055

Abstract: A device for the coherent management of data deriving from different surveillance systems of an aircraft includes: a flight management system, the function of which is to assist the crew in following a flight plan of the aircraft and an associated trajectory; a surveillance system, the function of which is to detect any obstacles in proximity to the aircraft; a warning management system, the function of which is to detect abnormal situations and to display for the crew, where appropriate, warnings, such as potentially critical alarms or non-critical alerts, and the associated procedures to be followed when such exist; in which said flight management system, said surveillance system and said warning management system are interconnected and cooperate so that at least the warning management system has access to the flight plan of the aircraft, and is configured to display for the crew a summary of the situation when the surveillance system detects an obstacle that the aircraft should avoid according to the flight plan, and to not display, consequently, unnecessary warnings.

Abstract translation: 用于对来自飞行器的不同监视系统的数据进行连贯管理的装置包括：飞行管理系统，其功能是协助船员遵循飞行器的飞行计划和相关轨迹; 监视系统，其功能是检测飞机附近的任何障碍物; 一种警告管理系统，其功能是检测异常情况，并在适当情况下向船员显示警告，如潜在的关键警报或非关键警报，以及当存在时要遵循的相关程序; 所述飞行管理系统，所述监视系统和所述警告管理系统相互联系并配合，使得至少所述警告管理系统可以访问所述飞行器的飞行计划，并且被配置为向船员显示情况​​的概要 当监视系统根据飞行计划检测到飞机应避免的障碍物，并且不显示时，因此不必要的警告。

公开(公告)号：US20120215436A1

公开(公告)日：2012-08-23

申请号：US12478367

申请日：2009-06-04

Applicant: Laurent Flotte ,  Nicolas Marty ,  Pascal Gayraud

Inventor： Laurent Flotte ,  Nicolas Marty ,  Pascal Gayraud

IPC: G08G5/04

CPC classification number: G01S13/94 ,  G01S7/22 ,  G01S7/24 ,  G01S7/41 ,  G01S13/87

Abstract: The invention relates to a device for monitoring obstructions for an aircraft including data storage, an anticollision device and viewing devices, wherein the monitoring device comprises a detector to detect in real-time obstructions, of terrain type and of human constructions type, in a close environment of the aircraft in a flight situation, a sensor to identify the obstructions at risk calculating identification parameters, a circuit to calculate criticality of the obstructions, a display to display both the obstructions with the identification and criticality parameters of the obstructions, and a generator of alerts to describe the situation according to a combination of the identification and criticality parameters. One or more embodiments of the invention is a monitoring system adapted for zones close to the aircraft and in the flight zones not visible to the crew. One or more embodiments of the invention applies particularly to helicopters executing low-altitude flights. It relates more particularly to military carriers such as rescue carriers.

Abstract translation: 本发明涉及一种用于监视飞机的障碍物的装置，包括数据存储装置，防撞装置和观察装置，其中监视装置包括一个检测器，用于实时检测地形类型和人类结构类型的实时障碍物 航空器在飞行情况下的环境，传感器识别风险计算识别参数的障碍物，计算障碍物临界值的电路，显示障碍物与障碍物的识别和临界参数的显示器，以及发生器 的警报，以根据识别和临界参数的组合来描述情况。 本发明的一个或多个实施例是适用于靠近飞行器的区域和飞行区域中对于机组人员不可见的监视系统。 本发明的一个或多个实施例特别适用于执行低空飞行的直升机。 它更具体地涉及诸如救援载体的军事载体。