公开(公告)号：US08897934B2

公开(公告)日：2014-11-25

申请号：US12268798

申请日：2008-11-11

申请人： Hugues Meunier ,  Nicolas Marty ,  Aurélie Sallier

发明人： Hugues Meunier ,  Nicolas Marty ,  Aurélie Sallier

IPC分类号： G01C5/00 ,  G05D1/00 ,  G05D3/00 ,  G06F7/00 ,  G06F17/00 ,  G01S13/94 ,  G08G5/00 ,  G08G5/02

CPC分类号： G01S13/94 ,  G08G5/0065 ,  G08G5/0086 ,  G08G5/025

摘要： Described is a method of protecting an aircraft in approach by signalling against risks of collision with a terrain in steep-sided environments in order to avoid unwanted warnings emanating from clearance sensors of the on-board TAWS (Terrain Awareness and Warning System) while protecting the aircraft when the aircraft fails to observe a published procedure which includes a landing procedure and a take-off procedure. The method, in some embodiments, includes modifying characteristics of at least one of the clearance sensors according to the position deviation of the aircraft relative to a published RNP (Required Navigation Performance) trajectory.

摘要翻译： 描述的是通过在陡峭的侧面环境中发信号通过与地形碰撞的风险来保护飞行器的方法，以避免在机载TAWS（地形意识和警告系统）的间隙传感器发出的不必要的警告，同时保护 飞机未遵守包括着陆程序和起飞程序在内的已发布程序的飞机。 在一些实施例中，该方法包括根据飞行器相对于所公布的RNP（所需导航性能）轨迹的位置偏差改变至少一个间隙传感器的特性。

公开(公告)号：US08576093B2

公开(公告)日：2013-11-05

申请号：US12870663

申请日：2010-08-27

申请人： Laurent Flotte ,  Gabrielle DeBrito ,  Christian Nouvel ,  Nicolas Marty

发明人： Laurent Flotte ,  Gabrielle DeBrito ,  Christian Nouvel ,  Nicolas Marty

IPC分类号： G08G5/04

CPC分类号： G01C23/00 ,  G08G5/0021 ,  G08G5/0086 ,  G08G5/045

摘要： 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.

摘要翻译： 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：US08515593B2

公开(公告)日：2013-08-20

申请号：US13080372

申请日：2011-04-05

申请人： Nicolas Marty ,  François Coulmeau ,  Xavier Boone

发明人： Nicolas Marty ,  François Coulmeau ,  Xavier Boone

IPC分类号： G05D1/00

CPC分类号： G05D1/0022

摘要： A flight management system of an unmanned aircraft linked to a control station by communication means includes: a first set of a number N of successive navigation functions (iND with i=1, . . . N) remotely situated within the control station, a control function on board the aircraft, generating, from guidance setpoints, commands intended to control the aircraft so that it observes the guidance setpoints, and a second set of a number N of successive navigation functions (iNE, with i=1, . . . , N) on board the aircraft, and configuration means, capable of performing a combination of a number N of successive functions, each of the successive functions being chosen from the first and second sets, said combination of successive functions generating the guidance setpoints transmitted to the onboard control function.

摘要翻译： 通过通信装置链接到控制站的无人飞行器的飞行管理系统包括：远程位于控制站内的N个连续导航功能（iND，i = 1，...）的第一组，控制 在飞行器上的功能，从指导设定点产生用于控制飞机的命令，以使其观察到指导设定点，以及第二组连续导航功能（iNE，i = 1，...， N），以及配置装置，能够执行N个连续功能的组合，每个连续功能是从第一组和第二组中选择的，所述连续功能的组合产生传送给 车载控制功能。

公开(公告)号：US08504224B2

公开(公告)日：2013-08-06

申请号：US12544926

申请日：2009-08-20

申请人： Nicolas Marty ,  Hugues Meunier ,  Philippe Salmon

发明人： Nicolas Marty ,  Hugues Meunier ,  Philippe Salmon

IPC分类号： G06F7/00

CPC分类号： G01C23/00 ,  G01C21/00 ,  G01S13/953 ,  Y02A90/18

摘要： The invention relates to a method and a device for monitoring risky atmospheric areas.The invention relates to an onboard device connected to meteorological measurement systems making it possible to calculate danger detection areas in front of the aircraft in order to detect potential areas of penetration of the aircraft into risky atmospheric areas.The areas of intersection between the detection areas and the risky meteorological areas are calculated according to the trajectory of the aircraft stored in the navigation system.The method makes it possible to generate alerts and force the display of the meteorological situation in front of the aircraft in case of danger.

摘要翻译： 本发明涉及用于监测大气区风险的方法和装置。 本发明涉及一种连接到气象测量系统的车载设备，使得可以计算飞机前方的危险检测区域，以便检测飞机在危险的大气区域中的穿透的潜在区域。 根据导航系统中存储的飞机的轨迹，计算出检测区域与危险气象区域的交点。 该方法使得有可能产生警报并强制在有危险的情况下显示飞机前面的气象情况。

公开(公告)号：US08145365B2

公开(公告)日：2012-03-27

申请号：US12487919

申请日：2009-06-19

申请人： Laurent Flotte ,  Nicolas Marty ,  Aurélie Sallier

发明人： Laurent Flotte ,  Nicolas Marty ,  Aurélie Sallier

IPC分类号： G05D1/00

CPC分类号： G05D1/0646

摘要： 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.

摘要翻译： 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：US08090526B2

公开(公告)日：2012-01-03

申请号：US12094656

申请日：2006-11-11

申请人： Nicolas Marty ,  Gilles Francois ,  Elias Bitar

发明人： Nicolas Marty ,  Gilles Francois ,  Elias Bitar

IPC分类号： G01C21/00 ,  G01C23/00

CPC分类号： G08G5/0034 ,  G01C21/00

摘要： The present invention relates to the definition, in a flight plan, of the horizontal profile of an air route with vertical flight and speed profile prescribed on departure and/or on arrival, by a stringing together of check-points and/or turn points associated with local flight constraints and called “D-Fix” because they are not listed in a published navigation database like those called “Waypoints”. It consists in charting, on curvilinear distance maps, a direct curvilinear path joining the departure point to the destination point of the air route while complying with vertical flight and speed profiles prescribed on departure and/or on arrival and while guaranteeing a circumnavigation of the surrounding reliefs and compliance with regulated overfly zones, then in approximating the series of points of the direct curvilinear path by a sequence of straight segments complying with an arbitrary maximum deviation threshold relative to the points of the series and an arbitrary minimum lateral deviation threshold relative to the set of obstacles to be circumnavigated and in adopting as “D-Fix” points the points of the intermediate intersections of the rectilinear segments.

摘要翻译： 本发明涉及在飞行计划中通过在起飞和/或到达时规定的垂直飞行和速度分布的空中航线的水平轮廓的定义，通过将检查点和/或转向点相关联在一起 具有本地飞行限制，并称为“D-Fix”，因为它们未列在已发布的导航数据库中，如“Waypoint”。 它包括在曲线距离图上的曲线图，将出发点连接到航空路线的目的地点的直接曲线路径，同时遵守在出发和/或抵达时规定的垂直飞行和速度曲线，同时保证周围的环绕 然后通过一系列符合任意最大偏差阈值的直线段相对于该系列点和相对于该系列的任意最小横向偏差阈值逼近直线曲线路径的一系列点， 一系列要循环的障碍，并采用“D-Fix”来表示直线段的中间交点的点。

公开(公告)号：US08073579B2

公开(公告)日：2011-12-06

申请号：US12118129

申请日：2008-05-09

申请人： Nicolas Marty ,  Julia Percier ,  Aurélie Sallier

发明人： Nicolas Marty ,  Julia Percier ,  Aurélie Sallier

IPC分类号： G05D1/04 ,  G06F17/00

CPC分类号： G08G5/0086 ,  G01C5/005 ,  G08G5/0021

摘要： The present invention relates to a method and a device for extracting terrain altitudes notably for a display of a sectional view of a terrain overflown by an aircraft. The device for extracting terrain altitudes along a trajectory of an aircraft in flight includes an interface taking into account selected flight parameters of the aircraft; a terrain altitudes extraction requests manager; a geographical zones manager; a terrain data manager; a terrain profile provider. The disclosed embodiment is configured to be used within the framework of an anticollision device for preventing collision between an aircraft and the terrain.

摘要翻译： 本发明涉及一种用于提取地形高度的方法和装置，特别是用于显示由飞行器溢出的地形的剖视图。 用于沿飞行器的轨迹提取地形高度的装置包括考虑飞行器的选定飞行参数的界面; 地形高度提取要求经理; 地理区域经理; 地形数据管理器; 地形资料提供者。 所公开的实施例被配置为在防冲突装置的框架内使用，以防止飞机和地形之间的碰撞。

公开(公告)号：US20110245997A1

公开(公告)日：2011-10-06

申请号：US13080372

申请日：2011-04-05

申请人： Nicolas Marty ,  Coulmeau François ,  Boone Xavier

发明人： Nicolas Marty ,  Coulmeau François ,  Boone Xavier

IPC分类号： G05D1/00

CPC分类号： G05D1/0022

摘要： A flight management system of an unmanned aircraft linked to a control station by communication means includes: a first set of a number N of successive navigation functions (iND with i=1, . . . N) remotely situated within the control station, a control function on board the aircraft, generating, from guidance setpoints, commands intended to control the aircraft so that it observes the guidance setpoints, and a second set of a number N of successive navigation functions (iNE, with i=1, . . . , N) on board the aircraft, and configuration means, capable of performing a combination of a number N of successive functions, each of the successive functions being chosen from the first and second sets, said combination of successive functions generating the guidance setpoints transmitted to the onboard control function.

摘要翻译： 通过通信装置链接到控制站的无人飞行器的飞行管理系统包括：远程位于控制站内的N个连续导航功能（iND，i = 1，...）的第一组，控制 在飞行器上的功能，从指导设定点产生用于控制飞机的命令，以使其观察到指导设定点，以及第二组连续导航功能（iNE，i = 1，...， N），以及配置装置，能够执行N个连续功能的组合，每个连续功能是从第一组和第二组中选择的，所述连续功能的组合产生传送给 车载控制功能。

公开(公告)号：US07999699B2

公开(公告)日：2011-08-16

申请号：US12134719

申请日：2008-06-06

申请人： Christophe Caillaud ,  Guy Deker ,  Nicolas Marty

发明人： Christophe Caillaud ,  Guy Deker ,  Nicolas Marty

IPC分类号： G08B21/00

CPC分类号： G08G5/065 ,  G01C21/00

摘要： The general field of the invention is that of systems for aiding the guidance of an aircraft on an airport. The system according to the invention comprises means for determining at least one element of the topology of the airport in relation to the position of the aircraft for selecting. Selecting means are provided by the pilot of the aircraft for the element. Generating means are provided to generate at least one guidance or safety set-point using the topological element. Presenting means are provided for the element or the associated set-point on a man-machine interface to the pilot of the aircraft.

摘要翻译： 本发明的一般领域是用于协助飞机在机场上的引导的系统。 根据本发明的系统包括用于相对于飞机的位置来确定机场的拓扑的至少一个元件用于选择的装置。 选择装置由飞行员的飞行员提供。 提供生成装置以使用拓扑元素生成至少一个引导或安全设定点。 在飞机的飞行员的人机接口上为元件或相关联的设定点提供呈现装置。

公开(公告)号：US20110172914A1

公开(公告)日：2011-07-14

申请号：US13004704

申请日：2011-01-11

申请人： François COULMEAU ,  Nicolas MARTY ,  Xavier BLANCHON ,  Pierre GAMET

发明人： François COULMEAU ,  Nicolas MARTY ,  Xavier BLANCHON ,  Pierre GAMET

IPC分类号： G01C21/00

CPC分类号： G08G5/0034

摘要： A method and device checks the conformity of a trajectory calculated by a flight management system of an aircraft in relation to reference data comprising a reference map. The method includes: geo-referencing of a reference map; determination of a reference trajectory from the geo-referenced reference map; detection of nonconformity in the trajectory calculated by the flight management system by comparison of the trajectory calculated by the flight management system with the reference trajectory; and emission of a warning if a nonconformity is detected.

摘要翻译： 一种方法和装置检查由飞行器的飞行管理系统计算的轨迹与包括参考图的参考数据的一致性。 该方法包括：参考地图的地理参考; 从地理参考参考图确定参考轨迹; 通过飞行管理系统计算的轨迹与参考轨迹进行比较，检测飞行管理系统计算出的轨迹中的不符合度; 并且如果检测到不合格，则发出警告。