公开(公告)号：US08897935B2

公开(公告)日：2014-11-25

申请号：US12440513

申请日：2007-08-29

申请人： Hugues Meunier ,  Nicolas Marty ,  Julia Percier

发明人： Hugues Meunier ,  Nicolas Marty ,  Julia Percier

IPC分类号： G06F7/00 ,  G08G5/00 ,  G01C23/00 ,  G05D1/06 ,  G08G5/04

CPC分类号： G01C23/005 ,  G05D1/0607 ,  G05D1/0676 ,  G08G5/0086 ,  G08G5/045

摘要： This disclosure relates to a system for preventing collisions with a terrain. The system includes a detecting means for detecting risks of collision with the terrain after a predetermined forecasting delay. The system further includes a determining means for determining, based on a trajectory followed by the aircraft, a possible limit point for success of the vertical terrain avoidance maneuver. The system further includes indication means for giving indications on azimuth clearance sections, around the direction in which the aircraft is moving, suitable for success of the vertical terrain avoidance maneuver. The system further includes means for estimating a free-travel distance in each azimuth clearance sector on a straight distancing trajectory with constant gradient and over a distance correspond to more than one minute of flight, the free-travel distance being free of potential conflicts with the terrain. The system further includes means for signaling azimuth clearance sections and free-travel distances.

摘要翻译： 本公开涉及一种用于防止与地形碰撞的系统。 该系统包括用于在预定的预测延迟之后检测与地形相撞的风险的检测装置。 该系统还包括确定装置，用于基于飞机跟随的轨迹确定用于垂直地形避免机动的成功的可能的极限点。 系统还包括指示装置，用于在方位角间隙部分周围围绕飞行器移动的方向进行指示，适于垂直地形回避机动的成功。 该系统还包括用于在具有恒定梯度的直线间距轨迹上估计每个方位角间隙扇区中的自由行程距离的装置，并且在距离对应于多于一分钟飞行的距离上，自由行程距离没有与 地形。 该系统还包括用于信号传递方位角间隙部分和自由行进距离的装置。

公开(公告)号：US20100042273A1

公开(公告)日：2010-02-18

申请号：US12440513

申请日：2007-08-29

申请人： Hugues Meunier ,  Nicolas Marty ,  Julia Percier

发明人： Hugues Meunier ,  Nicolas Marty ,  Julia Percier

IPC分类号： G06F7/00

CPC分类号： G01C23/005 ,  G05D1/0607 ,  G05D1/0676 ,  G08G5/0086 ,  G08G5/045

摘要： This system accompanies the alarms of TAWS type and in particular the alarms of “Avoid terrain” type indicating to the pilot that he has passed the limit point of success of a standard vertical avoidance maneuver, indications (32, 33) of free-travel distances in azimuth sectors suited to a clearance maneuver and one or more recommended relief avoidance maneuvers (A, B), both lateral and vertical. For the determination of the limit point, it monitors the penetration of a model of the terrain being flown over into a first protection volume (1) linked to the aircraft and configured in such a way as to model a standard vertical avoidance maneuver trajectory executed without notable delay. For the determination of the azimuth sectors open to a clearance maneuver, it analyzes the penetrations of the model of terrain being flown over in a second protection volume with large azimuth aperture, linked to the aircraft and configured in such a way as to contain the limit point protection volume (1). To evaluate the free-travel distances, it searches for limit points of effectiveness of a standard vertical avoidance maneuver, on arbitrary distancing trajectories in the azimuth sectors open to the clearance maneuvers. Based on the determination of these free-travel distances, the system determines the limit instant of manual initiation by the pilot or automatic initiation of an avoidance trajectory and determines the optimum route alteration to be initiated prior to the avoidance maneuver.

摘要翻译： 该系统伴随TAWS型的报警，特别是“避免地形”类型的报警指示飞行员已经通过标准垂直回避机动的成功的极限，自由行程距离的指示（32,33） 在适合于清除机动的方位角扇区和一个或多个推荐的避免避免机动（A，B），横向和垂直方向。 为了确定极限点，它监测飞越的地形的模型穿透到与飞行器相关联的第一保护体积（1）中，并以这样的方式进行配置，以便模拟在不执行的情况下执行的标准垂直回避机动轨迹 显着延迟 为了确定通向间隙机动的方位角扇区，它分析了在具有大的方位角的第二保护体积中飞行的地形模型的穿透，其连接到飞行器并且被配置为包含极限 点保护量（1）。 为了评估自由行程距离，它搜索标准垂直回避机动的有效性的极限点，对于清除机动的方位角的任意距离轨迹。 基于这些自由行程距离的确定，系统通过飞行员确定手动启动的限制时刻或自动启动回避轨迹，并确定在回避机动之前启动的最佳路线更改。

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：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：US20090138145A1

公开(公告)日：2009-05-28

申请号：US12270305

申请日：2008-11-13

申请人： Hugues Meunier ,  Nicolas Marty ,  Aurelie Sallier

发明人： Hugues Meunier ,  Nicolas Marty ,  Aurelie Sallier

IPC分类号： G05D1/00

CPC分类号： G08G5/0086 ,  G01C23/00 ,  G05D1/0055 ,  G08G5/025

摘要： The present invention relates to a method of protecting an aircraft in approach by signalling against the risks of collision with the terrain in steep-sided environments, in order to avoid unwanted warnings emanating from the clearance sensors of the onboard TAWS system while protecting the aircraft when it fails to observe the published procedure, and this equally in a landing procedure and in a take-off procedure. The method includes conferring an additional function on the conventional TAWS functions, specific to the detection of the potential risks of collision of the aircraft with the terrain when following procedures of reduced protection corridor type, and this without modifying either the logics or the characteristics of the clearance sensor or sensors as currently defined in the TAWSs of the state of the art.

摘要翻译： 本发明涉及通过在陡峭的侧面环境中发信号通知抵抗与地形碰撞的风险的方法来保护飞行器的方法，以避免在机载TAWS系统的间隙传感器发出的不期望的警告，同时保护飞行器时 它没有遵守已发布的程序，同样在着陆程序和起飞程序中也是如此。 该方法包括赋予传统TAWS功能的附加功能，特别是在跟踪减少保护走廊类型的过程时，检测飞机与地形的潜在风险，并且不修改任何逻辑或特性 当前在现有技术的TAWS中定义的间隙传感器或传感器。

公开(公告)号：US20070078592A1

公开(公告)日：2007-04-05

申请号：US11529336

申请日：2006-09-29

申请人： Hugues Meunier ,  Nicolas Marty

发明人： Hugues Meunier ,  Nicolas Marty

IPC分类号： G06F19/00

CPC分类号： G08G5/0082

摘要： A method for evaluating the licitness of the situation of a craft on the surface of an airport including the steps of: modelling of a first licitness cost surface covering a surface of the airport where the craft is deploying, termed the deployment surface, related to this deployment surface and defined by quantities assigned to its points, which quantities are representative of their memberships in flow constraint zones and of the severity in relation to the craft, of the flow constraints, modelling of a second licitness cost surface covering the deployment surface, related to the craft and defined by quantities assigned to its points, which quantities are representative of their memberships in a girth zone covering a neighbourhood of the current position of the craft, and calculation of a score evaluating the significance of the risk of violation of a flow constraint incurred by the craft on the basis of a cross-correlation function of the two licitness cost surfaces referred to one and the same benchmark.

摘要翻译： 一种用于评估机场表面情况的合法性的方法，包括以下步骤：覆盖被称为部署表面的飞机正在部署的机场的表面的第一合法成本面的建模与此有关 部署表面并由分配给其点的数量定义，哪些数量代表其在流动约束区域中的隶属关系以及与工艺有关的严重程度的流动约束，覆盖部署表面的第二个合法成本表面的建模 按照分配给其点的数量定义，哪些数量代表其覆盖工艺当前位置的邻域的围裙的成员身份，以及计算评估违反流程风险的重要性的分数 基于两个合法成本曲面的互相关函数的手段所引起的约束 和同样的基准。

公开(公告)号：US07739047B2

公开(公告)日：2010-06-15

申请号：US11529336

申请日：2006-09-29

申请人： Hugues Meunier ,  Nicolas Marty

发明人： Hugues Meunier ,  Nicolas Marty

IPC分类号： G05D1/02

CPC分类号： G08G5/0082

摘要： A method for evaluating the licitness of the situation of a craft on the surface of an airport including the steps of: modelling of a first licitness cost surface covering a surface of the airport where the craft is deploying, termed the deployment surface, related to this deployment surface and defined by quantities assigned to its points, which quantities are representative of their memberships in flow constraint zones and of the severity in relation to the craft, of the flow constraints, modelling of a second licitness cost surface covering the deployment surface, related to the craft and defined by quantities assigned to its points, which quantities are representative of their memberships in a girth zone covering a neighborhood of the current position of the craft, and calculation of a score evaluating the significance of the risk of violation of a flow constraint incurred by the craft on the basis of a cross-correlation function of the two licitness cost surfaces referred to one and the same benchmark.

摘要翻译： 一种用于评估机场表面情况的合法性的方法，包括以下步骤：覆盖被称为部署表面的飞机正在部署的机场的表面的第一合法成本面的建模与此有关 部署表面并由分配给其点的数量定义，哪些数量代表其在流动约束区域中的隶属关系以及与工艺有关的严重程度的流动约束，覆盖部署表面的第二个合法成本表面的建模 按照分配给其点的数量定义，哪些数量代表其覆盖工艺当前位置的邻域的围裙的成员身份，以及计算评估违反流程风险的重要性的分数 在两个合法成本表面的互相关函数的基础上引发的技术约束一个 提出相同的基准。

公开(公告)号：US20070078591A1

公开(公告)日：2007-04-05

申请号：US11529314

申请日：2006-09-29

申请人： Hugues Meunier ,  Nicolas Marty

发明人： Hugues Meunier ,  Nicolas Marty

IPC分类号： G01C23/00

CPC分类号： G05D1/0274 ,  G05D1/0083 ,  G05D1/0278 ,  G08G5/0082 ,  G08G5/065

摘要： The invention relates to aiding airport navigation by emission of an alert reminding the pilot of a craft moving on the surface of an airport of the circulation constraints encountered locally over his route. The method comprises the following steps: partitioning of the circulation surfaces of the airport into elementary circulation constraint zones each enclosing a set of adjoining points subject to the same local circulation constraints, identifications of the elementary zones and of their specific circulation constraints, detection of the encroachment of the craft into the elementary zones, and upon each encroachment of the craft into an elementary zone, reminder by alert generation, to the commander of the craft, of one at least of the circulation constraints specific to the elementary zone concerned.

摘要翻译： 本发明涉及通过发出警报来帮助机场导航，提醒在机场表面上移动的飞行员的飞行员在其路线上局部遇到的循环约束。 该方法包括以下步骤：将机场的循环表面划分为基本循环约束区，每个区域围绕相同局部循环约束的一组相邻点，基本区域的标识及其特定循环约束的检测 将工艺侵入基本区域，并且每次将工艺侵入基本区域时，通过警报生成提醒工艺的指挥官，至少对有关的基本区域具有特定的循环限制。

公开(公告)号：US08280622B2

公开(公告)日：2012-10-02

申请号：US12092798

申请日：2006-10-31

申请人： Hugues Meunier ,  Nicolas Marty

发明人： Hugues Meunier ,  Nicolas Marty

IPC分类号： G06G7/78

CPC分类号： G01C5/005 ,  G01C21/005 ,  G05D1/101 ,  G08G5/0086 ,  G08G5/045

摘要： A system indicating to a pilot that an aircraft has passed the limit-point of success of a standard vertical avoidance maneuver is disclosed. To determine the limit-point, the system monitors a penetration of a model of the terrain being flown over into a first protection volume linked to the aircraft and configured so as to model a standard vertical avoidance maneuver path executed without delay. To determine disengagement azimuth sectors, the system monitors the penetrations of the model of the terrain being flown over into a second protection volume with large azimuth aperture, linked to the aircraft and configured so as to contain the limit-point protection volume and, for the various azimuths covered, paths of a composite maneuver beginning with change-of-heading maneuvers with which to reach the azimuth concerned and continuing with the standard terrain vertical avoidance maneuver.

摘要翻译： 公开了向飞行员指示飞机已经通过标准垂直回避机动的成功极限的系统。 为了确定极限点，系统监测正在飞行的地形的模型的穿透到与飞行器相关联的第一保护体积并且被配置为对没有延迟地执行的标准垂直回避机动路径进行建模。 为了确定分离方位角扇区，系统监测地面的模型穿透到具有大的方位角孔的第二保护体积，其连接到飞行器并被配置为包含极限点保护体积，并且对于 覆盖的各种方位角，复合机动的路径开始于转向方向的机动，以达到相关方位，并继续进行标准地形垂直回避机动。

公开(公告)号：US08400347B2

公开(公告)日：2013-03-19

申请号：US12542535

申请日：2009-08-17

申请人： Bernard Fabre ,  Nicolas Marty ,  Hugues Meunier

发明人： Bernard Fabre ,  Nicolas Marty ,  Hugues Meunier

IPC分类号： G01S13/93 ,  G01S13/91 ,  G01S13/00

CPC分类号： G08G5/06

摘要： The invention relates to a monitoring device and method allowing surveillance of an aircraft in relation to aircraft and/or craft on an airport displacement zone. The invention is a system comprising a dedicated transmitter and receiver to receive the information regarding the location and displacement of the cooperative aircraft and to monitor the location of the said aircraft in relation to the cooperative aircraft. The monitoring application is based on the detection of conflict zones by inter-correlation of constraint surfaces of the airport zone. The invention applies to aircraft carrying communication moans for ADS-B networks for an airport zone monitoring application.

摘要翻译： 本发明涉及一种监视装置和方法，其允许飞机相对于机场位移区上的飞行器和/或飞行器进行监视。 本发明是一种包括专用发射机和接收机的系统，用于接收关于合作飞机的位置和位移的信息，并且监视所述飞机相对于协作飞机的位置。 监测应用是基于通过机场区域的约束表面的相互关系来检测冲突区域。 本发明适用于携带用于机场区域监视应用的用于ADS-B网络的通信呻吟机的飞行器。