公开(公告)号：US08436750B2

公开(公告)日：2013-05-07

申请号：US12557366

申请日：2009-09-10

申请人： Bernard Fabre ,  Pascal Gayraud ,  Nicolas Marty

发明人： Bernard Fabre ,  Pascal Gayraud ,  Nicolas Marty

IPC分类号： G05B5/00

CPC分类号： G08G5/02 ,  G08G5/0086 ,  G08G5/0091

摘要： The invention is a method making it possible to calculate and monitor the provisional landing distance and the configuration of the aircraft and flight parameters during the changes in the landing phase manoeuvre. The method consists in determining the landing runway then in analyzing the configuration and the dynamic parameters of the aeroplane, the meteorological and airport data in order to assess, from a performance database, whether the planned braking is suitable and will stop the aeroplane before the end of the runway.

摘要翻译： 本发明是一种在着陆阶段机动的变化期间可以计算和监视临时着陆距离以及飞行器的构型和飞行参数的方法。 该方法在于确定着陆跑道，然后分析飞机的配置和动态参数，气象和机场数据，以便从性能数据库中评估计划制动是否合适，并在结束前停止飞机 的跑道。

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：US20120215436A1

公开(公告)日：2012-08-23

申请号：US12478367

申请日：2009-06-04

申请人： Laurent Flotte ,  Nicolas Marty ,  Pascal Gayraud

发明人： Laurent Flotte ,  Nicolas Marty ,  Pascal Gayraud

IPC分类号： G08G5/04

CPC分类号： G01S13/94 ,  G01S7/22 ,  G01S7/24 ,  G01S7/41 ,  G01S13/87

摘要： 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.

摘要翻译： 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。

公开(公告)号：US08190310B2

公开(公告)日：2012-05-29

申请号：US12366667

申请日：2009-02-06

申请人： François Coulmeau ,  Nicolas Marty ,  Alain Cordonnier

发明人： François Coulmeau ,  Nicolas Marty ,  Alain Cordonnier

IPC分类号： G06G7/70

CPC分类号： G08G5/0065 ,  G01S19/14 ,  G01S19/15 ,  G01S19/48 ,  G08G5/025 ,  G08G5/065

摘要： The present invention relates to the field of methods and systems for optimizing the locating of an aircraft in airports and, more particularly, in the take-off and landing phases, and notably in the air-ground and ground-air transition phases. The method of optimizing the locating of an aircraft during the take-off or landing phase comprising a transition step (21), the latter being defined between two events (A0, AS), the first event being a condition of contact between the aircraft and the runway and the second event being a threshold condition defining a stabilized flight phase, is wherein the transition step (21) comprises the determination of at least one “transition position” of the aircraft by a weighting between the “ground position” (LOC_SOL) determined by the ground locating system and the “flight position” (LOV_VOL) determined by the in-flight locating system.

摘要翻译： 本发明涉及用于优化飞机在机场中的定位的方法和系统领域，更具体地涉及起飞和着陆阶段，特别是在空地和地空过渡阶段。 在起飞或着陆阶段期间优化飞行器定位的方法包括过渡步骤（21），后者在两个事件（A0，AS）之间定义，第一个事件是飞行器和 跑道和第二事件是限定稳定飞行阶段的阈值条件，其中转换步骤（21）包括通过“地面位置”（LOC_SOL）之间的加权来确定飞行器的至少一个“转换位置” 由地面定位系统确定，并由飞行定位系统确定的“飞行位置”（LOV_VOL）。

公开(公告)号：US08121746B2

公开(公告)日：2012-02-21

申请号：US11689460

申请日：2007-03-21

申请人： Gilles François ,  Nicolas Marty ,  Frédéric Thomas

发明人： Gilles François ,  Nicolas Marty ,  Frédéric Thomas

IPC分类号： G05D1/08

CPC分类号： G08G5/0086 ,  G01C5/005 ,  G01C21/00 ,  G08G5/045

摘要： The present invention relates to a method and a device for monitoring the minimum flying altitude of an aircraft. The method comprises a phase for calculating a vertical flight profile describing the changing altitude of the aircraft during an arbitrary period taking into account its instantaneous speed and its instantaneous angle of climb or descent; a phase for calculating a minimum vertical flight profile describing the changing minimum flying altitude over the future route of the aircraft during the period taking into account its instantaneous heading and its instantaneous speed, the minimum altitude values being determined for a coverage of the route of the aircraft during the period by disks centered on points on the route using requests to a database containing airspace zones corresponding to a minimum flying altitude, each request returning the zones intersected by a disk, the minimum altitude retained in a disk being the maximum value of the minimum altitudes for each type of zone returned; and a phase for generating a warning message based on the relative position of the vertical flight profile compared with the minimum vertical flight profile.

摘要翻译： 本发明涉及一种用于监视飞行器的最低飞行高度的方法和装置。 该方法包括一个阶段，用于计算描述飞机在任意时段内随着其瞬时速度及其瞬时爬升或下降角度而改变飞行高度的垂直飞行剖面; 该阶段用于计算描述在考虑其瞬时航向及其瞬时速度的期间飞机未来路线上变化的最小飞行高度的最小垂直飞行剖面，该最小高度值是为 飞行器在期间内以盘点为中心的路线，使用对包含对应于最小飞行高度的空域区域的数据库的请求，每个请求返回由磁盘相交的区域，保留在磁盘中的最小高度为 返回的每种类型的区域的最小高度; 以及基于与最小垂直飞行剖面相比的垂直飞行剖面的相对位置产生警告消息的阶段。

公开(公告)号：US08032266B2

公开(公告)日：2011-10-04

申请号：US11547777

申请日：2005-03-22

申请人： Elias Bitar ,  Nicolas Marty

发明人： Elias Bitar ,  Nicolas Marty

IPC分类号： G01C21/00 ,  G06F17/00 ,  G05D1/08 ,  G08G5/04 ,  G01S13/94

CPC分类号： G01C21/005 ,  G01S13/94 ,  G05D1/0005 ,  G08G5/0086 ,  G08G5/045

摘要： This method facilitates the joining, by an aircraft, of a secure zone, without constraint of deployment in the horizontal plane, in particular when the latter is threatened by a risk of collision with the ground or by a risk of penetration into a forbidden zone which cannot be resolved by a purely vertical avoidance maneuver. It consists in selecting a point for joining a zone of free lateral deployment by means of a criterion of minimum cost of the initial maneuver of turning at the start of the trajectory for joining the possible points of access to the zones of free lateral deployment.

摘要翻译： 这种方法有利于航空器加入安全区域，而不受部署在水平面内的限制，特别是当后者受到与地面碰撞的危险的威胁或有渗入危险区域的危险时， 无法通过纯粹的垂直回避机动来解决。 它包括选择一个加入自由横向部署区域的点，通过在轨迹开始时初始机动转动的最小成本的标准来加入进入自由侧向部署区域的可能点。

公开(公告)号：US08024078B2

公开(公告)日：2011-09-20

申请号：US12106546

申请日：2008-04-21

申请人： François Coulmeau ,  Bernard Dubourg ,  Xavier Louis ,  Nicolas Marty

发明人： François Coulmeau ,  Bernard Dubourg ,  Xavier Louis ,  Nicolas Marty

IPC分类号： G01C23/00

CPC分类号： G08G5/065 ,  G08G5/0013 ,  G08G5/0021

摘要： A system on an aircraft used during taxiing or air/ground and ground/air transitions. The system groups together a set of devices for mapping the airport zone presenting the crew with a set of elements catalogued in a database and/or updated as a function of information received dynamically. The system group has control or monitoring of compliance with regulations and other mobile craft, consolidating the airport topological information, the ground control instructions and the applicable operational rules. The system groups have routing, that is preparation of the taxiing phase during an arrival or preparation for takeoff, by depicting the interactions with the ground control for receiving the taxiing instructions, and from the aircraft to the ground control to inform the same of the aircraft capabilities. The system groups have guidance in the form of instructions presented to the crew, and of automatic speed management capabilities, for managing emergency situations.

摘要翻译： 在滑行或空中/地面和地面/空中过渡期间使用的飞机上的系统。 系统将一组设备组合在一起，用于映射向机组提供的机场区域，该区域以数据库中编目的一组元素和/或根据动态接收的信息更新。 系统组对控制或者监控是否符合规定和其他手机，整合机场拓扑信息，地面控制指令和适用的操作规则。 系统组有路由，即准备到达或准备起飞期间的滑行阶段，通过描绘与地面控制接收滑行指示的相互作用，以及从飞机到地面控制以通知飞机的相同 能力 系统组以向船员提供的指示和自动速度管理能力的形式提供指导，用于管理紧急情况。

公开(公告)号：US20110160938A1

公开(公告)日：2011-06-30

申请号：US12980525

申请日：2010-12-29

申请人： Christophe CAILLAUD ,  François COULMEAU ,  Gilles FRANCOIS ,  Nicolas MARTY

发明人： Christophe CAILLAUD ,  François COULMEAU ,  Gilles FRANCOIS ,  Nicolas MARTY

IPC分类号： G05D1/00

CPC分类号： G06Q10/06

摘要： The present invention relates to a device for centralized management of tasks to be carried out by a crew of an aircraft. A task to be carried out includes a triggering condition and an instruction to be executed. The device includes a man-machine interface for managing tasks by the crew, a module for creating, modifying, deleting tasks, a module for triggering a task, a module for acknowledging a task performed, a module for executing a task, and an interface with systems of the aircraft which are able to create and to execute tasks. The invention applies to the piloting tasks carried out by the pilots of an aircraft.

摘要翻译： 本发明涉及一种用于集中管理由飞行员的船员进行的任务的装置。 要执行的任务包括触发条件和要执行的指令。 该设备包括用于管理船员任务的人机接口，用于创建，修改，删除任务的模块，用于触发任务的模块，用于确认所执行的任务的模块，用于执行任务的模块和接口 与飞机的系统能够创建和执行任务。 本发明适用于飞机驾驶员执行的驾驶任务。

公开(公告)号：US07777647B2

公开(公告)日：2010-08-17

申请号：US12030392

申请日：2008-02-13

申请人： Aurélie Sallier ,  Julia Percier ,  Nicolas Marty

发明人： Aurélie Sallier ,  Julia Percier ,  Nicolas Marty

IPC分类号： G01C21/00

CPC分类号： G01C23/005 ,  G01C5/005

摘要： The field of the invention is that of the display in map form of an operating zone of an aircraft on a screen, and more particularly a method of processing topographic data of this operating zone of an aircraft in real time, based on a calculation of radials (R) centred on a reference point (O) defining an angular segment of topographic data. According to the invention, the method includes a subdivision of the operating zone to be mapped into a plurality of angular segment sections, each forming an individual zone (3), and an assignment of a processing priority and a refresh frequency specific to each individual zone defined according to a criterion of operational interest of the element to the aircraft.

摘要翻译： 本发明的领域是在屏幕上飞行器的操作区域的地图形式的显示，更具体地说，一种基于径向的计算来实时地处理飞行器的该操作区的地形数据的方法 （R）以定义地形数据的角度段的参考点（O）为中心。 根据本发明，该方法包括将要映射到多个角度段部分的操作区域的细分，每个角度段部分形成一个单独的区域（3），以及对每个单独区域特定的处理优先级和刷新频率的分配 根据飞机的元件的操作兴趣的标准来定义。

公开(公告)号：US07733243B2

公开(公告)日：2010-06-08

申请号：US11575969

申请日：2005-07-04

申请人： Elias Bitar ,  Nicolas Marty

发明人： Elias Bitar ,  Nicolas Marty

IPC分类号： G08G5/04

CPC分类号： G01C23/00 ,  G01C21/00

摘要： The device relates to the signaling, to the pilot of a moving vehicle, for example an aircraft, of its lateral maneuvering margins taking into account obstacles placed in its maneuvering zone. This device determines, over the maneuvering zone of the moving vehicle, the contours of a first type of risk region that must be bypassed and those of two other types of risk region consisting of lateral margins surrounding the first type of risk region, of widths less than separation thresholds or their upper limit considered necessary for a lateral maneuver without space constraint and displays them for the pilot of the moving vehicle. The determination of the separation thresholds takes into account the bearing angle under which a point of the contour of a region of the first type is seen from the moving vehicle.

摘要翻译： 该装置涉及考虑到放置在其操纵区域中的障碍物的信号，向其移动的车辆的飞行员（例如飞行器）提供其侧向机动余量。 该装置在移动车辆的机动区域上确定必须绕过的第一类风险区域的轮廓以及包括第一类风险区域的侧向边缘的两种其他类型的风险区域的轮廓，宽度较小 比分离阈值或其上限被认为是没有空间限制的横向机动所必需的，并将其显示给移动车辆的飞行员。 分离阈值的确定考虑了从移动的车辆看到第一类型的区域的轮廓的点的轴承角度。