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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。
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公开(公告)号：US08676404B2
公开(公告)日：2014-03-18
申请号：US12979404
申请日：2010-12-28
申请人： Nicolas Marty , François Coulmeau , Fabien Guilley
发明人： Nicolas Marty , François Coulmeau , Fabien Guilley
CPC分类号： G08G5/0021 , G08G5/0052
摘要： In a centralized navigation information management system installed on board an aircraft which is in a current position at a current time, the aircraft having a warning management system and a route management system with means for creating a route plan, the route plan having a future route plan corresponding with the part of the route plan beginning at the current position and at the current time, the system includes: means for creating a task comprising at least one task parameter relating to an item of navigation information, including a task variable corresponding to a condition of execution of the said task, the means for creating a task having means for determining a predicted time meeting the execution condition; and means for detecting a possible inconsistency between the created task and the route plan or the future route plan and for transmitting, when an inconsistency is detected, a message relating to the inconsistency to a first display means of a centralized warning management system to display the inconsistency message on a first man-machine interface.
摘要翻译： 在安装在目前当前位置的飞机上的集中式导航信息管理系统中，飞机具有警告管理系统和具有用于创建路线图的装置的路线管理系统，路线图具有未来路线 计划对应于从当前位置和当前时间开始的路线计划的部分，系统包括：用于创建任务的装置，其包括与导航信息项有关的至少一个任务参数，包括对应于 所述任务的执行条件，用于创建任务的装置具有用于确定满足执行条件的预测时间的装置; 以及用于检测所创建的任务与路线计划或未来路线规划之间可能的不一致的装置，并且用于当检测到不一致时发送与集中警告管理系统的第一显示装置不一致的消息，以显示 第一个人机界面上的不一致信息。
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公开(公告)号：US08437957B2
公开(公告)日：2013-05-07
申请号：US13004704
申请日：2011-01-11
IPC分类号： G01C21/20
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。
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公开(公告)号：US20100100308A1
公开(公告)日：2010-04-22
申请号：US12579272
申请日：2009-10-14
CPC分类号： G08G5/006
摘要： The invention relates to a device for formulating a flight plan ensuring sufficient safety margins for a duration of a few minutes in relation to the set of flight constraints that could arise and comprising means for: detecting the surrounding moving objects (aircraft or meteorological phenomena), evaluating their type and the danger that they represent, formulating a reconfiguration flight plan ensuring a separation with these phenomena and taking best account of the constraints of the initially followed flight plan, avoiding prohibited or regulated airspaces and avoiding the surrounding relief with ad hoc operational margins.
摘要翻译： 本发明涉及一种用于制定飞行计划的装置，其确保相对于可能出现的一组飞行约束，持续几分钟的足够的安全裕度，并且包括用于：检测周围的运动物体（飞机或气象现象）的装置， 评估他们的类型和他们所代表的危险，制定重新配置飞行计划，确保与这些现象分离，并充分考虑到最初跟踪的飞行计划的限制，避免被禁止或受规管的空域，并避免周围的特殊运营利润减轻 。
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公开(公告)号：US20120029737A1
公开(公告)日：2012-02-02
申请号：US12979404
申请日：2010-12-28
申请人： Nicolas Marty , François Coulmeau , Fabien Guilley
发明人： Nicolas Marty , François Coulmeau , Fabien Guilley
IPC分类号： G05D1/00
CPC分类号： G08G5/0021 , G08G5/0052
摘要： In a centralized navigation information management system installed on board an aircraft which is in a current position at a current time, the aircraft having a warning management system and a route management system with means for creating a route plan, the route plan having a future route plan corresponding with the part of the route plan beginning at the current position and at the current time, the system includes: means for creating a task comprising at least one task parameter relating to an item of navigation information, including a task variable corresponding to a condition of execution of the said task, the means for creating a task having means for determining a predicted time meeting the execution condition; and means for detecting a possible inconsistency between the created task and the route plan or the future route plan and for transmitting, when an inconsistency is detected, a message relating to the inconsistency to a first display means of a centralized warning management system to display the inconsistency message on a first man-machine interface.
摘要翻译： 在安装在目前当前位置的飞机上的集中式导航信息管理系统中，飞机具有警告管理系统和具有用于创建路线图的装置的路线管理系统，路线图具有未来路线 计划对应于从当前位置和当前时间开始的路线计划的部分，系统包括：用于创建任务的装置，其包括与导航信息项有关的至少一个任务参数，包括对应于 所述任务的执行条件，用于创建任务的装置具有用于确定满足执行条件的预测时间的装置; 以及用于检测所创建的任务与路线计划或未来路线规划之间可能的不一致的装置，并且用于当检测到不一致时发送与集中警告管理系统的第一显示装置不一致的消息，以显示 第一个人机界面上的不一致信息。
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公开(公告)号：US08751061B2
公开(公告)日：2014-06-10
申请号：US13018111
申请日：2011-01-31
申请人： François Coulmeau , Nicolas Marty , Stéphane Gomez
发明人： François Coulmeau , Nicolas Marty , Stéphane Gomez
IPC分类号： G05D1/00
CPC分类号： G08G5/0069 , G08G5/0013
摘要： A system for aiding the navigation of an aircraft able to be piloted remotely by an operator includes means for transmitting data allowing the operator to dialogue with an air traffic controller according to at least one mode of dialogue and means for monitoring the flight parameters, notably aircraft state parameters and navigation parameters. The system also includes a means for detecting flight events, a means for formulating a message corresponding to a flight event, a means for scheduling the message in a list of messages, and a means for synthesizing the message in a mode of dialogue.
摘要翻译： 用于帮助能够由操作者远程驾驶的飞行器的导航的系统包括用于发送允许操作者根据至少一种对话模式与空中交通管制员对话的数据的装置的装置和用于监视飞行参数的手段的装置，特别是飞行器 状态参数和导航参数。 该系统还包括用于检测飞行事件的装置，用于制定对应于飞行事件的消息的装置，用于在消息列表中调度消息的装置，以及用于以对话模式合成该消息的装置。
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7.发明授权Method of forming a 3D safe emergency descent trajectory for aircraft and implementation device 有权形成用于飞机和实施装置的3D安全紧急下降轨迹的方法公开(公告)号：US07925394B2
公开(公告)日：2011-04-12
申请号：US11870338
申请日：2007-10-10
申请人： Guy Deker , Nicolas Marty , François Coulmeau
发明人： Guy Deker , Nicolas Marty , François Coulmeau
IPC分类号： G01C21/18
CPC分类号： G08G5/0039 , G01C21/00 , G05D1/0676
摘要： The method in accordance with the invention is a method of providing a 3D emergency descent trajectory for aircraft comprising the steps of searching for at least one possible better trajectory allowing a secure continuation in relation to the relief and/or the surrounding conditions towards a homing point as soon as a situation requiring an unscheduled modification of the current trajectory occurs, wherein this trajectory is updated as a function of the alterations in the surrounding conditions, as a function of the information provided by the onboard sensors and/or outside information received.
摘要翻译： 根据本发明的方法是提供用于飞行器的3D紧急下降轨迹的方法，包括以下步骤：搜索至少一个可能的更好的轨迹，允许相对于所述浮雕和/或围绕归位点的周围条件的安全延续 一旦出现需要对当前轨迹进行不定期修改的情况，其中根据由机载传感器提供的信息和/或所接收的外部信息，该轨迹作为周围环境变化的函数被更新。
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8.发明授权公开(公告)号：US08190310B2
公开(公告)日：2012-05-29
申请号：US12366667
申请日：2009-02-06
IPC分类号： G06G7/70
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）。
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公开(公告)号：US08024078B2
公开(公告)日：2011-09-20
申请号：US12106546
申请日：2008-04-21
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。
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10.发明授权Method of protecting an aircraft by signalling against the risks of collision with the terrain in procedures with reduced protection corridor 有权通过在减少保护走廊的程序中发信号反对与地形碰撞的风险来保护飞机的方法公开(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
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。
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