公开(公告)号：US08594863B2

公开(公告)日：2013-11-26

申请号：US12896698

申请日：2010-10-01

Applicant: François Coulmeau ,  Xavier Blanchon ,  Christophe Caillaud

Inventor： François Coulmeau ,  Xavier Blanchon ,  Christophe Caillaud

IPC: G01C23/00 ,  G06F7/00 ,  G06F19/00 ,  G05D1/00 ,  G05D3/00

CPC classification number: G08G5/0013 ,  G08G5/0039

Abstract: A method for aiding the management of an aircraft flight according to an active flight plan receiving a control clearance transmitted at a current time includes a step of computing a reception flight plan based on the said control clearance, a step of storing the said reception flight plan in a memory space dedicated to the said reception flight plan. The method also includes, prior to the step of computing a reception flight plan: a step of determining the time, called the recognition time, assumed to have to elapse between the current time and a time at which the said control clearance is assumed to be recognized; a step of attribution, to the said control clearance, of a destination flight plan as a function of the recognition time, the said destination flight plan being the temporary flight plan when the recognition time is included in a first time slot and the destination flight plan being a secondary flight plan when the recognition time is included in a second time slot longer than the first time slot.

Abstract translation: 根据在当前时间发送的接收到控制许可的主动飞行计划来帮助管理飞行器飞行的方法包括基于所述控制许可计算接收飞行计划的步骤，存储所述接收飞行计划的步骤 在专用于所述接收飞行计划的存储空间中。 该方法还包括在计算接收飞行计划的步骤之前：确定称为识别时间的时间的步骤，假定在当前时间与假定所述控制间隙之间的时间为止 认可的 将目的地飞行计划归因于所述控制许可的步骤作为识别时间的函数，所述目的地飞行计划是当第一时隙中包括识别时间的目的地飞行计划和目的地飞行计划 当识别时间被包括在比第一时隙长的第二时隙中时，作为辅助飞行计划。

公开(公告)号：US08386158B2

公开(公告)日：2013-02-26

申请号：US12632562

申请日：2009-12-07

Applicant: Xavier Blanchon ,  François Coulmeau ,  Manuel Gutierrez-Castaneda

Inventor： Xavier Blanchon ,  François Coulmeau ,  Manuel Gutierrez-Castaneda

IPC: G06F19/00

CPC classification number: G08G5/025 ,  G05D1/104 ,  G08G5/0008 ,  G08G5/0021 ,  G08G5/0052

Abstract: A method for providing for the optimized regulation of the relative spacing between aircraft is disclosed. This method can be implemented by a system whose physical architecture can rely mainly on existing computers on board most current aircraft. The method includes a main step of determining the changing trend of the relative spacing, in distance or in time, between a target aircraft (C) and a following aircraft (S).

Abstract translation: 公开了一种用于提供飞行器之间的相对间距的优化调节的方法。 该方法可以由物理架构主要依赖当前飞机上的现有计算机的系统来实现。 该方法包括确定目标飞机（C）和下一架飞机（S）之间距离或时间上的相对间距的变化趋势的主要步骤。

公开(公告)号：US08244453B2

公开(公告)日：2012-08-14

申请号：US12766892

申请日：2010-04-25

Applicant: Antoine Lacombe ,  Xavier Blanchon ,  François Coulmeau

Inventor： Antoine Lacombe ,  Xavier Blanchon ,  François Coulmeau

IPC: G05D1/00

CPC classification number: G08G5/0065 ,  G05D1/0661

Abstract: A method of adjusting the trajectory of an aircraft flying a climb circuit, of substantially helical form corresponding to a succession of racetracks, denoted HOLD, the last HOLD, called the exit HOLD, having predefined geometric characteristics and comprising a lock-on point, allowing the aircraft to enter and to exit in the HOLD, the aircraft attaining the setpoint altitude of the climb circuit during the flight of the exit HOLD, comprises at least three steps, including: a step of computing the prediction of the position of the aircraft when the setpoint altitude will be attained; a step of computing the remaining distance to be traveled, between the position of the aircraft when the setpoint altitude will be attained and the lock-on point; and a step making it possible to carry out an adaptation of the form of the exit HOLD so as to minimize the remaining distance to be traveled DELTA.

Abstract translation: 调整飞行爬升电路的飞行器的轨迹的方法，其基本上螺旋形式对应于连续的赛道，表示为HOLD，称为出口HOLD的最后一个HOLD，具有预定义的几何特征并包括锁定点，允许 所述飞机进入并在所述HOLD中退出，所述飞机在所述出口HOLD的飞行期间达到所述爬升回路的设定点高度，包括至少三个步骤，包括：计算所述飞行器的位置的预测的步骤 将达到设定点高度; 在达到设定点高度时计算飞机剩余距离，飞行器位置和锁定点之间的步骤; 以及使得可以执行出口保持装置的形式的适应，以便最小化要行驶的剩余距离DELTA。

公开(公告)号：US20110137493A1

公开(公告)日：2011-06-09

申请号：US12790596

申请日：2010-05-28

Applicant: Benoît Dacre-Wright ,  Guy Deker ,  Xavier Blanchon

Inventor： Benoît Dacre-Wright ,  Guy Deker ,  Xavier Blanchon

IPC: G06F7/00 ,  G05D1/00

CPC classification number: G05D1/101

Abstract: Method for generating a flight speed profile of an aircraft (100) according to an RTA constraint, characterized in that it permanently calculates, at any point of the flight plan, a speed setpoint VΩ(X) of the aircraft determined on the basis of reference speed profiles, comprising at least a minimum speed profile Vmin(X), and a maximum speed profile Vmax(X). The method can also take into account an optimum speed profile Vopt(X) determined, for example, on the basis of a cost or performance index.

Abstract translation: 用于根据RTA约束产生飞行器（100）的飞行速度曲线的方法，其特征在于，其在飞行计划的任何点处永久地计算基于以下方式确定的飞行器的速度设定点V＆OHgr;（X） 参考速度曲线，包括至少最小速度曲线Vmin（X）和最大速度曲线Vmax（X）。 该方法还可以考虑例如基于成本或性能指标确定的最佳速度曲线Vopt（X）。

公开(公告)号：US20140200752A9

公开(公告)日：2014-07-17

申请号：US12633508

申请日：2009-12-08

Applicant: Antoine Lacombe ,  Xavier Blanchon ,  François Coulmeau

Inventor： Antoine Lacombe ,  Xavier Blanchon ,  François Coulmeau

IPC: G01C23/00

CPC classification number: G05D1/0202 ,  G01W1/08 ,  G01W1/10 ,  G08G5/0039 ,  G08G5/0091

Abstract: The invention relates to a meteorological modelling method for calculating an aircraft flight plan, the aircraft comprising a communication means and a navigation management system.The method comprises at least the following steps: the communication means carries out the acquisition of meteorological prediction data related to waypoints in proximity to the nominal route in addition to the waypoints belonging to the nominal route, the navigation management system allocates by projection onto the current route of the aircraft the prediction data for the said waypoints not belonging to the current route, the navigation management system calculates the meteorological prediction data for the waypoints of the current route of the flight plan according to the prediction data allocated by projection onto the current route of the aircraft.The invention is a modelling method for aircraft navigation management systems.

Abstract translation: 本发明涉及一种用于计算飞行器飞行计划的气象建模方法，该飞行器包括通信装置和导航管理系统。 该方法至少包括以下步骤：除了属于标称路线的航路点之外，通信装置还执行与标称路径附近的航路点相关的气象预测数据的获取，导航管理系统通过投影分配到当前 航空器的路线是不属于当前路线的所述航路点的预测数据，导航管理系统根据通过投影到当前路线上分配的预测数据来计算飞行计划的当前路线的航路点的气象预测数据 的飞机。 本发明是用于飞机导航管理系统的建模方法。

公开(公告)号：US08437957B2

公开(公告)日：2013-05-07

申请号：US13004704

申请日：2011-01-11

Applicant: François Coulmeau ,  Nicolas Marty ,  Xavier Blanchon ,  Pierre Gamet

Inventor： François Coulmeau ,  Nicolas Marty ,  Xavier Blanchon ,  Pierre Gamet

IPC: G01C21/20

CPC classification number: G08G5/0034

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20100152931A1

公开(公告)日：2010-06-17

申请号：US12633508

申请日：2009-12-08

Applicant: Antoine Lacombe ,  Xavier Blanchon ,  François Coulmeau

Inventor： Antoine Lacombe ,  Xavier Blanchon ,  François Coulmeau

IPC: G01C23/00

CPC classification number: G05D1/0202 ,  G01W1/08 ,  G01W1/10 ,  G08G5/0039 ,  G08G5/0091

Abstract: The invention relates to a meteorological modelling method for calculating an aircraft flight plan, the aircraft comprising a communication means and a navigation management system.The method comprises at least the following steps: the communication means carries out the acquisition of meteorological prediction data related to waypoints in proximity to the nominal route in addition to the waypoints belonging to the nominal route, the navigation management system allocates by projection onto the current route of the aircraft the prediction data for the said waypoints not belonging to the current route, the navigation management system calculates the meteorological prediction data for the waypoints of the current route of the flight plan according to the prediction data allocated by projection onto the current route of the aircraft.The invention is a modelling method for aircraft navigation management systems.

Abstract translation: 本发明涉及一种用于计算飞行器飞行计划的气象建模方法，该飞行器包括通信装置和导航管理系统。 该方法至少包括以下步骤：除了属于标称路线的航路点之外，通信装置还执行与标称路径附近的航路点相关的气象预测数据的获取，导航管理系统通过投影分配到当前 航空器的路线是不属于当前路线的所述航路点的预测数据，导航管理系统根据通过投影到当前路线上分配的预测数据来计算飞行计划的当前路线的航路点的气象预测数据 的飞机。 本发明是用于飞机导航管理系统的建模方法。

公开(公告)号：US08473120B2

公开(公告)日：2013-06-25

申请号：US12624725

申请日：2009-11-24

Applicant: Xavier Blanchon ,  Philippe Chaix ,  Christophe Caillaud

Inventor： Xavier Blanchon ,  Philippe Chaix ,  Christophe Caillaud

IPC: G05D1/00

CPC classification number: G05D1/0005 ,  G08G5/0052 ,  G08G5/0078

Abstract: The invention relates to the field of civil aviation and, more specifically, relates to the flight management systems, more commonly known by the English acronym FMS. The method for assisting in the management of the flight of an aircraft in order to keep to a time constraint according to the present invention allows for a control of the keeping to the time constraint that presents a rapid dynamic, by avoiding as far as possible having the estimated time of arrival (ETA) at a particular point (P) able to drift relative to a required time of arrival (RTA) at said particular point (P), thanks to the use of a maneuvering margin (M) granted to the guidance module of the aircraft.

Abstract translation: 本发明涉及民用航空领域，更具体地涉及飞行管理系统，其通常被英文首字母缩略词FMS所熟知。 为了保持根据本发明的时间限制的协助飞行器飞行的管理的方法允许通过避免尽​​可能避免具有快速动态的时间约束来控制， 在特定点（P）处可以相对于在所述特定点（P）处的所需到达时间（RTA）漂移的特定点（P）的估计到达时间（ETA），这归功于使用授予 飞机的指导模块。

公开(公告)号：US20110246053A1

公开(公告)日：2011-10-06

申请号：US12896698

申请日：2010-10-01

Applicant: François Coulmeau ,  Xavier Blanchon ,  Christophe Caillaud

Inventor： François Coulmeau ,  Xavier Blanchon ,  Christophe Caillaud

IPC: G08G5/00 ,  G05D1/00

CPC classification number: G08G5/0013 ,  G08G5/0039

Abstract: A method for aiding the management of an aircraft flight according to an active flight plan receiving a control clearance transmitted at a current time includes a step of computing a reception flight plan based on the said control clearance, a step of storing the said reception flight plan in a memory space dedicated to the said reception flight plan. The method also includes, prior to the step of computing a reception flight plan: a step of determining the time, called the recognition time, assumed to have to elapse between the current time and a time at which the said control clearance is assumed to be recognized; a step of attribution, to the said control clearance, of a destination flight plan as a function of the recognition time, the said destination flight plan being the temporary flight plan when the recognition time is included in a first time slot and the destination flight plan being a secondary flight plan when the recognition time is included in a second time slot longer than the first time slot.

Abstract translation: 根据在当前时间发送的接收到控制许可的主动飞行计划来帮助管理飞行器飞行的方法包括基于所述控制许可计算接收飞行计划的步骤，存储所述接收飞行计划的步骤 在专用于所述接收飞行计划的存储空间中。 该方法还包括在计算接收飞行计划的步骤之前：确定称为识别时间的时间的步骤，假定在当前时间与假定所述控制间隙之间的时间为止 认可的 将目的地飞行计划归因于所述控制许可的步骤作为识别时间的函数，所述目的地飞行计划是当第一时隙中包括识别时间的目的地飞行计划和目的地飞行计划 当识别时间被包括在比第一时隙长的第二时隙中时，作为辅助飞行计划。

公开(公告)号：US20110153204A1

公开(公告)日：2011-06-23

申请号：US12973438

申请日：2010-12-20

Applicant: François COULMEAU ,  Antoine LACOMBE ,  Xavier BLANCHON ,  Fany BARAILLER

Inventor： François COULMEAU ,  Antoine LACOMBE ,  Xavier BLANCHON ,  Fany BARAILLER

IPC: G01C21/00

CPC classification number: G06Q10/04 ,  G08G5/0052

Abstract: The invention relates to a method and a device for calculating a time window for a time constraint of arrival of an aircraft at a given point, the aircraft receiving wind predictions and including a sensor for measuring the wind. The method includes a calculation of a first time window, and the calculation of an overall confidence index having the determination of a first confidence index on the basis of a deviation between wind predictions and wind measurements performed by the aircraft, the calculation of a margin for the time constraint on the basis of the overall confidence index, and the calculation of a second window on the basis of the first time window and of the calculated margin.

Abstract translation: 本发明涉及一种用于计算飞行器在给定点的到达时间约束的时间窗的方法和装置，飞行器接收风预测并且包括用于测量风的传感器。 该方法包括第一时间窗口的计算，以及基于风预测与飞行器执行的风测量之间的偏差确定第一置信指数的总体置信指数的计算， 基于总体信心指数的时间约束，以及基于第一时间窗口计算的第二窗口和计算的余量。