公开(公告)号：US20160093223A1

公开(公告)日：2016-03-31

申请号：US14862431

申请日：2015-09-23

Applicant: THALES

Inventor： Bertrand CAUDRON ,  Sonia VAUTIER ,  Patrick MAZOYER

IPC: G08G5/00 ,  B64D45/00

CPC classification number: G08G5/0039 ,  B64D45/00 ,  B64D2045/0075 ,  G01C23/005 ,  G01D7/00 ,  G08G5/0021 ,  G08G5/0047 ,  G08G5/0052 ,  G08G5/0065 ,  G08G5/025

Abstract: A method implemented by computer for the management of the flight of an aircraft comprises the steps of receiving flight directives and flight information associated with these directives; determining a flight context of the aircraft; as a function of the context determined, selecting information from among that associated with the formulation of a directive and/or with a current flight directive and/or with a change of a flight directive; sensorially restoring the selected information. Various developments are described, notably links to documentary resources, the determination of anomalies, the use of predefined logic rules and configuration options. System aspects and software aspects are described.

Abstract translation: 用于管理飞机飞行的计算机实施的方法包括以下步骤：接收与这些指令相关联的飞行指令和飞行信息; 确定飞机的飞行情况; 根据确定的上下文的功能，从与指令的制定和/或与当前航班指令和/或随着飞行指令的改变相关联的信息中选择信息; 感觉恢复所选信息。 描述了各种发展，特别是与文献资源的链接，异常的确定，使用预定义的逻辑规则和配置选项。 描述系统方面和软件方面。

公开(公告)号：US20160083107A1

公开(公告)日：2016-03-24

申请号：US14860480

申请日：2015-09-21

Applicant: THALES

Inventor： Sonia VAUTIER ,  Patrick MAZOYER ,  Bertrand CAUDRON

IPC: B64D45/00

CPC classification number: B64D45/00 ,  G07C5/0816 ,  G08B21/18 ,  G08G5/0021

Abstract: An alert management method implemented by a flight management system for triggering alerts during flight of an aircraft, using a look-up table associating, with each alert, at least one flight parameter and establishing, for each alert and the associated flight parameter, a correspondence between the value of the associated parameter and a plurality of predefined ordered priority levels. The method comprises when an alert is triggered: loading a value of the associated flight parameter, as a function of the state of the aircraft in real time, determining the priority level of the current alert out of the plurality, the priority level being determined by the value and from the look-up table; at regular time intervals and for each active alert, reiterating the preceding steps to determine, for each active alert, an associated priority level that is a function of the state of the aircraft in real time.

Abstract translation: 一种由飞行管理系统实现的警报管理方法，用于在飞行器飞行期间触发警报，使用与每个警报相关联的查找表与至少一个飞行参数，并为每个警报和相关联的航班参数建立一个对应关系 在相关参数的值和多个预定义的有序优先级之间。 该方法包括当触发警报时：根据飞行器的状态实时加载相关航班参数的值，确定多个当前警报的优先级，优先级由 价值和从查表; 以规则的时间间隔和对于每个主动警报，重复上述步骤以针对每个主动警报确定作为飞行器状态的实时功能的相关优先级。

公开(公告)号：US20180366011A1

公开(公告)日：2018-12-20

申请号：US16003649

申请日：2018-06-08

Applicant: THALES

Inventor： Xavier BLANCHON ,  Guillaume BOYER ,  Guillaume MEULLE ,  Sonia VAUTIER

IPC: G08G5/00 ,  G01C21/20

Abstract: A method for assisting in the flight management of an aircraft calculates a local operating cost function CF(xi, hj) at various altitudes hj along a planned reference flight trajectory over a discrete set of points P(xi, hj) which forms a two-dimensional grid in which the planned vertical reference flight trajectory varies, the local cost function CF(xi, hj) being calculated locally at each point P(xi, hj) according to aircraft data and environmental data predicted at said local point P(xi, hj). Then, for each point P(xi, hj) of the grid, the method determines a neighbourhood including the point P(xi, hj), and associates a colour K(xi, hj) therewith that is dependent on the value of the local cost function CF(xi, hj) using a predetermined bijective lookup transformation. Next, the method displays the coloured grid formed by the coloured neighbourhoods. The method is implemented in an onboard flight management avionics system, in an onboard tablet of EFB type, in a ground tool of the operator which is interfaced with the onboard flight management system, or by distribution over the three types of systems.

公开(公告)号：US20160116917A1

公开(公告)日：2016-04-28

申请号：US14885866

申请日：2015-10-16

Applicant: THALES

Inventor： Valérie BATAILLON ,  Sonia VAUTIER ,  Emmanuel DEWAS

IPC: G05D1/06 ,  G08G5/02 ,  G08G5/00

CPC classification number: G05D1/0676 ,  G01C21/20 ,  G05D1/0005 ,  G05D1/101 ,  G08G5/0039 ,  G08G5/006 ,  G08G5/025

Abstract: A method implemented by computer for calculating a lateral approach trajectory of an aircraft, comprises the steps of receiving selection of a landing runway; determining a zone Z1, the zone defining trajectory limits to carry out a last turn with a view to landing on the indicated runway; receiving indication of a trajectory point FF defining a point of alignment of the aircraft; determining a joining trajectory bound for a point FAF2, the joining trajectory going from the aircraft to the point FAF2 and then to the point FF and then to the indicated landing runway without passing through the zone Z1. Developments describe the use of a zone Z2 associated with visibility conditions, the calculation of the energy to be dissipated, the use of a predefined descent profile, the emission of alerts and trajectory adaptations by increasing the length of the joining trajectory or use of the airbrakes.

Abstract translation: 一种由计算机实现的用于计算飞行器的侧向进近轨迹的方法，包括以下步骤：接收对着陆跑道的选择; 确定区域Z1，区域定义轨迹限制以执行最后一个转弯，以便着落在指示的跑道上; 接收限定飞行器对准点的轨迹点FF的指示; 确定对于点FAF2限定的联接轨迹，从飞行器到点FAF2的接合轨迹，然后到点FF，然后到达指示的着陆跑道，而不通过区域Z1。 发展描述了与可见度条件相关联的区域Z2的使用，要耗散的能量的计算，预定义的下降轮廓的使用，通过增加连接轨迹的长度或使用空气制动器的警报和轨迹适应的发射 。

公开(公告)号：US20170132939A1

公开(公告)日：2017-05-11

申请号：US15344775

申请日：2016-11-07

Applicant: THALES

Inventor： Franck PRENOT ,  Sonia VAUTIER ,  Philippe CHAIX

IPC: G08G5/00 ,  B64D45/00

CPC classification number: G08G5/0065 ,  B64D45/00 ,  B64D2045/0085 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/0056 ,  G08G5/0091

Abstract: A method for managing the trajectory of an aircraft implemented by computer comprises the steps consisting of: receiving the aeroplane performance levels, receiving a flight plan, receiving ground relief data, receiving weather data, determining the coordinates of a safety point according to the aeroplane performance levels, the relief data and the weather data, the safety point making it possible to continue the flight according to a predefined SID landing trajectory in case of outage of one or more engines of the aircraft. Developments are described, notably in computation of the spatial coordinates of the safety point, the management of several safety points and/or of EOSID trajectories, the insertion or the activation of an EOSID trajectory including in the absence of engine outage, the management of the Disarm Point flight plan point. System and software aspects are described.

公开(公告)号：US20150332490A1

公开(公告)日：2015-11-19

申请号：US14712796

申请日：2015-05-14

Applicant: THALES

Inventor： François COULMEAU ,  Sonia VAUTIER ,  Frédéric BONAMY

IPC: G06T11/20 ,  B64D43/00 ,  G09G5/36 ,  G01C21/00

CPC classification number: G06T11/206 ,  B64D43/00 ,  G01C21/00 ,  G01C23/005 ,  G06T2210/32 ,  G06T2210/61 ,  G09G5/36 ,  G09G2380/12

Abstract: A method for assisting the navigation of an aircraft comprises: assembly by families of data by a processing unit of predetermined data and acquired data, including meteorological data, the families being predefined, each data value being associated with a time window of validity; formatting the data of the families to associate with each data value a type of graphical representation as text or a scalar, vector, surface, or volume; selection of families of data to be displayed; choice of a display time window for each family of data to be displayed; spatio-temporal discretization of the trajectory; spatio-temporal correlation of the discretized trajectory with each family of data as a function of the time windows of validity, in the display time windows of the family, to extract a sub-assembly from each family of data, by the processing unit; display of the sub-assemblies in a single representation on the same display screen.

Abstract translation: 一种辅助航空器导航的方法包括：由预定数据的处理单元组合数据的数据，以及所获取的数据，包括气象数据，预定义的系列，每个数据值与有效时间窗口相关联; 将家族的数据格式化为与每个数据值相关联的一种图形表示作为文本或标量，向量，表面或体积; 选择要显示的数据族; 选择要显示的每个数据系列的显示时间窗口; 轨迹的时空离散化; 通过处理单元，在家庭的显示时间窗口中从每个数据系列提取子组件，将离散轨迹与每个数据系列作为时间窗的函数的时空相关性; 在同一显示屏幕上以单个表示形式显示子组件。