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    Management of the energy in an approach trajectory
    2.
    发明授权
    Management of the energy in an approach trajectory 有权

    公开(公告)号：US09709991B2

    公开(公告)日：2017-07-18

    申请号：US14885866

    申请日：2015-10-16

    Applicant: THALES

    Inventor： Valérie Bataillon ,  Sonia Vautier ,  Emmanuel Dewas

    IPC: G05D1/06 ,  G08G5/00 ,  G08G5/02 ,  G01C21/20 ,  G05D1/10

    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.

    Method for assisting the navigation of an aircraft with correlation of dynamic information with a 4D flight trajectory
    3.
    发明授权
    Method for assisting the navigation of an aircraft with correlation of dynamic information with a 4D flight trajectory 有权
    用于协助航空器导航的方法，其具有与4D飞行轨迹的动态信息的相关性

    公开(公告)号：US09524571B2

    公开(公告)日：2016-12-20

    申请号：US14712796

    申请日：2015-05-14

    Applicant: THALES

    Inventor： François Coulmeau ,  Sonia Vautier ,  Frédéric Bonamy

    IPC: G01C21/00 ,  G01C23/00 ,  G06T11/20 ,  B64D43/00 ,  G09G5/36

    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。

    Managing the trajectory of an aircraft in case of engine outage
    4.
    发明授权
    Managing the trajectory of an aircraft in case of engine outage 有权

    公开(公告)号：US10026327B2

    公开(公告)日：2018-07-17

    申请号：US15344775

    申请日：2016-11-07

    Applicant: THALES

    Inventor： Franck Prenot ,  Sonia Vautier ,  Philippe Chaix

    IPC: B64D45/00 ,  G08G5/00

    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.

    Contextual aid to flight management
    8.
    发明授权
    Contextual aid to flight management 有权
    对飞行管理的情境援助

    公开(公告)号：US09530322B2

    公开(公告)日：2016-12-27

    申请号：US14862431

    申请日：2015-09-23

    Applicant: THALES

    Inventor： Bertrand Caudron ,  Sonia Vautier ,  Patrick Mazoyer

    IPC: G08G5/00 ,  B64D45/00 ,  G01C23/00 ,  G01D7/00 ,  G08G5/02

    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。

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