公开(公告)号：US20160078770A1

公开(公告)日：2016-03-17

申请号：US14848061

申请日：2015-09-08

Applicant: THALES

Inventor： François COULMEAU ,  Frédéric BONAMY ,  Vincent SAVARIT

IPC: G08G5/00

CPC classification number: G08G5/0039 ,  G06F3/04845 ,  G06F3/04847 ,  G06F3/04883 ,  G08G5/0021 ,  G08G5/0034

Abstract: A method of graphical manipulation of the trajectory of an aircraft comprises the steps of receiving an indication of a deformation point associated with the trajectory of the aircraft; determining a zone of local modification of the trajectory of the aircraft as a function of the deformation point; computing a modified trajectory and graphically restoring the modified trajectory. A parameter associated with the indication of the deformation point, notably a speed and/or acceleration value (for example of the contact point on the touch-sensitive interface, or else of a cursor), is received or determined. A modified trajectory is computed by selecting a computation algorithm from among a plurality of faster or slower predefined algorithms; the selection being performed as a function of the parameter. Various other developments are described (configurable selection, trajectory modification bounds, processing of an arbitrary deformation point, i.e. one other than a point of the flight plan, etc.).

Abstract translation: 图形操纵飞行器轨迹的方法包括以下步骤：接收与飞机轨迹相关联的变形点的指示; 确定作为变形点的函数的飞机轨迹的局部修改区域; 计算修改的轨迹并以图形方式恢复修改的轨迹。 接收或确定与变形点的指示相关联的参数，特别是速度和/或加速度值（例如触敏界面上的接触点或光标的其他）。 通过从多个更快或更慢的预定义算法中选择计算算法来计算修改的轨迹; 该选择是根据参数进行的。 描述各种其他发展（可配置选择，轨迹修改界限，任意变形点的处理，即除了飞行计划的点之外的其他变化点等）。

公开(公告)号：US20160065497A1

公开(公告)日：2016-03-03

申请号：US14842253

申请日：2015-09-01

Applicant: THALES

Inventor： François COULMEAU ,  Frédéric SANCHEZ ,  Laurent CASTET ,  Laurent DEWEERDT

IPC: H04L12/911 ,  H04L29/08

CPC classification number: H04L47/821 ,  H04L67/10 ,  H04L67/2828 ,  H04L67/322

Abstract: The system executes services by an application called “server” for at least one application called “client.” A preliminary step establishes for each service a list of calculation parameters that can be varied in a given range, called “adjustable parameters” as well as time and quality of the said service information according to the value of the said parameters. At the request of a client for a given service, the method adjusts the value of the adjustable calculation parameters as a function of a given constraint, the service being executed using the adjusted values of the said parameters.

Abstract translation: 系统对称为“客户端”的至少一个应用程序，称为“服务器”的应用程序执行服务。初步步骤为每个服务建立可以在给定范围内变化的计算参数列表，称为“可调参数”，以及 所述服务信息的时间和质量根据所述参数的值。 根据给定服务的客户端的请求，该方法根据给定的约束调整可调节计算参数的值，该服务使用所述参数的调整值来执行。

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。

公开(公告)号：US20150005992A1

公开(公告)日：2015-01-01

申请号：US14316666

申请日：2014-06-26

Applicant: THALES

Inventor： François COULMEAU ,  Jérôme SACLE ,  Emmanuel DEWAS

IPC: G08G5/02

CPC classification number: G08G5/02 ,  G05D1/0676 ,  G08G5/0039 ,  G08G5/025

Abstract: A method for calculating a flight plan used by a flight management system of an aircraft in a runway approach phase comprises: loading an initial procedure ending at a first end point not corresponding to a threshold of the runway and a first associated missed approach procedure; determining an additional procedure and a second associated missed approach procedure; concatenating the initial procedure and the additional procedure in order to generate a continuous concatenated flight plan comprising the initial procedure, the first missed approach procedure, the additional procedure and the second missed approach procedure; loading the concatenated flight plan into an active flight plan; selecting a second procedure from a set comprising the first missed approach procedure and the additional procedure; activating the selected second procedure.

Abstract translation: 用于计算在跑道接近阶段中的飞行器的飞行管理系统使用的飞行计划的方法包括：加载在不对应于跑道的阈值的第一终点处终止的初始过程和第一相关联的错过的接近程序; 确定附加过程和第二相关联的错过接近程序; 连接初始过程和附加过程，以便产生包括初始过程，第一次错过接近程序，附加过程和第二次错过接近程序的连续级联飞行计划; 将连接的飞行计划加载为主动飞行计划; 从包括所述第一错过的过程和附加过程的集合中选择第二过程; 激活所选择的第二过程。

公开(公告)号：US20140375479A1

公开(公告)日：2014-12-25

申请号：US14310940

申请日：2014-06-20

Applicant: THALES

Inventor： Patrick MAZOYER ,  Antoine LACOMBE ,  François COULMEAU

IPC: G08G5/00

CPC classification number: G08G5/0021 ,  G01C23/00 ,  G08G5/003 ,  G08G5/0047 ,  G08G5/0052

Abstract: A method, system and computer program for providing, on a human-machine interface, data relating to an aspect of the operation of an aircraft and grouped into one and the same area of the interface, the method comprising the following steps. A step of detecting a request to display an aspect of the operation of the aircraft. The method also includes a step of computing a flight situation and generating a consolidated aeroplane situation. A step of associating the elementary data linked to the consolidated aeroplane situation to extract therefrom updated situational data. The method then includes a step of grouping the updated situational data into a plurality of sub-sets to allow display of the data in the display area. Finally the method includes a step of displaying, in the display area, the sub-sets of data.

Abstract translation: 一种方法，系统和计算机程序，用于在人机界面上提供与飞行器的操作的一个方面有关的数据，并将其分组成界面的一个和同一区域，该方法包括以下步骤。 检测显示飞机操作方面的请求的步骤。 该方法还包括计算飞行情况并产生综合飞机情况的步骤。 将与联合飞机情况相关联的基本数据相关联以从中提取更新的情景数据的步骤。 该方法然后包括将更新的情境数据分组成多个子集以允许在显示区域中显示数据的步骤。 最后，该方法包括在显示区域中显示数据子集的步骤。

公开(公告)号：US20140012500A1

公开(公告)日：2014-01-09

申请号：US13936034

申请日：2013-07-05

Applicant: THALES

Inventor： Vincent SAVARIT ,  Emmanuel DEWAS ,  François COULMEAU

IPC: G01C21/00

CPC classification number: G01C21/00 ,  G08G5/0021 ,  G08G5/0039

Abstract: In the field of the definition of a flight plan for an aircraft, a method is provided for determining an offset lateral trajectory from an initial lateral trajectory comprising a set of initial waypoints. The initial lateral trajectory and the offset lateral trajectory have two junction points in common, namely a point of entry and a point of exit. At least one of the junction points is distinct from the initial waypoints and from the current position of the aircraft. This first junction point can notably be defined so that the flight duration or the flight distance between the first and second junction points corresponds to a defined value.

Abstract translation: 在飞行器飞行计划的定义领域中，提供了一种用于从包括一组初始航路点的初始横向轨迹确定偏移横向轨迹的方法。 初始侧向轨迹和偏移侧向轨迹具有共同的两个连接点，即入口点和出口点。 至少有一个交汇点不同于初始航点和飞机的当前位置。 可以明显地定义该第一连接点，使得第一和第二连接点之间的飞行持续时间或飞行距离对应于定义的值。