公开(公告)号：US09329045B2

公开(公告)日：2016-05-03

申请号：US14540756

申请日：2014-11-13

Applicant: THALES

Inventor： Francois Coulmeau ,  Arnaud Bonnafoux ,  Nicolas Rossi

IPC: G01C21/00 ,  G06F19/00 ,  G01S13/95 ,  G08G5/04 ,  G05D1/10 ,  G08G5/00

CPC classification number: G01C21/00 ,  G01S13/953 ,  G05D1/101 ,  G08G5/0034 ,  G08G5/0052 ,  G08G5/04

Abstract: A method for determining a result path of an aircraft, the result path including a set of successive positions of the aircraft between an initial global point and a final global point that are predetermined for a mission of the aircraft is provided.The aircraft includes a plurality of calculating members, each able to guide the aircraft during at least part of the mission and to calculate an elementary path of the aircraft during that part, each elementary path including a set of successive positions of the aircraft between an initial elementary point and a final elementary point.The device includes calculating a portion of the result path from elementary paths coming from at least two distinct calculating members.

Abstract translation: 提供了一种用于确定飞行器的结果路径的方法，所述结果路径包括飞行器在为飞行器的任务预定的初始全局点和最终全局点之间的连续位置的集合。 飞行器包括多个计算构件，每个计算构件能够在至少部分任务期间引导飞行器，并且在该部分期间计算飞行器的基本路径，每个基本路径包括飞行器在初始位置之间的连续位置的集合 基本点和最终基本点。 该装置包括从至少两个不同的计算部件的基本路径计算结果路径的一部分。

公开(公告)号：US20180061248A1

公开(公告)日：2018-03-01

申请号：US15684155

申请日：2017-08-23

Applicant: Thales

Inventor： Cédric D'Silva ,  Jérôme Sacle ,  Nicolas Rossi

IPC: G08G5/00

CPC classification number: G08G5/0039 ,  G05D1/101 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0047

Abstract: An aid method for piloting an aircraft including acquiring an instruction intended to alter the flight plan, determining an applicability period of the instruction made up of a plurality of applicability moments of the instruction in which the application of the instruction is compatible with the operational capabilities of the aircraft and with the constraints of the flight plan, for each applicability moment of the instruction, determining an altered flight plan in case of application of the instruction at this applicability moment and calculating values of the operational parameters associated with this flight plan, and selecting an optimal applicability moment based on values of the operational parameters associated with the altered flight plan and operational parameters associated with the current flight plan.

公开(公告)号：US09881505B2

公开(公告)日：2018-01-30

申请号：US15085857

申请日：2016-03-30

Applicant: THALES

Inventor： Stéphane Gomez ,  Cécile Gadat ,  Nicolas Rossi

IPC: G08G5/00 ,  H04W4/14 ,  H04L12/721 ,  B64D43/00 ,  H04B7/185

CPC classification number: G08G5/0013 ,  B64D43/00 ,  G08G5/0021 ,  H04B7/18506 ,  H04L45/66 ,  H04W4/14

Abstract: A method and electronic device for control of messages exchanged between an aircraft and a ground station, and associated computer program product are disclosed. In one aspect, the method includes acquiring a message, extracting descriptive data from the acquired message, and determining the identifier of the acquired message. If the identifier of the acquired message corresponds to a shared identifier of the messages of a dialog in progress, the method includes associating that acquired message with that dialog. If not, the method includes associating the acquired message with a new dialog. The method further includes determining the position of a symbol corresponding to the dialog associated with the acquired message, the position being determined based on the type and start date of this dialog, the symbol being configured to be displayed in a display zone of the symbols corresponding to the different dialogs.

公开(公告)号：US20150134153A1

公开(公告)日：2015-05-14

申请号：US14540725

申请日：2014-11-13

Applicant: THALES

Inventor： Francois Coulmeau ,  Arnaud Bonnafoux ,  Nicolas Rossi

IPC: G05D1/00

CPC classification number: G05D1/00 ,  G05B23/0283

Abstract: A supervision device for an aircraft including a plurality of avionics systems, each avionics system being able to generate parameters representative of its operation on a reference date, includes a plurality of prediction modules, each prediction module including a computer for computing projections representative of the trajectory of the aircraft and/or representative of the operation of at least one avionics system on a corresponding prediction date, the prediction date being after the reference date, at least one projection computed by a prediction module depending on at least one other projection computed by another prediction module.

Abstract translation: 一种用于包括多个航空电子系统的飞行器的监视装置，每个航空电子系统能够在参考日期上产生表示其操作的参数，包括多个预测模块，每个预测模块包括用于计算表示轨迹的投影的计算机 的飞机和/或代表在相应的预测日期上的至少一个航空电子系统的操作，预测日期在参考日期之后，由预测模块计算的至少一个投影取决于由另一个计算的至少一个其他投影 预测模块。

公开(公告)号：US11536570B2

公开(公告)日：2022-12-27

申请号：US16719409

申请日：2019-12-18

Applicant: THALES

Inventor： Nicolas Rossi ,  Benoît Dacre-Wright ,  Cédric D'Silva

IPC: G01C21/20 ,  G08G5/00 ,  G08G5/02

Abstract: A method for determining an optimized trajectory to be followed by an aircraft, the method being implemented by a determining system of the aircraft and comprising: a first step for acquiring at least one constraint relative to at least one parameter of the trajectory to be followed, the constraint being determined by a control system of a remote station as a function of the air traffic and/or the aircraft mission; a step for calculating a desired trajectory as a function of the constraint; a step for transmitting the desired trajectory to the remote station; a second step for acquiring an instruction comprising an authorization to follow the desired trajectory or a refusal of the desired trajectory.

公开(公告)号：US10360802B2

公开(公告)日：2019-07-23

申请号：US15684155

申请日：2017-08-23

Applicant: Thales

Inventor： Cédric D'Silva ,  Jérôme Sacle ,  Nicolas Rossi

IPC: G05D1/10 ,  G08G5/00

Abstract: An aid method for piloting an aircraft including acquiring an instruction intended to alter the flight plan, determining an applicability period of the instruction made up of a plurality of applicability moments of the instruction in which the application of the instruction is compatible with the operational capabilities of the aircraft and with the constraints of the flight plan, for each applicability moment of the instruction, determining an altered flight plan in case of application of the instruction at this applicability moment and calculating values of the operational parameters associated with this flight plan, and selecting an optimal applicability moment based on values of the operational parameters associated with the altered flight plan and operational parameters associated with the current flight plan.

公开(公告)号：US10117260B2

公开(公告)日：2018-10-30

申请号：US15134135

申请日：2016-04-20

Applicant: THALES

Inventor： Fany Barailler ,  Nicolas Rossi ,  Antoine Lacombe

IPC: H04W72/10 ,  H04B7/185 ,  G08G5/00

Abstract: A method and system for communicating and sharing information for an aircraft are disclosed. In one aspect, the method includes identifying a situation from among a set of predetermined situations and obtaining, from a data structure recorded beforehand, a first set of information elements associated with the identified situation. The method also includes determining, from the first set of information elements, and from pieces of information recorded beforehand, a set of pieces of information unavailable in the first system and establishing at least one first request to be sent from the first system to at least one second system. The method further includes sending the at least one first request from the first system to the at least one second system.

公开(公告)号：US20150142221A1

公开(公告)日：2015-05-21

申请号：US14540756

申请日：2014-11-13

Applicant: THALES

Inventor： Francois Coulmeau ,  Arnaud Bonnafoux ,  Nicolas Rossi

IPC: G01C21/00 ,  G01S13/95 ,  G08G5/04

CPC classification number: G01C21/00 ,  G01S13/953 ,  G05D1/101 ,  G08G5/0034 ,  G08G5/0052 ,  G08G5/04

Abstract: A method for determining a result path of an aircraft, the result path including a set of successive positions of the aircraft between an initial global point and a final global point that are predetermined for a mission of the aircraft is provided.The aircraft includes a plurality of calculating members, each able to guide the aircraft during at least part of the mission and to calculate an elementary path of the aircraft during that part, each elementary path including a set of successive positions of the aircraft between an initial elementary point and a final elementary point.The device includes calculating a portion of the result path from elementary paths coming from at least two distinct calculating members.

Abstract translation: 提供了一种用于确定飞行器的结果路径的方法，所述结果路径包括飞行器在为飞行器的任务预定的初始全局点和最终全局点之间的连续位置的集合。 飞行器包括多个计算构件，每个计算构件能够在至少部分任务期间引导飞行器，并且在该部分期间计算飞行器的基本路径，每个基本路径包括飞行器在初始位置之间的连续位置的集合 基本点和最终基本点。 该装置包括从至少两个不同的计算部件的基本路径计算结果路径的一部分。