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    QUALITY OF SERVICE OF A FLIGHT MANAGEMENT SYSTEM
    2.
    发明申请
    QUALITY OF SERVICE OF A FLIGHT MANAGEMENT SYSTEM 审中-公开
    飞行管理系统的服务质量

    公开(公告)号：US20160182687A1

    公开(公告)日：2016-06-23

    申请号：US14975135

    申请日：2015-12-18

    Applicant: THALES

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

    IPC: H04L29/06 ,  H04L12/24 ,  H04L29/08

    CPC classification number: H04L67/42 ,  G06F9/54 ,  G06F2209/541 ,  H04L41/14 ,  H04L67/10 ,  H04L67/32

    Abstract: A method implemented by computer in or for a flight management system or FMS, comprises the steps of receiving requests issued by clients; determining a correspondence between the requests and predefined unitary services executable by at least one server associated with the FMS; queuing the unitary services determined in one or more queues; determining a response time associated with each request; and notifying at least one client of the response time to its request. Developments describe the processing of queues, the management of priorities, the existence of fixed-price contracts, caching mechanisms, interruptions of queues, cancellations of requests, voting mechanisms, etc. The unitary services in particular can be avionics services of ATA (Air Transport Association) type. Systems aspects and software aspects are described.

    Abstract translation: 由计算机在飞行管理系统或飞行管理系统中实施的方法包括以下步骤：接收由客户发出的请求; 确定所述请求与由至少一个与所述FMS相关联的服务器可执行的预定单位服务之间的对应关系; 排队在一个或多个队列中确定的统一服务; 确定与每个请求相关联的响应时间; 并通知至少一个客户端对其请求的响应时间。 发展描述了队列的处理，优先级的管理，固定价格合同的存在，缓存机制，队列中断，请求的取消，投票机制等。单一服务特别可以是ATA（航空运输）的航空电子服务 协会）类型。 描述系统方面和软件方面。

    TACTILE INTERFACE FOR THE FLIGHT MANAGEMENT SYSTEM OF AN AIRCRAFT
    3.
    发明申请
    TACTILE INTERFACE FOR THE FLIGHT MANAGEMENT SYSTEM OF AN AIRCRAFT 审中-公开
    飞机飞行管理系统的触觉界面

    公开(公告)号：US20160103579A1

    公开(公告)日：2016-04-14

    申请号：US14879796

    申请日：2015-10-09

    Applicant: THALES

    Inventor： François COULMEAU ,  Frédéric BONAMY ,  Patrick MAZOYER

    IPC: G06F3/0488 ,  G06T19/00 ,  G08G5/00 ,  G06F3/0484

    CPC classification number: G06F3/0488 ,  G01C21/00 ,  G01C23/00 ,  G06F3/0484 ,  G06F3/04842 ,  G06T19/006 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/0047 ,  G08G5/0052

    Abstract: A graphic interaction method for piloting an aircraft, comprises receiving an indication of an object selected on a display screen of the aircraft; determining one or more flight plan revisions of the aircraft associated with the selected object and displaying one or more of said flight plan revisions; receiving an indication of selection of a displayed revision; determining a revision type associated with the revision displayed and selected; and as a function of the revision type determined, displaying a tactile interface data entry graphic symbol. Developments notably concern the symbology used, the validation or the modification of a selected revision, the taking account of the flight context, the taking account of the speed of manipulation of the tactile interface, etc. System and software aspects are described. In particular, the human-machine interface may be exclusively of tactile type.

    Abstract translation: 一种用于驾驶飞行器的图形交互方法，包括接收在飞行器的显示屏上选择的对象的指示; 确定与所选对象相关联的飞机的一个或多个飞行计划修订，并显示所述飞行计划修订中的一个或多个; 接收对所显示的修订的选择的指示; 确定与显示和选择的修订相关联的修订类型; 并且根据确定的修订类型的函数，显示触觉界面数据条目图形符号。 发展特别涉及所使用的符号系统，所选修订的验证或修改，考虑到飞行情境，考虑到触觉界面的操纵速度等。系统和软件方面被描述。 特别地，人机界面可以仅仅是触觉类型。

    Onboard edge computation device, associated electronic system and method for executing software applications
    4.
    发明公开
    Onboard edge computation device, associated electronic system and method for executing software applications 审中-公开

    公开(公告)号：US20240211313A1

    公开(公告)日：2024-06-27

    申请号：US18542715

    申请日：2023-12-17

    Applicant: THALES

    Inventor： Sébastien RAZE ,  François COULMEAU ,  Bruno CAPELLE ,  Yannick LE ROUX ,  Pierre MARIANI

    IPC: G06F9/50

    CPC classification number: G06F9/5027

    Abstract: An edge computation device on board an aircraft is configured for communicating with one or a plurality of onboard electronic devices having certified operation, and with at least one remote computation system. Same includes local computational resources, and is configured for implementing a management module for a plurality of software applications suitable for providing at least one control parameter and/or receiving at least one datum from at least one onboard electronic device, a module for activating the execution of at least one of the stored software applications, a management module for an execution stack, configured for determining, for each software application to be executed, an allocation of local computation resources and, where appropriate, for executing locally a first part of the application, and for requesting remote execution, by means of the remote computation system, of a second part of the application to be executed.

    DISTRIBUTED LEDGERS FOR THE MANAGEMENT OF THE LIFECYCLE OF DATA IN AERONAUTICS
    5.
    发明申请
    DISTRIBUTED LEDGERS FOR THE MANAGEMENT OF THE LIFECYCLE OF DATA IN AERONAUTICS 审中-公开

    公开(公告)号：US20200304290A1

    公开(公告)日：2020-09-24

    申请号：US16817516

    申请日：2020-03-12

    Applicant: THALES

    Inventor： François COULMEAU ,  Dorian MARTINEZ ,  Guillaume PABIA

    IPC: H04L9/06 ,  G06F21/60 ,  H04L9/08 ,  H04L9/30 ,  H04L9/00 ,  G06F16/27

    Abstract: Computer-implemented methods and systems for managing the lifecycle of aeronautical data stored in a blockchain, include steps of receiving or sending aeronautical data, and encrypting and/or decrypting these data using a smart contract. The use of a plurality of blockchains, and the facts and rules of management of the lifecycle of the data (e.g. programmed obsolescence, time-dependent quality indicator, etc.) are described. Transactional aspects; the use of oracle services; asymmetric, homomorphic and post-quantum encryption methods; the use of chameleon hash functions, so as to manipulate at least partially redactable blockchains; and machine-learning techniques, are in particular described with respect to a number of embodiments. Software and system aspects are described.

    MACHINE LEARNING FOR MISSION SYSTEM
    6.
    发明申请
    MACHINE LEARNING FOR MISSION SYSTEM 有权

    公开(公告)号：US20210103295A1

    公开(公告)日：2021-04-08

    申请号：US17039055

    申请日：2020-09-30

    Applicant: THALES

    Inventor： Ludovic BILLAULT ,  François COULMEAU

    IPC: G05D1/10 ,  G06N3/04 ,  G06N3/08 ,  G08G5/00

    Abstract: A method and devices for machine learning applied to the mission trajectories of an aircraft are provided. Learning data comprise mission trajectories determined by an MMS mission computer and the corresponding avionic trajectories, such as those determined by certified avionic systems. Developments describe in particular steps of evaluation, e.g. use of cost function or mission score, optimization of the mission trajectories by means of evolutionary, in particular genetic, methods, the use of fuzzy logic, the display of intermediate results or other things for explanatory purposes. Software and hardware aspects (e.g. neural networks) are described.

    METHOD OF COMPUTING AIRCRAFT TRAJECTORY SUBJECT TO LATERAL AND VERTICAL CONSTRAINTS
    8.
    发明申请
    METHOD OF COMPUTING AIRCRAFT TRAJECTORY SUBJECT TO LATERAL AND VERTICAL CONSTRAINTS 有权
    计算横向和纵向约束的飞机轨道的方法

    公开(公告)号：US20160163201A1

    公开(公告)日：2016-06-09

    申请号：US14958068

    申请日：2015-12-03

    Applicant: THALES

    Inventor： Mathieu LE MERRER ,  Benoit DACRE-WRIGHT ,  François COULMEAU

    IPC: G08G5/00

    CPC classification number: G08G5/003 ,  G05D1/0005 ,  G06Q10/047 ,  G08G5/0034

    Abstract: The present invention relates to a method for computing a setpoint trajectory of an aircraft comprising at least two subsets. It is characterized in that it comprises the formulation and the solving of an optimization problem for the trajectory, and that the formulation of the said problem comprises at least the formulation of a constraint related to a transition of legs on at least one first subset of the trajectory, and the formulation of a constraint related to a transition of vertical flight phases on at least one second subset of the trajectory. The invention also relates to a system and a computer program for the computation of a trajectory.

    Abstract translation: 本发明涉及一种用于计算包括至少两个子集的飞机的设定轨迹的方法。 其特征在于，其包括对轨迹的优化问题的公式和求解，并且所述问题的公式至少包括与腿的至少一个第一子集上的腿的转变有关的约束的公式 轨迹，以及与轨迹的至少一个第二子集上的垂直飞行相位的转变有关的约束的公式。 本发明还涉及用于计算轨迹的系统和计算机程序。

    METHOD FOR THE REAL TIME CALCULATION OF A PLANNED TRAJECTORY, NOTABLY OF A FLIGHT PLAN, COMBINING A MISSION, AND SYSTEM FOR MANAGING SUCH A TRAJECTORY
    9.
    发明申请
    METHOD FOR THE REAL TIME CALCULATION OF A PLANNED TRAJECTORY, NOTABLY OF A FLIGHT PLAN, COMBINING A MISSION, AND SYSTEM FOR MANAGING SUCH A TRAJECTORY 有权
    用于实际计算计划的轨道的方法，飞行计划的不限于组合任务的方法和用于管理这种轨道的系统

    公开(公告)号：US20160078769A1

    公开(公告)日：2016-03-17

    申请号：US14852316

    申请日：2015-09-11

    Applicant: THALES

    Inventor： François COULMEAU ,  Laurent DEWEERDT

    IPC: G08G5/00

    CPC classification number: G08G5/0034 ,  G01C21/20 ,  G01C23/00 ,  G08G5/0021 ,  G08G5/003 ,  G08G5/0039

    Abstract: The trajectory coming from a planned trajectory, managed by a system, and from at least one trajectory section sent by a third party system to the system, the method at least comprises: a preliminary step in which a knowledge base is produced comprising the calculation parameters and their field of use for the moving object, several envelopes of parameters being defined within the field of use corresponding to different operational constraints of the moving object; a first step in which the system initializes the planned trajectory according to the parameters of the preliminary step, the calculation parameters of the planned trajectory being contained in one of the envelopes; a second step in which the system receives a trajectory section sent by the third party system in order to be inserted in the planned trajectory by replacing a part of the trajectory; a third step in which the received and accepted section is simplified by segmentation in such a way that its calculation parameters are contained in the at least one of the envelopes; the system carrying out calculations on the basis of the simplified trajectory.

    Abstract translation: 来自计划轨迹的轨迹，由系统管理，以及由第三方系统发送到系统的至少一个轨迹部分，该方法至少包括：初步步骤，其中产生包括计算参数的知识库 及其运动对象的使用领域，在与运动对象的不同操作约束对应的使用领域内定义了若干参数包络; 系统根据预备步骤的参数初始化计划轨迹的第一步，计划轨迹的计算参数包含在一个信封中; 第二步骤，系统接收由第三方系统发送的轨迹部分，以便通过替换轨迹的一部分来插入到计划的轨迹中; 第三步骤，其中接收和接受部分通过分割被简化，使得其计算参数包含在所述至少一个信封中; 该系统在简化轨迹的基础上进行计算。

    Method and System for Monitoring Aircraft Flight Phase on Approach to a Runway
    10.
    发明申请
    Method and System for Monitoring Aircraft Flight Phase on Approach to a Runway 有权
    用于监控飞机飞行阶段对跑道进近的方法和系统

    公开(公告)号：US20140343764A1

    公开(公告)日：2014-11-20

    申请号：US14275057

    申请日：2014-05-12

    Applicant: THALES

    Inventor： Jérôme SACLE ,  François COULMEAU ,  Loïc CHARLES

    IPC: B64D45/04

    CPC classification number: B64D45/04 ,  G05B19/416 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/025

    Abstract: The method concerns monitoring the approach phase of an aircraft to a runway. This method includes determining successive gateways of the aircraft relative to at least one characteristic point of an approach flight plan of the aircraft or relative to the landing location, and measuring the aircraft speed upon crossing a given gateway. The method further comprises computing a minimum deceleration distance up to a predetermined target speed associated with the gateway following said given gateway, the minimum deceleration distance being an estimated flight distance corresponding to the speed reduction of the aircraft from the measured speed to said target speed; comparing the computed minimum deceleration distance with the distance remaining to be flow to the following gateway; and generating an alert, intended for the aircraft crew, when the distance remaining to be flown to the following gateway is smaller than the computed minimum deceleration distance.

    Abstract translation: 该方法涉及监视飞机进入跑道的进近阶段。 该方法包括相对于飞机的接近飞行计划或相对于着陆位置的至少一个特征点来确定飞行器的连续网关，以及在穿过给定的网关时测量飞机的速度。 该方法进一步包括：计算与所述给定网关之后的与所述网关相关联的预定目标速度的最小减速距离，所述最小减速距离是对应于所述飞行器从所述测量速度到所述目标速度的速度降低的估计飞行距离; 将计算出的最小减速距离与要流向下一个网关的距离进行比较; 并且当剩余的飞行到以下网关的距离小于所计算的最小减速距离时，产生针对飞行员的警报。

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