公开(公告)号：US20150338237A1

公开(公告)日：2015-11-26

申请号：US14717993

申请日：2015-05-20

申请人： THALES

发明人： Frederic BONAMY ,  Francois COULMEAU ,  Celia EBRARD

IPC分类号： G01C23/00

CPC分类号： G01C23/005 ,  G08G5/0021

摘要： A method implemented by computer for the display of information relating to the flight of an aircraft comprises receiving indication of a selection of an arbitrary display zone on a screen of an onboard computer of the aircraft; and reconfiguring the display, in response to the indication. Developments describe several geometric transformations, various display reconfigurations (e.g. centring of the display), the use of systems third party to the aircraft (e.g. taxiing computer, ground client, maintenance, terrain monitoring, traffic, weather), associated operations of revisions of the flight plan, the use of display rules (notably associated with the flight situation), and the emergency deactivation of the display reconfigurations. Computer programs and associated systems are also described (notably Man-System Interface, virtual and/or augmented reality).

摘要翻译： 由计算机实现的用于显示与飞机的飞行有关的信息的方法包括在飞行器的机载计算机的屏幕上接收任意显示区域的选择的指示; 以及响应于所述指示重新配置所述显示器。 发展描述几种几何变换，各种显示重新配置（例如显示器的中心），系统第三方对飞机的使用（例如滑行计算机，地面客户端，维护，地形监测，交通，天气），相关操作的修订 飞行计划，使用显示规则（特别是与飞行情况相关联），以及显示重新配置的紧急停用。 还描述了计算机程序和相关系统（特别是人机界面，虚拟和/或增强现实）。

公开(公告)号：US20130238174A1

公开(公告)日：2013-09-12

申请号：US13789595

申请日：2013-03-07

申请人： THALES

发明人： Emmanuel DEWAS ,  Vincent SAVARIT ,  Francois COULMEAU

IPC分类号： G05D1/06

CPC分类号： G05D1/0676 ,  G05D1/101

摘要： In the field of the calculation of the approach trajectory of an aircraft, and relating to a method for determining a corrected lateral approach trajectory as a function of the energy to be reabsorbed before the landing, and also to a flight management system making it possible to determine the corrected lateral trajectory, a method comprises: determining an energy of the aircraft Eaero upon crossing the runway threshold on the basis of a predetermined approach trajectory and of a current state of the aircraft, said state comprising at least one current altitude, a current ground speed and a mass of the aircraft; comparing the energy Eaero with a predetermined maximum energy Emax, and when the energy Eaero is greater than the energy Emax, determining the corrected lateral approach trajectory as a function of the difference between the energy of the aircraft Eaero and the maximum energy Emax.

摘要翻译： 在计算飞行器的进场轨迹的领域中，涉及一种用于确定作为在着陆之前要被吸收的能量的函数的校正的横向进场轨迹的方法，并且还涉及一种飞行管理系统， 确定校正的横向轨迹，方法包括：基于预定的进场轨迹和飞行器的当前状态，在越过跑道阈值时确定飞机Eaero的能量，所述状态包括至少一个当前高度，当前高度 地面速度和飞机的质量; 将能量Eaero与预定的最大能量Emax进行比较，并且当能量Eaero大于能量Emax时，确定作为飞行器Eaero的能量与最大能量Emax之间的差异的函数的校正的横向进场轨迹。

公开(公告)号：US20150334173A1

公开(公告)日：2015-11-19

申请号：US14696132

申请日：2015-04-24

申请人： THALES

发明人： Francois COULMEAU ,  Laurent CASTET ,  Laurent DEWEERDT ,  Frederic SANCHEZ

IPC分类号： H04L29/08 ,  G06F9/48 ,  H04L29/06

CPC分类号： H04L67/10 ,  G06F9/4881 ,  G06F9/4887 ,  H04L67/42

摘要： A system executes services by a “server” for a “client”. A preliminary step establishes a list of available services of the server, set up for the client, in which a processing time is determined releasable by the server for the client per code execution cycle MIF. The system creates on start-up: NT execution tasks for the client, each having a priority of execution level and an allocated average duration of execution, NT being at least 1, the sum of durations of the tasks being at most the releasable processing time; execution rules associating each of the tasks with at least one service of the list; then, during each MIF cycle, the system executes the services on their associated tasks, a task executed by priority and for at most its allocated average time of execution, the non-executed part of a service being executed on its associated task in the next cycle.

摘要翻译： 系统通过“服务器”为“客户端”执行服务。 初步步骤建立服务器的可用服务列表，为客户端设置，其中服务器为客户端每代码执行周期MIF确定可释放的处理时间。 系统在启动时创建：NT执行任务，每个执行任务具有执行级别的优先级和分配的平均执行持续时间，NT至少为1，任务持续时间的总和最多为可释放处理时间 ; 执行规则将每个任务与列表的至少一个服务相关联; 那么，在每个MIF周期期间，系统在其相关任务执行服务，按优先级执行的任务，并且至多为其分配的平均执行时间，在下一个执行的相关任务上执行的服务的非执行部分 周期。

公开(公告)号：US20150120095A1

公开(公告)日：2015-04-30

申请号：US14521239

申请日：2014-10-22

申请人： THALES

发明人： Francois COULMEAU ,  Jerome SACLE ,  Johan BOYER

IPC分类号： G05D1/00 ,  G08G5/00

CPC分类号： G05D1/00 ,  G01C23/00 ,  G05D1/042 ,  G05D1/0676 ,  G05D1/101 ,  G08G5/0021 ,  G08G5/003 ,  G08G5/0052 ,  G08G5/025 ,  Y02T50/84

摘要： A method is provided for managing the flight of an aircraft flying a trajectory calculated by a flight management system. The trajectory necessitates at least one transition between two different aerodynamic configurations of the aircraft. The method comprises: extraction of performance data of the aircraft from a database, at least one item of performance data being a function of an aerodynamic configuration, selection between a first determination step and a second determination step, a step of determination of a start point and of an end point of the transition between two aerodynamic configurations and engine speeds of an aircraft during a flight, the determination step being implemented by the flight management system and chosen from among the first and second determination steps, the determination step calculating the trajectory by numerical integration of the equations representative of the dynamics of the aircraft making use of the performance data of the aircraft.

摘要翻译： 提供了一种用于管理飞行由飞行管理系统计算的轨迹的飞行器的飞行的方法。 轨迹必须在飞行器的两种不同的空气动力学构型之间进行至少一个过渡。 该方法包括：从数据库中提取飞行器的性能数据，作为空气动力学配置的函数的至少一个性能数据项，第一确定步骤和第二确定步骤之间的选择，确定起始点的步骤 以及在飞行期间飞行器的两种空气动力学构型和发动机速度之间的转变的终点，所述确定步骤由飞行管理系统实施并且从第一和第二确定步骤中选择，所述确定步骤通过以下步骤计算轨迹： 代表使用飞机性能数据的飞机动力学的方程的数值积分。

公开(公告)号：US20130317739A1

公开(公告)日：2013-11-28

申请号：US13900215

申请日：2013-05-22

申请人： THALES

发明人： Francois COULMEAU ,  Guy DEKER ,  Xavier BLANCHON ,  Patrick MAZOYER

IPC分类号： G05D1/10

CPC分类号： G05D1/101 ,  G08G5/0039

摘要： A device and method for flight management of an aircraft along a flight plan comprises a plurality of waypoints comprising a computation of the temporal predictions determining the temporal situation of the aircraft for each waypoint of the flight plan, a temporal situation of the aircraft being defined by at least one set of information from among the group comprising the target time of transit at each waypoint the estimated minimum and maximum times of arrival at each waypoint, the estimated time of transit at the waypoint, and a formatting and display simultaneously presenting the temporal situations of the said plurality of waypoints

摘要翻译： 一种沿着飞行计划的飞行器的飞行管理的装置和方法包括多个航路点，其包括对飞行计划的每个航路点确定飞机的时间状态的时间预测的计算，飞行器的时间情况由 包括在每个航路点的目标传输时间的组中的至少一组信息，估计在每个航路点的最小和最大到达时间，在航路点的过境估计时间以及同时呈现时间情况的格式化和显示 的所述多个航路点

公开(公告)号：US20130317737A1

公开(公告)日：2013-11-28

申请号：US13767471

申请日：2013-02-14

申请人： THALES

发明人： Emmanuel DEWAS ,  Vincent SAVARIT ,  Francois COULMEAU

IPC分类号： G01C21/00

CPC分类号： G01C21/00 ,  G08G5/003 ,  G08G5/0034 ,  G08G5/0039 ,  G08G5/006

摘要： A method and device for determining a shifted circular segment on the basis of an initial circular segment, the shifted circular segment being shifted by a shift distance, the method being implemented by a computer dedicated to flight management, comprises: determining a shifted final point terminating a shifted circular segment, on the basis of the final point terminating the initial circular segment, through a shift of the final point determined on the basis of the shift distance and in the direction of shift, through the use of a straight line passing through the centre of the initial circular segment and the final point of the initial circular segment, and determining a shifted circular segment on the basis of the initial circular segment by construction of a circular segment between the shifted final point associated with the preceding shifted segment and the shifted final point associated with the shifted segment.

摘要翻译： 一种用于基于初始圆形段确定偏移的圆形段的方法和装置，所述偏移的环形段被偏移了移动距离，该方法由专用于飞行管理的计算机实现，包括：确定移位的最终点终止 基于最终点终止初始圆形段的移动圆形段，通过使用通过所述移动距离的直线，基于移动距离和移动方向确定的最终点的移动 初始圆形段的中心和初始圆形段的最终点，并且基于初始圆形段通过在与前一移位段相关联的移位的最终点之间构造一个圆形段来确定移位的圆形段，并且移位 与转移段相关联的最终点。

公开(公告)号：US20150187148A1

公开(公告)日：2015-07-02

申请号：US14565871

申请日：2014-12-10

申请人： THALES

发明人： Christian SANNINO ,  Xavier CHAZOTTES ,  Francois COULMEAU

IPC分类号： G07C5/08 ,  B64D45/00

CPC分类号： G07C5/0808 ,  B64D45/00 ,  B64D2045/0085 ,  G05B23/0286 ,  G06F11/0739 ,  G06F11/0784 ,  G07C5/0841

摘要： A device and method for assisting with reconfiguration of an aircraft, an aircraft including such a device and an associated computer program product are disclosed. In one aspect, the aircraft has an operational configuration, is configured to move in an operational environment, and includes at least one avionic system, at least one avionic member, and at least one monitoring system configured to detect an abnormality of an avionic member or a perturbation of the operational environment and to generate a fault information. The device is connected between at least one monitoring system and at least one avionic system, and includes a reception module configured to receive a fault information from the monitoring system, an impact computation module configured to compute an impact on the operational configuration of the aircraft, and a transmission module configured to transmit the computed impact to at least one avionic system.

摘要翻译： 公开了一种用于辅助重新配置飞行器的装置和方法，包括这种装置的飞机和相关联的计算机程序产品。 一方面，飞行器具有操作配置，被配置为在操作环境中移动，并且包括至少一个航空电子系统，至少一个航空电子部件和被配置为检测航空电子部件的异常的至少一个监视系统，或者 操作环境的扰动并产生故障信息。 该设备连接在至少一个监控系统和至少一个航空电子系统之间，并且包括被配置为从监控系统接收故障信息的接收模块，被配置为计算对飞行器的操作配置的影响的冲击计算模块， 以及传输模块，被配置为将所计算的冲击传递到至少一个航空电子系统。

公开(公告)号：US20150120100A1

公开(公告)日：2015-04-30

申请号：US14522469

申请日：2014-10-23

申请人： THALES

发明人： Jerome SACLE ,  Johan BOYER ,  Francois COULMEAU

IPC分类号： G05D1/00 ,  G08G5/00 ,  G05D1/04

CPC分类号： G05D1/00 ,  G01C21/20 ,  G01C23/00 ,  G05D1/0005 ,  G05D1/042 ,  G05D1/0676 ,  G06Q10/047 ,  G08G5/003 ,  G08G5/006 ,  G08G5/0095 ,  G08G5/025 ,  Y02T50/84

摘要： A method for aiding navigation for an aircraft between a descent start point and a computation end point, comprises the computation steps of: collecting a flight plan consisting of a succession of waypoints and of the associated vertical constraints; determining a corridor consisting of a floor trajectory and of a ceiling trajectory defining the minimum and maximum altitudes permitted to the aircraft; splitting the corridor into several cells defined between two waypoints furthest apart and between which the ceiling trajectory is distinct from the floor trajectory; determining for at least one cell a vertical trajectory complying with the altitude constraints and comprising the longest possible IDLE segment; and a step consisting in determining and displaying maneuvering points of the aircraft making it possible to follow the target vertical trajectory.

摘要翻译： 一种用于帮助航空器在下降起点和计算终点之间的导航的方法包括以下计算步骤：收集由一系列航路点和相关垂直约束组成的飞行计划; 确定由地板轨迹和限定飞机允许的最小和最大高度的天花板轨迹组成的走廊; 将走廊拆分成两个距离最远的两个航点之间定义的几个单元，天花板轨迹与地板轨迹不同; 为至少一个小区确定符合所述高度约束的垂直轨迹并且包括所述最长可能的空闲段; 并且包括确定和显示飞行器的机动点的步骤，使得可以跟随目标垂直轨迹。

公开(公告)号：US20140172204A1

公开(公告)日：2014-06-19

申请号：US14105012

申请日：2013-12-12

申请人： THALES

发明人： Francois COULMEAU ,  Guy DEKER ,  Patrick MAZOYER

IPC分类号： B64D45/00 ,  G08G5/00

CPC分类号： B64D45/00 ,  G01C23/005 ,  G08G5/0039

摘要： A method and a device is provided for supplying, in summary fashion on a single page of a screen for each point, the data relating to a flight plan. The method makes it possible to establish relevant groups of information according to the situation of the flight and to summarize the display of the data in folded-up mode or in an unfolded lateral mode. The unfolded display offers, on one and the same page, a more precise detail of the situation, by ergonomically and intuitively showing in the columns the predictions in relation to a type of constraint.

摘要翻译： 提供了一种方法和装置，用于以概括方式在每个点的屏幕的单页上提供与飞行计划相关的数据。 该方法使得可以根据飞行情况建立相关信息组，并且以折叠模式或展开横向模式总结数据的显示。 展开的显示器在同一页面上提供了一个更精确的情况细节，通过人体工程学和直观地在列中显示了与一种约束类型相关的预测。

公开(公告)号：US20140012436A1

公开(公告)日：2014-01-09

申请号：US13934854

申请日：2013-07-03

申请人： THALES

发明人： Francois COULMEAU ,  Xavier BLANCHON ,  Christophe PIERRE

IPC分类号： B64C19/00

CPC分类号： B64C19/00 ,  G05D1/0607 ,  G05D1/101 ,  G08G5/0021 ,  G08G5/0034

摘要： A method for aiding navigation is provided, implemented in a flight management system, for the construction of a vertical trajectory of an aircraft following a predetermined lateral trajectory between a departure point and an arrival point; the departure point and arrival point furthermore being characterized by predefined altitudes, respectively Hd and Ha, and predefined speeds, respectively Vd and Va. The method comprises the steps of: selection of a transition manoeuvre in terms of altitude and speed from a predetermined list of manoeuvres; determination of a manoeuvre point PM on the lateral trajectory, of altitude Hd and of speed Vd, from which the transition manoeuvre must be initiated so as to allow the aircraft to reach at the arrival point the predefined speed Va and the predefined altitude Ha.

摘要翻译： 提供了一种在飞行管理系统中实现的用于辅助导航的方法，用于在出发点和到达点之间的预定横向轨迹之后构建飞机的垂直轨迹; 出发点和到达点的特征还在于预定的高度，分别为Hd和Ha，以及预定速度，分别为Vd和Va。该方法包括以下步骤：从高度和速度的预定列表中选择过渡机动 机动 确定侧向轨迹上的机动点PM，高度Hd和速度Vd，从其开始转换机动，以允许飞机在到达点到达预定速度Va和预定高度Ha。