公开(公告)号：US20240038078A1

公开(公告)日：2024-02-01

申请号：US18268728

申请日：2021-12-21

申请人： THALES

发明人： Vincent SAVARIT ,  Bertrand CAUDRON ,  Guy DEKER

IPC分类号： G08G5/00

CPC分类号： G08G5/006 ,  G08G5/0052 ,  G08G5/0008

摘要： A method and device for assisting a pilot in flight management is provided, by enabling the pilot to anticipate situations involving a risk of collision with another aircraft or with the ground, or to anticipate a risk of deviation from a flight path.

公开(公告)号：US20190088143A1

公开(公告)日：2019-03-21

申请号：US15528455

申请日：2015-12-28

申请人： THALES

发明人： Guy DEKER ,  Michel ROGER ,  Vincent SAVARIT

IPC分类号： G08G5/00 ,  G01C21/20

摘要： A method for automatically calculating a trajectory for an aircraft to re-join a reference route of the aircraft executed iteratively, in particular when the aircraft is no longer locked onto its reference route, each iteration comprising a step of detection of deviation from the active segment of the route; if the deviation from the active segment of the route is detected, the method comprises a step of selection of a route segment to be re-joined, a step of calculation of a re-joining trajectory between a starting point and the route segment to be re-joined, and a step of validation of the trajectory of the route segment to be re-joined. Where this trajectory is validated, the method comprises a step of assignment of the re-joining trajectory for the segment to the re-joining trajectory for the route. Otherwise, it comprises a step of verification of the existence of a next route segment fulfilling a selection condition. If a next route segment fulfils a selection condition, it comprises a step of selection of the next route segment as route segment to be re-joined, and a return to the step of calculation of a re-joining trajectory for the route segment to be re-joined. If no route segment fulfils the selection condition, it comprises a step of application of an exit procedure. A computer program for implementing this method is provided.

公开(公告)号：US20200174502A1

公开(公告)日：2020-06-04

申请号：US16700790

申请日：2019-12-02

申请人： THALES

发明人： Michel ROGER ,  Adrien DE JAUREGUIBERRY ,  Guy DEKER

IPC分类号： G05D1/10 ,  B64C39/02

摘要： Automatic flight information determination device for automatically determining flight control information for an accompanying mobile machine accompanying a leader mobile machine, the said device being adapted for collecting the data pertaining to location of the leader mobile machine from among the data pertaining to the actual location derived from measurements relating to the current location of the leader mobile machine and the pertaining to the current trajectory of the accompanying mobile machine, and of determining, o the basis of the said location data collected, the information items for piloting the accompanying mobile machine as a function of a set of at least two values to be adhered to with respect to the location defined by the data collected, the said values to be adhered to being representative of the values included among: a minimum vertical/flight level separation value, a minimum longitudinal/along track separation value, and a minimum lateral/between tracks separation value.

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：US20180276999A1

公开(公告)日：2018-09-27

申请号：US15919630

申请日：2018-03-13

申请人： THALES

发明人： Benoit DACRE-WRIGHT ,  Didier POISSON ,  Guy DEKER ,  Vincent SAVARIT

IPC分类号： G08G5/00

CPC分类号： G08G5/0039 ,  G01C21/00 ,  G08G5/0021 ,  G08G5/0052

摘要： A method is provided for adjusting a flight plan rejoining trajectory of an aircraft, the method being implemented in a flight management system of the aircraft. In a first step, the rejoining trajectory comprises a guidance setpoint holding point to be reached situated in the extension of a guidance setpoint, and set manually or automatically, the guidance setpoint no longer being necessarily maintained when this setpoint holding point is passed. This first step can be preceded by a step of rejoining a guidance setpoint or a step of searching for the intersection of the current guidance setpoint trajectory with a segment of the flight plan.

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：US20240363011A1

公开(公告)日：2024-10-31

申请号：US18578668

申请日：2022-07-22

申请人： THALES

发明人： Michel ROGER ,  Pascal RIVES ,  Jérôme SACLE ,  Guy DEKER

IPC分类号： G08G5/00

CPC分类号： G08G5/0039 ,  G08G5/0017

摘要： A method for managing speed constraints of a flight plan of an aircraft, the method includes the following steps: identifying a current flight phase, determining CAS speed profile, the speed profile establishing a behavior of the aircraft with respect to a speed setpoint, determining a Mach speed profile, the Mach speed profile establishing a behavior of the aircraft with respect to a Mach setpoint, the Mach setpoint being a speed setpoint transcribed into an equivalent Mach number, determining a Cross-Over altitude, the Cross-Over altitude being an altitude of transition from an automatic control of the aircraft according to the CAS speed profile to an automatic control according to the Mach speed profile, determining an end-of-applicability criterion of the speed profile and of the Mach speed profile.

公开(公告)号：US20220406198A1

公开(公告)日：2022-12-22

申请号：US17776545

申请日：2020-10-27

申请人： THALES

发明人： Jérôme SACLE ,  François TERREE ,  Guy DEKER

IPC分类号： G08G5/00

摘要： A management of the elements of the context of one or more flight plans is provided. The systems, methods and computer programs allowing real-time collaborative work on and around one or more flight plans between multiple remote systems are provided. A first system comprises receiving a modification, made on a second system, to a flight plan and to a set of associated objects or to another set of non-associated objects, displaying the modification and, if the modification is validated, returning the modification, as applied to the first system, to the second system to ensure uniformity around the collaborative navigation space between remote parties.

公开(公告)号：US20150262490A1

公开(公告)日：2015-09-17

申请号：US14627645

申请日：2015-02-20

申请人： THALES

发明人： Guy DEKER ,  Michel ROGER ,  Bruno AYMERIC

IPC分类号： G08G5/00

CPC分类号： G08G5/0039 ,  G05D1/101 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0047 ,  G08G5/0052 ,  G08G5/0095

摘要： A method and system, for flight management of an aircraft flying on a trajectory shifted with respect to a flight plan comprising a plurality of constrained waypoints, comprises a step of determining and displaying at least one point of the trajectory, termed decision point, beyond which the aircraft can no longer rejoin a constrained waypoint of the flight plan by determining a point of intersection between the trajectory and a rejoining trajectory steering towards the selected constrained waypoint, the rejoining trajectory complying with at least one predefined criterion.

摘要翻译： 一种用于对在相对于包括多个受限航路点的飞行计划移动的轨迹上飞行的飞行器的飞行管理的方法和系统包括确定和显示所述轨迹的至少一个点（被称为决策点）的步骤，超过该点 飞行器不能再通过确定轨迹与朝向选定的受限航路点转向的重合轨迹之间的交点，重新加入飞行计划的约束航点，该重合轨迹符合至少一个预定准则。

公开(公告)号：US20150211859A1

公开(公告)日：2015-07-30

申请号：US14604308

申请日：2015-01-23

申请人： THALES

发明人： Benoit DACRE-WRIGHT ,  Guy DEKER ,  Xavier BLANCHON

IPC分类号： G01C21/00

CPC分类号： G01C21/00 ,  G05D1/101

摘要： A method assisting in navigation of aircraft following a flight plan subject to time constraints comprises: determining a minimum speed profile, a maximum speed profile, and minimum and maximum times of passage; determining, for each constraint of index i, a restricted interval and a required interval; the determination made by a first iterative computation, i being decremented from n−1 to 1 and comprising: determining a required interval of index i enabling the aircraft to observe a restricted interval of index i+1 by flying at a speed profile between the minimum and maximum speed profiles, the restricted interval of index i+1 determined on the preceding iteration for an iteration of index between 1 and n−2, or from the time constraint of index n for the iteration of index n−1; and determining a restricted interval of index i from the intersection of the time constraint and the required interval of index i.

摘要翻译： 根据时间限制，协助在飞行计划之后辅助导航的方法包括：确定最小速度曲线，最大速度曲线以及最小和最大通过次数; 对于索引i的每个约束，确定受限制的间隔和所需的间隔; 由第一次迭代计算确定的i从n-1减1，包括：确定索引i的所需间隔，使得飞机能够以最小的速度轮廓飞行来观察索引i + 1的受限间隔 和最大速度曲线，在前一次迭代中确定的索引i + 1的限制间隔，用于迭代1和n-2之间的索引，或从索引n-1的迭代的索引n的时间约束; 并且从时间约束和索引i的所需间隔的交点确定索引i的受限间隔。