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1. 发明授权

US11138891B2 Method and electronic system for managing the flight of an aircraft in a visual approach phase to a runway, related computer program 有权
公开(公告)号：US11138891B2
公开(公告)日：2021-10-05
申请号：US16921242
申请日：2020-07-06
申请人： THALES
发明人： Michel Roger , Valérie Bataillon
IPC分类号： G01C21/00 , G08G5/02
摘要： This method for managing the flight of an aircraft in a visual approach phase to a runway is implemented by an electronic flight management system and comprises: acquiring at least one set among a set of values of lateral visual approach trajectory parameters and a set of values of vertical visual approach trajectory parameters, at least one of said values of visual approach trajectory parameters being able to be designated by a user, computing at least one trajectory among a lateral visual approach trajectory from the values of said lateral visual approach trajectory parameters and a vertical visual approach trajectory from the values of said vertical visual approach trajectory parameters, and generating a visual approach trajectory to the runway from the lateral visual approach trajectory and/or the vertical visual approach trajectory.

2. 发明授权

US09530321B2 Flight management method and system 有权
公开(公告)号：US09530321B2
公开(公告)日：2016-12-27
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： G01C23/00 , G08G5/00 , G05D1/10
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.

3. 发明授权

US11435763B2 Electronical device, and method, for automatically determining piloting information of a mobile machine accompanying a leader mobile machine, associated computer program 有权
公开(公告)号：US11435763B2
公开(公告)日：2022-09-06
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, said device being adapted for collecting the location data of the leader mobile machine from among the actual location data derived from measurements relating to the current location of the leader mobile machine and the current trajectory data of the accompanying mobile machine, and of determining, on the basis of 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, 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.

4. 发明授权

US09575489B2 Method of error detection of an aircraft flight management and guidance system and high-integrity flight management and guidance system 有权
标题翻译：飞机飞行管理指导系统和高度完整性飞行管理指导系统的错误检测方法
公开(公告)号：US09575489B2
公开(公告)日：2017-02-21
申请号：US14951420
申请日：2015-11-24
申请人： THALES
发明人： Michel Roger , Alexandre Darbois
IPC分类号： G05D1/00 , G08G5/00
CPC分类号： G05D1/0077 , G08G5/003 , G08G5/0047
摘要： A method of error detection of a flight management system coupled with a guidance of an aircraft according to a flight plan, comprises the steps of: generating a first reference guidance order, monitoring the integrity of the first reference position, when the first reference position is not monitored as being dependable: invalidating the first FMS assembly and the associated guidance system, when the first reference position and the first reference trajectory are monitored as being dependable: generating a first monitoring guidance order, generating a first reference flight control, generating a first monitoring flight control, in monitoring the integrity of the first reference guidance order when the first reference guidance order is not monitored as being dependable: invalidating the first FMS assembly and the associated guidance.
摘要翻译：根据飞行计划与飞行器的引导相结合的飞行管理系统的错误检测方法包括以下步骤：产生第一参考指导指令，监视第一参考位置的完整性，当第一参考位置是不被监视为可靠的：当第一参考位置和第一参考轨迹被监视为可靠时，使第一FMS组件和相关联的引导系统无效：产生第一监视引导顺序，产生第一参考飞行控制，产生第一参考飞行控制监控飞行控制，在第一个参考指导指令不被监视为可靠时监视第一参考指南顺序的完整性：使第一个FMS组件和相关指导无效。

5. 发明授权

US10380901B2 Method for automatically rejoining a reference vertical profile of an aircraft 有权
公开(公告)号：US10380901B2
公开(公告)日：2019-08-13
申请号：US15492693
申请日：2017-04-20
申请人： THALES
发明人： Guy Deker , Michel Roger
IPC分类号： G08G5/00 , G01C21/20 , G05D1/06 , B64D31/02 , G01C21/00
摘要： A method, computer program and system are provided for calculating in an automatic manner a trajectory for rejoining a reference vertical profile of an aircraft. A reference vertical profile comprises a set of vertical constraints, and a method comprises a step of selecting an altitude constraint to be complied with, a step of calculating a vertical-profile prediction making it possible to comply with the constraint, a step of validating the vertical-profile prediction, if the vertical-profile prediction is validated, a step of applying the vertical-profile prediction, otherwise a step of determining the existence of a following altitude constraint to be complied with; if a following altitude constraint exists: a step of selecting a following altitude constraint to be complied with; a return to the step of detecting non-compliance with an altitude constraint; otherwise, a step of applying an exit procedure.

6. 发明授权

US09290262B2 Method for creating a vertical trajectory profile comprising multiple altitude levels 有权
标题翻译：用于创建包括多个高度水平的垂直轨迹轮廓的方法
公开(公告)号：US09290262B2
公开(公告)日：2016-03-22
申请号：US14186681
申请日：2014-02-21
申请人： THALES
发明人： Enrique Laso-Leon , Amandine Audouy , Guillaume Meulle , Michel Roger
IPC分类号： G08G5/02 , G05D1/04 , B64C19/00 , G05D1/00 , G05D1/06 , G01C21/20 , G08G5/00
CPC分类号： B64C19/00 , G01C21/20 , G05D1/0005 , G05D1/0607 , G08G5/0021 , G08G5/0034
摘要： A method for creating a vertical trajectory profile of an aircraft by optimization of a criterion representative of a flight cost, comprises: performing a first iterative computation of a profile free of altitude constraints as long as a condition dependent on the criterion is not reached, replacing each free level of the constraint-free profile with a permitted level so as to generate an initial constrained profile comprising a plurality of permitted levels, and, for each level, an altitude change point and a plurality of speeds, and performing a second iterative computation of a profile in which the altitude levels to be reached remain constant, equal to the initial permitted levels of the initial constrained profile, as long as a condition dependent on the criterion is not reached.
摘要翻译：一种用于通过优化表示飞行成本的标准来创建飞行器的垂直轨迹曲线的方法包括：只要没有达到取决于标准的条件，就执行没有高度约束的轮廓的第一迭代计算，替换每个具有允许级别的无约束简档的空闲级别，以便产生包括多个允许级别的初始约束简档，并且对于每个级别，对于每个级别，高度变化点和多个速度，以及执行第二迭代计算其中要达到的高度水平保持恒定，等于初始约束曲线的初始允许水平，只要不达到取决于准则的条件即可。

7. 发明授权

US09272771B2 System for anticipating required navigation performance 有权
标题翻译：用于预测所需导航性能的系统
公开(公告)号：US09272771B2
公开(公告)日：2016-03-01
申请号：US14075707
申请日：2013-11-08
申请人： THALES
发明人： Norbert Baloche , Bertrand Barnetche , Michel Roger
IPC分类号： G01C21/00 , B64C19/00 , G05D1/10
CPC分类号： B64C19/00 , G01C21/00 , G05D1/101
摘要： An onboard flight management system in an aircraft comprises means for continuously calculating first geolocation data, from data received from at least one external geolocation device, comprising a current position and future positions of an aircraft along a trajectory sequenced in several portions and comprising second data comprising demands required by an international navigation procedure called “Required Navigation Performance”, or RNP, for all the portions of the trajectory. The management system additionally comprises a means for displaying first and second data all the way along the trajectory, the first and second data being represented graphically and simultaneously on the said display means in order to enable the pilot to anticipate the flight characteristics for the aircraft and make them converge toward the required demands of the next trajectory portion.
摘要翻译：飞行器中的机载飞行管理系统包括用于从从至少一个外部地理定位装置接收的数据连续地计算第一地理位置数据的装置，其包括沿着以若干部分排序的轨迹的飞行器的当前位置和未来位置，并且包括第二数据，对于轨迹的所有部分，国际导航程序所要求的要求，称为“所需导航性能”（RNP）。管理系统还包括用于沿着轨迹一直显示第一和第二数据的装置，第一和第二数据在所述显示装置上以图形和同时的方式表示，以使驾驶员能够预测飞机的飞行特性，使它们朝着下一个轨迹部分的要求收敛。

8. 发明授权

US09983009B2 Device and method for calculating estimated navigation performance prediction 有权
公开(公告)号：US09983009B2
公开(公告)日：2018-05-29
申请号：US15642238
申请日：2017-07-05
申请人： THALES
发明人： Michel Roger , Christophe Pierre , Hervé Goutelard
IPC分类号： G01C21/20 , G01S19/49 , G01C21/16 , G01C23/00 , G08G5/00 , G01S19/48 , G05D1/02
CPC分类号： G01C21/20 , G01C21/16 , G01C23/00 , G01C23/005 , G01S19/48 , G01S19/49 , G05D1/02 , G08G5/003
摘要： A method is provided for calculating the estimated navigation performance prediction for a trajectory associated with a list of segments of a flight plan. A method for displaying the navigation performance in a corridor trajectory so as to guarantee compliance with the navigation performance requirements while offering immediate viewing of the navigation latitude in a corridor is also provided.

9. 发明授权

US09666082B2 Method and system for guidance of an aircraft 有权
公开(公告)号：US09666082B2
公开(公告)日：2017-05-30
申请号：US14978812
申请日：2015-12-22
申请人： THALES
发明人： Michel Roger , Mathieu Orvain
IPC分类号： G08G5/00 , G05D1/00
CPC分类号： G08G5/0034 , G05D1/0088 , G08G5/0021 , G08G5/0047 , G08G5/0052
摘要： A method of flight management and guidance of an aircraft executed by a flight management system FMS comprises the steps of: generating a reference trajectory, generating a short-term trajectory, periodically transmitting the short-term trajectory, generating a long-term trajectory, formatting the segments of the long-term trajectory, periodically transmitting the long-term trajectory, storing the long-term trajectory transmitted, testing the validity of the FMS sub-assembly, when the FMS sub-assembly is valid: identifying, by the autonomous guidance module, the active segment of the short-term trajectory, generating, by the autonomous guidance module, a first flight guidance order on the basis of the active segment of the short-term trajectory; when the FMS sub-assembly is not valid: identifying, by the autonomous guidance module, the active segment of the stored trajectory, generating, by the autonomous guidance module, a second flight guidance order on the basis of the active segment of the stored trajectory.

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