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公开(公告)号：US20070142981A1
公开(公告)日：2007-06-21
申请号：US11642659
申请日：2006-12-21
IPC分类号： G01C23/00
CPC分类号： G01C23/00 , G05B23/0256
摘要： The invention relates to a flight management system for aircraft which makes it possible to carry out tests of the results of the calculations of the main functions for formulating the flight plans and trajectories of the aircraft making it possible to anticipate errors in this formulation, to present them to the crew as a function of criticality criteria, to store them so as to be communicated and processed by the maintenance teams.
摘要翻译： 本发明涉及一种用于飞行器的飞行管理系统，其使得可以对用于制定飞机的飞行计划和轨迹的主要功能的计算结果进行测试，使得可以预期该配方中的错误，以呈现 他们按照关键性标准对机组人员进行存储，以便维护团队进行沟通和处理。
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2.发明申请公开(公告)号：US20090177341A1
公开(公告)日：2009-07-09
申请号：US12328683
申请日：2008-12-04
IPC分类号： G05D1/00
CPC分类号： G05D1/0061 , G05D1/101
摘要： The present invention relates to a method of decoupling the mode of automatic following of the lateral profile and the mode of automatic following of the vertical profile of an automatic guidance system of an aircraft (A) flying on a reference trajectory (T). The mode of automatic following of the vertical profile is not disengaged immediately on disengaging the mode of automatic following of the lateral profile. After disengaging the mode of automatic following of the lateral profile, the mode of automatic following of the vertical profile is disengaged automatically only if at least one criterion of lateral separation between the current or short-term position of the aircraft and the lateral profile corresponding to the reference trajectory is satisfied, having regard to the position error.
摘要翻译： 本发明涉及一种解除横向轮廓自动跟随的模式的方法以及在参考轨迹（T）上飞行的飞行器（A）的自动引导系统的垂直轮廓的自动跟随模式。 自动跟随垂直轮廓的模式在脱离自动跟随侧面轮廓的模式后立即不会脱离。 在脱离自动跟随侧面轮廓的模式之后，只有当航空器的当前或短期位置与对应于飞行器的横向轮廓之间的至少一个横向分离标准时，自动跟随垂直轮廓的模式才被自动分离 考虑到位置误差，满足参考轨迹。
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3.发明授权公开(公告)号：US08838299B2
公开(公告)日：2014-09-16
申请号：US12328683
申请日：2008-12-04
CPC分类号： G05D1/0061 , G05D1/101
摘要： The present invention relates to a method of decoupling the mode of automatic following of the lateral profile and the mode of automatic following of the vertical profile of an automatic guidance system of an aircraft (A) flying on a reference trajectory (T). The mode of automatic following of the vertical profile is not disengaged immediately on disengaging the mode of automatic following of the lateral profile. After disengaging the mode of automatic following of the lateral profile, the mode of automatic following of the vertical profile is disengaged automatically only if at least one criterion of lateral separation between the current or short-term position of the aircraft and the lateral profile corresponding to the reference trajectory is satisfied, having regard to the position error.
摘要翻译： 本发明涉及一种解除横向轮廓自动跟随的模式的方法以及在参考轨迹（T）上飞行的飞行器（A）的自动引导系统的垂直轮廓的自动跟随模式。 自动跟随垂直轮廓的模式在脱离自动跟随侧面轮廓的模式后立即不会脱离。 在脱离自动跟随侧面轮廓的模式之后，只有当航空器的当前或短期位置与对应于飞行器的横向轮廓之间的至少一个横向分离标准时，自动跟随垂直轮廓的模式才被自动分离 考虑到位置误差，满足参考轨迹。
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公开(公告)号：US08838293B2
公开(公告)日：2014-09-16
申请号：US11642659
申请日：2006-12-21
CPC分类号： G01C23/00 , G05B23/0256
摘要： The invention relates to a flight management system for aircraft which makes it possible to carry out tests of the results of the calculations of the main functions for formulating the flight plans and trajectories of the aircraft making it possible to anticipate errors in this formulation, to present them to the crew as a function of criticality criteria, to store them so as to be communicated and processed by the maintenance teams.
摘要翻译： 本发明涉及一种用于飞行器的飞行管理系统，其使得可以对用于制定飞机的飞行计划和轨迹的主要功能的计算结果进行测试，使得可以预期该配方中的错误，以呈现 他们按照关键性标准对机组人员进行存储，以便维护团队进行沟通和处理。
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5.发明授权Method for updating audio communication frequencies between aircraft and ATC stations on the ground 有权更新飞机与地面ATC站之间音频通信频率的方法公开(公告)号：US08149141B2
公开(公告)日：2012-04-03
申请号：US11955254
申请日：2007-12-12
申请人： François Coulmeau , Guy Deker
发明人： François Coulmeau , Guy Deker
IPC分类号： G08B21/00
CPC分类号： G08G5/006 , G08G5/0013
摘要： The present invention relates to a method for automatically preparing an update of audio communication frequencies between aircraft and ATC stations on the ground, a method making it possible to reduce the communication time associated with the necessary frequency changes between control sectors, therefore limiting the frequency space requirement, and reducing the workload due to the manipulations and control of these frequency changes, both for the air traffic controllers and for the aircraft crews, and wherein the flight plan or the current trajectory followed by the aircraft is dynamically coupled with the geometry information of the control sectors overflown by the aircraft and that, thereby knowing the intersection points of the flight plan with the sector limits, the frequency changes and sector name are prepared before each change of sector, while warning the pilot of their imminence.
摘要翻译： 本发明涉及一种用于自动准备飞机与ATC站在地面上的音频通信频率更新的方法，该方法使得可以减少与控制扇区之间的必要频率变化相关联的通信时间，从而限制频率空间 要求，并且由于对空中交通管制员和飞机机组的这些频率变化的操纵和控制而减少了工作量，并且其中飞行计划或飞机跟随的当前轨迹与 控制部门由飞机溢出，从而知道飞行计划与行业限制的交点，频率变化和行业名称在每个行业变化前准备，同时警告飞行员即将到来。
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公开(公告)号：US20100217510A1
公开(公告)日：2010-08-26
申请号：US12710483
申请日：2010-02-23
申请人： Guy Deker
发明人： Guy Deker
摘要： The invention relates to a method for managing the flight of an aircraft flying along a trajectory and being subject to an absolute time constraint (on a downstream point) or relative time constraint (spacing with respect to a downstream aircraft), the said aircraft comprising a flight management system calculating a temporal discrepancy to the said time constraint, wherein the said method includes the following steps: the calculation of a distance on the basis of the temporal discrepancy, the modification of the trajectory: if the temporal discrepancy to the time constraint corresponds to an advance, the lengthening of the trajectory by the distance; if the temporal discrepancy to the time constraint corresponds to a delay, the shortening of the trajectory by the distance.
摘要翻译： 本发明涉及一种用于管理沿着轨迹飞行并且经受绝对时间限制（在下游点）或相对时间约束（相对于下游飞机的间隔）的飞行器的飞行的方法，所述飞机包括 飞行管理系统计算与所述时间约束的时间差异，其中所述方法包括以下步骤：基于时间差异计算距离，轨迹修改：如果与时间约束的时间差异对应于 提前，延长轨道的距离; 如果与时间约束的时间差异对应于延迟，则缩短轨迹的距离。
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公开(公告)号：US20090045982A1
公开(公告)日：2009-02-19
申请号：US12134719
申请日：2008-06-06
申请人： Christophe Caillaud , Guy Deker , Nicolas Marty
发明人： Christophe Caillaud , Guy Deker , Nicolas Marty
摘要： The general field of the invention is that of systems for aiding the guidance of an aircraft on an airport. The system according to the invention comprises means for determining at least one element of the topology of the airport in relation to the position of the aircraft for selecting. Selecting means are provided by the pilot of the aircraft for the element. Generating means are provided to generate at least one guidance or safety set-point using the topological element. Presenting means are provided for the element or the associated set-point on a man-machine interface to the pilot of the aircraft.
摘要翻译： 本发明的一般领域是用于协助飞机在机场上的引导的系统。 根据本发明的系统包括用于相对于飞机的位置来确定机场的拓扑的至少一个元件用于选择的装置。 选择装置由飞行员的飞行员提供。 提供生成装置以使用拓扑元素生成至少一个引导或安全设定点。 在飞机的飞行员的人机接口上为元件或相关联的设定点提供呈现装置。
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8.发明申请METHOD OF FORMING A 3D SAFE EMERGENCY DESCENT TRAJECTORY FOR AIRCRAFT AND IMPLEMENTATION DEVICE 有权形成用于飞机和实施装置的3D安全紧急下降轨道的方法公开(公告)号：US20080177432A1
公开(公告)日：2008-07-24
申请号：US11870338
申请日：2007-10-10
申请人： Guy Deker , Nicolas Marty , Francois Coulmeau
发明人： Guy Deker , Nicolas Marty , Francois Coulmeau
IPC分类号： G01C23/00
CPC分类号： G08G5/0039 , G01C21/00 , G05D1/0676
摘要： The method in accordance with the invention is a method of providing a 3D emergency descent trajectory for aircraft comprising the steps of searching for at least one possible better trajectory allowing a secure continuation in relation to the relief and/or the surrounding conditions towards a homing point as soon as a situation requiring an unscheduled modification of the current trajectory occurs, wherein this trajectory is updated as a function of the alterations in the surrounding conditions, as a function of the information provided by the onboard sensors and/or outside information received.
摘要翻译： 根据本发明的方法是提供用于飞行器的3D紧急下降轨迹的方法，包括以下步骤：搜索至少一个可能的更好的轨迹，允许相对于所述浮雕和/或围绕归位点的周围条件的安全延续 一旦出现需要对当前轨迹进行不定期修改的情况，其中根据由机载传感器提供的信息和/或所接收的外部信息，该轨迹作为周围环境变化的函数被更新。
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9.发明授权Method for changing the path followed by an aircraft, the aircraft initially following a predefined path, the method allowing a possible return of the aircraft to the predefined path 有权用于改变飞机跟随的路径的方法，飞行器最初遵循预定义的路径，该方法允许飞机可能返回预定路径公开(公告)号：US08396615B2
公开(公告)日：2013-03-12
申请号：US11844473
申请日：2007-08-24
申请人： Christophe Caillaud , Guy Deker
发明人： Christophe Caillaud , Guy Deker
CPC分类号： G05D1/0202
摘要： The present invention relates to a method for changing the path followed by an aircraft, the aircraft initially following a predefined path on the basis of a sequence of waypoints, the method allowing a subsequent return of the aircraft to the predefined path in the same direction or in the reverse direction. The method allows a possible return of the aircraft to the predefined path in the same direction such that the waypoints of the predefined path are projected onto a new path according to a projection function ensuring that the order of the sequence of the projected image points complies with the order of the sequence of the original waypoints. The projection of a waypoint already reached by the aircraft also is considered as having been reached. The projections of the waypoints on the new path are considered reached by the aircraft progressively as the latter progresses along the new path. The aircraft eventually rejoins the predefined path at the first waypoint in the order of the sequence of points whose projection is not yet considered as reached on the new path.
摘要翻译： 本发明涉及一种用于改变飞机跟随的路径的方法，飞行器最初基于航路点序列遵循预定义的路径，该方法允许飞行器随后在相同方向上返回到预定路径，或 在相反的方向。 该方法允许飞行器在相同方向上可能返回到预定义的路径，使得根据投影函数将预定路径的路点投影到新路径上，确保投影图像点序列的顺序符合 原始航点的顺序顺序。 飞机已经达到的航路点的投影也被认为已经达到。 飞机在新路径上的预测由飞机逐渐被认为是随着新航道进展而来的。 飞机最终在第一个航路点以按照新路径未达到的投影顺序的顺序重新加入预定义的路径。
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10.发明申请Method for Continuously and Adaptively Generating a Speed Setpoint for an Aircraft to Observe an RTA 有权用于连续和适应地生成用于观察RTA的飞行器的速度设定点的方法公开(公告)号：US20110137493A1
公开(公告)日：2011-06-09
申请号：US12790596
申请日：2010-05-28
申请人： Benoît Dacre-Wright , Guy Deker , Xavier Blanchon
发明人： Benoît Dacre-Wright , Guy Deker , Xavier Blanchon
CPC分类号： G05D1/101
摘要： Method for generating a flight speed profile of an aircraft (100) according to an RTA constraint, characterized in that it permanently calculates, at any point of the flight plan, a speed setpoint VΩ(X) of the aircraft determined on the basis of reference speed profiles, comprising at least a minimum speed profile Vmin(X), and a maximum speed profile Vmax(X). The method can also take into account an optimum speed profile Vopt(X) determined, for example, on the basis of a cost or performance index.
摘要翻译： 用于根据RTA约束产生飞行器（100）的飞行速度曲线的方法，其特征在于，其在飞行计划的任何点处永久地计算基于以下方式确定的飞行器的速度设定点V＆OHgr;（X） 参考速度曲线，包括至少最小速度曲线Vmin（X）和最大速度曲线Vmax（X）。 该方法还可以考虑例如基于成本或性能指标确定的最佳速度曲线Vopt（X）。
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