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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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公开(公告)号：US20100100308A1
公开(公告)日：2010-04-22
申请号：US12579272
申请日：2009-10-14
CPC分类号： G08G5/006
摘要： The invention relates to a device for formulating a flight plan ensuring sufficient safety margins for a duration of a few minutes in relation to the set of flight constraints that could arise and comprising means for: detecting the surrounding moving objects (aircraft or meteorological phenomena), evaluating their type and the danger that they represent, formulating a reconfiguration flight plan ensuring a separation with these phenomena and taking best account of the constraints of the initially followed flight plan, avoiding prohibited or regulated airspaces and avoiding the surrounding relief with ad hoc operational margins.
摘要翻译： 本发明涉及一种用于制定飞行计划的装置，其确保相对于可能出现的一组飞行约束，持续几分钟的足够的安全裕度，并且包括用于：检测周围的运动物体（飞机或气象现象）的装置， 评估他们的类型和他们所代表的危险，制定重新配置飞行计划，确保与这些现象分离，并充分考虑到最初跟踪的飞行计划的限制，避免被禁止或受规管的空域，并避免周围的特殊运营利润减轻 。
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6.发明授权Method of plotting a portion of trajectory of an aircraft comprising a circular arc of constant radius 失效描绘包括恒定半径的圆弧的飞行器的轨迹的一部分的方法公开(公告)号：US08321068B2
公开(公告)日：2012-11-27
申请号：US12121086
申请日：2008-05-15
IPC分类号： G05D1/00
CPC分类号： G08G5/0034 , G08G5/0021
摘要： A method is disclosed for plotting a trajectory portion (6, 6″), using flight management means of an aircraft, and linking a known position (7) of the aircraft to a point in space (4), denoted the “exit point”. A circular arc is defined, the coordinates of whose centre (1) are known, comprising two ends (3, 4) of known coordinates, one end of which is the exit point (4). The position of a transition point (5) is determined which is situated on the arc. The trajectory (6, 6″) by the flight management means of the aircraft is automatically plotted. The trajectory is successively linking the known position (7) of the aircraft, and the transition point (5) and the exit point (4).
摘要翻译： 公开了一种使用飞行器的飞行管理装置绘制轨迹部分（6,6“）并将飞行器的已知位置（7）链接到空白处的点（4）的方法，表示出口点。 定义圆弧，其中心（1）的坐标是已知的，包括已知坐标的两端（3,4），其一端是出口点（4）。 确定位于弧上的转变点（5）的位置。 航空器的飞行管理装置的轨迹（6,6“）被自动绘制。 轨迹连续地连接飞行器的已知位置（7）和转换点（5）和出口点（4）。
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7.发明申请公开(公告)号：US20100217459A1
公开(公告)日：2010-08-26
申请号：US12707294
申请日：2010-02-17
IPC分类号： G06F19/00
CPC分类号： G05D1/0005 , G05D1/0676
摘要： The invention relates to a method for formulating the strategy of an aircraft, with a view to favouring adherence to a time constraint.With this aim, the method according to the invention consists in optimizing the margin available for the formulation of the aircraft's speed strategy, by calculating a first target required time of arrival (RTAtarget) which is higher, respectively lower, than the required time of arrival (RTA), in the case where said required time of arrival (RTA) is greater, respectively less, than the mean estimated time of arrival (ETAmean). According to the invention, the first target required time of arrival (RTAtarget) is used for the formulation of the aircraft's speed strategy. According to the invention, a second target required time of arrival (RTAtarget2) can be determined subsequently, and used for the formulation of the speed strategy, with the aim of utilizing the margin, previously optimized, available for the formulation of the aircraft's speed strategy.
摘要翻译： 本发明涉及一种用于制定飞行器的策略的方法，以期有利于遵守时间限制。 为此目的，根据本发明的方法在于通过计算比所要求的到达时间更高的第一目标所需到达时间（RTA目标），优化可用于制定飞行器速度策略的裕度 （RTA），如果所需的到达时间（RTA）大于平均预计到达时间（ETAmean），则较小。 根据本发明，第一目标需要到达时间（RTAtarget）用于制定飞行器的速度策略。 根据本发明，可以随后确定需要的到达时间（RTAtarget2）的第二目标，并用于制定速度策略，目的是利用先前优化的可用于制定飞行器速度策略的余量 。
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8.发明授权公开(公告)号：US08386158B2
公开(公告)日：2013-02-26
申请号：US12632562
申请日：2009-12-07
IPC分类号： G06F19/00
CPC分类号： G08G5/025 , G05D1/104 , G08G5/0008 , G08G5/0021 , G08G5/0052
摘要： A method for providing for the optimized regulation of the relative spacing between aircraft is disclosed. This method can be implemented by a system whose physical architecture can rely mainly on existing computers on board most current aircraft. The method includes a main step of determining the changing trend of the relative spacing, in distance or in time, between a target aircraft (C) and a following aircraft (S).
摘要翻译： 公开了一种用于提供飞行器之间的相对间距的优化调节的方法。 该方法可以由物理架构主要依赖当前飞机上的现有计算机的系统来实现。 该方法包括确定目标飞机（C）和下一架飞机（S）之间距离或时间上的相对间距的变化趋势的主要步骤。
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公开(公告)号：US08275499B2
公开(公告)日：2012-09-25
申请号：US12579272
申请日：2009-10-14
CPC分类号： G08G5/006
摘要： The invention relates to a device for formulating a flight plan ensuring sufficient safety margins for a duration of a few minutes in relation to the set of flight constraints that could arise and comprising means for: detecting the surrounding moving objects (aircraft or meteorological phenomena), evaluating their type and the danger that they represent, formulating a reconfiguration flight plan ensuring a separation with these phenomena and taking best account of the constraints of the initially followed flight plan, avoiding prohibited or regulated airspaces and avoiding the surrounding relief with ad hoc operational margins.
摘要翻译： 本发明涉及一种用于制定飞行计划的装置，其确保相对于可能出现的一组飞行约束，持续几分钟的足够的安全裕度，并且包括用于：检测周围的运动物体（飞机或气象现象）的装置， 评估他们的类型和他们所代表的危险，制定重新配置飞行计划，确保与这些现象分离，并充分考虑到最初跟踪的飞行计划的限制，避免被禁止或受规管的空域，并避免周围的特殊运营利润减轻 。
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公开(公告)号：US20090177342A1
公开(公告)日：2009-07-09
申请号：US12348444
申请日：2009-01-05
IPC分类号： G05D1/02
CPC分类号： G08G5/0039 , Y02T50/84
摘要： A method of applying a “Heading Then Merge Behind” (HTMB) guidance directive sent by an air traffic control center to an aircraft comprising a flight management system, the flight management system making it possible to automatically follow the trajectory of an active flight plan. The method includes reception and validation of the directive by the flight management system, confirmation by the pilot of the aircraft of the application of the directive, creation by the flight management system of a flight plan incorporating the directive, activation by the pilot of the flight plan incorporating the directive, so that the directive is executed automatically by the flight management system while following the trajectory of the flight plan incorporating the directive.
摘要翻译： 一种将由空中交通管制中心发送的飞行管理指导指令（HTMB）引导到包括飞行管理系统的飞机的方法，飞行管理系统可以自动跟踪主动飞行计划的轨迹。 该方法包括由飞行管理系统接收和验证指令，航空器飞行员对该指令的应用进行确认，由飞行管理系统创建一个包含该指令的飞行计划，飞行员飞行员激活 计划包含该指令，以便该指令由飞行管理系统自动执行，同时遵循包含该指令的飞行计划的轨迹。
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