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1.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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2.发明授权Method for continuously and adaptively generating a speed setpoint for an aircraft to observe an RTA 有权一种连续自适应地生成飞机观测RTA的速度设定值的方法公开(公告)号：US08332145B2
公开(公告)日：2012-12-11
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
IPC分类号： G05D1/00
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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3.发明授权公开(公告)号：US08352169B2
公开(公告)日：2013-01-08
申请号：US12870666
申请日：2010-08-27
CPC分类号： G05D1/101 , G08G5/0039 , G08G5/0052
摘要： Method for assisting in the flight management of an aircraft aiming to reach a constraint point on a predetermined lateral trajectory that is assumed to have to be followed by the aircraft, at a required time of arrival RTA, said aircraft occupying a current position defined by a current altitude with a current horizontal speed. The method including, when it follows a rallying flight plan, calculating a new rallying flight plan following the lateral trajectory to be followed and including a new estimated speed profile different from the estimated speed profile over at least one update area, the new estimated speed profile including, over said update areas, either a value greater than that of the estimated speed profile, if the arrival time difference is positive, or a value less than that of the estimated speed profile, if the arrival time difference is negative.
摘要翻译： 一种用于协助飞机管理飞行管理的方法，该飞行器旨在达到预定的横向轨迹上的约束点，该预定横向轨迹假设必须在飞行器的后方到达所需的到达时间RTA，所述飞行器占据当前位置 当前高度与当前水平速度。 该方法包括当遵循升级飞行计划时，根据要遵循的横向轨迹计算新的升降飞行计划，并且在至少一个更新区域上包括与估计的速度曲线不同的新的估计速度曲线，新的估计速度曲线 如果到达时间差为正，则在所述更新区域上包括大于估计速度曲线的值的值，或者如果到达时间差为负值则为包括估计速度曲线的值。
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公开(公告)号：US08340843B2
公开(公告)日：2012-12-25
申请号：US12613203
申请日：2009-11-05
IPC分类号： G06F7/00
CPC分类号： G05D1/0202 , G08G5/0043
摘要： The invention relates to a method for determining the speed of an aircraft that is subject to a time constraint. The invention consists no longer in calculating a single CAS/MACH pair during climb/descent but in adapting the speed in a continuous manner to the bounds of curves of minimum Vmin and maximum Vmax speed defining a flight envelope of the aircraft. The calculation of these speeds is carried out on the basis of constant maximum and minimum speed setpoints and of a coefficient taking into account a deviation to the time constraint.
摘要翻译： 本发明涉及一种用于确定经受时间限制的飞行器的速度的方法。 本发明不再在爬升/下降期间计算单个CAS / MACH对，而是以连续的方式将速度适应于限定飞机的飞行包线的最小Vmin和最大Vmax速度的曲线的边界。 这些速度的计算是基于恒定的最大和最小速度设定值以及考虑到时间约束的偏差的系数进行的。
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5.发明申请公开(公告)号：US20140200752A9
公开(公告)日：2014-07-17
申请号：US12633508
申请日：2009-12-08
IPC分类号： G01C23/00
CPC分类号： G05D1/0202 , G01W1/08 , G01W1/10 , G08G5/0039 , G08G5/0091
摘要： The invention relates to a meteorological modelling method for calculating an aircraft flight plan, the aircraft comprising a communication means and a navigation management system.The method comprises at least the following steps: the communication means carries out the acquisition of meteorological prediction data related to waypoints in proximity to the nominal route in addition to the waypoints belonging to the nominal route, the navigation management system allocates by projection onto the current route of the aircraft the prediction data for the said waypoints not belonging to the current route, the navigation management system calculates the meteorological prediction data for the waypoints of the current route of the flight plan according to the prediction data allocated by projection onto the current route of the aircraft.The invention is a modelling method for aircraft navigation management systems.
摘要翻译： 本发明涉及一种用于计算飞行器飞行计划的气象建模方法，该飞行器包括通信装置和导航管理系统。 该方法至少包括以下步骤：除了属于标称路线的航路点之外，通信装置还执行与标称路径附近的航路点相关的气象预测数据的获取，导航管理系统通过投影分配到当前 航空器的路线是不属于当前路线的所述航路点的预测数据，导航管理系统根据通过投影到当前路线上分配的预测数据来计算飞行计划的当前路线的航路点的气象预测数据 的飞机。 本发明是用于飞机导航管理系统的建模方法。
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公开(公告)号：US08437957B2
公开(公告)日：2013-05-07
申请号：US13004704
申请日：2011-01-11
IPC分类号： G01C21/20
CPC分类号： G08G5/0034
摘要： A method and device checks the conformity of a trajectory calculated by a flight management system of an aircraft in relation to reference data comprising a reference map. The method includes: geo-referencing of a reference map; determination of a reference trajectory from the geo-referenced reference map; detection of nonconformity in the trajectory calculated by the flight management system by comparison of the trajectory calculated by the flight management system with the reference trajectory; and emission of a warning if a nonconformity is detected.
摘要翻译： 一种方法和装置检查由飞行器的飞行管理系统计算的轨迹与包括参考图的参考数据的一致性。 该方法包括：参考地图的地理参考; 从地理参考参考图确定参考轨迹; 通过飞行管理系统计算的轨迹与参考轨迹进行比较，检测飞行管理系统计算出的轨迹中的不符合度; 并且如果检测到不合格，则发出警告。
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7.发明申请公开(公告)号：US20100152931A1
公开(公告)日：2010-06-17
申请号：US12633508
申请日：2009-12-08
IPC分类号： G01C23/00
CPC分类号： G05D1/0202 , G01W1/08 , G01W1/10 , G08G5/0039 , G08G5/0091
摘要： The invention relates to a meteorological modelling method for calculating an aircraft flight plan, the aircraft comprising a communication means and a navigation management system.The method comprises at least the following steps: the communication means carries out the acquisition of meteorological prediction data related to waypoints in proximity to the nominal route in addition to the waypoints belonging to the nominal route, the navigation management system allocates by projection onto the current route of the aircraft the prediction data for the said waypoints not belonging to the current route, the navigation management system calculates the meteorological prediction data for the waypoints of the current route of the flight plan according to the prediction data allocated by projection onto the current route of the aircraft.The invention is a modelling method for aircraft navigation management systems.
摘要翻译： 本发明涉及一种用于计算飞行器飞行计划的气象建模方法，该飞行器包括通信装置和导航管理系统。 该方法至少包括以下步骤：除了属于标称路线的航路点之外，通信装置还执行与标称路径附近的航路点相关的气象预测数据的获取，导航管理系统通过投影分配到当前 航空器的路线是不属于当前路线的所述航路点的预测数据，导航管理系统根据通过投影到当前路线上分配的预测数据来计算飞行计划的当前路线的航路点的气象预测数据 的飞机。 本发明是用于飞机导航管理系统的建模方法。
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8.发明授权公开(公告)号：US08473120B2
公开(公告)日：2013-06-25
申请号：US12624725
申请日：2009-11-24
IPC分类号： G05D1/00
CPC分类号： G05D1/0005 , G08G5/0052 , G08G5/0078
摘要： The invention relates to the field of civil aviation and, more specifically, relates to the flight management systems, more commonly known by the English acronym FMS. The method for assisting in the management of the flight of an aircraft in order to keep to a time constraint according to the present invention allows for a control of the keeping to the time constraint that presents a rapid dynamic, by avoiding as far as possible having the estimated time of arrival (ETA) at a particular point (P) able to drift relative to a required time of arrival (RTA) at said particular point (P), thanks to the use of a maneuvering margin (M) granted to the guidance module of the aircraft.
摘要翻译： 本发明涉及民用航空领域，更具体地涉及飞行管理系统，其通常被英文首字母缩略词FMS所熟知。 为了保持根据本发明的时间限制的协助飞行器飞行的管理的方法允许通过避免尽可能避免具有快速动态的时间约束来控制， 在特定点（P）处可以相对于在所述特定点（P）处的所需到达时间（RTA）漂移的特定点（P）的估计到达时间（ETA），这归功于使用授予 飞机的指导模块。
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9.发明申请Method and Device for Aiding the Management of An Aircraft Flight Receiving a Control Clearance 有权协助管理飞机飞行员接收控制许可的方法和装置公开(公告)号：US20110246053A1
公开(公告)日：2011-10-06
申请号：US12896698
申请日：2010-10-01
CPC分类号： G08G5/0013 , G08G5/0039
摘要： A method for aiding the management of an aircraft flight according to an active flight plan receiving a control clearance transmitted at a current time includes a step of computing a reception flight plan based on the said control clearance, a step of storing the said reception flight plan in a memory space dedicated to the said reception flight plan. The method also includes, prior to the step of computing a reception flight plan: a step of determining the time, called the recognition time, assumed to have to elapse between the current time and a time at which the said control clearance is assumed to be recognized; a step of attribution, to the said control clearance, of a destination flight plan as a function of the recognition time, the said destination flight plan being the temporary flight plan when the recognition time is included in a first time slot and the destination flight plan being a secondary flight plan when the recognition time is included in a second time slot longer than the first time slot.
摘要翻译： 根据在当前时间发送的接收到控制许可的主动飞行计划来帮助管理飞行器飞行的方法包括基于所述控制许可计算接收飞行计划的步骤，存储所述接收飞行计划的步骤 在专用于所述接收飞行计划的存储空间中。 该方法还包括在计算接收飞行计划的步骤之前：确定称为识别时间的时间的步骤，假定在当前时间与假定所述控制间隙之间的时间为止 认可的 将目的地飞行计划归因于所述控制许可的步骤作为识别时间的函数，所述目的地飞行计划是当第一时隙中包括识别时间的目的地飞行计划和目的地飞行计划 当识别时间被包括在比第一时隙长的第二时隙中时，作为辅助飞行计划。
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10.发明申请公开(公告)号：US20100131125A1
公开(公告)日：2010-05-27
申请号：US12624725
申请日：2009-11-24
IPC分类号： G01C23/00
CPC分类号： G05D1/0005 , G08G5/0052 , G08G5/0078
摘要： The invention relates to the field of civil aviation and, more specifically, relates to the flight management systems, more commonly known by the English acronym FMS. The method for assisting in the management of the flight of an aircraft in order to keep to a time constraint according to the present invention allows for a control of the keeping to the time constraint that presents a rapid dynamic, by avoiding as far as possible having the estimated time of arrival (ETA) at a particular point (P) able to drift relative to a required time of arrival (RTA) at said particular point (P), thanks to the use of a manoeuvring margin (M) granted to the guidance module of the aircraft.
摘要翻译： 本发明涉及民用航空领域，更具体地涉及飞行管理系统，其通常被英文首字母缩略词FMS所熟知。 为了保持根据本发明的时间限制的协助飞行器飞行的管理的方法允许通过避免尽可能避免具有快速动态的时间约束来控制， 在特定点（P）处可以相对于在所述特定点（P）处的所需到达时间（RTA）漂移的特定点（P）的估计到达时间（ETA），这归功于使用授予 飞机的指导模块。
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