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1.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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2.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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3.发明授权公开(公告)号：US08718933B2
公开(公告)日：2014-05-06
申请号：US12870683
申请日：2010-08-27
CPC分类号： G05D1/101 , G08G5/0039 , G08G5/0052
摘要： A method of flight management of an aircraft aimed at reaching a constrained point on a predetermined lateral trajectory assumed to be followed by the aircraft, at a required time of arrival RTA to within an absolute tolerance. The method including calculating a flight plan to be followed and a homing flight plan and when the estimated time of arrival ETA based on the homing flight plan strays from an absolute tolerance with respect to the calculation required time of arrival RTAc, calculating a new calculation required time of arrival NRTAc dependent on the calculation required time of arrival RTAc and a function f of the difference between the calculation required time of arrival RTAc and the estimated time of arrival ETA, and replacing the calculation required time of arrival RTAc with the new calculation required time of arrival NRTAc, before recalculating a flight plan to be followed.
摘要翻译： 一种飞行器的飞行管理方法，其目的是到达假定为飞行器所遵循的预定侧向轨迹上的约束点，在到达RTA的所需时间内达到绝对公差。 该方法包括计算要遵循的飞行计划和归位飞行计划，以及当基于归位飞行计划的估计到达时间ETA相对于计算所需到达时间RTAc的绝对公差偏离时，计算所需的新计算 到达时间NRTAc取决于计算所需的到达时间RTAc和计算所需到达时间RTAc与预计到达时间ETA之间的差异的函数f，并且用新的计算替换计算所需的到达时间RTAc 时间到达NRTAc，然后重新计算要遵循的飞行计划。
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4.发明申请METHOD FOR AIDING THE MANAGEMENT OF A FLIGHT WITH A VIEW TO ADHERING TO A TIME CONSTRAINT 失效用于支持飞行管理的方法，具有附加到时间约束的视图公开(公告)号：US20110077859A1
公开(公告)日：2011-03-31
申请号：US12870683
申请日：2010-08-27
IPC分类号： G01C21/00
CPC分类号： G05D1/101 , G08G5/0039 , G08G5/0052
摘要： A method of flight management of an aircraft aimed at reaching a constrained point on a predetermined lateral trajectory assumed to be followed by the aircraft, at a required time of arrival RTA to within an absolute tolerance. The method including calculating a flight plan to be followed and a homing flight plan and when the estimated time of arrival ETA based on the homing flight plan strays from an absolute tolerance with respect to the calculation required time of arrival RTAc, calculating a new calculation required time of arrival NRTAc dependent on the calculation required time of arrival RTAc and a function f of the difference between the calculation required time of arrival RTAc and the estimated time of arrival ETA, and replacing the calculation required time of arrival RTAc with the new calculation required time of arrival NRTAc, before recalculating a flight plan to be followed.
摘要翻译： 一种飞行器的飞行管理方法，其目的是到达假定为飞行器所遵循的预定侧向轨迹上的约束点，在到达RTA的所需时间内达到绝对公差。 该方法包括计算要遵循的飞行计划和归位飞行计划，以及当基于归位飞行计划的估计到达时间ETA相对于计算所需到达时间RTAc的绝对公差偏离时，计算需要的新计算 到达时间NRTAc取决于计算所需的到达时间RTAc和计算所需到达时间RTAc与预计到达时间ETA之间的差异的函数f，并且用新的计算替换计算所需的到达时间RTAc 时间到达NRTAc，然后重新计算要遵循的飞行计划。
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5.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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6.发明授权公开(公告)号：US08321072B2
公开(公告)日：2012-11-27
申请号：US12763880
申请日：2010-04-20
IPC分类号： G05D3/00
CPC分类号： G06Q20/00
摘要： A method for determining the quantity of fuel in an aircraft and an optimization criterion such as a cost index, notably used in an FMS, making it possible to maintain a time requirement of the RTA type, comprising a first step of computing the optimization criterion CIi as a function of the aircraft weight GWi-1 via a method of the RTA type and a second step of computing the weight of the aircraft GWi as a function of the optimization criterion Ci-1 computed in the first computation step and the aircraft weight GWi-1, executed by successive iterations, until the estimated flight time resulting from the computed parameters after the second computation step makes it possible to observe the time requirement to within a determined criterion δt, a last step determining the pair of values of aircraft weight GWi and of performance criterion CIi-1 allowing an optimal fuel payload and the maintenance of the RTA.
摘要翻译： 一种用于确定飞行器中的燃料量的方法以及诸如成本指数的优化标准，特别是在FMS中使用的，使得可以维持RTA类型的时间需求成为可能，包括计算优化标准CIi的第一步骤 作为通过RTA类型的方法的飞机重量GWi-1的函数，以及第二步骤，根据在第一计算步骤中计算的优化准则Ci-1和飞行器重量GWi计算飞机GWi的权重 -1，直到由第二计算步骤之后的计算参数产生的估计飞行时间使得可以观察到在确定的标准δt内的时间要求，确定飞机重量GWi的值的最后步骤 和性能标准CIi-1，允许最佳燃料有效载荷和RTA的维护。
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7.发明授权公开(公告)号：US08744768B2
公开(公告)日：2014-06-03
申请号：US12955832
申请日：2010-11-29
CPC分类号： G05D1/00 , G05D1/0005 , G06F19/00 , G08G5/0013 , G08G5/003 , G08G5/0052
摘要： A method and device establishes trajectory planning, predictions and guidance so as to obtain the satisfaction of a time constraint (RTA). This objective is achieved by undertaking a computation of a trajectory up to the point where the flypast time constraint applies, on the basis of a profile of altitude and speeds, and then by computing the profile of speeds and altitudes making it possible, throughout the computed trajectory, to comply with the RTA. The method is also a method for readapting the trajectory and the vertical profile when during a mission, the data outside the aeroplane have caused the time predictions to drift and the constraint is no longer complied with under the initial speeds and trajectory assumptions.
摘要翻译： 方法和设备建立轨迹规划，预测和指导，以获得时间约束（RTA）的满足。 该目标是通过基于高度和速度轮廓进行到达飞行时间约束点的轨迹的计算来实现的，然后通过计算速度和高度的轮廓使得在整个计算过程中 轨迹，符合RTA。 该方法也是在任务期间重新读取轨迹和垂直剖面的方法，飞机外的数据已经引起时间预测漂移，并且在初始速度和轨迹假设下不再遵守约束。
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8.发明授权System and method for merging meteorological data predicted and measured on an aircraft 有权用于合并飞机上预测和测量的气象数据的系统和方法公开(公告)号：US08543267B2
公开(公告)日：2013-09-24
申请号：US12553305
申请日：2009-09-03
申请人： Philippe Chaix , Alex Bourdon , Alexandre Grattard
发明人： Philippe Chaix , Alex Bourdon , Alexandre Grattard
摘要： The invention consists in merging together the predicted and measured meteorological data to supply them to the flight prediction calculation system so as to smooth the discontinuities brought about in the prior art by the simple update which is carried out. This merging is advantageously done by linear weighting of the data, the weighting coefficient depending upon the positioning in vertical and horizontal distances between the predicted point and the aeroplane in relation to chosen thresholds.
摘要翻译： 本发明将预测和测量的气象数据合并在一起，将其提供给飞行预测计算系统，以便通过执行的简单更新来平滑现有技术带来的不连续性。 这种合并有利地通过数据的线性加权来完成，加权系数取决于预测点和飞机之间相对于所选阈值的垂直和水平距离的定位。
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公开(公告)号：US08478752B2
公开(公告)日：2013-07-02
申请号：US13132622
申请日：2009-12-04
申请人： Pierre Gamet , Philippe Chaix
发明人： Pierre Gamet , Philippe Chaix
IPC分类号： G06F17/20
CPC分类号： G06F17/30241
摘要： A navigation database comprises a first set of elements comprising airports, beacons and waypoints; a second set of elements comprising procedures; and a third set of elements comprising routes. The method comprises a step of creating a pair of indices comprising an index comprising the elements of the three sets; identifier, a type and a functional identifier; a first list of pointers to the memory address where the elements are stored; a pre-index comprising a list of code, each code corresponding to the first characters of each element, the codes being indexed by a family of attributes of elements; a second list of pointers to the identifier of the first element in the first index.
摘要翻译： 导航数据库包括包括机场，信标和航路点的第一组元素; 包括程序的第二组元素; 以及包括路线的第三组元素。 该方法包括创建一对索引的步骤，该索引包括包括三组元素的索引; 标识符，类型和功能标识符; 指向存储元素的存储器地址的指针的第一个列表; 包括代码列表的预索引，每个代码对应于每个元素的第一个字符，代码由元素的属性族索引; 指向第一索引中的第一元素的标识符的指针的第二列表。
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公开(公告)号：US20120036124A1
公开(公告)日：2012-02-09
申请号：US13132622
申请日：2009-12-04
申请人： Pierre Gamet , Philippe Chaix
发明人： Pierre Gamet , Philippe Chaix
IPC分类号： G06F17/30
CPC分类号： G06F17/30241
摘要： A navigation database comprises a first set of elements comprising airports, beacons and waypoints; a second set of elements comprising procedures; and a third set of elements comprising routes. The method comprises a step of creating a pair of indices comprising an index comprising the elements of the three sets; identifier, a type and a functional identifier; a first list of pointers to the memory address where the elements are stored; a pre-index comprising a list of code, each code corresponding to the first characters of each element, the codes being indexed by a family of attributes of elements; a second list of pointers to the identifier of the first element in the first index.
摘要翻译： 导航数据库包括包括机场，信标和航路点的第一组元素; 包括程序的第二组元素; 以及包括路线的第三组元素。 该方法包括创建一对索引的步骤，该索引包括包括三组元素的索引; 标识符，类型和功能标识符; 指向存储元素的存储器地址的指针的第一个列表; 包括代码列表的预索引，每个代码对应于每个元素的第一个字符，代码由元素的属性族索引; 指向第一索引中的第一元素的标识符的指针的第二列表。
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