公开(公告)号：US09188978B2

公开(公告)日：2015-11-17

申请号：US14522469

申请日：2014-10-23

Applicant: THALES

Inventor： Jerome Sacle ,  Johan Boyer ,  Francois Coulmeau

IPC: G05D1/00 ,  G05D1/04 ,  G08G5/00 ,  G01C21/20 ,  G05D1/06 ,  G06Q10/04 ,  G08G5/02

CPC classification number: G05D1/00 ,  G01C21/20 ,  G01C23/00 ,  G05D1/0005 ,  G05D1/042 ,  G05D1/0676 ,  G06Q10/047 ,  G08G5/003 ,  G08G5/006 ,  G08G5/0095 ,  G08G5/025 ,  Y02T50/84

Abstract: A method for aiding navigation for an aircraft between a descent start point and a computation end point, comprises the computation steps of: collecting a flight plan consisting of a succession of waypoints and of the associated vertical constraints; determining a corridor consisting of a floor trajectory and of a ceiling trajectory defining the minimum and maximum altitudes permitted to the aircraft; splitting the corridor into several cells defined between two waypoints furthest apart and between which the ceiling trajectory is distinct from the floor trajectory; determining for at least one cell a vertical trajectory complying with the altitude constraints and comprising the longest possible IDLE segment; and a step consisting in determining and displaying maneuvering points of the aircraft making it possible to follow the target vertical trajectory.

Abstract translation: 一种用于帮助航空器在下降起点和计算终点之间的导航的方法包括以下计算步骤：收集由一系列航路点和相关垂直约束组成的飞行计划; 确定由地板轨迹和限定飞机允许的最小和最大高度的天花板轨迹组成的走廊; 将走廊拆分成两个距离最远的两个航点之间定义的几个单元，天花板轨迹与地板轨迹不同; 为至少一个小区确定符合所述高度约束的垂直轨迹并且包括所述最长可能的空闲段; 并且包括确定和显示飞行器的机动点的步骤，使得可以跟随目标垂直轨迹。

公开(公告)号：US09176499B2

公开(公告)日：2015-11-03

申请号：US14521239

申请日：2014-10-22

Applicant: THALES

Inventor： Francois Coulmeau ,  Jerome Sacle ,  Johan Boyer

IPC: G05D1/00 ,  G08G5/00 ,  G01C23/00 ,  G05D1/04 ,  G05D1/06 ,  G08G5/02

CPC classification number: G05D1/00 ,  G01C23/00 ,  G05D1/042 ,  G05D1/0676 ,  G05D1/101 ,  G08G5/0021 ,  G08G5/003 ,  G08G5/0052 ,  G08G5/025 ,  Y02T50/84

Abstract: A method is provided for managing the flight of an aircraft flying a trajectory calculated by a flight management system. The trajectory necessitates at least one transition between two different aerodynamic configurations of the aircraft. The method comprises: extraction of performance data of the aircraft from a database, at least one item of performance data being a function of an aerodynamic configuration, selection between a first determination step and a second determination step, a step of determination of a start point and of an end point of the transition between two aerodynamic configurations and engine speeds of an aircraft during a flight, the determination step being implemented by the flight management system and chosen from among the first and second determination steps, the determination step calculating the trajectory by numerical integration of the equations representative of the dynamics of the aircraft making use of the performance data of the aircraft.

Abstract translation: 提供了一种用于管理飞行由飞行管理系统计算的轨迹的飞行器的飞行的方法。 轨迹必须在飞行器的两种不同的空气动力学构型之间进行至少一个过渡。 该方法包括：从数据库中提取飞行器的性能数据，作为空气动力学配置的函数的至少一个性能数据项，第一确定步骤和第二确定步骤之间的选择，确定起始点的步骤 以及在飞行期间飞行器的两种空气动力学构型和发动机速度之间的转变的终点，所述确定步骤由飞行管理系统实施并且从第一和第二确定步骤中选择，所述确定步骤通过以下步骤计算轨迹： 代表使用飞机性能数据的飞机动力学的方程的数值积分。

公开(公告)号：US09188461B2

公开(公告)日：2015-11-17

申请号：US13728731

申请日：2012-12-27

Applicant: THALES

Inventor： Camille Rieunier ,  Jerome Sacle ,  Joseph Huysseune ,  Xavier Chazottes

IPC: G01D1/00 ,  G01C23/00 ,  G08G5/00

CPC classification number: G01C23/00 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/0052

Abstract: A configured aircraft flight management aid system comprises: means of interpretation receiving data taken from external instructions from an external control center, data relating to aircraft equipment failures, cabin problems and problems related to the environment of the aircraft; means of determination receiving data from the means of interpretation and determining at least one reference constraint associated with at least one parameter representative of a flight path, a reference constraint associated with a reference parameter comprising a new constraint, different from the initial constraint when the item of data effectively necessitates following a new path, different from the initial path, and a reference constraint comprising the initial constraint when the means of determination do not have access to any data relating to an event effectively necessitating following a new path; warning means generating a warning to an operator when the path actually flown does not comply with said reference constraint.

Abstract translation: 配置的飞机飞行管理援助系统包括：从外部控制中心接收外部指令的数据的解释手段，与飞机设备故障有关的数据，客舱问题以及与飞机环境有关的问题; 确定从所述解释装置接收数据并确定与代表飞行路径的至少一个参数相关联的至少一个参考约束的装置，与包括新约束的参考参数相关联的参考约束，所述参考参数与所述初始约束不同，当所述项目 的数据有效地需要遵循与初始路径不同的新路径，以及包括初始约束的参考约束，当确定方法不能访问与事件相关的任何数据时，有效地需要跟随新路径; 当路径实际飞行不符合所述参考约束时，警告意味着向操作者产生警告。