公开(公告)号：US09272771B2

公开(公告)日：2016-03-01

申请号：US14075707

申请日：2013-11-08

Applicant: THALES

Inventor： Norbert Baloche ,  Bertrand Barnetche ,  Michel Roger

IPC: G01C21/00 ,  B64C19/00 ,  G05D1/10

CPC classification number: B64C19/00 ,  G01C21/00 ,  G05D1/101

Abstract: An onboard flight management system in an aircraft comprises means for continuously calculating first geolocation data, from data received from at least one external geolocation device, comprising a current position and future positions of an aircraft along a trajectory sequenced in several portions and comprising second data comprising demands required by an international navigation procedure called “Required Navigation Performance”, or RNP, for all the portions of the trajectory. The management system additionally comprises a means for displaying first and second data all the way along the trajectory, the first and second data being represented graphically and simultaneously on the said display means in order to enable the pilot to anticipate the flight characteristics for the aircraft and make them converge toward the required demands of the next trajectory portion.

Abstract translation: 飞行器中的机载飞行管理系统包括用于从从至少一个外部地理定位装置接收的数据连续地计算第一地理位置数据的装置，其包括沿着以若干部分排序的轨迹的飞行器的当前位置和未来位置，并且包括第二数据， 对于轨迹的所有部分，国际导航程序所要求的要求，称为“所需导航性能”（RNP）。 管理系统还包括用于沿着轨迹一直显示第一和第二数据的装置，第一和第二数据在所述显示装置上以图形和同时的方式表示，以使驾驶员能够预测飞机的飞行特性， 使它们朝着下一个轨迹部分的要求收敛。

公开(公告)号：US08930130B2

公开(公告)日：2015-01-06

申请号：US13950187

申请日：2013-07-24

Applicant: Thales

Inventor： Romain Courteville ,  Bertrand Barnetche

IPC: G01C21/00 ,  G08G5/00 ,  G01C23/00 ,  G05D1/10

CPC classification number: G01C21/00 ,  G01C23/00 ,  G05D1/101 ,  G08G5/0034 ,  G08G5/0039

Abstract: A method for constructing a flight trajectory of an aircraft, comprises a step of computing a sequence of state vectors (Ei) representing the trajectory of the aircraft; a state vector (Ei+1) being determined on the basis of the state vector (Ei) preceding it by means of: a step of computing the speed components (Vi+1), consisting in determining: a flight setpoint, by selecting an objective navigation point, a joining strategy adapted to the flight setpoint and to the flight domain (DV) by means of a predefined library (LSr) of joining strategies, a manoeuvre by means of the flight domain (DV), making it possible to follow the joining strategy towards the flight setpoint; a step of computing the other components of the state vector (Ei+1), on the basis of the components of the speed vector (Vi+1) and of the preceding state vector (Ei).

Abstract translation: 一种用于构建飞行器的飞行轨迹的方法，包括计算代表飞机轨迹的状态矢量序列（Ei）的步骤; 根据前面的状态向量（Ei），通过以下步骤确定状态向量（Ei + 1）：计算速度分量（Vi + 1）的步骤，包括：确定：飞行设定点，通过选择一个 客观导航点，适应飞行设定点和飞行域（DV）的加入策略，通过加入策略的预定义库（LSr），借助于飞行域（DV）的操纵，使得可以跟随 加入飞行设定点策略; 基于速度矢量（Vi + 1）和前一状态矢量（Ei）的分量来计算状态向量（Ei + 1）的其他分量的步骤。

公开(公告)号：US09404752B2

公开(公告)日：2016-08-02

申请号：US13950701

申请日：2013-07-25

Applicant: THALES

Inventor： Romain Courteville ,  Bertrand Barnetche

IPC: G08G5/00 ,  G01C21/00 ,  G06Q10/04

CPC classification number: G01C21/00 ,  G06Q10/047 ,  G08G5/0034

Abstract: A method for processing a flight plan, implemented in a flight management system, consisting of at least one segment, comprises a step of determining the positions of the start point and of the end point of each of said segments constituting said flight plan by searching for at least two characteristic points of said segment, said characteristic points being explicit, fixed and non-floating, said positions being respectively characterized by a latitude, a longitude and an altitude.

Abstract translation: 一种用于处理由飞行管理系统实现的飞行计划的方法，由至少一个段组成，包括通过搜索来确定构成所述飞行计划的每个所述段的起始点和终点的位置的步骤 所述段的至少两个特征点，所述特征点是明确的，固定的和非浮动的，所述位置分别由纬度，经度和高度表征。