公开(公告)号：US20140350755A1

公开(公告)日：2014-11-27

申请号：US14285246

申请日：2014-05-22

Applicant: THALES

Inventor： Christophe CAILLAUD ,  Jerome SACLE

IPC: G08G5/02

CPC classification number: G08G5/02 ,  G01C23/00 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/025

Abstract: A method and system for aiding piloting when selecting a trajectory of approach of an airport or airfield, implemented on at least one processor, includes a first step of selecting a landing airport or airfield, and a second step of determining, for said landing airport or airfield, all or part of the possible trajectories of approach associated with a landing runway, on the basis of a database of the airports or airfields. A third step determines, for at least one of the possible approaches, whether or not said approach is compatible with an angular guidance mode, by geometrical analysis of the approach; and a fourth step displays all of said possible approaches, for said landing airport or airfield, and of displaying the compatibility with said angular guidance mode for the approaches analyzed.

Abstract translation: 一种用于在选择在至少一个处理器上实施的机场或机场的接近轨迹时辅助驾驶的方法和系统包括选择着陆机场或机场的第一步骤，以及为所述着陆机场或 机场，基于机场或机场的数据库，与着陆跑道相关的所有或部分可能的方法轨迹。 对于至少一种可能的方法，通过对该方法的几何分析，确定所述方法是否与角度引导模式兼容; 并且第四步骤针对所述着陆机场或机场显示所有可能的方法，并且为所分析的方法显示与所述角度引导模式的兼容性。

公开(公告)号：US20240038075A1

公开(公告)日：2024-02-01

申请号：US18013723

申请日：2021-06-28

Applicant: THALES

Inventor： Jérôme SACLE ,  Marion CHAILLOU ,  Christophe CAILLAUD ,  Fabien CHOVIN ,  Michel ROGER

IPC: G08G5/00 ,  G08G5/02

CPC classification number: G08G5/0039 ,  G08G5/025 ,  G08G5/0021

Abstract: In the field of air navigation, a computer-implemented method includes loading an initial active flight plan for an aircraft comprising a first approach procedure to a runway up to a missed approach point ending between the missed approach point and a final point; loading a secondary flight plan comprising an approach procedure to the runway between the missed approach point and the runway, and a second missed approach procedure at the end of the approach, and ending at a second final point; receiving an instruction from an operator of the aircraft to link the initial active flight plan and the secondary flight plan; in the event of a go-around by the operator at the latest at the missed approach point, activating the missed approach procedure; otherwise, automatically selecting the secondary flight plan as active flight plan and activating the second approach.

公开(公告)号：US20160356626A1

公开(公告)日：2016-12-08

申请号：US14622683

申请日：2015-02-13

Applicant: THALES

Inventor： Christophe CAILLAUD ,  Jérôme SACLE

IPC: G01C23/00 ,  G08G5/02

CPC classification number: G01C23/005 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/02 ,  G08G5/025

Abstract: A method and system is provided for determining the compatibility of an approach, to a landing runway, with an angular guidance mode, the approach being compatible with a linear guidance mode, the angular guidance being characterized by a lateral angle of precision, the linear guidance being characterized by a lateral divergence of precision. The method is implemented on a flight management system deployed aboard an aircraft and comprising a first step of determining a first distance representative of a maximum distance of use of the angular guidance, on the basis of the lateral angle of precision and of the lateral divergence of precision.

Abstract translation: 提供了一种用于确定方法与着陆跑道与角度引导模式的兼容性的方法和系统，该方法与线性引导模式兼容，角度引导以精确的横向角度表征，线性引导 其特征在于横向偏差。 该方法在飞行器上部署的飞行管理系统上实现，并且包括：第一步骤，基于横向角度精度和侧向偏差来确定代表角度引导的最大使用距离的第一距离 精确。

公开(公告)号：US20130245862A1

公开(公告)日：2013-09-19

申请号：US13797617

申请日：2013-03-12

Applicant: THALES

Inventor： Guilhem PUTZ ,  Christophe CAILLAUD ,  Francois COULMEAU

IPC: G01C23/00

CPC classification number: G01C23/00 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/025

Abstract: A method for assisting in the navigation of an aircraft comprises steps of calculating and displaying a linear deviation on a first linear section and an angular deviation on a second angular section. The method comprises a step of calculation of an anticipated deviation of the aircraft, expressed linearly or angularly, projected to a time DT, characteristic of a reaction time of the aircraft, and of a statistical error distribution associated with this anticipated deviation; and a step of calculation of a probability of exceeding a predetermined target deviation, by means of the anticipated deviation and of the statistical error distribution. The method also comprises a crew alert when the probability is above a predetermined threshold.

Abstract translation: 一种辅助飞行器导航的方法包括以下步骤：计算和显示第一线性部分上的线性偏差和在第二角度部分上的角度偏差。 该方法包括计算飞行器的预期偏差的步骤，线性或角度地表示，投影到时间DT，飞机的反应时间的特征，以及与该预期偏差相关联的统计误差分布; 以及通过预期偏差和统计误差分布计算超过预定目标偏差的概率的步骤。 当概率高于预定阈值时，该方法还包括机组警报。

公开(公告)号：US20130245861A1

公开(公告)日：2013-09-19

申请号：US13797485

申请日：2013-03-12

Applicant: THALES

Inventor： Guilhem PUTZ ,  Christophe CAILLAUD ,  Francois COULMEAU

IPC: G01C23/00

CPC classification number: G01C23/00 ,  G05D1/0202 ,  G05D1/0676 ,  G05D1/101 ,  G08G5/0021 ,  G08G5/025

Abstract: A method for assisting in the navigation of an aircraft comprises steps of calculating and displaying a linear deviation on a first linear section and an angular deviation on a second angular section. The method comprises a calculation step for converting an angular deviation into an equivalent linear deviation, and, conversely, converting a linear deviation into an equivalent angular deviation. The method comprises a step of graphic representation, called unified monitoring, intended for the crew, of a deviation of the aircraft, on a lateral deviation axis and a vertical deviation axis; each of the deviations, lateral and vertical, being able to be represented on a linear scale, an angular scale or a mixed scale.

Abstract translation: 一种辅助飞行器导航的方法包括以下步骤：计算和显示第一线性部分上的线性偏差和在第二角度部分上的角度偏差。 该方法包括用于将角度偏差转换为等效线性偏差的计算步骤，相反地，将线性偏差转换为等效的角度偏差。 该方法包括一个图形表示，称为统一监视，用于机组人员，在横向偏离轴线和垂直偏离轴线上有飞行器偏离; 横向和垂直的每个偏差能够以线性刻度，角度刻度或混合刻度表示。