公开(公告)号：US20240118706A1

公开(公告)日：2024-04-11

申请号：US18275489

申请日：2022-02-02

Applicant: THALES

Inventor： Sébastien DESCUDE ,  Christian SANNINO ,  Hugo BORONAT

IPC: G05D1/229 ,  G05D1/46 ,  G05D1/689

CPC classification number: G05D1/2295 ,  G05D1/46 ,  G05D1/689 ,  B64U2101/31 ,  B64U2201/10

Abstract: A method for guiding an autonomous aircraft, the aircraft includes an automatic pilot, a plurality of sensors and an imaging unit, the aircraft being configured to fly over a geographic zone comprising overflight prohibited zones, the guidance method can advantageously comprise a phase of real flight of the autonomous aircraft by using a given guidance law, comprising the following steps: determining a current state of the autonomous aircraft; determining an optimum action to be executed by using a neural network receiving the current state; determining a plurality of control instructions compatible with the guidance law based on the optimum action to be executed; transmitting to the automatic pilot the plurality of control instructions, which provides a new state of the autonomous aircraft.

公开(公告)号：US20150187148A1

公开(公告)日：2015-07-02

申请号：US14565871

申请日：2014-12-10

Applicant: THALES

Inventor： Christian SANNINO ,  Xavier CHAZOTTES ,  Francois COULMEAU

IPC: G07C5/08 ,  B64D45/00

CPC classification number: G07C5/0808 ,  B64D45/00 ,  B64D2045/0085 ,  G05B23/0286 ,  G06F11/0739 ,  G06F11/0784 ,  G07C5/0841

Abstract: A device and method for assisting with reconfiguration of an aircraft, an aircraft including such a device and an associated computer program product are disclosed. In one aspect, the aircraft has an operational configuration, is configured to move in an operational environment, and includes at least one avionic system, at least one avionic member, and at least one monitoring system configured to detect an abnormality of an avionic member or a perturbation of the operational environment and to generate a fault information. The device is connected between at least one monitoring system and at least one avionic system, and includes a reception module configured to receive a fault information from the monitoring system, an impact computation module configured to compute an impact on the operational configuration of the aircraft, and a transmission module configured to transmit the computed impact to at least one avionic system.

Abstract translation: 公开了一种用于辅助重新配置飞行器的装置和方法，包括这种装置的飞机和相关联的计算机程序产品。 一方面，飞行器具有操作配置，被配置为在操作环境中移动，并且包括至少一个航空电子系统，至少一个航空电子部件和被配置为检测航空电子部件的异常的至少一个监视系统，或者 操作环境的扰动并产生故障信息。 该设备连接在至少一个监控系统和至少一个航空电子系统之间，并且包括被配置为从监控系统接收故障信息的接收模块，被配置为计算对飞行器的操作配置的影响的冲击计算模块， 以及传输模块，被配置为将所计算的冲击传递到至少一个航空电子系统。

公开(公告)号：US20170148236A1

公开(公告)日：2017-05-25

申请号：US15358559

申请日：2016-11-22

Applicant: THALES

Inventor： Christian SANNINO ,  Jonathan SPRAUEL

IPC: G07C5/08 ,  G06F17/30 ,  B64D45/00

CPC classification number: G07C5/0825 ,  B64D45/00 ,  B64D2045/0085 ,  G05B23/0278 ,  G06F17/30994 ,  G07C5/0808 ,  G07C5/0841

Abstract: Disclosed is an electronic apparatus for assisting an aircraft pilot. The aircraft includes avionics equipment implementing operational capacities and a monitoring system configured to determine monitoring information from operational capacities and operating parameters of the avionics equipment. The assistance apparatus includes in an acquisition module configured to acquire the monitoring information and an anomaly detection module configured to detect at least one anomaly from among a breakdown of an avionics equipment and a failure of an operational capacity, from monitoring information and anomaly detection rules contained in a predefined database. The assistance apparatus includes an inference module configured to identify, for each anomaly, one or several causes that may have caused the anomaly, based on relationships between breakdowns and failures, the relationships being contained in the database.