公开(公告)号：US20250044093A1

公开(公告)日：2025-02-06

申请号：US18719776

申请日：2022-10-28

Applicant: THALES

Inventor： Gilles GENEVRIER ,  Warody LOMBARDI ,  Sébastien LEGOLL

IPC: G01C21/00 ,  G06T7/521 ,  G06T7/55

Abstract: An airborne measurement system borne by an aircraft, and comprising a plurality of conventional navigational-aid sensors generating data referred to as conventional data, at least one SPAD camera comprising a single-photon avalanche diode matrix-array detector and generating SPAD data comprising a first image and a second image of a scene to be observed, the system comprising a processing unit connected to the conventional sensors and to the at least one SPAD camera, the processing unit being adapted to: choose, in accordance with a predetermined criterion and on the basis of the conventional data and/or of the SPAD data, a use of the conventional data which is referred to as the conventional mode, or a use of the SPAD data, and possibly comprising conventional data, which is referred to as the SPAD mode, and for the conventional mode, generate measurement information referred to as conventional information on the basis of conventional data, for the SPAD mode: determine, on the basis of the first image and of the second image, an error band for the measurement of the horizontal position of the aircraft, called the protection radius, generate measurement information referred to as reinforced information on the basis of at least SPAD data.

公开(公告)号：US20160305977A1

公开(公告)日：2016-10-20

申请号：US15132978

申请日：2016-04-19

Applicant: THALES

Inventor： Gilles GENEVRIER ,  Jacques MANDLE ,  Cédric FLAVEN ,  Jean-Pierre SCHLOTTERBECK

IPC: G01P13/02 ,  G01C23/00 ,  B64D43/02 ,  G01S17/58

CPC classification number: G01P13/025 ,  B64D43/02 ,  G01C23/00 ,  G01P5/14 ,  G01P5/26 ,  G01P21/025 ,  G01S7/4813 ,  G01S17/023 ,  G01S17/58 ,  G01S17/95 ,  Y02A90/19

Abstract: A multifunction probe for primary references for an aircraft, an associated measuring system, aircraft and method for obtaining physical quantities are disclosed. In one aspect, the multifunction probe includes a base designed to be fastened on the cockpit of an aircraft, a plurality of static pressure taps arranged through the base and connected to pressure measuring devices and an optical window transparent to laser radiation and positioned in the base for the passage of laser radiation through the base. The multifunction probe further includes at least one laser anemometry optical head positioned to take laser anemometry measurements through the optical window and a static temperature probe mounted on the base.

Abstract translation: 公开了一种用于飞行器的主要参考的多功能探头，相关联的测量系统，用于获得物理量的飞行器和方法。 一方面，多功能探头包括被设计成紧固在飞行器的驾驶舱上的基座，多个静压抽头，其布置成穿过基座并连接到压力测量装置和对激光辐射透明并位于基座中的光学窗口 用于激光辐射通过基底。 多功能探头还包括至少一个激光测风光学头，其定位成通过光学窗口进行激光测风测量，以及安装在基座上的静态温度探头。

公开(公告)号：US20150168439A1

公开(公告)日：2015-06-18

申请号：US14608962

申请日：2015-01-29

Applicant: THALES

Inventor： Gilles GENEVRIER ,  Bernard LEDAIN ,  Jacques MANDLE ,  Jean-Pierre SCHLOTTERBECK

IPC: G01P5/14 ,  G01P5/02 ,  G01S17/58 ,  G01P5/26

CPC classification number: G01P5/14 ,  G01P5/02 ,  G01P5/26 ,  G01P21/025 ,  G01S7/4813 ,  G01S17/023 ,  G01S17/58 ,  G01S17/95 ,  Y02A90/19

Abstract: A probe system, mixed primary reference probe for an aircraft, associated aircraft and measuring method are disclosed. In one aspect, the probe system includes a base designed to be fastened on the cockpit of an aircraft, a plurality of regularly spaced static pressure taps, arranged through the base and designed to be connected to a pressure measurement device. The system includes at least one optical window transparent to laser radiation and inserted into the base.

Abstract translation: 公开了一种用于飞行器的探针系统，混合主参考探头，相关飞行器和测量方法。 在一个方面，探针系统包括被设计成紧固在飞行器的驾驶舱上的基座，多个规则间隔的静压抽头，布置在基座上并设计成与压力测量装置连接。 该系统包括至少一个对激光辐射透明并插入基座的光学窗口。