一种飞行器的防撞装置(10、38),所述防撞装置(10、38)包括多个传感器(S1、S2、…、Si、…SN),所述多个传感器包括至少两个单独的传感器(Si、Sj),每个传感器被配置成根据至少一个障碍物的接近度分别传送各自捕获的数据集合,所述防撞装置(10、38)包括:至少一个数据均质化模块(12),所述至少一个数据均质化模块(12)被配置成将至少一个捕获数据的集合(Eci)转换成相应的未标记数据的集合(Ebi),分别与至少一个传感器(Ci)相关联的每个未标记数据的集合(Ebi)由从一个未标记数据的集合到另一个未标记数据的集合的多个相同数据类型构成,数据处理模块(14),所述数据处理模块(14)被配置成根据所述未标记数据的集合(Eb1、Eb2、…、Ebi、…EbN)生成代表障碍物存在或不存在的至少一条信息。

    An anti-collision device of an aircraft including a plurality of sensors, the plurality of sensors including at least two separate sensors, each sensor being configured to respectively deliver its own set of captured data as a function of the proximity of at least one obstruction, the anti-collision device including: at least one data homogenization module configured to transform at least one set of captured data in a corresponding set of unmarked data, each set of unmarked data respectively associated with at least one sensor being made up of a plurality of identical data types from one set of unmarked data to another, and a data processing module configured to generate, from said sets of unmarked data, at least one piece of information representative of the presence or absence of obstruction(s).


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    Title :

    防撞装置和航空电子保护系统、防撞方法以及计算机程序


    Publication date :

    2024-07-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01S RADIO DIRECTION-FINDING , Funkpeilung / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen