The invention discloses an automatic aircraft positioning system and a method. The automatic aircraft positioning system (100) includes a first aircraft (102) including one more fiducials, and a second aircraft (104) including a positioning radar (108), control devices (112) that are configured to control operation of the second aircraft (104), and a control unit (110) in communication with the positioning radar (108) and the control devices (112). The positioning radar (108) is configured to transmit a radar (108) transmit signal. The one or more fiducials are configured to receive the radar (108) transmit signal and output one or more return signals (120) in response to the radar (108) transmit signal. The positioning radar is configured to receive the one or more return signals and determine a position and orientation of the second aircraft relative to the first aircraft, or vice versa, from the one or more return signals. The control unit (110) is configured to automatically control the second aircraft in relation to the first aircraft (102) during an automatic positioning mode.

    公开了自动飞机定位系统和方法。自动飞机定位系统(100)包括第一飞机(102)和第二飞机(104),该第一飞机(102)包括一个或多个基准件,该第二飞机(104)包括定位雷达(108)、被配置为控制第二飞机(104)的操作的控制装置(112)以及与定位雷达和控制装置通信的控制单元(110)。该定位雷达被配置为发射雷达发射信号。该一个或多个基准件被配置为接收雷达发射信号并且响应于雷达发射信号而输出一个或多个返回信号(120)。该定位雷达被配置为接收一个或多个返回信号并且从该一个或多个返回信号确定第二飞机相对于第一飞机的位置和定向,或反之亦然。该控制单元(110)被配置为在自动定位模式期间相对于第一飞机(102)自动控制第二飞机。


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    Title :

    AUTOMATIC AIRCRAFT POSITIONING SYSTEM AND METHOD


    Additional title:

    自动飞机定位系统和方法


    Contributors:

    Publication date :

    2021-09-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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