The invention discloses an aircraft pentagonal take-off and landing auxiliary system and method, and relates to the technical field of aircraft control. According to one specific embodiment, the system comprises an aircraft 100, a right transmitting antenna 1 is installed on a right wing of the aircraft 100, a head transmitting antenna 2 is installed on the head of the aircraft 100, a left transmitting antenna 3 is installed on a left wing of the aircraft 100, and a tail transmitting antenna 4 is installed on the tail of the aircraft 100, the transmitting angles and orientations of the right transmitting antenna 1, the head transmitting antenna 2, the left transmitting antenna 3 and the tail transmitting antenna 4 are fixed; the ground receiving end 200 comprises a receiving antenna 5 and a state indication assembly 6, the receiving antenna 5 is used for receiving signals transmitted by the right transmitting antenna 1, the head transmitting antenna 2, the left transmitting antenna 3 and the tail transmitting antenna 4, and the state indication assembly 6 indicates the flight state of the aircraft 100 according to the signals. And the five-side flight state of the aircraft can be conveniently indicated.

    本发明公开了提供了一种飞行器五边起降辅助系统和方法,涉及飞行器控制技术领域。该系统的一个具体实施方式包括:飞行器100,所述飞行器100的右翼安装有右发射天线1,头部安装有头发射天线2,左翼安装有左发射天线3,尾部安装有尾发射天线4,其中,所述右发射天线1、所述头发射天线2、所述左发射天线3和所述尾发射天线4的发射角度和朝向固定;地面接收端200,所述地面接收端包括接收天线5和状态指示组件6,其中所述接收天线5用于接收来自所述右发射天线1、所述头发射天线2、所述左发射天线3和所述尾发射天线4发射的信号,所述状态指示组件6根据所述信号指示所述飞行器100的飞行状态。便于指示飞行器五边飞行的状态。


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    Titel :

    Aircraft pentagonal take-off and landing auxiliary system and method


    Weitere Titelangaben:

    一种飞行器五边起降辅助系统及方法


    Beteiligte:
    WU QIANG (Autor:in) / ZHAO XUEDONG (Autor:in) / ZHU CHAOLEI (Autor:in) / JIN YU (Autor:in) / YI JIANPING (Autor:in) / GU QUANXIANG (Autor:in)

    Erscheinungsdatum :

    09.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge