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METHOD FOR TRANSMITTING FLIGHT PARAMETERS OF A LEAD AIRCRAFT TO AN INTRUDER AIRCRAFT

机译:引导飞机到飞行器的飞行参数传输方法

摘要

A method for transmitting flight parameters of a lead aircraft to an intruder aircraft. Transmission includes a collision avoidance system connected to which is a flight parameter transmission authorization system having a database including coordinates defining a volume of confidence smaller than the monitoring volume. The flight parameter transmission authorization system of the lead aircraft authorizes, only for an intruder aircraft identified as flying within the volume of confidence, transmission of at least one flight parameter of the lead aircraft, such that this intruder aircraft is able to calculate the position of centers of wake vortices generated by the lead aircraft or the flow strength of the wake vortices. Exchanging flight parameters of the lead aircraft only with intruder aircraft flying within the volume of confidence with limited dimensions makes it possible not to exceed the maximum capacity of the bandwidth of the automated communication.
机译:一种将领先飞机的飞行参数传输到入侵飞机的方法。传输包括连接的防撞系统,其是飞行参数传输授权系统,该系统具有数据库,该数据库包括定义比监视量小的置信量的坐标的数据库。牵头飞机的飞行参数传输授权系统仅对被确定为在置信量内飞行的入侵者飞机授权领导飞机的至少一个飞行参数的传输,从而使该入侵者飞机能够计算出飞行器位置。领头飞机产生的尾流涡流的中心或尾流涡流的流动强度。仅在限制范围内的置信体积内飞行的入侵飞机与入侵飞机交换飞行参数,才有可能不超过自动通信带宽的最大容量。

著录项

  • 公开/公告号US2018301044A1

    专利类型

  • 公开/公告日2018-10-18

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS (S.A.S.);

    申请/专利号US201815950111

  • 发明设计人 MATHIEU HIALE-GUILHAMOU;JEAN-LUC ROBIN;

    申请日2018-04-10

  • 分类号G08G5/04;G08G5;

  • 国家 US

  • 入库时间 2022-08-21 13:01:20

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