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Aircraft-antenna controlling device, aircraft, aircraft-antenna selecting program, and aircraft-antenna controlling method

机译:飞机天线控制装置,飞机,飞机天线选择程序以及飞机天线控制方法

摘要

A control unit of an aircraft includes a computer that predicts the current position of a wingman aircraft based on a temporal change in wingman-aircraft position information indicating the position of the wingman aircraft; an antenna selector that selects, from among multiple antennas, an antenna with which the elongation φt with respect to the center axis of the antenna at the predicted current position of the wingman aircraft predicted by the computer falls within a coverage angle θ; and a beam controller that executes communication with the wingman aircraft via the antenna selected by the antenna selector. Thus, the control unit of the aircraft can select an optimal antenna for communication with the wingman aircraft from among the multiple antennas.
机译:飞机的控制单元包括计算机,该计算机基于表示该机翼飞机的位置的机翼飞机位置信息的时间变化来预测机翼飞机的当前位置。天线选择器,从多个天线中选择在计算机所预测的机翼飞行器的预测当前位置处相对于天线的中心轴的伸长率φt处于覆盖角θ内的天线。波束控制器通过天线选择器选择的天线与机翼飞行器进行通信。因此,飞机的控制单元可以从多个天线中选择用于与机翼飞机通信的最佳天线。

著录项

  • 公开/公告号US10205502B2

    专利类型

  • 公开/公告日2019-02-12

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY INDUSTRIES LTD.;

    申请/专利号US201314417643

  • 发明设计人 SHOTA KIKUCHI;IPPEI MIYANISHI;

    申请日2013-09-30

  • 分类号H01Q1/28;H01Q3/24;H04B7/06;H04B7/08;G01S19/49;

  • 国家 US

  • 入库时间 2022-08-21 12:13:15

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