首页> 外国专利> LANDING SUPPORT DEVICE FOR AIRCRAFT, LANDING SUPPORT METHOD FOR AIRCRAFT, AND LANDING SUPPORT PROGRAM FOR AIRCRAFT

LANDING SUPPORT DEVICE FOR AIRCRAFT, LANDING SUPPORT METHOD FOR AIRCRAFT, AND LANDING SUPPORT PROGRAM FOR AIRCRAFT

机译:飞机着陆支持装置,飞机着陆支持方法以及飞机着陆支持程序

摘要

To estimate a wind direction and a wind velocity at a landing point with a higher degree of accuracy than ever.SOLUTION: A rotary-wing airplane 1 comprises a camera 13 for acquiring an image of the periphery of a landing point, an anemometer 15 for measuring a wind direction and a wind velocity over the landing point, and a control part 18. The control part 18 acquires a shape of the periphery of the landing point on the basis of the acquired image, and calculates the wind direction and the wind velocity at the landing point on the basis of the shape of the periphery of the landing point and the wind direction and the wind velocity over the landing point.SELECTED DRAWING: Figure 3
机译:为了以更高的精度估算着陆点的风向和风速。解决方案:旋翼飞机1包括用于获取着陆点周围图像的摄像机13,用于测量着陆点周围风速的风速计15测量着陆点上的风向和风速,以及控制部18。控制部18基于所获取的图像来获取着陆点的周围的形状,并计算风向和风速。根据着陆点周围的形状,着陆点的风向和风速确定着陆点的位置。选图:图3

著录项

  • 公开/公告号JP2020045049A

    专利类型

  • 公开/公告日2020-03-26

    原文格式PDF

  • 申请/专利权人 SUBARU CORP;

    申请/专利号JP20180176880

  • 发明设计人 ADACHI NORIHIKO;TOMONAGA YUKINOBU;

    申请日2018-09-21

  • 分类号B64D45/04;B64C27/04;B64C39/02;B64D47/08;G08G5/02;

  • 国家 JP

  • 入库时间 2022-08-21 11:37:18

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号