首页> 外国专利> METHODS AND SYSTEMS FOR TRANSITIONING AN AERIAL VEHICLE BETWEEN HOVER FLIGHT AND CROSSWIND FLIGHT

METHODS AND SYSTEMS FOR TRANSITIONING AN AERIAL VEHICLE BETWEEN HOVER FLIGHT AND CROSSWIND FLIGHT

机译:在悬停飞行和侧风飞行之间转换航空车辆的方法和系统

摘要

A method involves operating an aerial vehicle in a hover-flight orientation. The aerial vehicle is connected to a tether that defines a tether sphere having a radius based on a length of the tether, and the tether is connected to a ground station. The method involves positioning the aerial vehicle at a first location that is substantially on the tether sphere. The method involves transitioning the aerial vehicle from the hover-flight orientation to a forward-flight orientation, such that the aerial vehicle moves from the tether sphere. And the method involves operating the aerial vehicle in the forward-flight orientation to ascend at an angle of ascent to a second location that is substantially on the tether sphere. The first and second locations are substantially downwind of the ground station.
机译:一种方法涉及以悬停飞行方向操作飞行器。所述飞行器连接到系绳,所述系绳限定具有基于所述系绳的长度的半径的系绳球,并且所述系绳连接到地面站。该方法包括将飞行器定位在基本上在系绳球上的第一位置。该方法包括将飞行器从悬停飞行方向转变为前向飞行方向,以使飞行器从系绳球运动。并且该方法包括以向前飞行的方向操作飞行器以以上升角上升到基本上在系绳球上的第二位置。第一和第二位置基本上在地面站的顺风处。

著录项

  • 公开/公告号PT3046835T

    专利类型

  • 公开/公告日2019-09-06

    原文格式PDF

  • 申请/专利权人 MAKANI TECHNOLOGIES LLC;

    申请/专利号PT20140843632T

  • 发明设计人 ERIK CHRISTOPHER CHUBB;DAMON VANDER LIND;

    申请日2014-09-15

  • 分类号B64C31/06;B64B1/66;

  • 国家 PT

  • 入库时间 2022-08-21 12:00:58

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