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1.发明公开METHODS AND SYSTEMS FOR TRANSITIONING AN AERIAL VEHICLE BETWEEN CROSSWIND FLIGHT AND HOVER FLIGHT 审中-公开方法和系统用于飞机之间的飞行遭遇侧风HOVER TRANSFER
公开(公告)号：EP3046836A1
公开(公告)日：2016-07-27
申请号：EP14844368.2
申请日：2014-09-15
Applicant: Google Inc.
Inventor： CHUBB, Erik Christopher , LIND, Damon Vander
Abstract: A method may involve operating an aerial vehicle in a hover-flight orientation. The aerial vehicle may be connected to a tether that defines a tether sphere having a radius based on a length of the tether, and the tether may be connected to a ground station. The method may involve positioning the aerial vehicle at a first location that is substantially on the tether sphere. The method may involve 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 may involve 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 may be substantially downwind of the ground station.
Abstract translation: 一种方法涉及悬停飞行方向上的飞行器运行。 飞行器被连接到系链那样定义具有基于所述系绳的长度为半径的系绳球体，并且系绳连接到地面站。 该方法包括在第一位置处定位所述飞行器所做的是基本上在系绳球体。 该方法包括从悬停飞行方向的飞行器过渡到向前飞行方向，寻求做与拴系领域的飞行器移动。 并且该方法涉及在该系绳球体操作在向前飞行取向处上升的角度来提升到第二位置飞行器并基本上。 所述第一和第二位置是基本上顺风地面站。
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2.发明公开METHODS AND SYSTEMS FOR TRANSITIONING AN AERIAL VEHICLE BETWEEN HOVER FLIGHT AND CROSSWIND FLIGHT 审中-公开方法和系统之间的悬停和交叉出发飞机过渡
公开(公告)号：EP3046835A1
公开(公告)日：2016-07-27
申请号：EP14843632.2
申请日：2014-09-15
Applicant: Google Inc.
Inventor： CHUBB, Erik Christopher , LIND, Damon Vander
CPC classification number: B64C39/022 , B64C2201/021 , B64C2201/148 , F03D1/00 , F03D5/00 , F05B2240/917 , F05B2240/921 , Y02E10/70 , Y02E10/728
Abstract: 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.
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