Methods and systems for transitioning an aerial vehicle between crosswind flight and hover flight

    公开(公告)号:AU2014318448A1

    公开(公告)日:2016-02-18

    申请号:AU2014318448

    申请日:2014-09-15

    Applicant: GOOGLE INC

    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.

    Methods and systems for transitioning an aerial vehicle between hover flight and crosswind flight

    公开(公告)号:AU2014318437A1

    公开(公告)日:2016-02-18

    申请号:AU2014318437

    申请日:2014-09-15

    Applicant: GOOGLE INC

    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.

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