AN UNMANNED AERIAL VEHICLE
    81.
    发明公开
    AN UNMANNED AERIAL VEHICLE 有权
    UNBEMANNTES LUFTFAHRZEUG

    公开(公告)号:EP3087003A1

    公开(公告)日:2016-11-02

    申请号:EP13900333.9

    申请日:2013-12-24

    Inventor: CHAN, Keen Ian

    Abstract: An unmanned aerial vehicle (UAV) capable of vertical and horizontal flight modes, a method of assembling a UAV, and a kit of parts for assembling a UAV. The UAV comprises an elongated wing structure having an elongated axis along the longest dimension of the elongated wing structure, the elongated wing structure having a middle location at a substantially halfway point; a connecting structure extending substantially perpendicularly from the elongated wing structure, the connecting structure being offset from the middle location of the elongated wing structure at a first position along the elongated axis; and at least three sets of propellers, wherein at least two sets of propellers are mounted on the connecting structure, and wherein at least one set of propellers is mounted at a second position offset from the middle location in an opposite direction away from the connecting structure.

    Abstract translation: 一种能够进行垂直和水平飞行模式的无人驾驶飞行器(UAV),组装无人机的方法以及组装无人机的零件套件。 无人机包括细长机翼结构,其具有沿着细长机翼结构的最长尺寸的细长轴线,细长机翼结构在大致中途点处具有中间位置; 所述连接结构从所述细长翼结构基本上垂直延伸,所述连接结构在所述细长轴线的第一位置处从所述细长翼结构的中间位置偏移; 和至少三组螺旋桨,其中至少两组螺旋桨安装在连接结构上,并且其中至少一组螺旋桨安装在远离连接结构的相反方向偏离中间位置的第二位置 。

    METHODS AND SYSTEMS FOR DETERMINING FLEET TRAJECTORIES TO SATISFY A SEQUENCE OF COVERAGE REQUIREMENTS
    82.
    发明公开
    METHODS AND SYSTEMS FOR DETERMINING FLEET TRAJECTORIES TO SATISFY A SEQUENCE OF COVERAGE REQUIREMENTS 审中-公开
    FOR运动轨迹的检测方法和系统,以满足覆盖要求的序列

    公开(公告)号:EP2939372A4

    公开(公告)日:2016-08-24

    申请号:EP13869702

    申请日:2013-11-21

    Applicant: GOOGLE INC

    Abstract: Methods and systems for determining trajectories for vehicles of a fleet of vehicles are provided. In one example, a method comprises receiving an initial location of one or more vehicles, and receiving a sequence of coverage requirements for a region and an associated period of time. The region may be divided into a plurality of landmarks and the period of time may be divided into a plurality of phases. The method also comprises determining for each of one or more phases and at least one respective landmark, a set of starting landmarks from which a vehicle could reach the respective landmark during the phase. The method further comprises determining which respective landmark that the vehicle should travel to during the one or more phases based on the sequence of coverage requirements and the set of starting landmarks for the one or more phases and the at least one respective landmark.

    Abstract translation: 提供了对车队的车辆确定性采矿轨迹的方法和系统。 在一个实施例中,一种方法包括:接收在一个或多个车辆的初始位置,以及接收的覆盖要求的序列为一个区域和时间相关联的时间段。 的区域可以被划分成路标的多元性和所述时间段可被划分成相的复数。 因此,该方法包括用于每个一个或多个相以及至少一个界标respectivement,一组开始从车辆中的相位可能到达respectivement界标的地标确定性挖掘。 该方法还包括确定挖掘其中respectivement里程碑意义的基础上,覆盖要求的顺序和设定开始的一个或多个阶段的地标和至少一个respectivement里程碑意义的一个或多个阶段中没有车辆shoulderstand出行。

    DRONE HAUTE ALTITUDE
    83.
    发明公开
    DRONE HAUTE ALTITUDE 有权
    DROHNEFÜRGROSSEHÖHEN

    公开(公告)号:EP2996937A1

    公开(公告)日:2016-03-23

    申请号:EP14732257.2

    申请日:2014-05-09

    Applicant: Ridengineering

    Inventor: JONIOT, Jacques

    Abstract: The invention relates to a drone comprising: two contra-rotating annular propellers (2, 4) defining a plane therebetween which is referred to as an equatorial plane and is assumed to be horizontal, means for driving the propellers, a load arranged below the equatorial plane, and means (20) for moving the load relative to the equatorial plane, an enclosure referred to as an upper enclosure (6) filled with a gas or a gaseous mixture having a density of less than 1 and arranged essentially above the equatorial plane, and an enclosure referred to as a lower enclosure (8) filled with a gas or a gaseous mixture having a density of less than 1 and arranged essentially below the equatorial plane, the load being placed inside the lower enclosure (8).

    Abstract translation: 无人机技术领域本发明涉及一种无人机,包括:两个反向转动的环形螺旋桨(2,4),在其间限定一个平面,被称为赤道平面,并被假设为水平的,用于驱动螺旋桨的装置,设置在赤道 平面和用于相对于赤道平面移动负载的装置(20),被称为上部外壳(6)的外壳,其填充有密度小于1且基本上位于赤道平面上方的气体或气体混合物 ,以及被称为下部外壳(8)的外壳,其中填充有密度小于1且基本上位于赤道平面下方的气体或气体混合物,负载被放置在下部外壳内。

    Seamless replacement of a first drone base station with a second drone base station
    84.
    发明公开
    Seamless replacement of a first drone base station with a second drone base station 有权
    Nahtloser Austausch einer ersten Drohnenbasisstation mit einer zweiten Drohnenbasisstation

    公开(公告)号:EP2978258A1

    公开(公告)日:2016-01-27

    申请号:EP14290212.1

    申请日:2014-07-22

    Applicant: ALCATEL LUCENT

    Abstract: A method is provided of replacing a first drone base station with a second drone base station, the first drone base station, the method comprising: sending by the first drone base station first pilot signals indicating a cell identifier; receiving by the first drone base station information that the second drone base station is in the vicinity of the first drone base station; sending by the second drone base station second pilot signals which indicate the same cell identifier as the first drone base station; receiving by the first drone base station from the second drone base station an indication to cease to send first pilot signals; and dependent upon receiving by the first drone base station from the second drone base station the indication to cease to send first pilot signals, ceasing by the first drone base station the sending of first pilot signals.

    Abstract translation: 提供一种用第二无人机基站替代第一无人机基站的方法,所述第一无人机基站,所述方法包括:由所述第一无人机基站发送指示小区标识符的第一导频信号; 由第一无人机基站接收第二无人机基站在第一无人机基站附近的信息; 由第二无人机基站发送指示与第一无人机基站相同的小区标识符的第二导频信号; 由第一无人机基站从第二无人机基站接收停止发送第一导频信号的指示; 并且取决于第一无人机基站从第二无人机基站接收到停止发送第一导频信号的指示,由第一无人机基站停止发送第一导频信号。

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