AUTONOMOUS UNMANNED AERIAL VEHICLE DECISION-MAKING
    181.
    发明公开
    AUTONOMOUS UNMANNED AERIAL VEHICLE DECISION-MAKING 审中-公开
    新加坡欧洲自由行政管理委员会

    公开(公告)号:EP3101502A3

    公开(公告)日:2017-01-25

    申请号:EP16160403.8

    申请日:2016-03-15

    Abstract: A method and apparatus for autonomously managing operation of an unmanned aerial vehicle (202). Sensor data (228) is received by a computer system (224) located onboard the unmanned aerial vehicle (202). The sensor data (228) is processed by the computer system (224) to generate information of interest (230) related to at least one target, while the unmanned aerial vehicle (202) is out of a communications range (218) of a control station (210). A number of actions (225) to be performed is identified by the computer system (224) based on the information of interest (230) related to the at least one target, while the unmanned aerial vehicle (202) is out of the communications range (218) of the control station (210).

    Abstract translation: 一种用于自主管理无人驾驶飞行器(202)的操作的方法和装置。 传感器数据(228)由位于无人驾驶飞行器(202)上的计算机系统(224)接收。 传感器数据(228)由计算机系统(224)处理以产生与至少一个目标相关的感兴趣的信息(230),而无人驾驶飞行器(202)不在控制器的通信范围(218)内 站(210)。 基于与至少一个目标有关的感兴趣的信息(230),无人驾驶飞行器(202)在通信范围之外,由计算机系统(224)识别要执行的多个动作(225) (218)。

    Aerial photogrammetry and aerial photogrammetric system
    187.
    发明公开
    Aerial photogrammetry and aerial photogrammetric system 有权
    Luftfotogrammetrie und Luftfotogrammetriesystem

    公开(公告)号:EP2728308A3

    公开(公告)日:2014-12-17

    申请号:EP13189992.4

    申请日:2013-10-24

    Abstract: The invention provides an aerial photogrammetry by using two or more of flying vehicles each equipped with a GPS device and an image pickup unit, comprising a step of setting up two or more photographing points and of setting up a photographing point area respectively with each of the photographing points as the center, a step of measuring a position of the flying vehicle by said GPS device, a step where each of the flying vehicle reaches each corresponding photographing point area and maintains the position of the photographing point area, a step of acquiring a time when the flying vehicle finally reaches the photographing point area, a step of setting up a shutter timing time after a predetermined time from the moment when the flying vehicle has finally reached the photographing point area, and a step of taking aerial photographs by the two or more flying vehicles at the shutter timing time.

    Abstract translation: 本发明提供一种通过使用两个或更多个配备有GPS装置和图像拾取单元的飞行车辆的航空摄影测量,包括分别设置两个或更多拍摄点和设置拍摄点区域的步骤, 拍摄点为中心,通过GPS装置测量飞行器的位置的步骤,其中每个飞行器到达每个对应的拍摄点区域并维持拍摄点区域的位置的步骤,获取 飞行时间最终到达拍摄点区域的时间,从飞行器最终到达拍摄点区域的时刻开始的规定时间之后设定快门定时时间的步骤,以及由飞行时间 或更多的飞行车辆。

    SYSTEM UND VERFAHREN ZUR STEUERUNG EINES UNBEMANNTEN FLUGGERÄTS
    190.
    发明公开
    SYSTEM UND VERFAHREN ZUR STEUERUNG EINES UNBEMANNTEN FLUGGERÄTS 有权
    系统和方法,用于控制无人机

    公开(公告)号:EP2697700A1

    公开(公告)日:2014-02-19

    申请号:EP12715372.4

    申请日:2012-04-13

    Abstract: The invention relates to a geodetic measuring system (1) having a geodetic measuring unit (30), in particular a total station, a theodolite, a laser tracker or a laser scanner, having a beam source for emitting a substantially collimated optical beam (32), a base, a sighting unit which can be pivoted in a motorized manner about two axes relative to the base and is intended to orient an emission direction of the optical beam (32), and angle measurement sensors for determining the orientation of the sighting unit. The measuring system (1) also has an automotive, unmanned, controllable air vehicle (20) having an optical module (22), wherein the air vehicle (20) is designed in such a manner that the air vehicle (20) can be moved in a controlled manner and can be positioned in a substantially fixed position. An evaluation unit is also provided, wherein the evaluation unit is configured in such a manner that an actual state of the air vehicle (20), as determined by a position, an orientation and/or a change in position, can be determined in a coordinate system from interaction between the optical beam (32) and the optical module (22). The measuring system (1) has a control unit (60) for controlling the air vehicle (20), wherein the control unit (60) is configured in such a manner that control data can be produced using an algorithm on the basis of the actual state, which can be continuously determined in particular, and a defined desired state, and the air vehicle (20) can be automatically changed to the desired state, in particular to a defined tolerance range around the desired state, in a controlled manner using the control data.

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