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    METHODS AND APPARATUS TO COOPERATIVELY LIFT A PAYLOAD
    21.
    发明公开
    METHODS AND APPARATUS TO COOPERATIVELY LIFT A PAYLOAD 审中-公开
    共同提升有效载荷的方法和设备

    公开(公告)号：EP3210886A1

    公开(公告)日：2017-08-30

    申请号：EP17165314.0

    申请日：2014-09-18

    Applicant: The Boeing Company

    Inventor： Jones, Richard Donovan ,  Duffy, Michael J.

    IPC: B64C39/02 ,  B64D1/22 ,  G05D1/08 ,  G05D1/10

    CPC classification number: B64C19/02 ,  B64C39/024 ,  B64C2201/128 ,  B64C2201/143 ,  B64C2201/145 ,  B64D1/22 ,  G05D1/0858 ,  G05D1/104

    Abstract: Methods and apparatus to cooperatively lift a payload (110) are disclosed. An example method to control a lift vehicle (102) includes determining (704) a first positional state of the lift vehicle (102) with respect to a payload (110) controlled by a plurality of lift vehicles (102, 104, ...) including the lift vehicle (102), determining (706) a second positional state of the lift vehicle (102) with respect to a goal location, detecting distances (708) to the other ones of the plurality of lift vehicles (102, 104, ...), determining (710) a third positional state of the lift vehicle (102) based on the distances to the other ones of the plurality of lift vehicles (102, 104, ...), and calculating (712-720) a control command to control the lift vehicle (102) based on the first positional state, the second positional state, and the third positional state.

    Abstract translation: 公开了协作地提升有效载荷（110）的方法和装置。 控制升降车辆（102）的示例方法包括确定（704）升降车辆（102）相对于由多个升降车辆（102,104，...）控制的有效载荷（110）的第一位置状态。 ）包括所述提升车辆（102），确定（706）所述提升车辆（102）相对于目标位置的第二位置状态，检测到所述多个提升车辆（102,104）中的其他提升车辆 ，...），基于到多个升降车辆（102,104，...）中的其他升降车辆的距离来确定（710）升降车辆（102）的第三位置状态，并且计算（712- 720）基于所述第一位置状态，所述第二位置状态和所述第三位置状态来控制所述提升车辆（102）的控制命令。

    개인용 감각 드론
    25.
    发明公开
    개인용 감각 드론 审中-公开
    个人感官无人机

    公开(公告)号：KR20180012876A

    公开(公告)日：2018-02-06

    申请号：KR20187002267

    申请日：2016-05-25

    IPC: G05D1/00 ,  G05D1/02

    CPC classification number: G05D1/0027 ,  B64C2201/123 ,  B64C2201/143 ,  G05D1/0038 ,  G05D1/005 ,  G05D1/104 ,  G06T11/60 ,  H04N5/232 ,  H04N5/23293 ,  H04N7/185

    Abstract: 개인용감각드론을위한다양한시스템및 방법이여기서설명된다. 개인용감각드론시스템은, 드론집단―드론집단은적어도 2개의드론을포함함―이 실행할작업을드론집단에전송하는작업모듈; 작업에관련된정보를드론집단으로부터수신하는트랜시버; 및드론집단으로부터수신된정보에기초하여사용자인터페이스를프리젠팅하는사용자인터페이스모듈을포함하는드론원격제어시스템을포함한다.

    Abstract translation: 本文描述了用于个人传感无人机的各种系统和方法。 一种个人感应无人机系统，包括：任务模块，用于向无人机组发送待执行任务，其中，所述无人机组 - dron组包括至少两个无人驾驶飞机; 收发器，用于从一组无人机接收与任务有关的信息; 以及用户界面模块，用于基于从无人机组接收到的信息来呈现用户界面。

    SYSTÈME ET PROCÉDÉ D'INSPECTION AUTOMATIQUE DE SURFACE
    26.
    发明公开
    SYSTÈME ET PROCÉDÉ D'INSPECTION AUTOMATIQUE DE SURFACE 审中-公开
    用于自动表面检查的系统和方法

    公开(公告)号：EP3308232A1

    公开(公告)日：2018-04-18

    申请号：EP16741082.8

    申请日：2016-06-15

    Applicant: Donecle

    Inventor： CLAYBROUGH, Matthieu

    IPC: G05D1/00 ,  G01C11/02 ,  B25J19/02

    CPC classification number: B64C39/024 ,  B64C2201/12 ,  B64C2201/123 ,  B64C2201/143 ,  B64F5/60 ,  G05D1/0094 ,  G05D1/104

    Abstract: The invention relates to a system for automatically inspecting a surface of an object such as an aircraft (54), a transporting vehicle, a building or a work of art, said surface being liable to contain a defect. The system is characterized in that it comprises a fleet comprising at least one drone (14a, 14b, 14c), each drone comprising a module for acquiring images of at least one section of the surface to be inspected, and a module for processing the acquired images, which module is suitable for delivering a piece of information representative of the state of each inspected surface portion, which piece of information is called the result of the processing.

    FLYING DRONE TRAJECTORY SYNCHRONIZATION
    27.
    发明公开
    FLYING DRONE TRAJECTORY SYNCHRONIZATION 审中-公开
    特洛伊同步化einer fliegenden Drohne

    公开(公告)号：EP2927771A1

    公开(公告)日：2015-10-07

    申请号：EP14305488.0

    申请日：2014-04-03

    Applicant: Puy du Fou International ,  ACT Lighting Design

    Inventor： Vermeulen, Koert ,  Buys, Koen

    IPC: G05D1/10 ,  G08G5/00

    CPC classification number: G08G5/0069 ,  B64C2201/143 ,  G05D1/101 ,  G08G5/045

    Abstract: A flying drone (10) comprises a memory (16) for storing a forecasted flying trajectory, said trajectory being defined by a list (26) of 3D coordinates points, and a control and command computer (18) for driving drone directional and motorization means, said control and command computer (18) being connected to the memory (16) for reading the forecasted trajectory so that the flying drone (10) is able to move along said forecasted trajectory. The flying drone (10) further comprises:
    • a wireless receptor (20) able to receive a synchronization signal (28) emitted from a timecode (38);
    • the 3D coordinates points are associated to a timeline; and
    • the control and command computer (18) is adapted for synchronizing the flying drone timeline with the synchronization signal (28).

    Abstract translation: 飞行无人机（10）包括用于存储预测的飞行轨迹的存储器（16），所述轨迹由3D坐标点的列表（26）定义，以及用于驱动无人机方向和机动化装置的控制和命令计算机（18） 所述控制和命令计算机（18）连接到用于读取预测轨迹的存储器（16），使得飞行无人机（10）能够沿所述预测的轨迹移动。 飞行无人机（10）还包括：无线接收器（20），其能够接收从时间码（38）发射的同步信号（28）; ¢3D坐标点与时间轴相关联; 和控制和命令计算机（18）适于使飞行无人机时间线与同步信号（28）同步。

    Methods and apparatus to cooperatively lift a payload
    28.
    发明公开
    Methods and apparatus to cooperatively lift a payload 有权
    Verfahren und Vorrichtung zum gemeinsamen Anheben einer Nutzlast

    公开(公告)号：EP2881324A1

    公开(公告)日：2015-06-10

    申请号：EP14185249.1

    申请日：2014-09-18

    Applicant: The Boeing Company

    Inventor： Jones, Richard Donovan ,  Duffy, Michael J.

    IPC: B64C39/02 ,  B64D1/22

    CPC classification number: B64C19/02 ,  B64C39/024 ,  B64C2201/128 ,  B64C2201/143 ,  B64C2201/145 ,  B64D1/22 ,  G05D1/0858 ,  G05D1/104

    Abstract: Methods and apparatus to cooperatively lift a payload (110) are disclosed. An example method to control a lift vehicle (102) includes determining (704) a first positional state of the lift vehicle (102) with respect to a payload (110) controlled by a plurality of lift vehicles (102, 104, ...) including the lift vehicle (102), determining (706) a second positional state of the lift vehicle (102) with respect to a goal location, detecting distances (708) to the other ones of the plurality of lift vehicles (102, 104, ...), determining (710) a third positional state of the lift vehicle (102) based on the distances to the other ones of the plurality of lift vehicles (102, 104, ...), and calculating (712-720) a control command to control the lift vehicle (102) based on the first positional state, the second positional state, and the third positional state.

    Abstract translation: 公开了协同提升有效载荷（110）的方法和装置。 控制升降车（102）的示例性方法包括：确定（704）相对于由多个升降车（102,104，...）控制的有效载荷（110）的升降车（102）的第一位置状态 （102）相对于目标位置确定（706）第二位置状态，检测距离多个提升车辆（102,104）中的其他乘客（102,104）的距离（708） ，...），基于与所述多个电梯车辆（102,104，...）中的其他电梯车辆的距离来确定（710）所述电梯车辆（102）的第三位置状态，并且计算（712- 720）基于第一位置状态，第二位置状态和第三位置状态来控制提升车辆（102）的控制命令。

    Systems and methods for moving a load using unmanned vehicles
    29.
    发明公开
    Systems and methods for moving a load using unmanned vehicles 有权
    用于通过使用无人驾驶车辆移动的负载的系统和方法

    公开(公告)号：EP2813915A3

    公开(公告)日：2015-06-03

    申请号：EP14166365.8

    申请日：2014-04-29

    Applicant: The Boeing Company

    Inventor： Jenkins, Kevin M.

    IPC: G05D1/10 ,  B64C39/02 ,  B64C27/00 ,  B60P3/00 ,  B63B21/56 ,  B64D3/00

    CPC classification number: B64D3/00 ,  B60P3/00 ,  B63B21/56 ,  B64C39/024 ,  B64C2201/128 ,  B64C2201/143 ,  B64C2201/145 ,  G05D1/104

    Abstract: An actual position of a load tethered with a tether to a vehicle is determined using a plurality of sensors disposed on the vehicle. A required tether tension and required tether angle of the tether is determined to move the load from the actual position to a commanded position. An actual tether tension and actual tether angle of the tether is determined using the plurality of sensors. A determination is made as to a thrust vector to be applied by the vehicle to change the actual tether tension and the actual tether angle of the tether to the required tether tension and the required tether angle. The thrust vector is applied with the vehicle to reposition the vehicle to achieve the required tether angle and to create the required tether tension of the tether to move the load to the commanded position.

    MODULAR ARTICULATED-WING AIRCRAFT
    30.
    发明公开
    MODULAR ARTICULATED-WING AIRCRAFT 有权
    带翅膀的链接模块化飞机

    公开(公告)号：EP1924495A4

    公开(公告)日：2012-08-22

    申请号：EP06851409

    申请日：2006-06-28

    Applicant: SOMMER GEOFFREY S

    Inventor： SOMMER GEOFFREY S

    IPC: B64C37/02 ,  B64C39/02

    CPC classification number: B64C39/024 ,  B64C37/02 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/143 ,  B64C2201/165 ,  B64C2201/206

    Abstract: Systems and/or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are provided. In certain exemplary embodiments, autonomous modular flyers join together in a wingtip-to-wingtip manner. Such modular flyers may derive their power from insolation. The autonomous flyers may include sensors which operate individually, or collectively after a skybase is formed. The skybase preferably may be aggregated, disaggregated, and/or re-aggregated as called for by the prevailing conditions. Thus, it may be possible to provide a “forever-on-station” aircraft.

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