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    SYSTEM AND METHOD FOR CONTROLLING AUTONOMOUS FLYING VEHICLE FLIGHT PATHS
    301.
    发明公开
    SYSTEM AND METHOD FOR CONTROLLING AUTONOMOUS FLYING VEHICLE FLIGHT PATHS 审中-公开
    用于控制自主飞行飞行器飞行路径的系统和方法

    公开(公告)号：EP3241205A2

    公开(公告)日：2017-11-08

    申请号：EP15876241.9

    申请日：2015-12-30

    Applicant: Airmap Inc.

    Inventor： MARCUS, Benjamin Daniel

    IPC: G08G5/00 ,  B64C39/02

    CPC classification number: G08G5/0034 ,  B64C39/024 ,  B64C2201/123 ,  B64C2201/141 ,  G08G5/0008 ,  G08G5/0013 ,  G08G5/0039 ,  G08G5/006 ,  G08G5/0069 ,  G08G5/0078 ,  G08G5/0091

    Abstract: A method is provided for limiting access to airspace by drones. The method includes receiving position information from a user associated with a property identified by the position information. The method also includes assembling the position information with other position information to compile a comprehensive configurable flight zone database. The method further includes pushing the configurable flight zone database to at least one drone. The drone accesses the configurable flight zone database to determine if movement is allowed, and the drone is programmed to not fly into areas identified in the configurable flight zone database. In the method, the drone may be further programmed to prohibit directing a camera into the areas identified in the configurable flight zone database.

    UNMANNED AERIAL VEHICLE FLIGHT CONTROL SYSTEM
    302.
    发明公开
    UNMANNED AERIAL VEHICLE FLIGHT CONTROL SYSTEM 审中-公开

    公开(公告)号：EP3223097A2

    公开(公告)日：2017-09-27

    申请号：EP17159813.9

    申请日：2017-03-08

    Applicant: The Boeing Company

    Inventor： RANGARAJAN, Murali

    IPC: G05D1/00

    CPC classification number: G05D1/0055 ,  B64C39/024 ,  B64C2201/141 ,  B64D2045/0085 ,  B64F5/60

    Abstract: An onboard system for controlling flight of an unmanned aerial vehicle (10). The system comprises: a flight management system (40) configured for controlling flight of the unmanned aerial vehicle (10); a mission control module (2) configured to send commands to the flight management system (40) for guiding the unmanned aerial vehicle (10) to perform a mission; a safety module (8) configured to communicate commands to the flight management system (40) for guiding the unmanned aerial vehicle (10) to fly in a safe mode; a communication control component (6) which is switchable between a mission state in which the flight management system (40) receives commands from the mission control module (2) and a safety state in which the flight management system (40) receives commands from the safety module (8); and a monitor module (4) configured to determine whether a trigger condition warranting a change in mode is present or not and to cause the communication control component (6) to switch from the mission state to the safety state when the trigger condition is present.

    AN UNMANNED AERIAL VEHICLE
    303.
    发明公开
    AN UNMANNED AERIAL VEHICLE 有权
    UNBEMANNTES LUFTFAHRZEUG

    公开(公告)号：EP3087003A4

    公开(公告)日：2017-09-13

    申请号：EP13900333

    申请日：2013-12-24

    Applicant: SINGAPORE TECH AEROSPACE LTD

    Inventor： CHAN KEEN IAN

    IPC: B64C29/02 ,  A63H27/127 ,  A63H27/133 ,  A63H27/18 ,  B64C11/48 ,  B64C39/02

    CPC classification number: B64C29/02 ,  A63H27/12 ,  B64C11/48 ,  B64C27/08 ,  B64C27/10 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/122 ,  B64C2201/141

    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: 一种能够纵向和横向飞行模式的无人驾驶飞行器（UAV），一种组装无人飞行器的方法和一套用于组装无人飞行器的部件。 无人飞行器包括细长机翼结构，细长机翼结构具有沿着细长机翼结构的最长尺寸的细长轴线，细长机翼结构具有在大体中途点处的中间位置; 连接结构，所述连接结构从所述细长机翼结构大致垂直地延伸，所述连接结构在所述细长机翼结构的中间位置沿着所述细长轴线在第一位置处偏移; 以及至少三组螺旋桨，其中至少两组螺旋桨安装在所述连接结构上，并且其中至少一组螺旋桨安装在第二位置，所述第二位置偏离所述中间位置在远离所述连接结构的相反方向上 。

    FIXED DRONE VISUALIZATION IN SECURITY SYSTEMS
    304.
    发明公开
    FIXED DRONE VISUALIZATION IN SECURITY SYSTEMS 审中-公开
    安全系统中的固定无效可视化

    公开(公告)号：EP3207435A1

    公开(公告)日：2017-08-23

    申请号：EP15720569.1

    申请日：2015-10-16

    Applicant: Tyco Fire & Security GmbH

    Inventor： MUCCI, Anthony

    IPC: G05D1/00 ,  G05D1/10 ,  G08B17/00 ,  G08B17/12

    CPC classification number: B64C39/024 ,  B64C2201/127 ,  B64C2201/141 ,  G05D1/0094 ,  G06Q50/26 ,  G08B13/19695 ,  G08B25/001 ,  G08B25/08 ,  G08B29/185

    Abstract: An unmanned aerial vehicle is described and includes a computer carried by the unmanned aerial vehicle to control flight of the unmanned aerial vehicle and at least one sensor. The unmanned aerial vehicle is caused to fly to a specific location within a facility, where the unmanned aerial vehicle enters a hover mode, where the unmanned aerial vehicle remains in a substantially fixed location hovering over the specific location within the facility and sends raw or processing results of sensor data from the sensor to a remote server system.

    Abstract translation: 描述了一种无人驾驶飞行器，其包括由无人驾驶飞行器携带的用于控制无人驾驶飞行器和至少一个传感器的飞行的计算机。 使无人驾驶飞行器飞到设施内的特定位置，无人驾驶飞行器进入悬停模式，其中无人驾驶飞行器保持在设施内的特定位置上的大致固定位置，并发送原始或处理 传感器数据从传感器到远程服务器系统的结果。

    AIRCRAFT INFORMATION RETRIEVAL USING ONBOARD RFID TAGS
    305.
    发明公开
    AIRCRAFT INFORMATION RETRIEVAL USING ONBOARD RFID TAGS 审中-公开
    飞机信息检索使用在线RFID标签

    公开(公告)号：EP3193287A1

    公开(公告)日：2017-07-19

    申请号：EP16190037.8

    申请日：2016-09-22

    Applicant: The Boeing Company

    Inventor： GLATFELTER, John William

    IPC: G06Q10/00 ,  G06Q50/30 ,  B64F5/60 ,  G07C5/00

    CPC classification number: G05D1/0011 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/141 ,  B64F5/60 ,  G05D1/101 ,  G06K7/10366 ,  G06Q10/20 ,  G06Q50/30 ,  G07C5/00

    Abstract: A method for determining information about an aircraft (202) may include receiving at a base station (206) an RFID tag location map (244) for the aircraft (202) and transmitting to an unmanned aerial vehicle (UAV) (204) the RFID tag location map (244) for the aircraft (202). The method may include generating navigation signals by the UAV (204) based at least in part on the received RFID tag location map (244) appropriate for controlling navigation of the UAV (204) proximate to an RFID tag (213) supported on the aircraft (202) at an RFID tag location, the RFID tag (213) having aircraft-related identifying data. The method may include receiving, by the base station (206), read-related data (266) from the UAV (204). The read-related data (266) may include aircraft-related identifying data when the RFID tag (213) is at the RFID tag location. The method may include determining, at the base station (206) from the received read-related data (266), information about the aircraft (202).

    Abstract translation: 用于确定关于飞行器（202）的信息的方法可以包括在基站（206）处接收飞机（202）的RFID标签位置图（244）并且将RFID（无人飞行器）（204）发送到无人驾驶飞行器 用于飞机（202）的标签位置图（244）。 该方法可以包括至少部分地基于接收到的RFID标签位置图（244）由UAV（204）生成导航信号，所述RFID标签位置图适合于控制UAV（204）接近支撑在飞机上的RFID标签（213） （202）处于RFID标签位置处，所述RFID标签（213）具有与飞机相关的识别数据。 该方法可以包括由基站（206）从UAV（204）接收读取相关数据（266）。 当RFID标签（213）位于RFID标签位置时，读取相关数据（266）可以包括与飞机相关的识别数据。 该方法可以包括在基站（206）从所接收的读取相关数据（266）确定关于飞行器（202）的信息。

    UNMANNED HELICOPTER
    307.
    发明公开
    UNMANNED HELICOPTER 审中-公开
    无人直升机

    公开(公告)号：EP3147210A3

    公开(公告)日：2017-05-10

    申请号：EP16190742.3

    申请日：2016-09-27

    Applicant: Ewatt Technology Co., Ltd.

    Inventor： ZHAO, Guocheng ,  LUO, Wei ,  QI, Pengcheng

    IPC: B64C27/04 ,  B64C27/82 ,  B64C39/02 ,  B64D33/02 ,  B64D33/04 ,  B64D33/08

    CPC classification number: B64D33/02 ,  B64C27/82 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/044 ,  B64C2201/141 ,  B64C2201/146 ,  B64D27/08 ,  B64D33/06 ,  B64D33/08 ,  B64D2033/0246 ,  B64D2033/028

    Abstract: The present invention discloses an unmanned helicopter, and belongs to the technical field of unmanned aerial vehicles. The unmanned helicopter includes an air inlet system, an exhaust system, a cooling system and a dynamic balance system. The air inlet system is fixed on a second side; the exhaust system is fixed on a third side; and the cooling system is fixed on a first side, and the dynamic balance system is fixed on a tail. The airflow at the outside of the unmanned helicopter flows into the air inlet system smoothly, quickly and efficiently under the action of its own flow velocity relative to the unmanned helicopter, therefore the technical problem in the prior art that the air entering the fuselage with a unit volume is burnt insufficiently, which generates adverse effects on the normal flight of the unmanned helicopter, is solved.

    Abstract translation: 本发明公开了一种无人直升机，属于无人机技术领域。 无人直升机包括进气系统，排气系统，冷却系统和动态平衡系统。 进气系统固定在第二侧， 排气系统固定在第三侧， 冷却系统固定在第一侧，动平衡系统固定在尾部。 无人直升机外侧的气流在相对于无人直升机自身流速的作用下平稳，快速，有效地流入进气系统，因此现有技术中空气进入机身的技术问题 解决了单位体积燃烧不足，对无人直升机正常飞行造成不利影响的问题。

    SELECTIVE PROCESSING OF SENSOR DATA
    309.
    发明公开
    SELECTIVE PROCESSING OF SENSOR DATA 审中-公开
    SELEKTIVE VERARBEITUNG VON SENSORDATEN

    公开(公告)号：EP3123260A4

    公开(公告)日：2017-04-05

    申请号：EP14909276

    申请日：2014-12-31

    Applicant: SZ DJI TECHNOLOGY CO LTD

    Inventor： WANG TAO ,  YAN JIAQI

    IPC: G05D1/10 ,  G06T7/246 ,  G06T7/73

    CPC classification number: G05D1/101 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/146 ,  B64D47/08 ,  G01C21/20 ,  G06K9/0063 ,  G06K2009/366 ,  G06T7/246 ,  G06T7/73 ,  G06T2207/10032 ,  G06T2207/30252 ,  H04N5/23238 ,  H04N5/243 ,  H04N7/181 ,  H04N7/185

    Abstract: Systems and methods for navigating a vehicle within an environment are provided. In one aspect, a method comprises: (a) selecting, with aid of a processor, a subset of a plurality of sensors to be used for navigating the vehicle within the environment based on one or more predetermined criteria, wherein the plurality of sensors are arranged on the vehicle such that each sensor of the plurality of sensors is configured to obtain sensor data from a different field of view; (b) processing, with aid of the processor, the sensor data from the selected sensor(s) so as to generate navigation information for navigating the vehicle within the environment; and (c) outputting, with aid of the processor, signals for controlling the vehicle based on the navigation information.

    Abstract translation: 提供了用于在环境内导航车辆的系统和方法。 在一个方面，一种方法包括：（a）在处理器的帮助下，基于一个或多个预定标准，选择要用于在环境内导航车辆的多个传感器的子集，其中所述多个传感器是 布置在所述车辆上，使得所述多个传感器中的每个传感器被配置为从不同的视场获得传感器数据; （b）在处理器的帮助下处理来自所选传感器的传感器数据，以便生成用于在环境内导航车辆的导航信息; 和（c）在处理器的帮助下，基于导航信息输出用于控制车辆的信号。

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