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21. 发明公开

EP3346441A1 METHOD, USER TERMINAL, SERVER, AND DETECTING DEVICE FOR MONITORING FLIGHT OF UNMANNED AERIAL VEHICLE 审中-公开
公开(公告)号：EP3346441A1
公开(公告)日：2018-07-11
申请号：EP16842145.1
申请日：2016-08-12
申请人： Yu, Seong Hun
发明人： Yu, Seong Hun
IPC分类号： G06Q50/26 , G06Q50/10 , B64C39/02
CPC分类号： G08G5/0026 , B64C39/02 , B64C39/024 , B64C2201/14 , G06F17/30241 , G06Q50/10 , G06Q50/26 , G08G5/0082
摘要： According to an aspect of the present invention, a method for monitoring the flight of an unmanned aerial vehicle is provided, the method comprising the steps of: (a) when a user terminal or detecting device is located within a predetermined distance range from at least one unmanned aerial vehicle and acquires at least one piece of identification information from each of the at least one unmanned aerial vehicle, receiving, by a server, the acquired at least one piece of identification information from the user terminal or the detecting device; and (b) transmitting, by the server, detailed information on the unmanned aerial vehicle corresponding to the received at least one piece of identification information to the user terminal or detecting device, so as to support the user terminal or detecting device to provide the same to the user.

22. 发明公开

EP3336826A1 FLIGHT PLAN ANALYSIS SYSTEMS AND METHODS FOR UNMANNED AERIAL VEHICLES 有权转让
公开(公告)号：EP3336826A1
公开(公告)日：2018-06-20
申请号：EP17203858.0
申请日：2017-11-27
申请人： The Boeing Company
发明人： CLARK, Jason W. , FERMON, Andres Chapiro , PRICE, Matthew Robert , HATZENBUEHLER, Jonas
IPC分类号： G08G5/00 , B64C39/02 , G01C21/00 , G05D1/00
CPC分类号： G08G5/003 , B64C39/02 , B64C39/024 , B64C2201/14 , B64C2201/141 , G01C21/20 , G08G5/0034 , G08G5/0039 , G08G5/0069
摘要： A flight plan analysis system is configured to determine a flight plan decision regarding a proposed flight plan for an unmanned aerial vehicle (UAV). The flight plan analysis system includes a flight plan database that stores risk factor data, and a flight plan analysis unit communicatively coupled to the flight plan database. The flight plan analysis unit receives a proposed flight plan for the UAV and determines the flight plan decision based on an analysis of the proposed flight plan and the risk factor data.

23. 发明公开

EP3313731A1 CONTROL AERIAL MOVEMENT OF DRONE BASED ON LINE-OF-SIGHT OF HUMANS USING DEVICES 有权
标题翻译：利用器件控制基于人眼视线的无人机空中运动
公开(公告)号：EP3313731A1
公开(公告)日：2018-05-02
申请号：EP15896516.0
申请日：2015-06-24
申请人： Ent. Services Development Corporation LP
发明人： KAMALAKANTHA, Chandra H. , DOSHI, Parag
IPC分类号： B64C39/02 , B64D43/00 , B64D45/00 , H04Q9/00
CPC分类号： G05D1/0088 , B64C39/024 , B64C2201/127 , B64C2201/128 , B64C2201/14 , B64C2201/145 , G05D1/0094 , G08C17/00 , G08C17/02 , G08C2201/51 , G08C2201/93
摘要： Examples disclosed herein relate to control of a drone. In one example, aerial movement of the drone is controlled. In the example, it is determined, based on a plurality of devices, whether the drone is within a line-of-sight with at least a respective one of a plurality of humans within a physical proximity to a respective one of a the devices. In the example, the devices are used by the drone to track the humans. In the example, when the drone is determined to lack the line-of-sight, aerial movement of the drone is controlled to move the drone to become within the line-of-sight.

24. 发明公开

EP3274255A1 ROUTE PLANNING FOR UNMANNED AERIAL VEHICLES 审中-公开
标题翻译：无人机的路线规划
公开(公告)号：EP3274255A1
公开(公告)日：2018-01-31
申请号：EP16769780.4
申请日：2016-03-25
申请人： Matternet, Inc.
发明人： HINKLE, Christopher , RAPTOPOULOS, Andreas , LARSEN, Kendall , BARUCHIN, Ido
IPC分类号： B64C37/00 , B64C37/02 , B64C39/02 , G05D1/00 , G05D1/08 , G05D1/12 , H04W4/02
CPC分类号： G08G5/0034 , B64C39/024 , B64C2201/00 , B64C2201/027 , B64C2201/14 , G01C21/20 , G08G5/0013 , G08G5/0026 , G08G5/0039 , G08G5/006 , G08G5/0069
摘要： A system and process for dynamically determining a route for an unmanned aerial vehicle (UAV) is provided. In one example, at a computer system including one or more processors and memory, the process includes receiving a route request, the route request including an origin location and destination location for a UAV, receiving geospatial information associated with the origin location and the destination location, the geospatial information comprising at least one of physical obstacles and no-fly zones, determining a route of the UAV from the origin location to the destination location based at least in part on the geo-spatial information, and causing the route to be communicated to the UAV.

25. 发明公开

EP3183170A1 SURFACE CLEANING UNMANNED AERIAL VEHICLE 无效
标题翻译：表面清洁无人机飞行器
公开(公告)号：EP3183170A1
公开(公告)日：2017-06-28
申请号：EP15833197.5
申请日：2015-08-18
申请人： ELWHA, LLC
发明人： CHIN, Hon Wah , GROSS, William , HYDE, Roderick A. , KARE, Jordin T. , MYHRVOLD, Nathan P. , PETROSKI, Robert C. , TEGREENE, Clarence T. , WOOD, Lowell L., Jr.
IPC分类号： B64C39/02 , B64D47/00 , B64C27/08 , B64C27/20 , B64C11/00 , B64C13/20 , B64D45/00 , B64F3/02
CPC分类号： B08B5/02 , A47L1/02 , B08B1/00 , B08B1/002 , B08B3/02 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/14 , B64C2201/148 , E04G23/00 , E04G23/002 , H02G1/02
摘要： Described embodiments include an unmanned aerial vehicle and a method. The unmanned aerial vehicle includes an airframe and a rotary wing system coupled with the airframe and configured to aerodynamically lift the vehicle in the air. The unmanned aerial vehicle includes a flight controller configured to control a movement of the vehicle while airborne. The unmanned aerial vehicle includes a cleansing controller configured to manage a removal of a surface contaminant from a selected portion of a surface of an external object using an airflow generated by the rotary wing system.
摘要翻译：所描述的实施例包括无人驾驶飞行器和方法。该无人驾驶飞行器包括机身和与该机身耦合的旋翼系统，该旋翼系统配置成在空气中空气动力地提升该车辆。无人驾驶飞行器包括飞行控制器，该飞行控制器被配置为在空中传播时控制车辆的运动。无人飞行器包括清洁控制器，该清洁控制器被配置为使用由旋翼系统产生的气流来管理从外部物体的表面的选定部分移除表面污染物。

26. 发明授权

EP2780228B1 TRANSFORMABLE AERIAL VEHICLE 有权转让
标题翻译：可转换的空中车辆
公开(公告)号：EP2780228B1
公开(公告)日：2017-06-07
申请号：EP13826711.7
申请日：2013-12-25
申请人： SZ DJI Technology Co., Ltd.
发明人： ZHAO, Tao , DU, Hao , WANG, Mingxi , WANG, Tao
IPC分类号： B64C27/02 , B64C27/32 , B64C39/02 , B64C1/00 , B64C27/08 , A63H27/00 , B64C1/06 , B64D47/00 , B64D47/08 , G05D1/04
CPC分类号： B64C39/024 , A63H27/12 , B64C1/00 , B64C1/061 , B64C1/063 , B64C25/32 , B64C27/08 , B64C39/028 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/14 , B64C2201/146 , B64C2201/165 , B64D47/00 , B64D47/08 , G05D1/042
摘要： Discloses a transformable aerial vehicle (100) and a control method thereof. The transformable aerial vehicle (100) includes: a central body (10) and at least two transformable frame assemblies (20) respectively disposed on the central body (10), each of the least two transformable frame assemblies (20) having a proximal portion pivotally coupled to the central body (10) and a distal portion; an actuation assembly (13, 5) mounted on the central body (10) and configured to pivot the at least two transformable frame assemblies (20) to a plurality of different vertical angles relative to the central body (10); and a plurality of propulsion units (30) mounted on the at least two transformable frame assemblies (20) and operable to move the transformable aerial vehicle (100).
摘要翻译：提供了用于可变形的飞行器的系统，装置和方法。在一个方面，可变形的飞行器包括：中央主体和分别设置在中央主体上的至少两个可变形的框架组件，所述至少两个可变形的框架组件中的每一个具有枢转地联接到中央主体的近侧部分和远侧部分 ; 致动组件，所述致动组件安装在所述中央主体上并且构造成使所述至少两个框架组件相对于所述中央主体枢转至多个不同的竖直角度; 以及安装在所述至少两个可变形框架组件上并可操作以移动所述可变形空中交通工具的多个推进单元。

27. 发明授权

EP2909689B1 MICRO UNMANNED AERIAL VEHICLE AND METHOD OF CONTROL THEREFOR 有权
标题翻译：无人微弹箭与方法及其控制
公开(公告)号：EP2909689B1
公开(公告)日：2016-10-05
申请号：EP13785582.1
申请日：2013-10-22
申请人： BCB International Limited , Torquing Group Ltd.
发明人： REEDMAN, Ivan , DAVIES, Barry
IPC分类号： G05D1/10
CPC分类号： B64C39/024 , B64C19/00 , B64C39/028 , B64C2201/00 , B64C2201/14 , B64C2201/141 , B64C2230/00 , B64C2230/02 , G01S15/06 , G01S15/88 , G01S15/89 , G01S15/8913 , G01S15/8929 , G01S15/8993 , G01S15/93 , G05D1/0088 , G05D1/0202 , G05D1/101 , G05D1/102 , Y10S367/909

28. 发明公开

EP3031538A1 VERFAHREN ZUM STEUERN EINES UNBEMANNTEN DREHFLÜGELFLUGGERÄTS ZUR REINIGUNG WEITGEHEND GLATTER FLÄCHEN 审中-公开
标题翻译：一种用于控制无人SWING飞行机主要用于清洁光滑的表面
公开(公告)号：EP3031538A1
公开(公告)日：2016-06-15
申请号：EP15003393.4
申请日：2015-11-28
申请人： Fritzsche, Marcus
发明人： Fritzsche, Marcus
IPC分类号： B08B1/00 , A47L1/02 , B64C39/02 , F24J2/46
CPC分类号： B08B1/006 , A47L1/02 , A47L2201/04 , B08B1/008 , B64C39/024 , B64C2201/027 , B64C2201/12 , B64C2201/14
摘要： Verfahren zum Steuern eines unbemannten Drehflügelfluggeräts (8) zur Reinigung weitgehend glatter Flächen, wobei das Drehflügelfluggerät mit mindestens einem elektronischen Steuergerät (3), einer Vorrichtung zur Lokalisierung von weitgehend glatten Flächen (4), mindestens einem Energiespeicher sowie mindestens einer Reinigungsvorrichtung ausgestattet ist, und mindestens folgende Verfahrensschritte ausgeführt werden:
- Fortbewegung des Drehflügelfluggeräts zu Ort in Nähe der weitgehend glatten Fläche; und
- Erfassen der weitgehend glatten Fläche durch die Vorrichtung zur Lokalisierung; und
- Anflug und Andocken mit der Reinigungsvorrichtung, auf die erfasste weitgehend glatte Fläche; und
- Reinigen der weitgehend glatten Fläche mit der Reinigungsvorrichtung, indem mit dem elektronischen Steuergerät (3) das Drehflügelfluggerät so angesteuert wird, dass ein Anpressdruck und eine Fortbewegung in einer parallelen Richtung auf der erfassten weitgehend glatten Fläche ausgeführt werden.
摘要翻译：一种用于控制用于清洁很大程度上光滑表面无人驾驶旋翼飞行器（8）的方法，所述旋翼飞行器配备有至少一个电子控制单元（3），用于基本上光滑的表面（4），至少一个能量存储装置和至少一个清洁装置，和定位装置至少下列方法步骤被执行： - 在旋转翼飞行器的向前运动在基本上平滑的表面附近放置; 和 - 检测由用于定位该装置的基本上平滑的表面; 和 - 的方法和与之对接的清洗装置所检测到的大致光滑的表面; 以及 - 由所述旋翼飞行器纯化大致光滑的表面与清洁装置被控制，以便与所述电子控制单元（3），即执行在平行的方向上检测到的大致光滑的表面的压力和运动。

29. 发明公开

EP2909689A2 MICRO UNMANNED AERIAL VEHICLE AND METHOD OF CONTROL THEREFOR 有权
标题翻译：无人微弹箭与方法及其控制
公开(公告)号：EP2909689A2
公开(公告)日：2015-08-26
申请号：EP13785582.1
申请日：2013-10-22
申请人： BCB International Limited , Torquing Group Ltd.
发明人： REEDMAN, Ivan , DAVIES, Barry
IPC分类号： G05D1/10
CPC分类号： B64C39/024 , B64C19/00 , B64C39/028 , B64C2201/00 , B64C2201/14 , B64C2201/141 , B64C2230/00 , B64C2230/02 , G01S15/06 , G01S15/88 , G01S15/89 , G01S15/8913 , G01S15/8929 , G01S15/8993 , G01S15/93 , G05D1/0088 , G05D1/0202 , G05D1/101 , G05D1/102 , Y10S367/909
摘要： A micro unmanned aerial vehicle or drone ("UAV") 10 is remotely controlled through an HMI (309), although this remote control is supplemented by and selectively suppressed by an on-board controller (302). The controller operates to control the generation of a sonar bubble that generally encapsulates the UAV. The sonar bubble, which may be ultrasonic in nature, is produced by a multiplicity of sonar lobes generated by specific sonar emitters associated with each axis of movement for the UAV. The emitters produce individual and beamformed sonar lobes (80-102) that partially overlap to provide stereo or bioptic data in the form of individual echo responses detected by axis- specific sonar detectors (40-68). In this way, the on-board controller is able to interpret and then generate 3-D spatial imaging of the physical environment in which the UAV is currently moving or positioned. The controller is therefore able to plot relative and absolute movement of the UAV through the 3-D space by recording measurements from on-board gyroscopes (342), magnetometers (344) and accelerometers (346). Data from the sonar bubble can therefore both proactively prevent collisions with objects by imposing a corrective instruction to rotors (12-18) and other flight control system and can also assess and compensate for sensor drift.

30. 发明公开

EP2780228A4 TRANSFORMABLE AERIAL VEHICLE 有权转让
标题翻译：可变换式飞行器
公开(公告)号：EP2780228A4
公开(公告)日：2015-06-10
申请号：EP13826711
申请日：2013-12-25
申请人： SZ DJI TECHNOLOGY CO LTD
发明人： ZHAO TAO , DU HAO , WANG MINGXI
IPC分类号： B64C27/02 , B64C1/00 , B64C27/08 , B64C27/32 , B64C39/02
CPC分类号： B64C1/063 , A63H27/12 , B64C1/00 , B64C1/061 , B64C25/32 , B64C27/08 , B64C39/024 , B64C39/028 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/14 , B64C2201/146 , B64C2201/165 , B64D47/00 , B64D47/08 , G05D1/042
摘要： Discloses a transformable aerial vehicle (100) and a control method thereof. The transformable aerial vehicle (100) includes: a central body (10) and at least two transformable frame assemblies (20) respectively disposed on the central body (10), each of the least two transformable frame assemblies (20) having a proximal portion pivotally coupled to the central body (10) and a distal portion; an actuation assembly (13, 5) mounted on the central body (10) and configured to pivot the at least two transformable frame assemblies (20) to a plurality of different vertical angles relative to the central body (10); and a plurality of propulsion units (30) mounted on the at least two transformable frame assemblies (20) and operable to move the transformable aerial vehicle (100).

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