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101.发明申请公开(公告)号：US20160167799A1
公开(公告)日：2016-06-16
申请号：US14966180
申请日：2015-12-11
Applicant: AIRBUS GROUP SAS
Inventor： HICHEM SMAOUI , BRUNO RECHAIN , FABIEN RETHO
CPC classification number: F02B65/00 , B60K6/24 , B60K6/387 , B60K6/40 , B60K6/442 , B64C39/024 , B64C2201/024 , B64C2201/042 , B64C2201/048 , B64D2027/026 , F01D15/10 , F02B33/40 , F02B37/00 , F02C6/12 , F02C6/14 , F02C6/206 , F05D2220/329 , F05D2220/40 , F05D2220/62 , F05D2220/76 , F05D2220/90 , F05D2260/42 , Y02T10/144 , Y02T10/6234 , Y02T10/6295 , Y02T50/64 , Y02T50/671
Abstract: A method of managing a power demand to assure the operation of a pilotless aircraft. The aircraft includes an internal combustion engine supplying a maximum principal power which can vary. The management method is particularly suitable for a rotary wing pilotless aircraft. It guarantees the storage of an amount of electrical energy at least equal to a recovery energy of the aircraft in the event of failure of the internal combustion engine. This recovery energy enables the control of autorotation and landing of the aircraft.
Abstract translation: 一种管理电力需求以确保无人驾驶飞行器的操作的方法。 飞机包括提供可变化的最大主力的内燃机。 管理方法特别适用于旋翼飞行无人机。 在内燃机故障的情况下，它保证至少等于飞机的回收能量的一定量的电能的存储。 这种恢复能量可以控制飞机的自动和着陆。
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公开(公告)号：US20160159473A1
公开(公告)日：2016-06-09
申请号：US15012006
申请日：2016-02-01
Applicant: SZ DJI TECHNOLOGY Co., LTD
Inventor： Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
CPC classification number: B64C27/08 , A63H27/12 , B64C1/30 , B64C25/06 , B64C25/32 , B64C27/00 , B64C27/54 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/14 , B64C2201/141 , B64C2201/20 , B64D31/14 , B64D43/00 , G01R33/0047 , G01V3/16 , G05D1/00 , Y10T29/49117
Abstract: The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.
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公开(公告)号：US09353033B2
公开(公告)日：2016-05-31
申请号：US14485412
申请日：2014-09-12
Applicant: Google Inc.
Inventor： Damon Vander Lind , Thomas Van Alsenoy , Richard Wayne DeVaul
CPC classification number: F03D9/32 , B63H9/0685 , B63H2009/0692 , B64C27/00 , B64C31/06 , B64C39/022 , B64C2201/021 , B64C2201/024 , B64C2201/028 , B64C2201/145 , B64C2201/205 , B64C2201/206 , B64C2201/208 , B64D3/00 , B64D47/00 , B64F3/02 , C07C29/141 , F03D5/00 , F03D9/008 , F03D9/11 , F03D9/25 , F03D80/80 , F05B2240/917 , F05B2240/921 , H02K7/1838 , Y02E10/70 , Y02E10/725 , Y02E10/728
Abstract: A vehicle-based airborne wind turbine system having an aerial wing, a plurality of rotors each having a plurality of rotatable blades positioned on the aerial wing, an electrically conductive tether secured to the aerial wing and secured to a ground station positioned on a vehicle, wherein the aerial wing is adapted to receive electrical power from the vehicle that is delivered to the aerial wing through the electrically conductive tether; wherein the aerial wing is adapted to operate in a flying mode to harness wind energy to provide a first pulling force through the tether to pull the vehicle; and wherein the aerial wing is also adapted to operate in a powered flying mode wherein the rotors may be powered so that the turbine blades serve as thrust-generating propellers to provide a second pulling force through the tether to pull the vehicle.
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104.发明申请METHOD FOR CONSTRUCTING AIR-OBSERVED TERRAIN DATA BY USING ROTARY WING STRUCTURE 有权使用旋转结构构造空气观测地层数据的方法公开(公告)号：US20160132057A1
公开(公告)日：2016-05-12
申请号：US14646329
申请日：2014-05-09
Applicant: DURETEK INC.
Inventor： Hyungse KIM , Jaemin SONG , Junkyu KIM , Jihwan AN
CPC classification number: G05D1/0094 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/123 , B64D47/08 , G01C11/02 , G05D1/0011 , G05D1/102
Abstract: A method for constructing air-observed terrain data by using a rotary wing structure includes setting flight information including a photographing starting location and a photographing ending location on the basis of a flight route and a photographing location of the rotary wing structure; transmitting, to the rotary wing structure, the flight information so as to store the flight information in a flight control unit; capturing a ground image by a photographing unit of the rotary wing structure and storing the ground image in a storage unit when the rotary wing structure arrives at the photographing location; ending photographing and returning to the ground when the rotary wing structure arrives at the photographing ending location while repeatedly capturing a ground image; and constructing, by a computer in the control center, terrain data by using ground images stored in the storage unit.
Abstract translation: 通过使用旋转翼结构来构造空气观测地形数据的方法包括：基于旋转翼结构的飞行路线和拍摄位置来设置包括拍摄开始位置和拍摄结束位置的飞行信息; 向所述旋转翼结构传送所述飞行信息，以将所述飞行信息存储在飞行控制单元中; 通过所述旋转翼结构的拍摄单元捕获地面图像，并且当所述旋转翼结构到达所述拍摄位置时，将所述地面图像存储在存储单元中; 当旋转翼结构到达拍摄结束位置同时重复地拍摄地面图像时，结束拍摄并返回到地面; 以及通过使用存储在存储单元中的地面图像来构建控制中心中的计算机的地形数据。
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公开(公告)号：US20160122016A1
公开(公告)日：2016-05-05
申请号：US14528024
申请日：2014-10-30
Inventor： Stefano Mintchev , Ludovic Daler , Dario Floreano
IPC: B64C39/02
CPC classification number: B64C39/024 , A63H27/12 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/102 , B64C2201/108 , B64C2201/127
Abstract: An aerial vehicle including self-autonomous deployable arms and methods of deploying the vehicle are disclosed. The arms may include patterns located thereon that allow the arms to transition between wrapped, flat, and deployed configurations autonomously without the need for direct intervention by a user.
Abstract translation: 公开了一种包括自主部署臂的飞行器和部署车辆的方法。 臂可以包括位于其上的图案，其允许臂在包裹的，平坦的和部署的配置之间自主地转换，而不需要用户的直接干预。
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Patent Agency Ranking
公开(公告)号：US20160122015A1
公开(公告)日：2016-05-05
申请号：US14526790
申请日：2014-10-29
Applicant: QUALCOMM Incorporated
Inventor： Donald Bolden Hutson
CPC classification number: B64C39/024 , B60F5/02 , B64C2201/024 , B64C2201/108 , B64C2201/126 , B64C2201/162 , F41H11/12 , F41H11/28
Abstract: Unmanned aerial vehicles and methods for providing the same are disclosed. The unmanned aerial vehicles may have various configurations related to a support frame. The unmanned aerial vehicles may have various configurations with a continuous track for ground propulsion. The unmanned aerial vehicles may have various configurations related to payload clamps.
Abstract translation: 公开了无人驾驶飞行器及其提供方法。 无人驾驶飞行器可以具有与支撑框架相关的各种构造。 无人驾驶飞行器可以具有各种构造，具有用于地面推进的连续轨道。 无人驾驶飞行器可以具有与有效载荷夹具相关的各种构造。
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公开(公告)号：US09321530B2
公开(公告)日：2016-04-26
申请号：US14947923
申请日：2015-11-20
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor： Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
CPC classification number: B64C27/08 , A63H27/12 , B64C1/30 , B64C25/06 , B64C25/32 , B64C27/00 , B64C27/54 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/14 , B64C2201/141 , B64C2201/20 , B64D31/14 , B64D43/00 , G01R33/0047 , G01V3/16 , G05D1/00 , Y10T29/49117
Abstract: The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.
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公开(公告)号：US20160039541A1
公开(公告)日：2016-02-11
申请号：US14452819
申请日：2014-08-06
Applicant: DISNEY ENTERPRISES, INC.
Inventor： PAUL A. BEARDSLEY , MICHAEL ERIKSSON , JAVIER ALONSO-MORA , JOERN REHDER
CPC classification number: B64F1/362 , B60L11/1816 , B60L11/1818 , B60L11/1824 , B60L11/1833 , B60L11/1835 , B60L11/1846 , B60L2200/10 , B60L2230/10 , B64C39/024 , B64C2201/024 , B64C2201/042 , B64C2201/066 , B64C2201/141 , B64C2201/146 , B64C2201/182 , G05D1/0011 , G05D1/0088 , G05D1/042 , Y02T10/7005 , Y02T10/7088 , Y02T90/121 , Y02T90/125 , Y02T90/14
Abstract: A method of docking and recharging using a base station and a station-mating frame on the multicopter. The base station includes an upward-facing camera that is used by a docking controller to detect the presence, position, and orientation of a frame, with infrared light-emitting diodes arranged in a predefined pattern. The controller of the base station acts to emit wireless signals to the multicopter to guide the multicopter with its station-mating frame to a predefined position above the base station. The controller transmits a wireless signal to the multicopter to reduce thrust, and the multicopter lowers itself onto a sloped receiving surface that may be arranged in a crown pattern to provide passive gravity-driven centering, which causes the station-mating frame to slide to a lowest vertical point of the receiving assembly. A locking mechanism engages to lock the frame in place and provide electrical contact for recharging.
Abstract translation: 一种使用多台飞机上的基站和站对接框架进行对接和再充电的方法。 基站包括向上的摄像机，其由对接控制器用于利用以预定模式布置的红外发光二极管来检测框架的存在，位置和取向。 基站的控制器用于向多机器发射无线信号，以引导具有其站配对帧的多机器到基站上方的预定位置。 控制器将无线信号发射到多重飞行器以减小推力，并且多机器将自身降低到倾斜的接收表面上，该倾斜的接收表面可以布置成冠状图案以提供被动重力驱动的定心，这使得站配合框架滑动到 接收组件的最低垂直点。 锁定机构接合以将框架锁定在适当位置并提供用于再充电的电气接触。
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109.发明申请METHOD FOR CONTROLLING A PATH OF A ROTARY-WING DRONE, A CORRESPONDING SYSTEM, A ROTARY-WING DRONE IMPLEMENTING THIS SYSTEM AND THE RELATED USES OF SUCH A DRONE 审中-公开用于控制旋转刮刀的路径的方法，相应的系统，实施该系统的旋转式刮刀以及这种刮刀的相关用途公开(公告)号：US20150370258A1
公开(公告)日：2015-12-24
申请号：US14746311
申请日：2015-06-22
Applicant: THOMSON LICENSING
Inventor： Julien FLEUREAU , Francois-Louis TARIOLLE , Paul KERBIRIOU , Francois Le CLERC
CPC classification number: G05D1/101 , B64C39/024 , B64C2201/024 , B64C2201/141 , G05D1/0088 , G05D1/102
Abstract: A method for controlling a path of a rotary-wing drone wherein said method comprises: Establishing a first-order temporal relation between flight control parameters and flight dynamics for said rotary-wing drone comprising: An Explicit Discrete Time-Variant State-Space Representation of a translation control of said rotary-wing drone; An Explicit Discrete Time-Variant State-Space Representation of a course control of said rotary-wing drone; Controlling the path of said rotary-wing drone by: Estimating a course of said rotary-wing drone on the basis of said Explicit Discrete Time-Variant State-Space Representation of a course control of said rotary-wing drone; Estimating a position of said rotary-wing drone on the basis of said Explicit Discrete Time-Variant State-Space Representation of a translation control of said rotary-wing drone; said steps of estimating being performed independently.
Abstract translation: 一种用于控制旋转翼无人机的路径的方法，其中所述方法包括：为所述旋转翼无人机建立飞行控制参数和飞行动态之间的一阶时间关系，包括：显式离散时变状态空间表示 所述旋转翼无人机的平移控制; 显式离散时变状态空间表示所述旋转翼无人机的航向控制; 通过以下步骤控制所述旋转翼式无人机的路径：基于所述旋转翼无人机的航向控制的所述显式离散时变状态空间表示来估计所述旋翼飞机的航向; 基于所述旋转翼无人机的平移控制的所述显式离散时变状态空间表示来估计所述旋转翼式无人机的位置; 所述步骤是独立执行的估计。
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110.发明申请MAGIC WAND INTERFACE AND OTHER USER INTERACTION PARADIGMS FOR A FLYING DIGITAL ASSISTANT 有权用于飞行数字助理的魔术界面和其他用户交互参数公开(公告)号：US20150370250A1
公开(公告)日：2015-12-24
申请号：US14688998
申请日：2015-04-16
Applicant: Skydio, Inc.
Inventor： Abraham Bachrach , Adam Bry , Matthew Donahoe
CPC classification number: G05D1/0016 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64D47/08 , G01C21/165 , G01C23/00 , G05D1/0027 , G05D1/0044 , G05D1/0094
Abstract: Methods and systems are described for new paradigms for user interaction with an unmanned aerial vehicle (referred to as a flying digital assistant or FDA) using a portable multifunction device (PMD) such as smart phone. In some embodiments, a magic wand user interaction paradigm is described for intuitive control of an FDA using a PMD. In other embodiments, methods for scripting a shot are described.
Abstract translation: 描述了使用诸如智能电话的便携式多功能装置（PMD）与无人驾驶飞行器（称为飞行数字助理或FDA）进行用户交互的新范例的方法和系统。 在一些实施例中，描述了魔术棒用户交互范例，用于使用PMD直观地控制FDA。 在其他实施例中，描述了用于脚本化镜头的方法。
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