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公开(公告)号:JP2016165215A
公开(公告)日:2016-09-08
申请号:JP2016019465
申请日:2016-02-04
Inventor: ダグラス エー.ムーア
IPC: H02J50/10 , H02J50/80 , H02J50/40 , H02J7/02 , A63H27/133 , A63H30/04 , A63H29/22 , A63H27/04 , B64C39/02 , B64D27/24 , B64F1/16 , H02J7/00
CPC classification number: B64F1/00 , B64C39/024 , H01F38/14 , H02J7/00 , B64C2201/00 , B64C2201/042 , B64C2201/066 , H01R13/6205 , H01R33/92
Abstract: 【課題】無人空中移動体に対する係留及び充電箇所を提供する充電ステーションを提供する 【解決手段】、無人式空中移動体用の充電システムは、光源ソケットに対して結合されるべく構成された光源ソケット用コネクタと、光源ソケット用コネクタに対して電気的に結合された電力回路と、電力回路に対して電気的に結合された一つ以上の電気接触領域を有する充電ステーション胴体と、を有する無人式空中移動体用の充電ステーション含む。 【選択図】図1
Abstract translation: 要解决的问题:提供充电站为无人驾驶飞行器提供对接和充电位置。解决方案:无人驾驶飞行器充电系统包括无人驾驶飞行器充电站,其具有:被配置为耦合到灯插座的灯插座连接器; 电耦合到所述灯插座连接器的电源电路; 以及具有电耦合到电源电路的一个或多个电接触区域的充电站主体
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公开(公告)号:WO2019061442A1
公开(公告)日:2019-04-04
申请号:PCT/CN2017/104883
申请日:2017-09-30
Applicant: 深圳市大疆创新科技有限公司
CPC classification number: B60R25/04 , B60R25/2045 , B60R25/23 , B60R2325/302 , B64C2201/00 , B64D45/00
Abstract: 一种飞行器安全保护方法、设备、飞行器及无人机系统,通过为飞行器设置预设授权指令(S101),在开启飞行器时,需要获取到与预设授权指令匹配的授权指令,才能够启动飞行器(S102)。如果飞行器丢失或者被盗后,在不知道授权人的授权指令的情况下,非授权人则不能使用或者操控飞行器,从而确保飞行器,尤其是无人飞行器在丢失或被盗后也不能使用,提供了对飞行器的安全保护。
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公开(公告)号:WO2017040254A1
公开(公告)日:2017-03-09
申请号:PCT/US2016/048904
申请日:2016-08-26
Applicant: LAUFER WIND GROUP LLC
Inventor: LAUFER, Eric, David , KNAG, John , PETR, Rodney
CPC classification number: G01S7/38 , B64C39/024 , B64C2201/00 , B64C2201/027 , F41G7/224 , F41G7/2253 , F41G7/2293 , F41G7/30 , F41G9/002 , F41H11/02 , G01S13/52 , G01S13/72 , G01S13/867 , G01S13/878 , G05D1/12
Abstract: Described are systems and methods for drone interdiction. A target aircraft is detected based on data from one or more of one or more radars, a fixed camera image from one or more fixed cameras, and an interceptor aircraft image from a camera mounted to an interceptor aircraft. An interception location is generated describing where the interceptor aircraft and the target aircraft are expected to meet. The interceptor aircraft is directed to the interception location to immobilize the target aircraft.
Abstract translation: 描述了无人机停电的系统和方法。 基于来自一个或多个雷达的一个或多个的数据,来自一个或多个固定照相机的固定照相机图像以及来自安装到拦截机的照相机的拦截器飞机图像来检测目标飞机。 产生拦截位置,描述拦截机和目标飞机预计在哪里相遇。 拦截机被引导到拦截位置以固定目标飞机。
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公开(公告)号:WO2015198004A1
公开(公告)日:2015-12-30
申请号:PCT/GB2015/000200
申请日:2015-06-26
Applicant: BAE SYSTEMS PLC
Inventor: THOMAS, Peter Norman
CPC classification number: G05D1/0005 , B64C39/024 , B64C2201/00 , G01C21/20 , G08G5/0069
Abstract: Disclosed is a method and apparatus for determining a route for a vehicle (2). The method comprises generating, by a processor (12), a grid (16) by specifying a start node (18), specifying one or more movement operations performable by the vehicle (2), and iteratively adding edges and further nodes (20 - 24) to the grid (16), each edge corresponding to a respective movement operation and each further node corresponding to a location for the vehicle (2). The one or more processors (12) then select a path through the grid (16) from a first node of the grid to a second node of the grid. The first node corresponds to a first location (A) for the vehicle (2) and the second node corresponds to a second location (B) for the vehicle (2). Thus, a route for the vehicle (2) from the first location (A) to the second location (B) is determined.
Abstract translation: 公开了一种用于确定车辆(2)的路线的方法和装置。 该方法包括通过指定开始节点(18)由处理器(12)生成网格(16),指定由车辆(2)执行的一个或多个移动操作,以及迭代地添加边缘和另外的节点(20- 24)到网格(16),每个边缘对应于相应的移动操作,并且每个另外的节点对应于车辆(2)的位置。 一个或多个处理器(12)然后选择从网格的第一节点到网格的第二节点的网格(16)的路径。 第一节点对应于车辆(2)的第一位置(A),第二节点对应于车辆(2)的第二位置(B)。 因此,确定从第一位置(A)到第二位置(B)的车辆(2)的路线。
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公开(公告)号:WO2015196253A1
公开(公告)日:2015-12-30
申请号:PCT/AU2015/050350
申请日:2015-06-23
Applicant: ORBITAL AUSTRALIA PTY LTD
Inventor: UTLEY, Tyron Dean , BUTERS, Nicolass Harry , NARAYAN, Jayesh
CPC classification number: F02D41/009 , B64C39/024 , B64C2201/00 , B64C2201/044 , F02D41/222 , F02D2200/101 , F02D2400/08 , H02K11/21 , Y02T10/40
Abstract: Redundancy in engine timing position sensing maintains a UAV operational in the event of failure of a primary engine timing position sub-system. The redundancy avoids duplication of the primary crankshaft timing position sensing components, and avoids adding weight, cost and component complexity. Conditioned (square) waveform(s) (102) is/are created from respective sinusoidal waveform(s). Each consecutive leading edge (103a) and trailing edge (103b) of the pulses of the square waveform (102) is derived from the crossing of the zero voltage value by consecutive sinusoidal waveforms A,B,C (e.g. Voltage (V) vs Time (t) or angular degrees). The square pulse waveform (102) is output (104) to a microcontroller (106) to create and output a pseudo crankshaft timing position signal (108) to be used by an ECU to determine ignition and fuel injection events in the event that the primary timing signal from the crankshaft position sensor (CPS) has failed. The signal (108) output to the ECU can have a missing pulse (116) (i.e. indicative of a TDC position of the engine crankshaft) as well as multiple square pulses (114) corresponding to the pulses of the initial square pulse waveform (102). The waveform signal (108) is therefore derived from the alternator waveform signal(s) and provides a pseudo crankshaft timing position signal in the event of failure of the primary or initial CPS signal.
Abstract translation: 发动机定时位置检测的冗余在主发动机定时位置子系统发生故障的情况下维持UAV的运行。 冗余避免了主曲轴定时位置检测部件的重复,并避免了增加重量,成本和部件复杂度。 从相应的正弦波形产生条件(平方)波形(102)。 方波(102)的脉冲的每个连续的前缘(103a)和后沿(103b)是从零电压值与连续的正弦波形A,B,C的交叉导出的(例如,电压(V)vs时间 (t)或角度)。 方波脉冲波形(102)被输出(104)到微控制器(106),以产生并输出伪曲轴定时位置信号(108),以由ECU使用以确定点火和燃料喷射事件, 来自曲轴位置传感器(CPS)的定时信号失败。 输出到ECU的信号(108)可以具有缺失脉冲(116)(即,表示发动机曲轴的TDC位置)以及对应于初始方波脉冲波形(102)的脉冲的多个平方脉冲(114) )。 因此,波形信号(108)从交流发电机波形信号导出,并且在初级或初始CPS信号故障的情况下提供伪曲轴定时位置信号。
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公开(公告)号:WO2009108885A2
公开(公告)日:2009-09-03
申请号:PCT/US2009/035525
申请日:2009-02-27
Applicant: CESSNA AIRCRAFT COMPANY , BALL, Danny , PFEIFFER, Kevin
Inventor: BALL, Danny , PFEIFFER, Kevin
CPC classification number: B64C11/26 , B32B9/00 , B32B27/00 , B32B27/38 , B32B37/00 , B32B37/02 , B32B37/18 , B64C11/00 , B64C11/02 , B64C11/04 , B64C11/20 , B64C2201/00 , Y10T29/49332 , Y10T156/1057 , Y10T156/1089
Abstract: A method for making a propeller product is disclosed. The propeller is formed using polyurethane cores adhered to a laminate hub to form a core assembly. An encapsulating structural laminate skin is then formed on the core assembly using a resin-transfer-molding process to create a single-piece composite propeller.
Abstract translation: 公开了制造螺旋桨产品的方法。 螺旋桨使用粘附到叠层轮毂上的聚氨酯芯形成芯组件。 然后使用树脂传递模塑工艺在芯组件上形成封装的结构层压板表层以产生单件复合螺旋桨。
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公开(公告)号:US09985825B2
公开(公告)日:2018-05-29
申请号:US15060619
申请日:2016-03-04
Applicant: International Mobile IOT Corp
Inventor: Jung-Tang Huang
CPC classification number: H04L41/0668 , B64C2201/00 , H04L43/0817 , H04L43/16 , H04L67/1021 , H04L67/12 , H04W4/02 , H04W4/70 , H04W4/80 , H04W84/12
Abstract: An IoT device management system and method that automatically monitors and dynamically reacts to events and reconstructs application systems is provided. The IoT device management system can be a location-based network system includes a plurality of communication nodes.
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公开(公告)号:US20180054004A1
公开(公告)日:2018-02-22
申请号:US15240980
申请日:2016-08-18
Applicant: Echodyne Corp
Inventor: Tom Driscoll , John Desmond Hunt , Nathan Ingle Landy , Milton Perque , Charles A. Renneberg , Ioannis Tzanidis , Robert Tilman Worl , Felix D. Yuen
IPC: H01Q21/00 , H01Q3/26 , G01S13/93 , G05D1/00 , G05D1/02 , B60W10/04 , B60W10/20 , B60W30/09 , B64C1/36 , B64C39/02
CPC classification number: H01Q21/0037 , B60W10/04 , B60W10/20 , B60W30/09 , B60W2420/52 , B60W2550/10 , B60W2710/18 , B60W2710/20 , B64C1/36 , B64C39/024 , B64C2201/00 , G01S13/9303 , G01S13/931 , G01S2013/9342 , G01S2013/9346 , G05D1/0088 , G05D1/0257 , H01Q1/3233 , H01Q3/2641 , H01Q3/443 , H01Q13/28 , H01Q15/0066 , H01Q21/0012 , H01Q21/005
Abstract: An embodiment of an antenna includes first and second transmission lines, first antenna elements, and second antenna elements. The first transmission line is configured to guide a first signal such that the first signal has a characteristic of a first value, and the second transmission line is configured to guide a second signal such that the second signal has the same characteristic but of a second value that is different than the first value. The first antenna elements are each disposed adjacent to the first transmission line and are each configured to radiate the first signal in response to a respective first control signal, and the second antenna elements are each disposed adjacent to the second transmission line and are each configured to radiate the second signal in response to a respective second control signal. Such an antenna can have better main-beam and side-lobe characteristics, and a better SIR, than prior antennas.
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公开(公告)号:US20180039272A1
公开(公告)日:2018-02-08
申请号:US15672264
申请日:2017-08-08
Applicant: PARROT DRONES
Inventor: Henri SEYDOUX , Frédéric PIRAT , Arnaud VAN DEN BOSSCHE
CPC classification number: G05D1/0088 , A63H30/04 , B64C39/024 , B64C39/10 , B64C2201/00 , B64C2201/028 , B64C2201/104 , B64C2201/141 , B64C2201/146 , B64C2203/00 , B64D47/08 , G05D1/0038 , G05D1/101
Abstract: A module for a drone that integrates an electronic circuit and one or more sensors for the attitude, altitude, speed, orientation and/or position of the drone in the same one-piece housing. The module also integrates an electronic power circuit that receives set command values prepared by the processor of the electronic circuit on the basis of the data provided by the integrated sensors and provides, as an output, corresponding signals for directly supplying current or voltage to the propulsion means of the drone and to the control surfaces.
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公开(公告)号:US20180004064A1
公开(公告)日:2018-01-04
申请号:US15472328
申请日:2017-03-29
Applicant: Yehong Production
Inventor: Do Hun KIM
CPC classification number: G03B17/561 , B64C2201/00 , B64D47/08 , F16F15/08 , F16M11/10 , F16M11/18 , F16M11/2071 , F16M13/02 , F16M2200/04 , G03B15/006 , G03B37/04
Abstract: A stabilizer for camera shooting, which enables correction of a position of a camera module, includes a frame having an inner space, a plurality of camera modules mounted on the frame, each of the plurality of camera modules including a lens for shooting an outside of the frame, a first brushless motor arranged in the inner space and rotating the frame around a first rotation axis, and a second brushless motor arranged in the inner space and rotating the frame around a second rotation axis crossing the first rotation axis on a same plane, in which the frame is rotatably coupled to the first brushless motor via a first shaft, the frame capable of rotating with respect to the first brushless motor, and a height of each lens in a Z-axis direction is within a range of a shortest dimension in a transverse direction between the frame and a center of the inner space of the frame with respect to the first shaft.
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