公开(公告)号：WO2017152067A1

公开(公告)日：2017-09-08

申请号：PCT/US2017/020683

申请日：2017-03-03

Applicant: ANIMUSOFT LLC

Inventor： RODRIGUEZ, Daniel

IPC: G05D1/00

CPC classification number: G05D1/0088 ,  B63B2035/006 ,  B63G2008/002 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/108 ,  B64C2201/14 ,  G05D1/0027 ,  G05D1/0274

Abstract: A system may be configured to manage at least one robotic device. The system may comprise one or more databases and one or more processors in communication with the one or more databases. The one or more processors may be configured to provide an operating system for the at least one robotic device, control motion of the at least one robotic device, configure at least one sensor removably coupled to the at least one robotic device, process data collected by the at least one sensor, and/or perform localization and/or area mapping for the at least one robotic device by comparing data collected by the at least one sensor with data in the one or more databases to generate localization and/or area mapping data.

Abstract translation: 系统可以被配置为管理至少一个机器人设备。 该系统可以包括一个或多个数据库以及与该一个或多个数据库通信的一个或多个处理器。 所述一个或多个处理器可以被配置为为所述至少一个机器人设备提供操作系统，控制所述至少一个机器人设备的运动，配置可移除地耦合到所述至少一个机器人设备的至少一个传感器，处理由 和/或通过比较由至少一个传感器收集的数据与一个或多个数据库中的数据来执行至少一个机器人设备的定位和/或区域映射以生成定位和/或区域映射数据

公开(公告)号：WO2017120110A1

公开(公告)日：2017-07-13

申请号：PCT/US2016/069423

申请日：2016-12-30

Applicant: RUSSELL, David, Wayne

Inventor： RUSSELL, David, Wayne

IPC: B64C39/02 ,  H04W16/26 ,  F41G7/28

CPC classification number: H04W16/26 ,  B64C2201/14 ,  F41G9/00 ,  H04B7/18506 ,  H04B7/2606

Abstract: Unmanned Aerial Vehicles also known as UAVs or Drones, either autonomous or remotely piloted, may be fitted with an Identify Friend or Foe (IFF) transponder for tracking and identification. Remotely piloted drones require a high bandwidth RF transceiver for video and/or control inputs, but the IFF system does not. Fully autonomous vehicles might utilize only the low bandwidth IFF transponder. This invention utilizes the existing cellular network and physical infrastructure to provide UAV command and control functionality over most of the national area.

Abstract translation: 无人机也称为无人机或无人机，无论是自动还是遥控驾驶，都可以安装识别敌友（IFF）转发器进行跟踪和识别。 遥控驾驶无人机需要高带宽的RF收发器用于视频和/或控制输入，但IFF系统不需要。 完全自动驾驶车辆可能只使用低带宽IFF应答器。 本发明利用现有的蜂窝网络和物理基础设施在全国大部分地区提供无人机指挥和控制功能。

公开(公告)号：WO2017106697A1

公开(公告)日：2017-06-22

申请号：PCT/US2016/067252

申请日：2016-12-16

Applicant: GLOBAL TEL*LINK CORP.

Inventor： VOLKART, Mitch

IPC: B64C39/02

CPC classification number: G06K9/00288 ,  B64C39/024 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/14 ,  G05D1/0094 ,  G06K9/00335 ,  G06K9/0063 ,  G06K9/00771 ,  G06K9/209 ,  G06K9/32 ,  G06K2009/3291 ,  G10L17/00 ,  G10L17/005

Abstract: Disclosed herein are system, method, and computer program product embodiments for locating, identifying, and tracking a known criminal, fugitive, missing person, and/or any other person of interest. An embodiment operates by deploying an unmanned aerial vehicle, determining the mode of operation of the UAV, operating the UAV in accordance with the mode of operation of the UAV, determining whether a subject has been detected, capturing a first voice sample associated with the subject, authenticating the identity of the subject, and transmitting the GPS location of the unmanned aerial vehicle to a computing device.

Abstract translation: 这里公开了用于定位，识别和跟踪已知犯罪，逃犯，失踪者和/或任何其他感兴趣的人的系统，方法和计算机程序产品实施例。 一个实施例通过部署无人飞行器，确定UAV的操作模式，根据UAV的操作模式操作UAV，确定是否已经检测到对象，捕获与对象相关联的第一语音样本 ，验证主体的身份，并将无人驾驶飞行器的GPS位置发送给计算设备。

公开(公告)号：WO2017105266A1

公开(公告)日：2017-06-22

申请号：PCT/RO2016/000026

申请日：2016-12-16

Applicant: RĂZVAN, Sabie ,  IOSIF, Tăposu

Inventor： RĂZVAN, Sabie

IPC: B64C39/00

CPC classification number: B64C39/001 ,  B64C2201/027 ,  B64C2201/14 ,  B64C2201/162 ,  B64C2201/167 ,  B64C2201/185

Abstract: The invention relates to an aircraft with vertical takeoff and landing and its operation method. Aircraft with vertical takeoff and landing of aerodyne type according to the invention comprises a circular symmetrical aerodynamic body (1) having an internal stiffening platform (2) located on the chord of the aerodynamic profile and which supports the components of the aircraft, at least four vertical ducted propellers (3a), (3b), (3c), (3d) arranged symmetrically to the central vertical axis of the carrier body (1), but also to the predetemined flight axis and to the transverse axis of the carrier body (1), propellers (3a) and (3c) having the same rotational direction opposite to that of propellers (3b) and (3d) at least two horizontal ducted propellers (4) with opposite rotation directions located inside the carrier body or outside of it, placed parallel symmetrical with the predetermined flight axis and on both sides of it, vector nozzles (5), one for each horizontal propeller (4), which provides vector orientation to jets of the horizontal ducted propellers (4), the means of power supply (6), which are designed to provide electricity necessary to operate all engines and all electrical and electronic devices on board, an electronic control and management flight module (7) and a landing gear (9), which aims to promote contact between the aircraft and the ground.

Abstract translation: 本发明涉及一种具有垂直起降的飞机及其操作方法。 具有根据本发明的飞梭式垂直起飞和降落的飞机包括具有位于空气动力学型材的翼弦上并且支撑飞机的部件的内部加强平台（2）的圆形对称空气动力学体（1），至少四个 垂直管道式螺旋桨3a，3b，3c，3d与载体主体1的中心垂直轴线对称布置，但也与预定的飞行轴线和载体主体的横轴线 具有与螺旋桨（3b）相反的旋转方向的螺旋桨（3a）和（3c）以及（3d）具有相反旋转方向的至少两个水平管道螺旋桨（4） ，其与预定的飞行轴线平行对称地布置在其两侧，矢量喷嘴（5），每个水平螺旋桨（4）一个，其为水平管道螺旋桨（4）的射流提供矢量取向，pow （6），其设计用于提供操作所有发动机和船上所有电气和电子设备所需的电力，电子控制和管理飞行模块（7）以及起落架（9），其旨在促进 飞机和地面。

公开(公告)号：WO2017098412A1

公开(公告)日：2017-06-15

申请号：PCT/IB2016/057399

申请日：2016-12-07

Applicant: IDEAFORGE TECHNOLOGY PVT. LTD.

Inventor： BHAT, Ashish

IPC: B64C27/00 ,  B64C17/00 ,  G05D1/08

CPC classification number: B64C17/00 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/14

Abstract: The present disclosure provides a multi-rotor Aerial Vehicle comprising at least five arms. Pairs of coaxial contra rotating rotors/propellers are configured on each arm defining a polygon. In the event of failure of any one of the rotors/propellers, a control system incorporating an autopilot, shuts off corresponding contra rotating rotor/propeller of the pair to maintain yaw stability thereby rendering the corresponding arm non-functional; and adjusts throttles of the coaxial contra rotating rotors/propellers of remaining functional arms to maintain tilt and lift stability of the Aerial Vehicle.

Abstract translation: 本公开提供了一种包括至少五个臂的多旋翼飞行器。 成对的同轴对旋转子/螺旋桨配置在每个限定多边形的臂上。 在任何一个转子/推进器发生故障的情况下，包含自动驾驶仪的控制系统关闭该对转子/螺旋桨的相应的对转动以保持偏航稳定性，从而使相应的臂不起作用; 并调整其余功能臂的同轴对旋转转子/螺旋桨的节流阀，以保持飞行器的倾斜和升力稳定性。

公开(公告)号：WO2017095610A1

公开(公告)日：2017-06-08

申请号：PCT/US2016/061783

申请日：2016-11-14

Applicant: CLOUD CAP TECHNOLOGY, INC.

Inventor： ALLEN, Michael, J.

IPC: G05D1/08 ,  B64C27/08 ,  B64C39/02 ,  B64D31/02 ,  G05D1/00

CPC classification number: B64C27/57 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/14 ,  B64D31/02 ,  G05D1/0072 ,  G05D1/0858

Abstract: A method for controlling each rotor on a multirotor aircraft includes receiving one or more sensed states of the multirotor aircraft, and determining a control scheme dynamically using the sensed one or more states of the multirotor aircraft. Receiving one or more sensed states can include receiving one or more of a rotational rate or acceleration of the aircraft, or any other suitable aircraft state.

Abstract translation: 用于控制多旋翼飞行器上的每个转子的方法包括接收多旋翼飞行器的一个或多个感测状态，以及使用感测的多旋翼飞行器的一个或多个状态动态地确定控制方案。 接收一个或多个感测状态可以包括接收飞行器的旋转速率或加速度或任何其他合适的飞行器状态中的一个或多个。

公开(公告)号：WO2017041070A1

公开(公告)日：2017-03-09

申请号：PCT/US2016/050315

申请日：2016-09-04

Applicant: VAN CRUYNINGEN, Lzak

Inventor： VAN CRUYNINGEN, Lzak

IPC: G05D1/02

CPC classification number: G05D1/101 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/14 ,  B64D45/00

Abstract: Figure 1 shows airframe (10) with powertrain (11) supporting electromagnetic field strength sensor (12), reference electromagnetic field strength (14), comparator (16), and shutdown (18) flying along a transmission line with towers (40, 42, and 44), phase conductors (46, 48), and 50, and shield wires (52 and 54). Reference electromagnetic field strength (14) is adjusted before the flight to set the minimum electromagnetic field strength before shutdown (18) reduces the power to powertrain (11). The reference electromagnetic field strength (14) corresponding to a characteristic radial dimension (58), and thus virtual tunnel (22), outside of which airframe (10) cannot fly without automatic shutdown (18), regardless of the state of the autopilot, GPS signal, or radio link.

Abstract translation: 图1示出了具有支撑电磁场强度传感器（12）的动力总成（11），参考电磁场强度（14），比较器（16）和关闭（18）的机身（10），其沿着传输线与塔（40,42 和44），相导体（46,48）和50以及屏蔽线（52和54）。 参考电磁场强度（14）在飞行前进行调整，以在关闭前设置最小电磁场强度（18）降低功率到动力总成（11）。 与自动驾驶仪的状态无关地，对应于特征径向尺寸（58）的参考电磁场强度（14）以及虚拟隧道（22），其中机身（10）外不能自动停机（18） GPS信号或无线电链路。

公开(公告)号：WO2017025884A1

公开(公告)日：2017-02-16

申请号：PCT/IB2016/054760

申请日：2016-08-05

Applicant: HERE GLOBAL B.V. ,  HERE NORTH AMERICA, LLC

Inventor： BERNHARDT, Bruce ,  SHEYNMAN, Arnold ,  XU, Jingwei

IPC: G01C21/00 ,  B64C39/02 ,  G05D1/10 ,  G08G5/00

CPC classification number: G08G5/0069 ,  B64C39/024 ,  B64C2201/14 ,  B64C2201/141 ,  G01C21/005 ,  G05D1/101 ,  G08G5/0021 ,  G08G5/0034 ,  G08G5/0039 ,  G08G5/006 ,  G08G5/0086

Abstract: A method including retrieving a multi-dimensional map (30) from a navigation system memory (27); determining an aerial route (64) between two locations (60, 62) based at least partially upon the multi-dimensional map (30); and storing the aerial route (64) in the navigation system memory (27). The multi-dimensional map (30) includes terrain information (32) and object information (34). The object information (34) includes information regarding location (42) and size (44) of objects (68, 70, 72) extending above ground level. The objects (68, 70, 72) are in uncontrolled airspace, and the object information (34) includes height information (46) regarding a height above ground level of at least some of the objects (68, 70, 72). The aerial route (64) is limited to the uncontrolled airspace, where the aerial route is over and around at least some of the objects (68, 70, 72), and where the aerial route (64) is determined, at least partially, based upon the height information (46) of the objects (68, 70, 72).

Abstract translation: 一种包括从导航系统存储器（27）检索多维地图（30）的方法; 至少部分地基于多维图（30）确定两个位置（60,62）之间的空中路线（64）; 以及将所述空中路线（64）存储在所述导航系统存储器（27）中。 多维图（30）包括地形信息（32）和对象信息（34）。 对象信息（34）包括关于在地平面上方延伸的对象（68,70,72）的位置（42）和大小（44）的信息。 物体（68,70,72）处于不受控制的空域中，并且物体信息（34）包括关于物体（68,70,72）中的至少一些物体的地面高度以上的高度信息（46）。 空中航线（64）限于不受控制的空域，其中空中航线结束，并且至少一些物体（68,70,72）以及至少部分确定空中航线（64）的地方， 基于对象（68,70,72）的高度信息（46）。

公开(公告)号：WO2016167946A1

公开(公告)日：2016-10-20

申请号：PCT/US2016/024521

申请日：2016-03-28

Applicant: NORTHROP GRUMMAN SYSTEMS CORPORATION

Inventor： CLARK, Ryan T.

IPC: G05D1/00 ,  G06F3/01

CPC classification number: G06F3/017 ,  A63H27/12 ,  B64C39/024 ,  B64C2201/14 ,  B64C2201/146 ,  G05D1/0016 ,  G05D1/0022 ,  G06F3/014 ,  G06F3/0346 ,  H04W4/80

Abstract: An apparatus includes a wearable device having a multi-sensor detector to sense operator gestures directed at an unmanned vehicle (UV). The multi-sensor detector includes at least two sensors to detect motion and direction of the operator gestures with respect to operator hand movement, operator hand movement with respect to the earth, rotational movement of the operator hand, and finger movement on the operator hand. A controller monitors the multi-sensor detector to determine the operator gesture based on input data received from the sensors. The controller generates a command to the UV based on the determined operator gesture.

Abstract translation: 一种装置包括具有多传感器检测器的可佩戴装置，用于感测针对无人驾驶车辆（UV）的操作者手势。 多传感器检测器包括至少两个传感器，用于相对于操作者手的移动来检测操作者手势的运动和方向，操作者手相对于地球的移动，操作者的手的旋转运动和手指在操作者手上的移动。 控制器监视多传感器检测器，以基于从传感器接收的输入数据来确定操作者手势。 控制器基于确定的操作员手势生成对UV的命令。

公开(公告)号：WO2016154551A1

公开(公告)日：2016-09-29

申请号：PCT/US2016/024251

申请日：2016-03-25

Applicant: MATTERNET, INC. ,  HINKLE, Christopher ,  RAPTOPOULOS, Andreas ,  LARSEN, Kendall ,  BARUCHIN, Ido

Inventor： HINKLE, Christopher ,  RAPTOPOULOS, Andreas ,  LARSEN, Kendall ,  BARUCHIN, Ido

IPC: B64C37/00 ,  B64C37/02 ,  B64C39/02 ,  G05D1/00 ,  G05D1/08 ,  G05D1/12 ,  H04W4/02

CPC classification number: G08G5/0034 ,  B64C39/024 ,  B64C2201/00 ,  B64C2201/027 ,  B64C2201/14 ,  G01C21/20 ,  G08G5/0013 ,  G08G5/0026 ,  G08G5/0039 ,  G08G5/006 ,  G08G5/0069

Abstract: 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 geospatial information, and causing the route to be communicated to the UAV.

Abstract translation: 提供了用于动态地确定无人机（UAV）的路线的系统和过程。 在一个示例中，在包括一个或多个处理器和存储器的计算机系统中，该过程包括接收路由请求，路由请求包括UAV的原始位置和目的地位置，接收与原始位置和目的地位置相关联的地理空间信息 所述地理空间信息包括物理障碍物和禁止飞行区域中的至少一个，至少部分地基于所述地理空间信息来确定所述UAV从所述起始位置到所述目的地位置的路线，并且使所述路线被传送到 无人机。