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    ACCIDENT IDENTIFICATION AND COMMUNICATION IN VEHICLES
    302.
    发明申请
    ACCIDENT IDENTIFICATION AND COMMUNICATION IN VEHICLES 审中-公开
    车辆中的事故识别和通信

    公开(公告)号：WO2017142520A1

    公开(公告)日：2017-08-24

    申请号：PCT/US2016/018201

    申请日：2016-02-17

    Applicant: FORD GLOBAL TECHNOLOGIES, LLC

    Inventor： NEUBECKER, Cynthia M. ,  RAO, Jayanthi ,  HOELLERBAUER, Jakob Nikolaus

    IPC: B64F1/04

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/08 ,  B64C2201/122 ,  B64C2201/208

    Abstract: A drone control method includes commanding a drone launched from a vehicle to execute a predefined schedule of flight commands such that the drone occupies a series of locations within a predefined radius from a buoy, which is also launched from the vehicle, to identify a drone position relative to the buoy associated with a maximum signal strength of the communication signal. The execution of the predefined schedule may be in response to receipt of a communication signal from an emergency responder.

    Abstract translation: 无人机控制方法包括命令从车辆发射的无人驾驶飞机执行预定的飞行命令时间表，使得无人机占用浮标的预定半径内的一系列位置，该浮标也从 该车辆识别与该通信信号的最大信号强度相关联的与该浮标相关的无人机位置。 预定时间表的执行可以是响应于从紧急响应者接收到通信信号。

    TETHERED UNMANNED AERIAL VEHICLE SYSTEM
    303.
    发明申请
    TETHERED UNMANNED AERIAL VEHICLE SYSTEM 审中-公开
    无人驾驶的无人驾驶飞机系统

    公开(公告)号：WO2017117608A1

    公开(公告)日：2017-07-06

    申请号：PCT/US2017/012054

    申请日：2017-01-03

    Applicant: TRIBUNE BROADCASTING COMPANY, LLC

    Inventor： HUNDEMER, Hank, J.

    IPC: B64C39/02 ,  B64F3/02 ,  E01F3/00 ,  B66D1/60 ,  H02G11/02

    CPC classification number: B64C39/022 ,  B64C39/024 ,  B64C2201/148 ,  B64C2201/182 ,  B64C2201/208 ,  B64D2201/00 ,  B64F1/02 ,  B64F3/00 ,  B64F3/02

    Abstract: In one aspect, an example system includes: (i) a base including a bottom surface and a first coupling-point; (ii) a vertically-oriented elongate structure comprising a lower end, an upper end, and an inner channel, wherein the inner channel comprises an upper access-point disposed proximate the upper end, wherein the base is coupled to the elongate structure proximate the lower end; (iii) a deployable cushioning-device coupled to the elongate structure; and (iv) a tether comprising a first portion, a second portion, a third portion, and a fourth portion, wherein the first portion is coupled to the first coupling-point, the second portion is coupled to a second coupling-point of the UAV, the third portion extends through the inner channel, the fourth portion extends from the upper access-point to the second coupling-point, and the fourth portion has a length that is less than a distance between the upper access-point and the bottom surface.

    Abstract translation: 在一个方面，示例系统包括：（i）包括底面和第一耦合点的基底; （ii）包括下端，上端和内部通道的垂直定向的细长结构，其中所述内部通道包括设置在所述上​​端附近的上接入点，其中所述基部接近所述细长结构连接到所述细长结构 低端; （iii）连接到细长结构的可展开的缓冲装置; 和（iv）系链，其包括第一部分，第二部分，第三部分和第四部分，其中所述第一部分连接到所述第一连接点，所述第二部分连接到所述第一连接点的第二连接点 UAV，第三部分延伸穿过内部通道，第四部分从上部接入点延伸到第二联接点，并且第四部分的长度小于上部接入点和底部之间的距离 表面上。

    PIGGYBACKING UNMANNED AERIAL VEHICLE
    304.
    发明申请
    PIGGYBACKING UNMANNED AERIAL VEHICLE 审中-公开
    不可思议的空中客车

    公开(公告)号：WO2016022646A1

    公开(公告)日：2016-02-11

    申请号：PCT/US2015/043754

    申请日：2015-08-05

    Applicant: QUALCOMM INCORPORATED

    Inventor： PRAKASH, Arjun ,  CERIBELLI, Marcelo

    IPC: B64C39/02

    CPC classification number: G08G5/025 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/208 ,  B64D35/02 ,  B64F1/00 ,  G06Q10/083 ,  G08G5/0069

    Abstract: Various embodiments include methods for piggybacking an unmanned aerial vehicle UAV (100) on a vehicle (210), e.g., motor vehicles and trailers coupled to motor vehicles, to reach a destination (B). Various embodiments may include determining whether to dock on a vehicle (210). One or more candidate vehicles (210, 213, 215) may be identified for docking. Travel profile characteristics of the one or more candidate vehicles may be identified. A first vehicle (210) may be selected from the one or more candidate vehicles based on one or more travel profile characteristics that assist the UAV in reaching the UAV destination (B). The UAV may dock with the first vehicle. While docked to the first vehicle (210) the UAV (100) may charge an onboard battery (150) via an electrical connection (415) in a docking structure (410) or by harvesting energy in the wind caused by movement of the vehicle by configuring the UAV rotors (101) to charge the battery.

    Abstract translation: 各种实施例包括用于将无人驾驶飞行器UAV（100）搭载在车辆（210）上的方法，所述车辆（210）例如与机动车辆相连的机动车辆和拖车到达目的地（B）。 各种实施例可以包括确定是否停靠在车辆（210）上。 可以识别一个或多个候选车辆（210,213,215）用于对接。 可以识别一个或多个候选车辆的行驶轮廓特征。 可以基于一个或多个辅助无人机到达UAV目的地（B）的旅行简档特征，从一个或多个候选车辆中选择第一车辆（210）。 无人机可以与第一辆车停靠。 在停靠在第一车辆（210）上的情况下，无人机（100）可以经由对接结构（410）中的电连接（415）对车载电池（150）进行充电，或者通过在车辆的运动引起的风中收集能量 配置无人机转子（101）以对电池充电。

    SYSTEMS AND METHODS FOR UAV DOCKING
    305.
    发明申请
    SYSTEMS AND METHODS FOR UAV DOCKING 审中-公开
    无人机锁定系统与方法

    公开(公告)号：WO2015180180A1

    公开(公告)日：2015-12-03

    申请号：PCT/CN2014/079012

    申请日：2014-05-30

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： WANG, Ming yu

    IPC: G05B19/418

    CPC classification number: B64F1/222 ,  B60L11/1846 ,  B60R9/00 ,  B64C39/024 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/18 ,  B64C2201/208 ,  B64F1/00 ,  B64F1/007 ,  B64F1/22 ,  G05D1/0684

    Abstract: Systems and methods are provided for docking an unmanned aerial vehicle (UAV) with a vehicle. The UAV may be able to distinguish a companion vehicle from other vehicles in the area and vice versa. The UAV may take off and/or land on the vehicle. The UAV may be used to capture images and stream the images live to a display within the vehicle. The vehicle may control the UAV. The UAV may be in communication with the companion vehicle while in flight.

    Abstract translation: 系统和方法用于将无人驾驶飞行器（UAV）与车辆对接。 无人机可能能够区分伴侣车辆与该地区的其他车辆，反之亦然。 无人机可以起飞和/或着陆在车辆上。 无人机可用于捕获图像并将图像流直接传输到车辆内的显示器。 车辆可以控制无人机。 在飞行中，无人机可能与伴侣通信。

    SYSTEM FOR PROVIDING A RAPIDLY ELEVATED AEROSTAT PLATFORM
    307.
    发明申请
    SYSTEM FOR PROVIDING A RAPIDLY ELEVATED AEROSTAT PLATFORM 审中-公开
    提供快速高空作战平台的系统

    公开(公告)号：WO2012099699A1

    公开(公告)日：2012-07-26

    申请号：PCT/US2011/068207

    申请日：2011-12-30

    Applicant: INFORMATION SYSTEMS LABORATORIES, INC.

    Inventor： VAN STAAGEN, Peter, K. ,  MCDANIEL, William, Douglas ,  BOSCHMA, James, H., Jr.

    IPC: B64F3/00

    CPC classification number: B64B1/50 ,  B64B1/58 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/123 ,  B64C2201/201 ,  B64C2201/208 ,  B64F1/14

    Abstract: A system and method for deploying a payload with an aerostat uses a mobile transporter for moving the system to a deployment site. Structurally, the system includes a base unit with a rotation head mounted thereon. An envelope container for holding a deflated aerostat is mounted on the rotation head and a rotation of the container on the rotation head positions the aerostat for optimal compliance with the existing wind condition. Also included in the system is an inflator that is mounted on the base unit to inflate the aerostat with a Helium gas. And, the system includes a tether control unit for maintaining a connection with the aerostat during its deployment, in-flight use, and recovery. Preferably, a deployment computer is used for a coordinated control of the rotation head, inflator and tether.

    Abstract translation: 用空气净化器部署有效载荷的系统和方法使用移动运输装置将系统移动到部署现场。 在结构上，该系统包括其上安装有旋转头的基座单元。 用于保持放气空气净化器的信封容器安装在旋转头上，并且旋转头上的容器的旋转定位了空气调节器，以最佳地符合现有的风况。 还包括在系统中的是充气机，其安装在基座单元上，以用氦气对空气净化器进行充气。 而且，该系统包括一个系绳控制单元，用于在其部署，飞行中使用和恢复期间维持与浮空器的连接。 优选地，部署计算机用于旋转头，充气机和系绳的协调控制。

    UNMANNED VEHICLE
    308.
    发明申请
    UNMANNED VEHICLE 审中-公开
    未经规定的车辆

    公开(公告)号：WO2005123502A3

    公开(公告)日：2007-03-29

    申请号：PCT/US2004041583

    申请日：2004-12-13

    Applicant: ADVANCED CERAMICS RES INC ,  MULLIGAN ANTHONY C ,  TROUDT CHRISTOPHER D ,  DOUGLAS JASON MICHAEL K

    Inventor： MULLIGAN ANTHONY C ,  TROUDT CHRISTOPHER D ,  DOUGLAS JASON MICHAEL K

    IPC: G01S19/48 ,  G05D1/02 ,  B64C15/00 ,  B64C39/02 ,  G01S13/76 ,  G06F17/12

    CPC classification number: G05D1/0094 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/044 ,  B64C2201/104 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/205 ,  B64C2201/208

    Abstract: Methods and apparatuses provide surveillance of a convoy (12). At least one unmanned aerial vehicle (UAV) (10) obtains images around the convoy's position to provide information about potential hostile activity while th UAV follows a generally curvilinear path around the convoy as instructed by one of the convoy vehicles. Path planner algorithm software is executed by the controlling convoy vehicle in which position and velocity information regarding the unmanned aerial vehicle and the convoy are processed to determine values of control variables. The determined values are sent to the unmanned aerial vehicle over a wireless communications channel. The path of the surveillance vehicle may be changed in order to provide evasive measures to avoid an attack on the surveillance vehicle by an adversary.

    Abstract translation: 方法和设备对车队进行监视（12）。 至少一架无人机（UAV）（10）获得围绕车队位置的图像，以提供关于潜在敌对行为的信息，而无人机遵循车队之一的指示，沿着车队周围的大致曲线路径。 路径规划器算法软件由控制车队车辆执行，其中处理关于无人机和车队的位置和速度信息以确定控制变量的值。 所确定的值通过无线通信信道发送到无人驾驶飞行器。 监视车辆的路径可能会改变，以便提供回避措施，以避免对手对监控车辆的攻击。

    MICRO-ROTOCRAFT SURVEILLANCE SYSTEM
    309.
    发明申请
    MICRO-ROTOCRAFT SURVEILLANCE SYSTEM 审中-公开
    MICRO-ROTOCRAFT监控系统

    公开(公告)号：WO03059735A2

    公开(公告)日：2003-07-24

    申请号：PCT/US0241280

    申请日：2002-12-19

    Applicant: ARLTON PAUL E ,  ARLTON DAVID J

    Inventor： ARLTON PAUL E ,  ARLTON DAVID J

    IPC: B64C27/10 ,  B64C39/02 ,  B64C

    CPC classification number: G08B13/19621 ,  B64C27/10 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/201 ,  B64C2201/203 ,  B64C2201/208 ,  G08B13/19619 ,  G08B13/1963

    Abstract: A flying micro-rotorcraft unit is provided for remote tactical and operational missions. The unit includes an elongated body having an upper and a lowe end. The body defines a vertical axis. The unit further includes a navigation module including means for determining a global position of the elongated body during flight of the unit. Rotor means of the unit is coupled to the upper end of the elongated body for generating a thrust force that acts in a direction parallel to the verical axis to lift the elongated body into the air. The rotor means is located between the elongated body and the navigation module.

    Abstract translation: 提供了一个飞行的微型旋翼航空器，用于远程战术和作战任务。 该单元包括具有上端和下端的细长体。 身体定义垂直轴。 该单元还包括导航模块，其包括用于在单元飞行期间确定细长主体的全局位置的装置。 该单元的转子装置联接到细长主体的上端，用于产生一个推力，该推力作用在平行于虚拟轴线的方向上，以将细长主体提升到空气中。 转子装置位于细长主体和导航模块之间。

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